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标题: 维修术语 [打印本页]

作者: 帅哥    时间: 2008-12-29 23:32:04     标题: 维修术语

维修术语

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作者: 帅哥    时间: 2008-12-29 23:40:58

维修术语 . F" u% k5 ^9 R; ]4 B . f2 |, @& z" o) r 0 O7 x6 v3 H, p6 ], X8 P! o, A(灯)不亮 not come on   不可用 not serviceable 2 S0 m$ |5 S! ?$ g$ w4 R& _ m“工”型 type I   不锈钢 stainless steel 0 f% |& y; s: o% LAPU 舱门 APU bay door   部件 part + c+ s0 B+ m$ \) m* s) k6 JT 型件 Tee extrusion   材料 material$ F& i' [4 F' }& j, j% c+ q 阿罗钉 alodine   参考 reference $ _* q8 k, Y+ G' A8 U安全带 safety belt   餐板 feed panel + f ~) P/ q1 @+ h" L, |9 |安装 install   餐车 diner! z. u& g. y7 w4 e) l }) G 安装座 attach fitting   操纵 control+ F$ U4 W1 q. `6 m$ ? 按钮 button   操作检查 operational* ~. f8 f( A: \. H 按需要 as required   槽 spout- d7 J6 c$ a1 N+ L: h. r 凹槽 notch   侧板 sidewall4 R8 J# X! A+ Y, P+ A9 Q 凹坑 dent   测量 measure 3 U3 ] S" h2 U* C# A3 {把手,扶手 handle   测试 test5 V: a# O" b0 ?$ v 包皮 cowl   插钉 pin ' Y# q* n( y5 F# s0 R% M保护层 coating   插头 plug( L+ }3 D0 n. E- D F8 k 保险 fuse   插座 receptacle ( f# v' h# h5 E6 h3 _% y2 N5 G报废 discard   拆下 remove $ I5 s& q# I8 B. h0 u! B报告工程师 report to engineer   长桁 stringer% _3 B9 p1 p5 j& J" } 杯子 cup   超标 out of limit4 D( l9 r8 R+ p 比率转换器 ratio changer   超标 exceed the limit ! @ ?5 @4 T# L6 f6 T, H% j0 k壁橱 closet   超过 exceed- @) x1 N4 S& J 边缘 edge   超控手柄 override handle$ {( v, D/ O0 k7 E 便于检查 easily to inspect   彻底修理 drastically repair % \( ^" \. e! g0 T2 }0 b7 D% ]变形 deformation (n)   陈旧的 worn5 f0 J# [- X% N9 S: j; |5 ^$ p 变形 deform (v)   衬板 liner' ?/ w5 i0 l, _0 R 变压器 transformer   衬套 bush 8 a' Z: i3 }5 x1 H标牌 placard   成型 shaping; |# Y9 e, m" e! J$ p& S; i 标识 sign   乘务员 attendant " l; u9 |3 A. M标志 instruction   尺寸 size: T" J8 l, y$ y. W 玻璃 pane   充足的 sufficient + O4 B# M8 S ^玻璃纤维 fiberglass   冲水按钮 flush button ) A) F6 j% G! d: h$ {) f5 J补片 patch   冲洗 flush7 b0 ~" l* C4 N% H' F2 V7 P 补片 filler   冲压 ram 6 |& J G+ w4 z8 c; d' k" e冲压空气 ram air   低压压气机 LP-compressor 5 D2 `) L2 N: ]3 t抽油 defuel   底部 bottom 0 y5 ~$ V; J- ^1 I: q' D; C# \出口 exit   底盘 base 8 `: }" `; Q$ K! P7 o除腐区 reworked area   底漆 primer9 a0 ~9 s. G3 Y _" \8 r 厨房 galley   底座(结构件) mounting + w! @. O5 }4 N5 G- w* ]厨房烤箱 galley oven   底座(螺母) plate 1 v2 s6 R7 H$ ]/ U: P, t1 p储物柜 closet   底座(天线) base \* D- X3 c6 k- s处理 treatment   地板梁 floor beam: i" n7 c% M% @! v2 p/ P. Y3 `; h 处理 dispose   地面 ground+ U6 K3 X0 f' C9 ]. s; _' j 传感器 sensor   地毯 carpet ; j- j {6 H1 f" \/ `传输 transmission   第二层 two layer3 X! k; I! f2 l/ p 垂直的 vertical   点火电嘴 ignitor 6 s" [4 u' X4 q$ R存放处 location   电路 circuit9 f: B# Y2 Z( `. T6 }+ K 错位 migration   电门,开关 switch5 C% s1 f- N t9 o5 C 搭地线 jumper   电气 electrical / ]2 `8 a+ h2 w( q8 _& O% p$ J搭接处 interface   电气接地 ELEC bonding 1 s; R; ~% [* |搭接片 splice strap   电源通电 power0 Y2 A" q# x3 i9 ?1 `8 N" k/ z 搭接片 splice   电子 avionics % M, Y( C) U9 S3 v0 x& x- V打磨 blend out   电子架 E rack' m8 F7 z2 l: x5 Q 打磨片 blent disk   电子架 shelf& d0 Z3 K7 X- G& Z5 S 打止裂孔 drill stop hole   电阻 elec resistance ; x5 h+ g& j z# e% D大翼 wing   电阻 resistance, o, _1 v- O- z& u( Z X 大于 more than   垫片 washer ' C( f ?/ d0 L4 N9 m$ _% }单向活门 check-valve   吊仓 nacelle $ F: C( F$ i) A& \0 I; g# d7 a4 j弹簧片 spring seal   吊点 mount cone - U' }7 v7 [* \+ }. `挡块 retainer   调节 adjust # @ o& G, {( T' @4 ?$ m挡雨板 fender   调整片 tap ' d- p5 h1 @; f2 |6 A% B导线 wire   顶板 ceiling $ L3 R I1 V. B% R, x- }# L! m灯 light   顶部 top6 r, p' a8 M# c, K9 R 灯泡 bulb   顶部 overhead " W g( }; V! s灯泡 lamp   定中弹簧 decentering spring 5 J. B$ h& k$ k5 N灯箱 light case   丢失 miss; _. R9 w2 @! _ {) t3 h' j9 G 灯罩 light lens   堵盖 plug8 v5 C0 p1 v, H- {" x( ?* q 登机门 ENTRY DOOR   堵塞 clog - t/ i4 i3 m3 v% K7 }4 V8 J! @端头 ending   腐蚀 corrosion( g. x( e- C$ F: Q) Y7 z 段 section   腐蚀 corrode # u1 y% a1 E3 I5 H5 Z& n5 ]断 break   附件(大) accessary @5 s3 {& ?& C( `, R; M 断开 disconnect   附件(小) attach$ A% R, D7 [4 Q 断裂 fracture   附近 adjacent to 0 l) ^! y2 v( I9 F断裂的 broken   复合 complex, O2 H2 [* F+ J; L# }4 i7 r 断丝,磨损 fray   副驾驶员做椅 first offcer's seat7 M0 h1 u6 {" @- L% L: x0 o4 l2 C, c$ F 锻件 forged part   副翼 aileron . |; D' F8 c5 F$ y+ ^- |多处 numerous   改装 modification 9 p& t6 m* Q+ d4 W1 z发动机 engine   盖 cap 9 S0 ^/ _* E- |+ B$ ^3 M翻新 overhaul   杆 rod ! c, f# Z$ d) y& [. p反光镜 mirror   钢丝 steel ! W% I! _0 r6 t$ v: ^方向舵 rudder   钢索 cable8 t! c* a( P+ g 防冰管 anti-ice duck   割除 cut out" W. u- e& Q: J7 ~+ X 防腐 corrosion-inhibition   割断,割下 cut off ) U* B' X3 A" s# h防静电 static-free   隔板 clapboard,partition 8 e' ?# [7 r1 q' h; [8 i9 S! ?防磨条 wear strip   隔框 bulkhead7 D$ Y* z" d# q6 U: C4 O 防滞 antiskid   隔热棉 insulation-blanket 7 J; @6 Q% V8 f" u3 S; G防撞灯 anti-collision light   隔栅 grille " C& b2 u, U1 u; }' T. J, ^放 extend   各有 each has/ X+ F% A& I+ A! t 放电刷 discharger   根据方案 in according to disposition* ^2 K% l/ E7 Z$ K& ]0 u; U) k 分层 delamination   根据监控指令单 condition monitor order… " K# u! L" u+ |4 Z风层,脱胶 delaminate   更换 replace + c* y; j/ F7 z0 l4 w风挡 windshield   工程师 engineer 2 C% Z0 B' o" r2 G8 c) A9 `4 n风挡玻璃 windscreen   功能测试 functional test n/ f* Z1 |# x" X* L 风扇整流罩 FAN COWL   功能检查 functional & ~/ F# U0 N, [6 i+ r风蚀 erode   供应系统 feed system 8 a7 _1 K% ~, n) T& C/ S封严 sealing   供油管 OIL TUBE , o8 J0 D8 H, a9 d" p封严条 seal   鼓轮 drum: @# K3 d) P t. o6 O! W 蜂窝芯 stagger core   鼓起 bulge & n3 G0 V8 Z0 t9 w扶手 armrest   固定 secure: j1 O$ i, l) m3 v, B* P+ [- y 扶手盖板 armrest cover   固化 harden: U0 }& c8 E3 t3 S 辅助滑轨 assistant track   固化剂 hardener ; k+ ^2 }( K* ^9 I8 Q故障 fault   划痕,划伤 scratch , o4 D! j" ~( Q9 b. @3 z刮伤 scratch   划窝 countersink* }9 A2 J: N7 D0 @# u( c4 l7 s4 F/ N# G 挂 attach   环氧树脂 epoxy resin 0 N( L4 @ o+ O0 {; Q6 M! L挂钩 hook   恢复 restore; c# t. M v6 Q; a6 Q; O- r+ @ 挂上 hang up   活动窗 slide window ' S" o6 r! R9 {; z1 C2 E- _4 m9 I7 s关上 close   活门 valve 1 O. b+ w2 p7 } q4 F+ W8 o观察镜 view glass   货舱 cargo compt # \. c/ i* J# z4 m6 N% p7 N观察镜 viewer   机构 mechanism, w0 z# d4 ^! n2 g8 ` 观察员 observer   机身 fuselage ) C2 J m; g w; `/ s0 |观察员 observer   迹象 mark 5 q4 ?# L) f' c+ V) u' v2 P2 h光滑地 smoothly   加强 doubling! \% t8 b' [. j0 o 滚轮 roller   加强件 stiffener % D. E4 \& }1 d. l过道 aisle   加强块 doubler2 a! S3 y2 Q; s% l) ?! B( V 过期 expire   加强肋 intercostal T9 k G3 ~2 C8 B 过热传感元件 overheat sensing element   加强修理 reinforcement, {5 D$ m' L. |2 b- T 海绵 sponge   加温导线 hot wire" |& h' P4 o) s" b. W7 ~ 焊接 weld   加油面板 refuel panel/ a; b1 [6 J- }7 u 焊条 welding rod   加油站面板 fueling station panel: _6 R) d( h% Q \2 v 恒速传动装置 CSD case   夹子 clip" s4 f: A, n- e; N) A2 x 横梁 latitudinal beam   驾驶舱 cockpit3 S" i5 f8 X9 } 横向 lateral   间隙 gap 4 L. G: i; K9 R8 t5 Z后端 rear   减速板 speedbreak : B: V+ W9 L$ ~- i' _8 ~8 Z* v后缘 T/E   减压器 reducer - m5 g; r! k8 }3 d% E5 `厚度 thickness   减震器 shock absorber" {6 I% H: J( b x- `9 [ 呼叫灯 call light   减震支柱 shock strut , f! A! {: b% Y护板 protect strap   检查 inspect3 R- `( F7 R: `6 d7 { 护目镜 goggles   检修门 access door / T# _0 F, f$ v% D: e3 ?! Q护罩 shroud   胶 sealant6 Q+ a5 j8 G' u. n0 L& P 花键 spline   胶带 tape , r& n* A; `1 M5 s4 H滑轨 track   胶垫 mat8 `# g/ J. L q0 H& B 滑轮 pulley   胶垫圈 rubber washer; ~: j% w7 l$ E% U p6 }, f 滑丝 cross thread   胶套 rubber # A! V7 v8 h+ K 滑梯罩 slide cover   胶纸 tape * F f3 b. g6 @( k1 x1 j滑油量 oil lever   角材 angler3 q* k' K, x$ Y% ] 角型件 angle shape   喇叭 megaphone u/ |5 `4 R# M9 t脚登板 pedal   拦网 block* g; V7 i. s. D0 T% n- O 铰链 hinge   牢固性 security ' o: z8 c4 ^- _0 _接地点 ground point   老化 aged/ ^' ^6 c; F) |. w 接耳 lug   老化,退化 deteriorate: t6 V5 R- X7 |( N 接通,提供 supply   雷达罩 radome # {# G/ J" A* Q5 U7 o接头 fitting   肋 rib4 q: N) h- J* x2 @4 D; n5 b 接线管 splice   离合器 clutch( D1 p' `3 S7 l6 q4 B 接线片 terminal lug   立柱 pole : G! {5 {: p% c结构的 structural   例行 routine6 n r! f/ P0 W" X 金属屑 metal particle   连杆 link & m! Y t! ^ y襟翼 flap   连接 attatch - e9 P- S+ o5 j: Y2 ^! D* G; i紧固件 fastener   连接板 attach plate }7 Q2 _0 m1 K# P% U紧急出口 exit   连接口 coupling 8 @& }- x9 Q; \4 k, E: U4 E9 D 进气道 inlet duct   连接销 lockwire4 D5 t+ j1 P- O' N$ x/ a 进气口 inlet port   联锁 interlock9 b3 X9 W; I, R( { 径向驱动轴 radial drive shaft   裂 crack# y( F- v- l, O3 W, t2 q* I 静电,静压 static   另一个 another) o" O/ b+ n; W+ ^ 救生衣 lifevest   龙骨梁 keel beam ) \8 o R- ?8 P9 x9 P& K' c咖啡壶 coffee maker   滤网 filter 2 t! q: E2 i7 v6 I+ C卡箍 clamp   铝箔 foil ; S9 w0 @0 e6 G6 R* ~# `+ [+ H卡环 collar   轮舱 wheel well8 k5 m" n/ C2 E/ \/ [( r) A 开口销 cotter pin   轮子 wheel 3 H: v8 c. g6 f1 a' i7 H靠背 back panel   逻辑 logic) f6 H4 j1 U; G 壳体 case   螺钉 screw % Y N4 y7 }3 }4 U B- j1 R 可用 available   螺钉孔 screw hole2 S" ~1 V! }: v6 t" s4 C% i5 x 客舱 cabin   螺杆 bolt* ^( W" }! ^# ?: Z 空气循环隔栅 air return grille   螺帽 nut / { M2 s( R. l: ]: d口 port   螺套 insert* ]/ a& R& S: ^# F) F& w 块 piece   螺纹压伤 cross threading* E/ I* Y- C- F& G 框架 frame   马桶 toilet 1 F9 i2 Z) ?# |5 G7 E1 Q' e: |垃圾箱 dustbin   慢车 IDLE 6 i3 r4 |, F% T6 [) i拉紧 pull   毛刺 bur3 j' i8 q" e1 |. A; M+ c 毛胚件 rough   破损 damage * R4 B l0 N) i4 A铆钉 rivet   漆层 coating3 ?( _6 A/ k7 M8 z 门槛 sill   其中之一 one of3 j5 M: T. b6 N$ [ 门框 door frame   启动活门 start valve 5 `4 z6 L8 q( Z6 ^! A# [蒙皮 skin   启动机 starter4 M4 C8 n- Y5 Z# R4 b7 |& ~9 I 密度 density   起落架 landing gear f1 ?, i/ x, y( k密度计 densitometer   气瓶 cylinder. x: u! L& [( u 面板 panel   千层片 shim; c! e5 i3 ]4 i; Q& j0 [- i o 面漆 enamel   前厕所 fwd lav 9 E X9 T& O$ q( k- e/ s模糊 blur   前缘 L/E1 r3 V! y( w9 p5 G; C 模糊不清 obscure   腔体 cavity5 a3 e) L* g/ G" D 磨损 wear   墙纸 wallpaper5 \9 n2 Z8 E, `" f5 e: B 目视 visual   切口 cutout! |; V- y3 \) c1 t3 l0 B6 j 内侧 interior board   勤务面板 service panel, i1 f, r0 [, A 内层 inner   轻度 light: ]: a* W+ x2 O6 R3 \ 尼龙搭扣 nylon fastener   轻微 slight8 W+ a% l3 B0 ] 尼龙扣 nylon hook   清洁 clean # Z! H0 {& N! E3 F9 ]/ \8 k拧紧 tighten   清洁剂 cleaner* b6 h: I5 S5 v! U) |6 C" _: { 扭力管 torsional tube   区域 zone7 i/ ~6 e4 ^" l+ j3 Q 扭曲 kink   曲柄 crank ) W5 |) G9 ~$ Q4 d& E3 B排 row   去除深度 remove depth . U& h X* n8 U: x9 K排放 drain   去毛刺 deburr$ C, p$ F1 P% v+ d4 G 排水槽 gutter   缺口 nick) s" h# M. d+ Q$ g; L3 i 排水管 drain tube   群边 skirt edge ' L2 b$ g2 v! ~- l配平 trim   燃油 fuel9 k. {% |" m3 v; T( F1 a" U 喷漆 paint   燃油泵 fuel pump , X5 t B- F+ k, D5 h$ T q# I喷砂 sand blast   扰流板 spoiler. _9 [" |# Y1 e 皮带,片 strap   热水器 water boiler 0 A5 D/ d: ?+ R6 O皮托管 pitot   人工行程限制 manual travel limit R, y2 Z$ d, C8 e0 C6 w6 w偏航阻尼器 yaw damper   日光灯 daylight lamp % M2 P; g3 T3 _8 j& i平衡机构 equalizer   软管,软护套 hose 6 U- H7 P+ A7 \平滑的,使平滑 smooth   润滑剂 lubricant% H0 A3 [7 Q) J) [, j8 K( j 平行 balance   三段 three section& h- o% D& n+ N7 L 散装 bulk   逃离滑梯 escape slide ' h% S+ N& {5 z& `* ~% @刹车 brake   天花板 ceiling4 W6 h2 l" V1 o0 i2 M 上表面 upper surface   天线 antenna 4 j) J0 n4 t8 u8 {上述 above   填补 fill 8 I) W5 y/ B+ O- ^深度 depth   跳开关 breaker; _' l' u- L2 y/ S) n 渗漏 leakage   凸轮 cam, s8 m; I5 f. Y: c9 z3 S2 n 升降舵 elevator   图纸 DWG 5 a4 M, `* Q1 ~, b# F2 N" ^0 G绳 rope   涂,粘贴 apply: e9 ^; k" x7 I! q 失效 inoperative   退漆 strip paint $ Y/ a$ @9 }: y湿安装 wet installed   退色 badly faded6 ]0 Z6 Y3 M7 t; \& f! u' T: p+ } 试车 run up   托板 pallet2 S0 G) K8 q$ I0 j; P8 Z 释压 pressure-release   托板螺帽 plate nut+ w8 l, P( {. l9 Z$ T 收 retract   脱开 disengage * N6 c; k4 b3 v4 v收发机 tranceiver   外 outer ; B; X' U& @5 Z; B手柄 towing lever   外侧 outer board+ Q0 s& R- h* _! ? 手册 manual   完成 complete 7 t4 `7 C3 V$ v D, y/ m手电 torch   完成 finish, G w& ^4 s5 ]5 t* k, K 手工 handwork   万向接头 gimbal- y* P" @% H! \. A- x; c2 x 手提的 portable   维护 maintain & w& g/ i- @' i手提灭火瓶 extinguish bottle   尾部 tail ; O' h' R) z& G o: K 树脂 resin   尾舱 tail compartment- y: _5 t: z( l0 @ 双倍 double   尾喷管 exhaust nozzle - y7 c" {# N8 O, X# @水平安定面 horizontal stabilizer   尾锥 TAIL CONE, A- }" a8 X/ u; Y# j/ r1 \# ~ 撕裂 tear   位置 locate 3 F* N% V4 _0 F' [- B+ F伺服 servo   温度 temp# h4 d2 J+ V8 ~& Y( [: X 松动,松脱 loose   涡杆 jackscrew. Q& f/ Y# _! i1 o3 p" J" K: S 送修 send to repair   涡杆 worm bolt - { o( S1 @- R9 f$ O; b: O塑料 plastic   涡轮 turbine; J2 }3 E7 N8 ]# r 随动盖板 hinge access door   污染物 contamination3 q9 i! [1 y2 A: r1 _7 B; { 锁 lock   污物 dirt v$ N$ u {) l9 J, e$ s锁定 lockout   无线电高度表 radio altimeter + l; i0 p1 x9 i1 E! M锁扣 latch   稀释剂 thinner , ?* l& q ^8 b7 k7 `锁销 lockpin   铣 mill 8 Y% Y' s! s% B0 I7 c系统 system   溢出 spill' S7 b5 s; y4 p2 a! ] 下部 lower   翼尖 tip 7 C& C2 z& {* i$ b1 z下角 LWR corner   翼间 wing tip6 y. l- V4 b; Z4 D; _ 下位锁 downlock   翼梁 spar% C$ z0 @- g" p' | 下陷 concave   引进 introduce ; _, X' _& U/ V1 o+ G4 M下缘条 chord   引孔 make guiding hole P' k" [3 F- F- ?9 O纤维板 fibre board   引孔 drill hole 0 Z( N# R; v5 v8 J- e7 R# r相关的 relative   引气 bleed+ V! b( F! R! W6 U9 | 相磨 chafe   引气管 bleed hose4 ^6 I1 l7 x* ?: a- j7 H: M 消音板 accoustic panel   应急 emergency; v$ _0 v, L. @/ M6 |: ^; y 销子 pin   永久性修理 permanence repair7 K% Y0 J" z* [1 Z0 h, p$ l 楔形块 wedge   用…填补 fill it up with…6 c2 W/ l. l1 `) i# Q/ |8 O6 x 信号灯 annunciator   油封 preservation3 @( S7 Q, d# ?/ m, v% Y& j9 G& t 行李架 luggage-rack   油箱 fuel tank $ F, s3 Z6 [# }! b& p, H1 X行李箱 stowage   游动梁 walk beam# ^0 B: V& {. t/ E% A 修边 reform   雨刮 wiper' Q4 f# _) J2 C, z4 r( ~7 x& q 修理 repair   语音记录器 voice recorder , ]: X6 X# \0 o' f* r锈蚀 rust   预冷器 precooler1 p4 d. z" R% Z 循环 cycle   预位 ARM$ Q* a; J {: Z' Z+ r& x1 T 压紧 gland   原厚度 original thickness, d) Y( d; |+ \* n" ^3 f# v 压力通风系统 plenum system   原来 originally 3 F/ A3 _$ p( B) J4 Z5 \5 s压条 cover   阅读灯 reading light 2 b# c$ R! p1 D严重的 serious   允许损伤 allowable damage 5 @9 N3 s- F- T5 M j阳极化 anodize   杂志袋 literature container 9 E8 v2 P8 \/ S# r8 J8 U氧气 oxygen   载荷调整 preload adjust w! g! i; D t0 F氧气面罩 oxygen mask   再循环 recirculation8 @6 E( y0 W( {1 L 液压 HYD   在位 be in place) c' \/ Y" h- `" F1 S k 液压泵 HYD PUMP   脏 dirty - E J/ I% E6 o% ?9 _9 ?3 ^液压管 HYD duct   增压 pressurization # p3 f' @% M0 Z" V2 h0 _7 j液压系统 hydraulic system   增压泵 boost pump$ R2 Z) g* C. g% C! ^ s7 z 液压油管组件 TUBE ASSY   粘贴 bond7 o+ e, s/ Y' F 液压油箱 hydraulic reservior   照明 illuminate * @0 e/ |; S3 ]- o移到 move to   遮阳板 shade ) x9 T( Z) Y/ L( O# O真空泵 vacuum pump   自动刹车 autobrake . \1 E# S5 E* |' ~3 V, _拯救 salvation   自动油门 auto thrust% \) Q7 B5 E) P# n X$ U5 g: h 整流罩 fairing   自锁螺帽 jam nut x, `/ {2 [# f整流锥 spinner   自由移动 move freely W5 e$ ~' q: T) A整形 rework   总管 manifold [( B+ B. a% h1 S' V 正常 normal   纵梁 longeron % O2 C: m& \+ m正常位置 normal position   纵向 longitudial( Y& D- L0 d/ x E2 d" T 正驾驶员座椅 captain's seat   阻力支柱 drag strut 2 W4 C: X, u) x* n9 J之间 between   组件 assembly,pack + }1 B* V0 w6 b( R支撑架 bracket   组件(电气) unit # L3 g9 O, M8 Y5 q支撑座 support mount   组件(机械) assy 1 {' `) A" b& S, t* ^支架 bracket   最薄 min thickness % |, H5 ]) b; V, K支拄 support   作动筒 actuator / P5 p! J; \4 W+ z止动固定块 stop block   坐垫 cushion . L/ v+ p. _ Y1 s7 f; F. y止动块 atopper   座椅 seat 7 Q8 d# Z& t: f- y) p3 u$ `指点信标 marker beacon antenna   注意 caution $ x$ d: U u; t2 T D4 i2 H* `指示 indication   转接器 adapter! x8 L, A) g+ c" n# ^ 制作 fabricate   转弯灯 runway turnoff light 3 N& @0 x9 I7 t2 o" S3 F1 \8 ?1 ^ p/ _中厕所 mid lav   转向 turn : ~0 ^' U- ]5 o8 G) _9 }! |8 q中间,中央 center   装饰条 trim strip" C9 m* \- H; t+ \( u5 O* v 周围 around   准备 prepare 9 u; X' p1 N0 a. W' |轴 shaft   着陆灯 landing light $ G. q7 o/ e6 r" `轴承 bearing   自动关闭 auto close 5 ~: C8 g% q1 Y/ x- q- F主轮 main wheel   助推机构扳机 power assist trigger! r4 r, F: M' t" i ! E+ Z7 b/ _9 y7 t' f# E2 g , W( A# ?. s# X* Q$ d1 ]6 r u) d( E: S! N3 P: { ! L! c3 P0 A" ~. @) i) j' l) ? 6 E* X8 r2 u7 L9 L l& L b3 \. a T# Y# ?8 t8 L. O# s2 r1 n( ? # D- k" x9 O4 h# ~ & o$ w/ E$ P3 |: z$ O3 P! o& ~9 o8 S + `) P% B4 L! n& [& ?( } " k5 q! r, y! U3 a8 X# \% O# V - ]* m3 K' r$ C x# I; I* a/ s! m0 t7 W) h3 t, T+ @" p / A1 N8 i! o9 V5 m; M) {$ C 8 t( g) j; r3 [8 z7 D& ?8 T M ! \' ]; M/ K; \( s+ x9 u8 V \% R3 r: e4 |4 Y( Q+ \2 o 7 q+ B: b2 N4 `2 a2 C) s* J. J! X. S) Y8 A2 H- v4 q" X7 D ( t2 U* }0 o8 }, V: J7 p6 O/ w7 q1 n6 F* P6 @% Z; D* ^ i / x* p% N. Z$ a3 v. K% _ ) K- ~+ F3 ?% |# I 5 m6 S, e) y. T* t+ ], \ E3 ^0 a/ J- B5 I# s |1 B+ B1 M* a$ { " D2 V. X2 E5 Q" R* x( b ' b- ~/ x' @9 |1 z " r" w% O- t! ^, s- \0 O4 u % Q# r, c/ I+ \2 `* h) a1 Y1 b" ?' x: B " }) E6 G$ L+ r% [: {$ @ & b1 H; C2 f# x/ p+ W1 r+ L/ F Categories of Defect : V1 {: n7 d% T, f Categories of defect depends on experience of maintenance practice .In this manual, the default ' j# N" h) } t% l Method used to categorize the defect found on the aircraft into four areas. Structure defect , Material defect, Common parts and Components defect and General defect. ! [6 o- U0 d; [3 t* y- @ 缺陷分类 3 l9 r0 P% q) f 缺陷的分类一般依照维修实践中的经验来分。在本手册中,我们将缺陷分为四类:结构缺陷、材料缺陷、零部件缺陷和一般性缺陷。 # e' y; [, n& r/ y * c) q& S2 L0 `" N5 B1. Common Structure Defects Terms/ X; j/ m- v2 q4 `/ I* s) _- I' | 结构缺陷术语2 E% T; [/ G5 x, n" U z& ^ 9 o9 |+ A/ e$ o% L凹坑(1) dent " e4 I1 A: O. v Y5 r# f1 S凹槽(2) notch8 t2 d5 u5 k& b$ P i/ ] 变形(3) deform s' D, N6 E g划痕(4) nick 3 ]! ]7 H" Z6 b. l8 F点腐蚀(5) pitting! N6 M: B4 s5 h% J- ` 断裂(6) broken 1 J' l% I$ o" Z腐蚀(7) corrode6 g. H3 [' n5 u: h3 H, C+ P G. H 划伤(8) scratch 2 G: f5 ]0 J# W) N2 M( K$ U裂纹(9) crack 6 b q3 p. u3 ?* y2 ]& s毛刺(10) butt" P6 Y! n* t& a J& M 磨损(11) chafe9 z C2 D5 g% ?) b$ T3 g 凸起(12) protrude ! e0 L0 l8 ^; e/ y7 E/ i凹陷(13) sag3 ^; e, L- b: I9 H1 q! i 粗糙(14) rough % q" {- O2 S" c! u漆层剥落(15) finish missing 4 R& C0 D2 H5 ~# W褪色(16) fade! f; x9 A# [1 v+ `; g' {; g+ a1 ? 积水(17) entrapped water, n3 K/ `% [8 g 3 l6 j& H; V1 n" u+ b2. Common material defect terms8 U# d D9 ~; { y) J" ?$ Q6 [ 材料缺陷术语 $ F- m% Y% ^7 B2 I% M Material is divided in two categories: metallic and non-metallic. 8 t9 ~* l/ q. F0 @/ a 材料分为两类:金属材料及非金属材料 2 ^7 d$ l2 w# N6 n4 m9 s 9 U* b" f7 K5 _+ E/ } 1)Common metallic defect: & E; p: d& Q1 }+ {+ i2 f 一般性金属材料缺陷:' o8 l' X6 R. e4 s , K" ?) P* s4 `& F" N9 [. q 氧化(18) oxidize ' S6 l: y6 a4 p 划伤(8) scratch & E P. {7 r/ l1 ~! K 扭曲(19) distort& x! g) w0 e, g# @/ \, z& K# U5 z7 Z 跷起(20) not in contour + c# e3 a) @3 ^4 _! a7 s8 W 穿孔(21) puncture& ?6 f/ W: o1 ]- P( M3 x( y 碎屑(22) chip & g- L! a# D/ l/ l4 F& H+ R3 E0 Q 腐蚀(7) corrode# ~& U# d( u. [, n% t 磨损(11) chafe , r% E( x& u' r( l* x+ V1 O变形(3) deform 5 m8 F4 s; e* P9 L' M! \! ]风蚀/风化(23) erode; z5 a& M. h% ]& t; q 裂纹(9) crack' S) s" o1 d3 H. M" h 2) Common non-metallic defect:9 j$ u: t5 V- g5 ^$ I 一般性非金属材料缺陷:# R0 h3 ?5 G4 x ( D, }7 j8 R7 C9 |4 h. G& c 发霉(24) mildew ; \- U# x% K9 y5 r& v" |* M( U 分层(25) delaminate6 ~ ]: t- ]' U. _7 f 风蚀/风化(23) erode U) N; l2 I" ^' b裂纹(9) crack# i6 Y+ ^# B4 I1 m* B0 X 老化(26) deteriorate% E, m& j8 d, v9 }; f$ A 起皱(27) wrinkle; T# i4 A" i: K( I6 H 受潮(28) saturated3 R# e: K2 B6 f7 f6 s1 K) t: | 撕裂(29) tear2 a' k8 Q( y1 Q; n 穿孔(21) puncture6 \: ?5 R) [# V2 R 变色(16) fade # u: n) _5 ~: R7 Q陈旧(30) worn$ _6 a/ J$ S% q 脱胶(31) adhere1 y& N* E, X$ O ; y2 A8 }$ J0 u6 z1 [4 ?* Y3 l) u$ ~ 3. Common part component defect terms" V2 K' A* P4 W4 J) K 设备及零部件缺陷术语 * {0 ]' H' r0 d7 ~& I5 x) }$ JCommon part and component including : Plumbing, Wiring, Mechanical linkage, Fastener and Miscellaneous.: E7 u; g6 I9 a2 R. L1 i 设备及零部件分为:管路、线路、传动机构、紧固件及其他。 ; {7 V& |$ e& z% {! f, g , T4 c6 j# d" D# X5 Q9 A 1) Plumbing defect 管路缺陷 6 k. [3 m( I6 e3 Y; t . p& x! g& O2 S# V7 X' O: O凹坑(1) dent 9 G' v4 k" l( A8 P: j: n 爆裂(32) burst. }0 B( ^& z2 c; d! n$ y) P, s 擦伤(11) chafe3 \ {* Z3 p: A9 r h 滑丝(33) cross thread 3 j& ]" D& ?; W2 `9 K& v) {扭曲(34) twist5 ]2 _ [/ v0 \: d& a 渗漏(35) leak6 Q* f) P# ^! p; O" x 堵塞(36) obstruct 3 e/ e( V3 R: C5 A. r . S6 J8 c9 c. M0 J, `) J( n4 S: _: V 2) Wiring defect 线路缺陷0 @' g$ `5 g6 L) I) x* P + [5 e% _* I# ~" O3 P% w腐蚀(7) corrode ; k8 E; f6 x) l$ [+ V" ~ 磨损(11) chafe 2 U# I. O9 @' N相碰(37) contact 3 t5 S: Y+ V* p0 m" b, D/ W* I# B断丝(38) fray 7 d( ^( B( g2 B' ^% ~6 L熔断(39) fused ) u# }9 b; w, b8 p9 |$ g弯曲(40) bend% Y7 G' C8 P7 j4 ]9 b) z& S0 Y( t ( B' [/ E7 }- V 3) Mechanical linkage defect 传动机构缺陷9 R1 q6 D/ g/ k7 I$ t, { . _# V/ |# x/ s) Y 断丝(38) fray - @, b" _9 X. [4 u松弛( ) slack6 a- g! J7 ?; ]1 d" | 扭结(34) twist ' @# G, W; Q( x8 u$ O磨损(11) chafe . Z. b3 S9 _2 d8 u6 V' i9 B, _脱开(41) disconnect. p9 w+ J1 n/ j5 H6 V4 n " X8 S# i# U, w J% N 4) Fastener defect 紧固件缺陷( T: n* n- l2 S# _4 I8 G , t7 F; b0 x/ J/ S 丢失(42) missing ; X8 |% N4 L1 ?! j/ W( N; w 松动/松脱(43) loose / @5 m; E. ?% W+ g, q! p 腐蚀(7) corrode7 ?; ?) S( }8 a, X i 磨损(11) chafe * L; W6 z% a. p, V- W 未关(扣)紧(44) not secure " A: ~4 h+ v, n: a ! ~% [7 b5 c) n& y5) Miscellaneous category consist of many parts and components ,five kinds of these parts have been selected. They are Sealant, Wheel Assembly, Life Limited Parts, Placard and Marking, Slide/life Vest. " G0 J+ h1 c2 y& q! }+ C2 U" s 其他类包含很多种其他的部件或零件,在此我们选择了其中五种,它们是:封严、轮胎、时寿件、标牌/标识、滑梯/救生衣。/ N4 ~, H; J' Y4 y: }0 Y! T1 C , Z- W: D# A5 f& u0 p a). Sealant 封严; D0 Y$ g2 q3 T % {% R! ^% @0 v9 s; X8 m% Y 脱胶(31) adhere* z+ \# C2 J/ H, V$ \' ?( \ 老化(26) deteriorate9 u# n( S! s% I) k2 K- l 不均匀(45) inconsistent2 ^' w/ A2 K' q* ~% {4 Q ' n: |7 C" _* |" ] b). Wheel Assembly 轮胎( e4 N o5 o5 A% F4 L 见线(46) exposed cords- I$ N+ W) f8 e, w3 g% d6 t4 }, e 磨平(47) bald . C+ w8 d, n, ^# J0 B! ? 扎伤(21) puncture1 U- y2 S/ }0 o, c 气压不足(48) insufficient-air-pressure: k: N! A- m+ U$ O N - b. B7 s$ I( t c). Life Limited Parts 时寿件 ' Q. J L, n9 C* Z ( [0 Q) ~5 a, P6 h4 P' f. _ 过期(49) expire6 R' U1 p4 v( [- M- V& M- l: V% U ) F" ]1 T2 o: ~% v d). Placard and Marking 标牌/标识+ Y9 \. c9 B. a1 E( M - r. s" r8 E8 z0 r1 o 模糊(50) illegible% Z/ [& W9 L* W) n+ i2 g1 Y- v2 E 缺损(51) damage 5 {7 j8 d' L0 Y6 F 丢失(42) missing / i# M# q4 Y* ]: M$ D翘起(52) lifting : o, e. C' G; Z9 j" g1 n, n 0 X- ~" V% \8 c$ f" S' z$ |" Z/ i9 o3 E e). Slide/life Vest 滑梯/救生衣 " l; N6 Y4 w4 s1 B/ j 6 O5 |/ w! g3 j 散包(53) not properly packed0 F# z* ~# ?3 P( O 变形(54) not properly sealed 2 r( i7 j$ e, H1 L' ~! @; w& c % V* t2 W+ z: P4 d. z$ W# B4.general defect terms 一般性缺陷术语, B" T0 J8 i" Y ) A/ @2 V+ ~$ ]/ G0 X! [6 [ 脏(55) dirty t1 z* T2 m8 m# _8 S2 y, F" Y 陈旧(30) worn. s# ~1 u1 `( r 断裂(56) fracture; I& u; R$ \3 y. [( K 磨损(11) chafe ' R6 _9 S6 p0 I: r( M1 k 超标(57) exceed-the-limit1 J9 l9 u4 Z9 l 丢失(42) missing + n$ g! a; V+ g; _ 腐蚀(7) corrode- t. S$ |( Q' }' Q' q. u 裂纹(9) crack- N# p3 ]( b2 \0 Z, Z& }% \2 i 空行程/无效行程(58) backlash. C# \8 s4 B5 L; } 卡阻/阻塞(59) block " [2 L0 P% i: V# n1 } 鼓起(60) bulge / Q/ E+ ~4 I2 v& A 污染(61) contaminate 8 z `4 P$ t! W, N 不一致(62) disagree / `, P/ s) `2 u; D, S0 h* ` (电池/气瓶)被释放(63) discharge6 d5 `# q' g3 Z3 N; K 装错(64) dislocate 5 p7 W: |0 A$ @4 E/ T 失效(65) fail# ^" N! [4 ]; U9 n. B C+ ^4 S 摆动(66) fluctuate ! r* S/ F% a, \* q# { 抖动(67) flutter + i1 W9 H. M& d; G, p# p5 i 不够/不足(68) insufficient : L& W) S" l# l Z) c$ o& R 不工作(69) inoperative* v/ [ R2 j$ j (不)亮(70) (not) illuminate . v0 p0 p% d9 U& S0 } 干扰(71) interfere, I0 r) z, D, ]( Y, F 扭结/缠结(72) kink3 O3 \ q2 P! D7 x9 \' V 走向错误(73) misrouted 1 p3 d( {& X6 H- {; `; @ 漏装(74) not installed! E' s. z6 H8 f! ^& q6 W 相磨(75) rubbing . i+ A. g k4 c# s0 I2 s1 ^ 干涩/缺乏润滑(76) un-lubricated ; z, N0 g$ `; |2 g# L/ j8 {0 b 不能复位(77) will-not-reset + Y/ G4 l/ B& P 4 i) h0 S/ z# b, x4 l- d* } (1) dent: 凹坑 ( Q. j+ d# F# I! f1 vA depression in a surface caused by pressure or impact. $ n6 [2 r2 e: r2 A受压力或冲击造成表面的下陷。 : j" y: C: f* G" d) K N For example: Left horizontal stabilizer outboard leading edge at WL 368.25 dented approximately 2 inches in diameter.(Area marked in red) 2 g4 {# n/ n, W2 Z" H 左水平安定面外侧前缘水平站位368.25处有直径为2英寸的凹坑(已用红笔标出)。/ X4 E( i- B4 w. N; F& n# u Removed left horizontal stabilizer leading edge. Reformed dent back to its original contour with reference to SRM---NDT inspection revealed crack.. Carried out permanent repair in accordance with SRM--- ! y1 g3 S: b X6 z" @, e: T 拆下左水平安定面前缘,根据SRM—对其进行整形,NDT检查发现损伤处有裂纹,按照SRM—完成永久性修复。 ) R: K" z: t1 g+ i0 ` {" H6 H 4 p+ z5 _ y1 O- c (2) notch: 凹槽 4 T3 E; d6 O1 q% W" P- l A “V” shaped cut or protrusion+ X) i5 L2 J% X, w. ^9 {2 y# q! w V字形的切口或者突起6 R/ [5 o1 k: w9 C5 S! _* z For example: Forward L1 entry door number 1 floor panel has a 1-inch notch 6 inches from the forward right edge. , b# w0 ~' K1 |- Y- X左1号登机门过道一号地板离右前边缘6英寸处有一条1英寸深的凹: R; x! z6 A8 `: j$ e* E+ N( j 槽。 9 C# X7 a" P" y7 P0 t7 }, {Detailed inspection carried out with reference to SRM---no delamination noted. Carried out permanent repair by filling damaged area with potting compound BMS-287 with reference to SRM---.& r$ @+ `: {! y$ ]) ? 根据SRM—详细检查该区域,没有发现其它缺陷,根据SRM—进行永久性修理,对损伤部位填充BMS-287填充剂。- B2 c7 ]( ~& q6 U : o, i4 x/ @1 b6 s (3) deform: 变形 ! F8 d+ \) _1 pTo misshape the original form3 ] d: J, t& k6 J2 z. `% F: k1 N 原有的形状发生变化" |& G8 F, ^ |) o For example: Left wing number 2-fuel access door is deformed.0 \( O8 L0 s/ `7 s$ e# s 左大翼二号油箱盖板变形。7 V$ \# P7 u0 M" V Replaced number 2 deformed access door in accordance with AMM--- Carried out fuel leak check in accordance with AMM--- with no defects noted. S7 F8 t( z" C9 O 根据AMM—更换左大翼二号油箱盖板,按照AMM—的要求进行渗漏测试,检查正常。/ H" _9 F( _3 l) T" U% h* K# I 2 B( l) K' @4 g# G5 h (4) nick: 划痕, o1 q5 }! C( f3 O% l' w& s A shallow notch, cut, or indentation on a surface. 3 p7 n7 b/ i* q: \- _. G' |/ S) n 表面上的较浅的刻槽、刻痕或缺口。 & f1 x. h6 b8 d# J* x For example: Right environmental control system (ECS) access door, after right corner has 4 nicks on external surface . Area marked in red., Z l: g5 h" Z% M. C 右空调舱门右后角表面有四条刻痕(已用红笔标出)。. p, K6 `* O" R7 @ 3 r0 Z9 F" E& h$ u$ o- R Detailed inspection carried out with reference to SRM---no delamination # ^7 g2 l4 Y. l( m6 [5 znoted. Carried out permanent repair by filling nicks with fiberglass and epoxy 7 Z$ M5 A( z W9 Hresin BMS-387 with reference to SRM---., y( V$ |3 i" N. s& z$ g/ @9 V 根据SRM—详细检查该区域,没有发现分层。按照SRM—进行永久性修1 T& p& }" n; Q2 k4 X 理,使用玻璃纤维及环氧树脂BMS-387填平刻痕。' [* }0 r, g" b R" p: Q. V , x9 q( `( a) h(5) pitting: 点腐蚀/砂眼# y. ^0 f& L( k Small cavities, depressions or scars on a surface.4 X+ C% P) Y" Z6 N( E" [0 s U 表面上的较小的空穴,凹陷或凹痕。" Z, O/ k! x6 N7 t For example: Left main landing gear number 1 brake aluminum hydraulic line has pitting. ; T2 {* ~& @8 ?& S ^# `% s 左起落架一号刹车铝液压管发现点腐蚀。 8 t. ~* j# G3 U1 F$ e+ Y- ]$ L Replaced left main landing gear number 1 brake aluminum hydraulic line with0 }( V; V0 O* U8 [% @$ T3 v* x$ } serviceable hydraulic line in accordance with AMM---, w3 N( f$ N$ l 根据AMM—更换左起落架一号刹车铝液压管。! a' S3 U# r% F1 P: l( M: s# G& y2 C 1 R; H/ u# `/ g2 \* ~+ _! t/ ^7 i4 R (6) broken: 断裂$ r5 _ a& F# x* [ Forcibly separated into two or more pieces. 1 q a' l5 F8 m5 Y$ t" X 被分成两半或更多块" ^0 U' P4 ?. A# |7 u For example: Flight deck entrance door has broken door latch and will not lock. - E6 z8 W+ t9 h7 t# m3 \ 驾驶舱门锁销断裂,锁不上。 : ~% ^, `. W1 F1 P G, A# Z Replaced broken door latch on flight deck entrance door in accordance with AMM--- Operational and functional check good., V4 T9 T1 ~: f: c- v 根据AMM—更换驾驶舱门锁销,操作检查正常。 - P* a. B/ o. |9 K( Q3 c. E( @2 n 8 {- M5 _% [1 Q( V9 I(7) corrode: 腐蚀 1 h" Y3 S: }: J4 B# P, x To dissolve or wear away gradually by chemical action.. C3 _3 s" B3 z$ h 氧化或化学污染造成金属表面逐见破坏的化学反应。8 t4 _8 U. v# g9 L$ |) v1 n For example: Floor beam at body station 360 and wbl 25.1 has moderate corrosion 2 inches in length and 1 inch in diameter. % a; O& O5 m+ C! { 机身战位360和机身水平站位25.1处的地板梁有中度腐蚀(长2英寸,直径一英寸)。 3 U1 l- o' Z% U7 I. B Removed corroded area by grinding and polishing in accordance with SRM---. NDT revealed remaining thickness out of limit. Carried out permanent floor beam repair in accordance with attached Boeing TELEX 530092-23 and attached Gameco engineering order 53-099-84. ) Z/ z8 E1 l2 g$ K 根据结构修理手册—打磨去除腐蚀。NDT检查发现该地板梁厚度超标。! K8 |% H3 \6 W$ ?& j' @ 根据波音电传530092-23及GAMECO 工程指令53-098-84,对该地板梁进行永久性修复。; v+ K* G) X- k) w2 e2 ^+ u6 @: C / N2 q+ J( x, b, o& x- B1 T (8) scratch: 划伤: C% P9 T9 ]4 a7 X% u( M; g A thin shallow cut or mark on a surface3 |2 H, }( k1 y) o# _ 表面的薄而浅的切口或痕迹。/ z- I ?& V0 p& ]2 t; O7 [$ V For example: Left cabin external windows numbered 12, 16, 17, 21 and 27 are scratched (obstructing view) " h! j* i1 C6 x6 O q 左客舱外部12#、16 #、17#、21#、27#窗户被划伤(阻碍视线)。 ' K2 [5 [0 T3 C' x# i* S: p7 Y Replaced left cabin external windows with serviceable windows in positions 12, 16, 17, 21 and 27 in accordance with AMM--- Pressurized aircraft and leak check is OK. + S6 O8 z! X! U [, h! n6 U+ ] 根据AMM—更换左客舱外部12#、16 #、17#、21#、27#窗户玻璃,增压检查正常,无渗露。! L; g0 P8 r5 m 3 B7 M1 H" j; ~$ [(9) crack: 裂纹/龟裂 9 K. j8 _/ A3 Q# }. G$ g To break apart without dividing into two parts.- o! S/ {# p8 c1 ^ 裂开但没有分成两部分的破裂。 ; p% q$ X9 k3 f |, T0 r For example: Number 2 engine fuel control cable located at Body Station 360 and Water / i3 s( p. D( m+ OBody Line 25.7 has cracked turnbuckle.9 y8 n, O" d: T1 X# V 位于机身战位360和机身水平站位25.7的二号发动机燃油控制钢索松紧螺套有裂纹。9 J* |2 f: H% P' R; J- z" [ e Replaced cracked turnbuckle with new turnbuckle in accordance with5 n' T7 j# v3 { AMM--- Travel and functional check carried out in accordance with AMM---, 0 [4 r3 u/ a8 o# E/ s5 C- Eno defects noted.* _1 @ _ ~1 u1 d) l 根据AMM—更换有裂纹的松紧螺套。按照AMM的要求进行行程及功能测试,检查正常。" ^9 M! T$ ]' R$ G 6 o# s. ?. z- v0 n) H (10) burr: 毛刺& y/ D, W0 i( | {! P" T% I% R4 e A rough edge remaining on metal or other material after it has been cut or drilled # h& m& \% v$ b. f1 r- g) Y, D被切割或钻孔后留在金属或其他材料上的粗糙的边缘. : c5 e5 y6 w1 f( P- |4 F) x, ?For example: External fuselage repair at body station 727 and stringer 9R~11R has burrs at 3 P4 L8 I+ ~) G5 x* N& I" Mall drill holes. 4 r' k/ N2 Q; k9 N( l8 X& C% E# S# g 位于机身站位727和长桁9R~11R的外部机身修理的所有钻孔边缘有毛刺。 ' C% `) E1 i5 ^. ^1 T$ z' _& w Removed burrs with rotary file in accordance with standard practices and6 T/ m. C, c* O/ h/ G1 B5 t3 u* K SRM---. % R- @& s4 l( ~4 A, q 根据标准施工手册及结构修理手册—的要求打磨去除毛刺。 2 |' p2 m7 [, ] l0 R . J4 S3 [# s/ h9 W# Y! _ (11) chafe: 擦伤 ( S3 L# p3 l; l/ jTo wear away by rubbing. 3 ^ s4 j5 q6 e( f' I因为摩擦而损坏。7 V: W/ S3 D& ?% C For example: Forward cargo compartment after corner threshold chafed by cargo door. / Y. N: P: w7 ~8 ]5 Q 前货舱门槛的后下角因与货舱门相磨导致擦伤。7 [7 o' L1 g% d% a Forward cargo door upper support bracket worn. Replaced support bracket in , _4 j" H; m' s- ~' y! M6 `! qaccordance with AMM---eliminated chafing.! `; c b2 s+ D" I 检查发现前货舱门上支架磨损,根据AMM—更换该支架。; {! [+ \0 p0 Z; G . u& k/ N' r! k4 m1 T1 h0 _8 N (12) protrude: 凸起/突出 - f# C. `) X, R6 Q- \$ Y/ T" [( K lTo push outward.1 l/ Q, P- ?$ e1 l 向外伸出。( b; U3 G8 U; J. R3 x2 ?/ j) r/ ? For example: Forward external fuselage servicing doorstop is protruding through access 3 _) S+ K/ C9 Y% K1 n! m$ q# P# ldoor.( N5 w1 m+ d J2 t9 g/ m- c4 E 前外机身勤务门止动点凸起。 : H, f+ M2 o& [6 s3 @ G Repaired forward external fuselage servicing access door to original contour with reference to SRM---. Adjusted doorstop to eliminate protrusion in accordance with AMM---.9 l* w6 {1 r1 e( @ L/ l 根据SRM—修理前外机身勤务门,按照AMM—的要求调节该门的止动点。 & n9 V( Z$ w/ O( l9 ^3 ?! K 0 p' O: w7 t1 T: s' X/ R(13) sag: 凹陷 ( `' [+ u( Q5 Y# |3 I6 y; dTo sink, droop, or settle from pressure or weight. * V- ^7 m8 F9 I5 j% C因压力或重力而下沉,下垂或下陷。) `" S4 R, u; ?2 r5 _4 n- K/ ? For example: After cargo compartment overhead ceiling panels are sagging. ( g, i+ F) w9 d, }) T9 W 后货舱天花板凹陷。' x. k: B7 H, |( h5 F Detailed inspection revealed ceiling panel screw holes worn. Replaced - J' D7 R# n" }9 x/ d$ V' t8 ~unserviceable sagging ceiling panels with new as referenced in AMM---. : e, B7 @, _; k5 |5 Y详细检查发现后货舱天花板安装螺钉孔磨损。根据AMM—更换该天花 1 z- N% i1 h0 n# L3 M+ Q' g b板。7 w1 v1 \% ~+ ]- j: u( Z 4 S$ L0 g- r; ^' N8 l(14) rough: 粗糙 3 D* Y0 b- |' ]7 s: L9 ^4 {" YHaving a bumpy, uneven surface. . c4 ?1 H8 j5 E& | S6 r' C$ Y表面不平坦,有起伏。, L. ^3 A" I. w0 K) o4 g7 T For example: The protective finish is rough at the number 1 engine inboard pylon. 9 A2 I" \$ ]# O/ L: X 一号发动机吊架内部的保护层粗糙。 8 A7 `9 v6 b8 I' S( n3 {% O; l Removed rough protective finish at the number 1 engine inboard pylon in) T6 @. P# I" I# K2 ` accordance with SRM---. Applied 2 coats of enamel to restore protective . w( J6 w" u/ z! Q1 N7 U0 ~finish with reference to SRM---.3 N/ |3 V8 K( ?2 D! e( B% L# M 根据SRM—拆下一号发动机吊架内部的保护层,按照SRM—的要求涂两层瓷釉以恢复该保护层。 " j1 C( l, U8 ?6 o8 K 7 b9 e; j' F7 K t3 h; X+ o2 n2 M (15) finish (missing): 漆层(剥落) h$ o4 b$ Z% @0 w$ m# m) NTo protective material used in surfacing and finishing flake off.5 E; G# ?$ O, I1 @% G. ~' B 用于保护表面材料的涂层或保护层 因失去黏附力而剥落,脱落。( J, u9 r) D. n) x For example: Fuselage skin protective finish at pilots and copilots number 1 and number 2% U \: F! Y F( Y$ Q, S' r6 [ windows missing. & L2 Z4 y& A5 M正副驾驶1号和2号窗上的机身蒙皮保护漆层剥落。( H, x& R% x; F Prepared affected area of fuselage skin at pilots and copilots number 1 and ) k; q! S* \5 j! B) m6 x& Tnumber 2 windows. Anodized affected area in accordance with SRM---. Applied primer BMS 25-89 in accordance with SRM---. Applied 2 coats of enamel paint in accordance with SRM---. Protective finish restored." h6 M8 y/ |- {3 |1 C* W; i 根据SRM—对正副驾驶1号和2号窗上的机身蒙皮涂阿罗丁;根据SRM—刷涂底漆BMS25-89;根据SRM—涂两层面漆,以恢复保护漆层。 : q3 J( g) K, `, T" t- ]+ c " P" \$ x/ y' W+ D# ^# c6 p4 I(16) fade: 褪色/变色 / J' ]+ p' c; x& l% l" Y) [1 uTo lose original brightness or color., p& U8 H5 w J# j 失去原有的光泽或颜色。 / {7 a% ]; X/ U1 N" iFor example: Number 1 and number 2 engine intake cowling chrome is faded. 9 B1 ?6 b; b1 p1 m `+ O 1 号和2号发动机进气道的铬层褪色。; K; x8 X! d1 y* Y: ` Polished number 1 and number 2 engine intake cowling chrome with reference6 @; o [0 |6 l: o, n g, K* R+ { to SRM---.1 D+ X+ c. t$ `" ] 根据结构修理手册,对1号和2号发动机进气道铬层进行抛光。 0 R: x: G* B6 r1 B5 {: S ; |4 c2 ^) j( O; p9 x(17) entrapped (water): 积/含(水) . P+ j6 U2 M$ u. D. jTo collect in an area.! g6 t) Y' Y$ J& d 水或水汽在某区域内聚集。 9 l8 T9 {7 d1 {5 L, |6 R% L0 ^For example: After cargo compartment forward bilge area at body station 840 has entrapped' H/ w' y) f* f ^ potable water. ; n2 Z9 _0 H ]9 z: M1 V$ H8 d后货舱在机身战位840处的前部区域有积水。4 c0 t) ?; b. M8 H' O Detailed inspection found pressure drain valve clogged. Removed,cleaned and reinstalled pressure drain valve in accordance with AMM--- Removed residual entrapped potable water.' }2 G$ k) D6 R3 ` 详细检查发现该处排水活门堵塞。根据AMM—拆下并清洁该排水活门后重装,并清洁该处的积水。' j; C6 r" t" E8 ~5 ~' r0 c, y $ X0 r. H0 m3 C$ L% H (18) oxidize: 氧化: k/ K- I# Z2 x* N The containing of oxygen usually caused by natural elements. - o& I0 b7 q$ x物质的原子失去电子的化学反应,也就是物质和氧化合的过程,如金属的生锈等等。5 a9 u. y7 g. U' | For example: E-3 rack lower after corner is heavily oxidized. 0 W8 N. }' S9 q0 _% f+ { E-3架后下角氧化严重。 ; [9 t8 c ~0 o2 S5 C2 X# N Removed oxidation at the corner of E-3 rack in accordance with SRM---. 5 [4 e. W$ `6 N% t0 w 根据SRM—去除E-3架后下角的氧化。 ! S4 U* @" M) |& z / [/ p; I2 g3 e' @% f (19) distort: 扭曲 : T0 _9 V7 P! C9 R* N5 S$ ~2 `: Z! G' wTo twist out of a proper or natural state.! f+ ^- A2 q$ O3 j) W 因受到扭力而导致原有的形状发生改变。" F) [8 i. E$ D For example: Access panel 2145J to left wing number 3 slat actuator distorted. & v4 K, |* H! f& |* x9 h1 G. X 左大翼3号缝翼作动筒的接近面板2145J扭曲。5 @- H) W' i4 H3 k, o, C' e2 k' y# R Replaced access panel 21458 with new panel in accordance with standard5 B6 ^' L3 w* V# L8 S practices and AMM---. Original panel declared scrap, tagged panel as much3 Z+ _# p/ q: i9 q! t( w( t and routed to MSC to return to customer. / [' E( c, g. i- p! d, h# c根据标准施工手册及AMM—更换21458盖板。旧件挂牌送航材处理。 2 p! _8 |- y7 Y' ]0 q ( d3 y, Z! E; `- D(20) (not in) contour: 外形/轮廓翘起3 ]4 i' f0 @, \! a) e+ W3 p A shape or outline is deformed.- ]& j. Q e' O) Z6 { 形状或外形轮廓变形。 . [* e" L& \3 Q5 oFor example: After lower corner of after fuselage external servicing door is not in contour 1 L6 [& Z) D* A% a" W4 ?7 Gwith the fuselage.) h' c9 s1 c' |' r, G2 } 后机身外勤务门后下角翘起。 3 L. N" ?3 Y' t( T2 P' UAdjusted after fuselage external servicing door to contour of fuselage in t; v4 d" o [; B) ]& R% g5 Y3 | accordance with AMM---. h- @2 T) T0 t 根据AMM—调节后机身外勤务门正常。 7 s$ N: N5 J) X6 h( N' }; k8 R # g# C8 M$ ^' h( e4 ?5 U+ j. f; m E (21) puncture: 穿孔/扎伤 / D" ]! Y/ d/ ^& R# [( BTo pierce with a pointed object. 1 s+ o+ F/ R. ^; C9 m7 r被尖锐的物体刺穿。 2 @2 k- h/ ^/ w) O( gFor example: Number 4 tire is punctured. 8 w4 Y4 c. m4 q/ F1 z9 p; B 四号轮胎扎伤。 1 v* o6 d- R1 h; P5 f5 [ Replaced number 4 punctured tire with serviceable wheel assembly in 8 I+ |- N$ O& Q3 Q9 _accordance with AMM---. Pressure check normal. 7 _) t& p, t9 ]0 G8 L4 r7 x3 l$ y 根据AMM—更换四号轮胎,检查压力正常。 ! A& l P7 f8 P) e& y; I l 9 z0 h0 `7 Z" ^. b x, e( {6 c6 G(22) chip: 碎屑 9 `6 O- k( l5 X0 _A small piece broken and missing from a surface. , Q' `0 X# }& H从表面剥落的小碎片。$ W `" y# b+ b' y: B4 y7 | For example: Starter magnetic chip detector has evidence of metal chips.8 s4 _% {) ?* W& p% ^/ X 起动机磁性堵塞上发现有明显的金属屑。. m* p- b' ~+ x8 l. K Removed metal chips from starter MCD. Drained and replaced oil, operation3 b0 Q P, G* Q! n! g- x$ P and leak check good in accordance with AMM---. Reinspect next “A” check as , ]# J Z( v- C$ R. Z( i! F7 U+ ] per attached EO 80-003-1.4 e" |8 z0 ^! k: J( ^$ ~2 h O 去除起动机磁性堵塞上的金属屑,更换起动机的滑油。根据AMM—操作检查正常,无渗漏。根据EO 80-003-1,下个“A”检重复检查。+ _" D9 ~9 M0 N* ?% r 5 k. h, K E! n2 C9 E2 I(23) erode: 风蚀/风化( E8 }2 l1 v3 G7 e) R To wear a surface away by weathering, abrasion, or foreign particle.% R4 m/ r4 x; K" U* @1 u1 m 因天气或外来颗粒等原因导致表面被磨蚀。' ]" m+ @8 e% W For example: Number 1 engine intake cowling eroded 360 degrees, 2 inches in width from7 _ u/ [6 Q) S' H2 \5 H center of forward leading edge. & ?' s/ v9 o% @9 L一号发动机进气道周边风蚀(2英寸宽)。 ' T/ t- {! P9 L# {Removed erosion by polishing surface with reference to SRM---. NDT * [: R% U; Z v; y3 ~# vinspection revealed 0.02 inches of material removed, remaining material 0.23 & b5 g* P4 s: bof an inch within limits to SRM---.5 V- [$ p$ Q! P; z+ _! e 根据结构修理手册—抛光该处表面以去除风蚀。NDT检查发现该处厚度减. F$ V# ~% z+ ^0 D+ Q6 h 少0.02英寸,尚余0.23英寸,在SRM—规定的范围内。" C8 Q; ^& V @3 z! j$ M - o& K( ^2 c4 w8 c; W (24) mildew: 发霉 1 S" I$ `4 b5 |0 F9 wA fungus growth.9 P! W. e7 K9 V n 有机质滋生霉菌而变质,常见白色的生长物。! u* S9 A+ ` _6 v For example: Forward cargo compartment insulation blankets in after floor area are moist - [% v. T# `( g: s7 j0 Hand have mildew.! q, D) D% B+ S/ O" U- l/ M* } 前货舱后部区域隔热棉潮湿发霉。6 M1 J/ ]1 [6 E4 B: n Eliminated mildew and moisture of forward cargo compartment insulation % T: I3 @3 {& G' o6 ~+ ^- M9 nblankets in after floor area by fabricating and installing new in accordance with 6 L6 R1 I: z1 {& N' e! _& I. TSRM--- and AMM---.9 p/ S3 s9 E$ ~6 p7 \6 v* [ 根据SRM—和AMM—制作并安装新的隔热棉,除去前货舱后部区域潮湿+ B& \- z5 s9 s' r5 y 发霉的隔热棉。 8 ^7 S U0 ]/ E/ |4 l: M b3 t+ i* X9 B+ s; c9 ^(25) delaminate: 分层, J* J2 b2 b1 w The act of separating into layers." h$ r& M7 t6 M; O4 R/ m 压合在一起的材料互相脱离或分开。 / m4 \8 j2 Q4 q' m" }For example: Nose radome delaminated from impact of “bird-strike”. " Q6 [9 H G. ^. V: ? 前雷达罩因鸟撞导致分层。 4 g/ z& `6 D p7 d. K- Y Removed delaminated core section and replaced with new with reference to8 }$ u2 E( R# Y2 \' H' \1 t$ P SRM--- impact test carried out. Nose radome OK for service. + B; q9 u1 Q% Y根据SRM—更换分层的核心部分并进行冲击测试,检查正常。8 u2 b3 E! N5 t7 F" V H: R" J. k, z & M. u% U! z1 Y4 x(26) deteriorate: 老化 4 {' r% m3 L* a- }The diminish or impair in quality, character, or value.) |4 t1 K1 {- M# u 橡胶、塑料等高分子化合物,在光、热、空气、机械力等的作用下,变得黏软或硬脆。 4 ~! t7 K1 W E. f" O/ U$ @, @" _9 qFor example: Number 2 engine to pylon fire seal deteriorated.$ F5 y# ?9 F7 [ 二号发动机吊架防火封严老化。 . N5 m8 z4 L% B6 K U+ a# S Replaced number 2 engine to pylon deteriorated fire seal with new seal in & p1 m7 r2 ?2 n6 xaccordance with AMM---.; i v7 S2 D% R3 m* q B- N 根据AMM—更换二号发动机吊架防火封严。# u y. ]& s/ Y3 [& ^ 5 z. b( z) M2 D' K$ q (27) wrinkle: 起皱3 N5 {, {4 e: {& q) M. g% O& P5 y A furrow, ridge or crease on a normally smooth surface. 0 {9 o( M6 Y2 y. Q5 p正常的平滑的表面上出现的皱纹,或折痕。5 g, e: g, x3 Y% X For example: Forward galley wall at flight deck entrance has areas of wrinkled wallpaper. w$ S! _/ n' S2 V 驾驶舱门过道的前厨房墙纸起皱。/ z2 k* s2 } I4 X! v( K Eliminated wrinkled wallpaper at forward galley wall at flight deck entrance by ; s. f* C3 }! w' w$ U* ^ replacing with new in accordance with standard practices and AMM---. / {" t* d% ^/ r- W 根据AMM—更换驾驶舱门过道的前厨房墙纸。2 {9 v* w1 f3 ?! R ! c5 j. Q* g0 s Z3 i) L: \) f (28) saturated: 受潮 ; i/ P7 H* R5 U1 VSoaked with moisture. U4 X' \7 X; m& l. J4 s: b物体吸收了水分的状态。 & ^- q$ ]. d/ S7 J3 ?# s9 q3 hFor example: After cabin floor carpet between lavatories B and C is saturated with water. $ s5 X9 d5 v) n 后客舱厕所B和厕所C之间过道的地毯受潮。 ' l; m8 v+ h& g3 _ Eliminated saturation of after cabin floor carpet between lavatories B and C by 9 S/ c! K* `/ G. X) ^$ x- F+ N3 e0 Preplacing with new in accordance with standard practices and AMM---.* A0 i2 n- K9 h 根据标准施工手册和AMM—更换后客舱厕所B和厕所C之间过道的地毯。 + W7 ]: b* e. J- r: a* d2 e! | 7 n: F# f: t# u5 Q' Z (29) tear: 撕裂 * T, y; l, h. c7 O$ `: w D To pull apart resulting in a tip. . ? Y. Y+ V4 |3 M裂开后分离。$ X7 f2 u0 Z A0 U. C& ]* ]( ~& F For example: Number 8R window shade in main cabin has a tear.2 B m4 P6 L1 f 客舱8R窗户遮光板撕裂。 7 ~: d" u1 u' I0 S8 ~ Replaced number 8R window shade with serviceable window shade in3 s' ?! W3 ]6 t: q0 ?0 g7 [ accordance with AMM---. / q, d! R Y9 Q, _, ^! ~根据AMM—更换客舱8R窗户遮光板4 W( d+ D/ F4 d+ }7 y9 ] ) E& h) z2 i) @3 G, a(30) worn: 磨损/陈旧 & x+ d x3 E) c* d! _! UUnserviceable due to excessive wear.; l6 ?9 r* ]& _: `4 p0 K- V+ O 由于过度磨损而不可用。, d& k9 p [2 D3 i& l; \% L$ @ For example: R1 service door upper guide and door latch on doorframe is worn. " r$ H1 _- j% Q" _ R1服务门上导轨和门框的门闩陈旧并且磨损。! ]6 ^$ ~7 ~4 C Replaced worn upper guide and door latch on doorframe in accordance with % }3 y# @3 ^ k9 s AMM---. Operational and functional check good.6 n0 G. M: N, K 根据AMM—更换上导轨门框的门闩,功能测试,操作检查正常。 3 z5 d" G" r G4 m 0 y3 n% t/ p$ l0 X% ](31) be not adhered: 脱胶 ( E# W% x! R) F9 z% HUnsecured and not positioned in place by glue or sealant. - m/ e( y9 b4 `- E1 Q! o因附着力减弱导致脱开。 / Q; o: u; Z7 r1 mFor example: Left emergency exit hatch external “EMERGENCY EXIT” placard is not # C! m( d h; }( w4 [8 V0 ~adhered in place. & @" ` a7 }$ O8 v) a左紧急出口舱门口盖“EMERGENCY EXIT”标牌脱胶。 : j: a6 J" l2 iResealed left emergency exit hatch external “EMERGENCY EXIT” placard in 6 A1 q2 F% |! Q/ daccordance with standard practices and AMM---. 7 ?( i/ C8 H3 h4 `根据标准施工手册及AMM—重粘左紧急出口舱门口盖“EMERGENCY6 p% Z) [# @0 s8 k. W9 A EXIT”标牌1 K1 X, U% F" o3 z$ ^" g) p ' N/ [$ O$ Z! k- X a (32) burst: 爆裂6 t6 N3 L; E: a' E4 U2 R; A To open and suddenly come apart from internal pressure.7 @3 L& j+ }1 Q' e. S 因为内部的压力突然炸破或剧烈的爆开。- S# ^" I% y- ?3 K( T+ @9 o; W" T For example: “A” system hydraulic pressure line located in forward left wheel well burst & q6 B* a" @0 {$ dduring landing gear functional check.3 l$ ]5 z5 c% P+ x& x/ @ 在起落架功能测试时,位于前左轮舱的“A”系统液压管突然爆裂。) K. O* B+ C+ ~- K4 M" G( S4 t# w Detailed inspection of “A” system hydraulic pressure line,revealed grommet $ ^+ Z5 K# A) F( P+ f% ^of retaining clamp missing resulting in chafing. Installed new “A” system & ]& K0 t) ]% u6 o7 Ghydraulic pressure line and clamp in accordance with AMM---. Operational; E" f- a8 ^+ s$ W. G$ \ and leak check good.# }8 }3 c4 i. I$ p3 A; X$ f 详细检查“A”系统液压压力管,发现因磨损,管路安装夹的垫子丢失。根 * V/ j% i- B! r/ d据AMM—更换新的“A”系统液压压力管和安装夹,操作检查正常,无渗7 f- \6 w' L6 l! Z% V. o 漏。, i* D& W" A. _5 Y% G$ M % n5 U0 k4 p& M! z1 h0 S' E (33) cross-thread (pertain to plumbing) 滑丝(限于管路)' S* X4 Z5 m3 @9 u To damage threads to an unserviceable condition.1 T( D! \' h2 L, p- n8 q 螺纹损坏后不可用。 . [% r1 [3 G! L( e( B8 B4 n- _For example: Left wing number 1 ground spoiler actuator hydraulic pressure line has- w4 |: r2 j- m1 a' h' ? cross-threads at “B” nut. ' J/ A, d4 q5 j6 ^0 B! ?左大翼一号地面扰流板作动筒液压管B螺母滑丝。 . |& n' ^: q2 v4 Z6 IInstalled serviceable hydraulic pressure line at left wing number 1 ground+ ?6 l9 E( B$ a% Z/ c3 x; C% L spoiler actuator in accordance with AMM---. Operational and leak check good. # W1 c5 |6 r$ ]0 j9 R根据AMM—更换左大翼一号地面扰流板作动筒液压管,操作检查正常, # J$ e6 }' ^% S& ?无渗漏。. K* E) J/ k! u( B1 J6 _ 8 o+ b* c6 _2 s; Z3 |0 D! ^ (34) twist: 扭结/弯曲 2 a/ z1 }; U& V9 a2 _" |/ iTo alter the normal aspect resulting from torsional stress or strain. 3 n( S: s/ I& S1 P& c因为扭曲的压力或者张力导致改变了正常的面貌。! W5 F1 g7 ?9 R# C' n For example: Right environmental control system intake door linkage twisted along routing: R2 j4 i# p. w to exhaust louver. & f" v5 _% r2 ` y右空调系统进气门传动连杆朝排气口的方向弯曲。* V$ g7 T( b0 ? Detailed inspection found broken bolt at eyelet connected to exhaust louver." W* N; @( \ Q+ @9 Y: L/ j Replaced broken bolt with new and reattached eliminating twisting with 8 Q6 l( a; K2 Breference to AMM---. Operational and functional check good. 8 {& b! k( c7 w6 h/ s4 h9 X详细检查发现排气口的螺杆断裂,根据AMM—更换该螺杆,操作检查正 0 I$ s& u4 l1 P w; e4 S4 {常。 ) k7 q5 \' R9 B7 Z5 [ ( a2 P& |: f1 G# t* w+ x (35) leak: 渗漏 4 Z! k6 u& ]4 `7 [. _9 b6 \7 M1 qThe escape of a liquid or air in a system.4 E$ p6 y1 p2 N5 E3 E, A 系统里的液体或空气逃逸出来。 6 R1 L: y+ c# P3 d9 zFor example: With reference to routine task card 37-265-1 pilots pitot static probe test failed/ N* t. K6 f3 h, @5 U+ d due to leak in the system. 0 T" u9 X. \& E& i3 I/ G参考例行工卡37-265-1测试皮托静压探头时发现系统有渗漏。 " W" Z" ^# U" i& Y5 mDetailed inspection found loose connection at pilots static port. Removed “B” - V5 _! J3 X, G" b; Q# B. J nut and inspected with no defects noted. Reassembled connection and leak+ q$ ~2 c% B, g+ M) C$ z check good with reference to AMM---. ( K2 N+ ]: o9 U/ W7 t, S 详细检查发现皮托静压探头连接管松,拆下“B”螺母检查没有发现其它缺 . D% V' M5 r1 t% S) p陷,根据AMM—重装接头,渗漏测试检查正常。7 n, I& p( A% C) n# P2 A7 s' `; _. d $ m$ y0 d5 B N0 g(36) obstruct: 堵塞6 K, P9 G0 i9 i' j+ b4 m0 R. s9 [ Blockage by foreign matter. 0 ]! l. ^: V: E. p! {# _' ]外物妨碍管道的通畅。 ; P4 [5 d9 s9 o8 u( V- H+ @1 G5 sFor example: After lavatory service panel inoperative, suspect obstruction. ) r5 z4 g; m/ g- s/ Y5 k/ G( Q; q 后厕所勤务面板失效,怀疑有堵塞。 5 R. W) v: d" R: [7 J Detailed inspection revealed drain system plumbing obstructed with foreign matter. Cleared foreign matter from drain system plumbing, operation check good in accordance with AMM---. ; @ V2 n! ?$ {) C+ x$ @& U" ^ 详细检查发现排放管路被异物堵塞,已将排放管路中的异物清除,根据AMM—功能检查正常。: B, a2 v# x: r1 C / }7 f7 N- Z' s& }+ ~( f, Z- B(37) contact: 相碰 1 @# |) A9 M% G' ]% f: L, r Touching of two surfaces or objects. ) W) \! c. U/ {# X6 @$ H- t$ R两个表面或物体的相碰或搭接。 " T" o3 a6 {4 [5 Y8 T" }+ Y* KFor example: Left wing trailing edge has aileron control cable contacting pulley bracket at ; t2 t! }# Y5 g, x. TWB Station 245.9.& g4 _" `' b0 X) }' o' v 左大翼后缘在WB位置245.9处副翼控制钢索和滑轮架相碰。 0 z# W' h1 b) Q8 L. c8 SDetailed inspection revealed pulley bearing worn beyond limits. Replaced with 0 l# C4 g y# n; Q" F/ c' w9 Ynew pulley in accordance with AMM--- travel and clearance check OK. 3 x9 c7 Y5 }% O2 `' p详细检查发现滑轮轴承磨损超标,根据AMM—更换该滑轮,检查行程及( G% y0 ~# J8 U9 K$ x" e 间隙正常。 9 z8 i0 Z) e- n/ N ) R# o; @( {$ E& t* d8 _ (38) fray: 断丝/磨损 9 d3 W7 I7 f1 ]7 M4 I/ HTo wear away by rubbing. 9 i/ @( [1 [1 G3 T因相磨或反复拉伸导致的损耗。8 y0 a5 {" @4 p: l0 {, k* U6 f& t. D9 R For example: The lanyard attached to the after end of the right access door to the APU0 m) z! G2 | C! A& H+ W compartment is frayed. ; x" w# Q* h6 h( L右APU舱门后端系留绳断丝。. d' s2 I( O8 @# n; ^ Removed and replaced frayed lanyard in accordance with AMM---.( R8 P8 L# e5 g0 W9 U! c 根据AMM—更换系留绳。. a( |/ N0 b- j; [ 4 S* b( U2 q" \2 K( }; M2 o (39) fused: 熔断/ a, l) @0 @- k/ V+ p5 L* a& v To become united by melting from heat.* Q6 R/ F2 b# p, h6 `/ q. h1 p) { P 因为高热而融化连接在一起。 ! D$ a7 r2 r' \& Y% I8 @- u For example: After galley coffee maker inoperative. Detailed inspection of after galley coffee w% S7 V7 {. R4 Qmaker revealed thermostat wire D34768 fused to temperature controller wire & x( y. @; e: s; PE57689.' U+ b1 A1 O/ W, n3 h+ h 后厨房咖啡壶不工作,对后厨房咖啡壶进行详细检查后,发现温度调节装& f0 L- `$ H9 a 置导线D34768与温度控制器导线E57689熔断在一起。& b; z/ v! O6 d* j* M Replaced wiring with new, operational and functional check good with / e& a/ N! s7 X5 ]( s, |5 Ureference to OHM---.$ n5 v% s9 l7 T+ i) d 根据OHM—更换线路,功能测试正常。+ h6 A: ^/ b% O6 R ' t/ R$ \7 s7 q% S1 z" _ (40) bend: 弯曲; ?( a, {3 A2 s+ Y) P& N; s' f Altered from straightness or original position.+ Q7 u J! V& Z" x0 f# Q 改变平直或者原有的形状。! G1 M* q* y: Y4 o/ f; p$ @ For example: Forward electronic bay door left hinge bent. - I. B" y, v0 Q5 X o3 C 前电子舱门左铰链弯曲。 ' \2 B. F& V! v5 F9 \2 _8 s( N# A Replaced left hinge with serviceable hinge on forward electronic bay door with 8 @/ P! r) \9 j1 O/ |9 K' l; Jreference to AMM---operational and pressure check good.. 0 E* z' L5 @/ l$ ~6 _: n8 Y根据AMM—更换前电子舱门左铰链,功能检查正常。5 R. w% h9 \# I, c' V7 m1 c 2 h: F5 o/ R; O4 I8 Y( Q" b: W(41) disconnect: 脱开0 r8 G6 r. P" q- R9 ?) C Not joining resulting in failure.$ p, ~0 f( C6 r" C' p. z. j 因没有连接而失效。' ~! R, U- L# C, S( ^' R For example: Left environmental control system pack temperature control has disconnected 6 _& `1 m8 @6 q2 H9 x' Acannon plug. + A3 `6 ?+ n9 C) R$ h/ b左空调系统组件温度控制插头脱开。- [6 i& \2 L/ ?. C; s7 U; J" t3 c' A Reinstalled left environmental control system pack temperature controllers ; }" C3 T7 Q' Y3 H( wcannon plug, operational and functional check good with reference to AMM---.( b3 A& K: s2 i. C+ R& W' f) m3 v1 h6 | 重装左空调系统组件温度控制插头,根据AMM—进行功能测试,操作检 * P! l& ]7 p9 k0 u8 b& A5 ~查正常。 ; [2 K8 M6 P4 ^/ A: J! v' c& I6 V n3 k( w7 k6 F, {9 l4 Z- X (42) missing: 丢失 ! U: O$ U3 z2 z/ M0 |/ c Not present." v% L7 N c: Z3 v( r 不在位。 j/ ^5 d- H! j3 j$ u" X6 `' h For example: L1 entry door has 3 each door stop pads missing at the after middle section of 9 ? R: L+ E7 X9 dthe door frame. 3 s( d3 g- F3 S0 s# k0 @左1号登机门后门框中间位置有3个止动钉丢失。( b' Y+ O2 }+ A, T; I Installed 3 each door stop pads at the after middle section of the L1 entry door 7 s% }6 {; H1 M' M- n2 `+ x( d) Kframe in accordance with AMM---.* Y! i6 k$ |% f. s! c; C 根据AMM—安装左1号登机门后门框中间位置的3个止动钉。. u6 ?8 r4 Y: [) D3 W 7 N7 t6 E0 U7 x8 \- j; l. j! y (43) loose: 松动/松脱 ! d9 \4 ?$ s# U& rNot secure. , f8 c! |' C! t' ?; v3 A没有紧固;活动+ l+ ?- W4 E( B1 q% s/ d9 A For example: Forward right wing to body fairing has several loose screws.2 D8 Z0 H- \+ y2 D 右大翼机身整流罩前部有几颗螺钉松动。 # K# {; z1 ^ {4 n4 q Z( ]- k3 j Found 17 screws loose. Tightened loose screws with reference to AMM---. 7 @8 g+ j- v4 I3 c' |" \ 检查发现共有17颗螺钉松动,根据AMM—将所有松动的螺钉紧固。) N9 M" H, c0 F4 m. }* h ) r% j* q- O5 d2 q: g( _& S! H (44) not secure: 未关(扣、夹、卡)紧 + R7 [, U; o6 o# vNot fastened, to make firm or tight.# _. Y" A+ Y1 ^: N7 p 没有扣紧,(使)紧密。6 p1 r5 X! d/ q For example: Number 1 engine cowling; number 3 latch is not secure.+ j5 a& j! L6 d 一号发动机整流罩的三号锁扣未扣紧。 2 E! o; ?) \' s; B) Z! }6 [ Number 1 engine cowling; number 3 latch has damaged hook. Replaced+ [; [# s; w+ }7 G# C7 T0 G number 3 latch with new part in accordance with AMM---. Operation check 0 z; ~' }' D; Z; @ iOK.2 T8 q- r( M6 c$ ?% A8 q& H 检查发现一号发动机整流罩的三号锁扣损坏,根据AMM—更换该锁扣, ; Q4 w4 |4 K# @: h8 t3 ?5 j操作检查正常。 ! v( b7 w" k4 k% t " X% ~2 Q$ ~$ g2 I (45) inconsistent: 不均匀9 B" d" S6 Y$ ]( N3 M Not in agreement, erratic ) F" k5 g; ?4 h g' c缺乏连续性。 ; g5 F; V- F$ u4 R' {/ v- J7 aFor example: Left wing-to-body fairing seal is inconsistent in relation to fuselage.6 l [) Y! G& Q# ^ 左大翼-机身整流罩封严胶不均匀。 ' V7 ^" K8 i2 H* ^9 J Re-sealed the left wing-to-body in accordance with standard practices and5 |- G2 H" \% S" T AMM---.4 G/ g) L- U/ O# s- e 根据标准施工手册和AMM—对左大翼-机身整流罩进行重新封严。 3 L7 S2 ?7 R1 Q( A G" r; A5 q $ D, ?* O6 ~& f4 o(46) exposed cords: 见线 ( Z8 \9 @" v. R3 K& e; LVisual tire cords. $ V* v; M! k& R5 ]0 c轮胎编织线裸露。 K# l# \0 E. k For example: Number 3 tire has exposed cords.) m% v3 b! Y8 W, ?+ K) T- } 三号轮胎见线。( V" b$ A, Q/ @! f Replaced number 3 tire with exposed cords with serviceable wheel assembly in& m& P5 \2 n+ A accordance with AMM---. Pressure check normal.6 p2 x# r$ Q) q0 [8 ~ 根据AMM—更换三号轮胎,检查压力正常。6 Z7 H0 c" K. p) l, D! v7 s3 w . Y# r- @3 |/ m1 D! a) z (47) bald: 磨平8 T2 c X8 z( `3 a Lacking a natural or usual covering.& z3 ^. @3 ]. b7 O6 q: c 轮胎表面排水槽由于磨损而消失。0 N6 j q G& A3 s" H9 p d For example: Number 3 tire is bald and requires change prior to flight for no serviceable * { Q: y* D' ?5 y. ~4 Aspare at scheduled flight sector out stations. + h4 ] H$ @- p三号轮胎磨平,因下一航站没有备件,请在航前更换。 , V/ Z2 P5 C+ PReplaced number 3 tire with serviceable wheel assembly in accordance with , g4 {1 n* B9 p% r4 oAMM---. Pressure check normal. 5 g0 d) w2 D: P1 e根据AMM—更换三号轮胎,检查其压力正常。0 ^& [$ ?% n: M% b0 p 7 v [# Q' R5 k- d# n5 G2 \(48) insufficient-air-pressure: 气压不足 " l( y e8 l2 |' VAir pressure does not meet manufacturers requirements. + s; B" S, W# z' \# W# A |4 E, s空气压力没有符合生产厂家的要求。3 X2 t: P: ~* O4 u& D6 m For example: Number 1 tire has insufficient-air-pressure. 7 i8 Y" u$ L( m 一号主轮气压不足。- Y) L" \6 R8 z* W2 O* E/ M Measuring air pressure revealed 5 psi. Air pressure required within limit as $ e6 K5 ~3 o) I7 s6 _* gcalled out in AMM---. Serviced number 1 tire with Nitrogen as referenced in - v7 Y6 P3 ^9 n; k% }AMM---. OK for service.; `- H6 K& G, H t7 d 测量一号主轮气压为5PSI,根据AMM—对一号主轮充氮气至要求。% Z1 k: a2 s: }" b0 m2 G: h) A5 W 4 D1 A0 x/ }! }2 K, _& }5 z$ z (49) expire: 过期 * s; P& ?- K- d" M0 }) L9 gTo come to an end or terminate. 6 c; Z0 K6 ~; ]/ F: `4 s- ]超过时限、期限。$ R/ E7 o2 e9 ~& ]! x For example: 2 each life vests located at L2 entry door flight crew station expired. # I9 f% o$ l4 h& w 位于左2号登记门机组人员位置的两个救生衣过期。 ' p8 q" M; A2 i8 c( D. c2 Z Replaced 2 each life vests located at L2 entry door flight crew station with8 Q5 b5 a# w7 w" L( x- N0 h* S, O1 B serviceable life vests due at 9-2005 with reference to FAR 121.6. $ \1 ]: D" \( l* ] z P 根据FAR 121.6的要求,更换位于左2号登记门机组人员位置的两个救生8 c1 y8 y- W2 g 衣。 * Z4 d$ H8 \8 ?) T8 C# v1 h + n0 m2 F0 B, [: B% j/ R' _( W (50) illegible: 模糊 # U, n+ F+ {: ]0 T4 ?Not capable of being read or deciphered.+ h+ J2 B2 v& q, ?" V/ _ 难以辨认的,无法读出或解释的。# u2 E1 W) Y' W" E1 m For example: Left over wing external emergency exit hatch “EMERGENCY EXIT” placard1 }8 y' H! W9 W is illegible. ' H& k3 q* P- b7 C5 Z6 v左翼上紧急出口舱盖处的“EMERGENCY EXIT”(紧急出口)的标牌模糊。2 D5 {( u' `! m3 M9 I Removed and replaced left over wing external emergency exit hatch8 f# @8 R u, Y) V! O+ Q “EMERGENCY EXIT” placard with new in accordance with AMM---. ' k- v4 C; H% a8 D, K9 h根据AMM—更换左翼上紧急出口舱盖处的“EMERGENCY EXIT” (紧急出口)的标牌。 ( _! ]" u; a) o0 T# p) w. ~" m ' e# e/ j. p5 p# I8 n (51) damage: 破损/缺损 - _/ x2 y( U4 yNot useful or functional.1 n9 F0 T8 n7 @& e/ N 不能用或者功能失效。* k6 w/ _! d+ y) j* X For example: Left wheel well landing gear door “NO-STEP” placard damaged.: z l1 i7 f7 W$ s2 E2 i* v 左起落架门的“NO-STEP”标牌缺损。' p' Y6 z; `' S; V5 u Replaced damaged placard “NO-STEP” at left wheel well landing gear door. ) d+ N3 _/ }2 Z 更换左起落架门的“NO-STEP”标牌。 - U8 a3 ?! _* K# Z5 ~* k0 w , T8 M: L Y. Q' s O(52) lifting: 翘起) E' y& H$ o: M2 f( } To become raised, not intact.1 \7 C- m% v+ b- Y- U" t$ b) k 没有紧固;活动8 h* E4 Y: j6 z! \ For example: R2 service door escape slide operation placard is lifting.' D6 e0 Q2 k e* J: F 右2号服务门逃生滑梯操作标牌翘起。 ' H! i/ ~' P# N4 S& |' T, ^' ~1 g Removed lifting R2 service door escape slide operation placard, cleaned and , `: Q3 P/ G3 }# `/ Ere-adhered to in accordance with AMM---." C1 J5 a. ?" w4 R 拆下翘起的右2号服务门逃生滑梯操作标牌,根据AMM—清洁并重新将* b1 Q, u; g# l7 W/ T 该标牌粘好。- R$ V7 s& c3 L J {! O% t9 l(53) not properly sealed: 变形/密封不佳 + x, d( v* x; MRetaining package torn exposing contained contents. & `1 C7 W$ R, U. ~固定的包装撕裂而露出里面的东西。9 p; B! O6 j) s* S$ e2 R For example: L1 entry door flight crew station portable breathing equipment not properly: D: i8 d6 j; D& O& T8 d sealed. 4 }% ^3 t$ z6 ~* h7 g8 o# \左一号登记门机组手提防烟设备变形。 9 B. I( d( X+ s7 p3 xReplaced not properly sealed portable breathing equipment with serviceable! V: e/ H0 S* x0 `; u portable breathing equipment with reference to FAR 121.25 as required for- i5 C' Y+ l$ i' @( E; W dispatch . Tagged and routed unserviceable PBE to MSC to return to customer.1 j2 E {3 o6 W& m 根据FAR 121.25放行要求,更换变形的手提防烟设备。旧件挂牌送航材处$ O8 _* z; Y$ A1 f U* @ 理。% F, C) i. G' g6 s' A: [( E ; ?5 N, O7 G5 \* n: I( x; ?" t1 P(54) not properly packed: (滑梯)散包 $ Y! J; c/ h$ N1 J! nThe condition of a released slide., j; f1 R) B' e# Y/ _7 x 滑梯包散开的状态。/ F- m8 T+ B0 }0 A2 m For example: With reference to reliability work order and task card 25-456-01, replace R21 c- S2 Y" \! C4 O6 ]- V& x service door escape slide, provided escape slide from workshop S/N 4321 is not2 g( d' F3 n, m y$ j" }. `, J properly packed. - r A& e3 c$ u$ ?) ?% Z$ t按可靠性工作单和工卡25-456-01,更换R2号服务门的逃生滑梯,因为由7 A, g* H K5 B! `! f+ a 车间提供的(S/N 4321)件已经散包。 $ C h! P! j' b' ~: JTagged and routed emergency escape slide S/N 4321 to MSC to be re-pack in % g6 k. K* |8 Lworkshop. Obtained serviceable emergency escape slide S/N 8765 and installed4 b& U6 q" P9 n1 B+ K& x1 w7 e at the R2 service door position with reference to task card 25-456-01 and & C& l% Y% M& e: D9 {) o5 {AMM---. ( e2 [- U7 f; t' ]% {& W1 O 将序号为4321的紧急逃生滑梯挂牌送航材给车间重新打包,根据工卡5 o" P; u# e9 S# z% a$ g 25-456-01及AMM—在右2号服务门安装序号为8765的紧急滑梯。 # ^8 n; I; a2 r# C 5 K+ I" ], V2 W) ]3 a2 [' W (55) dirty: 脏 7 j3 i& Z5 N* c2 cUnclean, soiled with dirt, grease etc. & I7 @$ {. v- E不干净,有灰尘或油渍。5 ~3 _3 k+ A! T0 p3 p; |4 Y* q For example: Flight deck external window are dirty.0 i5 j0 e; q. T, c$ o0 m/ v 驾驶舱外层玻璃脏。! L: a( m2 O: J Cleaned dirt from flight deck external window in accordance with AMM---. S4 p/ _# \1 B8 A5 ? 根据AMM—对驾驶舱外层玻璃进行清洁。1 d8 w4 v7 G. I1 M+ _ ; P* ] k9 d" D# H( f) t6 L(56) fracture: 断裂! v. n: N ?- c7 m' | A break, rupture or crack. : T, Z N% c; Z7 F2 _- L7 L$ @破碎,破裂或裂缝。! {8 _: f" W4 _) U3 M; @3 W For example: Reference Gameco routine task card 53-004-12, NDT X-Ray inspection at right * d3 F+ d/ n a( T, {7 {2 Rwing emergency exit hatch frame revealed 4 inch fracture at forward lower sill. 7 \4 g1 p6 F4 r+ K) I参考Gameco例行工卡53-004-12,NDT进行的X光检查中,发现右翼紧: g5 g I6 v- B4 Q 急出口舱门框前下角断裂(长约4英寸)。 ' S9 q" [/ M( @) |$ `4 K. l' WRepaired fracture with permanent repair in accordance with SRM---, attached1 Z" q- N1 ^2 b6 t; H! m Gameco engineering order 53078-4, and attached Boeing TELEX 53-0987-1.8 L3 V9 m s0 Q& a4 L7 J. z+ \4 K Applied protective finish in accordance with reference to SRM---. a% \. r6 E& S8 Q. E* x根据SRM---,Gameco 工程指令53078-4及波音电传 53-0987-1,对断裂进 . m n0 M* D- B9 H: a5 A2 O行修理。参考SRM—进行保护漆层的恢复。, c# @" z; T% c+ D' X * h k" R+ ]( I5 d6 H/ f; O(57) exceed-the-limit: 超标' R' r. E1 Z2 |) P: z Does not meet manufacturers specifications. : {9 x) Q) H% H6 j, |6 p; k1 o) i超出生产厂家的技术标准或规格要求的范围。% |* G# q3 G6 A2 t( ?# g For example: Reference routine task card 32-098-01 landing gear functional check, nose, L" f. B; c, s! B) d; y8 Y landing gear doors faired to fuselage skin exceed-the-limit during functional ' c% _9 p+ W% W7 |9 w; W6 s/ qcheck. . F8 V' P5 s( a; O0 G- G* V1 ]参考例行工卡32-098-01做起落架功能测试时,在功能测试中发现前起落; l6 v) g* w% l 架门与机身蒙皮间隙超标。1 [2 X. g% o1 D- O4 } Adjusted push-pull control rods at nose landing gear doors to obtain proper5 y. N* w: ?1 X8 X fairing to fuselage skin in accordance with AMM---. Clearance and functional + K/ H/ K" U+ ycheck good in accordance with routine task card 32-098-01. + q& x6 `+ a0 u根据AMM—调节前起落架门推拉杆,按照例行工卡32-098-01检查间隙及0 Q) V2 \8 e& m: ~/ u$ o+ L; F, } 进行功能测试,检查正常。 : m' \% F0 K( F: y1 ~ ( V/ c6 o; e8 J (58) backlash: 空行程/无效行程# N% x* X/ W$ y+ l To measure play resulting from loose connections between gears or other mechanical& p6 g5 Q9 ]6 ~2 k elements.8 [( @( @$ ~1 L3 q/ x; d 传动装置或者其他机械元件之间连接的松动而导致的空隙。 6 p; k; \0 ?# H) K H$ kFor example: Horizontal stabilizer jackscrew clutch failed backlash test with reference to# R) t) [0 J2 r, z7 J2 w1 R routine task-card 27-0345-01. u) S: E! T* r按例行工卡27-0345-01进行测试,水平安定面蜗杆离合器有空行程。 9 c2 `( `0 z# {) A4 f/ hRemoved horizontal stabilizer jackscrew clutch. Detailed inspection revealed1 a2 M% }# e! i b( h worn clutch plates. Tagged and routed unserviceable clutch unit to MSC for7 j8 y( Y/ U: c* z return to customer. Installed serviceable horizontal stabilizer jackscrew clutch , v5 C- }5 b0 I; m* Oin accordance with AMM---backlash and operational check good./ s2 K" \8 e' N* | 拆下水平安定面蜗杆离合器,详细检查离合盘,将不可用的离合器挂牌送% Q9 W. r9 |8 @ 航材。根据AMM—安装新的水平安定面蜗杆离合器,功能检查正常。 1 [% B* A, v* M 2 X5 O3 H) d5 i9 z9 r; m8 N8 k (59) block: 卡阻/阻塞 . C, F9 y3 K L9 KThe act of obstructing.1 v. J" o- \% l 通道堵塞:运动部件的动作不顺畅。; J# f& k2 m+ y2 L For example: Forward cargo compartment door forward actuator is blocked when opening , r+ H Y% m4 B' g* z* h/ P& dthe door. . l9 V2 n9 N: X1 I" n. M前货舱门在打开时有卡阻。 L& v8 d: n% b4 Q% \! hDetailed inspection revealed there was a dent on the actuator rod. Replaced the - m: m: K k/ x+ k# linoperative actuator in accordance with AMM---. Operational and functional! ?2 ~7 }% S$ N# n! r8 s4 d check good.# c% j- G' R( F$ f0 G 详细检查发现在前货舱门作动筒杆上有凹坑,根据AMM—更换该作动筒, - [# N% y, \. n7 W, I; k# @操作检查正常。 3 K- ]4 h1 W' J) ^" Z6 s4 b' P 9 ^( d. f) }; N" `* n# A(60) bulge: 鼓起 ( m8 J; C; Q, q( _An outward curve or swelling.! [" J# h6 I, u* G$ m# s 向外凸起。 5 K7 j# \& V( ]3 t! u9 qFor example: Forward cabin lavatory floor panel is bulging." s; f: C3 H. V1 J% ?# a 前货舱厕所过道地板鼓起。* g2 j" r& Y: [' `. r& x O \ Removed forward cabin lavatory floor panel, no defects noted. Re-adhered4 ~8 m, m2 B$ L, n- M2 \6 n4 B forward cabin lavatory floor panel and eliminated bulging in accordance with. F' p! Q; P1 K' j4 M standard practices and AMM---.8 ]/ y/ c) A# {1 @9 c( @ 拆下前货舱厕所过道地板,检查没有其他损坏。根据标准施工手册及 . X- K$ P" f# Z, X( ~6 `* JAMM—重新粘接该地板。 6 t2 T! C2 h5 W& @/ u ) f9 x5 |8 N4 w* T(61) contaminate: 污染 0 ]$ Y" y+ W! uImpure mixture. 9 \1 Z1 |7 L! L% [% x- Z# b有不纯的杂质或异物。 ; g4 w% v/ ^. ^: sFor example: Fuel sample reveals positive contamination of microorganism growth. 5 L, q/ J* Q" ^" V! I/ B' [, D 燃油样品检查发现有微生物污染。) b/ y4 i! f4 @5 t+ k! G9 y+ g Treated fuel tank with biocides with reference to attached Engineering Order 6 C1 Z4 `. B: YG2009619.. J) Z2 r5 M. R) J j 根据工程指令G2009619,使用杀菌剂对油箱进行杀菌处理。' o) t9 [* d; B ! @. t& ^! N6 m1 C$ J (62) disagree: 不一致 5 i- q1 B; {9 r7 W6 J* vFail to be in agreement.4 H# N) {' w5 |1 W" J* v! s* e8 Y" { z 对应关系不正确。1 n1 r; j, b2 Z4 y" U; q. d For example: Flap control lever disagrees with flap indication gauge through all detents.( [9 b6 ?; |. d; J2 O( E. V 襟翼控制手柄在所有卡槽位与襟翼位置指示表指示不一致。; l$ N; }* G5 c* [7 z1 f2 t Adjusted left and right wing flap indicators in accordance with AMM---. ' H; |4 D$ t6 i* COperational check good through all detents.2 e4 F0 q) G4 q# j. e5 P" n 根据AMM—调节左和右襟翼位置指示表,操作检查襟翼手柄与位置指示" Z, ~' ]: c1 K$ c( ? 表指示一致。9 p9 @1 n( [& X0 Z' l ~+ Q 3 `& w( s1 ^! c @$ b7 v& O/ \( R6 u(63) discharge: (电池/气瓶)被释放$ i9 k2 v3 e, i! T To relieve retained contents to an empty state.9 x) r3 [9 O' }; y$ P9 i" h 放出;腾空 + f$ x6 Z: {; M5 o- g6 mFor example: R2 service door assist accumulator discharged. 6 A( }/ Q6 Z& v3 L" E 右二号服务门助推气瓶被释放。 . @: Q5 H+ ~% B$ V/ N R2 service door assist accumulator detailed inspection revealed damaged5 n1 b. X/ |6 @ pressure gauge. Replaced pressure gauge, serviced with dry air as called out in 7 B( A8 l o. T5 [- |) Q9 ~+ ZAMM---leak check good. 4 ~0 T$ Z( k; t/ M6 \5 y详细检查右二号服务门助推气瓶,发现其压力表损坏。根据AMM—更换1 B' O; F3 T5 q& X9 h 压力表,对助推气瓶进行勤务,渗漏检查正常。 # i9 f( H- R, k3 D1 u- |/ h. i6 h 5 y2 M, C! R* U% R (64) dislocated: 装错 - ^0 E, ?: R* `$ \# w' {3 wNot in proper relationship with joining part.: k/ M8 k. r. _2 p 零部件没有安装在正确的位置。 : b* v4 }) ^7 d8 k. mFor example: Forward cargo door pressure seal is dislocated from retaining track along after3 M2 C% x1 c3 _& v1 J and bottom section of door. & n8 T9 x" K8 M7 V前货舱门后底部固定轨道的压力封严条装错。 ^0 c* E2 n: w/ A Detailed inspection revealed pressure seal retainer damaged along after and$ ?- ?/ ?/ ^& L5 p8 Q/ s7 o. B' v bottom section of forward cargo door. Replaced affected section of pressure3 W! n# O9 W- a+ @' N seal retainer and reinstalled original pressure seal in accordance with AMM---.7 n& D. G& e- i, k Operational and pressure check good.* ~$ D0 M! v- l% G! F/ ` 详细检查发现前货舱门后底部压力封严条安装槽损坏。根据AMM—更换5 i0 S+ U9 j( u$ T6 R c 该安装槽并重装封严条,操作并增压检查正常。 9 b+ |4 s4 A" e/ r / P& A h# i1 Z* t/ f% D( }3 ~# a0 j& o(65) fail: 失效) g( a( H4 N8 c" | Note: must have detailed description of failure. ) L |- t V- j7 Z注:如用此术语,必须给出故障失效的具体描述。 - G/ ~/ L' e2 U, qTo perform ineffectively or inadequately.6 J% a' E/ y) g 不能执行或不能完全执行原有的功能。% _# T' u$ n( s8 k& ] For example: 13F seat actuator failed to adjust.# b6 T0 D" v; @* d# J6 I/ r8 v 第13排F座椅作动筒失效,不能调节。% k9 X8 @6 D9 Q2 X0 f) S; H Replaced 13F seat actuator with new part, functional check good.* g! {/ \8 q/ Q% C8 A 根据AMM—更换第13排F座椅作动筒,功能测试正常。. i; a; z3 ~9 o; U+ Z( l/ e8 Y 7 z1 M8 P; S; f; `(66) fluctuate: 摆动+ m! |0 I: L2 O To continually change or vary in an irregular way.) k. K# w# ~* B4 S4 @' G0 B 无规律连续的起伏不定,变化。' y4 F& o5 e: D, F! G For example: During engine run the number 1 engine oil pressure gauge fluctuates. ! o" v4 o8 v$ A, z 试车时,一号发动机滑油压力表指示摆动。7 x; J' G! i9 Q# F9 c( [ Replaced the number 1 engine oil pressure gauge in accordance with AMM---. Carried out engine run, oil pressure gauge normal.4 ?6 Y8 C, e+ D5 E 根据AMM—更换一号发动机滑油压力表,试车检查滑油压力表指示正常。2 N _6 B& N I) ]6 r# Y/ Q5 j 7 a f1 x- v2 o$ q4 D(67) flutter: 抖动2 F* H8 _/ S' k1 d" ^+ [ y A rapid waiving or flapping movement. 0 u: ]0 f+ X/ M! {1 F! J快速的摇动或者上下振动。1 ^+ @9 A+ o' T5 y+ e" \ For example: Pilot report on flight logbook page 908701 fluttering sound from left side of ; j: s- B2 J/ Sairplane during descend beginning at 11000 feat. 5 Q; \! G$ w9 X7 ?/ _ I6 `9 Z飞行记录本第908701页驾驶员报告:当飞机丛11000英尺下降时,飞机左 t4 z0 Q; E F 侧有抖动的声音。 . z- D6 y4 a6 G) ]0 yInvestigated fluttering sound from left side of aircraft as squawked on page , Y8 f( M5 n# a( y8 ^* c908701 of flight logbook. Found number 3 flight spoiler actuator leaking. ; X2 H" p) V) ^ Replaced number 3 flight spoiler actuator in accordance with AMM---; d* T" y% W: x8 s) F& ] A operational, leak, functional check good. Flight crew briefed prior to flight. " V' y/ Z* V/ h对飞行记录本第908701页记录的飞机左侧抖动进行排故,检查发现3号飞行扰流板作动筒漏油。根据AMM—更换3号飞行扰流板作动筒,功能测试正常,无渗漏。机组飞前报告。 4 v) Q1 ~' e$ W7 {+ U' A" | ; F9 `' H( b. K2 H' l1 m (68) insufficient: 不够/不足 ; P' y- A" c: W. j$ R0 i0 }# wNot sufficient, inadequate.* b( j+ o4 g* u8 P! r% `, _ 达不到所要求的数量,数目。% i) ~* Q. e9 C For example: Left main landing gear alternate extension control cable has insufficient- L7 Q+ T) b" Y% s7 K lubrication. 3 f" r _$ D) D! u! ~1 B# q/ u7 G. e左主起落架备用控制钢索润滑不足。 ' u3 C& `0 ~2 O6 i8 f& TLubricated left main landing gear alternate extension control cable with , b' h' H" D1 a& K7 t3 kAero-shell 12 grease as called out in AMM---.! K. d" s4 o/ t' r( J9 l5 c( V 根据AMM—用Aero-shell 12润滑左主起落架。 7 R/ P2 L( j! a+ g4 K # w" G: d1 }# p# U* K (69) inoperative: 不工作( N! x6 S5 h9 a# N5 z% M/ l Not working.8 X n- W* N+ x+ P 不能正常的发挥功能,作用。- Y! J6 w+ M/ }% } For example: Forward electronics bay door indication light in flight deck is inoperative. + N0 X/ E4 J# m W' y9 m 驾驶舱前电子舱门指示灯不工作。 " A) |; X" N+ g0 i- }7 E: l2 c1 @ Detailed inspection revealed 2 each bulb filaments fused in electronics bay % M* \6 m! c% ]0 @, C3 R* Fdoor indicator. Replaced 2 each bulbs in accordance with AMM--- operational 6 e! g% U1 Y$ h+ _, b: y6 X' i& Echeck good.4 m/ R$ @: n+ w, r# k4 ~ ? M 详细检查发现前电子舱门指示灯2个灯泡的灯丝烧断,根据AMM—更换 . M4 X& {" x5 f6 e! }. |2 O0 d这两个灯泡,操作检查正常。 - M4 Y# x" j: f. y! v8 L" i/ P 2 t7 Q- r: m( W& t. l(70) (not) illuminate: (不)亮$ w) R- ?" Y8 O- p6 r5 l Not brighten with light. 1 y, ^5 Q5 c) _: z" N不照明,不发光。$ I2 H; |% U C For example: Passenger reading light at cabin rows 12AB, 14C, and 17AD, will not 9 ~; c2 @& S& G! c# I# Silluminate., s8 Z' K% `" ]8 g 12AB, 14C, 和 17AD座位的旅客阅读灯不亮。4 ]/ F3 I2 L5 e Replaced passenger reading light bulbs at cabin rows 12AB, 14C, and 17AD in) d4 A9 a, _4 w) t; Q: s accordance with AMM--- operational check good. ; ~/ u9 X) D( u( V7 _2 r6 s: |% i根据AMM—更换12AB, 14C, 和 17AD座位的旅客阅读灯,操作检查正 ; t* S$ N1 w9 H/ q3 A常。: b7 w; ?% y; P6 X- k* [ 5 w( |4 n9 \( v (71) interfere: 干扰/ r9 ]4 L% [4 u/ Q8 j+ \, v To come between so as to be a hindrance or an obstacle. ' b% e/ O. S" F& h妨碍无线电设备正常接受信号的电磁振荡。; }& Y u& m+ c% \4 |& l+ h# Q For example: Functional check L VHF radio revealed interference static and abnormal noise. 1 k4 |" P; W; A3 X% N2 C 功能检查左VHF设备发现其工作有干扰及静电噪音。1 f+ Q! G" b' k. ? Replaced L VHF radio in accordance with AMM--- and tagged and routed the $ U0 j! |8 D4 \& _" _. ~, U# o1 o6 ^removed part to MSC. 4 R4 y% T+ ]- a: u- X6 B根据AMM—更换左VHF设备,旧件挂牌送航材。 : Y/ z: N8 C0 E( a4 j. _ 7 k% h8 R, Z! y% S0 U% A8 m (72) kink: 扭结/缠结7 j5 [4 }( v- M! K" v A tight curl or sharp twist. ; x+ K1 @& t2 e4 E(钢索,条壮物)缠绕在一起。 . w# l5 b; }* K9 A' g- ~For example: Right wing inboard flap control cable at control mechanism located in after0 G6 V$ E, z" T$ W2 p right wheel well is incorrectly routed and kinked.0 r; z; L- @9 ]; s 右后轮舱的襟翼控制机构里的右内襟翼控制钢索走向错误,且有扭结。 ! [& U7 ?+ I+ N' @Replaced with new flap control cable from Body Station 760 to flap control9 `. t9 W( L2 l mechanism in accordance with AMM---. Travel and functional check carried out in accordance with AMM--- check OK. Carried out detailed inspection of area of misrouting, no defects noted. " h N3 |$ C5 K$ S9 J! n) u根据AMM—更换从机身站位760到襟翼控制机构的襟翼控制钢索,按照AMM—对其进行功能测试和行程检查,检查正常。详细检查钢索错误走向的区域,没有发现其他缺陷。1 f, l0 c% K5 ^; ?% @+ _ # q! g- {7 P# K, c(73) misrouted: 走向错误 2 |3 }/ G: c. f/ e, u! t- bNot properly aligned through a course of travel. 0 M/ y9 o8 _0 _* \在行程中没有正确对折。 " {+ \, U+ j" m o$ \For example: Left main landing gear manual extension cable is misrouted through pulley attached bulkhead in the left wheel well. ; T' d( |, J6 P! B* Q. ?' Z 左主起落架人工放下钢索在左轮舱经过滑轮后走向错误,与前压力隔框相磨- P* g: B$ i' Q6 ?" u( j+ g Removed pulley and carried out detailed inspection of surrounding area resulting in no defects noted. Reinstalled original pulley eliminating. Misrouting in accordance with AMM---. Functional and operations check good. - {: y+ d% z2 } 拆下钢索滑轮,详细检查周围区域,没有发现其他缺陷。根据AMM—将 2 Q6 Q: p7 @+ e该滑轮重新安装,功能测试,检查正常。 h/ N' \( n; M/ V H 7 x4 F/ R& k6 G8 J! f+ Z1 d (74) not installed: 漏装 $ m7 r, [4 [/ k1 MMissing. 1 j8 f4 b$ z& o根据要求本应安装的零部件未安装。 B0 W2 z& c" U2 z! W* [2 fFor example: Life vests not installed at L1 entry door flight crew station. 5 m9 o$ ]& M! z0 U" g9 e- O1 c L1登机门飞行机组位置救生衣未安装。 , s9 a# ~3 W9 G! c2 q0 Y. O Installed required life vests at L1 entry door flight crew station.% E3 [1 @+ h9 c/ g! {# Y! k 在L1登机门飞行机组位置安装救生衣。. A) i5 _+ ^6 l$ s$ q . \5 ~3 N" e4 n. M: Q# e# q (75) rubbing: 相磨 o, n2 E* C9 ?% G* sMaking contact with an unrelated surface! ~' r( [; ?: D 相对运动的两个物体表面因接触而导致磨损。5 m3 m- y- J( q( o( H8 R For example: Wire harness for cabin PSU’s running through floor beam at body station 360: H4 i8 Y7 X4 s and wbl 21.52 is rubbing against floor beam cutout., ~: p3 _+ @( \) k- _ 客舱的PSU组件的导线束在机身站位360和机身水平站位21.52处穿过地 1 D' f( K7 a6 P) s+ F, s" \板梁时与地板梁切口相磨。, i6 E! H5 C9 ?3 j6 v8 D Detailed inspection revealed broken clamp at body station 360 and wbl 21.52. Replaced broken clamp with new clamp eliminating rubbing at floor beam cutout at body station 360 with reference to standard practices and AMM---. 1 p* i0 C& Z+ Y7 |8 t: ?7 q( z8 m 详细检查发现位于机身站位360和机身水平站位21.52处的安装夹破损, 1 [! D" P# P- a, Q m/ ?2 N根据标准施工手册及AMM—更换并调节该处的安装夹,消除导线束与该% d( o5 X- c; P$ k/ O* j& H( I 处地板梁切口相磨的情况。 & e+ F/ @3 z/ {7 \7 ^4 o3 F. } ; h E! r# Q9 t. C/ P5 |, t(76) un-lubricated: 干涩/缺乏润滑2 V: b7 D3 l* D9 E0 e" N7 R Without lubrication resulting in friction, heat and wear. ; E% L1 M4 ]/ u( K, @ E没有润滑而导致相磨,发热和磨损。 0 E2 _+ n) k9 B, j2 T. h! s4 XFor example: After aircraft wash, all 3 landing gears were found un-lubricated.6 M2 F3 o- u% V) S1 O 洗飞机后,发现三个起落架都缺乏润滑。' m) N% Y% l# d Lubricated all 3 landing gears with aero shell 17 grease with reference to 6 r2 ~/ E1 B, _& Z+ \AMM---.2 h) ^: j/ D4 ?/ A 根据AMM—润滑三个起落架。: | v! V1 u8 U7 Q/ |3 Z / K& e6 ?" q9 x$ e% r' j: D& V (77) will-not-reset: 不能复位) K, t& q( Z8 [0 K4 ?' p Will not return to its operating(original) position.) j! X# N7 q! p 不能回到原来的位置。 ~; E+ c+ U, \" \1 C$ l$ q For example: APU circuit breaker will-not-reset.0 b7 X! q# g6 j9 S7 u! s0 a" Y APU跳开关不能复位。 8 c5 f# } u3 O3 X; V, ? Detailed inspection found APU circuit breaker faulty. Replaced APU circuit: ^7 m; A1 m8 i1 i( ~' R5 V breaker in accordance with AMM---.Operational check good. 6 O4 w1 X7 F h- }$ [. Q4 U详细检查发现APU跳开关故障。根据AMM—更换APU跳开关,操作检查正常。
作者: bluegate3    时间: 2009-10-17 16:38:16

gggggggggggggggggggg
作者: liu0705    时间: 2009-10-18 14:16:04

hao de tie zi
作者: maxkerry    时间: 2009-10-20 21:10:50

zhun me

作者: championking    时间: 2009-10-29 20:59:24

dddddddddddddd
作者: huhongyan    时间: 2009-12-3 18:09:40

资料很好

( m1 V/ W V+ t$ Q

 


作者: tantao    时间: 2009-12-8 10:45:56     标题: 好东西,看看

好东西,看看
作者: jmhuang05    时间: 2009-12-8 15:53:57

需要术语。。谢谢
作者: jordanxcw    时间: 2009-12-12 23:10:06

专业人士就是专业人士 为人民大众服务了 雷锋!!!
作者: slhan_05    时间: 2009-12-14 12:23:11

required   槽 spout 凹槽 notch   侧板 sidewall 凹坑 dent   测量 measure 把手,扶手 handle   测试 test 包皮 cowl   插钉 pin 保护层 coating   插头 plug 保险 fuse   插座 receptacle 报废 discard   拆下 remove 报告工程师 report to engineer   长桁 stringer 杯子 cup   超标 out of limit 比率转换器 ratio changer   超标 exceed the limit 壁橱 closet   超过 exceed 边缘
作者: jdj172    时间: 2009-12-27 08:41:29

谢谢楼主了
作者: hjhhm2010    时间: 2010-1-18 10:19:47

kkkkkkkkkkk
作者: weite    时间: 2010-1-31 22:00:09

lj;/k';J'olhn;klhjupilgtckdfulizkyg;oploiutyjrthrg
作者: 失速    时间: 2010-6-11 00:51:07     标题: 回复 1# 帅哥 的帖子

先顶在下载!!!!!!!!!
作者: ceaice    时间: 2010-6-15 15:48:00

 
作者: chaozi    时间: 2010-6-20 20:43:15

需要术语。。谢谢
作者: flycat    时间: 2010-6-26 18:25:31

THANKS FOR SHARING
作者: scylla    时间: 2010-6-29 13:07:20

好好看下啦
作者: qwuue    时间: 2010-6-29 16:03:16

感谢楼主慷慨分享
作者: guomai127    时间: 2010-7-12 19:28:03


作者: 空中加油    时间: 2010-7-20 23:32:00

好东西哈   谢谢哈!
作者: 空中加油    时间: 2010-7-20 23:40:41     标题: 作为机务维修人员我应该迈哪一步?

从事航空发动机维修事业的我即将离开学校了,等我的是步入社会的那一天。可是在充满传奇色彩的航空公司,听说有无数的机会和广阔施展才能的舞台,而作为将来机务人员的我应该怎么做呢,现在的我真不知道该将迈哪一步?如果大家能告诉我应该怎么做,进到公司又应该怎么做,我将万分感谢!!!!
作者: netwang    时间: 2010-7-28 11:37:49

谢谢楼主,看看
作者: lost0508    时间: 2010-7-28 17:06:00

看看是什么
作者: zhgq412    时间: 2010-8-2 10:24:16

这帖子要给顶起来啊
作者: nowfranchise    时间: 2010-8-13 19:56:01     标题: 43软4325让他一人同意呀

43塔32他4如同一条人影
作者: lxz_0502    时间: 2010-8-16 16:22:59

谢谢LZ~~~~
作者: xheleon    时间: 2010-8-28 18:18:35

感谢楼主发布资源!!!!!
作者: 半罐旋风    时间: 2010-9-18 18:03:48     标题: 回复 1# 帅哥 的帖子

顶。。。。。。。。。。。。。。。。。。。。
作者: fengxinghuajing    时间: 2010-9-20 18:08:41     标题: 1

好好学习,天天向上
作者: denglh26646595    时间: 2010-9-29 21:03:31     标题: 术语好!

术语好,好术语!
作者: hotisverygood    时间: 2010-10-4 20:16:22

寻找已久。。。
作者: willman888    时间: 2010-10-11 10:49:59     标题: 回复 1# 帅哥 的帖子


作者: danny    时间: 2010-10-26 15:29:09

upppppppppp

作者: wwe11    时间: 2010-10-27 11:40:36

我要下来看看,好好学习学习
作者: wgjinshan    时间: 2010-10-29 09:23:26

!!!!!!!!!!!!!!!!!!!!!!11
作者: 机场的风    时间: 2010-10-31 19:20:03

顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶 顶
作者: Lee999    时间: 2010-12-17 14:57:07

挺好的术语,谢谢
作者: kinran    时间: 2010-12-29 14:33:50

需要术语。。谢谢
作者: l200272    时间: 2010-12-30 10:31:22

bbbbbbbbbbbbbbbbb
作者: vicky51668    时间: 2011-1-13 16:39:39

谢谢楼主!辛苦了!


作者: wdswds    时间: 2011-1-14 16:53:12

VERY GOOD.
作者: gf2175    时间: 2011-1-19 08:14:04

不错!!!
作者: blueguard2007    时间: 2011-1-24 13:32:22

谢谢分享,看看
作者: artic    时间: 2011-3-1 09:07:45

sVVeervRWBRRRER
作者: annie    时间: 2011-3-3 14:12:52

多谢分享,楼主辛苦,谢谢!

' z1 F- W/ A" ~8 n, D: f: u2 I6 x

 


作者: flora    时间: 2011-3-7 14:31:12     标题: 看上去不错

非常感谢啊 应该有用
作者: jhchen_08    时间: 2011-3-8 23:37:28

感谢lz,,,
作者: RowanZhang    时间: 2011-3-15 17:53:55

This file must be the best
作者: 979199501    时间: 2011-4-9 20:06:32     标题: 回复 1# 帅哥 的帖子

民航网确实很多好东西,基本上都是帅哥的 ,谢谢分享
作者: guochun618    时间: 2011-5-14 20:30:22

楼主辛苦了~~
作者: sillycat    时间: 2011-5-16 14:51:44

好东西,顶!
作者: sunflower723    时间: 2011-5-22 13:45:33

感谢分享!!!!
作者: 淡紫色的风    时间: 2011-8-28 00:38:49

 很有用的东东,下载下来收藏~~
作者: 天若有情    时间: 2011-11-6 20:18:08

内容精彩,呵呵
作者: 苦行僧    时间: 2011-11-6 22:49:36

谢谢分享!
作者: SilentHill2011    时间: 2011-11-7 20:59:56

资料就要下~~
作者: charlieqin    时间: 2011-12-21 15:58:18

GOODGOODGOODGOODGOODGOODGOODGOODGOODGOODGOOD
作者: 徐卫东    时间: 2011-12-23 08:34:38

谢谢楼主,学习学习
作者: snowmantony    时间: 2013-9-12 10:25:11

这个东东真好
作者: jetboatpool    时间: 2013-10-29 22:30:48

辛苦了 謝謝
作者: 喷喷    时间: 2014-10-15 12:23:07

http://www.dailyedu.com/zhiye/hangkong/5165.html
作者: levis02    时间: 2014-10-19 21:27:50

谢谢分享 学习了
作者: yknet    时间: 2014-10-24 10:24:52

Thank you!
作者: dasfyf    时间: 2014-10-25 08:56:16

国际惯例~
作者: kuuga711    时间: 2014-11-6 09:37:29


& l5 s; }6 e4 [4 b' u$ T好东西,看看
作者: stellahui    时间: 2014-11-26 16:26:13

huguibnkn oihhnk
作者: Williamray    时间: 2014-11-29 20:38:08

下来看看 背不背再说嘛
作者: 你家大大卷    时间: 2015-8-27 00:08:56

thanks a lot3 D, {; W1 ?& _

作者: wang490502    时间: 2016-8-26 15:12:32

THANKS A LOT.




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