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维修术语! ^+ {) a7 u# B2 F
3 g4 W8 M5 C! @2 w) r
# R* Y g" Q' N! f" L. z3 G(灯)不亮 not come on 不可用 not serviceable( W/ s' R! P2 `
“工”型 type I 不锈钢 stainless steel% N% @7 `" |: Y7 {
APU 舱门 APU bay door 部件 part
4 l$ Z5 U/ A9 T& L, C7 d5 @/ JT 型件 Tee extrusion 材料 material
4 f' F" H, J. q! e t4 k& k阿罗钉 alodine 参考 reference
" k0 D6 t0 W7 u6 D! z, o& o9 W安全带 safety belt 餐板 feed panel6 k V: g2 A' T5 M# Z0 ^
安装 install 餐车 diner9 y. c, E0 r. A8 c- s% ^
安装座 attach fitting 操纵 control
, J! ]- V5 a5 W0 Q9 b! d9 w按钮 button 操作检查 operational& D$ b. w7 ]8 X* ?/ V
按需要 as required 槽 spout' m* ~( W* a; n% r$ Z7 f
凹槽 notch 侧板 sidewall
8 O3 _- c) ]- b: H: O# V1 h6 \凹坑 dent 测量 measure
: u! d# _% @/ }+ q8 ]把手,扶手 handle 测试 test' n9 U1 p: x% n' M5 b$ s/ o
包皮 cowl 插钉 pin
+ |) p; a/ G1 a: c! }. p% {- s8 B保护层 coating 插头 plug
1 P( `- G/ t5 d8 x; L& \保险 fuse 插座 receptacle: E% C/ N: N* n) M2 L
报废 discard 拆下 remove. Z* w& {: u' r' U, h! B3 U
报告工程师 report to engineer 长桁 stringer
9 a0 v4 t! X4 o! D* N杯子 cup 超标 out of limit" I4 P( I) c! K. ?; Z
比率转换器 ratio changer 超标 exceed the limit
5 c/ Y& E) _' `3 P. Q$ I壁橱 closet 超过 exceed e% B5 ]9 v6 Y% z& S
边缘 edge 超控手柄 override handle
8 V- d) ]* ~7 Y便于检查 easily to inspect 彻底修理 drastically repair
! g/ O5 f) m: b) ?- l5 Y变形 deformation (n) 陈旧的 worn
; K" | R' g- t [, r# b ~变形 deform (v) 衬板 liner
! M; e! `8 j/ ~" N: J& L* @变压器 transformer 衬套 bush$ u# y& U- y l$ }, q
标牌 placard 成型 shaping
- V( K' y+ R6 ^2 B3 M+ A7 ~& a标识 sign 乘务员 attendant
4 K2 z9 M3 e; C) k, r1 g) J& A标志 instruction 尺寸 size+ O0 l4 M6 u, P _* G+ }( H R2 M' K( I
玻璃 pane 充足的 sufficient
4 d+ @0 J C) s' ]( t/ j玻璃纤维 fiberglass 冲水按钮 flush button
7 {1 v' K/ D+ h$ ]# s" u4 f2 z7 B补片 patch 冲洗 flush
5 }6 O, k3 W, E2 i# c补片 filler 冲压 ram$ W- I5 `) b4 A) R6 i1 z( U
冲压空气 ram air 低压压气机 LP-compressor+ [" _4 i/ T: y/ r
抽油 defuel 底部 bottom
$ C3 i: c% r4 y8 B& R: X出口 exit 底盘 base/ {! O* \: r9 g b
除腐区 reworked area 底漆 primer, f2 x9 n1 w1 e6 e {" L( D
厨房 galley 底座(结构件) mounting+ H+ C6 H9 W: r
厨房烤箱 galley oven 底座(螺母) plate, F9 z# k# A, `& S
储物柜 closet 底座(天线) base
* n: d8 |2 _$ G7 h9 n+ g+ n处理 treatment 地板梁 floor beam k+ S) P0 l$ F8 }( ]- a
处理 dispose 地面 ground* a! D' v0 b6 F* k! Y
传感器 sensor 地毯 carpet
8 h; q4 O [/ R3 N! w. ^' S传输 transmission 第二层 two layer3 |0 \$ N1 q3 I# f- D, c
垂直的 vertical 点火电嘴 ignitor
: X3 h. a7 p& v! K# W x存放处 location 电路 circuit
/ w5 J9 C5 W, u( X错位 migration 电门,开关 switch
5 G1 ?/ R. o- I搭地线 jumper 电气 electrical$ j0 {' o& W4 C: H& {9 A+ I: l6 R5 m
搭接处 interface 电气接地 ELEC bonding5 g8 U0 v. e' j8 x" \! |5 s) ?
搭接片 splice strap 电源通电 power
( e% D3 Q+ W: D搭接片 splice 电子 avionics. [2 r7 W9 k2 Z$ Z9 N4 d# {
打磨 blend out 电子架 E rack: Q0 E7 u% Q- I$ f, F; k
打磨片 blent disk 电子架 shelf) E" ~' H! w* p
打止裂孔 drill stop hole 电阻 elec resistance7 H, [! e3 X, o5 o8 K0 [. X
大翼 wing 电阻 resistance+ S; z2 ] I' p9 n2 N: R
大于 more than 垫片 washer
8 N- v4 P6 z8 P. g8 C* H# N9 T8 p单向活门 check-valve 吊仓 nacelle
7 i8 I8 [! B v# k弹簧片 spring seal 吊点 mount cone
6 G- p+ c8 T8 K: M7 O! @- I挡块 retainer 调节 adjust
! `$ ^8 a5 ?% g: P) }0 x挡雨板 fender 调整片 tap" |) Y: P( l0 _9 T9 m2 u3 m1 j
导线 wire 顶板 ceiling
0 q5 j9 E8 A. u0 t9 M灯 light 顶部 top
) k' }( M1 ]* `# b* M" s灯泡 bulb 顶部 overhead2 W" R; _- G: @, P
灯泡 lamp 定中弹簧 decentering spring
# \+ v x& ?1 x6 {灯箱 light case 丢失 miss0 d+ |; a2 b! w# g
灯罩 light lens 堵盖 plug' M% [) r! J8 ]6 U1 C0 w* Q
登机门 ENTRY DOOR 堵塞 clog0 T4 d N: M& U6 }
端头 ending 腐蚀 corrosion4 J0 q! V7 B; c- b/ D1 W
段 section 腐蚀 corrode
% H0 _( d0 C9 F4 [$ `5 c |9 m4 u断 break 附件(大) accessary
% g. L+ @, m" j+ s l4 u& D断开 disconnect 附件(小) attach
7 H8 T, K9 _1 }: y! E6 ?. O/ |3 l! Z断裂 fracture 附近 adjacent to
+ a8 r4 w' p7 ~7 C- O断裂的 broken 复合 complex
/ N4 D( J, o9 y T" ` S1 ^; i断丝,磨损 fray 副驾驶员做椅 first offcer's seat* X! z8 }4 l( u4 X
锻件 forged part 副翼 aileron3 Z0 e& B9 M- ]1 k- v; b
多处 numerous 改装 modification
9 m# }! E; \6 m' ?1 y* ~& d0 _发动机 engine 盖 cap; d9 B% n* _# i: s+ J3 L( [
翻新 overhaul 杆 rod
' P7 I. [4 r* L2 a. D$ C$ e1 a反光镜 mirror 钢丝 steel
; [$ b2 F$ S$ U J+ i方向舵 rudder 钢索 cable2 `! E3 K9 W8 z# ?$ T( a+ |7 y
防冰管 anti-ice duck 割除 cut out4 w! Q7 ~. r7 C2 X: [6 t
防腐 corrosion-inhibition 割断,割下 cut off
. |6 d1 R& M5 Y' O防静电 static-free 隔板 clapboard,partition, W; N* [% W5 M) Y& V
防磨条 wear strip 隔框 bulkhead
0 N8 m; Y, q5 X7 V/ ]6 \防滞 antiskid 隔热棉 insulation-blanket& ?4 E% S# [! L2 s
防撞灯 anti-collision light 隔栅 grille
# w3 q: [8 }! W+ q; G放 extend 各有 each has
9 A1 q/ z! m0 b5 x, H8 u! B放电刷 discharger 根据方案 in according to disposition
6 a4 A9 ^9 A' ]分层 delamination 根据监控指令单 condition monitor order…
6 b( c( `) B' D% a. ?# q风层,脱胶 delaminate 更换 replace
- N0 P% _" e: E% _1 |+ J0 A1 ~风挡 windshield 工程师 engineer \; I% B" R$ u
风挡玻璃 windscreen 功能测试 functional test; I& b$ O8 ~: W2 [: M, J
风扇整流罩 FAN COWL 功能检查 functional
( @, y7 X: i& {( v9 o$ K* _风蚀 erode 供应系统 feed system5 A n) x2 ~6 q- D0 g! n) i
封严 sealing 供油管 OIL TUBE; X3 X, s3 h' N; A9 v; F s/ b
封严条 seal 鼓轮 drum5 _0 Y0 D3 P6 u+ c/ n$ u- m
蜂窝芯 stagger core 鼓起 bulge
G8 `- W2 @9 y7 t/ T扶手 armrest 固定 secure' U2 f4 e7 g0 @
扶手盖板 armrest cover 固化 harden
4 m# i; n1 ^) f! S辅助滑轨 assistant track 固化剂 hardener
2 T! X! b3 e5 j+ v& K1 }5 ~; I& ~故障 fault 划痕,划伤 scratch
& b' [: p0 S/ ^" Q" U. N刮伤 scratch 划窝 countersink
% Q/ Q Y5 _, ~7 B ]; r+ B' i挂 attach 环氧树脂 epoxy resin
' H) C& a7 m) ~3 R) D挂钩 hook 恢复 restore
& ]; I. @: ]" @& Y/ g挂上 hang up 活动窗 slide window+ Z7 H' c0 S. C7 |2 W# T
关上 close 活门 valve& x+ c2 c _8 W% H
观察镜 view glass 货舱 cargo compt9 s- _* y. @0 A. Y, X; m% R
观察镜 viewer 机构 mechanism! M) d$ g9 p' p% z! E- s2 A
观察员 observer 机身 fuselage
8 w5 P I7 ~6 H+ a观察员 observer 迹象 mark
" g3 R" {; ]6 i2 \0 v光滑地 smoothly 加强 doubling- q2 a+ r% V6 N2 _+ B0 n. D# {
滚轮 roller 加强件 stiffener
+ I; Q- c" P _4 @7 p* J5 W) g过道 aisle 加强块 doubler6 d9 m3 a5 W. J
过期 expire 加强肋 intercostal
4 e5 ^8 C2 W8 V8 M过热传感元件 overheat sensing element 加强修理 reinforcement5 n" J+ R- r+ F9 R/ n; S
海绵 sponge 加温导线 hot wire
. u; U) [( [- ~焊接 weld 加油面板 refuel panel
, R$ O% o& ~: {. l焊条 welding rod 加油站面板 fueling station panel- E: F3 ^) L' H2 U; r
恒速传动装置 CSD case 夹子 clip
7 x G; N7 G ]/ t7 E横梁 latitudinal beam 驾驶舱 cockpit
) M2 q( m8 a8 _: K1 S% t横向 lateral 间隙 gap7 n, f7 {% T% G0 z ^. |
后端 rear 减速板 speedbreak# B! p, q/ @4 O- X( v# E
后缘 T/E 减压器 reducer
@9 b/ ~% }/ S; N% ?% \厚度 thickness 减震器 shock absorber
. @, U' r" w+ h7 j5 \+ D( p呼叫灯 call light 减震支柱 shock strut% i5 c' S6 |2 e4 k/ B" w' G
护板 protect strap 检查 inspect" m: c" ]# k1 o- f! U+ [2 W D
护目镜 goggles 检修门 access door
+ g7 C+ e5 Z" I9 T2 m护罩 shroud 胶 sealant
n4 c/ t. C2 _* L% r% a3 i( ~! h花键 spline 胶带 tape
4 P" G4 p! R; ]6 }滑轨 track 胶垫 mat2 t; G, l4 X6 V) ~" A8 p
滑轮 pulley 胶垫圈 rubber washer, i7 b% Y: S9 k% j/ \4 P
滑丝 cross thread 胶套 rubber
8 ]0 F; t J8 i- V7 O滑梯罩 slide cover 胶纸 tape
6 C: K* K8 z, M w滑油量 oil lever 角材 angler
( M" v$ [7 N2 N& T角型件 angle shape 喇叭 megaphone
* y; i+ z0 G0 `$ L+ y, U脚登板 pedal 拦网 block2 f" P3 y( T. N) t }
铰链 hinge 牢固性 security
8 }( p* J# ?3 J/ b) L/ O- B6 c' `* W接地点 ground point 老化 aged7 T1 x- u- T% ? K$ d+ b
接耳 lug 老化,退化 deteriorate6 X. J, m& M1 x E4 d$ R( X: C
接通,提供 supply 雷达罩 radome3 m' |; A0 ?+ @; I+ G. J- Q1 P
接头 fitting 肋 rib
& E& L& K3 y7 L5 r7 t0 l7 O接线管 splice 离合器 clutch
* f3 `2 L5 R3 c3 Z* z6 S2 V接线片 terminal lug 立柱 pole
+ R6 o1 l6 e d2 n结构的 structural 例行 routine
! y2 n+ w: I' f+ r; w金属屑 metal particle 连杆 link, J& u& Z8 h8 o$ u
襟翼 flap 连接 attatch
" N7 `* F* i( K+ n2 ~2 a) ]) [( e紧固件 fastener 连接板 attach plate
+ F& z: Y; ]* E) K6 _) {& I紧急出口 exit 连接口 coupling ' L# e( Q1 e( v/ Y/ |/ X
进气道 inlet duct 连接销 lockwire' Z7 x* ]% n5 }+ Q) {6 c0 g
进气口 inlet port 联锁 interlock
$ E. R* p# \ \7 T& _/ o径向驱动轴 radial drive shaft 裂 crack
" ^) t( R4 L& X# e. u静电,静压 static 另一个 another
% @) h6 l; i8 x救生衣 lifevest 龙骨梁 keel beam' X8 r; Z) v9 A: o
咖啡壶 coffee maker 滤网 filter
& J0 x( W$ [8 r8 A0 a卡箍 clamp 铝箔 foil
! \5 q0 ]; G& y: q: @! v) L卡环 collar 轮舱 wheel well0 f5 `* p+ `0 x
开口销 cotter pin 轮子 wheel & X5 I! h" m1 f8 O; g
靠背 back panel 逻辑 logic
+ [ L3 R/ u5 c$ ]壳体 case 螺钉 screw
1 z3 r Q8 U) r$ ~# i9 z可用 available 螺钉孔 screw hole
8 A$ ?0 H V9 s9 j0 l' P; ^客舱 cabin 螺杆 bolt
/ U/ _: a) H7 Y5 A# H! C; N& c空气循环隔栅 air return grille 螺帽 nut$ F5 X" w! B. v/ \
口 port 螺套 insert
. i$ i+ Y' _+ D% N1 M+ V5 ?块 piece 螺纹压伤 cross threading. [4 H+ q0 g2 D2 c2 i( X
框架 frame 马桶 toilet
% e) B6 U9 e) k& \1 K' p8 P垃圾箱 dustbin 慢车 IDLE
; j3 a* S8 }# w9 Z拉紧 pull 毛刺 bur
9 N+ W) Y/ @$ u( X1 r B毛胚件 rough 破损 damage
4 v5 w! q: Z3 G4 ?! l$ L铆钉 rivet 漆层 coating
1 q) b, G# g+ h$ e z门槛 sill 其中之一 one of
8 p; m6 c+ p! G5 @$ z门框 door frame 启动活门 start valve" t) c; v) \" g3 D- T6 j* E, q% V; M. ?
蒙皮 skin 启动机 starter3 _& v6 ~+ U, h3 u! o
密度 density 起落架 landing gear
, h! y, z0 d# P密度计 densitometer 气瓶 cylinder
: \; r; o9 L3 f% w3 I面板 panel 千层片 shim- t: ~" ?& I! l* V& J! S
面漆 enamel 前厕所 fwd lav! h: h/ f% e1 Z5 Q9 r' x
模糊 blur 前缘 L/E
" M* b0 \6 \1 w" M3 J8 G模糊不清 obscure 腔体 cavity/ c8 q! }$ ]1 {
磨损 wear 墙纸 wallpaper
8 ^' \2 _" N+ Z7 m# [: e目视 visual 切口 cutout$ }2 N3 m6 r" e/ n! Z1 y
内侧 interior board 勤务面板 service panel1 p" n9 L# S3 M# }
内层 inner 轻度 light
, t! k3 T o5 b |- n+ r" J尼龙搭扣 nylon fastener 轻微 slight
- m6 t, B% T( p尼龙扣 nylon hook 清洁 clean
( o, s1 Q9 x# ~3 e+ v, p+ _拧紧 tighten 清洁剂 cleaner
$ e, R5 j' N! h( }2 |$ o6 |7 P- ]( q扭力管 torsional tube 区域 zone2 r$ J" \) I- i5 n- k4 Y& e
扭曲 kink 曲柄 crank" Z2 Z/ N7 T9 R2 b/ M8 X
排 row 去除深度 remove depth
! e: g* u" y0 G+ |0 t3 Y排放 drain 去毛刺 deburr4 u: U9 p/ o' @# J; V
排水槽 gutter 缺口 nick
3 q) q+ a5 p9 [: o! e排水管 drain tube 群边 skirt edge
$ f: H5 {/ O; V* U配平 trim 燃油 fuel
- U! {# E0 z9 |) \喷漆 paint 燃油泵 fuel pump
& D6 j' c1 P* ^) j; W g' `( X% Q喷砂 sand blast 扰流板 spoiler
f6 N/ L; E* W皮带,片 strap 热水器 water boiler
# t; k+ B3 R: @, \* w: x皮托管 pitot 人工行程限制 manual travel limit( b0 C) M- v3 F0 ?; h8 P
偏航阻尼器 yaw damper 日光灯 daylight lamp) `( Q F, U( B/ \$ ^1 U
平衡机构 equalizer 软管,软护套 hose+ A/ l9 Z/ B8 V6 A) v3 k5 p
平滑的,使平滑 smooth 润滑剂 lubricant
q. p9 j# F) A2 U平行 balance 三段 three section2 e. R. x! k2 F; ] R
散装 bulk 逃离滑梯 escape slide
; d+ R% e. r" l8 e0 V8 I# R刹车 brake 天花板 ceiling
6 f6 |+ e3 B6 @1 X上表面 upper surface 天线 antenna
, z8 t0 R! ~- _4 Q' R; T% [) P上述 above 填补 fill
, b& a' l$ Y6 a! _深度 depth 跳开关 breaker
+ X8 K* W2 _7 t* e- q' _渗漏 leakage 凸轮 cam5 |' j8 T( ?! S* c" V8 w
升降舵 elevator 图纸 DWG
' L4 O6 {% U5 A. b, Q绳 rope 涂,粘贴 apply0 l2 S) K: Y& ]4 v& W H' v% o+ M7 [
失效 inoperative 退漆 strip paint( r1 _8 x/ R# U9 q
湿安装 wet installed 退色 badly faded( w& E' }- ?, _' E5 U7 u
试车 run up 托板 pallet* k* i$ X0 |% |- ~1 o4 Z
释压 pressure-release 托板螺帽 plate nut" }& n i# x/ N; V, \' {2 `: ]: Q
收 retract 脱开 disengage
" n/ @: `+ X. l9 b- H% t% q0 @+ L收发机 tranceiver 外 outer
! b$ T2 Y9 b3 n手柄 towing lever 外侧 outer board5 ]5 J% C/ v6 L* @6 u1 W
手册 manual 完成 complete
! A+ e8 Q3 R. k o1 x1 b- v手电 torch 完成 finish
7 W# M6 {; |) r0 `' ~3 Y% q( Q6 ?手工 handwork 万向接头 gimbal
. b% Q5 l& p3 g1 K手提的 portable 维护 maintain' R; G" a' p: K: r* r
手提灭火瓶 extinguish bottle 尾部 tail
" M% B3 {, O" `4 z' Z# R6 Y树脂 resin 尾舱 tail compartment4 X8 E/ e/ H6 ]
双倍 double 尾喷管 exhaust nozzle
) K0 L6 k- ?, w" @& r3 z水平安定面 horizontal stabilizer 尾锥 TAIL CONE2 Y5 L2 I- q) |9 Z
撕裂 tear 位置 locate( W P; w+ `* A" }" Q7 x
伺服 servo 温度 temp
' I+ g9 V4 U: d$ g X松动,松脱 loose 涡杆 jackscrew) H% b. g2 |9 Q/ {3 g7 U U @
送修 send to repair 涡杆 worm bolt& v2 p; W/ Y7 y" S( |
塑料 plastic 涡轮 turbine2 f- l/ C Y$ X, ~- U% B* b
随动盖板 hinge access door 污染物 contamination
7 @) `5 ]/ s, G& H' @+ t锁 lock 污物 dirt" c1 y3 u8 J5 O) K! a0 Z- E
锁定 lockout 无线电高度表 radio altimeter0 o1 y3 ~. M- [4 @- e
锁扣 latch 稀释剂 thinner+ g8 \9 l! ^) o# ]+ n; q
锁销 lockpin 铣 mill ^ [9 V/ B) J) ]! ^3 N
系统 system 溢出 spill" K1 F. ]( T( x) q3 Y/ u1 L# U
下部 lower 翼尖 tip8 j3 M3 ? y5 f! y( n
下角 LWR corner 翼间 wing tip1 V2 R: R1 f, X& Z5 {3 @
下位锁 downlock 翼梁 spar c+ @, x+ n' T7 q4 A4 r- u
下陷 concave 引进 introduce9 N r F, m2 d$ D
下缘条 chord 引孔 make guiding hole% o) u2 N+ q/ e& M, ^! Q3 T
纤维板 fibre board 引孔 drill hole/ T3 E2 x' o& \( m
相关的 relative 引气 bleed
, q% H; ~3 N% H; X8 b6 k% r: N相磨 chafe 引气管 bleed hose( k% x- ]! e) \4 d* [, s
消音板 accoustic panel 应急 emergency
# H( G7 K G# n9 P% x7 ?0 t销子 pin 永久性修理 permanence repair. B+ Q8 G' }. D9 b A* [9 n
楔形块 wedge 用…填补 fill it up with…3 }7 @ o8 h9 y, U3 A/ q
信号灯 annunciator 油封 preservation" H- d J: O5 {% Y/ K+ X/ c1 {* G' T
行李架 luggage-rack 油箱 fuel tank: Z. S/ q0 p6 g4 D" m, _7 D6 V
行李箱 stowage 游动梁 walk beam. r( I. T) v. @
修边 reform 雨刮 wiper
/ k, \9 A [, Y修理 repair 语音记录器 voice recorder& e* i( ], u, ?+ h6 R1 U! W
锈蚀 rust 预冷器 precooler
: {( z4 d% I5 m- u循环 cycle 预位 ARM1 U( M7 v2 j% G2 N8 g3 D) e8 W
压紧 gland 原厚度 original thickness
; q. o; v1 a% R* {0 d/ E7 I压力通风系统 plenum system 原来 originally
" p8 e( G' V2 e' T- }2 K压条 cover 阅读灯 reading light& L B* q6 E6 t# | F& [
严重的 serious 允许损伤 allowable damage
' R9 ~0 s; S4 g- @. e阳极化 anodize 杂志袋 literature container
: e% _# l- {- M' @/ [ x氧气 oxygen 载荷调整 preload adjust7 X( F4 x5 h1 I* x
氧气面罩 oxygen mask 再循环 recirculation+ E" k0 B, n* M, z
液压 HYD 在位 be in place
% a9 v+ G9 t$ |# o) ~! r液压泵 HYD PUMP 脏 dirty# m2 g! F7 a0 p4 b
液压管 HYD duct 增压 pressurization
% ]2 f; _( A1 t+ N1 N9 T2 Y9 t: ~液压系统 hydraulic system 增压泵 boost pump
) O/ l/ E% f( I# { B: D; P1 O液压油管组件 TUBE ASSY 粘贴 bond
B4 F* p. S5 W7 F- z- t8 l! a' X液压油箱 hydraulic reservior 照明 illuminate
* l; w4 ]+ I) ]8 }4 T移到 move to 遮阳板 shade
% ~: ]" b# v" I4 S真空泵 vacuum pump 自动刹车 autobrake7 r6 O8 q# ^# I
拯救 salvation 自动油门 auto thrust0 q: b( c5 p+ V. l; c0 e( h5 A( E
整流罩 fairing 自锁螺帽 jam nut; y2 X2 g+ i8 ?3 {. I
整流锥 spinner 自由移动 move freely6 V* j2 n4 g+ k$ Y3 z; i0 b: X9 U
整形 rework 总管 manifold7 Y1 ]8 Y- P1 G) l y
正常 normal 纵梁 longeron5 S5 L* d2 {3 B& q5 ~. J
正常位置 normal position 纵向 longitudial5 ~2 D- d7 u7 b9 t' B
正驾驶员座椅 captain's seat 阻力支柱 drag strut
, {0 p/ T7 t5 u# H+ u: X之间 between 组件 assembly,pack
! a0 A$ s1 S( c( h* e; K b支撑架 bracket 组件(电气) unit
, M' G* h5 y8 D) j- j支撑座 support mount 组件(机械) assy- A/ |/ }" J7 f
支架 bracket 最薄 min thickness3 V4 B6 m4 i1 D! }) ?
支拄 support 作动筒 actuator
# W1 T0 [# |+ e T止动固定块 stop block 坐垫 cushion6 B% m% h; k4 G, S+ ]4 Y
止动块 atopper 座椅 seat
5 `9 ?1 E- |$ r; [- s* A指点信标 marker beacon antenna 注意 caution* l/ a4 N+ ]* {2 f6 D* ]. b0 h
指示 indication 转接器 adapter* ^' h; f$ ^, u: T. _! G3 {
制作 fabricate 转弯灯 runway turnoff light7 ^+ l; h% \- V% ^" u
中厕所 mid lav 转向 turn% z: T, E; t1 a! D) u
中间,中央 center 装饰条 trim strip
9 ^+ v2 O0 p0 h" q周围 around 准备 prepare% a& O9 J& u( [# \
轴 shaft 着陆灯 landing light# O4 Z, o( u6 S1 _: w# b
轴承 bearing 自动关闭 auto close! O' m1 b6 ]) y; s8 a' m3 {
主轮 main wheel 助推机构扳机 power assist trigger7 E/ ~; o! P& A: ]
- a$ A( e6 s+ K1 P! I, P9 S. ^$ D: V1 w3 o
5 J! z8 g0 J- f7 s
. t$ W F4 s- g
7 h. l* j3 ~7 i, C+ z. ?/ X1 @
3 j% @2 c9 U6 ?; i, G3 V7 M# G6 x k4 r7 Y" ^5 J2 Q% d
9 H1 x* b p! z3 C) V
' p9 t& H2 a: |
# n- m3 \6 f* f; G! q! B: r$ r4 o# e( X) I4 f
8 B6 V+ \5 @1 r, t% l
: _' G% q2 B9 J( N7 v
" h4 \: U& A' N9 `( s4 ~
9 u+ n6 T. B3 r2 v( m: C' R9 l! p- F z5 }1 l" B; l. {+ Q
4 J6 a2 H" D# ~# A- j& @1 [ J
9 ~) Y3 ]2 `! B9 A9 v8 N4 p t2 O9 B& O8 c) p; ^# ~' g
# @; X4 z- k5 u/ N
& o w- g* Y+ R! [; q! P$ W, E" h. W8 U. A- V
~& E9 f& G( R! J$ T) f/ V% P Q
" r1 n1 F$ `0 T3 R' Q6 C5 e; h, H5 R, C5 L& n. i- c2 J4 h
/ \6 g ^' i- t9 }! L: n; o
, ?" }5 ^; ^/ \. [6 @* R" v) b
7 X1 z8 D3 z' ]* W: t2 _0 ^' R; f2 W. l- p4 E
I; O, O' O+ B. t+ h% j j1 p0 ^" i: O* ]# x
7 T$ U0 a* }1 l" w- K! {0 J
Categories of Defect
# b7 A; L* |% J# s Categories of defect depends on experience of maintenance practice .In this manual, the default+ r3 g1 R. {! C, X: j& M1 U
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. 4 {' W7 B+ G' s' d: u$ o. D
缺陷分类
9 {: _5 P: w6 k% j7 [ 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。
/ |6 A; f0 {& V1 K
. i; y: Q, p) D/ j9 x3 R* e1. Common Structure Defects Terms
T9 `" S7 M/ G, m# `结构缺陷术语1 z, Q% T% S1 n
: ?# d r3 _' W$ g3 Q7 J凹坑(1) dent 1 _6 `/ j* f0 J+ G2 m0 ?
凹槽(2) notch3 }7 j/ A8 v( |4 H
变形(3) deform: @: x0 M7 k3 o
划痕(4) nick
1 G' ]0 l/ [) C3 o5 H k点腐蚀(5) pitting
" F9 X" y- f- ]5 M断裂(6) broken
! x# L- W! c/ H6 T! |7 T腐蚀(7) corrode
. M/ \# |/ Y# w( p, x0 |7 Z1 J划伤(8) scratch4 K0 b# b- \" F7 ~* M; _) l
裂纹(9) crack
& y8 ?* F+ Q% @: F# J毛刺(10) butt1 Z6 `& y. Z O* P: L$ |; r
磨损(11) chafe5 I) w5 \3 R3 `
凸起(12) protrude
# ]9 ^/ ~$ `+ \4 R% m' e; F, m3 ]凹陷(13) sag. X/ n* s: V3 R. e
粗糙(14) rough
3 N) j# _$ x$ X3 U0 i6 Z漆层剥落(15) finish missing
+ q/ O& s' |5 |$ W0 e; |1 R3 O5 U褪色(16) fade
& l) @# N. j$ `& ~积水(17) entrapped water3 l [* M& W# x
$ A" X9 W$ `' y2. Common material defect terms \4 Y* t% H" Z$ c. e2 d8 ?; N4 a
材料缺陷术语
0 G: @( d9 B- } Material is divided in two categories: metallic and non-metallic.8 }& B, W& d3 i+ z5 A8 \# Z
材料分为两类:金属材料及非金属材料
2 ^ H% c T; c8 F
6 ^, e/ Q' r! ]6 P6 S% ` 1)Common metallic defect:
! t, ]: t* r1 ?8 g; D* V& ^ 一般性金属材料缺陷:
/ T0 b5 W! F8 F7 v6 G + A% `8 B6 V1 n6 i
氧化(18) oxidize
9 Q) P$ |8 n6 e$ i4 ]7 Z 划伤(8) scratch% h2 Z5 S# h9 R# u$ g( i
扭曲(19) distort
5 b) S% ^' j* a( D, Q# c 跷起(20) not in contour4 ~7 E3 `8 m" ~% A; o
穿孔(21) puncture0 Q1 H0 Q) E: J1 {, |/ y' P
碎屑(22) chip; n6 o, Y/ E; i: ^, Q0 }
腐蚀(7) corrode
! s) x9 ^* N4 m0 t 磨损(11) chafe
) v& }! U+ s) q9 [变形(3) deform3 m1 Q6 p# h6 Y: g# I% }5 B
风蚀/风化(23) erode, x- G8 e x7 ?9 v/ k0 Y
裂纹(9) crack
. f! o, i6 a3 J) C6 ` 2) Common non-metallic defect:
# O3 w. s i$ h }/ J一般性非金属材料缺陷:
! A& G8 [# R( i ~ . H4 J- S* t. Y% i' w. O
发霉(24) mildew 1 j0 n% o' R% {/ B9 B
分层(25) delaminate/ h& N' F) J! F% I3 ] d: \
风蚀/风化(23) erode: v3 e7 [/ ~3 v) J% b6 e6 {
裂纹(9) crack
& i! v, `& ]' b/ i' w# h0 W* g7 _老化(26) deteriorate
. M w6 T6 \7 _! X# I7 k起皱(27) wrinkle
; I6 S. Z* i/ Z9 w9 E6 W. }' u/ X受潮(28) saturated- z4 z& c6 u; L: z: y' A
撕裂(29) tear I# q) _# x, [$ x; h
穿孔(21) puncture
+ W# n9 j. g1 M& r变色(16) fade: n7 C$ E5 p/ S
陈旧(30) worn' l& b3 Z/ F% _: j9 c0 d
脱胶(31) adhere
) U- G) S% u% s ~! j" d
; H5 c- p* }0 C3 e E# ^& z3. Common part component defect terms" f; O% x. e% C7 K3 c' z
设备及零部件缺陷术语2 g! j6 M3 S$ Z+ m
Common part and component including : Plumbing, Wiring, Mechanical linkage, Fastener and Miscellaneous.7 y( N% ^- o. [& T: I9 o
设备及零部件分为:管路、线路、传动机构、紧固件及其他。
- ?' D( s; C1 R6 n1 b7 z) W
- T' }5 A7 a# J- Z0 X7 Q" p) {1) Plumbing defect 管路缺陷
+ u6 v) P- W2 G0 n6 ]3 p ! r1 L8 h& }) I( C" { e
凹坑(1) dent
e* A( d9 _: P! g' {7 g5 @爆裂(32) burst, I/ k- Q, { l6 X$ K8 i( \ m, M; ^
擦伤(11) chafe
$ J- G# D& y ] T4 U3 r- h滑丝(33) cross thread p. G5 H, ~4 Y, I
扭曲(34) twist5 m7 i! ]- D1 \, x' Q2 y7 U
渗漏(35) leak
. F* L2 m4 i7 a" M- X) c堵塞(36) obstruct : f5 P; U$ |- R/ i6 d
3 F: q! W$ q$ h2) Wiring defect 线路缺陷
# S' ?+ b" m% Q2 B9 F & v1 L% t6 h, y: {9 o' f6 v
腐蚀(7) corrode
1 Y2 H! E0 |, X. G, }3 e9 z; F$ y磨损(11) chafe3 \+ y" R' h) H6 ?3 i. u
相碰(37) contact
6 v- q% g+ G6 ~' C) D# @断丝(38) fray
7 D T* m; i4 w( z6 P; S! f( ^熔断(39) fused, |+ S" K- T* A" ~
弯曲(40) bend
5 E6 y7 } l, V" r: U
8 U& `/ H; ]; N+ `( j: Z3) Mechanical linkage defect 传动机构缺陷3 V$ o9 ]3 ]; Q# N. u/ g% t
& S: t, S: g7 y$ R/ f# z5 z" D# ^断丝(38) fray " r, L$ D) T3 S1 U, V8 A( c+ B
松弛( ) slack
6 N* x. z- B* h; E. `/ p扭结(34) twist; t! w- c# N, K2 G
磨损(11) chafe- s; g/ w9 A: c2 g- H; B
脱开(41) disconnect1 z- z; e* k' a7 x' Q
+ U# N4 S& p7 b' ^! |, Z3 q4) Fastener defect 紧固件缺陷
. m8 B; N4 a Z/ Q9 G7 ]
' J/ T; s! K3 E" b# W4 s( d4 _$ g 丢失(42) missing
6 D! v6 `' ?0 C7 { 松动/松脱(43) loose
7 x* G& V. u8 X 腐蚀(7) corrode1 g, q+ H/ S! q- Q" [
磨损(11) chafe
/ ]0 M; Q: ?. a3 v" X% z u 未关(扣)紧(44) not secure
m. ~% U/ ~, ~4 }+ x
0 r Q4 z$ ?4 d R+ y4 B5) 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. ' g* A5 H6 d& s7 G+ Y. [6 C
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。9 S. l, I( b+ P% M" B
: U4 L! M# D- z$ _7 _" e! S4 L
a). Sealant 封严: P- x, g0 Y5 ?8 n
: q0 ^3 t, F, T( R$ y
脱胶(31) adhere0 V/ N3 b4 V! ^( t N: q6 }' W
老化(26) deteriorate
# S' H6 s6 O% ]. y# ~# [ 不均匀(45) inconsistent
6 s! r( i/ |5 B: P9 l
: |' J# Z0 L8 D) E: o& n* z b). Wheel Assembly 轮胎- `& h9 I' Y4 ^' q# r
见线(46) exposed cords
) [6 V7 J" f! j. h; o 磨平(47) bald
# t+ ]& m0 J9 T6 u- P4 b' z a" e 扎伤(21) puncture* c6 }+ K4 \% y# q( g! e5 d
气压不足(48) insufficient-air-pressure' n4 M. o( o8 s- X, n
4 l% i) u; a d4 F1 d c). Life Limited Parts 时寿件
! P9 C% U. A- l2 k9 E 2 |5 \6 s- [4 P) e
过期(49) expire
8 ]% s2 T& c" A0 H, W, D( ^ h ' z# u- z2 z8 N" R. S" F
d). Placard and Marking 标牌/标识1 v* Y; U, J% f4 M; J
+ G D* w$ L* U ~! c
模糊(50) illegible. S# r0 i) D& a. ^
缺损(51) damage0 v4 a: }! M6 B0 n3 O1 ^3 q( }& F. z
丢失(42) missing
" L$ @5 z4 B5 D8 T翘起(52) lifting
e* O; e( i( ^8 [/ b/ q 8 A8 H" O9 P r7 z1 G0 y. W
e). Slide/life Vest 滑梯/救生衣7 E( M' w3 Q. A, d( x+ M, x! t
% p. b( x9 q- O; L0 A* G 散包(53) not properly packed
6 Y: V( [+ f6 ` 变形(54) not properly sealed* G( D7 m u M* w% I
7 Y5 k: J( x6 { b8 s$ S
4.general defect terms 一般性缺陷术语
, [$ J9 A3 n' i' r. @, M! |+ S! I
1 o/ ~5 o( _# _: T* U8 V/ ^6 `2 w 脏(55) dirty* N: D* i+ n3 M5 q
陈旧(30) worn2 n) n& g: a9 D) |) J! z% a2 \
断裂(56) fracture
: M& u6 A* i8 m P 磨损(11) chafe ?( B# a- J( f* J9 L2 n) ~9 n
超标(57) exceed-the-limit
5 R3 U& b4 y: i* o' @, ~' d+ ^3 W5 X 丢失(42) missing
, k" }0 W9 F; P* k# z; V) b8 j6 v 腐蚀(7) corrode
7 z+ i0 z/ R2 K/ G! P7 R7 s 裂纹(9) crack
M6 h: Z* y& B+ b- w 空行程/无效行程(58) backlash
; I- e+ E$ r5 P1 o% N8 w 卡阻/阻塞(59) block
$ [+ d5 V4 N* T' c7 _ 鼓起(60) bulge
- v& v6 q# v7 P0 B; i2 K 污染(61) contaminate
# p9 G/ d% {. Y" w, E 不一致(62) disagree
) C! l( O2 o/ }, W; s- q6 _ (电池/气瓶)被释放(63) discharge
3 Z$ H4 ]. d( M' T, U7 ^ 装错(64) dislocate
3 y' `8 t& ^, Z7 o4 G 失效(65) fail
8 B5 N0 V$ s, X/ x1 \4 g" { 摆动(66) fluctuate2 ]/ G0 h2 `8 z( W
抖动(67) flutter
8 X( W3 q% t2 E0 O i; ^ 不够/不足(68) insufficient' K& p$ l4 _" J. o. n: C7 q2 {
不工作(69) inoperative
3 `1 ~; S* { z (不)亮(70) (not) illuminate1 N: |2 | d5 F" ?/ B
干扰(71) interfere: ?2 @6 m+ B4 ^
扭结/缠结(72) kink
. m6 H3 R% Y5 u1 Z+ j& U* c8 C 走向错误(73) misrouted( ]' V$ A4 V" H6 t: b8 F- W) u
漏装(74) not installed
& v0 q* x2 V$ b% E* i8 L0 ?/ { 相磨(75) rubbing
4 w9 L* N0 |& c- J; R 干涩/缺乏润滑(76) un-lubricated
, S, K! X3 r3 q: e" H9 J 不能复位(77) will-not-reset
, r& z0 Q( r1 l- @3 O: n! b( `
6 c0 Q$ a7 c. j* b& W( t7 |' y (1) dent: 凹坑
1 D: |1 L6 R- L$ M1 Z: [A depression in a surface caused by pressure or impact.8 o/ Y6 }2 Y5 L" Q1 N
受压力或冲击造成表面的下陷。
" D3 N3 c8 g2 n9 }% R2 D3 P For example: Left horizontal stabilizer outboard leading edge at WL 368.25 dented approximately 2 inches in diameter.(Area marked in red)) U! [1 {% ]0 k7 i$ T ?, `
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)。
% N. d( L. q( Z1 }2 i 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---8 \3 A4 J" c! y, W9 r
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。4 O0 t k, ?; @1 t9 p+ X& O" b" j
- b: \- e. t V" u [
(2) notch: 凹槽
a4 m) H5 f, Z6 x4 @" S A “V” shaped cut or protrusion
- x& q' {! I. E3 H! n V字形的切口或者突起
" D% `2 h2 E: o8 S For example: Forward L1 entry door number 1 floor panel has a 1-inch notch 6 inches from the forward right edge. 8 p, b; L1 `' z
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
4 i; v: f; l' o. U) |) X2 X6 h槽。/ R" v7 q2 \6 D/ X+ C' \
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---.$ y5 U: v- n: l( a
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。
* N1 z) ~: s, S% I3 u; q& t' I" D7 v! S 6 y& c2 D4 i- ]2 c w
(3) deform: 变形
6 F1 F G: }# @. m8 z7 o$ ^2 ^To misshape the original form
9 ?$ J k$ n: x" u" x8 j原有的形状发生变化
( B( f6 {# f+ }; nFor example: Left wing number 2-fuel access door is deformed.$ T6 u; B5 ^7 H5 V; h; o' O+ H, i% `4 d
左大翼二号油箱盖板变形。3 _. h2 ^( ]$ T$ f8 `: N
Replaced number 2 deformed access door in accordance with AMM--- Carried out fuel leak check in accordance with AMM--- with no defects noted.
" \2 s8 M# y/ ?; a0 u2 U3 @0 S 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。. n. i1 E; \& g2 S
3 t" u# ~; T5 t f(4) nick: 划痕# L9 d: b3 W |5 S; O
A shallow notch, cut, or indentation on a surface.
# I K N, E$ ]1 M$ C% R 表面上的较浅的刻槽、刻痕或缺口。 j+ u- i. l! r7 P: K1 t
For example: Right environmental control system (ECS) access door, after right corner has 4 nicks on external surface . Area marked in red.
, E2 g$ K7 c2 E) e0 D' L3 ~1 R2 `% h5 | 右空调舱门右后角表面有四条刻痕(已用红笔标出)。
@/ S- k" f8 a S. ?' K& D1 {( O7 _: s 4 x: ^& `( |1 u7 T+ e+ A1 C; k
Detailed inspection carried out with reference to SRM---no delamination+ E0 k" F' E9 [1 J# w$ M
noted. Carried out permanent repair by filling nicks with fiberglass and epoxy/ `' W6 i& B$ Y6 d$ }
resin BMS-387 with reference to SRM---.+ J' {1 `- d8 e0 F! U: q. F2 {4 N
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
% `/ I) g1 J2 C" U" i理,使用玻璃纤维及环氧树脂BMS-387填平刻痕。* o1 O( x g8 U$ o$ y
# c( r3 Z6 Y- @, D4 L/ p: e& |(5) pitting: 点腐蚀/砂眼& c9 X- n% n3 ~9 @/ q
Small cavities, depressions or scars on a surface.2 N9 |6 j; v/ q/ x
表面上的较小的空穴,凹陷或凹痕。
! L& X5 T, n2 b% o5 g+ ^ eFor example: Left main landing gear number 1 brake aluminum hydraulic line has pitting.
+ B4 f* u6 c- \/ r: S* H* M 左起落架一号刹车铝液压管发现点腐蚀。& V: ^; R, K% O+ \ r& W0 {( ?
Replaced left main landing gear number 1 brake aluminum hydraulic line with
; i/ @6 p' z/ oserviceable hydraulic line in accordance with AMM---+ N* }( N# @/ h# n9 b4 L
根据AMM—更换左起落架一号刹车铝液压管。
" L+ E* U" ~2 J) P V; I& M - B& X- [# [- l
(6) broken: 断裂
$ N: O' C+ u5 ?4 _2 l Forcibly separated into two or more pieces.' x2 U0 V% Y& q- B8 f
被分成两半或更多块
1 ?; [: k6 M+ r$ I For example: Flight deck entrance door has broken door latch and will not lock.2 a' i3 [& c2 x4 y4 U+ a; ^
驾驶舱门锁销断裂,锁不上。
0 l5 d+ \4 c/ O/ Q( q& ]1 S Replaced broken door latch on flight deck entrance door in accordance with AMM--- Operational and functional check good.
9 @9 j" T w# C7 g 根据AMM—更换驾驶舱门锁销,操作检查正常。
( ]. b9 R: }' |5 x% P% E
4 f3 y& E# h9 n(7) corrode: 腐蚀6 R1 _/ h- j# U- p1 I
To dissolve or wear away gradually by chemical action.; _* h" T% ~" w$ d+ ^* W
氧化或化学污染造成金属表面逐见破坏的化学反应。
F3 z' _1 ]" y6 n: |; P/ Q, kFor example: Floor beam at body station 360 and wbl 25.1 has moderate corrosion 2 inches in length and 1 inch in diameter.# U% y$ u3 P' Q1 y
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)。
4 K! K& F; {6 A3 C. s 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.
3 ?1 k: S: s" p% \+ P$ S( r 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。
5 [) h" L$ R: |+ i( C" {! G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。2 G( A( V( w4 u+ D
5 ?1 Q0 D! S; Z, w
(8) scratch: 划伤
9 T- p4 w, X5 e- M( }/ f$ C- o A thin shallow cut or mark on a surface) ]& ]6 ]3 w; ]9 ~4 L V C
表面的薄而浅的切口或痕迹。; A4 z4 `+ ~' Q" f9 n
For example: Left cabin external windows numbered 12, 16, 17, 21 and 27 are scratched (obstructing view)
* k; l1 [( c/ a9 s& r 左客舱外部12#、16 #、17#、21#、27#窗户被划伤(阻碍视线)。1 H" w/ e5 a* w' W6 v& J2 X% v
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.
8 ^6 r3 V" r: i- Z; ^- y* s/ |0 h/ p+ ]% T) Z 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。% \0 c5 z; t- t6 M. k
3 ]: o( s/ u$ S( ]0 S' L3 p9 O(9) crack: 裂纹/龟裂# V: w0 x/ F( n7 w+ @6 _
To break apart without dividing into two parts.
% y2 I: _. Z, o6 b3 d 裂开但没有分成两部分的破裂。1 M! p5 F H# O9 B! @# I5 x
For example: Number 2 engine fuel control cable located at Body Station 360 and Water4 H5 f& S& s# I0 x
Body Line 25.7 has cracked turnbuckle.0 [- M9 z, h6 n
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。1 g# G: N6 C& g) Q- |0 g; M* ]
Replaced cracked turnbuckle with new turnbuckle in accordance with
, b; T/ W* A' m W, q" }AMM--- Travel and functional check carried out in accordance with AMM---,# C4 \7 w1 g% R; q5 H5 u
no defects noted.
g: w" A/ w% m* Y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。& ^' M* H- _5 }; P; @9 Z
1 L- Z2 U* W. f4 I/ ~(10) burr: 毛刺
' m! N, ?4 ]% W! a6 cA rough edge remaining on metal or other material after it has been cut or drilled
) n0 K2 \+ b, b$ D被切割或钻孔后留在金属或其他材料上的粗糙的边缘.
+ T. ]! }+ B! L1 e$ Z! W. oFor example: External fuselage repair at body station 727 and stringer 9R~11R has burrs at
4 i) U r% R3 M8 `) a2 z* G& t& h% Ball drill holes., f3 u8 E: t( P) W9 e/ Q
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。6 I3 |+ f: x$ O; S9 N, v, I
Removed burrs with rotary file in accordance with standard practices and/ @9 E- r3 v! D$ ^7 B, X
SRM---.* @& n) `0 o2 ^
根据标准施工手册及结构修理手册—的要求打磨去除毛刺。 Y" O H# O8 I; `! _0 E1 Y; O4 J
0 |. y2 C$ a) p
(11) chafe: 擦伤
& U- O' Y& B* l [To wear away by rubbing.
# e' R- g& I$ W" [4 h因为摩擦而损坏。7 U) |# @4 ]# P0 h* X2 {8 s
For example: Forward cargo compartment after corner threshold chafed by cargo door.: u8 w; y1 {1 z1 Z) c" V: x' }- h
前货舱门槛的后下角因与货舱门相磨导致擦伤。( h+ D, ?3 |, }
Forward cargo door upper support bracket worn. Replaced support bracket in( H& O0 |* A- Q) @, [2 j8 E9 b* A
accordance with AMM---eliminated chafing.
. j) m4 Q9 J! o1 p% z$ N& N' H检查发现前货舱门上支架磨损,根据AMM—更换该支架。
$ W- Z( x6 U( _ C3 F8 L4 |$ Z$ ] 0 X$ @( a' y$ a* u/ C: x
(12) protrude: 凸起/突出- C3 s% |$ |* X9 c
To push outward.
+ G' l8 H# }; X0 V4 k- ^# I- K+ F向外伸出。
. Y" ?& |, `: q: p& ~* b' dFor example: Forward external fuselage servicing doorstop is protruding through access& {7 O# U8 u' b( A+ y) k" n/ Z
door.* ]! z' x! N5 v( X( w4 z8 t
前外机身勤务门止动点凸起。
' [- }% W: c# q0 a2 P Repaired forward external fuselage servicing access door to original contour with reference to SRM---. Adjusted doorstop to eliminate protrusion in accordance with AMM---.
7 C! j& m+ x7 J. a; i" m$ M0 D8 O! s 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。
/ ?7 B* m+ I8 m$ k$ k, ~) \" q6 O . l. M4 W4 E4 E4 P1 h5 k, R) H
(13) sag: 凹陷% A2 U" M$ g# T( ?1 D+ M' F
To sink, droop, or settle from pressure or weight., K& A' \" W1 V$ Z
因压力或重力而下沉,下垂或下陷。
7 a/ q+ G6 i6 F5 c5 @ @For example: After cargo compartment overhead ceiling panels are sagging.
$ p& a) P+ V( F7 r5 z, M& s 后货舱天花板凹陷。& n, [! m6 b. d" L# r/ y
Detailed inspection revealed ceiling panel screw holes worn. Replaced' d: I- g' F+ H% C: y* n
unserviceable sagging ceiling panels with new as referenced in AMM---.; P% K) y, ]$ A: A* Z
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
( [, @4 }" t. Y: ?' f板。2 O& {5 M/ f' |. r4 o
9 m- |, r1 g \0 C' n
(14) rough: 粗糙0 E# ?8 o# e7 O, ~4 ~: ^( A" C1 d
Having a bumpy, uneven surface.
9 G M6 E5 f3 k u R) X% x表面不平坦,有起伏。* r2 b5 u! G; I9 ]8 i1 H7 o4 |
For example: The protective finish is rough at the number 1 engine inboard pylon.
$ D8 r. {8 K' E& o" H5 o 一号发动机吊架内部的保护层粗糙。
( W7 e' \- m/ d7 s Removed rough protective finish at the number 1 engine inboard pylon in
5 _: ^0 i' q9 x; t3 haccordance with SRM---. Applied 2 coats of enamel to restore protective" }8 x; o5 e0 s0 N* e' f
finish with reference to SRM---.
* M* G: Y2 x W0 Z 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。$ W# D6 I' \$ w, Z
' W: h1 K( Y [: Z(15) finish (missing): 漆层(剥落)
; _6 X0 R4 {' o' ]+ qTo protective material used in surfacing and finishing flake off.
: L8 y4 P3 g! i1 t5 R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。3 Z# ~, K' i, q9 F
For example: Fuselage skin protective finish at pilots and copilots number 1 and number 2
1 p: L: b% M7 R& J& M4 _ C* Ewindows missing.
/ f* G- @. ], Z! W2 r, ?正副驾驶1号和2号窗上的机身蒙皮保护漆层剥落。
" @/ R$ Z, S9 jPrepared affected area of fuselage skin at pilots and copilots number 1 and* B& \' C! d) M! ^8 s" s' \) K
number 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.
% G: x, |7 T- b7 _; q( J& S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。
6 W% U" E# O! l& E! |' a
5 v8 o! V/ z! k1 u(16) fade: 褪色/变色/ f8 `& t1 g7 v5 |9 Y
To lose original brightness or color.- b \5 Q( G2 e' ~* Q' F6 q. u7 c
失去原有的光泽或颜色。
6 c* X5 Z/ Y) u6 J/ y8 i7 fFor example: Number 1 and number 2 engine intake cowling chrome is faded.: [ {/ e5 S! b0 u* H, b1 ]! a3 M
1 号和2号发动机进气道的铬层褪色。
, |! Q4 H7 C: z5 r7 [4 n Polished number 1 and number 2 engine intake cowling chrome with reference3 w9 U8 {1 g" n+ r6 Y
to SRM---.& H% k' e( b* s. z
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。
: B& L4 S$ S5 W1 k
- n+ g: z. P$ G: }3 ](17) entrapped (water): 积/含(水)
& x& `( I: [; q8 o+ DTo collect in an area.$ `! c- f+ G2 u( ~/ \1 V, W" Z
水或水汽在某区域内聚集。! C+ [5 j! C) R
For example: After cargo compartment forward bilge area at body station 840 has entrapped' T7 s( q9 c2 ~" U" `
potable water.
4 x8 X/ |+ v+ |" y3 d后货舱在机身战位840处的前部区域有积水。+ _. ]- M% I' d# z" H
Detailed inspection found pressure drain valve clogged. Removed,cleaned and reinstalled pressure drain valve in accordance with AMM--- Removed residual entrapped potable water.( Y/ W% d5 K( P6 ^
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。
$ |2 l' {8 o+ P% o : x8 W$ A3 @" d
(18) oxidize: 氧化3 X% u' D1 u. [) i' d3 L
The containing of oxygen usually caused by natural elements.
% x# O" }6 W, A" i6 A- ?1 {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。6 |! _8 k# M9 H& ]! k" b
For example: E-3 rack lower after corner is heavily oxidized.
5 A- n, |- \# q E-3架后下角氧化严重。2 i( L* _6 q* i/ t8 j9 C9 k
Removed oxidation at the corner of E-3 rack in accordance with SRM---.2 l5 W2 W" }$ Q9 X5 x
根据SRM—去除E-3架后下角的氧化。) R- R& F3 t1 A7 @
4 t/ }2 _4 R5 [- r(19) distort: 扭曲
$ U q c3 S+ FTo twist out of a proper or natural state.& P n/ W% D& L: F, L
因受到扭力而导致原有的形状发生改变。$ c: K& U" q5 F* F, Z- W! q6 u; e
For example: Access panel 2145J to left wing number 3 slat actuator distorted.
* F/ {! D& ?4 ~" w 左大翼3号缝翼作动筒的接近面板2145J扭曲。
# h2 p8 J% R7 h Replaced access panel 21458 with new panel in accordance with standard
7 `6 t5 ]/ D0 E: y$ Spractices and AMM---. Original panel declared scrap, tagged panel as much& Z4 v& u3 ~7 }( @- j- B- }
and routed to MSC to return to customer.7 W( s2 P& t7 Q* q* J+ U" {4 H! T7 {
根据标准施工手册及AMM—更换21458盖板。旧件挂牌送航材处理。
, h' W5 o+ ]# ^: d# s
' V" \" h- s/ }0 W0 R% N2 d' ?; z' q(20) (not in) contour: 外形/轮廓翘起4 g0 |6 X6 W3 Q+ V
A shape or outline is deformed.
) ]+ P R2 t1 y& ?. |* ]形状或外形轮廓变形。- |! f4 k) P, D$ j
For example: After lower corner of after fuselage external servicing door is not in contour6 f/ @) R( }; \: T& T e$ d' k
with the fuselage., k& r0 C0 V. j" a0 }( y
后机身外勤务门后下角翘起。7 U8 s; [3 ~0 o3 o
Adjusted after fuselage external servicing door to contour of fuselage in. g& f' K2 X$ x% T. ~9 M
accordance with AMM---.6 q) w5 |/ ~% y5 _. K
根据AMM—调节后机身外勤务门正常。
; @- N5 `( L, `. m8 f " K# W0 w e8 E! D$ x
(21) puncture: 穿孔/扎伤
/ {$ F; d. a" T, tTo pierce with a pointed object./ M/ m, g% A9 D# D" \! y
被尖锐的物体刺穿。
9 V6 Q. J0 O" uFor example: Number 4 tire is punctured.% f s% [5 g1 b8 ]) N
四号轮胎扎伤。
2 i# t3 [1 a2 D7 b" U: m Replaced number 4 punctured tire with serviceable wheel assembly in6 E& u3 g4 y( v- |
accordance with AMM---. Pressure check normal.4 y: {7 Y! I" m; @ m$ w
根据AMM—更换四号轮胎,检查压力正常。
; u8 K! U' R! d8 ^
" B6 N# C4 s1 R8 E5 ](22) chip: 碎屑
w5 {+ g2 q8 M4 DA small piece broken and missing from a surface.* }( g2 L: X9 D0 x" `" l# d
从表面剥落的小碎片。
1 o2 M) P6 Z! D: @1 O5 q) K0 {For example: Starter magnetic chip detector has evidence of metal chips.$ b7 D+ X$ E; f: U6 m1 D U' l
起动机磁性堵塞上发现有明显的金属屑。
2 l8 ~% K: u; w* |1 _! w, s Removed metal chips from starter MCD. Drained and replaced oil, operation
. t; J7 S2 a0 O* A4 t( K" \and leak check good in accordance with AMM---. Reinspect next “A” check as* K3 N0 v- m. j( S4 }
per attached EO 80-003-1.
& O, v3 h% A) g q' S2 |1 K 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。
6 f$ H! h$ \, E$ K( |2 Q) q6 C7 @ & @+ u1 e! h+ X, x) M* U
(23) erode: 风蚀/风化
% C6 t6 D# y4 e) h& `6 j' nTo wear a surface away by weathering, abrasion, or foreign particle.: b+ L* b8 N! s2 j* q
因天气或外来颗粒等原因导致表面被磨蚀。
3 F" v9 C# o1 G9 _$ VFor example: Number 1 engine intake cowling eroded 360 degrees, 2 inches in width from
+ z, V; j% R/ ^& Hcenter of forward leading edge.) y" Q4 _/ q) t' |6 ~, X3 U; L2 U `
一号发动机进气道周边风蚀(2英寸宽)。
) ~7 A4 ?+ `. t% O+ {6 {, x" MRemoved erosion by polishing surface with reference to SRM---. NDT( d. G8 _* V" K @4 @
inspection revealed 0.02 inches of material removed, remaining material 0.23* L" s; y; X3 M( v+ P& |: @) s
of an inch within limits to SRM---. @' F, @3 L' m$ W. m4 E7 [; X
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
& s8 V+ l5 o% z; H少0.02英寸,尚余0.23英寸,在SRM—规定的范围内。
% m% E+ B) @. ]7 A/ }* Z6 h' r
1 H8 J& m. I# H+ b+ x! G8 R3 p(24) mildew: 发霉2 b) X' }+ m$ F3 K- t
A fungus growth.
% a. ]" j4 B" A7 B7 s# ~; ~8 v有机质滋生霉菌而变质,常见白色的生长物。
S# t$ }" Q+ jFor example: Forward cargo compartment insulation blankets in after floor area are moist' P% w. e" ?* U) J6 M6 n* k! z' b
and have mildew.& I7 W7 X8 t0 s
前货舱后部区域隔热棉潮湿发霉。2 J! b$ N- y1 O# l
Eliminated mildew and moisture of forward cargo compartment insulation
/ p) `, K$ r; W) ?blankets in after floor area by fabricating and installing new in accordance with
1 b4 a8 S5 y/ d4 t8 o7 u3 _) A# c, sSRM--- and AMM---.; A8 u1 @3 J" f7 [. X3 P
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5 b; t% U8 Z: D+ n
发霉的隔热棉。' `& }7 ]) e" ]
/ A% Q P* A) L7 q
(25) delaminate: 分层
* |" q2 F/ g4 u9 D' eThe act of separating into layers.
0 a& }% e3 u1 m" g7 l& F& V压合在一起的材料互相脱离或分开。
- x6 B6 @! O. g! |, P0 JFor example: Nose radome delaminated from impact of “bird-strike”.
2 o U# R7 b# w( Q 前雷达罩因鸟撞导致分层。8 E N/ p# y5 h0 t
Removed delaminated core section and replaced with new with reference to
9 A+ o% M7 }( O7 K) SSRM--- impact test carried out. Nose radome OK for service.) O$ {/ Z8 f. Z5 H& R5 E% g
根据SRM—更换分层的核心部分并进行冲击测试,检查正常。% L' Q8 q4 |% W7 X* d4 z* J
2 o6 Y6 }) M$ ?$ u2 V, w. @(26) deteriorate: 老化 ~$ w. | W9 I6 t) A" I
The diminish or impair in quality, character, or value.& E+ @5 d" ^2 p7 @# f1 O* P( q
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。
) H/ U/ o) j$ }For example: Number 2 engine to pylon fire seal deteriorated.
8 {/ }. o# h% Q 二号发动机吊架防火封严老化。
4 |) p. E- R+ I2 N Replaced number 2 engine to pylon deteriorated fire seal with new seal in; @) j, P: c& U+ C+ e6 B: b- [
accordance with AMM---.3 v" ~- s7 Y5 \% S0 L
根据AMM—更换二号发动机吊架防火封严。
/ \ S2 K: M1 r# D( `* i ' W+ t! J& f" |0 |
(27) wrinkle: 起皱
- ]2 c( X) s# P3 OA furrow, ridge or crease on a normally smooth surface.) U3 S+ Q7 p8 a6 E+ n
正常的平滑的表面上出现的皱纹,或折痕。
' u6 R9 [4 f( u% ZFor example: Forward galley wall at flight deck entrance has areas of wrinkled wallpaper.9 u1 ~7 [% y, l3 a, G, o
驾驶舱门过道的前厨房墙纸起皱。& C0 b% h3 g0 F* g) V
Eliminated wrinkled wallpaper at forward galley wall at flight deck entrance by$ N7 r$ g, b5 h* y* [9 N
replacing with new in accordance with standard practices and AMM---.; P1 h) q6 v7 K: Q" B& a9 w
根据AMM—更换驾驶舱门过道的前厨房墙纸。7 G. l- h* H4 j2 y2 H. L1 @
& z7 H! j, N+ q
(28) saturated: 受潮0 ?; n! X3 z. k( a( ~5 H
Soaked with moisture.% V8 Y5 D+ v2 k9 V2 U1 @2 S; U
物体吸收了水分的状态。
6 g3 G9 X5 k$ C: \0 vFor example: After cabin floor carpet between lavatories B and C is saturated with water.7 L% |6 l9 b1 B- F5 v
后客舱厕所B和厕所C之间过道的地毯受潮。
* }# }! @* E( z; A. A- u( N Eliminated saturation of after cabin floor carpet between lavatories B and C by9 O$ t3 w4 Q! {( ?$ m8 {
replacing with new in accordance with standard practices and AMM---.2 ~. y# \7 Z8 q/ {9 \
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。
! n4 C* p* r2 k! H
7 E5 r* W$ @1 j* U(29) tear: 撕裂 5 B/ Q9 }0 ]2 T! M0 S, d* u" k8 {
To pull apart resulting in a tip.
- A0 u e+ ~' V; g, V. O2 D9 K5 q裂开后分离。 H# R* t. B9 z" U
For example: Number 8R window shade in main cabin has a tear.
& }6 {0 {, u+ D; ^% d% `5 w& k 客舱8R窗户遮光板撕裂。/ x P6 U* n. Z- Y, r
Replaced number 8R window shade with serviceable window shade in2 m( {% ]$ Z1 o# l; t
accordance with AMM---.
! `& E( h' z" @& U8 b& r根据AMM—更换客舱8R窗户遮光板
; d3 e- x% }' k1 e8 z
( B9 o- Q- z6 A4 q+ m1 g(30) worn: 磨损/陈旧6 m+ W; S( I6 d T7 U" `
Unserviceable due to excessive wear.# @* Z/ o$ k% D+ ]9 P" n2 i7 t
由于过度磨损而不可用。* D0 Y& }3 y$ q/ U
For example: R1 service door upper guide and door latch on doorframe is worn." D, M1 M$ C0 ]& h
R1服务门上导轨和门框的门闩陈旧并且磨损。; O7 H& u0 S" _, G
Replaced worn upper guide and door latch on doorframe in accordance with8 E9 C5 o0 o" t" l( z
AMM---. Operational and functional check good.# s( l& a' ~$ j. M/ ]
根据AMM—更换上导轨门框的门闩,功能测试,操作检查正常。( ]% @, o3 P5 _
0 x0 w7 v; j/ l& a1 ?: S(31) be not adhered: 脱胶
) g) L' i' o* |8 kUnsecured and not positioned in place by glue or sealant.
9 } @7 [7 d5 Z5 U2 j& W; c9 c因附着力减弱导致脱开。
: [& j$ T: s5 w& E5 vFor example: Left emergency exit hatch external “EMERGENCY EXIT” placard is not5 u) i# S% w, A& G
adhered in place.
% A1 M4 q9 n6 o9 N; r+ [2 ?左紧急出口舱门口盖“EMERGENCY EXIT”标牌脱胶。
" [ ~6 @( J3 a* M8 W& _% gResealed left emergency exit hatch external “EMERGENCY EXIT” placard in
' _0 K+ K( I9 P6 u/ k/ `: gaccordance with standard practices and AMM---.
, o% p+ I; I- I! K( {$ `根据标准施工手册及AMM—重粘左紧急出口舱门口盖“EMERGENCY- U& x+ ^) P2 a
EXIT”标牌$ G% B ^# U; ]8 f5 P8 o* ~& z" l* S$ q, x
0 u$ Y! ?, W0 k5 W+ H d(32) burst: 爆裂
8 a/ ~/ y5 F3 U) Q6 @$ ^, W3 xTo open and suddenly come apart from internal pressure.2 I0 p. z* K m, z; e) `) {
因为内部的压力突然炸破或剧烈的爆开。, j% d' h6 Q: L
For example: “A” system hydraulic pressure line located in forward left wheel well burst8 R& U# s( ~1 R! p. L, T0 r
during landing gear functional check.' |3 T3 z; E! }7 s- G
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。 o |) L( Z$ G5 E8 v- I! g) w
Detailed inspection of “A” system hydraulic pressure line,revealed grommet
Q P9 c4 Q8 S/ I+ G" Vof retaining clamp missing resulting in chafing. Installed new “A” system
) d* l$ d$ C2 D# j/ Lhydraulic pressure line and clamp in accordance with AMM---. Operational
2 p9 ] M1 `; K( b) e and leak check good./ K: K/ w7 J, o: u. L+ {
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# X3 s' L0 O7 B% V2 ^) P
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: J1 J$ q& U0 ]& Q2 \( G, t
漏。
) N+ q3 }# g8 K; }% c
: E6 l8 d& E f1 Q `4 o, u4 p(33) cross-thread (pertain to plumbing) 滑丝(限于管路)
0 j, i/ `+ j7 Y, a( w: XTo damage threads to an unserviceable condition.6 S) V3 f; \1 e5 D
螺纹损坏后不可用。
5 s, j, l7 r& t3 A* RFor example: Left wing number 1 ground spoiler actuator hydraulic pressure line has
- @- h6 Y9 z' w3 U- H; Hcross-threads at “B” nut.
7 P% |& [ J/ C l. R$ g1 K左大翼一号地面扰流板作动筒液压管B螺母滑丝。
, s' y7 h) g- ~: [Installed serviceable hydraulic pressure line at left wing number 1 ground3 m7 N" ^: _& O6 j
spoiler actuator in accordance with AMM---. Operational and leak check good.
/ ^4 N' ?2 q" V7 f0 V. S# w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,
$ q/ P0 ~" f# g# G7 e& v无渗漏。5 D" j4 N- H6 ~% S) @
) S. {7 x0 a3 U" P2 H
(34) twist: 扭结/弯曲
8 @% F* x2 t7 mTo alter the normal aspect resulting from torsional stress or strain.+ A- i6 W7 M ?; X
因为扭曲的压力或者张力导致改变了正常的面貌。4 q. U3 o! \6 Q$ W5 P- \
For example: Right environmental control system intake door linkage twisted along routing
5 p7 E; P4 ?7 Z0 E" g1 Dto exhaust louver.
/ t; c4 k' S, ^0 h' S7 N右空调系统进气门传动连杆朝排气口的方向弯曲。
% f b! f/ J: m9 h+ \- dDetailed inspection found broken bolt at eyelet connected to exhaust louver.
8 o+ t' d' F% Z% [0 lReplaced broken bolt with new and reattached eliminating twisting with9 b m3 a& _ O* a/ R- l b
reference to AMM---. Operational and functional check good.( c( {8 h0 M* H
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
" d1 z. y9 a* X常。6 r/ {, u' d* O# }9 J v
% ]* G( ?0 b$ s' ~; f( u) B7 c(35) leak: 渗漏& P- s* d0 L% W5 H. A
The escape of a liquid or air in a system., B+ ?* Y8 i7 ?2 g2 h6 |
系统里的液体或空气逃逸出来。! c$ @) r7 e# ?+ x; [# t
For example: With reference to routine task card 37-265-1 pilots pitot static probe test failed
% w; o$ |* Y% K$ p2 X. A7 O' d: ]due to leak in the system.
5 D7 R. J4 P6 b9 s6 O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。
I$ ~8 a( ^1 n: z4 V, ?Detailed inspection found loose connection at pilots static port. Removed “B”% I, V( ]- I) g- N# ]+ p& s! T
nut and inspected with no defects noted. Reassembled connection and leak5 T1 X2 |+ K0 c
check good with reference to AMM---.+ K$ x6 ~4 f+ g
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5 X9 z" s6 r) r$ X
陷,根据AMM—重装接头,渗漏测试检查正常。
4 G+ D# I: R6 W/ q) x * m1 F w6 k7 h+ h& K, ?) E
(36) obstruct: 堵塞
/ u1 u; }4 t; s* `" Y# l# |. mBlockage by foreign matter.+ x7 G5 |4 ~0 z6 l! }8 S( {' w
外物妨碍管道的通畅。
5 d& e+ F. _: n, ^For example: After lavatory service panel inoperative, suspect obstruction.
- ^: V" B( e( I) a 后厕所勤务面板失效,怀疑有堵塞。5 V8 }9 {+ [! Y3 G+ K- s
Detailed inspection revealed drain system plumbing obstructed with foreign matter. Cleared foreign matter from drain system plumbing, operation check good in accordance with AMM---.
6 l" P( \, u o9 g: C 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。
" h1 U$ r9 Z; g D; M
; d/ K* r! _& ]$ T2 [' D# d(37) contact: 相碰 * t$ N6 L/ `/ z* ]* ?' S' d
Touching of two surfaces or objects.
- k, }. J5 Q4 D% u) b, J两个表面或物体的相碰或搭接。
0 c! ~$ M. |1 D" D! R1 B8 g" `1 `; PFor example: Left wing trailing edge has aileron control cable contacting pulley bracket at* F( P' i, U1 x8 c5 q* w! n9 \$ B
WB Station 245.9.
; l% n, n; [/ ?4 M2 p% d6 l左大翼后缘在WB位置245.9处副翼控制钢索和滑轮架相碰。
( m w9 t" E( \: ?0 u6 H# p- |Detailed inspection revealed pulley bearing worn beyond limits. Replaced with
* E' s2 `' I+ z6 c- ~new pulley in accordance with AMM--- travel and clearance check OK.4 o- \; N, m8 H7 M5 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
$ e8 J& r2 C' `4 a! d& C% Q, W6 P间隙正常。+ P- }& N, M* l' m* T
5 A1 F( N9 I$ q7 E' _# m
(38) fray: 断丝/磨损* i6 @& E2 Y' F
To wear away by rubbing.# v5 o8 y- N }8 G! x& M4 h- w
因相磨或反复拉伸导致的损耗。( Y3 i7 T+ E; q0 H9 k1 \
For example: The lanyard attached to the after end of the right access door to the APU$ f% B1 O- \: f! I$ `7 A
compartment is frayed./ g6 }4 A: M6 f6 N- p* p) a& j
右APU舱门后端系留绳断丝。
. q$ v6 N: K) I$ t3 mRemoved and replaced frayed lanyard in accordance with AMM---.( d5 M9 L- F0 w: C
根据AMM—更换系留绳。3 y: I4 d& x+ n5 g9 R# l
' \4 e% [; j% H5 g(39) fused: 熔断: o6 ]- X {: t" Z( a# Z
To become united by melting from heat.+ j5 O7 z# e4 J8 \! {2 n
因为高热而融化连接在一起。 - O0 w; g4 ~0 S) r) C Z- P; \/ Q
For example: After galley coffee maker inoperative. Detailed inspection of after galley coffee
" L6 h5 g+ K2 S# i: r7 F2 smaker revealed thermostat wire D34768 fused to temperature controller wire
9 P0 E' I9 x5 Q3 fE57689.7 p2 ]# r$ d1 v, [; v0 @! ~8 e
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& j5 D* i+ A: n! H8 N5 H
置导线D34768与温度控制器导线E57689熔断在一起。
5 _9 J) F0 |6 d- M+ g3 `/ YReplaced wiring with new, operational and functional check good with
- Q" m8 L i7 n3 Y* oreference to OHM---.: k1 ^+ ^4 \* P/ |( c+ ]- h
根据OHM—更换线路,功能测试正常。" D" V! B3 l9 j* f% C; d. @+ g
) o/ ?- i, k, A(40) bend: 弯曲
, M, k7 G# L) V' sAltered from straightness or original position.
: v5 l0 N# o1 \* Z$ S改变平直或者原有的形状。, E. F$ E" N# n. h7 {0 Q- N
For example: Forward electronic bay door left hinge bent.
( ~3 k9 U0 f- t" c, X+ ~ 前电子舱门左铰链弯曲。
" `, F* U3 q( e* M4 r Replaced left hinge with serviceable hinge on forward electronic bay door with1 }7 N8 K& h1 J0 u' }5 J: K
reference to AMM---operational and pressure check good..8 Z/ J4 J+ U7 m/ s8 s W4 }, [2 i
根据AMM—更换前电子舱门左铰链,功能检查正常。/ D5 x* \" j2 D+ G+ Z0 k! ?
& q! _0 F+ V; ^
(41) disconnect: 脱开
5 j. q( ?! P& E5 R: |Not joining resulting in failure.$ [3 u+ B* \- q+ S) s
因没有连接而失效。
4 {2 T# m# {* |, |For example: Left environmental control system pack temperature control has disconnected2 s$ p2 E, c+ r
cannon plug.% N" j5 s- h6 @! \
左空调系统组件温度控制插头脱开。
' x- Q2 K/ \! Y( t) hReinstalled left environmental control system pack temperature controllers
j9 q9 R/ L icannon plug, operational and functional check good with reference to AMM---.1 \: j7 o7 ~- ^' k6 t
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' Q( t, k1 |" F0 D/ s, C
查正常。. K7 M5 S$ l% x+ r
" J& ?! w) d' I! a* G(42) missing: 丢失& V7 s5 B1 B. k2 d
Not present.
2 K0 u7 [# m* O2 J 不在位。
. ]9 s% g3 y+ ] For example: L1 entry door has 3 each door stop pads missing at the after middle section of
j( D5 D/ m6 F4 ]8 T% z/ Kthe door frame.
K. N, x% K0 Y) @ I* h) {6 ]左1号登机门后门框中间位置有3个止动钉丢失。2 @1 n+ e- Q" t4 w
Installed 3 each door stop pads at the after middle section of the L1 entry door" [; B, K# o6 W
frame in accordance with AMM---.
: Z: a3 p, Q: f, P) u根据AMM—安装左1号登机门后门框中间位置的3个止动钉。
. B( W. f+ x6 C6 u3 A # m2 _! b- s* \- p" S, j
(43) loose: 松动/松脱0 Y; w/ N# P; y' N; f' L
Not secure.7 e( T X' T; ?, Q1 `
没有紧固;活动0 t( r2 t8 v0 O" l( q
For example: Forward right wing to body fairing has several loose screws.6 a6 y4 E' g- a8 f, l
右大翼机身整流罩前部有几颗螺钉松动。
( s D# B o% Z6 h: s8 Q; p Found 17 screws loose. Tightened loose screws with reference to AMM---.6 C A- j- ]2 Z) I
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。' o8 P2 q5 t: h9 t4 b& Q# H
& n( ^" P) W, d0 [# ]$ |' ]( D(44) not secure: 未关(扣、夹、卡)紧
; W0 e; d8 l, R( U9 Z4 |5 x. [Not fastened, to make firm or tight.% a; x8 x, {2 o! t* n0 Q7 x' H3 ^
没有扣紧,(使)紧密。9 S# f: Y8 C5 o6 y, l ?8 s
For example: Number 1 engine cowling; number 3 latch is not secure.
- S/ @7 Y5 l7 Q$ M) |) u 一号发动机整流罩的三号锁扣未扣紧。
) q# P+ Z7 h3 e' L4 R2 B# b) ~+ Q' {5 s Number 1 engine cowling; number 3 latch has damaged hook. Replaced
8 e+ [4 @- E& k8 bnumber 3 latch with new part in accordance with AMM---. Operation check( b# w( K5 x$ \
OK.4 W& D1 i/ | 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,
; d5 v. Y& u) [0 Y, E( x8 X Z操作检查正常。* b/ Y8 n' B' E W6 p5 z2 F4 d& E
! L$ U3 e3 y" A(45) inconsistent: 不均匀9 v% G, z/ C) h. z i
Not in agreement, erratic; Q' M1 r; E/ \" i( I: g7 u2 U x% `
缺乏连续性。
7 T( |' \3 k( y' C# iFor example: Left wing-to-body fairing seal is inconsistent in relation to fuselage.$ G0 W t8 }# l- N
左大翼-机身整流罩封严胶不均匀。- ?6 k% t. X" Y! i1 }& ]( A
Re-sealed the left wing-to-body in accordance with standard practices and
5 z1 _* z2 E, s: O; L% h VAMM---.# Z( V" W) O/ q' P0 Y! \: N+ L5 I7 [, ~
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。1 h x! Z! H8 S0 o d: I, _( ^ l
0 W" }8 w& _. X' [" ~# D(46) exposed cords: 见线
$ }4 L- {: C5 b' i. y7 jVisual tire cords. d! r8 t; L( @% L0 Y$ c
轮胎编织线裸露。3 z3 _/ i) V; b5 T& x3 ]- m" p$ a! k
For example: Number 3 tire has exposed cords.
T$ A, O/ ?0 D& D* G. i 三号轮胎见线。
! L- r6 T% R% f7 P- i! Q# | Replaced number 3 tire with exposed cords with serviceable wheel assembly in
" ^. i# c, u- P; {8 v laccordance with AMM---. Pressure check normal.# ^' V: h' r$ m0 f6 n# C0 ]' F3 n
根据AMM—更换三号轮胎,检查压力正常。
. t; @ Y& |/ T0 I7 a s5 A: `# C
' |- I& F" P) ?# b S/ Z(47) bald: 磨平6 M* o1 A( ]( v& f P
Lacking a natural or usual covering.
) \. ]' h* w& S, d* ~- J$ U6 D" r轮胎表面排水槽由于磨损而消失。% W7 A5 L4 r. O1 J3 X3 d( B% H
For example: Number 3 tire is bald and requires change prior to flight for no serviceable" i( F3 n6 l9 D# r% d
spare at scheduled flight sector out stations.' [+ r" {" R6 Y( A4 J1 }; e1 B0 b S* A) J
三号轮胎磨平,因下一航站没有备件,请在航前更换。
# h& e: k7 t) Q# ?) IReplaced number 3 tire with serviceable wheel assembly in accordance with* c7 E1 e0 R8 M
AMM---. Pressure check normal.
: ?: I& K5 J& b% n+ i2 z根据AMM—更换三号轮胎,检查其压力正常。
# ?" q: e# C& f @: \( E
9 n$ j5 Q4 \0 Z5 ?# c7 \(48) insufficient-air-pressure: 气压不足# Y9 [, l2 I! J
Air pressure does not meet manufacturers requirements.
$ b/ N4 o7 x, M+ S& d0 q空气压力没有符合生产厂家的要求。2 O& E4 W& d: x/ W/ G$ \8 ^
For example: Number 1 tire has insufficient-air-pressure.& c! f/ l9 H. J7 w, Z3 n @
一号主轮气压不足。
: l! k6 V3 i# u/ c1 } Measuring air pressure revealed 5 psi. Air pressure required within limit as
3 V. A! i0 ?8 ~( X1 _called out in AMM---. Serviced number 1 tire with Nitrogen as referenced in& |* r6 I. T( l; w
AMM---. OK for service.
; w! \* {+ x7 m* i% `# M测量一号主轮气压为5PSI,根据AMM—对一号主轮充氮气至要求。0 w1 t2 u- X" |5 j- S, ^6 g
* O! c" B0 U( j Y& W, _, P( L: [3 j
(49) expire: 过期 i7 A; h1 n' g& Z+ W6 f) x# F
To come to an end or terminate./ ?8 t9 y) h0 ^- I7 c7 S3 ~% M
超过时限、期限。
+ W# ~" p& N7 M; S; j" oFor example: 2 each life vests located at L2 entry door flight crew station expired.
" S2 m5 e1 P" C0 M- Z T0 X 位于左2号登记门机组人员位置的两个救生衣过期。6 Q/ F' X2 T+ k3 E' [% ~( w- ]
Replaced 2 each life vests located at L2 entry door flight crew station with
3 D8 X6 ~3 U/ P$ \ N* f0 D7 dserviceable life vests due at 9-2005 with reference to FAR 121.6.
2 w; a+ ^; U8 w6 T$ x 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4 b1 i, \* q$ S, L! A4 T. p: E
衣。) V5 Q; g1 J- y: Z0 R2 I7 h
- D. v. H! T4 c) Z9 j4 h$ s(50) illegible: 模糊2 Z# {7 T% y# j4 Q
Not capable of being read or deciphered.7 r4 T5 T6 ~0 W) x/ g: Y9 A
难以辨认的,无法读出或解释的。
$ }) H% v9 H1 f' CFor example: Left over wing external emergency exit hatch “EMERGENCY EXIT” placard9 V6 A6 @9 b/ x( ~$ k
is illegible.
% c+ A) |5 O& w# A+ A* |2 w" g左翼上紧急出口舱盖处的“EMERGENCY EXIT”(紧急出口)的标牌模糊。
' l4 e7 u; [1 Y% O6 NRemoved and replaced left over wing external emergency exit hatch
+ o" Q2 t9 o d9 n1 {- W“EMERGENCY EXIT” placard with new in accordance with AMM---.1 S, P; n& l, I; ]$ p/ 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。7 `9 P/ P. `# ^ W
# D; D$ I( n1 ~: J5 g+ L8 a(51) damage: 破损/缺损
3 H6 m6 D* g5 w* e& ?/ YNot useful or functional.
2 r/ @$ |! B& A0 p不能用或者功能失效。
z' |. B, q2 A2 g! D" v) s2 LFor example: Left wheel well landing gear door “NO-STEP” placard damaged.
, N2 q% j: m) c$ o) z' j8 i2 P 左起落架门的“NO-STEP”标牌缺损。
5 n+ H2 j5 I* b1 X# E7 X Replaced damaged placard “NO-STEP” at left wheel well landing gear door.3 _3 @" X$ b, M# R
更换左起落架门的“NO-STEP”标牌。- Q2 D5 O, X( |; ~) v( c
1 y; @% H. s7 B# Z# p# N. H
(52) lifting: 翘起' @4 t h9 R/ u$ A
To become raised, not intact.
& s4 E: L' E8 D, _* B& n A没有紧固;活动& M+ \8 U* A% J; Q: ?
For example: R2 service door escape slide operation placard is lifting.
6 L$ D' ~: J G" q) K( O 右2号服务门逃生滑梯操作标牌翘起。: c2 t B3 W' W/ n4 T0 M9 w
Removed lifting R2 service door escape slide operation placard, cleaned and
5 @+ C" i4 p k" T- Sre-adhered to in accordance with AMM---.
: O( F$ j# f; q' v% X9 E0 `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# h+ S, ~, l F& O6 Z, p* a
该标牌粘好。
$ M1 z" L/ k$ ~( X, O4 |7 X $ z ?2 V8 B t3 [; ~
(53) not properly sealed: 变形/密封不佳% f- Q% m; @; `- Z! t! n ^4 b2 Z
Retaining package torn exposing contained contents.; A8 C/ U9 u" t
固定的包装撕裂而露出里面的东西。
6 A- ` j1 D5 [0 H; tFor example: L1 entry door flight crew station portable breathing equipment not properly
2 b% g# B( S; L$ y; B0 T$ b$ ] b/ Msealed.3 M9 V: j. P8 ]& l) k
左一号登记门机组手提防烟设备变形。9 A. ~ d' j. x: W" N
Replaced not properly sealed portable breathing equipment with serviceable2 F4 O7 G# P1 h5 h$ l8 s+ S
portable breathing equipment with reference to FAR 121.25 as required for
+ V% W& P$ z+ c8 }- G3 Y- M7 t3 Idispatch . Tagged and routed unserviceable PBE to MSC to return to customer.
) }6 a" r/ F+ ?9 ~* u- \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7 W( y; i. Z0 O) F
理。+ s: J% v& K7 a9 M
5 _+ ~* I. U& }7 P1 }% y
(54) not properly packed: (滑梯)散包% K& E; f" V. `
The condition of a released slide.' g" o6 j; J% t, f! Y& J
滑梯包散开的状态。
0 Y- w6 U1 Z( T2 Y/ |3 g9 E$ b. f9 k" C, ^For example: With reference to reliability work order and task card 25-456-01, replace R2
+ q' L( z( }1 h" u" r3 ~; M. U& C, Eservice door escape slide, provided escape slide from workshop S/N 4321 is not
% F) {/ W9 z# w$ Jproperly packed.
6 T5 ~" Z, m# T+ A6 Y$ ~& O# R$ h: n8 G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; }) Z1 y8 d( j
车间提供的(S/N 4321)件已经散包。
6 ~- N# w. s- f! s* }Tagged and routed emergency escape slide S/N 4321 to MSC to be re-pack in
, u! M6 t/ w8 q" L* L1 Oworkshop. Obtained serviceable emergency escape slide S/N 8765 and installed
: [" \9 G( G( D% f, d" yat the R2 service door position with reference to task card 25-456-01 and
3 V( r, C5 ^1 k# \' RAMM---.
9 F4 o w2 _! C6 o' P( e 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; l1 ^# f# s. v; F9 A
25-456-01及AMM—在右2号服务门安装序号为8765的紧急滑梯。
3 a( A$ m+ H5 E. i1 s( b4 ]$ g / s: u- x0 _: E4 u
(55) dirty: 脏$ e7 H! p- N: u8 j
Unclean, soiled with dirt, grease etc.
( y9 Z# H- \4 N7 Q: V5 f不干净,有灰尘或油渍。. W2 g3 \1 T* u" x; a C* y. Q8 w
For example: Flight deck external window are dirty.
" @/ W' [9 ] q$ u: p$ C7 Y) l) ]* ] 驾驶舱外层玻璃脏。
8 G' a% a% S8 V; r: ^ Cleaned dirt from flight deck external window in accordance with AMM---.; W9 Z7 K: _5 e# v
根据AMM—对驾驶舱外层玻璃进行清洁。8 h* ^ K2 j' M. M3 J- {
* ~) Q7 W& K& j7 N9 X( x: X' d' m
(56) fracture: 断裂
7 M m. [+ ]% e% n; Y: kA break, rupture or crack.
; K8 E5 S: \" m: _4 b破碎,破裂或裂缝。
: i% l0 L! E8 T1 _7 Y! LFor example: Reference Gameco routine task card 53-004-12, NDT X-Ray inspection at right) C3 T+ {8 H: U$ R( c+ c
wing emergency exit hatch frame revealed 4 inch fracture at forward lower sill.% {2 F* K2 B1 d! }
参考Gameco例行工卡53-004-12,NDT进行的X光检查中,发现右翼紧
" ?# v. t3 n0 V7 Q, v急出口舱门框前下角断裂(长约4英寸)。
& C$ a: \# m- d) U8 J1 fRepaired fracture with permanent repair in accordance with SRM---, attached7 {! |6 v" r5 ?
Gameco engineering order 53078-4, and attached Boeing TELEX 53-0987-1.! |1 J0 r: ]1 |
Applied protective finish in accordance with reference to SRM---. e# h' G( ^) i0 ` Y T- c
根据SRM---,Gameco 工程指令53078-4及波音电传 53-0987-1,对断裂进
" w2 O( G M7 {# ? b( S. Q7 ^行修理。参考SRM—进行保护漆层的恢复。2 U: e/ i, c6 ^! K% y3 x
" ^ Z% ~& j" C1 u6 n4 h. R) i6 L(57) exceed-the-limit: 超标
C' ?# r2 [! s' [$ IDoes not meet manufacturers specifications.3 u' u4 F. x) c9 ~* Z
超出生产厂家的技术标准或规格要求的范围。- ^& i7 ], f; O! {9 F. Z# R: y
For example: Reference routine task card 32-098-01 landing gear functional check, nose
c1 Z" U, v. z2 C; Nlanding gear doors faired to fuselage skin exceed-the-limit during functional7 s/ F2 @( f) W8 s3 @( D }
check.
8 _' \3 |+ E3 q$ O T4 B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& O5 K% u7 a6 s& w2 g0 x
架门与机身蒙皮间隙超标。9 X3 G" u' R, S$ h$ y" C
Adjusted push-pull control rods at nose landing gear doors to obtain proper9 S. s: _/ ^; E; G
fairing to fuselage skin in accordance with AMM---. Clearance and functional. N7 l3 j, C6 g) v; z" @
check good in accordance with routine task card 32-098-01.
( o I4 g: h. G# u# I" v% B: 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
/ V' t, m5 H+ q2 L: B# s* r) @* H进行功能测试,检查正常。/ y% I- k# J+ [* J0 g" u% I, j
; ~4 ^5 i9 W) \9 B4 }
(58) backlash: 空行程/无效行程
' s9 r( Z" T7 z8 g6 gTo measure play resulting from loose connections between gears or other mechanical9 P |# t a8 a$ v5 Z
elements., X; o j+ G# U' s+ Z
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。
" _5 t; W+ V. k1 h; n0 OFor example: Horizontal stabilizer jackscrew clutch failed backlash test with reference to; W+ o- v6 i k' v X) C1 u5 A
routine task-card 27-0345-01.
: s' t& ?$ V, Z7 P7 _* J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。
0 ~* e L, t6 d+ u6 K$ ]2 r: F) lRemoved horizontal stabilizer jackscrew clutch. Detailed inspection revealed
; z3 N! s/ J7 ^8 ]; z o( g1 _worn clutch plates. Tagged and routed unserviceable clutch unit to MSC for
2 g/ x) @9 e* b5 oreturn to customer. Installed serviceable horizontal stabilizer jackscrew clutch5 z; C A% w) R, F( Y0 s2 C1 V
in accordance with AMM---backlash and operational check good.
% N) w4 K! J6 d' t9 r% L9 s1 b2 B 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
" e0 G/ C' ~8 Y: i& t) `1 k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。
' @. e1 S/ B) u: Y- U$ F* u % k* D$ A1 r! H7 x9 S' n7 e
(59) block: 卡阻/阻塞( ^" }) ]0 t, M2 G( ?. \/ R: q; F7 {/ w
The act of obstructing.
}8 q( h" S; u/ m$ T通道堵塞:运动部件的动作不顺畅。& W6 M7 [- B/ l% J
For example: Forward cargo compartment door forward actuator is blocked when opening
' j. ^0 ]* R0 E+ O2 fthe door.
6 X5 s# }. V$ {& I0 k1 B前货舱门在打开时有卡阻。
* ^- I9 C* B% v- I- a: W" @8 WDetailed inspection revealed there was a dent on the actuator rod. Replaced the
; _7 B7 q2 S2 o: @6 _5 U( u+ Oinoperative actuator in accordance with AMM---. Operational and functional! X) U. m; i: p: w2 E4 j/ J
check good.3 L% |' w2 G5 c( F3 p* ~
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,
0 b1 J. y2 ]- x, m5 V操作检查正常。& H! V7 ~9 D$ \3 u/ T
3 o5 @7 n( X- n$ {. I' y/ Y
(60) bulge: 鼓起
0 ^4 j2 k: G/ [: U1 \8 RAn outward curve or swelling.. B) r# b5 t% ]) ?( @+ S0 I2 a
向外凸起。
0 b: B% m/ t- z6 `+ J& n: |For example: Forward cabin lavatory floor panel is bulging.$ d7 J* j. |' v# E* I6 z7 K
前货舱厕所过道地板鼓起。) v1 o; g# {; s# A$ o8 w! Y: R
Removed forward cabin lavatory floor panel, no defects noted. Re-adhered5 ?& T, i& ]3 R! c3 {, h0 v
forward cabin lavatory floor panel and eliminated bulging in accordance with1 k8 m/ V& _/ U9 F0 W% S5 L8 |9 A
standard practices and AMM---.- b. w) }8 z X& n
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. }+ F6 Z- R6 n# v9 Z/ D7 N' k3 P
AMM—重新粘接该地板。# }1 z' r/ i% F7 [6 c/ H- `$ R% L
6 U9 n8 i) e$ r3 e
(61) contaminate: 污染
A1 u* C+ ~; BImpure mixture." q1 W: t$ k' ?* E
有不纯的杂质或异物。
9 c4 L) `) |. G! [, @3 pFor example: Fuel sample reveals positive contamination of microorganism growth.$ L1 e* A6 w" S5 m# O
燃油样品检查发现有微生物污染。
8 \4 W5 x+ l3 r, ^+ A' g Treated fuel tank with biocides with reference to attached Engineering Order
}( e+ N5 p' k0 qG2009619.& v \; k8 S0 A* c
根据工程指令G2009619,使用杀菌剂对油箱进行杀菌处理。
1 d( l" C: e+ v$ }& C6 i $ h5 ^* p) R9 ?- b$ H2 f) I
(62) disagree: 不一致
! U: u5 g5 H u" p9 @# ~( z4 TFail to be in agreement.$ K$ n$ a1 o/ j D3 Q' R; C
对应关系不正确。7 y* ]5 e/ R; X& [* z5 g# ?5 b
For example: Flap control lever disagrees with flap indication gauge through all detents.
y. {6 t! Y1 m Q/ S! t$ t8 S 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。9 x) L, E* K: V) q- t" m
Adjusted left and right wing flap indicators in accordance with AMM---.
8 @, H' ~; o4 H$ l6 jOperational check good through all detents.3 G7 j4 ~( S9 C7 U9 c
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" v3 |" k% H6 C7 M8 w+ C
表指示一致。
9 W! g( F: c0 C( V * g( k3 s9 \; y9 q8 b( J4 j
(63) discharge: (电池/气瓶)被释放. J0 |& _. n6 \. @( i7 G
To relieve retained contents to an empty state.
3 @8 u+ ?, | x% z+ P放出;腾空0 i, @( U+ k8 n- i
For example: R2 service door assist accumulator discharged.
8 S1 a, P# A0 W8 V2 K) a+ o2 d 右二号服务门助推气瓶被释放。3 o" e' k, F8 F4 E
R2 service door assist accumulator detailed inspection revealed damaged
- u* V! @2 r/ d6 Apressure gauge. Replaced pressure gauge, serviced with dry air as called out in
3 R, t) j, ?& y% uAMM---leak check good.
1 v& l0 C2 [4 V5 B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
+ H6 G9 p7 I4 H1 y0 W压力表,对助推气瓶进行勤务,渗漏检查正常。
9 C" K8 u) ~; N8 x6 H) ^, D 6 S4 C! |1 _* e8 \) u- e; H
(64) dislocated: 装错# [% i' A% W3 Q. v' O5 }
Not in proper relationship with joining part.
$ R: B+ [) ~* B7 w* ?' K零部件没有安装在正确的位置。
: r9 @' C' F& ?) s& ^4 o/ jFor example: Forward cargo door pressure seal is dislocated from retaining track along after5 w% `, }7 ^8 l+ m; L# b
and bottom section of door.
. e" ?: y# z0 T4 I前货舱门后底部固定轨道的压力封严条装错。
5 B; R1 @% s3 } K6 MDetailed inspection revealed pressure seal retainer damaged along after and) ~: V( H' J. O6 ~7 c( G
bottom section of forward cargo door. Replaced affected section of pressure
1 u$ z" l& c' N4 B8 zseal retainer and reinstalled original pressure seal in accordance with AMM---.
* U) M! O5 g, a# wOperational and pressure check good.
( q1 p4 Y A- }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
# x* d6 z% [" }% u( t该安装槽并重装封严条,操作并增压检查正常。
4 @9 G$ [" G! k+ _
% J8 I' I- |) S4 f& X(65) fail: 失效
9 g- j- ]$ L6 `1 y: f8 t' HNote: must have detailed description of failure.
0 s. G3 z# q7 t [9 @% P6 y注:如用此术语,必须给出故障失效的具体描述。
9 t3 `0 f$ w+ [/ LTo perform ineffectively or inadequately.
' P' R1 \$ ?, f不能执行或不能完全执行原有的功能。8 K! u8 P6 q( K- q$ H8 x
For example: 13F seat actuator failed to adjust.
/ K. k# q9 W- P. `$ X4 z6 S 第13排F座椅作动筒失效,不能调节。
; t5 g( Y1 C! S1 z- h Replaced 13F seat actuator with new part, functional check good." c5 l2 u- C/ n& H9 A( E
根据AMM—更换第13排F座椅作动筒,功能测试正常。4 `% C4 y* l: I' U$ z
) G8 Q" ]7 b: H(66) fluctuate: 摆动
4 y- L) O; a# XTo continually change or vary in an irregular way.0 F3 f8 L( X5 h3 W+ Y* `2 E" X0 u
无规律连续的起伏不定,变化。9 {+ I# l3 k. d8 E. d; R0 H
For example: During engine run the number 1 engine oil pressure gauge fluctuates.( g+ P1 f. d& }3 ]) x
试车时,一号发动机滑油压力表指示摆动。
1 s' |* R$ L: x& f, H0 k2 o9 Q Replaced the number 1 engine oil pressure gauge in accordance with AMM---. Carried out engine run, oil pressure gauge normal.
' a$ ]' Z' \% i7 G6 g0 g2 Y 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。
* E* D6 R8 ^* r- Q: f/ q, N0 D
3 f1 Q" R `9 P+ t, W- E(67) flutter: 抖动
) |+ ?: V& f6 R/ pA rapid waiving or flapping movement.
% T9 w1 t! U5 u. \ Z; @快速的摇动或者上下振动。
6 D5 z2 v2 O: f0 O: s; N2 l0 `For example: Pilot report on flight logbook page 908701 fluttering sound from left side of0 y; [, _5 K6 C( d1 x a
airplane during descend beginning at 11000 feat.6 i; p* j$ R7 C ?
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
( i/ Y" J6 r4 T7 [; ~) E2 u5 V侧有抖动的声音。
8 e. L# o2 f% q( D. @Investigated fluttering sound from left side of aircraft as squawked on page! ~9 k6 T) p8 n. z w+ L( M
908701 of flight logbook. Found number 3 flight spoiler actuator leaking.
) o8 c; a3 ]5 [, }1 Q" K; |8 e Replaced number 3 flight spoiler actuator in accordance with AMM---. O( p- {6 h, P$ O4 h5 P$ w7 N3 \
operational, leak, functional check good. Flight crew briefed prior to flight.2 @, N5 p! ^+ ^" V5 J# v
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。
: Y+ g+ K0 P. a 6 N3 u+ K+ v' |' \# k
(68) insufficient: 不够/不足5 d8 @6 O, }- V* a3 `2 c) B
Not sufficient, inadequate.
" ~1 p3 E9 ^- c5 S: w5 m% M2 ]. J达不到所要求的数量,数目。
1 t; v* Z" h9 P, qFor example: Left main landing gear alternate extension control cable has insufficient& v6 E9 k( u1 }
lubrication.6 e, l3 O1 o" [! T: l9 S. X* E8 l
左主起落架备用控制钢索润滑不足。
# ^: s+ A( B$ k i- mLubricated left main landing gear alternate extension control cable with
2 h+ W3 C2 ~6 Z' CAero-shell 12 grease as called out in AMM---.6 m7 e4 s: ^/ P9 s+ P
根据AMM—用Aero-shell 12润滑左主起落架。2 d" P+ k H0 Z: H! ^& t' [ p+ S
8 X( k" [# i. m% I- z8 x(69) inoperative: 不工作9 K) ?/ [4 B8 D1 z( F
Not working.
k1 {. W. i! u8 [: w不能正常的发挥功能,作用。5 {9 t( |2 U9 { A5 y
For example: Forward electronics bay door indication light in flight deck is inoperative.% @ B$ i# a! V" I. Z+ h
驾驶舱前电子舱门指示灯不工作。
' O8 m/ n, i P Detailed inspection revealed 2 each bulb filaments fused in electronics bay
D$ Z2 J: i: t) idoor indicator. Replaced 2 each bulbs in accordance with AMM--- operational
& }6 l; N2 b( w+ T: B$ Ncheck good.% d; E. j1 F: z0 y, F1 h7 W, E
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3 p7 J% I" z, d( q( T+ C
这两个灯泡,操作检查正常。- b: F4 O4 U" } u7 y
8 ` b; a6 `- |4 R/ ]4 Y
(70) (not) illuminate: (不)亮( X/ m3 q( H) ~. p. d* N
Not brighten with light.
7 q5 A8 E$ p- `! |不照明,不发光。
" {8 S/ W3 j$ }/ fFor example: Passenger reading light at cabin rows 12AB, 14C, and 17AD, will not
8 z" \& z; M+ _( @illuminate.
- ~& _" o7 X" w3 e12AB, 14C, 和 17AD座位的旅客阅读灯不亮。8 U4 u3 O! {) ] q7 Q" d
Replaced passenger reading light bulbs at cabin rows 12AB, 14C, and 17AD in
3 c1 {6 j, R, [8 m: xaccordance with AMM--- operational check good.6 V0 P x$ e0 h+ P0 w( g' P
根据AMM—更换12AB, 14C, 和 17AD座位的旅客阅读灯,操作检查正
4 v7 B( L7 P% @6 P常。
! z I1 H5 B5 w6 g" O
: a9 L% v2 d0 [- L' o2 f4 f- N(71) interfere: 干扰
; v F+ k4 I0 A, V# qTo come between so as to be a hindrance or an obstacle./ }3 g0 W6 C% J' w" q) J8 c& l
妨碍无线电设备正常接受信号的电磁振荡。
! ^0 m/ R- X- I8 o, f" VFor example: Functional check L VHF radio revealed interference static and abnormal noise.3 j8 P: Y5 K$ e+ Y
功能检查左VHF设备发现其工作有干扰及静电噪音。5 E; x% J; |5 ^8 } h
Replaced L VHF radio in accordance with AMM--- and tagged and routed the& v! r# o5 M3 [. B) Z
removed part to MSC.9 R7 \& Z- L/ r8 X( [
根据AMM—更换左VHF设备,旧件挂牌送航材。
Y0 ~2 p" ~- P2 u2 w) B7 F 3 _7 ]" A; q8 u
(72) kink: 扭结/缠结
* {0 y! |) s! Y- HA tight curl or sharp twist.
9 A! ^3 c/ x' v6 q2 v(钢索,条壮物)缠绕在一起。) x/ p4 N" F0 p. x
For example: Right wing inboard flap control cable at control mechanism located in after
$ ~" G3 z5 ~5 z* G7 ?1 i) Pright wheel well is incorrectly routed and kinked.
3 {3 m8 h: g0 \: k! e; D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。
5 a" |) w1 K4 tReplaced with new flap control cable from Body Station 760 to flap control! j$ \4 ]1 c' y- l/ g
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. B7 n: x+ \, g8 j6 l( B6 b! ~
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。
; U7 L' w3 _' O! r
6 o g/ B7 U* C. C" ]' n3 T(73) misrouted: 走向错误
2 k3 a0 k% P4 o/ y* p, }8 PNot properly aligned through a course of travel.3 X* f7 A8 U; I' R% h7 N
在行程中没有正确对折。
4 t0 w' L" W' I" m: bFor example: Left main landing gear manual extension cable is misrouted through pulley attached bulkhead in the left wheel well., g" t! v0 s- J3 V5 W/ T9 Q
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7 s( u! s% W% Z- Y {' y" ~/ F( `
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.
( \7 ?& X3 D& F: I2 O5 v 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
/ o+ \+ X. ~2 I, S% V# L0 O0 c该滑轮重新安装,功能测试,检查正常。5 X g) E" H+ @4 ~" ?
) X8 ]! C0 k6 P/ O2 S) [(74) not installed: 漏装5 p0 d7 ^ W/ W
Missing.
* M1 y+ B7 w ]6 D- k% ~根据要求本应安装的零部件未安装。3 n: _+ E; R& P7 j7 j
For example: Life vests not installed at L1 entry door flight crew station.
+ e E/ i9 P9 f! k m- E7 e8 L4 Z! v L1登机门飞行机组位置救生衣未安装。. \' }" T+ k/ \
Installed required life vests at L1 entry door flight crew station.4 t# G9 h& h+ j, M0 Z
在L1登机门飞行机组位置安装救生衣。
* R9 x V$ l" q2 c% i7 m
6 I- n# F T) {* D8 t(75) rubbing: 相磨
4 T6 ~; }1 h0 j) v* B' t) bMaking contact with an unrelated surface
2 E& N# I2 j8 M3 Y0 i. L相对运动的两个物体表面因接触而导致磨损。
* s* B! w! F2 Y; yFor example: Wire harness for cabin PSU’s running through floor beam at body station 360
3 x! u* }( d: r$ I( E) Qand wbl 21.52 is rubbing against floor beam cutout.& y' \' | r1 A& b P
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8 ]2 n" t. r0 p! S- e0 H$ ~
板梁时与地板梁切口相磨。* o( _& M6 N- J; M
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---.
& J* g M% Q# T 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,
- ?: r2 p7 l5 ?: f: j+ v$ Q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4 i5 m/ b1 a# h7 V& K- X
处地板梁切口相磨的情况。1 k U' c5 J) ?6 b5 P
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(76) un-lubricated: 干涩/缺乏润滑
- d. T. U: \$ s" BWithout lubrication resulting in friction, heat and wear.* ]# N2 ?( k( K0 k& @5 V
没有润滑而导致相磨,发热和磨损。
4 a, |- H% e% AFor example: After aircraft wash, all 3 landing gears were found un-lubricated./ y: f. O8 P# j8 a2 o- {9 y
洗飞机后,发现三个起落架都缺乏润滑。
4 l; e! N) q4 L0 w Lubricated all 3 landing gears with aero shell 17 grease with reference to, y3 G( P' @; C' x
AMM---.+ X; `0 o' V( o
根据AMM—润滑三个起落架。3 d7 f8 v0 W5 N1 q" |
, |3 X+ w& Q4 \$ t7 U8 V(77) will-not-reset: 不能复位0 p: x! S6 `9 @
Will not return to its operating(original) position.' q+ k2 N- p& Z" J! Z& U% A
不能回到原来的位置。
5 A, }" E+ \ A8 T' I M, h5 ]For example: APU circuit breaker will-not-reset.. T4 f# X" v( q
APU跳开关不能复位。/ c$ R' I! g; {, B; m
Detailed inspection found APU circuit breaker faulty. Replaced APU circuit+ G$ d3 N* j: k( }" Y$ v c M
breaker in accordance with AMM---.Operational check good.; s/ \$ S6 _& p" X
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。 |
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