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维修术语 [复制链接]

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发表于 2008-12-29 23:32:04 |只看该作者 |倒序浏览

维修术语

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发表于 2008-12-29 23:40:58 |只看该作者
维修术语8 r' _! q( I' ?6 S5 h q1 b, T5 O) r$ Q0 Z$ F1 r8 K2 K4 b( F: N (灯)不亮 not come on   不可用 not serviceable; u* {: p5 T y. T. L “工”型 type I   不锈钢 stainless steel+ p+ H$ j4 W j) c9 q% f APU 舱门 APU bay door   部件 part 7 X5 Q# t9 H8 WT 型件 Tee extrusion   材料 material 1 \- q* D/ K: q9 y6 |阿罗钉 alodine   参考 reference; o! Y1 Y& W& t9 q% S( x 安全带 safety belt   餐板 feed panel4 ]$ i+ l9 p; { 安装 install   餐车 diner: C1 N: {8 Q4 [! c( ^4 g 安装座 attach fitting   操纵 control ) O R4 [- N2 u5 }) A按钮 button   操作检查 operational ) U. `$ _ [5 p5 C5 v* t按需要 as required   槽 spout4 F7 t! u5 G5 J9 L 凹槽 notch   侧板 sidewall/ W2 E4 X9 P a2 S 凹坑 dent   测量 measure 8 S& b5 z& `# D8 C9 x( ]- `8 I! {把手,扶手 handle   测试 test0 M2 [1 ?' ?. r& R: ]3 N9 m* h 包皮 cowl   插钉 pin 6 f& j: y ?6 b+ h/ P; Q保护层 coating   插头 plug% K; y+ Z0 @- |* b2 ~; X$ } 保险 fuse   插座 receptacle 6 d k# D( P( t# |7 D2 ~报废 discard   拆下 remove ! g4 u7 m5 m% m" ~报告工程师 report to engineer   长桁 stringer 3 P8 ^( B4 ~3 ~$ z杯子 cup   超标 out of limit! Z& b; t) |7 G9 ^: O F! F 比率转换器 ratio changer   超标 exceed the limit: v4 y# O u! h& k 壁橱 closet   超过 exceed ' ^. x3 P) n k1 F8 D+ _& _边缘 edge   超控手柄 override handle6 r. s! F5 R9 T2 v9 X4 @ u 便于检查 easily to inspect   彻底修理 drastically repair $ L* g/ T& C, V- O变形 deformation (n)   陈旧的 worn $ o: B" N- \! H9 G变形 deform (v)   衬板 liner . a6 C n& E# G( g变压器 transformer   衬套 bush : J* \' V1 d6 s" }2 V标牌 placard   成型 shaping * ^$ e" d* L" K0 o3 s8 n标识 sign   乘务员 attendant; Y! [" e. q+ W( _. N( }' Y 标志 instruction   尺寸 size- n7 Q3 ?, J/ X' _/ \ 玻璃 pane   充足的 sufficient : k, ]- N" z6 k2 c1 B) u1 @7 C5 L玻璃纤维 fiberglass   冲水按钮 flush button 4 l, b4 s; l9 G: ~+ w, e+ R6 T补片 patch   冲洗 flush5 z0 ]; O, v* V2 Q F. z$ y! s 补片 filler   冲压 ram : w% p8 T; [7 r冲压空气 ram air   低压压气机 LP-compressor : p6 p. T8 {- a抽油 defuel   底部 bottom , U" a( {4 m, ~出口 exit   底盘 base [3 c9 L4 C9 l; k; z 除腐区 reworked area   底漆 primer8 z* ?( d4 g K0 U4 H 厨房 galley   底座(结构件) mounting. b/ Q0 S; I' h0 M$ a/ y; A% J 厨房烤箱 galley oven   底座(螺母) plate 6 }9 H3 B0 v, I储物柜 closet   底座(天线) base : K3 ~' x4 H5 k1 v& T- {3 |5 Y, P处理 treatment   地板梁 floor beam $ J9 T" J& a, H# O# U处理 dispose   地面 ground 2 e8 U* n+ K0 [3 n# d0 \* I% O传感器 sensor   地毯 carpet ) L4 v( ?: N4 H9 k0 F, ^传输 transmission   第二层 two layer' a# J c. Q4 N' {, |( J$ N, [ ~ 垂直的 vertical   点火电嘴 ignitor) `! R1 _* e3 H T, b0 {; o% g 存放处 location   电路 circuit7 y- L J7 o3 O! q& K" o 错位 migration   电门,开关 switch * N3 h& o1 D5 B; j搭地线 jumper   电气 electrical# g$ A/ ~ e5 Q6 n 搭接处 interface   电气接地 ELEC bonding % h6 E; N9 w8 u搭接片 splice strap   电源通电 power % m1 R. B7 z2 e$ n8 o搭接片 splice   电子 avionics . T* B2 a9 V2 Q! A# M打磨 blend out   电子架 E rack* ^! s7 j' c% @! w5 s 打磨片 blent disk   电子架 shelf 3 @! E0 F4 f M打止裂孔 drill stop hole   电阻 elec resistance 6 p( L* {( G( o, Z' b7 w6 N大翼 wing   电阻 resistance _( @% i5 {* H1 R+ B 大于 more than   垫片 washer' P. z9 k5 Q1 f& U9 E2 g 单向活门 check-valve   吊仓 nacelle1 c% h# b0 @! w2 K+ \0 Y. y 弹簧片 spring seal   吊点 mount cone: {" \& Z% M& z; U. W1 w, C* m8 p 挡块 retainer   调节 adjust ' c7 w5 I# X- g" X9 ~挡雨板 fender   调整片 tap. x+ g$ I+ E4 K7 S0 L7 e6 Z' w4 g1 N. G; N 导线 wire   顶板 ceiling 5 w- v# I) P" m) a, y' z灯 light   顶部 top ' O) @, j8 I% B1 S* d9 c8 E9 {6 Z灯泡 bulb   顶部 overhead, R' u2 J) L/ o/ ? 灯泡 lamp   定中弹簧 decentering spring . B4 E. G. I( X& G; w灯箱 light case   丢失 miss " m( {" P1 y9 ^& O" x# t, t; [. [, _灯罩 light lens   堵盖 plug 4 j9 I' B" |9 U& K6 I% Y登机门 ENTRY DOOR   堵塞 clog: L8 M/ T( w' U, h$ g( b& B* F 端头 ending   腐蚀 corrosion 2 v/ D `' G4 ?) D" e& K$ V" ? N段 section   腐蚀 corrode 6 t- W- ?7 G# v& k: z4 k# Y" P断 break   附件(大) accessary . ]5 u7 s Q: ^( W7 O断开 disconnect   附件(小) attach2 |3 n5 E+ u6 q* o! j 断裂 fracture   附近 adjacent to 9 o4 s! I% B0 M; |3 _断裂的 broken   复合 complex 8 z: x v$ M4 F' E% T5 I断丝,磨损 fray   副驾驶员做椅 first offcer's seat& Q) D# E' r; Z3 |# |4 P 锻件 forged part   副翼 aileron: }7 Z7 X6 E; I( G# c( F 多处 numerous   改装 modification # q0 m" z* m6 y- i% K# J* \发动机 engine   盖 cap # j* }& k8 P/ Y* [- x) s6 J翻新 overhaul   杆 rod: W& s7 S6 ?& _7 m9 \7 Q 反光镜 mirror   钢丝 steel ' i( f" n/ h8 }$ x. |9 q方向舵 rudder   钢索 cable/ v' Z3 l; x: |2 o 防冰管 anti-ice duck   割除 cut out+ G3 |1 a2 B' {# r. v 防腐 corrosion-inhibition   割断,割下 cut off4 A* ~( c, v% E! Y 防静电 static-free   隔板 clapboard,partition, G4 b0 x% j* o% a/ J$ j+ {; }4 r" g 防磨条 wear strip   隔框 bulkhead * K- r; `; i) W: ~9 f; Q8 Q5 d3 v) ]防滞 antiskid   隔热棉 insulation-blanket 6 B& I. C" q+ n0 J; S# _/ X防撞灯 anti-collision light   隔栅 grille " B0 x& D" S) N6 Q3 S& _放 extend   各有 each has 7 b O1 m; N# u; i1 F. |2 l放电刷 discharger   根据方案 in according to disposition # D3 t7 w/ ~; X7 o1 U! L分层 delamination   根据监控指令单 condition monitor order… : n' U0 A) m+ j/ ?6 P风层,脱胶 delaminate   更换 replace 8 U a/ z" J) J+ `% o! n风挡 windshield   工程师 engineer 7 B2 t2 O% W% k风挡玻璃 windscreen   功能测试 functional test . S5 W/ D7 K2 J8 l" d3 {$ S3 K+ m风扇整流罩 FAN COWL   功能检查 functional 3 Z, x) S" U! L9 I/ z风蚀 erode   供应系统 feed system % o3 {/ [( Q; M8 @. n e& V封严 sealing   供油管 OIL TUBE 3 k$ W0 }. |$ J8 N) L6 n封严条 seal   鼓轮 drum 1 R# T1 `8 p1 S: a6 R$ U蜂窝芯 stagger core   鼓起 bulge 5 D/ W. J, T# c G3 B2 a扶手 armrest   固定 secure% L; \8 \. n* w 扶手盖板 armrest cover   固化 harden 3 P- [0 i0 l2 p6 Z5 Y. u% p辅助滑轨 assistant track   固化剂 hardener" o" \1 `% {5 S- B s 故障 fault   划痕,划伤 scratch) D, [4 x; p+ { 刮伤 scratch   划窝 countersink " G) B# w+ j* ]! j& z: v0 k8 U$ w挂 attach   环氧树脂 epoxy resin ! A& U! k. ]8 [1 a* Y& O挂钩 hook   恢复 restore Y" T i6 H8 b! B5 a7 M8 O挂上 hang up   活动窗 slide window2 R' q# e! }& U N4 @ 关上 close   活门 valve % X& k; L- `( {" V9 x6 L1 x观察镜 view glass   货舱 cargo compt ( p& }6 j* }: }# o5 Z p观察镜 viewer   机构 mechanism ( F8 C8 Y+ H/ s# D观察员 observer   机身 fuselage 6 ]4 I! \: l- ?. V8 y观察员 observer   迹象 mark 7 C. p$ V# Y- B光滑地 smoothly   加强 doubling . N1 f9 L; z- M& G1 H4 e# _滚轮 roller   加强件 stiffener ' C+ z9 w, ~- P1 W过道 aisle   加强块 doubler 0 P' d# t5 X8 M% X: G9 R过期 expire   加强肋 intercostal; v# |) p8 l; t8 O8 m' M6 V* A- [" V5 R 过热传感元件 overheat sensing element   加强修理 reinforcement + H- `9 D# w5 @& O5 r, ?海绵 sponge   加温导线 hot wire 5 i# Y# J. a+ K0 ~焊接 weld   加油面板 refuel panel ' ~& ~! V; K e5 H9 T0 E焊条 welding rod   加油站面板 fueling station panel ( O2 d8 ]* ^" G \) T恒速传动装置 CSD case   夹子 clip : L1 i+ L3 b8 M7 A) @4 o横梁 latitudinal beam   驾驶舱 cockpit k1 A+ Z* y( S% V$ o1 ?3 h i 横向 lateral   间隙 gap # Z0 `( e/ F1 z3 F% H9 J后端 rear   减速板 speedbreak5 V, \3 |1 D/ v# H) Y 后缘 T/E   减压器 reducer $ \8 Y1 Q; O" A W; A厚度 thickness   减震器 shock absorber- W' D' B; Z7 Q. u' r 呼叫灯 call light   减震支柱 shock strut+ V. A4 U9 n! R( R! d 护板 protect strap   检查 inspect - B7 L5 C) W# X" }+ Z+ n护目镜 goggles   检修门 access door 6 {8 s) R% T) {% d; Z* u: W护罩 shroud   胶 sealant5 s o% {( Z% u. w 花键 spline   胶带 tape $ X7 Y9 R+ A; \3 d$ N滑轨 track   胶垫 mat7 I; ]" J$ n c 滑轮 pulley   胶垫圈 rubber washer. S6 d7 N% L9 A% I$ ~: @& `6 o 滑丝 cross thread   胶套 rubber 5 C0 W; h& r* P3 L! s( f- A: {* E滑梯罩 slide cover   胶纸 tape1 o) ]$ [9 W( U6 Y5 Z' s* i+ a2 K# d 滑油量 oil lever   角材 angler + p2 h% a% C- Z( K& Z角型件 angle shape   喇叭 megaphone8 g- F9 x4 }; V 脚登板 pedal   拦网 block3 G0 k. T! g6 A# d; ?& K3 s8 | 铰链 hinge   牢固性 security 8 [' C% V# {4 \5 b' q* B接地点 ground point   老化 aged( {) k1 O9 q1 W, n Y9 J g 接耳 lug   老化,退化 deteriorate3 J% Y, \: f9 V& c( { 接通,提供 supply   雷达罩 radome( [9 s( M' F; ^, x1 E ?- P 接头 fitting   肋 rib / B. I {' C4 m" r7 o接线管 splice   离合器 clutch & d% u7 k& u2 `7 F: N) Q2 A6 m接线片 terminal lug   立柱 pole8 V7 C% P# i4 o. } { 结构的 structural   例行 routine 5 n( ?: x: C+ E- m" m( d; w金属屑 metal particle   连杆 link9 ^ J3 k+ i" Z; y7 f* |+ N 襟翼 flap   连接 attatch/ Z' _% ?1 ?* ?+ W, k4 ` 紧固件 fastener   连接板 attach plate $ Z. P2 R) Y! e8 l4 [紧急出口 exit   连接口 coupling , Q8 k# ?, G9 t- f7 {进气道 inlet duct   连接销 lockwire 9 g0 L/ Q- S; _* Z进气口 inlet port   联锁 interlock+ e' m* l. D5 W Z9 d- }- ~% X 径向驱动轴 radial drive shaft   裂 crack2 I4 W- V( W3 R; n: ?6 W6 q4 U2 S 静电,静压 static   另一个 another. ~; G% X& n" k2 m 救生衣 lifevest   龙骨梁 keel beam* X5 r4 a* L$ |0 R! c 咖啡壶 coffee maker   滤网 filter & [! ^; ^9 w: m5 `卡箍 clamp   铝箔 foil 4 y6 i$ L/ E/ d+ W卡环 collar   轮舱 wheel well2 u4 K0 M6 K& s& x* w( X% I 开口销 cotter pin   轮子 wheel 4 }5 m* g4 S% z& j( l6 @靠背 back panel   逻辑 logic" m# h3 y- O4 |6 E% T% n 壳体 case   螺钉 screw 6 v1 X v# `. i0 q) x; R6 i- o可用 available   螺钉孔 screw hole0 h2 e9 f- N( C 客舱 cabin   螺杆 bolt ) ?6 Q( R% J" {) J3 w! c; t( }4 D空气循环隔栅 air return grille   螺帽 nut l# S: K" R8 Z* C 口 port   螺套 insert 8 t0 }5 l$ L1 a* w8 @' S' G4 ~: |块 piece   螺纹压伤 cross threading1 W- t: \3 n- F9 n/ R 框架 frame   马桶 toilet $ Y0 h/ m! T$ J8 Z垃圾箱 dustbin   慢车 IDLE1 \1 a. K/ W4 _, T) l3 n8 O 拉紧 pull   毛刺 bur- n {# G( O7 L7 ]% \" G! q( s 毛胚件 rough   破损 damage * D4 E& V* i1 y9 g; D3 P铆钉 rivet   漆层 coating: T/ |$ R! V6 A! W& N. V/ i 门槛 sill   其中之一 one of2 o. I! F9 w$ ^6 d4 h4 P c8 { 门框 door frame   启动活门 start valve ; U4 ]# [0 k! {4 V蒙皮 skin   启动机 starter 0 r. ^0 c5 ^& ?. m密度 density   起落架 landing gear 1 O0 K- P: T. C6 |# U- \密度计 densitometer   气瓶 cylinder , I/ n: ]4 P3 o, z, }+ O. U面板 panel   千层片 shim3 i4 u7 g9 `& P* @; W% l' L 面漆 enamel   前厕所 fwd lav , i# T' p7 E8 X3 N5 n模糊 blur   前缘 L/E9 m/ o" R+ V0 S8 m 模糊不清 obscure   腔体 cavity+ e# v1 d1 l+ w9 Q1 I) V! J2 h 磨损 wear   墙纸 wallpaper + m6 ~9 h! U0 P/ O2 ]目视 visual   切口 cutout 6 E# X1 |% m$ R( W) ?内侧 interior board   勤务面板 service panel% D% ~: c4 Z4 S( Q, t* N1 I 内层 inner   轻度 light $ l2 x/ ?. S F) r7 ?尼龙搭扣 nylon fastener   轻微 slight ) k3 r# [. P/ F! C! `9 H5 j1 V尼龙扣 nylon hook   清洁 clean 9 b0 ?6 z& F- v/ Z9 M# F拧紧 tighten   清洁剂 cleaner) {/ X) q' [0 X# W3 L6 d% M 扭力管 torsional tube   区域 zone' R) F3 z. i1 \( N" ]5 | 扭曲 kink   曲柄 crank* X- `% T" t8 R9 P# s# _7 C+ A 排 row   去除深度 remove depth $ I7 K6 `. A6 q% L排放 drain   去毛刺 deburr3 t' x% ^5 b5 H& X4 W: z 排水槽 gutter   缺口 nick + ^1 ?0 Z* |) |排水管 drain tube   群边 skirt edge ' r9 N6 x* _ v* J: v配平 trim   燃油 fuel / w1 _* m% k- f喷漆 paint   燃油泵 fuel pump 3 G8 T3 N H! u# k喷砂 sand blast   扰流板 spoiler & f8 v4 B% Z$ [# z+ \2 J皮带,片 strap   热水器 water boiler 6 _& Q# v( O2 s; u' a6 c3 M$ @皮托管 pitot   人工行程限制 manual travel limit$ \+ \4 ?0 r4 L" t) o. ~ 偏航阻尼器 yaw damper   日光灯 daylight lamp 6 C/ t! z: j" w: c8 h& T平衡机构 equalizer   软管,软护套 hose % A4 M( ^8 ?. O( G0 z- o. v! B/ Z平滑的,使平滑 smooth   润滑剂 lubricant! e; D% F. X( N; i 平行 balance   三段 three section: U( s5 l. G" Z8 |6 y 散装 bulk   逃离滑梯 escape slide 7 d9 P$ y' ]" k3 z1 M/ @ q {1 g刹车 brake   天花板 ceiling. Q; {1 ^7 \( R$ p& A 上表面 upper surface   天线 antenna( {; P; Z! p- a$ C 上述 above   填补 fill 9 q# F, J& e, f2 f3 E1 A: ?深度 depth   跳开关 breaker i! ^/ e! R S& }- R8 w 渗漏 leakage   凸轮 cam* F5 m. d5 P+ W( d0 @ 升降舵 elevator   图纸 DWG 1 g* I% O; Q t% r& ~* ]2 q绳 rope   涂,粘贴 apply4 J: N2 j+ i* @# ?6 b 失效 inoperative   退漆 strip paint! }5 t' y' T( K A5 c/ t; u 湿安装 wet installed   退色 badly faded: X2 ~( F& k r0 x& ?8 ~" H& L 试车 run up   托板 pallet - C# j. ]& V, Z/ x释压 pressure-release   托板螺帽 plate nut * U6 G% x* l9 O6 F/ R0 N% F3 M收 retract   脱开 disengage - r8 b3 `: L+ r. w3 _收发机 tranceiver   外 outer % J0 `0 ?- p% i% J手柄 towing lever   外侧 outer board - a! K" P+ F6 \8 i手册 manual   完成 complete 2 V( k+ _3 n- F+ U8 z2 e! D p0 K手电 torch   完成 finish ! j% \6 p: M: m" J" h% J- a手工 handwork   万向接头 gimbal5 r1 V. C, l% n" g 手提的 portable   维护 maintain ( D6 q1 H4 L& c1 e4 o* G1 k( q: m( h手提灭火瓶 extinguish bottle   尾部 tail 8 h4 X6 h3 G# n; I+ J* X4 ~树脂 resin   尾舱 tail compartment 1 P# l, B. |. b- {& q/ {* b, C4 C双倍 double   尾喷管 exhaust nozzle / i C& F6 M* j+ w( R水平安定面 horizontal stabilizer   尾锥 TAIL CONE 7 \2 k. a7 ]9 Z `撕裂 tear   位置 locate " j1 l0 S s& I/ |3 {3 s伺服 servo   温度 temp0 l! L" Q% A+ i! {% o 松动,松脱 loose   涡杆 jackscrew0 J2 ?- Y: J' g, U/ B* z 送修 send to repair   涡杆 worm bolt; |, P% ?9 N$ I 塑料 plastic   涡轮 turbine2 C. F& W/ N' K) `$ I- d 随动盖板 hinge access door   污染物 contamination9 f6 L! ~0 F& {- a/ e3 n 锁 lock   污物 dirt ' Q3 t! u7 A, Y+ Q4 G3 M. N+ G锁定 lockout   无线电高度表 radio altimeter8 N! w# d3 O$ E$ R5 t+ O L 锁扣 latch   稀释剂 thinner + H4 g+ F5 O9 E, Z# A8 @& h锁销 lockpin   铣 mill1 G2 ] k" ^$ r 系统 system   溢出 spill! h3 }0 a: q' t" o( R4 G; F 下部 lower   翼尖 tip 4 _7 z! [5 D1 p8 Z4 W( M7 m3 s" w下角 LWR corner   翼间 wing tip ; D0 ]: C5 z8 Z! v1 y* b下位锁 downlock   翼梁 spar 8 T8 G( z4 c) E) M. f下陷 concave   引进 introduce ; d. q6 \; C" p- X/ w6 U+ R0 F. l4 b下缘条 chord   引孔 make guiding hole 2 z9 @% \- F) w/ l$ B' a; `纤维板 fibre board   引孔 drill hole6 Z. p' r! }6 Y# B) p4 t* X; J 相关的 relative   引气 bleed 7 E2 x9 B! F5 F4 ?- n相磨 chafe   引气管 bleed hose% U/ \& i% B( X" k f% t 消音板 accoustic panel   应急 emergency; M$ R5 b9 h$ h% w 销子 pin   永久性修理 permanence repair & N1 R, i$ d2 g$ \: I8 @. }* r! E楔形块 wedge   用…填补 fill it up with…2 i1 ?( z" g+ Q 信号灯 annunciator   油封 preservation 6 V. V0 |. e: y/ D0 r6 N) J, j行李架 luggage-rack   油箱 fuel tank : X4 o6 H+ A1 j3 ^) m/ v2 B- j行李箱 stowage   游动梁 walk beam* }) e, Y; \/ ]$ Y, u 修边 reform   雨刮 wiper' d# A1 N J5 Y+ ^% C6 L) I 修理 repair   语音记录器 voice recorder ' [; |$ J, y- _* O$ R# ?# B2 U锈蚀 rust   预冷器 precooler7 [7 {3 ~- G8 m! ^ 循环 cycle   预位 ARM/ p7 r1 w! v- f 压紧 gland   原厚度 original thickness9 H/ c6 Z$ X# r$ k6 y7 o2 c 压力通风系统 plenum system   原来 originally " q7 e8 _0 H F. t& f0 ?) Z压条 cover   阅读灯 reading light" H% i i& L/ v! | 严重的 serious   允许损伤 allowable damage 9 N5 l/ g; Q& D/ r G3 m B阳极化 anodize   杂志袋 literature container ) h9 j& k. V8 z! a* |氧气 oxygen   载荷调整 preload adjust % O; J& w P- g( p氧气面罩 oxygen mask   再循环 recirculation * W7 ?) ]' D! a- K& J% D& k液压 HYD   在位 be in place7 b' w0 J! k' g4 {: z* `" x2 O 液压泵 HYD PUMP   脏 dirty( c8 p) G. t& P4 p 液压管 HYD duct   增压 pressurization 8 M" }7 {- h, p" S# s5 U3 O$ d液压系统 hydraulic system   增压泵 boost pump( G& w" i3 l" O4 s 液压油管组件 TUBE ASSY   粘贴 bond ' d; r9 t* f9 n/ H液压油箱 hydraulic reservior   照明 illuminate + Y7 b8 [' Z' Y& Y: V/ K) _移到 move to   遮阳板 shade ! z3 e) G' g" k7 X0 ~0 Z真空泵 vacuum pump   自动刹车 autobrake- ?( K# m0 k5 @% r& o! F 拯救 salvation   自动油门 auto thrust) M, Y% g2 ^% w" f 整流罩 fairing   自锁螺帽 jam nut+ W: `' G# C1 g# y3 V3 x _; f$ b# i y 整流锥 spinner   自由移动 move freely ' B" {4 I% C! Z9 L! N0 l, a6 \整形 rework   总管 manifold ) m( m9 [" J4 C9 U正常 normal   纵梁 longeron : \: x/ l. f& x) @3 E' I正常位置 normal position   纵向 longitudial" A& n; O0 R8 I" T- z 正驾驶员座椅 captain's seat   阻力支柱 drag strut# a! U) m4 O7 i. r X 之间 between   组件 assembly,pack * }" c2 U4 v$ H! u X支撑架 bracket   组件(电气) unit t4 t* M) H' \6 f) _# U2 r 支撑座 support mount   组件(机械) assy + l: f! \1 l9 u2 g支架 bracket   最薄 min thickness 3 q* c" \% b3 \- _( Q1 ?, H支拄 support   作动筒 actuator 8 [, H3 l. ]% F( b止动固定块 stop block   坐垫 cushion- g9 J+ V5 p: T 止动块 atopper   座椅 seat, Z5 c) `. H. |4 Y% E# m) Y; L 指点信标 marker beacon antenna   注意 caution ( x( H! g5 N( Z: O指示 indication   转接器 adapter " i4 g" h, y# O. a制作 fabricate   转弯灯 runway turnoff light / P" Y# l7 h+ i: u) E( |' J中厕所 mid lav   转向 turn ( j5 H# x% s% B中间,中央 center   装饰条 trim strip* v! e* R: b; N |& N- h' n 周围 around   准备 prepare ' `+ i. V {9 P' A$ G: {轴 shaft   着陆灯 landing light% _3 p8 n" i7 O/ ~8 b 轴承 bearing   自动关闭 auto close+ A% }9 K [5 }! p/ j 主轮 main wheel   助推机构扳机 power assist trigger 0 G: I1 }$ S* t& t( s 0 q- m3 Z5 r6 y% O# H- l7 `9 V% ` v9 `; z7 H9 m& y v; F5 d% A4 D3 l ' n, T3 ]9 Q6 N7 Q5 X. j x& K) ?' V; Z0 I9 J' V4 J ! D+ S6 _3 C% G+ G! W" h) ^* I 9 ^1 X( u* x2 A # h* P% [' _9 q6 X; j# `6 p- P" O7 E. W 2 \, B* Z, L" W. K c2 D 8 ^5 e) R# u8 a# s. ^5 n + N# q- r5 }1 ?# [+ M 2 G) S* m U9 c7 r+ L4 I5 o / g% _' J. l! l1 ~, q 0 ?7 }) ^0 v; Z8 v+ ]4 I( Z- | 8 e: P* d/ g9 m" x3 P! q" u 3 ~. M! Q3 K: r" ~ M; W4 \1 s4 ?) c$ a" R6 f; Q' @; B ; J/ P; w$ O% t2 o0 h. Y3 U! y 0 q" g/ W( N) f, D/ }5 z% Q; k3 t! y" A4 J+ F' `( i: Y# ~/ Q, v 7 J! { B, t7 |& x + K, \ Y- W9 D. K! ]0 a' X% G$ ]9 w% _: c& A4 S( Z 0 D+ z: a7 z" G; J7 D, w+ @5 k9 m8 l* I ! ^ N& `; M; g- w- o1 O' C, Q6 n6 Q) j1 L D 8 X9 A4 V" |8 Q( z6 O+ f; e% o ' I- w7 d' S( J- r! a # T& @1 q" I3 l& }1 X8 e7 q- x8 [" L$ l' _2 ^1 Z4 C8 T: b Categories of Defect ; T& h/ |0 E! n7 M2 C* k Categories of defect depends on experience of maintenance practice .In this manual, the default . Z( h: T2 r$ P 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. ) D4 C; w: C" v+ l. { 缺陷分类 0 @1 S( b F4 T3 _ 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。% w; H# n- r1 z" p } F" T) R- \$ `- Q2 E: B% c! T1. Common Structure Defects Terms 1 ?+ X) V' n7 m6 Q" U1 B0 S( e C结构缺陷术语 " C0 R* w0 M! a% F- h. V0 j $ o* G( L) L4 k) ^凹坑(1) dent " r0 s/ |" f; w7 e 凹槽(2) notch1 X* s9 @% p& ` 变形(3) deform+ T1 U- G4 j+ H+ ~- X 划痕(4) nick " Y: h7 A1 x: p, b% p+ T点腐蚀(5) pitting ( z0 U' P1 B8 R7 I断裂(6) broken& x6 d" X1 R" Q/ K: V 腐蚀(7) corrode& t0 i4 k3 C/ P$ [" G+ m 划伤(8) scratch ( {, U5 i4 m. [) E6 i5 n裂纹(9) crack , |8 W9 T9 d# v毛刺(10) butt& w+ J# s0 _7 z* d5 }+ U M/ f. z 磨损(11) chafe % q% [9 H e, _ n/ u凸起(12) protrude 0 \4 g1 m+ z/ X$ p2 s; n凹陷(13) sag& o7 d( y; e6 g- b& l7 P) I! r4 _' X 粗糙(14) rough ; g1 P( u. K. k8 _9 l漆层剥落(15) finish missing , E! S* z6 w. b, W褪色(16) fade- E E n; _" Y* V' o) t( f$ S 积水(17) entrapped water 7 t7 M: j6 }/ C$ v1 [3 U/ h * J/ B$ T: l" n( F/ _0 n6 s 2. Common material defect terms ' }2 ?- u" i, D- d7 {; ?4 j材料缺陷术语; H+ v, V8 B. \1 }5 S; u% Z2 Z- ^# J; [ Material is divided in two categories: metallic and non-metallic.6 K7 u. F+ L* p$ E& [0 N 材料分为两类:金属材料及非金属材料 X4 M* R8 S7 P% F9 Y 4 A% d! \* T% ?' h$ a/ ~ 1)Common metallic defect: : j# k# a' [: A0 { 一般性金属材料缺陷:, D/ L9 U4 n$ E% I! _( a( b 4 u# Q+ u- S+ C, i 氧化(18) oxidize # a+ M; \# L3 R3 J/ i 划伤(8) scratch7 D/ z* ~0 _4 ?+ |7 ~6 W) B 扭曲(19) distort9 Q% v8 w: ~7 l) H' r( z 跷起(20) not in contour , i9 Q C/ q! ?6 W4 Y2 s( `" M6 H2 O 穿孔(21) puncture) ~! @$ |5 u" V0 r) T 碎屑(22) chip 5 i8 A5 p! M5 B 腐蚀(7) corrode 4 P, W- b6 I9 W 磨损(11) chafe 8 U+ T/ m. l2 [8 C+ i u$ w变形(3) deform9 W0 j: E) R% r. L2 p) u 风蚀/风化(23) erode% P# j/ e- \3 u: j5 u7 ^% f% v4 q 裂纹(9) crack x2 t" Q1 p( G2 E: h" C2 K3 H- | 2) Common non-metallic defect:0 Q b" \" [9 {$ |' h* E$ x 一般性非金属材料缺陷:7 ]% q+ f- r6 D - g4 R, F" w" I4 n; N* z3 e9 o 发霉(24) mildew , x& q( s5 o7 s" H7 l. n分层(25) delaminate ; L3 ^& f; v3 J& Z6 a# r* {7 f) {风蚀/风化(23) erode . E ]. Y) H; b% _) T裂纹(9) crack9 }$ W4 \) M, K% q- t 老化(26) deteriorate5 _4 g5 K' ?2 F+ X: R: h 起皱(27) wrinkle 6 M5 t! r& A6 R/ J! F6 z/ ~受潮(28) saturated w) f3 y3 b _撕裂(29) tear# `/ v5 k9 Q2 F2 z/ {3 E 穿孔(21) puncture $ s- F' A; o. ~8 S变色(16) fade 6 S6 H+ E. a1 G2 y, N陈旧(30) worn - x8 z+ P9 S9 ]9 P脱胶(31) adhere; z( u# Q0 d' ~ . g+ J: x+ h r1 n! C3 J3. Common part component defect terms) w v9 [2 W% C1 ?. b6 P6 Y( Y4 E 设备及零部件缺陷术语3 ^) ?( ?8 [3 G8 x Common part and component including : Plumbing, Wiring, Mechanical linkage, Fastener and Miscellaneous.# _' d9 N3 W; N; O 设备及零部件分为:管路、线路、传动机构、紧固件及其他。 ! x& U1 Q; F. F( H . D1 q" ]* `5 O+ `% [; T. u8 a 1) Plumbing defect 管路缺陷 : }, A8 f5 c0 @! K& ? 7 j# `/ |+ H; y4 H( I凹坑(1) dent 9 a/ X- v* f( m+ O% n4 p 爆裂(32) burst # o" _# G6 F. m9 Z# P, I擦伤(11) chafe4 h' Q; Q3 I v 滑丝(33) cross thread$ y" |+ O( y* T 扭曲(34) twist . X: V8 F1 r" U& f& N渗漏(35) leak . t( b& U/ v3 |9 v( C& Z堵塞(36) obstruct - U2 c8 }$ w4 z- L/ p& x- ~( I& ?& l # [+ S" x/ G! Z n2) Wiring defect 线路缺陷 1 } F) V% W& _' z 9 P+ k/ _. X4 W 腐蚀(7) corrode / T5 j3 D6 u( c! x5 R7 R' y ] 磨损(11) chafe 0 B# h* B0 O2 ~( }/ r相碰(37) contact/ m1 b; a5 \4 h8 o& j+ @3 m 断丝(38) fray ' |& c5 `: i7 g熔断(39) fused% ]4 D9 M4 F; V 弯曲(40) bend: F9 b* p) W2 {4 ?, o [ ( `: z* W+ K2 u, R 3) Mechanical linkage defect 传动机构缺陷 & d% [( i# `$ X5 l& ~ ' m% X9 o* |/ \ 断丝(38) fray 7 n9 K/ ~" H) h+ ]松弛( ) slack , }2 ]2 x7 U4 f7 `6 v P扭结(34) twist: q: R; d0 [% S8 P$ ]/ Z9 N( X 磨损(11) chafe* M- _" Q1 \ P& a$ ]9 n 脱开(41) disconnect; y' o* X9 i+ J" ?4 D4 _; r & n2 Q3 _, P1 T0 Z4) Fastener defect 紧固件缺陷 , H2 I/ \( H& z" k$ `2 d " S' u A, {' D! ]. I 丢失(42) missing, S. Q, a/ V6 J; H) _ B1 N 松动/松脱(43) loose, w1 R9 P Z1 |. k+ o2 r 腐蚀(7) corrode 2 O, N& e- Q5 E; R* O 磨损(11) chafe ! I/ z1 c8 a7 i 未关(扣)紧(44) not secure * ]4 r ~2 ]1 z# |, @ 6 v' I% U* r6 I0 t& @! l6 X S9 d5) 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. * k/ R, t0 r, o- \- ]9 m4 M, 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。 ( g; O* n+ y4 X& W' Y* y/ q6 o ( J8 @0 M- G0 p3 J- `" X+ Z4 r a). Sealant 封严 : Z4 d' ^9 e2 M& b; I ' ^0 H# ]* [! f$ X2 E" x 脱胶(31) adhere / O% U3 i( V8 a0 O( z7 s7 Q 老化(26) deteriorate7 U% l4 J* ~) Y7 F& Z: { 不均匀(45) inconsistent, q$ C3 e* y ~& }$ }/ S" ]5 \ ! n9 l# z, v+ ~7 M7 h b). Wheel Assembly 轮胎& f$ }% n/ {) i6 }" s' j% F 见线(46) exposed cords 6 ]) J3 k4 L. I2 ] 磨平(47) bald ! v% O5 m; s! u8 r$ L% y* ] 扎伤(21) puncture! r/ r6 E o6 ^ ~' z- I% `+ }4 s, S 气压不足(48) insufficient-air-pressure/ D+ d( g( D, g2 p ; i# D& s" c1 ~; y# X* H, m" C/ F c). Life Limited Parts 时寿件 % |: U, R6 E# K- v; Y0 x7 [ 7 F6 s2 `# F, z8 f" k 过期(49) expire$ ~: M: ~5 \; R( `8 K( z3 R8 Z 6 w; J1 T G$ v$ a+ A d). Placard and Marking 标牌/标识3 |! D; P& s4 k0 I' r w3 _+ j6 F! S 5 y) Q! l A# u* T& Q 模糊(50) illegible; @1 K' k3 }. c! W( o6 r9 D: c 缺损(51) damage " \0 s- b ` T: ^ 丢失(42) missing; G! u% V+ w5 u, O X+ q/ r5 S& j' { 翘起(52) lifting , ^! N3 E" K1 K0 ` 0 U! P5 ?' }' z9 K* b: f+ Y& j e). Slide/life Vest 滑梯/救生衣 & D* q, Q9 p( C3 t% ^9 R* B3 c 3 L- K" j( G5 j) _( \ y 散包(53) not properly packed $ s0 d) O) H) a0 {% N 变形(54) not properly sealed: d# Z' b/ y @9 z; }6 ?( y ' e) O# Y9 E' r8 T' Q4.general defect terms 一般性缺陷术语 5 i* L/ S( h! ]+ K 9 B; G3 D1 r. Q' r) z* R r. e$ b 脏(55) dirty6 ^! ]. k7 i5 S6 e: y$ R 陈旧(30) worn 5 J7 q5 ~. `. c, d 断裂(56) fracture; M/ O( ~0 i0 H2 B4 Y8 z2 @* q 磨损(11) chafe 0 V0 w0 P) y4 v7 {: t; W4 i 超标(57) exceed-the-limit$ g* ]- [/ S" C" G 丢失(42) missing& Q; y6 c2 J& d$ H D$ d1 ]% Z 腐蚀(7) corrode+ G1 A. f# X" ~4 o: P! M! l5 ^ 裂纹(9) crack) ?) O, g' f& K4 U# ` 空行程/无效行程(58) backlash* d4 v7 E9 M" x: B7 W 卡阻/阻塞(59) block % p: h" H8 |; Q+ L: q( z 鼓起(60) bulge 3 i' m4 |' w6 y3 b! @; D3 x 污染(61) contaminate" N, E/ @+ s+ E1 Q& T 不一致(62) disagree ) Y" J* d0 F. j4 t8 j D (电池/气瓶)被释放(63) discharge 0 f( l9 x y, r4 R5 s. Y 装错(64) dislocate3 w6 D" b8 ^" P9 R$ s2 H0 R* W 失效(65) fail * b1 h' i( l8 D/ g 摆动(66) fluctuate/ n! y1 G: w+ m! N6 t9 D 抖动(67) flutter ! t3 \* k+ V) z) {. A 不够/不足(68) insufficient4 j! ~2 g3 s7 m: s' U# U! R 不工作(69) inoperative% h x* C# }+ o* L* S (不)亮(70) (not) illuminate" u- {8 N5 e |+ l* R D6 H6 e) s 干扰(71) interfere 8 z e( }' R/ n' i 扭结/缠结(72) kink& P4 H& M( }2 e 走向错误(73) misrouted# R1 M2 I2 e' }% V5 [ 漏装(74) not installed ) o8 \4 }1 x% w# i r 相磨(75) rubbing r2 X6 X& u2 R- k) E# r 干涩/缺乏润滑(76) un-lubricated7 D5 K' f3 Y9 r, I 不能复位(77) will-not-reset/ p4 R q1 [) ~ " }2 B; H# F' C7 v! w# x/ R (1) dent: 凹坑8 |5 S2 ?& O" O9 i2 e A depression in a surface caused by pressure or impact., ~) y" P+ {$ I! L 受压力或冲击造成表面的下陷。 # g* o( s. t. t2 K For example: Left horizontal stabilizer outboard leading edge at WL 368.25 dented approximately 2 inches in diameter.(Area marked in red)5 T3 \! ^6 m( F+ t* R+ L n8 g 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)。/ p; \% g3 A0 O, h& g! I2 {$ Q6 `$ y 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---& t7 g; K7 x# ?. D 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 q Q/ }% {& @& ?# A3 F6 s 9 @, Y5 r2 ~8 o% y/ z3 }(2) notch: 凹槽 / P8 N3 S7 i3 b; Q1 p& X A “V” shaped cut or protrusion / Z; n6 T9 o3 C7 r3 H+ U$ q- Q5 q V字形的切口或者突起6 V$ G% ]5 }6 H7 X+ q For example: Forward L1 entry door number 1 floor panel has a 1-inch notch 6 inches from the forward right edge. ' v$ t3 ]& ^3 O 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 ; m; X7 \, B. F( U2 b- p! }- A; [槽。 ; w( @! c5 L( X% LDetailed 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---.8 b- j2 Q* Q3 X( t4 N 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。* i+ q1 `% a0 g+ O! l9 I. B : V/ a' K2 l/ o% s# L9 q (3) deform: 变形" s* d. I2 z7 \+ ^ To misshape the original form& y: f9 e8 a0 `7 |) i* x3 ? 原有的形状发生变化) h6 M4 F& |7 s For example: Left wing number 2-fuel access door is deformed. . u" S( M$ X( p 左大翼二号油箱盖板变形。7 d5 a2 t6 J0 q, J) I( G Replaced number 2 deformed access door in accordance with AMM--- Carried out fuel leak check in accordance with AMM--- with no defects noted. ( E. f6 T4 a6 ]% ]9 u 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。9 o# e# m! i" k 8 K. i' f. B: j+ Z& w' u (4) nick: 划痕* m3 I3 e. c5 U5 W4 J5 D* o A shallow notch, cut, or indentation on a surface.: ^2 N. m4 j' }+ H 表面上的较浅的刻槽、刻痕或缺口。 6 x# l Y2 {; l7 u* r For example: Right environmental control system (ECS) access door, after right corner has 4 nicks on external surface . Area marked in red. ) I. T. {% c5 X( S 右空调舱门右后角表面有四条刻痕(已用红笔标出)。1 T: N2 i; |6 D z( j / K1 A# e4 x3 |! b3 b Detailed inspection carried out with reference to SRM---no delamination ! N3 |4 q9 V0 g" Q. H4 Z7 cnoted. Carried out permanent repair by filling nicks with fiberglass and epoxy& ^# ?; B, g; E& ^8 u' d resin BMS-387 with reference to SRM---. . n3 O8 i$ P& b+ P d: W( T0 R4 j0 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 / V2 m! _9 c0 q, M! d. B) g4 i理,使用玻璃纤维及环氧树脂BMS-387填平刻痕。# s' l/ x% o$ t) n* Q ' l2 ^1 e& O- g( Q2 A/ m' x* L (5) pitting: 点腐蚀/砂眼1 h5 D2 D; u( t" _+ Z, D; u+ r Small cavities, depressions or scars on a surface. 1 q$ l/ I" {% |4 F 表面上的较小的空穴,凹陷或凹痕。' T' q8 C' i9 i5 \1 W$ d7 Y( b, g& t/ ` For example: Left main landing gear number 1 brake aluminum hydraulic line has pitting. : p% I8 ?+ W- V6 z- \ 左起落架一号刹车铝液压管发现点腐蚀。 ; ~9 X3 c; z/ @ Y) R0 Q% o3 u, y Replaced left main landing gear number 1 brake aluminum hydraulic line with6 _& b p$ e. t! Z- a serviceable hydraulic line in accordance with AMM--- : P* w0 T- {' F6 Y* A 根据AMM—更换左起落架一号刹车铝液压管。 - p1 b& B' Q% K a ' U0 O& h1 P* A# I0 E+ P; \(6) broken: 断裂 , _5 m# @8 D- ^9 R6 H7 X% b4 y Forcibly separated into two or more pieces. + }+ y$ c3 P1 n9 z5 j* U! [/ \/ B( q 被分成两半或更多块 ( g5 b8 f+ y; v* L' |- S8 Z For example: Flight deck entrance door has broken door latch and will not lock. * q. f) X6 v2 g8 |$ b 驾驶舱门锁销断裂,锁不上。 6 M! P" \/ ]: C/ A1 Z& c+ o Replaced broken door latch on flight deck entrance door in accordance with AMM--- Operational and functional check good. ) d3 H) M) p& g" X5 I 根据AMM—更换驾驶舱门锁销,操作检查正常。 ( j' X, M# m# f* h; `& y5 i& V 6 N+ g- y& m! Z( u7 l( u(7) corrode: 腐蚀 4 M" @# q" i$ _& ]9 O4 G To dissolve or wear away gradually by chemical action.' _1 Y5 C0 U: t 氧化或化学污染造成金属表面逐见破坏的化学反应。 3 f6 X0 ~2 b/ Q, L- l* F- `( SFor example: Floor beam at body station 360 and wbl 25.1 has moderate corrosion 2 inches in length and 1 inch in diameter.. W* E. i+ N2 ~, L/ V' G9 b; } 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)。1 T! B3 x5 D4 V 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 53-099-84.7 W* A, y; Q( T5 ? 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。 " x4 u" ]: a 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。 6 y8 ^3 S3 @6 |) _" l4 { & C' z$ ^" U0 Q (8) scratch: 划伤" m- b6 a x5 L A thin shallow cut or mark on a surface: d1 k& [ [1 A4 z k2 i/ f 表面的薄而浅的切口或痕迹。" J) O& s8 \- {1 c. y" I. H For example: Left cabin external windows numbered 12, 16, 17, 21 and 27 are scratched (obstructing view) " k7 {+ K1 x4 X& I% c6 p& l. N% { 左客舱外部12#、16 #、17#、21#、27#窗户被划伤(阻碍视线)。 , K, o9 i1 ]$ s) B' V z; q! N9 D 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.1 v) Y K% {$ O/ o 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。 ; c; {0 e2 u. F) t4 D / z+ i8 Q+ \7 V! c3 V0 n/ S3 A, G (9) crack: 裂纹/龟裂9 L; U: D4 F) b6 ]! U4 U8 ~$ k To break apart without dividing into two parts.- l1 M& W* R% l* e5 \$ |+ C$ S 裂开但没有分成两部分的破裂。- e' Z( _4 i' h# M) j For example: Number 2 engine fuel control cable located at Body Station 360 and Water" t) V& _- K2 ~9 }3 W. a9 F Body Line 25.7 has cracked turnbuckle.0 X/ `- L3 l" h0 Y ]" v: W: B 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。; H8 B- k) r! ]9 g; l Replaced cracked turnbuckle with new turnbuckle in accordance with * v; |% H7 b+ o3 | x# r# y/ LAMM--- Travel and functional check carried out in accordance with AMM---,. `" Z5 u, T6 {9 G; H+ }" M: ? no defects noted. 5 `( q! A% q/ o# V. w8 o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。" B# o2 P* F# \) v0 u0 I1 U5 M3 v + x, z9 ]- ?" D( j& o0 T0 R' B (10) burr: 毛刺 3 ~: I6 |& P- u# }( YA rough edge remaining on metal or other material after it has been cut or drilled) }0 o) l+ I# P1 k2 V/ i 被切割或钻孔后留在金属或其他材料上的粗糙的边缘.) q& U* B& Y! t0 d For example: External fuselage repair at body station 727 and stringer 9R~11R has burrs at. J. X. Y( n8 M9 u8 ]5 V all drill holes. * r7 `% A8 j1 q( Y 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。 $ S! R0 E5 w1 l8 s' Y: h Removed burrs with rotary file in accordance with standard practices and( I: d* g ?( M9 R9 n' } SRM---. * ^+ `! Y( Q; u6 T. Y5 A& E% Y' a 根据标准施工手册及结构修理手册—的要求打磨去除毛刺。: y6 o/ ?$ l2 C }* g : f: b5 ~+ R) i' q(11) chafe: 擦伤, _' s# Z+ s' r3 Y9 E4 q' y To wear away by rubbing. 9 L7 W( y5 I- \; Y$ I) \9 H因为摩擦而损坏。 ( E6 k" A7 s* W5 Y- WFor example: Forward cargo compartment after corner threshold chafed by cargo door. : Q/ l: p) v9 f" Z- c 前货舱门槛的后下角因与货舱门相磨导致擦伤。 * s9 \" t. Z+ D$ u8 d8 I' l$ ?$ b Forward cargo door upper support bracket worn. Replaced support bracket in* ~5 ?4 N. [, f* m6 P; F: U7 p accordance with AMM---eliminated chafing. & r: |6 b& I7 N, O8 v% T检查发现前货舱门上支架磨损,根据AMM—更换该支架。5 i& w o: F+ U7 g9 x0 l3 ]3 U 9 t: Q, F$ ^% A3 D(12) protrude: 凸起/突出8 m- F4 H5 V! R* B8 L To push outward.3 {3 \& V$ L$ D7 m 向外伸出。 / ^1 {0 d) a+ C" x m9 Z/ o. zFor example: Forward external fuselage servicing doorstop is protruding through access8 G, W6 X- b8 ^9 ^1 z door. * P7 E" R/ k7 Z& F3 T 前外机身勤务门止动点凸起。 - y' t6 e* l+ O Repaired forward external fuselage servicing access door to original contour with reference to SRM---. Adjusted doorstop to eliminate protrusion in accordance with AMM---. - a: {) o. F# {+ s* R( e- } 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。; B8 D* e3 j! z; p+ _+ `2 Z 9 H' ~: \0 A& e) D: z( [2 L$ Q" m (13) sag: 凹陷! F" {. B! V5 ?% w To sink, droop, or settle from pressure or weight.. O( J3 F! y0 V 因压力或重力而下沉,下垂或下陷。- r: D4 v0 N1 u; p9 z For example: After cargo compartment overhead ceiling panels are sagging.% h( k [3 I" N/ K 后货舱天花板凹陷。 R& {' K8 G1 U7 T) {) E a# z. uDetailed inspection revealed ceiling panel screw holes worn. Replaced _, \0 C- H. t% k, x, g' kunserviceable sagging ceiling panels with new as referenced in AMM---. 0 L3 i; L- l0 C8 Z& x) N4 H, F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# u$ I0 L. A# C/ n 板。) H: p3 r0 |" P9 _ ( C. K3 a+ V4 z6 R& J4 ?0 x6 y (14) rough: 粗糙2 q) J; z! k/ ~6 [6 l Having a bumpy, uneven surface." u. c- K1 D3 P1 Z% O F7 o$ }4 d 表面不平坦,有起伏。3 y0 ~/ {7 Z& x, D For example: The protective finish is rough at the number 1 engine inboard pylon. / k2 y @$ Q! l 一号发动机吊架内部的保护层粗糙。& X% |, N4 J' _ Removed rough protective finish at the number 1 engine inboard pylon in ) l! H; j5 U4 E8 z* zaccordance with SRM---. Applied 2 coats of enamel to restore protective 8 h7 a0 z8 d+ Cfinish with reference to SRM---. ' ?( @& E }( U+ |' c* X) I 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。 ( E& N+ k8 P- G5 m / o1 R j/ z, |' Z* b' G$ o' u (15) finish (missing): 漆层(剥落) ( H! J( r% H4 p6 R9 p' V3 {5 xTo protective material used in surfacing and finishing flake off.5 ]# T4 j8 P- [9 x 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。6 c$ d* I& U: q- {$ b/ L Z+ ?* o For example: Fuselage skin protective finish at pilots and copilots number 1 and number 2 1 |2 F2 n3 }3 z( a; k8 }/ b# Xwindows missing. # P5 s' M% [2 r4 V% o3 J5 K4 x正副驾驶1号和2号窗上的机身蒙皮保护漆层剥落。 , t& C; A3 ]# c" u" JPrepared affected area of fuselage skin at pilots and copilots number 1 and " z$ u' L; X5 t2 B4 Vnumber 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. . i7 w% f5 `; n A/ {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。2 _( Q' P# L2 x) [ % g1 e7 ^. a6 O! {6 S$ d# \ (16) fade: 褪色/变色 & v6 z" y5 W) T i3 U XTo lose original brightness or color.( }! g8 T$ w: R8 T* v 失去原有的光泽或颜色。 . j) d+ a4 v$ T- |* FFor example: Number 1 and number 2 engine intake cowling chrome is faded." H+ a* Z+ x6 V ]' H* Y 1 号和2号发动机进气道的铬层褪色。 / ]- V) m \; [' l! s8 S Polished number 1 and number 2 engine intake cowling chrome with reference ) K y9 ?* m$ v. N, q; ~to SRM---. 5 H8 b' H x2 E& z' E5 E 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。- T- I4 I$ [5 e l) { 4 ]( g0 r; @, ]9 d7 V$ y1 }- K/ O* m (17) entrapped (water): 积/含(水) 7 a6 M( Q6 y- J/ j" b9 H$ w- }6 iTo collect in an area. ; ]8 R) U+ B% D1 a1 R水或水汽在某区域内聚集。 0 L: N5 E& ~% t1 {7 xFor example: After cargo compartment forward bilge area at body station 840 has entrapped$ f7 r9 j# }3 V0 b1 ~% s potable water.+ D! q! w% g; C7 Z+ P0 p7 ` 后货舱在机身战位840处的前部区域有积水。! l+ E G- H0 T7 F. K Detailed inspection found pressure drain valve clogged. Removed,cleaned and reinstalled pressure drain valve in accordance with AMM--- Removed residual entrapped potable water./ W2 ~# s" d' T3 y7 f 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。& {0 A9 A9 Y" { e% p % \2 T8 Y% ]1 |* C! ?1 [6 a8 s (18) oxidize: 氧化 5 ?1 f: J9 x5 I2 AThe containing of oxygen usually caused by natural elements.2 c. j0 y9 X" g; _ 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。 f: g" x; F& E9 r; bFor example: E-3 rack lower after corner is heavily oxidized., |! I' v2 ?7 S4 y E-3架后下角氧化严重。0 D* G% b" e/ S2 ]$ z: t9 \, f$ m Removed oxidation at the corner of E-3 rack in accordance with SRM---. 1 n: B2 C# V6 `7 g3 A5 ~ 根据SRM—去除E-3架后下角的氧化。 & L9 n: c5 m( D6 a. e4 v" S+ D ( d0 F% n2 X* c6 J- _5 {(19) distort: 扭曲; _! p6 X8 s D7 _ To twist out of a proper or natural state.: l/ P$ H8 s) J4 k2 P2 H 因受到扭力而导致原有的形状发生改变。 / Q1 j% o8 B* f- wFor example: Access panel 2145J to left wing number 3 slat actuator distorted. / \' O+ ~% o8 K& k! u b7 n( v. | 左大翼3号缝翼作动筒的接近面板2145J扭曲。9 ~) \) F. |9 A6 e2 D Replaced access panel 21458 with new panel in accordance with standard 0 |" E' C. X+ {# epractices and AMM---. Original panel declared scrap, tagged panel as much 5 G, p/ }1 b4 p% @and routed to MSC to return to customer.8 U& ?- b5 l' k5 R: m 根据标准施工手册及AMM—更换21458盖板。旧件挂牌送航材处理。 & m8 g# c" W( {$ R: ~ 6 i1 ?6 ? ]! |$ o* }(20) (not in) contour: 外形/轮廓翘起" y5 }7 ^9 j1 a& s+ O6 w [& u A shape or outline is deformed./ t( F" u0 t0 T' z, x 形状或外形轮廓变形。 & Y6 q/ ~ H( KFor example: After lower corner of after fuselage external servicing door is not in contour0 C* v' M! ~/ `4 v$ c with the fuselage. 4 Z' ~ `, @! ?2 H% V后机身外勤务门后下角翘起。7 a2 k$ P6 Y4 p# M$ r Adjusted after fuselage external servicing door to contour of fuselage in # C& z B! J3 v% {% paccordance with AMM---./ N" X* H/ o7 f0 u0 V4 M 根据AMM—调节后机身外勤务门正常。% G9 X( H4 Z! E% `( e7 [ , u6 [. s2 }' c# H# o0 a1 ^. R" C(21) puncture: 穿孔/扎伤) P5 o' ]1 t6 B, u To pierce with a pointed object.7 X7 ^. O0 i; N- D7 {6 L9 _ 被尖锐的物体刺穿。+ x: U' e0 H- O8 E# q0 S For example: Number 4 tire is punctured. * s- P& [ V6 Q 四号轮胎扎伤。 ( w: `& Z' i+ \& b1 M Replaced number 4 punctured tire with serviceable wheel assembly in! N9 z0 B8 }$ a1 x) { accordance with AMM---. Pressure check normal. 0 O0 J$ W: ~+ V1 {; {0 ]9 E 根据AMM—更换四号轮胎,检查压力正常。" W0 ?5 p; d; ^9 { 0 ]# n3 |% j" Q! J4 t5 L! o u4 | (22) chip: 碎屑 ' Q3 f2 F: c& N$ hA small piece broken and missing from a surface.4 B, i( s g" O, ?; h) L Q 从表面剥落的小碎片。+ f3 g0 o2 G$ P& G5 h. p+ O For example: Starter magnetic chip detector has evidence of metal chips. , a' S7 o, \' S- O) J/ E 起动机磁性堵塞上发现有明显的金属屑。7 u. q7 e* i) _: t, e: S Removed metal chips from starter MCD. Drained and replaced oil, operation ( H F1 `4 @) [and leak check good in accordance with AMM---. Reinspect next “A” check as( s& H& O1 S# J$ V per attached EO 80-003-1.8 i6 J4 t) R. u. v$ ?2 T% F; c; [ 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。 1 t6 R4 B1 _6 Q7 n# X3 J% y # w' m' b5 h3 A6 y+ w1 X- y$ b( j! Z(23) erode: 风蚀/风化5 E8 J6 m* T1 F! O. q( x7 F To wear a surface away by weathering, abrasion, or foreign particle.! d- V- i0 j, u- b n3 p& }. W 因天气或外来颗粒等原因导致表面被磨蚀。 & d9 t) S1 t+ p' jFor example: Number 1 engine intake cowling eroded 360 degrees, 2 inches in width from 4 z$ A. C* o% k5 Pcenter of forward leading edge.6 i7 I+ i, M4 Y) C+ W5 e 一号发动机进气道周边风蚀(2英寸宽)。 & P8 }+ u( O4 _Removed erosion by polishing surface with reference to SRM---. NDT 0 B* y% H9 g* U+ [8 C. s. l: Linspection revealed 0.02 inches of material removed, remaining material 0.231 l9 n0 g, C7 ~6 l8 S: u of an inch within limits to SRM---. % m9 }0 i" _/ v/ g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% T" Y& i' ]: r; s% s7 L 少0.02英寸,尚余0.23英寸,在SRM—规定的范围内。 + I k! ]4 Y# b& x% _2 L 6 Y! ?* [2 s$ y: P(24) mildew: 发霉5 ]3 J1 \1 X9 l$ r* t A fungus growth.& h. @0 X) o% Z1 W7 T7 ` 有机质滋生霉菌而变质,常见白色的生长物。' T- P# \" B- }7 `* T For example: Forward cargo compartment insulation blankets in after floor area are moist % y2 Z3 f6 i w- l1 W6 u' \, sand have mildew. % {3 t$ D" u; r8 Z" {前货舱后部区域隔热棉潮湿发霉。 . ]3 G" O/ `3 `% X% X0 m/ |* \Eliminated mildew and moisture of forward cargo compartment insulation$ H1 O: r& n# t6 l blankets in after floor area by fabricating and installing new in accordance with( b: p' q6 Y( O SRM--- and AMM---.0 c0 v* o8 d# ~5 b/ ~4 U- w& |8 s$ Z 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 ' R; G' x% \5 l# C4 ~/ V发霉的隔热棉。 ) g1 }" N& e" Y. c# ^, B: ]! s! O. |" ` & ^; |" D& k5 [5 y9 \(25) delaminate: 分层 , x& i$ W3 i; }0 h1 BThe act of separating into layers. ( C# D3 v# w9 B) b压合在一起的材料互相脱离或分开。 4 t' A% ]; g1 Q9 _& v! N+ {For example: Nose radome delaminated from impact of “bird-strike”.5 P/ K( j ` a4 @) g 前雷达罩因鸟撞导致分层。 ; r+ p* x3 `7 f Removed delaminated core section and replaced with new with reference to( J% O5 [8 w( S% ~4 ]$ Z( K h SRM--- impact test carried out. Nose radome OK for service.; s- g$ E1 d& ~4 s. \1 v 根据SRM—更换分层的核心部分并进行冲击测试,检查正常。* j1 z6 v, c" s5 T7 D! {1 v6 R( E : X1 G/ l" C3 O5 [2 G5 ]+ ] (26) deteriorate: 老化/ i3 C- `4 O1 N6 Z; ? The diminish or impair in quality, character, or value. & [; h! d3 q2 Y9 ^* d5 \橡胶、塑料等高分子化合物,在光、热、空气、机械力等的作用下,变得黏软或硬脆。9 |% T4 e& R2 q" B! _9 D" c, b For example: Number 2 engine to pylon fire seal deteriorated. S; i1 ~0 C. v' }9 ~% I# f 二号发动机吊架防火封严老化。/ m3 y+ S5 a% E8 T) r K3 i* [ Replaced number 2 engine to pylon deteriorated fire seal with new seal in 0 B5 \! C% \" c" I. o" f3 O$ x4 faccordance with AMM---.. X# W4 X1 r8 U; l6 [ 根据AMM—更换二号发动机吊架防火封严。" D# f$ \$ D8 [" G- P $ z& N$ l2 \) M, V (27) wrinkle: 起皱 1 Q3 Q7 K8 k6 [A furrow, ridge or crease on a normally smooth surface.7 z. z7 u& T- t6 ]8 B X7 r 正常的平滑的表面上出现的皱纹,或折痕。 : j3 o+ h# w. `/ r7 tFor example: Forward galley wall at flight deck entrance has areas of wrinkled wallpaper. 6 _) z, t( i+ D5 D+ F 驾驶舱门过道的前厨房墙纸起皱。 7 D! D0 P" ~* T( l Eliminated wrinkled wallpaper at forward galley wall at flight deck entrance by4 ^$ c& Q# [7 y' D3 y G replacing with new in accordance with standard practices and AMM---.! H7 Z7 I N# v) M 根据AMM—更换驾驶舱门过道的前厨房墙纸。! O! v9 e! f1 y 7 ^/ n# V+ y& s+ m2 ?5 h" Q (28) saturated: 受潮 : T0 N3 a. W9 Q6 Y1 RSoaked with moisture.: R; U0 ^* ]1 t* s# l$ ^9 @ 物体吸收了水分的状态。 / O$ t* B5 }, x- C% Z" z9 _For example: After cabin floor carpet between lavatories B and C is saturated with water. 5 }% A1 l8 J* a0 Z 后客舱厕所B和厕所C之间过道的地毯受潮。 ; l7 ^! @0 @% j Eliminated saturation of after cabin floor carpet between lavatories B and C by' f3 y- M5 D5 s. u; p replacing with new in accordance with standard practices and AMM---.+ L" j: J/ k! R 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。0 i$ v, c0 ~, G, H P; R . ~. a; H3 v% M% k. e1 w2 J( m+ J9 I (29) tear: 撕裂 8 A N# k e* U# C* ]To pull apart resulting in a tip.9 ^2 M% ^# f$ H' X 裂开后分离。- i8 T7 z+ b- f8 r9 |" i For example: Number 8R window shade in main cabin has a tear. % ?4 H& d7 c' E 客舱8R窗户遮光板撕裂。, e7 q4 F' T$ M1 J; y/ l Replaced number 8R window shade with serviceable window shade in - h6 _7 k: s) S+ {1 @* Q+ taccordance with AMM---. ! h/ ^& _3 n6 ] x/ n, F9 N# m7 S根据AMM—更换客舱8R窗户遮光板 & _% F9 y2 p4 v& Z/ V, b' X ( f1 l: m& R2 r" U* G/ j0 x (30) worn: 磨损/陈旧 % n7 g- V+ d8 H" i0 _* {: |$ P5 @Unserviceable due to excessive wear. & @/ b3 S3 n/ s由于过度磨损而不可用。 & _1 d* h+ [3 @8 LFor example: R1 service door upper guide and door latch on doorframe is worn.$ _0 _2 G( J0 ?$ L z R1服务门上导轨和门框的门闩陈旧并且磨损。; x9 N y5 K$ U: C3 } Replaced worn upper guide and door latch on doorframe in accordance with 1 l8 f* O3 @' q( N3 ^0 z0 y AMM---. Operational and functional check good.& ~& r; F" G% _$ m b) R7 z 根据AMM—更换上导轨门框的门闩,功能测试,操作检查正常。$ u' k8 I3 Z; Z1 H q; U" a 4 l |- B4 L3 ~, w9 D$ o (31) be not adhered: 脱胶 0 u @& V- Q: m: l1 P, o% n) ?Unsecured and not positioned in place by glue or sealant.6 B& Z3 F" W2 t: K- f 因附着力减弱导致脱开。& V7 D% R( V* m; k For example: Left emergency exit hatch external “EMERGENCY EXIT” placard is not R! z3 a/ s8 U" Y( Z) k2 j adhered in place. 9 z, r& ~& T: Z- [% c) g2 p左紧急出口舱门口盖“EMERGENCY EXIT”标牌脱胶。! a* `4 g0 A6 G R Resealed left emergency exit hatch external “EMERGENCY EXIT” placard in$ n; w/ B5 S0 L6 G8 Y3 ? accordance with standard practices and AMM---.- H( A, }9 ~ [# M$ | 根据标准施工手册及AMM—重粘左紧急出口舱门口盖“EMERGENCY ' x. I! x" O1 AEXIT”标牌 # o1 f6 d. u0 ]! R( V: h 1 F ]- _; _4 v5 W; }+ Z. N: @ (32) burst: 爆裂' v( e' `2 ]2 {' W4 a To open and suddenly come apart from internal pressure." \, d3 X4 N. m5 k, ` 因为内部的压力突然炸破或剧烈的爆开。7 j1 x+ k% T- \& ?' J9 u For example: “A” system hydraulic pressure line located in forward left wheel well burst: t& K N+ [" U' d" `/ s& } during landing gear functional check.! \& [1 u- t' x( @; A1 \' {: 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。 6 E5 r2 z/ I6 ODetailed inspection of “A” system hydraulic pressure line,revealed grommet# c* ]; T9 P0 U of retaining clamp missing resulting in chafing. Installed new “A” system, L1 r( [- W, P+ ], S9 S hydraulic pressure line and clamp in accordance with AMM---. Operational6 T6 B0 ]0 G7 _8 I and leak check good. t* W. W z9 |2 N) b4 N 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 X* E* g4 m0 e! L# G4 P6 `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% O$ E1 t' h6 V; ?* X: E 漏。 & g+ e( e7 c& X% W- L+ @ 0 S& V: {* U: S$ g& K9 U (33) cross-thread (pertain to plumbing) 滑丝(限于管路)% ~/ E# H1 S( I7 I+ H To damage threads to an unserviceable condition. - k6 i& w4 C' P螺纹损坏后不可用。 : _4 J3 w4 i! S* v8 D' F+ R8 C, l2 C6 tFor example: Left wing number 1 ground spoiler actuator hydraulic pressure line has $ e ]4 \3 e; \5 Y7 Ycross-threads at “B” nut. ; G- ]8 T. u5 T6 x* p! B3 o左大翼一号地面扰流板作动筒液压管B螺母滑丝。& e8 t7 }4 a1 I, S& W Installed serviceable hydraulic pressure line at left wing number 1 ground 1 I! X+ I- S: e6 C: sspoiler actuator in accordance with AMM---. Operational and leak check good.8 j/ y2 i/ g: M. e 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, 1 r+ a6 z" I! P5 ]* }' W无渗漏。 : Y2 } I! k& k7 }2 @. {& j9 R5 y. B * ` X6 i; f/ z$ J! I(34) twist: 扭结/弯曲 5 E8 q* n L% k" y! B/ X. bTo alter the normal aspect resulting from torsional stress or strain." q& ~7 M( n) ~8 R6 V1 f; J 因为扭曲的压力或者张力导致改变了正常的面貌。2 s% A" Y" [/ Z! }! V1 `! @ For example: Right environmental control system intake door linkage twisted along routing 9 v. i6 B$ j ^4 G- z0 gto exhaust louver. 6 r- g4 ?0 c6 q' ^4 z/ i8 a右空调系统进气门传动连杆朝排气口的方向弯曲。 8 T$ B# O% d( I0 t) yDetailed inspection found broken bolt at eyelet connected to exhaust louver. $ P$ ]# X8 P& n( O+ c! dReplaced broken bolt with new and reattached eliminating twisting with ' `% {! _0 E% c8 g6 xreference to AMM---. Operational and functional check good. + } y) q7 d% u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 8 @% i% U0 E) y" h: b1 V+ w; q/ P常。% n1 P# X" z% Y) c# Z' q" a7 p% P7 L 2 `# R t1 @$ I/ l2 t3 O" i (35) leak: 渗漏 + p: \) d# V p6 H B$ EThe escape of a liquid or air in a system. 1 b* D+ ?4 E) H+ w系统里的液体或空气逃逸出来。 ( @9 o9 N" t$ p% H5 H) {For example: With reference to routine task card 37-265-1 pilots pitot static probe test failed, k5 B& P- ]; m* M: s8 v due to leak in the system. 4 Z6 V; R6 W* l* W4 \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。 0 ^: N. n. G! K |& CDetailed inspection found loose connection at pilots static port. Removed “B” # m% K3 m( D6 h- D3 C% P nut and inspected with no defects noted. Reassembled connection and leak 9 E8 ?( V: `( y& _6 F: v) I check good with reference to AMM---.. u! z! j9 g! F k 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 d& ]: Z5 J7 m. i# g, o0 _/ d 陷,根据AMM—重装接头,渗漏测试检查正常。 2 z, Q" u" b7 O) v " l( |; E% q0 R& U(36) obstruct: 堵塞 * M9 F) l# f2 ~6 p5 F- t4 L' }Blockage by foreign matter.) g0 r1 V) C9 x8 h% Q 外物妨碍管道的通畅。$ b0 z, C) W) x+ y0 H) V For example: After lavatory service panel inoperative, suspect obstruction.; k$ y& ^8 |5 Q U5 S2 s7 `# i% N 后厕所勤务面板失效,怀疑有堵塞。 + \9 D1 V4 S% d- r; s/ f Detailed inspection revealed drain system plumbing obstructed with foreign matter. Cleared foreign matter from drain system plumbing, operation check good in accordance with AMM---. * d, o$ n4 z# _/ g% a3 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。 % t5 O8 ?+ D+ ^7 P C) k; @) c% c- I# L! c6 H (37) contact: 相碰 / H( b4 \1 L/ \7 V% ~; ]: RTouching of two surfaces or objects. % @, B" Y) o& b; D) Y( k两个表面或物体的相碰或搭接。! \* [* X$ H, ^4 o+ F For example: Left wing trailing edge has aileron control cable contacting pulley bracket at$ r/ P! {0 e( ~! e9 I* f4 E2 D4 X+ U WB Station 245.9. $ w* v1 w# L& p2 h: U左大翼后缘在WB位置245.9处副翼控制钢索和滑轮架相碰。4 m" i5 p2 T" B* f Detailed inspection revealed pulley bearing worn beyond limits. Replaced with 0 r. P# B- _, xnew pulley in accordance with AMM--- travel and clearance check OK.! n9 k/ K% N/ c4 @ 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 : [0 V3 [% X4 @) ?7 H* ^7 y% B6 A间隙正常。, S/ Q6 J2 e6 @ - ^; Q* D; g; s) |( v(38) fray: 断丝/磨损3 ?& g- G, H5 x l# v1 F4 P To wear away by rubbing.2 s! H* V/ b/ e6 S; {! p6 T3 v9 ^ 因相磨或反复拉伸导致的损耗。 ( a$ L# Q. V3 c0 i' ]+ H0 \0 `For example: The lanyard attached to the after end of the right access door to the APU4 g5 x4 l9 H9 l( h, { R1 J compartment is frayed.) {6 |) _8 J+ ] p 右APU舱门后端系留绳断丝。 , @% y/ b. ?2 j# V2 i' ]& URemoved and replaced frayed lanyard in accordance with AMM---. ! l7 V1 d1 a. F/ x根据AMM—更换系留绳。0 \) N& i6 d0 T8 S+ u* e 5 D; C# a% ?0 P$ w2 P (39) fused: 熔断8 k: L( \2 N+ y: p To become united by melting from heat. ' ]4 j* ~- w* ]) j. u3 ^) n( U因为高热而融化连接在一起。 2 c |' B' x% [# _; u2 A For example: After galley coffee maker inoperative. Detailed inspection of after galley coffee! c' s* ]7 P8 z maker revealed thermostat wire D34768 fused to temperature controller wire- V4 q& u7 C4 R. a. q E57689. 4 ?$ g9 J, x9 u @: E6 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2 l/ e* {, Z9 {* ^3 B- T9 i 置导线D34768与温度控制器导线E57689熔断在一起。 5 v; t+ y1 a$ h' e. Z9 XReplaced wiring with new, operational and functional check good with : i. }# e% a" rreference to OHM---. 5 y0 r0 }- r; f8 v/ ^根据OHM—更换线路,功能测试正常。 ' x1 F+ E7 ?1 M; V/ ^; q: e * ^ W0 [* w3 [; }2 } (40) bend: 弯曲 2 T' p- d% O4 A" C$ b; `4 zAltered from straightness or original position. 1 l' Z" g* M4 S% s! H改变平直或者原有的形状。: L8 }# ]3 ~1 a/ r- H) M/ v# ^ For example: Forward electronic bay door left hinge bent.5 L: x; D2 i& X+ R, u$ } 前电子舱门左铰链弯曲。) P3 s3 Y% {2 B2 K Replaced left hinge with serviceable hinge on forward electronic bay door with0 T: c. Y) |+ Q( P reference to AMM---operational and pressure check good..; a2 C: G- {0 L# Y/ u2 Q 根据AMM—更换前电子舱门左铰链,功能检查正常。; Y" q& ~7 o; ]0 k* F 7 Q9 ^9 ~8 |: q/ o7 _; \ (41) disconnect: 脱开 i! L+ U: u( L8 e: pNot joining resulting in failure.3 z; o( ^* N) r* ~$ [! y' k S- l 因没有连接而失效。 5 n, W, R3 @; l; ]+ u8 aFor example: Left environmental control system pack temperature control has disconnected ( Y' S# D+ I7 @* B. Ocannon plug. 3 }5 @" Q% m! s- s. L' C左空调系统组件温度控制插头脱开。) R, S6 i4 {( V, n$ N Reinstalled left environmental control system pack temperature controllers6 _$ h4 p* @/ X9 d3 u0 d cannon plug, operational and functional check good with reference to AMM---.3 u* s1 K& a: E. \9 q 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 ( x G- G9 \! ]' b查正常。, M5 I o3 {& g8 g$ x " `; k5 E3 \+ W, ` (42) missing: 丢失 : q1 N8 @6 r; P# S$ {8 K) w5 f# L Not present. 9 z' y1 @& Z5 d4 E 不在位。 7 w: m% A) o$ Z For example: L1 entry door has 3 each door stop pads missing at the after middle section of5 u; R5 G6 W+ O) W a1 p- q m the door frame. # L* N9 ^$ w: @7 j- W# \4 K, Q g8 V5 r9 ~左1号登机门后门框中间位置有3个止动钉丢失。 + ?; A! \/ a- f4 N; j4 OInstalled 3 each door stop pads at the after middle section of the L1 entry door$ k" [$ s% q* [3 o frame in accordance with AMM---./ Z/ V0 @+ U1 T/ b' z 根据AMM—安装左1号登机门后门框中间位置的3个止动钉。' v7 }8 g3 c* H0 [+ B ; ]6 V0 ~2 S. n) v, j5 ^! h(43) loose: 松动/松脱- d& p& Z9 v/ l+ V Not secure.' T- ?+ ~ d! t, o" A" n' T+ J 没有紧固;活动0 [. k8 y- r5 M& S For example: Forward right wing to body fairing has several loose screws. # @" w$ [+ \. u! T+ ` 右大翼机身整流罩前部有几颗螺钉松动。 * X) K! L3 u9 X4 V3 B Found 17 screws loose. Tightened loose screws with reference to AMM---.& s1 J' U, N( G" g4 a 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。 : B% Y& Q0 |- a$ p' ] + |$ R/ ]4 g& I, v(44) not secure: 未关(扣、夹、卡)紧 ; X( J1 G' S$ S: INot fastened, to make firm or tight.. G" e5 F$ b, L% Z 没有扣紧,(使)紧密。 + ~2 |! G8 `& X! t- g( V( Q2 |For example: Number 1 engine cowling; number 3 latch is not secure. 1 M% J* N& k- q" X. H* P 一号发动机整流罩的三号锁扣未扣紧。 % p1 _' b! N3 h7 `, V Number 1 engine cowling; number 3 latch has damaged hook. Replaced P; d% ~$ L* A, M+ mnumber 3 latch with new part in accordance with AMM---. Operation check 4 a, g# y, b! h* O% Q, kOK. $ H' @) J/ I1 w1 p! P- n9 z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,: b# @: [* N2 ?, P( e 操作检查正常。 q5 ~" |: n1 w2 U# r( Z, k% l 9 {, k0 E! A! v1 {( P4 Z+ T (45) inconsistent: 不均匀 % N& e; D3 v' Q' }+ {" nNot in agreement, erratic : J8 Q% p0 A8 ]* w% s' o0 q缺乏连续性。 ; g5 X# H. {* m) yFor example: Left wing-to-body fairing seal is inconsistent in relation to fuselage. ) C" |8 @% H5 o% E$ S4 X/ g; K 左大翼-机身整流罩封严胶不均匀。' v/ Z: s5 |6 d Re-sealed the left wing-to-body in accordance with standard practices and % X1 [; Y, D( C% ]: J0 A6 ?5 B2 C+ w: HAMM---. : W* O8 [3 n( i6 z3 D! z) ]7 q 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 T- N. t8 [8 j2 q- z2 s M 3 j4 c: p" Q0 Q+ K$ w% I* W) o (46) exposed cords: 见线 ( i* @* E( ^ a mVisual tire cords. ! M0 U" { `6 _4 C轮胎编织线裸露。 ' D" n+ l" V$ w' F* QFor example: Number 3 tire has exposed cords. # r" X7 u" |+ Z# H1 v( l3 ^$ E% X 三号轮胎见线。 1 W. |9 e o/ h0 U! i Replaced number 3 tire with exposed cords with serviceable wheel assembly in4 X: _ D4 g1 s# r2 E9 m N accordance with AMM---. Pressure check normal.& ]. A& m/ } s' F/ b1 M% t0 E 根据AMM—更换三号轮胎,检查压力正常。, Q. c4 Q* q: p- u & N" f$ ]& c3 V (47) bald: 磨平 4 W6 E5 e# g" u+ m+ [Lacking a natural or usual covering.: t+ u( K* t0 r# ~, m 轮胎表面排水槽由于磨损而消失。 ( z' K T. f, c s7 {: \. MFor example: Number 3 tire is bald and requires change prior to flight for no serviceable0 `) w) u9 ]: t7 d1 Z D: m! Y spare at scheduled flight sector out stations. 4 C+ C1 _7 o4 f4 D三号轮胎磨平,因下一航站没有备件,请在航前更换。 ) J/ f! a6 @. N' m! Q# Q) P8 iReplaced number 3 tire with serviceable wheel assembly in accordance with, V, m F6 g- H4 J$ d AMM---. Pressure check normal. % d3 m7 P" [; n; f" i( t根据AMM—更换三号轮胎,检查其压力正常。 6 D( A% ]( o$ v. b " V( U( R8 e" t" h3 [. z6 q G; S (48) insufficient-air-pressure: 气压不足 * u* T$ S/ S- ]/ NAir pressure does not meet manufacturers requirements. ' L1 Z( y; J; v2 E/ |# E/ ^空气压力没有符合生产厂家的要求。 e; b, n% _. n2 s For example: Number 1 tire has insufficient-air-pressure./ {3 h! ?; I# C( ^) n r1 M- i; D 一号主轮气压不足。/ o3 {5 Q9 s# I Measuring air pressure revealed 5 psi. Air pressure required within limit as' t( f* E5 k1 t2 ^ called out in AMM---. Serviced number 1 tire with Nitrogen as referenced in C) j7 j+ K, Q+ ]AMM---. OK for service.9 e6 B5 s6 k! I6 c( _ 测量一号主轮气压为5PSI,根据AMM—对一号主轮充氮气至要求。 % m' K2 d& j3 J9 a* O ' x) x) R0 ]/ G(49) expire: 过期 % l J* s7 U* PTo come to an end or terminate. ) g F$ g: J* y/ Q8 b+ G( x超过时限、期限。+ y% f3 p9 {& J# K( n+ \ For example: 2 each life vests located at L2 entry door flight crew station expired.. _ j7 b0 M' t) U! c 位于左2号登记门机组人员位置的两个救生衣过期。7 S8 L! ?' N9 b9 n& g Replaced 2 each life vests located at L2 entry door flight crew station with' ^ p9 T3 H! A3 T serviceable life vests due at 9-2005 with reference to FAR 121.6.$ |5 E) ~7 l8 j5 z6 S+ J 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7 I$ p( V. Q* N- U y 衣。" M9 \; y! j1 U$ }" B- n& P! e2 _ ; p' F$ g2 p1 h0 M2 `! ` (50) illegible: 模糊- ?! P& ` I( C' z( F2 `/ @ Not capable of being read or deciphered." i! r$ ]1 X' f& A+ f0 \ 难以辨认的,无法读出或解释的。" r2 ^0 B. s1 k1 {5 `1 w For example: Left over wing external emergency exit hatch “EMERGENCY EXIT” placard( L- }( _! ?% n. S" a% B5 Y is illegible. - ]3 x' f0 K* l' m左翼上紧急出口舱盖处的“EMERGENCY EXIT”(紧急出口)的标牌模糊。 8 s# U2 n' b0 H7 _ {Removed and replaced left over wing external emergency exit hatch + O: n A# T1 U: v/ W5 X% K4 p, z“EMERGENCY EXIT” placard with new in accordance with AMM---.5 J0 N6 I9 |+ Z: s( v3 g5 }& f 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。 - j1 a7 K8 ~- o( x ( ]; f9 S+ U4 w) b(51) damage: 破损/缺损 , ]5 m; m2 h5 s( Z INot useful or functional.2 P' X. ~6 y1 M9 Q6 M 不能用或者功能失效。; m/ B% t$ d8 {1 v. | For example: Left wheel well landing gear door “NO-STEP” placard damaged.1 R! ^. @/ {; S& A* k, K 左起落架门的“NO-STEP”标牌缺损。/ ?2 S- T- v2 x, ` Replaced damaged placard “NO-STEP” at left wheel well landing gear door. / n/ N0 q6 Q/ r( g& u$ X+ H6 o 更换左起落架门的“NO-STEP”标牌。 3 l2 [$ \. t$ h 9 d6 u+ {6 d6 s (52) lifting: 翘起 3 H2 H7 }! A4 h0 N9 g" o7 xTo become raised, not intact." x5 l9 W, P) i! \ } 没有紧固;活动7 ^9 ~- B7 X( _* O* O @ For example: R2 service door escape slide operation placard is lifting. 1 A- h; a% U( r( a* q* ~ 右2号服务门逃生滑梯操作标牌翘起。 7 z# ]; t* U; C1 n5 P7 m& K5 N Removed lifting R2 service door escape slide operation placard, cleaned and( N+ o" M; k( O4 ^/ L- o! D7 \" b re-adhered to in accordance with AMM---. . E G7 U7 v& w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& l# o' B0 u4 R8 T* M6 J( X 该标牌粘好。: W! [; H9 G. \6 l" G2 G* i! C; a 3 ^" d( J( q9 b7 b (53) not properly sealed: 变形/密封不佳 8 V/ V# ]$ u8 s/ e6 FRetaining package torn exposing contained contents.; k! e& m% v+ n/ [ 固定的包装撕裂而露出里面的东西。8 |0 U3 v9 G8 B+ f x For example: L1 entry door flight crew station portable breathing equipment not properly 1 [0 u" ^8 U) Q1 i2 Xsealed. 3 l- R* _& V- h$ [ m2 z! y4 h7 S$ ?左一号登记门机组手提防烟设备变形。- o& o7 G0 v2 X! g% v0 e8 N Replaced not properly sealed portable breathing equipment with serviceable 4 _2 R- j4 N, }, g2 xportable breathing equipment with reference to FAR 121.25 as required for! t2 {& C J2 X7 H, o; { dispatch . Tagged and routed unserviceable PBE to MSC to return to customer.- B6 b& G/ z; k$ j 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& Q1 ]2 [4 k8 r 理。6 H0 g. [! \9 i3 h9 Y5 a8 m 4 O A2 l: C6 b0 b; Z$ E(54) not properly packed: (滑梯)散包8 `+ }; x% o% r" H! [* F# K The condition of a released slide. ' W4 ^( {4 n4 e% D5 f' |: g8 y+ @滑梯包散开的状态。& p0 U+ u' \, E' S8 O For example: With reference to reliability work order and task card 25-456-01, replace R26 Y; p" A4 ~: A/ C; W, V service door escape slide, provided escape slide from workshop S/N 4321 is not " ^+ X% k3 M2 C1 E2 }0 }8 s% y. pproperly packed.( Y' h( ?$ Y* b9 D& F5 h: m5 ] 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 ^/ v2 T& e$ _# ^车间提供的(S/N 4321)件已经散包。 + C8 S0 D7 r( \/ u! b4 j; }2 gTagged and routed emergency escape slide S/N 4321 to MSC to be re-pack in8 m6 R+ c) F+ i5 `6 y( J# F; O workshop. Obtained serviceable emergency escape slide S/N 8765 and installed) }; ?' O+ }! c0 c+ [# x9 A4 z at the R2 service door position with reference to task card 25-456-01 and & d/ h2 D/ U: w, v" Y6 F, TAMM---. 9 T }! X5 A, @6 j7 k9 x 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( K! _9 v9 l$ I, Q, ~8 j 25-456-01及AMM—在右2号服务门安装序号为8765的紧急滑梯。 , z5 W+ g7 z$ F* r7 E% B9 e 7 Y# @6 |# p# ^9 }# J6 s$ D( F(55) dirty: 脏 , R9 Z+ @6 y$ rUnclean, soiled with dirt, grease etc., ~" |% _2 L9 h) c 不干净,有灰尘或油渍。 0 A% W/ Z W4 m% vFor example: Flight deck external window are dirty. 8 f Z" p0 ]4 N7 j6 f 驾驶舱外层玻璃脏。& u9 X* O) k4 {/ y3 Q Cleaned dirt from flight deck external window in accordance with AMM---.8 b1 H! X5 t; b' q) ]- H+ M 根据AMM—对驾驶舱外层玻璃进行清洁。 0 c3 L9 i$ _$ y 6 @( C6 b% P1 o9 M ? ]. E$ R(56) fracture: 断裂2 U6 g0 _7 y. ^. U/ w& s) u- ] A break, rupture or crack.& O1 n# \0 H1 g* J$ ^ 破碎,破裂或裂缝。, u. s% p$ A- i# ^ |( e: W For example: Reference Gameco routine task card 53-004-12, NDT X-Ray inspection at right. w; V' ?1 {2 L' j$ Z wing emergency exit hatch frame revealed 4 inch fracture at forward lower sill.. d& O: g; J2 L) }( B 参考Gameco例行工卡53-004-12,NDT进行的X光检查中,发现右翼紧 6 d' e4 `9 ~1 u( D+ N急出口舱门框前下角断裂(长约4英寸)。 5 f! B. z: D9 B% HRepaired fracture with permanent repair in accordance with SRM---, attached! |! W% H7 |2 [* G9 b' R& Y Gameco engineering order 53078-4, and attached Boeing TELEX 53-0987-1.- x- {, [/ x5 g* e) i Applied protective finish in accordance with reference to SRM---. 0 L. `" D( s6 O1 Q" ~; S根据SRM---,Gameco 工程指令53078-4及波音电传 53-0987-1,对断裂进 / s0 i7 M H% }& ~行修理。参考SRM—进行保护漆层的恢复。, K/ d9 @: C' n% n0 S: B% i ; E7 ]. J/ V4 D% ^; V( R3 e8 `' K: y (57) exceed-the-limit: 超标 ' l9 A r1 x8 y4 w$ L8 k$ v% p. s$ x& DDoes not meet manufacturers specifications. $ ~ L6 D! f' @ \$ i4 E超出生产厂家的技术标准或规格要求的范围。 ( v- c9 N& K* q6 KFor example: Reference routine task card 32-098-01 landing gear functional check, nose " T1 c6 n' [/ x6 ?- m/ planding gear doors faired to fuselage skin exceed-the-limit during functional 5 x$ R7 O# {) C' @" Lcheck. . ?4 k# p# N9 N/ n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 ' q& U/ @; D- r4 O1 j$ S; m架门与机身蒙皮间隙超标。$ A6 P' a/ k: r7 j; ~ Adjusted push-pull control rods at nose landing gear doors to obtain proper ) O* Z2 D) Y" N# ]1 U2 V- pfairing to fuselage skin in accordance with AMM---. Clearance and functional/ ]% l" W$ T0 ]# Z check good in accordance with routine task card 32-098-01. : U6 ? _& z: k8 E% i5 R# ^0 z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$ z1 j4 y2 o) P6 D& s9 L 进行功能测试,检查正常。 + p! f0 N2 m! T- |: Z. |6 ` / Y3 }8 s6 X7 w& O (58) backlash: 空行程/无效行程 . l" j. a8 a0 _" M6 T$ _: C: PTo measure play resulting from loose connections between gears or other mechanical- o6 P3 V. W' `. n; l elements. ( Q( d* h* t' F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。, M4 t+ J6 Q# C For example: Horizontal stabilizer jackscrew clutch failed backlash test with reference to ( q0 W* l8 v- y |( V9 Z# v1 h _routine task-card 27-0345-01. $ F4 `- X5 Y3 |* w, A/ i G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。 & ^ _, t. r3 V% l8 NRemoved horizontal stabilizer jackscrew clutch. Detailed inspection revealed& b$ B* k: c0 R( g2 r% `8 N. e worn clutch plates. Tagged and routed unserviceable clutch unit to MSC for- Q: |0 _" f: | return to customer. Installed serviceable horizontal stabilizer jackscrew clutch / f% X3 E7 r; ^9 Yin accordance with AMM---backlash and operational check good. 9 G, ?- j& J+ W 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4 J! p; O; K; c8 d5 J0 Z! D 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。5 k* Q s! | z! o- |9 B , B1 e/ J8 M" T2 l(59) block: 卡阻/阻塞 ( U# |; X/ P! NThe act of obstructing. ; E) P0 z. s6 w y! P# k# e# |" F通道堵塞:运动部件的动作不顺畅。& U% x: h' X! x: q0 v# H! k For example: Forward cargo compartment door forward actuator is blocked when opening % v4 t% d# ]6 k7 ~the door. W- ?" y; p0 ]前货舱门在打开时有卡阻。- }/ _; i- R# E4 ]# F& a( l% h Detailed inspection revealed there was a dent on the actuator rod. Replaced the $ t* t5 O x2 F* tinoperative actuator in accordance with AMM---. Operational and functional% V- y& D0 W! [+ o" X3 ] check good. 4 u5 U J5 d- s0 W- @% d 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, 4 G6 c3 X, A4 w* R( i7 B; h操作检查正常。 # F# E" N& B- z9 p5 i1 s- }: } ! q* G% |; n* [ (60) bulge: 鼓起 ' X2 f" e6 ~( @An outward curve or swelling. a7 t# N# ~9 D; o向外凸起。; d! ^/ F; j$ R For example: Forward cabin lavatory floor panel is bulging.. d" A6 M7 ^+ t* {4 e! @ 前货舱厕所过道地板鼓起。 + c$ j1 \8 D8 K Removed forward cabin lavatory floor panel, no defects noted. Re-adhered/ f4 N* S; _/ H! p5 c forward cabin lavatory floor panel and eliminated bulging in accordance with 6 n; H" w4 [, {7 i2 ]standard practices and AMM---. , g* |! |% K i& e$ ]7 X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 / z# a) q8 w3 ZAMM—重新粘接该地板。$ P, J& i4 ^" g; F5 ?) I $ X* o/ T' X! l, _(61) contaminate: 污染 ; T Z0 o/ ~0 X4 @& gImpure mixture. 4 L( z' n( V" F" x% B5 ^; Q有不纯的杂质或异物。; q' c7 ~. Q) C$ | For example: Fuel sample reveals positive contamination of microorganism growth. ( D3 i" Z( x7 t2 g; w 燃油样品检查发现有微生物污染。8 c: H9 y9 b5 }: X2 q+ f Treated fuel tank with biocides with reference to attached Engineering Order! N% X. c# ~: J3 ?% f+ s G2009619. / i, ^, r/ V5 t2 Z' L2 l根据工程指令G2009619,使用杀菌剂对油箱进行杀菌处理。" e, |7 M+ a* ^6 v3 m6 m% k + C6 x+ Y2 _ X3 A) h, u(62) disagree: 不一致+ r* \: {# F$ \0 u Fail to be in agreement. ( h4 u" \% G1 `; n+ j& |/ V( F对应关系不正确。 . } U& Z* [) l3 n. LFor example: Flap control lever disagrees with flap indication gauge through all detents.' w$ q+ q. ^ u' S* B& v# [3 q6 N1 J 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。 6 Q) V" w: t. m R# }5 P7 s Adjusted left and right wing flap indicators in accordance with AMM---. , r" c& L# ?4 W" R! e) LOperational check good through all detents.! L* Q. ]: J+ i- N9 l7 ]# m# j0 f 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 0 {: w/ M9 E8 w7 f" g表指示一致。 & q. p1 A1 Z; a1 e, q, D 9 h. q: s1 t% k9 a$ ?: f& P(63) discharge: (电池/气瓶)被释放$ z6 i# s, N8 w6 T To relieve retained contents to an empty state. 8 [; P- Y7 E3 b" ~6 Q放出;腾空 0 E u5 ~1 |; qFor example: R2 service door assist accumulator discharged.2 M6 r$ h; K; F Z' G 右二号服务门助推气瓶被释放。 * n( F+ ^! I! q5 `: i- x+ _; c R2 service door assist accumulator detailed inspection revealed damaged 8 x" ?0 B! ^" {pressure gauge. Replaced pressure gauge, serviced with dry air as called out in r; H6 {5 b" n/ L' ~; v AMM---leak check good. 7 C; T/ t" x% {/ ^: v3 B# Q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 + q& }* }; C# m8 R压力表,对助推气瓶进行勤务,渗漏检查正常。 . X/ M; z+ u& W7 {* x y $ A/ w4 \+ M0 y6 N9 Y. i- A; F (64) dislocated: 装错 3 ^+ ^ Y; V) u% hNot in proper relationship with joining part.3 z0 O( ~# o* g! Z! P 零部件没有安装在正确的位置。 p$ o. v/ p" r1 z; Y5 ]+ q: lFor example: Forward cargo door pressure seal is dislocated from retaining track along after# B3 E9 D) T' Z- U( f and bottom section of door.0 F9 R( q5 F3 ], {( D 前货舱门后底部固定轨道的压力封严条装错。 : C9 ], T j9 V8 t* N2 U- iDetailed inspection revealed pressure seal retainer damaged along after and, f6 l- ~: @9 ?' o0 [" g bottom section of forward cargo door. Replaced affected section of pressure8 O# C7 t; [6 \. v* U; R seal retainer and reinstalled original pressure seal in accordance with AMM---./ T5 p4 t0 a* g8 b4 {1 t3 r' S6 o v7 q Operational and pressure check good. : H0 T& V# a1 Y% @6 W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 : p; z3 X# j1 z, T. k! F! V该安装槽并重装封严条,操作并增压检查正常。 2 N- O! | y2 J0 g: b6 z # h' N; I0 j' }9 a (65) fail: 失效8 I7 O* M0 h; `- ^" L5 v# i6 x Note: must have detailed description of failure.3 z2 Z0 r* @' P% H w3 p% K4 z) t 注:如用此术语,必须给出故障失效的具体描述。# k8 j3 K. |4 f/ S# ` To perform ineffectively or inadequately. c( t8 y) j* `+ B不能执行或不能完全执行原有的功能。. t( q; S, q7 Y! ^6 b4 ~ For example: 13F seat actuator failed to adjust." Z% U: l9 B6 a0 f0 w+ {; G 第13排F座椅作动筒失效,不能调节。 $ @% k; {4 _/ u( y: z Replaced 13F seat actuator with new part, functional check good.; V$ F# n8 ^/ R9 L Q5 \& H6 i 根据AMM—更换第13排F座椅作动筒,功能测试正常。 + G A* h' ~& O" c6 i/ s : a0 q# s: C, O (66) fluctuate: 摆动 $ [# |! [! Z- l( {% N4 KTo continually change or vary in an irregular way. 9 P( c* o3 e* {5 U* ^% _无规律连续的起伏不定,变化。6 e) J( X# J( O1 [3 W: { For example: During engine run the number 1 engine oil pressure gauge fluctuates., |. I2 d% X5 a9 f) H 试车时,一号发动机滑油压力表指示摆动。/ N( `- z/ B4 A1 D& ~ Replaced the number 1 engine oil pressure gauge in accordance with AMM---. Carried out engine run, oil pressure gauge normal. * X M( I+ t b& }- B) a: u. F5 ]+ H 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。4 ?: A: g9 T. d7 L0 } 1 }9 C+ ^' m4 s( Q (67) flutter: 抖动 1 ~7 W. k7 E; a0 {6 n7 |A rapid waiving or flapping movement. 1 |; k: E; p9 `/ @; l快速的摇动或者上下振动。& }) F% Y% z8 s% F% H For example: Pilot report on flight logbook page 908701 fluttering sound from left side of * D) F& V3 c& r. _& Gairplane during descend beginning at 11000 feat. 5 e. O/ f! p. I* O+ a6 b" l1 Q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* g: O7 z# p% p U$ G 侧有抖动的声音。 2 H4 s5 D& b! u9 J$ Z0 kInvestigated fluttering sound from left side of aircraft as squawked on page: c2 @9 X7 y5 s# k/ ?. Z 908701 of flight logbook. Found number 3 flight spoiler actuator leaking.4 p5 U+ c# N. l. N: `( u9 j Replaced number 3 flight spoiler actuator in accordance with AMM--- ' B, i7 g. V. s! Goperational, leak, functional check good. Flight crew briefed prior to flight.! M% S1 C$ u M5 k) O 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。" I+ A! p' h3 l6 }: x7 P+ S& d$ f 9 ^8 p$ y' H! c. e+ g' a(68) insufficient: 不够/不足 # e4 P+ A9 g: {0 a8 gNot sufficient, inadequate. 0 v& j$ p) Q$ W" I! V达不到所要求的数量,数目。 / A+ o% F6 |: nFor example: Left main landing gear alternate extension control cable has insufficient ' J8 Q( k. Z5 J; t; I% B: N/ y: Zlubrication.5 N/ Z# {" E, k* q 左主起落架备用控制钢索润滑不足。0 E7 F& h+ u# l2 U: I7 _# ~6 ^* ~ Lubricated left main landing gear alternate extension control cable with 1 _# e$ y1 I( \ Z& tAero-shell 12 grease as called out in AMM---. 3 U+ Z0 U1 X' P& X/ P8 P/ Y2 t! k! ?根据AMM—用Aero-shell 12润滑左主起落架。6 S3 @- |. s# l2 `) Q 4 J h4 Y; x5 D0 d* N (69) inoperative: 不工作 " e! p1 ?8 G# Z9 e7 zNot working." n: x% i+ T% T5 [, T! b 不能正常的发挥功能,作用。 % R( L2 p, |1 E b9 K; G. @For example: Forward electronics bay door indication light in flight deck is inoperative. / L2 H9 _7 F: R# _8 _/ V/ I3 I4 D 驾驶舱前电子舱门指示灯不工作。0 f0 J7 e1 u5 }" |6 a Detailed inspection revealed 2 each bulb filaments fused in electronics bay' }, L3 L+ |1 ^7 u/ r E door indicator. Replaced 2 each bulbs in accordance with AMM--- operational % Q3 l1 Q/ _& H; w! i6 icheck good. * H; K7 z5 |# r* S* \, ]1 p* p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) |( r4 `/ j( ^ 这两个灯泡,操作检查正常。5 ]9 @9 z- c8 z 0 v4 `/ C' w7 T1 G$ w (70) (not) illuminate: (不)亮 8 N6 {4 S' Q/ C, ?+ p9 NNot brighten with light. $ q" L3 D! B! H不照明,不发光。$ W3 K" O9 Y, F# P, C For example: Passenger reading light at cabin rows 12AB, 14C, and 17AD, will not B2 {, |0 S# {$ Q, t: x& n illuminate.; _+ M- L! W0 P7 B 12AB, 14C, 和 17AD座位的旅客阅读灯不亮。0 r6 y! X! |3 b- n1 H/ V Replaced passenger reading light bulbs at cabin rows 12AB, 14C, and 17AD in - m& n* y6 x! W; h# M7 eaccordance with AMM--- operational check good.( Y' |+ K6 G4 \; d3 e$ L) ^8 R 根据AMM—更换12AB, 14C, 和 17AD座位的旅客阅读灯,操作检查正5 A5 R7 _9 n5 K v) P# L 常。 0 s# s8 L" b& v, p& Q / G$ y* {8 I4 ~% h4 |' T (71) interfere: 干扰8 g4 d( M7 g2 M/ B( P2 x& }3 m' Y To come between so as to be a hindrance or an obstacle./ ^, w! h: I! ]0 _6 F 妨碍无线电设备正常接受信号的电磁振荡。( J. r5 k& u* T% ~$ v For example: Functional check L VHF radio revealed interference static and abnormal noise. 4 x( r% v$ c5 G' m& y9 @( a7 | 功能检查左VHF设备发现其工作有干扰及静电噪音。/ I& _& t+ N" i8 L Replaced L VHF radio in accordance with AMM--- and tagged and routed the & `& g/ f9 V* E q, q; x V. Kremoved part to MSC.3 l" X; Y6 [, ]# l% f 根据AMM—更换左VHF设备,旧件挂牌送航材。+ m' ~4 e8 g! y+ r3 {, Z( Y% V " b3 o; C2 i* G' f9 T+ c1 T3 n5 Y# i(72) kink: 扭结/缠结 ) X, K2 E! H5 A% @6 F& ^ aA tight curl or sharp twist.3 |0 S4 B2 t# M7 ^ (钢索,条壮物)缠绕在一起。! ~( @5 D- D+ C U- n. h9 z/ V For example: Right wing inboard flap control cable at control mechanism located in after6 ~" m. J. ]2 Z. S8 [$ z' Y; G right wheel well is incorrectly routed and kinked.- t R- m5 }9 W* K/ y 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。) q) n/ V0 i/ }3 a' `, X Replaced with new flap control cable from Body Station 760 to flap control 5 e; s8 j6 L5 N0 n) c' `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. & x7 {& t* j5 R4 h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。 8 c# {% s! ?) [) [# J+ m 1 u( t- }$ a, H (73) misrouted: 走向错误- R' q% C" s7 F# q6 c3 ]4 t Not properly aligned through a course of travel. / Q- ?9 u7 c, O; q' X, f在行程中没有正确对折。 ; Q, F3 |8 V3 k: j' LFor example: Left main landing gear manual extension cable is misrouted through pulley attached bulkhead in the left wheel well. y# I9 S# d% E# S% [1 g9 o 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& Y/ f" e1 c6 m' F; C$ h/ e9 ]( v 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. 9 K2 H3 A0 C8 ]& V& V" H: l0 u. m 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" t. w9 o, s# V" Z 该滑轮重新安装,功能测试,检查正常。 * V( |: V5 \& J: p: R$ c4 R7 A/ t " L8 T( F6 @: G" e' `& v% i (74) not installed: 漏装3 E7 W8 Y6 w( S$ v! R, w/ t Missing. ! A! j9 I( V4 F F' V根据要求本应安装的零部件未安装。 ( R/ \% I/ ], Q4 K" @$ bFor example: Life vests not installed at L1 entry door flight crew station. & }4 @. K+ X* W7 D8 z L1登机门飞行机组位置救生衣未安装。 / y; _3 u; m) k Installed required life vests at L1 entry door flight crew station. " M' h+ \- z. ?4 E' M) I 在L1登机门飞行机组位置安装救生衣。 & e! L: Z3 o6 Z, ~4 } 4 s7 F$ I0 E0 A (75) rubbing: 相磨 + t0 n& d' a9 }. e5 z$ U7 d7 [Making contact with an unrelated surface2 _2 b0 N" n8 O3 x% h! C4 m 相对运动的两个物体表面因接触而导致磨损。; r( Y; X/ Z' d8 ^+ q) _* L& V1 ^ For example: Wire harness for cabin PSU’s running through floor beam at body station 360 1 |( P: ]6 |8 O u6 }. b7 Xand wbl 21.52 is rubbing against floor beam cutout. 4 k4 h7 g" x% U% ^. k$ c {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 " W% n$ v; o5 T板梁时与地板梁切口相磨。 " {: [) x; D' E# |) p. QDetailed 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---. . h$ }, E+ ]2 V# C1 y 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,# O7 Z8 }9 q* C7 m: e7 b 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( {: D2 P6 Y8 ?5 x Y- g0 q处地板梁切口相磨的情况。0 c/ ^3 T, ]7 U& t: e1 B' i- b" x0 ^ 5 [0 b5 t5 ` O$ k: ^# L) G, h) h(76) un-lubricated: 干涩/缺乏润滑3 C/ P9 f4 U8 U Without lubrication resulting in friction, heat and wear. ) O2 A9 Z% m0 K G+ L: h没有润滑而导致相磨,发热和磨损。 - e* P( R" _4 n) ?& G3 Y5 ?4 w9 P! rFor example: After aircraft wash, all 3 landing gears were found un-lubricated. 2 K3 r$ J# s+ q- Q7 | 洗飞机后,发现三个起落架都缺乏润滑。8 ~* x& P( l+ [7 j. n; U9 A/ N2 j1 Q Lubricated all 3 landing gears with aero shell 17 grease with reference to ) V& r/ |2 [$ R- o" x! H& R7 @ yAMM---.% L; [# Z! x4 L: Y7 l2 ~ 根据AMM—润滑三个起落架。7 k. I0 `1 @' [/ u l6 [2 I& g & A( K* M, J- d& C8 q (77) will-not-reset: 不能复位% ~& q3 S; _0 b/ C Will not return to its operating(original) position. ! j0 Q6 h4 F7 {: S3 \3 C& V不能回到原来的位置。 : d0 D: ^( ~7 L! k9 _For example: APU circuit breaker will-not-reset.* L- P3 G' w9 g( N$ c7 A APU跳开关不能复位。 7 S% \2 p$ T) ]( e! f9 {2 d Detailed inspection found APU circuit breaker faulty. Replaced APU circuit 8 A/ z- r+ X" v* Z9 vbreaker in accordance with AMM---.Operational check good.) ?9 @! t2 L- q5 I+ g7 s 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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3#
发表于 2009-10-17 16:38:16 |只看该作者
gggggggggggggggggggg

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4#
发表于 2009-10-18 14:16:04 |只看该作者
hao de tie zi

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5#
发表于 2009-10-20 21:10:50 |只看该作者
zhun me

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6#
发表于 2009-10-29 20:59:24 |只看该作者
dddddddddddddd

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7#
发表于 2009-12-3 18:09:40 |只看该作者

资料很好

% `0 F/ E; e4 r8 p+ G. v! ]

 

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8#
发表于 2009-12-8 10:45:56 |只看该作者

好东西,看看

好东西,看看

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9#
发表于 2009-12-8 15:53:57 |只看该作者
需要术语。。谢谢

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10#
发表于 2009-12-12 23:10:06 |只看该作者
专业人士就是专业人士 为人民大众服务了 雷锋!!!

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