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维修术语0 g* C$ t) m$ o; ^; ]
@- O6 h G. r; I1 |
. B3 k( K+ G- |(灯)不亮 not come on 不可用 not serviceable* I! z, a0 ~. _8 b8 W
“工”型 type I 不锈钢 stainless steel' ^+ n: r1 c* b
APU 舱门 APU bay door 部件 part1 v4 \+ D% [* L6 \9 G) L+ E6 d
T 型件 Tee extrusion 材料 material
q8 i' ]1 I" a* \) l6 o& t9 b) n阿罗钉 alodine 参考 reference
% A2 y( _5 d5 e8 k安全带 safety belt 餐板 feed panel7 o) m( O0 ]; F' o
安装 install 餐车 diner! q5 J( R6 [/ l& J8 ^- G* p
安装座 attach fitting 操纵 control
0 C1 K7 s! q; ?0 h8 F按钮 button 操作检查 operational
) {9 f+ @, J6 ]5 a* |/ y' E按需要 as required 槽 spout# ?+ Z+ Y2 P; ^( }0 i) M
凹槽 notch 侧板 sidewall
8 ]0 e" k0 o) ?4 h凹坑 dent 测量 measure9 q" C1 x1 ^) a
把手,扶手 handle 测试 test' q/ [4 j' O f; u
包皮 cowl 插钉 pin
3 `1 C B) ?3 i% U4 ~5 _保护层 coating 插头 plug h( L8 c4 H' P' |' j
保险 fuse 插座 receptacle4 C* Z6 e0 b. ^$ ~! T J
报废 discard 拆下 remove+ G3 f w: M J/ E; x
报告工程师 report to engineer 长桁 stringer( c) V- x. c' ]
杯子 cup 超标 out of limit
" S" i" `2 ~ R* x比率转换器 ratio changer 超标 exceed the limit* O- z* p7 b$ G$ l
壁橱 closet 超过 exceed
; Y% p2 [7 F+ l边缘 edge 超控手柄 override handle n4 E" o2 z+ s/ J& u8 @) X
便于检查 easily to inspect 彻底修理 drastically repair
$ V& g! E* s- x变形 deformation (n) 陈旧的 worn
( ?# j7 c& z3 `' N变形 deform (v) 衬板 liner
/ W1 H- O* l3 f6 a8 e' E3 I# @7 M变压器 transformer 衬套 bush. p* ]6 `+ ?; _1 o- |/ F" q
标牌 placard 成型 shaping
8 @4 h6 m8 N" \' x8 j标识 sign 乘务员 attendant0 T3 J, U2 Z4 f: T
标志 instruction 尺寸 size
% C8 M$ ^- ]" ]- B! h玻璃 pane 充足的 sufficient
: Q; g8 T% k* A5 J5 V玻璃纤维 fiberglass 冲水按钮 flush button: @) H& I4 K8 s1 w( T
补片 patch 冲洗 flush( x4 L! K% x7 g& t$ K. y6 }8 d! s
补片 filler 冲压 ram" W3 P1 h4 a @5 Z
冲压空气 ram air 低压压气机 LP-compressor
9 t2 b' \/ |+ N1 E抽油 defuel 底部 bottom8 I! L& j$ t% }0 Q
出口 exit 底盘 base
( C# J1 J! ]% I' ~# K4 L除腐区 reworked area 底漆 primer
% R: R- _, q" N8 G) \9 _+ _厨房 galley 底座(结构件) mounting
5 h% M& B# S F0 [6 X& r- `# m厨房烤箱 galley oven 底座(螺母) plate, d$ t8 f( z. E' ] Q8 {' U# y* K
储物柜 closet 底座(天线) base5 r2 u* W; t4 j5 D7 o7 _
处理 treatment 地板梁 floor beam' D; Q$ K0 h. q# o8 ~$ b& t: m2 L
处理 dispose 地面 ground
8 g: g7 b6 p! C/ p传感器 sensor 地毯 carpet
% y/ s! L3 q Q7 U传输 transmission 第二层 two layer
- P# s, `7 P+ F7 y垂直的 vertical 点火电嘴 ignitor8 S( [/ f5 t- V4 W, ~( A: G# K
存放处 location 电路 circuit1 d6 z3 r0 q. ?$ Y# g9 a
错位 migration 电门,开关 switch/ I ]3 ^" y6 F! p
搭地线 jumper 电气 electrical
! C l9 H4 R: O3 I9 Q& v搭接处 interface 电气接地 ELEC bonding
( S* A% p, E( D" w搭接片 splice strap 电源通电 power
# v! z+ d6 |' N$ _搭接片 splice 电子 avionics
# r/ W9 L% S5 U8 m. c! \- J打磨 blend out 电子架 E rack
) ^3 g& `1 B4 G# K" b打磨片 blent disk 电子架 shelf' l& Y- {. _8 I/ m
打止裂孔 drill stop hole 电阻 elec resistance
% L) w" f. D( E: P: Q6 k R大翼 wing 电阻 resistance
8 t( T2 ?/ h' y2 ]1 z8 Y; B4 {& o& \大于 more than 垫片 washer
7 v4 b/ O5 \$ f" K+ r单向活门 check-valve 吊仓 nacelle
2 v9 D/ B, N+ A* H" {弹簧片 spring seal 吊点 mount cone, N2 G: Z+ `5 U B( p& j
挡块 retainer 调节 adjust
: M4 e3 [+ v" Q; |( M. H挡雨板 fender 调整片 tap
& e5 c+ y+ d( _/ V: Y$ X导线 wire 顶板 ceiling3 a( |" L) e3 S3 u+ s; ? ^
灯 light 顶部 top
) h% `1 I& k ]/ l# l6 p- n灯泡 bulb 顶部 overhead
) {- l- h/ E) h灯泡 lamp 定中弹簧 decentering spring
# I" D5 D2 a: w6 A灯箱 light case 丢失 miss
, \2 _+ l' I. W& W* a灯罩 light lens 堵盖 plug
* I: i' x ]' V( }; s2 n登机门 ENTRY DOOR 堵塞 clog' T2 u0 V: h1 p+ ~. U/ ?" B- `
端头 ending 腐蚀 corrosion
4 r T7 U5 T/ J段 section 腐蚀 corrode# `* h1 m) b% |( ]- O% a# _
断 break 附件(大) accessary% r2 s9 x' T0 l V! F" j/ ~2 B
断开 disconnect 附件(小) attach
Z h2 L/ I0 h" d断裂 fracture 附近 adjacent to
) K! Y% G! l/ N$ T断裂的 broken 复合 complex( q! c; m8 ?' q
断丝,磨损 fray 副驾驶员做椅 first offcer's seat! T7 J2 \7 k J( ~% n% h- J
锻件 forged part 副翼 aileron
# D! H2 V, ], b! S多处 numerous 改装 modification$ w( I* ]- X4 c$ ^$ B
发动机 engine 盖 cap
7 I0 `9 I4 h5 V翻新 overhaul 杆 rod0 v. ~5 w8 X* @& D7 B
反光镜 mirror 钢丝 steel3 u4 ~, X, c' C8 T/ Y
方向舵 rudder 钢索 cable/ `! G; s1 o3 W. K8 x. k. H3 j
防冰管 anti-ice duck 割除 cut out! [& H# y. X( G6 i! u8 t$ J
防腐 corrosion-inhibition 割断,割下 cut off
& G( Y1 Q' g3 y9 r9 B防静电 static-free 隔板 clapboard,partition0 ?2 p3 `; Y' @) ]( R& p6 J, ^
防磨条 wear strip 隔框 bulkhead* k! I# H' M |. S) \
防滞 antiskid 隔热棉 insulation-blanket
% D9 o( q$ J. l, k! c防撞灯 anti-collision light 隔栅 grille
3 A$ e2 F$ U4 a& S7 D& `放 extend 各有 each has
" Y! q# W/ |# P放电刷 discharger 根据方案 in according to disposition, k' ~1 Y- n" |$ s1 j0 v
分层 delamination 根据监控指令单 condition monitor order…
& j5 \* m1 Y: t. f2 f4 H) ~风层,脱胶 delaminate 更换 replace
7 S) D) ~* w7 K5 t! G b风挡 windshield 工程师 engineer* c f, y e' l! @
风挡玻璃 windscreen 功能测试 functional test- H8 a, n. B+ K0 \% j8 i s
风扇整流罩 FAN COWL 功能检查 functional 1 B1 H9 l8 N7 V0 N
风蚀 erode 供应系统 feed system+ x% e7 o8 Z/ M9 G) ] b
封严 sealing 供油管 OIL TUBE, d+ Y, O8 a" H F" i
封严条 seal 鼓轮 drum6 O4 j' w1 a6 W6 _* W1 Y- p
蜂窝芯 stagger core 鼓起 bulge' p6 T+ D% j3 l) Y S
扶手 armrest 固定 secure( D7 W6 S" F7 d+ }8 N A* W. V, y
扶手盖板 armrest cover 固化 harden
6 Z9 @# S. d$ _1 d辅助滑轨 assistant track 固化剂 hardener4 t+ ]& }; d( Z8 C1 _4 P5 ^
故障 fault 划痕,划伤 scratch$ P/ w6 M1 a* y2 q1 ?
刮伤 scratch 划窝 countersink
7 s1 {: l* g* Q; m1 W0 G挂 attach 环氧树脂 epoxy resin W& L- F6 ?: f
挂钩 hook 恢复 restore' a. N) b8 I/ _" k
挂上 hang up 活动窗 slide window
: Q% f/ I& _ E! |9 I: `关上 close 活门 valve" O6 a1 j$ o& I1 `% L
观察镜 view glass 货舱 cargo compt
, [6 E: c. s/ ^* q; v6 C. Q, p观察镜 viewer 机构 mechanism
; V2 _8 m, U$ j- M: P" w9 F' R观察员 observer 机身 fuselage# L8 R' ]1 a# ]
观察员 observer 迹象 mark
% O" m" K9 X G0 w4 ~$ `( N9 ]光滑地 smoothly 加强 doubling
7 H$ \+ s0 U. I: y滚轮 roller 加强件 stiffener: z8 @% W* I/ q5 v% x
过道 aisle 加强块 doubler) q' o1 ?! ? K4 Q3 S3 p& c
过期 expire 加强肋 intercostal
' V. `; L; Y3 l- o2 q$ \3 p# C* l+ k过热传感元件 overheat sensing element 加强修理 reinforcement6 E3 u8 h5 N. ?
海绵 sponge 加温导线 hot wire
% y; N0 \8 o3 e( s焊接 weld 加油面板 refuel panel
: Z0 m7 I% W5 z4 X4 ~# {8 Q焊条 welding rod 加油站面板 fueling station panel4 C W! P) u M
恒速传动装置 CSD case 夹子 clip
, z5 D2 A3 T3 q1 t+ C9 _4 u6 i横梁 latitudinal beam 驾驶舱 cockpit
% e, D$ w* Y/ J* V! F9 T; N, X横向 lateral 间隙 gap
8 @: R' X6 q) p+ f. y& b8 _后端 rear 减速板 speedbreak% T& {0 i# R6 K" V0 w
后缘 T/E 减压器 reducer* e* a$ j7 F, r
厚度 thickness 减震器 shock absorber# U; C% `- N7 l9 t- _9 |
呼叫灯 call light 减震支柱 shock strut
8 u6 T& B+ R! F0 v护板 protect strap 检查 inspect
H& C4 K5 l- x W4 ?护目镜 goggles 检修门 access door" I) Y! L# c. ~+ Z9 A4 e$ U2 _7 i, n+ s
护罩 shroud 胶 sealant
6 I: E; S, @+ N花键 spline 胶带 tape
; }- ^: \( N) t滑轨 track 胶垫 mat6 C! O7 I: y$ U) E. n
滑轮 pulley 胶垫圈 rubber washer+ k% {% R7 U& `! S; [; y
滑丝 cross thread 胶套 rubber 7 _) Z6 O8 Z* m& _8 y
滑梯罩 slide cover 胶纸 tape+ I/ U R9 ?7 Z! I
滑油量 oil lever 角材 angler0 g. I& ?( g C2 b
角型件 angle shape 喇叭 megaphone
, v' u: l+ s# ~/ m" k- }! V9 j脚登板 pedal 拦网 block
+ x* M& i, ^1 ~/ J铰链 hinge 牢固性 security
# p( K3 q5 H5 u8 I* V接地点 ground point 老化 aged0 b" `9 M N% n% S, A
接耳 lug 老化,退化 deteriorate) q; [5 o @( J+ l! ?/ {3 W
接通,提供 supply 雷达罩 radome
& ] Z4 i7 |* S, n7 A接头 fitting 肋 rib i2 f! Q# C: M! t) g; I
接线管 splice 离合器 clutch+ [4 N! u t, w% p7 H: Y8 m
接线片 terminal lug 立柱 pole* w/ q' |& A I. A4 F# \. q7 l8 ~
结构的 structural 例行 routine6 T4 U( \- B, C- o+ }* M# \$ j, @
金属屑 metal particle 连杆 link8 u* d( n: ?9 [4 L+ T. l( {. F8 p# u
襟翼 flap 连接 attatch
0 h t0 v1 W K9 F紧固件 fastener 连接板 attach plate
7 X8 z% A4 r. ^) X2 q紧急出口 exit 连接口 coupling ! e8 T* x/ J2 h. }: N
进气道 inlet duct 连接销 lockwire
& |9 E5 u: I. c/ ?/ E* m进气口 inlet port 联锁 interlock
; |+ u3 r/ E8 U径向驱动轴 radial drive shaft 裂 crack
4 ~! e9 K+ x: V" r静电,静压 static 另一个 another
/ z: D U* R2 Z( a$ j% |9 Y8 c救生衣 lifevest 龙骨梁 keel beam' D5 y: ?& A1 u, F9 v ]! C
咖啡壶 coffee maker 滤网 filter
! ]$ l& k, j- f卡箍 clamp 铝箔 foil9 v3 k2 d$ k1 b1 B' f! s
卡环 collar 轮舱 wheel well# }: A0 k6 ^4 O
开口销 cotter pin 轮子 wheel u- @5 }$ ^& m j4 X! L
靠背 back panel 逻辑 logic
; ~2 V9 |" Z. p Y* T0 G2 D壳体 case 螺钉 screw
, s3 T# V+ s; [' y3 X! i可用 available 螺钉孔 screw hole" j8 Z% c- J* V( n
客舱 cabin 螺杆 bolt
7 A. n8 x$ _- f2 O7 z3 _" `/ d空气循环隔栅 air return grille 螺帽 nut0 t q/ s; S9 p% a7 Y
口 port 螺套 insert5 Z; r8 }& T# ?8 x% k: f X8 j
块 piece 螺纹压伤 cross threading
b" j$ {$ _+ n9 d框架 frame 马桶 toilet
+ x( r$ s# r6 c, t垃圾箱 dustbin 慢车 IDLE
3 L; }! D0 R# T7 ~拉紧 pull 毛刺 bur7 q9 s6 |* B8 k' Y8 z
毛胚件 rough 破损 damage' B; D( r6 k4 ~3 \% h
铆钉 rivet 漆层 coating% C6 T( U! k$ }8 H
门槛 sill 其中之一 one of$ a8 B: C& f: e9 O2 N5 k; h& o
门框 door frame 启动活门 start valve
2 G4 G6 ~/ k% N+ @4 W7 ]蒙皮 skin 启动机 starter+ G! k* @) B7 C4 k
密度 density 起落架 landing gear
+ c& Y7 F8 C2 F5 b' {1 W( s密度计 densitometer 气瓶 cylinder
1 C! W1 Z! R) t& n面板 panel 千层片 shim' D. _. s+ D! R9 j/ C5 o7 k8 T. u
面漆 enamel 前厕所 fwd lav6 }. M( c' M9 X9 f. j* C
模糊 blur 前缘 L/E
; ?+ c( F3 i M. B# k. ~( h模糊不清 obscure 腔体 cavity) ]9 w1 V {" {& E; ?( B
磨损 wear 墙纸 wallpaper# U" P: L5 N& }2 Y# E) r
目视 visual 切口 cutout. e, J2 K, g1 o8 ~5 p/ ^: Z# C
内侧 interior board 勤务面板 service panel
5 r* R6 z- ]2 t内层 inner 轻度 light
S! T5 m: I, R/ K尼龙搭扣 nylon fastener 轻微 slight: d8 l5 T! h' |7 ?& P1 |
尼龙扣 nylon hook 清洁 clean& v; s) I( b) m: H/ P
拧紧 tighten 清洁剂 cleaner
" L" c1 w5 Y- a9 ^ S扭力管 torsional tube 区域 zone
( @9 _5 y; t5 B7 q/ W扭曲 kink 曲柄 crank' Y+ x6 c; d4 V. R* i" m
排 row 去除深度 remove depth& Z1 q. y3 c' M+ Y
排放 drain 去毛刺 deburr
# ~0 S. w4 X+ f排水槽 gutter 缺口 nick5 B$ x8 J9 c4 s/ T' d# d
排水管 drain tube 群边 skirt edge
' x Y @, @, h$ c/ L+ G配平 trim 燃油 fuel
* k ^' z9 t0 u- J8 A喷漆 paint 燃油泵 fuel pump
5 e2 c0 [4 V H- Z' ^6 k, z- o喷砂 sand blast 扰流板 spoiler
2 t ~: U" }' p; a皮带,片 strap 热水器 water boiler8 n0 v1 A4 O1 F" U5 t" Y$ w4 r
皮托管 pitot 人工行程限制 manual travel limit
, t Q9 a5 X% O' q' F偏航阻尼器 yaw damper 日光灯 daylight lamp( V; n8 |) q; f1 n1 w$ o: e
平衡机构 equalizer 软管,软护套 hose
0 |0 G4 G5 L+ p* M1 y$ O, g; i平滑的,使平滑 smooth 润滑剂 lubricant
$ \- e* M) A( y7 D平行 balance 三段 three section0 H7 k8 y" U. s2 q( S% k
散装 bulk 逃离滑梯 escape slide
# N) C0 S( x4 U$ X( Y6 y刹车 brake 天花板 ceiling
. l: ^( b/ S. Z% c+ b5 T2 |上表面 upper surface 天线 antenna
3 D9 N4 D! ^9 Q2 I* B' ^; z上述 above 填补 fill
; _. i/ A; W3 i0 @% j- F* G n深度 depth 跳开关 breaker9 T. k+ F3 a0 S7 E3 J I' f2 ]1 N
渗漏 leakage 凸轮 cam
$ y- X" S2 s+ z0 L9 {升降舵 elevator 图纸 DWG3 D5 F% B0 P* B+ t# L
绳 rope 涂,粘贴 apply7 F9 Y5 E" B( N5 ^+ g/ S
失效 inoperative 退漆 strip paint1 r7 E; {' [0 I2 q) J+ }6 D
湿安装 wet installed 退色 badly faded
/ T) M( \6 N8 M, |1 d) K5 I试车 run up 托板 pallet
4 _, W2 O& Q$ a; {. p& x释压 pressure-release 托板螺帽 plate nut
5 F4 K8 E2 p' V0 i) F% [! K收 retract 脱开 disengage0 l6 U( ^% m+ F& ?: p5 k+ ?
收发机 tranceiver 外 outer, r& ?5 e Z0 O2 e- M% Z( X
手柄 towing lever 外侧 outer board
$ b$ @# Q( q6 r! Z手册 manual 完成 complete3 a+ H' h8 ?4 Z$ h' M" G
手电 torch 完成 finish! v7 \1 ~! [& e+ r9 a6 f
手工 handwork 万向接头 gimbal- d6 b* r8 ~ U; s+ O0 y. w
手提的 portable 维护 maintain
* N: o0 {- N! k4 G手提灭火瓶 extinguish bottle 尾部 tail
" W# `5 p2 y3 E g树脂 resin 尾舱 tail compartment
5 M7 m5 ~, s/ E2 ]( {双倍 double 尾喷管 exhaust nozzle
, T' K# h; E3 f/ u水平安定面 horizontal stabilizer 尾锥 TAIL CONE
; W9 p, y5 ?1 v5 P9 b& e, @% M0 C撕裂 tear 位置 locate2 v: F" N4 i% |& ^9 Q( N
伺服 servo 温度 temp
- Y' s) V R" _0 p' q松动,松脱 loose 涡杆 jackscrew
! D, k7 }* d* f* H4 i3 y( ?6 }/ m送修 send to repair 涡杆 worm bolt Z- I6 _* b6 m! A6 y
塑料 plastic 涡轮 turbine# G4 o, J: w: d0 c* O
随动盖板 hinge access door 污染物 contamination6 f1 L- k% ^$ o2 [4 l6 Y
锁 lock 污物 dirt
6 J9 W4 Y! J0 U3 d3 M" X锁定 lockout 无线电高度表 radio altimeter. I l' ` V w
锁扣 latch 稀释剂 thinner
- c* g3 `5 k5 {4 c3 T锁销 lockpin 铣 mill" J* G+ s$ [* ?! F& z3 m5 E8 I
系统 system 溢出 spill- B2 g! H& ^& y s; ^- D9 b* S
下部 lower 翼尖 tip% q2 g9 J& u5 X4 `* x0 @
下角 LWR corner 翼间 wing tip( A4 _7 G# l& ?* s6 U
下位锁 downlock 翼梁 spar
$ o/ @) J* q2 Y) c9 b9 W' I( N下陷 concave 引进 introduce
2 ~1 b% r7 |$ j8 q下缘条 chord 引孔 make guiding hole, l8 m% _ i: |: C5 h2 l
纤维板 fibre board 引孔 drill hole
8 B* n1 S; F8 L5 Z- O1 o相关的 relative 引气 bleed- ~8 J: h: C) p, Q9 n
相磨 chafe 引气管 bleed hose
- a5 ]6 C: }7 T8 E" e消音板 accoustic panel 应急 emergency
7 x: p( K+ [7 _: ^$ T& z销子 pin 永久性修理 permanence repair% p& I. z, Y4 Q& M2 T
楔形块 wedge 用…填补 fill it up with…
3 L; c6 g0 \" }8 H. b信号灯 annunciator 油封 preservation* M1 G% Z( U% e& R
行李架 luggage-rack 油箱 fuel tank8 p: a5 e' }$ V# @9 z
行李箱 stowage 游动梁 walk beam
' Z. h% S1 n i: _修边 reform 雨刮 wiper# |# C7 o* [" u5 s
修理 repair 语音记录器 voice recorder( U* e i( i/ z9 J( p. e
锈蚀 rust 预冷器 precooler; u. I f4 _/ | F+ ^$ P! X
循环 cycle 预位 ARM
+ ?" B# ^* R: ?: B Z8 Z压紧 gland 原厚度 original thickness
2 @' B; M1 M' d$ J. _2 ?% g+ A压力通风系统 plenum system 原来 originally5 H7 Q! v4 l* z6 s' X3 A& i6 `
压条 cover 阅读灯 reading light
; f: }7 i1 A: L. l严重的 serious 允许损伤 allowable damage
" I) V2 D0 \1 n6 G阳极化 anodize 杂志袋 literature container( v; f1 ?+ Q3 f0 B& \; X2 Y
氧气 oxygen 载荷调整 preload adjust& w) n- Q, @+ I% Y
氧气面罩 oxygen mask 再循环 recirculation6 ~ P9 `4 x( i9 W1 [& a3 r
液压 HYD 在位 be in place
# i' }3 k' W' U9 t液压泵 HYD PUMP 脏 dirty |" G( e* ]$ i4 B0 T8 W
液压管 HYD duct 增压 pressurization: U6 r5 g' n7 K5 @
液压系统 hydraulic system 增压泵 boost pump
3 S! a7 c7 H0 h1 q: L* x- c4 ~液压油管组件 TUBE ASSY 粘贴 bond) E4 Z& r$ _1 h( S) k
液压油箱 hydraulic reservior 照明 illuminate
) a$ z2 \5 X8 S! y4 y8 j! _1 c移到 move to 遮阳板 shade2 B1 [* x- S. s
真空泵 vacuum pump 自动刹车 autobrake
* Y, T+ P6 P1 C+ c! N拯救 salvation 自动油门 auto thrust# C1 `' Q% r6 N2 h2 a, q
整流罩 fairing 自锁螺帽 jam nut+ j( t2 ~$ Q# M" u
整流锥 spinner 自由移动 move freely% y* D4 a0 V; T+ p
整形 rework 总管 manifold" ~( [6 Q# }" @* X; b; ]6 b
正常 normal 纵梁 longeron2 z# K& s& E1 u( D& Q3 M. U! m
正常位置 normal position 纵向 longitudial' E6 i' x' }, }& s0 D) s5 f. B
正驾驶员座椅 captain's seat 阻力支柱 drag strut
- _' _/ B# i N. r/ C之间 between 组件 assembly,pack5 \3 q; J6 m% T, ~
支撑架 bracket 组件(电气) unit
& P1 ?' E# c6 u0 U3 u. G/ G6 z9 }支撑座 support mount 组件(机械) assy# q' d" f5 O! v8 E, l# O3 o
支架 bracket 最薄 min thickness
$ A, w" u' `9 V' F* j支拄 support 作动筒 actuator9 V4 g7 ?" }( X* L8 R
止动固定块 stop block 坐垫 cushion
6 Y y# V; Z$ I8 x/ h! G/ O$ [0 Y# ~) y5 {止动块 atopper 座椅 seat
( Y; B4 C5 G' k5 P1 ?4 n# B" I l指点信标 marker beacon antenna 注意 caution# Q9 f" M1 y/ ^: w( l' X P
指示 indication 转接器 adapter, m% t }+ w. @, u5 s
制作 fabricate 转弯灯 runway turnoff light
* P" k% e6 f( E/ S中厕所 mid lav 转向 turn
4 h+ V1 A; E. i, z9 v! e. k中间,中央 center 装饰条 trim strip$ i1 S) Q0 B. ^: Y: L
周围 around 准备 prepare `) c; P: s) o) ], X3 d
轴 shaft 着陆灯 landing light) g% p& u, m6 D+ n
轴承 bearing 自动关闭 auto close! n3 ^4 k: q% d5 b# `! h+ Q0 Y
主轮 main wheel 助推机构扳机 power assist trigger" @0 h* \ O. Z. `( J; d
' P- M5 z) ?, m% }7 h
8 k: ^6 o( \1 i" v( n
8 S8 j$ ~% A7 K* J& m6 M6 g. k3 y9 y
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~; I7 o, j" J5 D6 o) T0 F, }0 B, N5 _+ ?
: w+ x. Y# H5 @3 e" e4 u/ M# m
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2 G8 T( N( s# c8 ^6 Q; p$ W
+ o( Z; s* w3 i, w* o' w" ~% A0 f2 b
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9 o! V" a" g8 }* S: i5 f$ m. t' ^* A3 l' m
$ Z. B" L& x$ e9 Y
0 ~& Z+ t( g# c, p6 Z! p8 M5 [+ F7 [% t3 I" N' t# }7 r1 }' Y
4 Z( W9 L$ J4 M" L" X6 B
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1 S/ h) \7 `8 ^3 R# ]
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2 q" c! q: M" z. c+ |; O9 W$ [3 h: s6 I8 H# c# E
4 L. X. ]) P6 _6 e2 k
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, i8 r* h9 X# y/ f# i" c7 \$ U/ ?8 k5 F( z; ^! c- a9 {+ V% @
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+ C5 {+ ^; @" F5 K% `& uCategories of Defect
( j, P$ y3 X1 b2 c/ } Categories of defect depends on experience of maintenance practice .In this manual, the default" g. B/ ? }% R$ d4 f
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.
1 o! v( C) x4 _3 V1 K缺陷分类
" p3 A" d1 _! q4 P3 W+ S1 S8 @ 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。
3 k( @0 K, z" J- R4 W; ?. p2 b / z9 a. C! l+ U: Y/ }
1. Common Structure Defects Terms
4 S& ], ]% P* F' Y6 \) Y: Z4 p结构缺陷术语* }5 W) d+ |- V' I7 D
9 P1 K& X `0 ]* X/ K, q凹坑(1) dent
4 i; I: \7 g0 w. s$ [凹槽(2) notch
) l2 w' S9 T$ i6 e变形(3) deform
( P) j1 k( Q. a划痕(4) nick5 g( H7 d. i) ` R
点腐蚀(5) pitting
2 Q9 \, e& z% m0 a' f& ^1 @ `断裂(6) broken1 W) E0 q* b' \+ n
腐蚀(7) corrode5 e. ~9 {- w8 I! \. M
划伤(8) scratch
$ s' w* m: F/ \裂纹(9) crack- r8 O( O, j# B9 P' [
毛刺(10) butt8 P( l/ g+ a: `% {
磨损(11) chafe
; I8 U1 V7 I" X" O凸起(12) protrude7 i2 s! d9 @. m1 o/ G0 }- j
凹陷(13) sag
. S0 d4 C1 a5 h$ l3 V! K3 Z: {- c- s0 ]粗糙(14) rough
& I9 Z- y0 L6 i* U2 f" ~& [漆层剥落(15) finish missing$ W% ?/ h: u8 C7 i9 ]) x) x4 x
褪色(16) fade
" c: S Z- `; o1 {, s; X积水(17) entrapped water
% g3 S3 W" W z+ I( P* i
9 O* Q: {' ?' Y/ _7 c4 V. {" d2. Common material defect terms
6 B2 {6 L1 N1 R9 `! b e材料缺陷术语% r7 @; [* h. j% i- Z
Material is divided in two categories: metallic and non-metallic.
B$ B; M6 @+ Y- N 材料分为两类:金属材料及非金属材料, I, k/ |# \) s6 F
P1 W' U: ^3 u7 g 1)Common metallic defect: % D8 ~) o% K( `4 W8 P) r
一般性金属材料缺陷:" b7 E4 c5 F y" _$ w0 ]: ]5 e
- I- I* G! t0 A, f
氧化(18) oxidize
1 l ]* Q2 m3 k; s3 Y* u% E 划伤(8) scratch
\- \+ u9 N- p8 ~ 扭曲(19) distort% h! {5 f+ P# G0 r, E2 L. y5 I( T# A
跷起(20) not in contour {7 Q0 Q6 U! O* Q; _
穿孔(21) puncture. V6 M3 e5 {% G$ N0 u6 b. S
碎屑(22) chip1 I1 Y8 N: I) s5 [. E9 ]; j9 I
腐蚀(7) corrode
7 z/ [7 W+ a' T+ P. S1 t 磨损(11) chafe4 e4 p5 u/ @5 v9 [3 o4 H
变形(3) deform
y- L9 v0 K, v8 f6 c7 |- N, C风蚀/风化(23) erode
- l; {3 N( U. O/ l+ @裂纹(9) crack- k, v( n( l. L1 n8 B/ o
2) Common non-metallic defect:4 Y' N; {$ g. N- R+ Y
一般性非金属材料缺陷:
: Z* K* b2 Y: b) g 2 ?/ `8 H9 t/ k, |
发霉(24) mildew ! B( ?) s* O6 c2 \1 c! T+ q
分层(25) delaminate l) [% q4 K8 {, S
风蚀/风化(23) erode
) Q a) f- C! R# _裂纹(9) crack; J8 j9 e" {4 X. X% A, k
老化(26) deteriorate
& W* Q) D2 a$ _2 Q/ Z起皱(27) wrinkle8 T, h, j$ H. O* a: f
受潮(28) saturated
2 }% R* ?+ N* j- L4 A9 s+ L+ }撕裂(29) tear
4 r& f9 f7 s# g# L4 t' a0 A% P% J穿孔(21) puncture
- _9 F$ n2 F% }* X6 ^5 R" o变色(16) fade0 L/ e( X2 {2 ^6 W+ a3 I4 N
陈旧(30) worn
+ A) d( x) ^: i. N- w! g脱胶(31) adhere: C; Z0 b2 N8 L9 E. K9 C& ?3 c
2 z. ^8 e& v7 w& }' O* m! ~( t z9 C3. Common part component defect terms
+ B1 J! _: Q7 }2 @: d# @+ w 设备及零部件缺陷术语% K6 i/ l# F& p2 T; |
Common part and component including : Plumbing, Wiring, Mechanical linkage, Fastener and Miscellaneous.$ T/ h( _1 q. U! D6 p3 K0 l& t+ k
设备及零部件分为:管路、线路、传动机构、紧固件及其他。5 `) R3 U* i8 I- Q) q0 p/ M
. ~2 j7 @4 t, ?4 d
1) Plumbing defect 管路缺陷
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凹坑(1) dent ) `. ?2 P- F, w: t# X c9 j
爆裂(32) burst9 i' W4 J, f6 \. Y" Q. A. T' B
擦伤(11) chafe. n# L% ~& }; l7 P2 g% ^
滑丝(33) cross thread
I% I& ~& J! f+ Y扭曲(34) twist& v' U1 u' Y2 J" G- H
渗漏(35) leak
! j; s" _+ ~! {6 O& U- ~1 f) A% a3 S堵塞(36) obstruct
" A2 y6 m! U0 v; r) O1 l/ c/ Z0 U' e; S5 r 7 Y p0 |" V; w8 ~) L! T; r% [
2) Wiring defect 线路缺陷, d5 c6 W% i' Y- ]
, O: e7 q- k( N+ [; E% |腐蚀(7) corrode
) P) ^+ m: {/ d4 T# Q1 G y磨损(11) chafe
; p; q5 G+ `0 q; g( O1 \相碰(37) contact h+ S1 L! U0 L/ n) G$ `
断丝(38) fray4 K6 J& C0 C0 I7 y8 W
熔断(39) fused
2 w( j+ K1 `. ?弯曲(40) bend
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" Q6 Q# ^/ K% Z3) Mechanical linkage defect 传动机构缺陷# P4 f% n) R( m0 Z
, ^: S$ d* b$ U$ k4 i" L断丝(38) fray X3 p! a3 F" X
松弛( ) slack
8 N2 N! |2 g4 @9 d! s! \扭结(34) twist' `9 M- m! C) P- Q: @* d+ r6 a
磨损(11) chafe
* d4 w1 ] L) y, z脱开(41) disconnect5 S O4 w% q$ X( @! `9 e
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4) Fastener defect 紧固件缺陷
5 e. {3 `4 l& \# ]4 S
. k+ P# H; J/ k* p' ] 丢失(42) missing
}" G3 D: a7 } i# q1 S 松动/松脱(43) loose6 V4 H l# D9 \' ?8 J8 ~9 ]
腐蚀(7) corrode
& Z `5 u! T. O2 `# b( c3 I 磨损(11) chafe
- F, i0 E2 ?2 M- g7 ^! s+ P7 i V7 Z 未关(扣)紧(44) not secure
+ { G) ^( g/ J/ O% y
% }% {3 c' V) P1 d; y$ [& B* o, ^! q3 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.
: Q$ P1 p, ` d, k 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。
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& `9 ^3 @9 e! c9 h0 E: O6 ?7 ~/ G a). Sealant 封严
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& U& Z B0 K4 \ 脱胶(31) adhere6 T2 y, E2 Y! `
老化(26) deteriorate
8 z- ~1 x5 E( v 不均匀(45) inconsistent# F# ^+ P5 U: z
" w. X' U. ?+ F* h% J# C b). Wheel Assembly 轮胎1 j1 v" S- K# r4 D% P/ C
见线(46) exposed cords
1 b+ R n$ m7 q2 W% ~6 G 磨平(47) bald2 I4 z9 g8 W) u7 [% R& H& C; P9 a
扎伤(21) puncture% D- c; n9 x7 a' |8 O% [
气压不足(48) insufficient-air-pressure
7 v b* l! }: }8 s3 s 9 }" k2 X" S; t* Z
c). Life Limited Parts 时寿件 ; W7 l- u7 Z! e3 U3 v" H& ]
! T. B% q2 |# @+ Q0 Z- D 过期(49) expire
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d). Placard and Marking 标牌/标识
7 c! C$ L _, S
# d4 c: j8 B3 c7 y9 S& j 模糊(50) illegible
! J" f$ H8 E7 u3 W/ i 缺损(51) damage
1 V3 m6 Z' Y: Q: M$ k 丢失(42) missing( D% U* I3 u8 z& U5 M. H
翘起(52) lifting 0 L8 r" X; K1 ]' T" t9 Q
9 q* O" ~6 @" K7 x5 k
e). Slide/life Vest 滑梯/救生衣( l' x4 V( ?9 Y* W, o
0 ]$ L2 l$ f3 {6 d# m6 Q 散包(53) not properly packed
- ?/ l6 h8 I( s8 d$ ] N. j 变形(54) not properly sealed' \ D% I% p" t6 ~- y+ G) m
5 L3 T; u* U' ?/ Z! w+ X: \' u0 t4.general defect terms 一般性缺陷术语
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' `- W ?$ a8 \ 脏(55) dirty
0 J) y: m0 S- U1 U% V 陈旧(30) worn, E9 H# b* e+ M& O$ Y0 g# }% `! x
断裂(56) fracture
: A0 e& S- n2 ]; {" i u 磨损(11) chafe
8 |$ w2 f' R, B( _# T/ ^ 超标(57) exceed-the-limit" e' h% q, |. v" b9 e( O9 r8 H' }
丢失(42) missing
: i9 v& [: @4 X( d; F* `( i9 M 腐蚀(7) corrode
6 V. D7 O: Z4 M* ~ X1 D Z 裂纹(9) crack
$ Z+ n" a+ [0 E% ? 空行程/无效行程(58) backlash1 E2 C5 z3 H; z- w* H: h( {+ v% a
卡阻/阻塞(59) block) n. ^8 [6 ?$ z0 b3 R
鼓起(60) bulge/ P( G, k! I8 v( F# e
污染(61) contaminate, l7 {0 x* ]( R# s. \0 m
不一致(62) disagree
8 H) m5 |, X! ?" A (电池/气瓶)被释放(63) discharge
% b, x: f# r! j2 k) ?1 B3 h B2 H% g 装错(64) dislocate E. N$ B! }5 H7 Q: \% G
失效(65) fail( b- Y/ j2 [! b( u+ N! c3 v( @/ _. |
摆动(66) fluctuate6 ^/ ~! n" Y; N5 o |$ ?
抖动(67) flutter4 _, I2 B4 F! k2 M, a
不够/不足(68) insufficient7 }3 ]3 I$ I8 u3 k
不工作(69) inoperative) o3 N7 I9 G8 M' A
(不)亮(70) (not) illuminate7 H8 [' h: V) p! Z( I
干扰(71) interfere. _ _' {9 H& ]0 y7 Y
扭结/缠结(72) kink
+ v4 p2 Z M, z( q: L! O5 u. c 走向错误(73) misrouted2 M- H# U% ?6 r4 S9 s K2 P' U
漏装(74) not installed( R) D8 T+ c& X" x' G1 l5 t5 Q6 C
相磨(75) rubbing
" {6 |9 x3 o- C! _8 F; L; P4 E 干涩/缺乏润滑(76) un-lubricated0 O6 e( T+ H! d' B" w% A. x Y# l
不能复位(77) will-not-reset
) F' V5 c9 m- z8 ?8 z
" @6 V8 R0 X1 c% I) K& u4 o7 d (1) dent: 凹坑5 \' d0 E( ]3 p" d2 L
A depression in a surface caused by pressure or impact.
, d J, B. @2 O受压力或冲击造成表面的下陷。
9 g9 I+ K4 y1 R0 L For example: Left horizontal stabilizer outboard leading edge at WL 368.25 dented approximately 2 inches in diameter.(Area marked in red)
) h8 e8 w* {1 O. r 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)。
) P5 M. C* ~, i. c: h 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---( J' C( m, t7 F$ `& `
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。3 _# z4 b" R o D
& ~: b3 S7 i" Q, o5 b1 N/ J(2) notch: 凹槽
. t9 P7 B4 V! u- L" F. O: K A “V” shaped cut or protrusion+ W( d2 o i- i" _ B6 y! V
V字形的切口或者突起 ~# c' ?4 ]+ y0 C$ _
For example: Forward L1 entry door number 1 floor panel has a 1-inch notch 6 inches from the forward right edge. ! @5 V8 ]5 \6 P
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
) ]$ Z6 q1 M: N槽。
* V/ k5 p2 ~+ }" R2 d p. _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---.$ X3 O# H1 M' _" l) u. w) @, z
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。
8 K' L$ P0 c6 ~3 B: J8 a 9 X) C U" Q7 T1 b9 B/ X
(3) deform: 变形
8 [ o6 }( B; F( \5 c; RTo misshape the original form
! ]( b0 l% C5 Z; t: F原有的形状发生变化
3 p3 r! q$ A" ]! w# e1 ~For example: Left wing number 2-fuel access door is deformed. r( `# a9 H, V4 E: u4 ~0 E: }& ~
左大翼二号油箱盖板变形。/ Z. ^ ^- I" y7 v2 `
Replaced number 2 deformed access door in accordance with AMM--- Carried out fuel leak check in accordance with AMM--- with no defects noted.# X) e" R v; x5 O N6 B" k% K8 k# y
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。* i3 B N1 b" o# J! o+ e p" H& P8 C v
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(4) nick: 划痕
9 t& y" [5 C b* `3 {; F; @ A shallow notch, cut, or indentation on a surface. }( Z7 _( P5 S, ~8 D; [1 Y4 c
表面上的较浅的刻槽、刻痕或缺口。# W4 J. ?5 n5 D1 D5 y3 g( F ?5 h
For example: Right environmental control system (ECS) access door, after right corner has 4 nicks on external surface . Area marked in red.
3 ^5 k- e; S# m; ~. U$ q 右空调舱门右后角表面有四条刻痕(已用红笔标出)。7 x2 r6 s- T6 W; }' U8 L" m
]. h% f! z! m1 y' v Detailed inspection carried out with reference to SRM---no delamination6 M" [" C* O+ w' H
noted. Carried out permanent repair by filling nicks with fiberglass and epoxy
. l7 h' g1 |1 W0 c- a, presin BMS-387 with reference to SRM---.' T$ C3 {) r5 i; D: a
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
" ^2 \* ^3 d6 t3 E% z4 Y8 X理,使用玻璃纤维及环氧树脂BMS-387填平刻痕。5 a+ b' m. s- u: X& M
- {4 H% _ t# f( q6 q6 d1 \(5) pitting: 点腐蚀/砂眼
9 E) j; S+ `0 f0 ?, g Small cavities, depressions or scars on a surface.
1 g7 A; {: O5 u 表面上的较小的空穴,凹陷或凹痕。
( D7 f8 [/ F7 i7 IFor example: Left main landing gear number 1 brake aluminum hydraulic line has pitting.( N7 `/ o' f7 G0 |0 [- }. U9 i0 R
左起落架一号刹车铝液压管发现点腐蚀。
k* l7 f+ [' o% s Replaced left main landing gear number 1 brake aluminum hydraulic line with: T: X+ k1 k* _' r4 l5 h/ s
serviceable hydraulic line in accordance with AMM---
( E: O6 G) P. ^/ n 根据AMM—更换左起落架一号刹车铝液压管。
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' T. y2 k! l2 y0 K(6) broken: 断裂) W" g8 o& ]# H' T) P
Forcibly separated into two or more pieces.
5 |- P4 D5 i/ U- z! W( S/ z 被分成两半或更多块/ J- E! E9 _: ^( w* q2 y
For example: Flight deck entrance door has broken door latch and will not lock.
$ y, V% y3 V" ^/ _' C* O8 f, _' i/ l 驾驶舱门锁销断裂,锁不上。
/ R. ^9 E; V; N4 F+ r9 ] Replaced broken door latch on flight deck entrance door in accordance with AMM--- Operational and functional check good.
O( E3 g+ U! s) y3 ?( ?8 Q# G" ` 根据AMM—更换驾驶舱门锁销,操作检查正常。
! P# |0 n# Z' }/ ?5 H" w3 H; _0 u
& O5 Y. r* F; L& I& T(7) corrode: 腐蚀
0 ~4 }( R0 H: j: t$ d To dissolve or wear away gradually by chemical action.: z2 [# _! Q) M# I# f4 k# d; [
氧化或化学污染造成金属表面逐见破坏的化学反应。
' Z; j/ ]+ _$ a2 j! g7 IFor example: Floor beam at body station 360 and wbl 25.1 has moderate corrosion 2 inches in length and 1 inch in diameter.$ _/ a5 y: S( d4 A8 @1 D
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 e/ i3 k% c* A# M1 @ 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 G. p& @$ n9 i8 U* ] 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。
3 w# d( K( ]- g1 ~/ ?* t z- W* l5 c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。5 j+ F' ?2 t- e& ?2 e
0 `5 V6 r) o' @- @) ?& b+ e
(8) scratch: 划伤- e; L n; ]% o7 e; |1 F& |
A thin shallow cut or mark on a surface' e2 S# d% v j8 l6 D
表面的薄而浅的切口或痕迹。' \" h; K2 q8 u. s/ U4 q$ K
For example: Left cabin external windows numbered 12, 16, 17, 21 and 27 are scratched (obstructing view)' x: A/ r8 w% t2 I
左客舱外部12#、16 #、17#、21#、27#窗户被划伤(阻碍视线)。
( @& { g+ `2 t- e, i 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.$ B2 e2 z- u/ z8 W8 ~) ^, e
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。! R8 |- Q8 O( @5 N' f) H4 }% _
# u- d- M' i6 i1 \: I' H, R, q, N+ ^(9) crack: 裂纹/龟裂9 z" E0 p D2 L$ p$ M! Z
To break apart without dividing into two parts.
0 N9 v& n4 x) o 裂开但没有分成两部分的破裂。8 d, w U7 [* ~- G5 k" _8 T( A
For example: Number 2 engine fuel control cable located at Body Station 360 and Water
' V ?! {0 e7 t; O7 mBody Line 25.7 has cracked turnbuckle.- I. K3 y5 \9 Q4 [9 P1 q, ?* C
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。
- R8 G; K$ g+ V3 xReplaced cracked turnbuckle with new turnbuckle in accordance with7 V; z2 d0 {% ?
AMM--- Travel and functional check carried out in accordance with AMM---,8 h+ V; [5 n' p j4 z( a N
no defects noted.
0 o2 Y, c l! q- ~$ i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。2 [" D; J- M" l& j- n) m
$ _" [% H9 ?7 _& F$ j% ?
(10) burr: 毛刺4 v! ~7 Q9 N: y$ E
A rough edge remaining on metal or other material after it has been cut or drilled3 I5 z1 V1 n# {# q3 G* @2 O
被切割或钻孔后留在金属或其他材料上的粗糙的边缘.
' D, e) Y0 F2 i4 PFor example: External fuselage repair at body station 727 and stringer 9R~11R has burrs at
8 u, l0 K+ o0 P: @/ y1 W: F6 R7 Tall drill holes.7 \& k2 p5 m" K* R3 i1 A
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。7 ~7 _# r9 E$ E
Removed burrs with rotary file in accordance with standard practices and
9 p0 C% y" Y+ M# S1 qSRM---.
% X, |" b" J8 k6 g, y 根据标准施工手册及结构修理手册—的要求打磨去除毛刺。
. K) h& P0 Z) X% q% \7 L8 P2 B; O 1 S, z/ x1 ~0 ]1 o1 I
(11) chafe: 擦伤, c% {# F( y: \) k4 d7 {8 c
To wear away by rubbing.( {" Z1 Y- d8 v o4 W5 C
因为摩擦而损坏。9 h( o+ } f# y& k: S: n* s
For example: Forward cargo compartment after corner threshold chafed by cargo door.& G) L8 \: S4 T) B$ y
前货舱门槛的后下角因与货舱门相磨导致擦伤。
8 V1 F7 c; I7 E7 v( @. m Forward cargo door upper support bracket worn. Replaced support bracket in
/ }+ X$ w. t4 Z' _1 Q& N- maccordance with AMM---eliminated chafing.7 |3 t: |$ `1 ` E8 w
检查发现前货舱门上支架磨损,根据AMM—更换该支架。- X- h, ]* p1 z9 S( z, B
. Z7 x0 n1 e( j
(12) protrude: 凸起/突出7 c. j2 {. I* E% `. D _/ w9 M
To push outward.
7 Y* x3 Q- G/ q4 V5 Q! y向外伸出。 w# Y2 ^$ m, U. o" ^! l' f, d
For example: Forward external fuselage servicing doorstop is protruding through access5 b) V' j: H/ G* _7 L
door.: T8 G% t, P0 [ s; r5 w0 `
前外机身勤务门止动点凸起。
' A3 b5 J( l* m j: P- V: [7 d Repaired forward external fuselage servicing access door to original contour with reference to SRM---. Adjusted doorstop to eliminate protrusion in accordance with AMM---.# f! O1 N# X( E& c+ z! c0 a- J
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 U! h3 g, Q& ^# e; N2 B8 c
5 A8 a& ^ u! [' i& Z8 n d6 O9 ]
(13) sag: 凹陷
3 [7 H9 E! `, J! _To sink, droop, or settle from pressure or weight.
" |. `) Y+ D. U# z! H" h0 G- p因压力或重力而下沉,下垂或下陷。5 v# F2 r0 \' Y3 v. n
For example: After cargo compartment overhead ceiling panels are sagging.! g) U& X A8 c9 l
后货舱天花板凹陷。
; h. E8 Z% W3 y$ GDetailed inspection revealed ceiling panel screw holes worn. Replaced4 U! m- {* ]9 D
unserviceable sagging ceiling panels with new as referenced in AMM---.4 b6 j7 D4 Q1 Y" y3 f$ 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: \9 S& q5 \' ]% J5 v
板。' d8 {- n. r$ I1 f9 [7 V! m
/ E8 y* x' H. {4 t(14) rough: 粗糙7 |% R) I7 w% B$ p9 r
Having a bumpy, uneven surface.
0 S$ w2 n' h j* T表面不平坦,有起伏。
0 V6 }2 Y3 H' }) ]: rFor example: The protective finish is rough at the number 1 engine inboard pylon.
+ q* r; f4 w2 q& f4 }4 k E5 Q 一号发动机吊架内部的保护层粗糙。
6 J: w0 I+ s( ~' a( `2 b Removed rough protective finish at the number 1 engine inboard pylon in( v& n% u% _* L7 C( k/ m3 `8 E
accordance with SRM---. Applied 2 coats of enamel to restore protective& E$ l% Q) c7 J3 f/ M: o, X
finish with reference to SRM---.
4 A! m' L) h0 | 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。3 u: `9 C- l( Q! K
e7 N# Y3 W% w! N(15) finish (missing): 漆层(剥落) |! l6 l# o5 R4 Z# M
To protective material used in surfacing and finishing flake off.# K9 W/ w. s6 O6 E- y9 A4 Y: q
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。
/ G$ w# s1 D( w3 j' R! {+ C* v6 J: aFor example: Fuselage skin protective finish at pilots and copilots number 1 and number 2
* c% F- [2 F5 P/ xwindows missing./ v% a8 e& {; }4 \! k5 }
正副驾驶1号和2号窗上的机身蒙皮保护漆层剥落。
k: b$ E; C& C k& k) c& _Prepared affected area of fuselage skin at pilots and copilots number 1 and$ M9 ^/ ^+ h- b! z9 H! G$ Y" Y
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.' W. K$ X3 h' t" }7 y; _
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。
. w, Q& ~: T r( e4 M/ ~
: C& C% e& e6 ^, c, Y3 p' W1 A( L, C(16) fade: 褪色/变色
1 n6 D8 {8 I" I4 B# vTo lose original brightness or color.( d! i* A# G2 W
失去原有的光泽或颜色。
( E+ O. E+ M# |! l) f2 dFor example: Number 1 and number 2 engine intake cowling chrome is faded.5 S& Y% H9 T/ y0 {+ @2 I* ^; @* J
1 号和2号发动机进气道的铬层褪色。; l$ C' a* A3 L3 e" X) l
Polished number 1 and number 2 engine intake cowling chrome with reference
* {6 S9 w: z3 Y3 |to SRM---.
/ E: p Y* b3 T' I1 ` 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。
" j6 o7 H: k- ^0 }% P# l: p " ~+ L& W6 | I8 E' q
(17) entrapped (water): 积/含(水)
9 I$ l. z. ~# O+ X! R' l4 d. g' S+ Q" hTo collect in an area.
! {7 S8 B" M! N% {8 ~6 ]水或水汽在某区域内聚集。
- l! L. l9 {( Z% x% _For example: After cargo compartment forward bilge area at body station 840 has entrapped
6 d5 ]" M' L% R3 ypotable water.- s; O5 m7 \) V( F M- c5 [7 |4 L, {
后货舱在机身战位840处的前部区域有积水。# e ~3 ?0 _ c
Detailed inspection found pressure drain valve clogged. Removed,cleaned and reinstalled pressure drain valve in accordance with AMM--- Removed residual entrapped potable water.
. r& R6 A/ G+ x% M6 m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。
& X2 a# h- }/ l1 a
9 ]! O$ O& [9 f- J% }(18) oxidize: 氧化- z; ^; V- F/ ?3 c$ v; O
The containing of oxygen usually caused by natural elements.) j5 H4 \5 c+ P5 a9 t6 f
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。
: y/ N: a+ U% T; AFor example: E-3 rack lower after corner is heavily oxidized.
5 ?3 A2 w+ C' z$ X/ U E-3架后下角氧化严重。1 s- y! D8 C8 e6 y: l) J+ S
Removed oxidation at the corner of E-3 rack in accordance with SRM---.
5 V! D% S6 `. C 根据SRM—去除E-3架后下角的氧化。! H \, B7 r" J
( E" U, ]" P) `% e
(19) distort: 扭曲9 ]0 R- Q o. I* [1 g4 v- }4 u, B
To twist out of a proper or natural state.' l% Q7 f! @# D; }& U
因受到扭力而导致原有的形状发生改变。
8 X+ e6 c4 h7 J# S; jFor example: Access panel 2145J to left wing number 3 slat actuator distorted.. ~8 b- W. R* q8 _. v E
左大翼3号缝翼作动筒的接近面板2145J扭曲。
$ C& Q7 l5 u6 ?7 C" | Replaced access panel 21458 with new panel in accordance with standard
& A2 V' t3 G; C. f0 \0 Epractices and AMM---. Original panel declared scrap, tagged panel as much
% l5 b a- N" z* G4 pand routed to MSC to return to customer.8 f! v7 x/ C7 g( @& D% W* A# K' \
根据标准施工手册及AMM—更换21458盖板。旧件挂牌送航材处理。
" S& D K7 z/ D . w! ?; q7 z: k5 H. K; s; j' A
(20) (not in) contour: 外形/轮廓翘起
1 A7 \/ h. Y# n4 g# SA shape or outline is deformed.
6 J: O3 S* @/ U5 C" i9 D* Q' R形状或外形轮廓变形。$ b8 \+ }" ?, i; q6 I
For example: After lower corner of after fuselage external servicing door is not in contour/ c9 U8 q3 K# _' {
with the fuselage.
$ Y1 H3 h, M( M1 C9 [) G! s" p后机身外勤务门后下角翘起。
/ z: v' x- j xAdjusted after fuselage external servicing door to contour of fuselage in+ S5 o/ c+ J& g; O' n5 I6 T
accordance with AMM---.
+ [$ K. Y# f9 l根据AMM—调节后机身外勤务门正常。- b9 M9 B2 `& Z) p' o, p, I
1 Z3 ~2 r# S( n7 u/ ]" x(21) puncture: 穿孔/扎伤3 W7 f5 G8 O! D" I
To pierce with a pointed object.- Q( A( l8 B4 f
被尖锐的物体刺穿。
6 t& Y6 E( y/ _3 aFor example: Number 4 tire is punctured.) x, [% L6 @7 h. j, u
四号轮胎扎伤。
" r% c6 h/ q6 U) y Replaced number 4 punctured tire with serviceable wheel assembly in
+ _( _9 e; L% w$ y9 d. L/ Haccordance with AMM---. Pressure check normal.5 B* [7 A" O$ a$ X; I
根据AMM—更换四号轮胎,检查压力正常。5 Z, C6 R* Z/ |0 p
" B% V3 `" V# |5 l7 r* C9 p(22) chip: 碎屑
' U, G) W" }) t! ]A small piece broken and missing from a surface.
3 Q" z0 l# J0 D2 ]6 \4 R/ Z从表面剥落的小碎片。% w9 c8 M: y. W+ D& G3 y
For example: Starter magnetic chip detector has evidence of metal chips., x/ q7 Q N* m3 D$ b
起动机磁性堵塞上发现有明显的金属屑。
+ z. R( j$ Z+ b Removed metal chips from starter MCD. Drained and replaced oil, operation
. d/ P" j9 P% F8 zand leak check good in accordance with AMM---. Reinspect next “A” check as+ {* B3 Y! v8 }; ~5 ]
per attached EO 80-003-1.
* L8 y+ l8 X: a3 T: m 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。2 ^' ?6 m) y" G; X% M/ X
6 B+ |/ e* y6 a: s' j3 h
(23) erode: 风蚀/风化8 ?: ?8 Q& Z1 q3 Y, D J) D- {$ I
To wear a surface away by weathering, abrasion, or foreign particle.
* ^0 H* n8 s# } f. `因天气或外来颗粒等原因导致表面被磨蚀。* S( Q) Q0 y# C9 }* _* N
For example: Number 1 engine intake cowling eroded 360 degrees, 2 inches in width from1 r; j, G% M( u& H$ h/ X
center of forward leading edge.
$ j. W& U5 P& }一号发动机进气道周边风蚀(2英寸宽)。
, i9 ^8 o! Q: D jRemoved erosion by polishing surface with reference to SRM---. NDT
, ^9 X" S; _+ _+ |inspection revealed 0.02 inches of material removed, remaining material 0.23
0 c; l7 b- h R, ]' q4 fof an inch within limits to SRM---.( p3 h F/ k6 g7 B* T
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
# G) j' S* n. E& S+ H# L. m$ a1 v5 S$ O少0.02英寸,尚余0.23英寸,在SRM—规定的范围内。
' {" w; p6 k; A
, d1 u# k$ r+ S! ~- D& S(24) mildew: 发霉6 F6 j: Z# P2 b9 f, D2 }* k
A fungus growth.* \7 c7 d* ]: Y s" T5 |* a. ~
有机质滋生霉菌而变质,常见白色的生长物。
. u4 {- z( \9 Z5 y$ D/ `For example: Forward cargo compartment insulation blankets in after floor area are moist
6 x- R& }' b7 r5 Q1 k. }& Mand have mildew.
' }9 V' |( E" M, K/ d前货舱后部区域隔热棉潮湿发霉。
8 b2 v: t8 C Z6 d; pEliminated mildew and moisture of forward cargo compartment insulation/ M2 i n/ c+ w3 a
blankets in after floor area by fabricating and installing new in accordance with
& u3 Q! d2 ~6 x8 [0 y% sSRM--- and AMM---.! e, T% Q8 ]! 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
" ^3 b! i/ N3 |/ ^$ o5 I: H2 _发霉的隔热棉。
& k" Q8 o" I# N6 G 8 V2 _1 i) p* h
(25) delaminate: 分层
9 E' b4 j4 S+ ~- A, C3 \The act of separating into layers.
+ W' b @- n" i6 [9 }/ y压合在一起的材料互相脱离或分开。
: O6 J1 R, A8 y3 JFor example: Nose radome delaminated from impact of “bird-strike”.1 C2 T+ [8 `4 L( i7 M ?- G0 G
前雷达罩因鸟撞导致分层。3 q! `& [ P% p8 P0 J7 f/ H P
Removed delaminated core section and replaced with new with reference to
4 ?7 y* [' ^ y; _SRM--- impact test carried out. Nose radome OK for service.
" F- ^) W \3 H/ y根据SRM—更换分层的核心部分并进行冲击测试,检查正常。
& W3 e' S! e* ~' [* J: ~ ; b0 ?+ C+ U9 W# V
(26) deteriorate: 老化4 _5 ^' X( s: P* b; m
The diminish or impair in quality, character, or value.) F: K. \1 f' D6 t+ k! A
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。
, j) |; y7 b# p. x2 }) PFor example: Number 2 engine to pylon fire seal deteriorated., U9 y" X* E2 r
二号发动机吊架防火封严老化。
3 M7 z* b) D" B Replaced number 2 engine to pylon deteriorated fire seal with new seal in
' y/ F* F2 [0 X' p" r. I3 } F3 \3 daccordance with AMM---.2 }1 ~1 ?0 r" I* K& t; A" _
根据AMM—更换二号发动机吊架防火封严。' u9 W5 G4 |/ q* `1 Y
. q! g3 {6 Z2 n! |8 U" O(27) wrinkle: 起皱. Z: p* I9 k% {' x3 v# E
A furrow, ridge or crease on a normally smooth surface.
+ \( \, J4 ^' b正常的平滑的表面上出现的皱纹,或折痕。
9 i) \5 |7 b( Q2 T: w4 p3 oFor example: Forward galley wall at flight deck entrance has areas of wrinkled wallpaper.
0 X# L% S' H/ v 驾驶舱门过道的前厨房墙纸起皱。2 C9 t! d q. C" M% _3 U3 j' ?- B
Eliminated wrinkled wallpaper at forward galley wall at flight deck entrance by4 a2 Z: `7 J5 c8 J# x6 X0 }
replacing with new in accordance with standard practices and AMM---.
( L/ r% e6 |: A( H" u9 j 根据AMM—更换驾驶舱门过道的前厨房墙纸。7 y1 D5 B5 }) f( H3 o5 Q
- y9 }! n! Y5 Z1 {" F, u( a(28) saturated: 受潮7 {( ?! O$ V# r1 z
Soaked with moisture.
1 p( h2 @! J- r3 q3 m& |物体吸收了水分的状态。3 O4 V* {/ R/ o: }: ]0 M1 R3 p2 S
For example: After cabin floor carpet between lavatories B and C is saturated with water.
2 ]1 J* V {- ^# h- K 后客舱厕所B和厕所C之间过道的地毯受潮。
$ d4 Z+ `. K" _. Q Eliminated saturation of after cabin floor carpet between lavatories B and C by
) ?) L4 I9 l4 a5 L6 ]* R) ereplacing with new in accordance with standard practices and AMM---.
' U1 ~" i5 ~, `6 b8 y2 ^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。; Q1 P$ h* t+ H# C, a1 K. L! Z( x
$ E1 i& V4 l4 d% R3 }(29) tear: 撕裂
3 F# O2 M2 O2 c5 Z" C. D; ~To pull apart resulting in a tip.# a d* |9 n% l+ }- P4 Z
裂开后分离。8 K0 W/ `$ T) A' N
For example: Number 8R window shade in main cabin has a tear.
3 D4 s5 [: T7 A0 }. } 客舱8R窗户遮光板撕裂。
3 v; j2 Q9 I& }; Z4 q: L, m Replaced number 8R window shade with serviceable window shade in
# s! f. I( m" d3 R( J' o) Waccordance with AMM---.
- k" O6 |: C& T# A' r7 t根据AMM—更换客舱8R窗户遮光板
1 q7 M2 X. Q% z: x) e + Q$ {2 g7 j7 }% R: |' S& P
(30) worn: 磨损/陈旧6 V$ i2 |9 W1 z. x0 V% `5 `
Unserviceable due to excessive wear.
# R& q; T1 ], H7 S1 H由于过度磨损而不可用。
% O# }: `# r A- [- \- jFor example: R1 service door upper guide and door latch on doorframe is worn.. h1 k F* Z: U2 k' S; i6 F
R1服务门上导轨和门框的门闩陈旧并且磨损。
: g9 d" I5 S( G2 E3 h- M Replaced worn upper guide and door latch on doorframe in accordance with0 @. F3 O: g5 C$ l5 t8 w" Z
AMM---. Operational and functional check good.( M6 A6 ` A& \' a% | k$ A% s _0 e% K
根据AMM—更换上导轨门框的门闩,功能测试,操作检查正常。
7 h) E: K t9 x6 d
. K6 U" K+ u: {- w/ h(31) be not adhered: 脱胶
! J2 ] r' {5 g5 o+ U' w; x4 xUnsecured and not positioned in place by glue or sealant.3 O! v6 `7 Q9 z Z# B8 d
因附着力减弱导致脱开。
' h3 ]! i- j$ a, S3 E: BFor example: Left emergency exit hatch external “EMERGENCY EXIT” placard is not
6 {- Y" h. [0 \4 _; I* i6 Ladhered in place.( C4 F- |7 C4 I
左紧急出口舱门口盖“EMERGENCY EXIT”标牌脱胶。
; k, S; }' D9 O3 n9 K7 SResealed left emergency exit hatch external “EMERGENCY EXIT” placard in9 W0 Z3 h1 C A: U/ O5 U' L+ G! C
accordance with standard practices and AMM---." ^" X5 M5 I8 ?! D& ^
根据标准施工手册及AMM—重粘左紧急出口舱门口盖“EMERGENCY5 X5 B. ]6 I/ V7 o% k5 U5 C) q4 Z
EXIT”标牌: t$ m2 t! b* z$ T
, v$ A9 U) l# k, b& U" D
(32) burst: 爆裂3 M6 B3 X3 O+ C# B8 u+ k: P
To open and suddenly come apart from internal pressure.: @/ Z2 |4 ^- d% Q) @- y
因为内部的压力突然炸破或剧烈的爆开。
% O$ ~: n9 A" n) C5 }4 b6 x9 b6 {For example: “A” system hydraulic pressure line located in forward left wheel well burst" |$ j& B+ g& x0 R
during landing gear functional check.
# L& U: m5 i/ R/ A6 }0 \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。: X: h8 N3 K5 x7 I9 h" \. V- u+ b" W$ h) r
Detailed inspection of “A” system hydraulic pressure line,revealed grommet5 e8 H: P; i( g* m2 ~
of retaining clamp missing resulting in chafing. Installed new “A” system: k, Q) Y5 }4 e4 Q! \. z1 [& r! z
hydraulic pressure line and clamp in accordance with AMM---. Operational4 w% i" e, g/ d! m! k, g
and leak check good.' Y/ q! U) D1 f) z
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
) M- Q* [5 z& O' T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+ u" _, e: Q1 q5 _" C$ W# }
漏。4 K5 @; U/ O3 ]/ N$ u
; ~* a. `) h# p" R(33) cross-thread (pertain to plumbing) 滑丝(限于管路), A6 k y. Z4 T4 t9 z) l( |$ L3 Q
To damage threads to an unserviceable condition.
" C3 h* Y0 A6 ^. J螺纹损坏后不可用。" V) t7 c3 V* v* x) d2 l
For example: Left wing number 1 ground spoiler actuator hydraulic pressure line has2 R0 Y' Z: r8 ^) q, h$ e
cross-threads at “B” nut." r7 D% T1 b* B4 s
左大翼一号地面扰流板作动筒液压管B螺母滑丝。8 v; \+ U3 K! J( w: V4 \7 [
Installed serviceable hydraulic pressure line at left wing number 1 ground' H, v9 ]( D" G# |+ \" B
spoiler actuator in accordance with AMM---. Operational and leak check good.
. L% n( Z% x6 b' t r6 v3 B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,
! d$ D3 s8 u0 {. Z无渗漏。& }6 ~3 B5 N8 x5 ?
4 v: {$ A. z- C2 L
(34) twist: 扭结/弯曲
/ T0 h9 E( ~; |# e PTo alter the normal aspect resulting from torsional stress or strain.! S& P$ Z3 l# [, w1 ]1 o& a
因为扭曲的压力或者张力导致改变了正常的面貌。+ {4 d! ]* [0 v/ `
For example: Right environmental control system intake door linkage twisted along routing
5 E2 H8 l# G* ~2 W5 i" nto exhaust louver.
' f- V# o5 l" E) a! z4 z右空调系统进气门传动连杆朝排气口的方向弯曲。
$ `+ m4 v+ O) M) D) {0 G/ pDetailed inspection found broken bolt at eyelet connected to exhaust louver.
2 N, @5 V% T6 i/ w9 ?; ?* U) ], PReplaced broken bolt with new and reattached eliminating twisting with2 F- O3 }" I" _, J# [. j
reference to AMM---. Operational and functional check good.
! c1 C* K) y; p4 a详细检查发现排气口的螺杆断裂,根据AMM—更换该螺杆,操作检查正0 P/ \6 \+ W0 }" F S& v6 x; r. ~
常。) \5 N# F) v0 c* n }3 t) U
p& \5 c" S% N; |7 A- q(35) leak: 渗漏% \' P+ X1 y- K6 K
The escape of a liquid or air in a system.
# n. |! I- Q- E7 _5 B7 I, T9 c系统里的液体或空气逃逸出来。& u& t. _9 \% @- P3 N& j& P: m
For example: With reference to routine task card 37-265-1 pilots pitot static probe test failed. S8 a! ^; k9 s' D: m, K/ l5 w1 ^5 i, {
due to leak in the system.
* b2 ]. W: p- E9 X( L5 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。; c1 L. U- w8 x
Detailed inspection found loose connection at pilots static port. Removed “B”
9 u6 j2 N8 O$ O: k; P nut and inspected with no defects noted. Reassembled connection and leak
7 E# o( y- O. L& w# m9 @; K4 R7 W check good with reference to AMM---.
: ~ h$ @, C9 D9 V* [, U) g, X 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
4 m U5 l# o. B陷,根据AMM—重装接头,渗漏测试检查正常。
$ _$ ]6 J8 X$ s) x5 E; u+ s4 j
% \3 ?! @. ?9 K2 L" M! @. H4 e(36) obstruct: 堵塞
, f& ^5 w/ q2 oBlockage by foreign matter.* Z0 ~. ^- U4 z0 k- y" c
外物妨碍管道的通畅。
: @5 y. N7 l w( p- E: nFor example: After lavatory service panel inoperative, suspect obstruction.- e' Y# o( O2 ~- o) C
后厕所勤务面板失效,怀疑有堵塞。
! i9 o2 [1 i" U& M& O# Y Detailed inspection revealed drain system plumbing obstructed with foreign matter. Cleared foreign matter from drain system plumbing, operation check good in accordance with AMM---./ D1 ]/ E; a: g$ m
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。
- v& L; B9 `' |# _" s
& z, g% x) x/ z, d' v(37) contact: 相碰 6 R: O; I6 _* o
Touching of two surfaces or objects.$ h3 _8 l! N% f
两个表面或物体的相碰或搭接。
( ~% f5 s2 L/ NFor example: Left wing trailing edge has aileron control cable contacting pulley bracket at/ v0 @4 a* d( d" t0 H
WB Station 245.9. i' x; o) ~/ n' Y0 g5 S% ^- Z1 P/ K
左大翼后缘在WB位置245.9处副翼控制钢索和滑轮架相碰。
* Y6 H/ C0 J! Q3 M3 R. C oDetailed inspection revealed pulley bearing worn beyond limits. Replaced with
- b% s4 s; w, M+ ^* f8 wnew pulley in accordance with AMM--- travel and clearance check OK.5 Z6 f2 M7 r+ r3 }& V
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$ _4 K& E6 E6 P
间隙正常。, B! V4 v( R g! k. X7 _
3 R! ?! @- i/ L) k(38) fray: 断丝/磨损# a7 \) U9 ~5 S! r" p
To wear away by rubbing.4 t3 Y$ _3 [; ~% ]+ V4 s$ {
因相磨或反复拉伸导致的损耗。! E8 _) R; j8 l. Y3 S1 |
For example: The lanyard attached to the after end of the right access door to the APU( g4 Y% w/ o9 j" W/ ~$ I
compartment is frayed. N R4 T; g* q; c% R0 a
右APU舱门后端系留绳断丝。
. `' a& ^! C c) YRemoved and replaced frayed lanyard in accordance with AMM---.
# S: m3 E. C. J% u# b3 M根据AMM—更换系留绳。$ N9 H6 H+ ~* \3 t) ~ E+ `) P# Z/ j& p
1 N1 I& j& ?( h) k9 ?: r(39) fused: 熔断0 \# o3 i* H( W! r' V% V
To become united by melting from heat.
1 @/ J) {8 g/ t% t; G& W' n因为高热而融化连接在一起。 7 k3 H8 w5 ?% Q# e+ ?" u. u
For example: After galley coffee maker inoperative. Detailed inspection of after galley coffee
' Q# W$ P) P" ?maker revealed thermostat wire D34768 fused to temperature controller wire
# w1 b. f2 J# u$ i+ q) PE57689.
5 r' [4 X' C; R D0 a$ I% ?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. {7 L* a2 o( l n
置导线D34768与温度控制器导线E57689熔断在一起。
0 _0 s! F5 ^9 f/ eReplaced wiring with new, operational and functional check good with
1 [5 b* m! W" k; l3 X6 }% u( zreference to OHM---.; X; a, z7 s: s
根据OHM—更换线路,功能测试正常。( C# \% g1 N3 `1 _
+ N) O1 B: p- F8 ?
(40) bend: 弯曲
# @' i5 `3 W, U/ u5 p, `Altered from straightness or original position.
$ j- c& V& `9 V1 W) z改变平直或者原有的形状。9 }; `# g, w g! |( a8 Q
For example: Forward electronic bay door left hinge bent.0 j4 U; ?# A/ Y }
前电子舱门左铰链弯曲。
9 m* W) g9 H" s8 \3 F Replaced left hinge with serviceable hinge on forward electronic bay door with
; ~' l5 V: }9 T5 ~ s* D6 Jreference to AMM---operational and pressure check good.., t: b( k! E8 W5 Z9 S$ o+ ?
根据AMM—更换前电子舱门左铰链,功能检查正常。; \: x) k: N5 _* w& S
5 \' E/ j4 k# ^& w% F8 S
(41) disconnect: 脱开
( G1 J' I- C/ x6 b" ]/ BNot joining resulting in failure.
, S7 X0 E8 m! Y8 q因没有连接而失效。# A+ o9 n- S- E3 z, I
For example: Left environmental control system pack temperature control has disconnected
1 ^; J7 M5 Q$ r( ~& y3 Z9 Ycannon plug.6 v3 c5 x+ W6 ^: t, @; T
左空调系统组件温度控制插头脱开。
" |/ ~- ]& }7 {+ @* I, l# ~Reinstalled left environmental control system pack temperature controllers7 |, d' p5 f! `7 P: Z2 S1 h2 _
cannon plug, operational and functional check good with reference to AMM---.! {8 i* R3 w, 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
- H; t7 |) q9 [6 Q+ N7 x& p查正常。
# a# v1 @. T, [" Z $ K8 W. x' O8 Z D0 g0 o, G
(42) missing: 丢失
' \7 d9 v: w; u: R/ j" N Not present.7 A" k" |6 ^, u) J7 D8 ]" e5 D' e
不在位。, q A. {" J( E4 ~7 Z) |, J
For example: L1 entry door has 3 each door stop pads missing at the after middle section of
a0 D1 h* G: L {1 D& b# h4 sthe door frame.
" W) W4 |0 F3 z9 [* M左1号登机门后门框中间位置有3个止动钉丢失。
* ?$ l" n" w7 XInstalled 3 each door stop pads at the after middle section of the L1 entry door
5 I/ \9 J& x+ d( cframe in accordance with AMM---.
- Y! Y% |5 c" f/ q% k# 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。& ~7 w) C9 {' N# q
8 u D0 }; m x6 v0 S6 }
(43) loose: 松动/松脱3 @7 F% j6 g! V$ Z7 L
Not secure.! B9 D/ E% [# n8 D+ y9 P1 \
没有紧固;活动0 y. W5 X$ b. G9 h3 f! N& U$ D
For example: Forward right wing to body fairing has several loose screws.
6 `8 e1 U* l0 z' v p8 R 右大翼机身整流罩前部有几颗螺钉松动。' c! v y W6 Z" W# Y
Found 17 screws loose. Tightened loose screws with reference to AMM---.
. U* ?7 e/ x) {% }7 i; o 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。3 Z! o# E$ l; e( w+ f
5 z8 V+ `' `4 A(44) not secure: 未关(扣、夹、卡)紧
& }; J! D8 u! H! m1 DNot fastened, to make firm or tight.
* ]% O: \: a& G6 X- a$ y8 t$ W没有扣紧,(使)紧密。
$ w* Q0 N6 I2 K( S; @6 dFor example: Number 1 engine cowling; number 3 latch is not secure.
8 V$ a# \4 A1 s- p ~! ^: L& f 一号发动机整流罩的三号锁扣未扣紧。
; f/ i+ ]% W+ p4 ?* r* e) S, d5 D Number 1 engine cowling; number 3 latch has damaged hook. Replaced3 A# }5 w7 G0 g
number 3 latch with new part in accordance with AMM---. Operation check
+ y2 z1 W. ^& P Z& o2 p) kOK.0 y' @& R3 G4 `8 {; p. E
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,
- D+ ^6 M( d* C8 g+ N+ s操作检查正常。
4 |( Q) t/ [$ l; x% M/ J
' s3 c- ^" r k% e; N(45) inconsistent: 不均匀
- m; W) N# C" n0 ]& O+ i+ XNot in agreement, erratic* L! l4 z( G1 {. M# O9 ?
缺乏连续性。
- m6 c! Y3 z" k; \3 mFor example: Left wing-to-body fairing seal is inconsistent in relation to fuselage.9 ~8 z& F; w4 Y7 x0 B
左大翼-机身整流罩封严胶不均匀。& A: p, J" u: E
Re-sealed the left wing-to-body in accordance with standard practices and6 v" Y( U. t' g$ K4 b+ D
AMM---.: g7 I9 f: u q( t* k7 s2 P
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。/ L" [% r! e2 y
. j( |0 G- D0 ` ` s' k
(46) exposed cords: 见线* M) R# r- |% c7 d# B( ?
Visual tire cords.
: s9 b# N; {9 ]) C% x+ S轮胎编织线裸露。
* x' P* L+ w$ ^8 @For example: Number 3 tire has exposed cords.$ N D3 }4 |0 `: e1 w
三号轮胎见线。
! L Q% \* I* u2 O4 g; v( ] Replaced number 3 tire with exposed cords with serviceable wheel assembly in
8 @- {* b* I6 taccordance with AMM---. Pressure check normal.
9 }- ^$ H1 _7 M根据AMM—更换三号轮胎,检查压力正常。' J! H% v5 p1 ?- j) h* D: d
$ m5 e* j o- n(47) bald: 磨平
0 g- i5 a! z# P7 D) g6 uLacking a natural or usual covering.; P: w: E/ c1 g7 t# I7 y
轮胎表面排水槽由于磨损而消失。8 z+ F4 r. Y7 ~6 E
For example: Number 3 tire is bald and requires change prior to flight for no serviceable
8 ]) h2 X7 x& [: x+ I/ V( }- Jspare at scheduled flight sector out stations.2 f4 d$ H( f3 Y
三号轮胎磨平,因下一航站没有备件,请在航前更换。2 F: j }4 C J+ P* y* F- }. W
Replaced number 3 tire with serviceable wheel assembly in accordance with/ D$ c9 \4 l P. A# T6 Y: m
AMM---. Pressure check normal.- r0 ^0 ], I5 D
根据AMM—更换三号轮胎,检查其压力正常。/ R' u9 f, w/ G- J; c' [
" _. C! K! d ]& _% j8 C(48) insufficient-air-pressure: 气压不足
' U% G2 @/ H7 d& J; ] E: L$ I- RAir pressure does not meet manufacturers requirements.
, G; C/ \& v( T- h7 U* n# C S空气压力没有符合生产厂家的要求。
+ e3 k6 R5 r( J s% xFor example: Number 1 tire has insufficient-air-pressure.
* b8 Z3 z8 H2 L2 y6 d 一号主轮气压不足。
! |( Z3 A1 a7 H) p; U, e0 X; I Measuring air pressure revealed 5 psi. Air pressure required within limit as* E+ H9 R! q& K' y* n8 s& s& O9 ?
called out in AMM---. Serviced number 1 tire with Nitrogen as referenced in, q7 ?: K6 j% l/ M5 h
AMM---. OK for service.
# c: R% R" p# r" X测量一号主轮气压为5PSI,根据AMM—对一号主轮充氮气至要求。" ?) s* \ B9 [4 _4 _: Q2 w$ J% g
+ ~# u p/ |% g- ?
(49) expire: 过期
/ j: Y9 K) ?% l% K# a+ l& OTo come to an end or terminate.+ Q* a8 ~- ~# F, D7 `, o
超过时限、期限。
4 @; `$ D n, @" F3 H$ D/ RFor example: 2 each life vests located at L2 entry door flight crew station expired.
/ v3 o) i- s, C 位于左2号登记门机组人员位置的两个救生衣过期。$ C! b v! o+ \8 T
Replaced 2 each life vests located at L2 entry door flight crew station with0 I- G3 U5 r- c1 l& `% `5 U
serviceable life vests due at 9-2005 with reference to FAR 121.6.
2 V; @! I4 X. O0 x9 t 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
+ D% F0 a5 D1 D0 N$ e, z衣。9 k& ^: r! ]5 r, }3 w6 i2 x3 f
6 i5 }$ h; E# x5 B3 K
(50) illegible: 模糊" U: d' s R0 K* s5 c7 B
Not capable of being read or deciphered.6 U/ X2 P r. ?, w
难以辨认的,无法读出或解释的。
7 R1 |1 y1 I) U/ t8 wFor example: Left over wing external emergency exit hatch “EMERGENCY EXIT” placard
9 q6 J& p. L% H. E; ?# Ois illegible.% A1 I2 i' j7 U2 g0 O9 I
左翼上紧急出口舱盖处的“EMERGENCY EXIT”(紧急出口)的标牌模糊。! Y" L( `2 E7 X7 I
Removed and replaced left over wing external emergency exit hatch
2 Q, y$ n' G4 l, K) i' a6 \“EMERGENCY EXIT” placard with new in accordance with AMM---.+ C- `. N7 [9 o
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。2 s9 M7 n" d/ G; ~" ?4 o/ P
3 \0 `8 w; U" o) a P(51) damage: 破损/缺损
" {. K. R4 ~3 a# {Not useful or functional.* {5 D/ @- W- e+ z9 u, c6 i. }
不能用或者功能失效。
, l* O# u; x% ^' h1 c8 r- uFor example: Left wheel well landing gear door “NO-STEP” placard damaged.! U/ s2 C* ]3 c: _3 L
左起落架门的“NO-STEP”标牌缺损。
) e* [0 j" c0 `; \: z Replaced damaged placard “NO-STEP” at left wheel well landing gear door.& x A1 U( e2 o
更换左起落架门的“NO-STEP”标牌。3 o" z% S5 Y/ q5 w2 N2 |
& m& H2 L! b0 n" |. s4 P( \
(52) lifting: 翘起2 f5 `' g- g$ q$ J- L; r/ I9 z
To become raised, not intact.2 ]4 H# G0 t# e
没有紧固;活动 K; g, Z! f7 e! n' z
For example: R2 service door escape slide operation placard is lifting.# G$ L: v) E" G1 c7 x
右2号服务门逃生滑梯操作标牌翘起。
0 l; F( f% F5 }! i9 ]% e, b Removed lifting R2 service door escape slide operation placard, cleaned and
$ r* k6 w( c( ]% l& Hre-adhered to in accordance with AMM---.
1 N0 y2 ]) z( M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$ {: A+ b' g, Y8 ~% {; Y9 c
该标牌粘好。
2 g+ Q( P, Z9 l1 E5 I 4 q% @$ E; p& Y. j8 x& D6 {
(53) not properly sealed: 变形/密封不佳7 T3 j1 ]% E) M8 ?
Retaining package torn exposing contained contents.# o# O h: \: y8 j; L
固定的包装撕裂而露出里面的东西。5 P. [8 C: a# k/ j) ~ {' R' D) [5 g
For example: L1 entry door flight crew station portable breathing equipment not properly7 j8 S) Z3 F; j& w& o8 X( r1 X
sealed.' `5 {$ i/ V0 c' e
左一号登记门机组手提防烟设备变形。% P: ^& N! E5 n7 N. _3 D, j8 j" a
Replaced not properly sealed portable breathing equipment with serviceable+ [9 V9 g6 e* A) I) N3 ?. X
portable breathing equipment with reference to FAR 121.25 as required for) r0 S. f. A6 E9 a
dispatch . Tagged and routed unserviceable PBE to MSC to return to customer.* b4 [ D# Y3 \/ T
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& P" j7 q, I/ L0 C4 h
理。
* `" _% n4 C( Z
1 B% G; D6 R" L; a' p(54) not properly packed: (滑梯)散包
: T! ?( y# R) j0 O6 g- C8 NThe condition of a released slide.
7 s: G8 e; \4 `4 Y8 h滑梯包散开的状态。2 v2 H9 Q% _1 i- c
For example: With reference to reliability work order and task card 25-456-01, replace R2
1 Q4 I) E1 ]6 v# b6 Q2 h& Xservice door escape slide, provided escape slide from workshop S/N 4321 is not$ ]% u( w$ A) Z7 S, \! B
properly packed." n6 ?: p n1 r& ?9 `% [0 l
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
# C8 [3 p! L. r+ G车间提供的(S/N 4321)件已经散包。6 ]; k: c' _- q6 Z" {
Tagged and routed emergency escape slide S/N 4321 to MSC to be re-pack in
5 ]: y! A7 e$ c' H2 M- m4 sworkshop. Obtained serviceable emergency escape slide S/N 8765 and installed/ k$ } M' R$ L- N; u% d
at the R2 service door position with reference to task card 25-456-01 and8 m* q8 |4 k* A' B! T, }# O+ o
AMM---.
$ A; O( ~) `- O @. Q! ^. A# J2 F+ 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
* _: h, H# N; g) s1 @7 j" T# r25-456-01及AMM—在右2号服务门安装序号为8765的紧急滑梯。
; ^4 G$ L4 O* I/ s
$ S# l& ^& {1 i7 ^(55) dirty: 脏
5 W5 Y# \# f2 {+ nUnclean, soiled with dirt, grease etc./ _+ {; }4 w8 k9 T2 d- p7 q
不干净,有灰尘或油渍。4 X7 T; o) |" a; @( p7 s6 M
For example: Flight deck external window are dirty.
' y( ?$ l( Y! B. p0 v 驾驶舱外层玻璃脏。
0 w. M9 ^" z& r3 S Cleaned dirt from flight deck external window in accordance with AMM---.
) D! f1 d" O9 ?根据AMM—对驾驶舱外层玻璃进行清洁。
4 ]7 d% X0 Z9 R6 k: Q' k$ W6 V0 U ( z1 Y1 `/ H4 x0 j: Z0 S
(56) fracture: 断裂, L2 H# N' i3 m( F; \+ i
A break, rupture or crack.
: \" m( a, L1 P# W破碎,破裂或裂缝。1 |1 R" r, ~9 Z! j$ p+ p1 B
For example: Reference Gameco routine task card 53-004-12, NDT X-Ray inspection at right
! p0 R" ^% d' r0 _$ i" i; Hwing emergency exit hatch frame revealed 4 inch fracture at forward lower sill.
0 ~. L2 B& u% X: y9 t参考Gameco例行工卡53-004-12,NDT进行的X光检查中,发现右翼紧* `/ A7 c7 `: v; `2 ?
急出口舱门框前下角断裂(长约4英寸)。
2 u( |" f0 o* {+ DRepaired fracture with permanent repair in accordance with SRM---, attached9 w" S, L" d0 T& L9 ~1 h
Gameco engineering order 53078-4, and attached Boeing TELEX 53-0987-1. L0 H( v1 y3 H. |
Applied protective finish in accordance with reference to SRM---.
7 H8 ]2 \$ r9 }. O/ `) \根据SRM---,Gameco 工程指令53078-4及波音电传 53-0987-1,对断裂进
1 v: l5 f* m$ \. g. E7 e" ?行修理。参考SRM—进行保护漆层的恢复。3 s6 h) G! {% F1 {) K$ d$ n2 [
& v4 ?7 J# q$ y0 y" S(57) exceed-the-limit: 超标
3 J% s8 P. Z) oDoes not meet manufacturers specifications.# ? l. J t% W
超出生产厂家的技术标准或规格要求的范围。8 `& h q' p5 Y' ?* w& n
For example: Reference routine task card 32-098-01 landing gear functional check, nose9 O. q% G2 L* n* E
landing gear doors faired to fuselage skin exceed-the-limit during functional
D2 ]" ?9 v4 B# q1 ?( Scheck./ k2 h" `; e1 j2 z% m* O- K
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1 t) Q4 R2 E/ Q! d, [
架门与机身蒙皮间隙超标。
1 e5 s6 F1 D) z+ e$ \Adjusted push-pull control rods at nose landing gear doors to obtain proper
( O% l# }1 G5 K0 }- G9 ~8 |fairing to fuselage skin in accordance with AMM---. Clearance and functional
* ~0 ?: a( ?3 J: Q" o3 Y! s4 icheck good in accordance with routine task card 32-098-01.# X9 r. k8 T# x" `0 X
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
9 f, [4 f H- Q- z6 q进行功能测试,检查正常。 _4 g% W& K8 ~3 P+ }. L4 {# `
$ p1 C" v* J$ J& e/ [8 C3 S(58) backlash: 空行程/无效行程
( D, z. N. `* k4 cTo measure play resulting from loose connections between gears or other mechanical3 j1 ]/ Y! X% F& j
elements.
% n) p3 g: v1 x4 a) r/ E& 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。
v6 U( `- f: P4 ? \# |# ?For example: Horizontal stabilizer jackscrew clutch failed backlash test with reference to
9 c' @9 U S, X: X" ~& D$ H; k, ~routine task-card 27-0345-01.
( K: b" Z" W( O0 p% o9 S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。; D7 y; `% S3 ^/ r( e
Removed horizontal stabilizer jackscrew clutch. Detailed inspection revealed! D# {7 H4 ]$ J( P( c
worn clutch plates. Tagged and routed unserviceable clutch unit to MSC for; M, I* m+ |6 a1 M6 ~, D5 Z3 {/ L
return to customer. Installed serviceable horizontal stabilizer jackscrew clutch: |. j& i' R2 c; y9 Q7 E
in accordance with AMM---backlash and operational check good.
2 ]% r% h' i1 R; N- h" m; [ 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 i x- |4 P8 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。
& r6 ^: e. X$ S+ ~ | 0 Q2 J2 x0 b \+ u6 r1 B
(59) block: 卡阻/阻塞
* j& I5 K3 U+ {+ B0 jThe act of obstructing.
1 K3 |9 N9 j* u! J G7 i' J1 U通道堵塞:运动部件的动作不顺畅。& |% u. l& \. v* d
For example: Forward cargo compartment door forward actuator is blocked when opening
, U$ K$ F$ {! V( T: C; _$ g. Ethe door.
3 I; X$ u5 Z( s: Q前货舱门在打开时有卡阻。
B( ]3 I$ ]$ I' Z# H& n2 Z, ^Detailed inspection revealed there was a dent on the actuator rod. Replaced the; w" v9 M0 \. K. V: i& h
inoperative actuator in accordance with AMM---. Operational and functional, l2 k" A7 c3 X) E2 a) g
check good.
; o9 |( V- k$ s 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,2 _# X0 ]% {3 A5 E/ e& a/ w) w, G
操作检查正常。
6 n+ g( E V: n; ?) L / D0 |1 h8 i+ V7 X0 y; c
(60) bulge: 鼓起
2 W/ G/ N/ }" U) z3 | J) eAn outward curve or swelling.
6 X$ c) `# R# y4 {% |( O向外凸起。
3 T- Z8 j1 } I$ kFor example: Forward cabin lavatory floor panel is bulging.& C7 [; X: K. S$ Y1 K8 N5 p" h
前货舱厕所过道地板鼓起。. Z( c- ^3 ]* G1 c e. {3 s7 |" X
Removed forward cabin lavatory floor panel, no defects noted. Re-adhered! O( K: A. t' y, X; \. k. s/ X
forward cabin lavatory floor panel and eliminated bulging in accordance with
+ T8 ]9 q* W! X/ Ystandard practices and AMM---.
) ]; j& \$ E9 o$ g3 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
; O, O% R Z- Z1 I; KAMM—重新粘接该地板。# i1 j* @; I- {* \5 r
2 j. k7 R) \" F' d9 i- f* J
(61) contaminate: 污染( ?& l1 s$ ~. b+ o2 p- O: `* m
Impure mixture.
& |7 O6 S! p' K& \% w2 t有不纯的杂质或异物。# n9 `0 i( s5 D2 Z! D# ^5 `+ B
For example: Fuel sample reveals positive contamination of microorganism growth.
' S8 J5 k; x* q+ D# X/ M( N. g. E 燃油样品检查发现有微生物污染。
' A) N' x" M& C1 P6 L Treated fuel tank with biocides with reference to attached Engineering Order6 ~( k$ z+ k: E* Z2 o. B! p
G2009619.
! k9 }& o) b5 \! Y5 k; m1 b根据工程指令G2009619,使用杀菌剂对油箱进行杀菌处理。3 ^& L9 y/ {6 h
) N/ m- I- `% v% ~+ ^! \9 ~3 B
(62) disagree: 不一致9 i! {0 ]- m! H0 o# K# p
Fail to be in agreement.
& r/ z& y$ Q5 V9 F: U( p7 r$ F对应关系不正确。+ q$ V `7 _' |% o$ k! p
For example: Flap control lever disagrees with flap indication gauge through all detents.! ~- Z# b/ ]: q: ^9 F. q
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。0 `0 G1 J3 |% y3 f4 g; G) a+ W
Adjusted left and right wing flap indicators in accordance with AMM---.
, v( e! L* p' ]; t8 |5 ~. hOperational check good through all detents./ `# s; k \6 f. K
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
m* |/ e* x& r% X4 j表指示一致。
' H" G% N% B/ v, J3 _% E( m) z2 f' V
) V- m5 A. f* N(63) discharge: (电池/气瓶)被释放/ s& x0 I, h9 X2 L8 r
To relieve retained contents to an empty state.' l* Q) b4 \+ R8 {& M3 j' L1 `6 M S
放出;腾空
9 j2 f0 B0 `* C3 v' IFor example: R2 service door assist accumulator discharged." w$ b5 n Q/ ^. l* A3 P
右二号服务门助推气瓶被释放。
$ x: K% l+ H. l8 I: X1 x/ j* f R2 service door assist accumulator detailed inspection revealed damaged
# d( E( q8 W r* u) Jpressure gauge. Replaced pressure gauge, serviced with dry air as called out in
; l* q( s; J! g. ^/ kAMM---leak check good." Y9 H% T, W2 n
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
5 Y7 t. j; O. e( d8 y; r压力表,对助推气瓶进行勤务,渗漏检查正常。
8 A' ~% o$ {2 F/ @: P: g $ v2 ^2 C8 D: h6 }% E1 s& P9 h8 q
(64) dislocated: 装错
/ e$ n; ]2 D) mNot in proper relationship with joining part.
5 S2 F- z. s" r' w' t9 j零部件没有安装在正确的位置。
) @- Y) g2 q1 H7 z3 q$ j rFor example: Forward cargo door pressure seal is dislocated from retaining track along after
' U' z0 E& Q* _; Zand bottom section of door.0 @! T3 n2 I6 B! i/ X
前货舱门后底部固定轨道的压力封严条装错。
% g, S i1 Q7 ^0 J% H0 G. U4 I- aDetailed inspection revealed pressure seal retainer damaged along after and
" X% v; j1 N! ]0 bbottom section of forward cargo door. Replaced affected section of pressure# ` w9 H/ Y: F' A! z, o
seal retainer and reinstalled original pressure seal in accordance with AMM---.8 n# p" m7 h- s- Z) E5 ~
Operational and pressure check good.
( F7 W8 u- i1 ]3 N" V# S) G4 z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
+ W4 B9 w* r0 H! t. ~) `, O+ j该安装槽并重装封严条,操作并增压检查正常。5 Q9 R: M! R. Q$ \( G( ?* E
/ p% V7 V& w. A$ j9 | s. R
(65) fail: 失效8 t- w- b% ?. O8 ^! k8 s
Note: must have detailed description of failure.9 E" [- y2 k; z3 q
注:如用此术语,必须给出故障失效的具体描述。6 Y5 c* b0 I5 k- _: ?0 O" k/ g( X
To perform ineffectively or inadequately.
/ R0 B9 B' \3 b' G5 ]不能执行或不能完全执行原有的功能。0 ~# _$ J5 A9 f2 W
For example: 13F seat actuator failed to adjust.# ~( m9 C6 W! ^
第13排F座椅作动筒失效,不能调节。
% J" O4 o. R5 T8 W Replaced 13F seat actuator with new part, functional check good.
) c$ M4 h$ |4 f3 A' n4 g 根据AMM—更换第13排F座椅作动筒,功能测试正常。5 h( C- t& n! g3 d7 o0 I& U$ u
' V. f H/ [+ a9 i9 |6 U* x" v(66) fluctuate: 摆动
! @* e2 t6 ?$ _4 n) dTo continually change or vary in an irregular way.
+ e( X" i, X9 c) y: [1 W无规律连续的起伏不定,变化。
# y, t1 {2 J" c6 Z3 j( c0 Z o6 XFor example: During engine run the number 1 engine oil pressure gauge fluctuates.# w0 f2 N& s& f4 O/ ~* I5 v
试车时,一号发动机滑油压力表指示摆动。! D& K4 e- c% d2 x; w
Replaced the number 1 engine oil pressure gauge in accordance with AMM---. Carried out engine run, oil pressure gauge normal.4 E- [5 `1 `2 d( ~
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。
( l* r( k% @' A* \9 ~
' [; S3 [* U! }(67) flutter: 抖动" `: R) {! p+ @5 k" n! P2 \* x6 @
A rapid waiving or flapping movement.8 Z2 j: a0 e6 ~& ?, A
快速的摇动或者上下振动。! ]" {1 I! N) B1 X- R7 r
For example: Pilot report on flight logbook page 908701 fluttering sound from left side of( Z/ P5 W" @2 A" P c
airplane during descend beginning at 11000 feat.* ?% m4 C0 y* L# F, \9 W
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, Y$ J \, ?& C B
侧有抖动的声音。$ b I% @/ p9 y% n
Investigated fluttering sound from left side of aircraft as squawked on page! K8 r2 M& B7 e$ E0 N
908701 of flight logbook. Found number 3 flight spoiler actuator leaking.
/ m' m1 f0 v* p" N( S! W# P& D Replaced number 3 flight spoiler actuator in accordance with AMM---
% ]( I4 L) i% A" O2 T1 yoperational, leak, functional check good. Flight crew briefed prior to flight.
) {( @/ E) \+ D+ \/ y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。
# ?% A- j3 ~8 V& }6 C6 Y' v * b+ K8 n! X+ U% o* j
(68) insufficient: 不够/不足# D" Y4 Y7 B8 S7 Y3 r m# g
Not sufficient, inadequate./ f; g% T7 @3 y
达不到所要求的数量,数目。
/ P9 d8 E0 {5 R* I' W5 ZFor example: Left main landing gear alternate extension control cable has insufficient
+ n/ n6 S9 W7 Dlubrication.
) J7 W5 h2 b! l0 B* [3 z" x. f左主起落架备用控制钢索润滑不足。2 D' O: l+ Z3 f: V( w# Z6 Y
Lubricated left main landing gear alternate extension control cable with" B4 t/ g H9 N3 q
Aero-shell 12 grease as called out in AMM---.
. T H+ j5 D U根据AMM—用Aero-shell 12润滑左主起落架。
* |+ w* q2 @9 j1 b; e: a' k& t
) b& X6 d; c6 M" s+ I(69) inoperative: 不工作+ z% n* O, h) d8 b0 {8 Y) g
Not working.3 ~( L2 X P* Q3 ]% a: A6 D
不能正常的发挥功能,作用。
: l& P+ K7 v; zFor example: Forward electronics bay door indication light in flight deck is inoperative., u$ ^' y3 {8 m9 b2 ~
驾驶舱前电子舱门指示灯不工作。
& H! w" @' r% T Detailed inspection revealed 2 each bulb filaments fused in electronics bay
' H6 @( H* M* Y2 @/ Ydoor indicator. Replaced 2 each bulbs in accordance with AMM--- operational) x) }1 p+ e5 J% T
check good.! A6 B+ G+ f& C5 w9 o2 Y* J
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: _) e9 T" l; l k1 ~5 V
这两个灯泡,操作检查正常。
$ m/ {0 X3 k9 h. _
8 p* K a# C. y; V. q3 d5 C1 A' X(70) (not) illuminate: (不)亮
* V' F, M3 S- f: KNot brighten with light.! j, E' g7 I. C E+ T4 f* Y
不照明,不发光。
% x* l; l2 H. X) C' m% |7 z0 qFor example: Passenger reading light at cabin rows 12AB, 14C, and 17AD, will not
/ j9 s! ?1 y3 F" u) P5 t3 V- ]illuminate.) {8 `/ a! V1 M
12AB, 14C, 和 17AD座位的旅客阅读灯不亮。) j& M+ e, q4 Z& A/ b1 _* w
Replaced passenger reading light bulbs at cabin rows 12AB, 14C, and 17AD in$ G0 `: ?+ ?$ Q& }3 Y5 C, j- c! f
accordance with AMM--- operational check good./ y6 R! O. a3 V! i2 r
根据AMM—更换12AB, 14C, 和 17AD座位的旅客阅读灯,操作检查正$ s& n& H3 b8 H G
常。; D& ]% w0 r U5 n' p
! F! |2 g' X$ [* R: X' o
(71) interfere: 干扰2 [' y( R. ]+ I( E
To come between so as to be a hindrance or an obstacle.
) V1 H0 H4 v% l- w5 C妨碍无线电设备正常接受信号的电磁振荡。( `0 S3 @7 @1 g' l4 u! F
For example: Functional check L VHF radio revealed interference static and abnormal noise./ B5 P5 x& ?$ H; z9 N" B! m
功能检查左VHF设备发现其工作有干扰及静电噪音。
- x! l+ X* b% F" p, y Replaced L VHF radio in accordance with AMM--- and tagged and routed the* I, s: |2 a# s% t/ S# q7 V9 z1 Z
removed part to MSC.5 v/ `" X' d. p0 n a1 N7 d
根据AMM—更换左VHF设备,旧件挂牌送航材。5 \/ ]- i* ^" j8 e
( s- U. [" W" {# V4 g" z(72) kink: 扭结/缠结
7 q2 C9 Z. f7 z1 a+ @$ UA tight curl or sharp twist.
O) q0 C0 U& X(钢索,条壮物)缠绕在一起。
: R: z9 Z% W D4 |# l1 j7 jFor example: Right wing inboard flap control cable at control mechanism located in after
- h @2 p7 E7 Fright wheel well is incorrectly routed and kinked.
0 i' U/ V4 X7 V9 I R/ z9 x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。$ {6 Q# i, A1 A0 m( l
Replaced with new flap control cable from Body Station 760 to flap control d: Q# x* v) t8 e/ t1 B 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., F! A2 Y/ F) C9 E9 t. g( S
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。
/ Z' l# z( o& b
[0 J$ e& V6 j- g6 n(73) misrouted: 走向错误
3 q! D2 @0 [% d; ^- J# W0 sNot properly aligned through a course of travel.; O0 o1 M# }# B \
在行程中没有正确对折。; @( y5 \4 A5 e; p& U
For example: Left main landing gear manual extension cable is misrouted through pulley attached bulkhead in the left wheel well.
; T7 z1 D' S2 X6 ^2 R: b 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/ e4 y- w; X. ~! ~+ a5 s* d5 p
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.8 G/ l# j0 G4 e E1 P
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
3 c* ]6 O2 {' K5 [) P该滑轮重新安装,功能测试,检查正常。9 f+ D, x5 F: R8 c
4 v1 k8 B" G9 z8 N5 s6 a(74) not installed: 漏装) R6 c" M6 ~# \, o. ^" R+ a. k8 ?+ K4 I: A
Missing.
. ~: H! K# Q/ w' J根据要求本应安装的零部件未安装。" v& ?0 O+ p" l- a* O$ o
For example: Life vests not installed at L1 entry door flight crew station.& P- l4 l7 R! r
L1登机门飞行机组位置救生衣未安装。
% F6 Y4 D W" E, E# _/ B# Y Installed required life vests at L1 entry door flight crew station.
3 ]3 `$ L. z; P5 ?& b 在L1登机门飞行机组位置安装救生衣。
( A+ S# F: v" H* y7 j 0 M; P7 U7 S' _4 [* N# p9 s
(75) rubbing: 相磨( b* w- K0 q. H# Y4 y ?
Making contact with an unrelated surface A" }" p `& L' T5 w
相对运动的两个物体表面因接触而导致磨损。4 T+ a7 e+ W) q% @$ u" y
For example: Wire harness for cabin PSU’s running through floor beam at body station 360
+ V: ^! @, z- D5 R+ ]" M, z9 C) D0 cand wbl 21.52 is rubbing against floor beam cutout.
, O/ T+ s0 i8 L( T2 R4 t' N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0 `9 T) H- f- r' R
板梁时与地板梁切口相磨。+ r0 ^8 x6 Q/ u8 J
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---.
. i" Z& A0 u$ T4 c3 r9 G 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,$ x$ a" H+ M' ^0 j; P
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
+ e4 |) h8 O% O8 v9 [7 N处地板梁切口相磨的情况。
7 A; M' R ~, I8 u4 O
! j$ U; D2 }7 h& I% W$ p* ](76) un-lubricated: 干涩/缺乏润滑" F& T8 T* k5 e+ D( X. B: b3 ~
Without lubrication resulting in friction, heat and wear.) O0 s0 ?. F5 g! I/ s
没有润滑而导致相磨,发热和磨损。
, W9 {7 E& d2 x. }1 SFor example: After aircraft wash, all 3 landing gears were found un-lubricated.$ U) i: N/ Q+ W D
洗飞机后,发现三个起落架都缺乏润滑。9 Q3 q& d. P" S
Lubricated all 3 landing gears with aero shell 17 grease with reference to
& o; J, O( w, \0 |, Y3 h" bAMM---.1 |3 @8 T* j/ ~) b/ H: Q9 t- {
根据AMM—润滑三个起落架。
5 [, f* q9 L f; B- u1 \; v0 {
5 V+ \* W$ \$ |2 ?) D- j( l(77) will-not-reset: 不能复位
, }3 u4 j5 n$ v& z7 }Will not return to its operating(original) position.. k+ s0 x, n% s0 s/ S6 ~) \
不能回到原来的位置。# ] }/ h0 I3 d% a/ Z1 q1 F2 z
For example: APU circuit breaker will-not-reset.. @8 i8 q/ v4 ?0 D
APU跳开关不能复位。) m$ d. R' C# w- O+ Z# r4 I
Detailed inspection found APU circuit breaker faulty. Replaced APU circuit
, w" X& h1 t" G. J- N* A" B. _breaker in accordance with AMM---.Operational check good.
V; n8 P. x" ^; Z3 o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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