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  
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维修术语3 R) w! T2 c9 o( _- R2 Z; h& ?
4 f3 [: V* O- Q" v* L2 r
. l# L. a( H/ T3 w: G4 C; R(灯)不亮 not come on 不可用 not serviceable
$ a" |( @* z& N& q7 K, C, N“工”型 type I 不锈钢 stainless steel
9 |4 _4 ?: N8 G4 d# ^4 `APU 舱门 APU bay door 部件 part. L2 k4 T0 I3 b5 t
T 型件 Tee extrusion 材料 material
@2 q& p- a- r+ X n阿罗钉 alodine 参考 reference
7 }0 V: } s. b" i安全带 safety belt 餐板 feed panel
9 R; D' P5 x& y5 D安装 install 餐车 diner
! F9 z8 Z& o, M2 S, R安装座 attach fitting 操纵 control
/ H! m9 ~5 ^3 t5 ]按钮 button 操作检查 operational2 }7 X: O! G3 l! Z; s% J: L& c& h
按需要 as required 槽 spout* B0 N, T& m; i# G0 v. t2 s
凹槽 notch 侧板 sidewall/ E3 s$ u8 [& D( T/ T
凹坑 dent 测量 measure
: A% ^8 v# x0 [- `: Y2 z$ r4 j! D; N3 s把手,扶手 handle 测试 test
! u8 p# v$ W( ~- r' L5 q6 G包皮 cowl 插钉 pin
; f( X3 T3 b) {保护层 coating 插头 plug
) g- q D4 ?& T3 b2 I! W5 Z) T% |保险 fuse 插座 receptacle" v, u+ S" M) u# D2 l: s9 d
报废 discard 拆下 remove
2 D- M% }, R+ S+ r报告工程师 report to engineer 长桁 stringer
# K! ]/ ^) O4 ~# q3 W' j$ q杯子 cup 超标 out of limit
8 N7 h3 x6 t- \/ i* ?1 u比率转换器 ratio changer 超标 exceed the limit; R2 ]# L7 A" V8 N& p, A' Q
壁橱 closet 超过 exceed! ]% R" T R) G- h9 v% m7 o+ T% E
边缘 edge 超控手柄 override handle: K" P+ ]& c5 S$ E8 z
便于检查 easily to inspect 彻底修理 drastically repair
# b; |: @8 Z5 h0 A' T+ Z$ z: J. G变形 deformation (n) 陈旧的 worn
: i, g5 a/ M4 Y3 F$ c! e6 U/ M3 G变形 deform (v) 衬板 liner
. J5 O; I0 b$ ^9 O! I变压器 transformer 衬套 bush3 S: r; ], A6 M& j- e
标牌 placard 成型 shaping
; |' `1 W; @0 n标识 sign 乘务员 attendant) d3 a! Z) U: L2 @% q& @4 C& o# o7 q9 }5 b
标志 instruction 尺寸 size
$ e9 l7 x* l" i) l6 h玻璃 pane 充足的 sufficient
$ M! x: C' ~4 ^$ L3 l玻璃纤维 fiberglass 冲水按钮 flush button$ _1 j) F: I$ C& z6 p& ]
补片 patch 冲洗 flush
' t7 k2 F* W* Y4 h; J0 O8 h补片 filler 冲压 ram
. ^! l% q6 F4 O7 K; |冲压空气 ram air 低压压气机 LP-compressor
6 H: B8 S/ s( p& k抽油 defuel 底部 bottom
% i- l }1 ?) ]7 T, S出口 exit 底盘 base
+ g E/ ~- X8 ^4 E r1 d8 ]: d: U除腐区 reworked area 底漆 primer
4 J* q& D4 ^& b6 p* A5 v6 a) K: E厨房 galley 底座(结构件) mounting
; T) R$ l' f2 u3 H厨房烤箱 galley oven 底座(螺母) plate
9 g! ^- b% `2 K+ `" c3 {7 l储物柜 closet 底座(天线) base
. A, W/ y6 H" @' V. P" d( n1 S% P) P处理 treatment 地板梁 floor beam( O6 h6 i' k2 z! \. x& R- W
处理 dispose 地面 ground# `3 g/ ~6 `- l* D
传感器 sensor 地毯 carpet+ s9 X( ^* L. f) T) d
传输 transmission 第二层 two layer
+ Q6 S: u# m. M垂直的 vertical 点火电嘴 ignitor; f4 E7 ?( K! L
存放处 location 电路 circuit! q9 W# j. @) n8 T. Y+ _0 y
错位 migration 电门,开关 switch; p8 g) P. @: h8 P# B0 |8 S2 f
搭地线 jumper 电气 electrical! @9 L/ p- x" V# t" _$ {4 _* X0 t
搭接处 interface 电气接地 ELEC bonding$ t S0 z9 L4 {1 `7 M/ o
搭接片 splice strap 电源通电 power4 h; d6 K. r- I/ L
搭接片 splice 电子 avionics
k8 l) s9 g5 W% U1 @0 b, I打磨 blend out 电子架 E rack
1 @; i- s+ p2 K; F% m0 N4 x* u打磨片 blent disk 电子架 shelf
* V$ T( x/ q4 y: l% z打止裂孔 drill stop hole 电阻 elec resistance
0 e9 G2 r; T8 S" C7 C! B大翼 wing 电阻 resistance
! w& w: F6 O( f/ ~- h+ @大于 more than 垫片 washer
% X3 s" z- T m/ p单向活门 check-valve 吊仓 nacelle
/ F- r' L) O! B弹簧片 spring seal 吊点 mount cone7 \. C5 I2 }0 e6 N
挡块 retainer 调节 adjust
3 i S" f A. l9 P2 K1 n' B+ H挡雨板 fender 调整片 tap
, E( L; x. O9 X6 B* L. j5 O; v* z. i导线 wire 顶板 ceiling
% D f" M& O/ W: S灯 light 顶部 top* `7 v2 n- c* x5 y# C1 y8 d# ^
灯泡 bulb 顶部 overhead
, f& @4 G- m3 a* y* `灯泡 lamp 定中弹簧 decentering spring
' d1 C2 ?' R! O+ |' q灯箱 light case 丢失 miss
# }, E9 m9 R9 q2 `9 o灯罩 light lens 堵盖 plug8 ]1 X. T7 l; X. c+ @
登机门 ENTRY DOOR 堵塞 clog
4 S9 r/ ]! {4 |: G# |4 |端头 ending 腐蚀 corrosion
: v" F$ l4 h! z6 \段 section 腐蚀 corrode
, U% G) C: k! D9 _断 break 附件(大) accessary
) N/ r3 `3 m$ U u r$ w- e" U断开 disconnect 附件(小) attach
1 `' P% b. S$ r: ~1 R# p断裂 fracture 附近 adjacent to7 V1 X! V% m* a% i
断裂的 broken 复合 complex
- a8 Q# B! q) e2 r+ Q9 ?/ Q0 r断丝,磨损 fray 副驾驶员做椅 first offcer's seat
& m; b$ G0 A4 E# u2 e6 r7 I8 y锻件 forged part 副翼 aileron5 p8 e9 q2 A+ n" S7 l- s$ A1 C
多处 numerous 改装 modification
) ~4 E% r; N; X% G4 r' `4 ?发动机 engine 盖 cap
! p8 C% u) T. h7 t翻新 overhaul 杆 rod
* V- J# U6 m! a5 z3 V8 B, s. @反光镜 mirror 钢丝 steel
- @' [3 x4 v$ z2 G; o方向舵 rudder 钢索 cable
, Q+ A: O6 p0 e s* U& `; [* K) d防冰管 anti-ice duck 割除 cut out- Z y V* D9 X# ^# }6 ~) [& N
防腐 corrosion-inhibition 割断,割下 cut off
( v3 K+ y0 |( [$ r防静电 static-free 隔板 clapboard,partition
0 H- N- M! d) q Z# i# K8 Z防磨条 wear strip 隔框 bulkhead
' Q7 ?& J2 M Y& k5 d; ]防滞 antiskid 隔热棉 insulation-blanket
J: P6 d' g& ~1 ^/ B防撞灯 anti-collision light 隔栅 grille; k; n; o- ~+ b! |0 ~; G: l
放 extend 各有 each has, O4 T$ p! L& Z
放电刷 discharger 根据方案 in according to disposition! r; |# g9 D" D7 J& E6 d. z
分层 delamination 根据监控指令单 condition monitor order…. T. e- O. }& d- j' ^
风层,脱胶 delaminate 更换 replace. E7 P; t3 |1 z- U' ~7 n
风挡 windshield 工程师 engineer
4 r/ f: V) t( E6 n2 q/ x3 D风挡玻璃 windscreen 功能测试 functional test& x% }: k! z6 c, E: S+ \' d+ O
风扇整流罩 FAN COWL 功能检查 functional 5 K+ o- M* x a, Z) g1 F# h
风蚀 erode 供应系统 feed system, r* B/ s* Y2 S% E6 N$ x
封严 sealing 供油管 OIL TUBE% M7 ~* r) _& d
封严条 seal 鼓轮 drum& v* C0 O5 {# _3 H9 W% ?5 l
蜂窝芯 stagger core 鼓起 bulge9 {( F" }9 w( i
扶手 armrest 固定 secure
6 ]5 D/ o: s2 h2 [' P扶手盖板 armrest cover 固化 harden% G& U1 ]9 n; p: ]! v; X A f: N* R
辅助滑轨 assistant track 固化剂 hardener
3 z3 h |- p$ U3 x1 u故障 fault 划痕,划伤 scratch2 h5 N9 l# w5 Q9 j% I6 A
刮伤 scratch 划窝 countersink
: w, `" q; Q6 k3 [) C% M挂 attach 环氧树脂 epoxy resin
& w* R4 s/ r0 w8 r& G; m, u挂钩 hook 恢复 restore* {' }7 H; f( ^) ?: {+ Q
挂上 hang up 活动窗 slide window0 z& [6 t" V$ ~6 b4 X- V" n: z
关上 close 活门 valve
! M( Y5 y9 N6 b4 }8 G8 z" t观察镜 view glass 货舱 cargo compt- F, u ^& B' f- `- T3 V
观察镜 viewer 机构 mechanism
. q' ~8 c- r8 w" m观察员 observer 机身 fuselage }; P4 G6 l, X, W$ y; u
观察员 observer 迹象 mark
2 [1 W7 t. m+ m9 D7 t光滑地 smoothly 加强 doubling2 W p, l$ ]! V
滚轮 roller 加强件 stiffener; n# O' u. T4 M0 e. Y' f" F
过道 aisle 加强块 doubler' J8 f0 ]2 H- r5 P
过期 expire 加强肋 intercostal
- c. n: D$ y1 ^) G9 |过热传感元件 overheat sensing element 加强修理 reinforcement
- F5 U& F: h4 l$ g6 L海绵 sponge 加温导线 hot wire9 B& N# f/ M$ R# F
焊接 weld 加油面板 refuel panel- A# p- m6 Q+ D) S0 N! v+ i
焊条 welding rod 加油站面板 fueling station panel
4 A) s3 s" |) u% @恒速传动装置 CSD case 夹子 clip- B+ m8 n' C) ]; A2 o
横梁 latitudinal beam 驾驶舱 cockpit
; }: X2 B! I; I" g横向 lateral 间隙 gap
+ i& J5 r9 s7 h) B, Q3 V后端 rear 减速板 speedbreak
+ x# G! a) O: h5 |/ Q0 k, D后缘 T/E 减压器 reducer! v& \- U7 @( j. X" }
厚度 thickness 减震器 shock absorber
' t# g) k4 a( T! \) z2 q. X$ a" a呼叫灯 call light 减震支柱 shock strut: q/ ^& G3 |( s7 v7 ~# T
护板 protect strap 检查 inspect
# T" x6 |, C8 {! R+ J护目镜 goggles 检修门 access door
- z' J$ v k8 K) v5 m6 [护罩 shroud 胶 sealant+ U" g. m v! C/ g: ~8 X9 k
花键 spline 胶带 tape2 a) {: S8 U) @4 v! m* I: R& f
滑轨 track 胶垫 mat
1 }7 A7 S- F( Y; E滑轮 pulley 胶垫圈 rubber washer( x7 V# |5 J& p- M' ~, i
滑丝 cross thread 胶套 rubber
9 n5 ]% @% q2 b0 Y9 T; e滑梯罩 slide cover 胶纸 tape" N; g! k' B- Q. ~: R/ ~1 I i
滑油量 oil lever 角材 angler. F- C6 q) u% m+ g1 Y. Z- K
角型件 angle shape 喇叭 megaphone
4 V$ Q/ T! M T! y) x! p. X脚登板 pedal 拦网 block
3 o1 Y' |' j" u' {2 b铰链 hinge 牢固性 security
# }$ \; f8 `3 n y9 `0 f$ e7 o7 c接地点 ground point 老化 aged. R8 }% h5 Y6 P9 v, N9 w# |4 A' H) N
接耳 lug 老化,退化 deteriorate! S( [# {% U* w {! n6 R
接通,提供 supply 雷达罩 radome* c- k0 b" e# H; a( _( H
接头 fitting 肋 rib
/ w3 m; e' O# l7 s# z8 S# h接线管 splice 离合器 clutch
; v9 H2 ^# ?# J- @! p接线片 terminal lug 立柱 pole' n% t* C4 E' v9 S( f" B
结构的 structural 例行 routine
3 m" K. L; m I$ z2 o金属屑 metal particle 连杆 link" ]$ ~# x8 T' |: b
襟翼 flap 连接 attatch3 D/ H2 B& r* A! F
紧固件 fastener 连接板 attach plate1 G1 {& [" D/ L' ~- I
紧急出口 exit 连接口 coupling
9 M( }6 q/ i g' i进气道 inlet duct 连接销 lockwire& Z7 z# U5 G. v/ M
进气口 inlet port 联锁 interlock
( {5 V" ^, n6 t% C0 a径向驱动轴 radial drive shaft 裂 crack
3 L. x7 U9 ?; K* R( D/ n& T: W静电,静压 static 另一个 another
) x7 T/ R& }' S6 J& ^8 j1 n救生衣 lifevest 龙骨梁 keel beam, a# `: f# C! j3 N' G) e
咖啡壶 coffee maker 滤网 filter7 C O7 p8 X# I: B) V7 K; z
卡箍 clamp 铝箔 foil
. |7 x4 S% G1 N' d8 T卡环 collar 轮舱 wheel well
: I0 @$ m1 K* \& I开口销 cotter pin 轮子 wheel
. o$ K! i# Y: N+ V0 ~1 B0 D" [靠背 back panel 逻辑 logic
1 n8 P8 i8 R: `7 K5 X( K; n3 F壳体 case 螺钉 screw & L. S5 W% X* z# P( }8 c( h
可用 available 螺钉孔 screw hole' e! m) M8 s4 k. X
客舱 cabin 螺杆 bolt
" i0 ^/ O! `, U0 {, S空气循环隔栅 air return grille 螺帽 nut; z& D( \; f: l% Z
口 port 螺套 insert
: B Y# K; L4 j- n7 J: Z块 piece 螺纹压伤 cross threading+ w9 n3 j( }; x& r! f
框架 frame 马桶 toilet" v3 p" y: D0 J* y1 K2 i
垃圾箱 dustbin 慢车 IDLE" z0 D3 D3 U4 W* R' j! j
拉紧 pull 毛刺 bur
$ H: O, R) G1 g4 f毛胚件 rough 破损 damage
* G$ I, `- [2 E3 O) M: u铆钉 rivet 漆层 coating
4 G: v/ t4 _) q0 v; ^: P8 b! r V& W7 o门槛 sill 其中之一 one of
1 d; L, N; ]1 M* n. U门框 door frame 启动活门 start valve! H8 I+ W5 U2 s6 g
蒙皮 skin 启动机 starter
/ w6 p7 S9 B0 d+ v( d' h& W4 i9 y% A密度 density 起落架 landing gear t) a7 F, A3 T% ?2 T% Q
密度计 densitometer 气瓶 cylinder
6 p+ @3 M) _6 A6 e$ V- M" ~" D面板 panel 千层片 shim
2 Z0 k1 {+ b1 x! ^5 M# N1 W$ l面漆 enamel 前厕所 fwd lav
9 | y6 z# i. e O模糊 blur 前缘 L/E3 ^& L# ?6 h0 A0 n5 n' y
模糊不清 obscure 腔体 cavity* a% w* z% w8 X: \- k
磨损 wear 墙纸 wallpaper
% H! Z, I1 ] ]) H目视 visual 切口 cutout. \4 K; Q0 }' G/ P' E
内侧 interior board 勤务面板 service panel5 A; a. \/ a8 g2 ? a- P
内层 inner 轻度 light% M" g5 G( p; o& d
尼龙搭扣 nylon fastener 轻微 slight8 x" w" B* h" n/ I; M
尼龙扣 nylon hook 清洁 clean
! c" U' K/ P: U! [" Q9 P拧紧 tighten 清洁剂 cleaner0 K4 J% q6 D8 p& \: Z# R
扭力管 torsional tube 区域 zone
* I9 t7 M1 r8 h" T7 W b扭曲 kink 曲柄 crank6 U4 o: o( I7 y4 a b: R
排 row 去除深度 remove depth) R U; m1 z) T! m
排放 drain 去毛刺 deburr+ ^$ f" X% }) v) Q% r8 f
排水槽 gutter 缺口 nick6 a- l6 R7 o. g' V* R% u+ n
排水管 drain tube 群边 skirt edge! ]! u2 h( [0 V0 X- Y, N7 _* |
配平 trim 燃油 fuel* L4 m1 v( X& L0 [! f0 |% r6 ]6 u
喷漆 paint 燃油泵 fuel pump
2 u. x" C. A3 h9 {3 S% R9 F2 }喷砂 sand blast 扰流板 spoiler1 f4 |4 O) V/ c# l/ D q5 j
皮带,片 strap 热水器 water boiler# v; E' g) I0 f* Q1 t# I) h, U# y
皮托管 pitot 人工行程限制 manual travel limit$ _) ~/ J; K, S" S* y: _
偏航阻尼器 yaw damper 日光灯 daylight lamp6 K9 x0 {5 a) p0 L" b" D
平衡机构 equalizer 软管,软护套 hose- `$ Q$ l0 E0 @$ r# R X+ X0 W
平滑的,使平滑 smooth 润滑剂 lubricant
9 f1 |5 d( }4 x5 S9 n5 n平行 balance 三段 three section$ ^# L' C7 M- u2 b8 S
散装 bulk 逃离滑梯 escape slide) l; Y- e% ~' u1 {. y4 K
刹车 brake 天花板 ceiling# v: W. O. y7 i- X, C. v$ x% S' w
上表面 upper surface 天线 antenna; r2 h2 N. A: u( B9 X
上述 above 填补 fill7 p" x* W3 b/ P5 s) @1 E
深度 depth 跳开关 breaker
2 O* I% z1 q- h1 N' y1 A$ ~( y8 ]渗漏 leakage 凸轮 cam% e$ g( K, T$ Z9 _. w0 K
升降舵 elevator 图纸 DWG. k, Z6 o6 s/ o1 @- e& x& ?; n
绳 rope 涂,粘贴 apply
) v x1 W, C( q失效 inoperative 退漆 strip paint
/ y: S- u i# B0 ^8 \3 ^湿安装 wet installed 退色 badly faded+ U4 B3 r0 ^) f9 h3 I5 `9 ^" t% S
试车 run up 托板 pallet
5 G. ~( M- x, ~) k. [1 e' u释压 pressure-release 托板螺帽 plate nut$ s. ^. B, E [" N, n
收 retract 脱开 disengage
/ V, n" D3 }! e' ]" Q, R收发机 tranceiver 外 outer$ X9 s: H. u# D v+ e- E5 D
手柄 towing lever 外侧 outer board. z5 z6 n1 B+ D! z& ]9 d P
手册 manual 完成 complete; G8 O/ G: {3 K
手电 torch 完成 finish
( X' f, `% C( \* a手工 handwork 万向接头 gimbal* n Q" M' S' K8 N/ M
手提的 portable 维护 maintain8 p6 O% u- `+ l( q
手提灭火瓶 extinguish bottle 尾部 tail 8 l* R. z5 K+ H6 @1 E
树脂 resin 尾舱 tail compartment
6 ?, {. b9 I9 z! Q: E双倍 double 尾喷管 exhaust nozzle
5 Z, j4 F! B3 a# C) E9 X2 m* O水平安定面 horizontal stabilizer 尾锥 TAIL CONE
7 ~* a5 J/ G' }1 ~1 O# n撕裂 tear 位置 locate% B4 p2 X" V) U) I9 d5 g. R
伺服 servo 温度 temp u. y! d% z. r4 C+ O$ t1 z
松动,松脱 loose 涡杆 jackscrew. V4 d/ ?- X4 c5 o+ {
送修 send to repair 涡杆 worm bolt
) e2 M+ r L7 H0 Y$ I+ e# k2 h p塑料 plastic 涡轮 turbine
4 ~% O4 K: E0 v随动盖板 hinge access door 污染物 contamination5 E1 N. {4 q4 r4 V1 G: C
锁 lock 污物 dirt
8 ~5 [ O: D f锁定 lockout 无线电高度表 radio altimeter
" y: R+ A1 S* f l* Q) `; s锁扣 latch 稀释剂 thinner8 _9 {# o. m+ O1 N) n- X
锁销 lockpin 铣 mill3 y) p) ]- P/ o- f/ ~3 e
系统 system 溢出 spill7 ?/ ]/ H5 Y( w& a8 t! [4 z1 Q
下部 lower 翼尖 tip, {) P. }# n# h! g
下角 LWR corner 翼间 wing tip8 a' t* h w/ a1 \$ P- ~
下位锁 downlock 翼梁 spar
5 Z' u! T# Y, ^. v下陷 concave 引进 introduce5 r. N0 i) L2 n+ C: M* S; C; d5 H, V, A
下缘条 chord 引孔 make guiding hole" h! L6 O' z+ g1 K, k0 s
纤维板 fibre board 引孔 drill hole
2 t, ], H! s9 _$ \: p- h相关的 relative 引气 bleed
% \! z9 x$ h" W( A6 ~* }1 v相磨 chafe 引气管 bleed hose7 i g9 B. x T" u( n* I3 H
消音板 accoustic panel 应急 emergency' E9 U' b$ ~ a& A# H
销子 pin 永久性修理 permanence repair
3 _/ _( y; K7 g7 |/ q6 W. ~3 I6 d楔形块 wedge 用…填补 fill it up with…
% w7 l; s9 z* k) N信号灯 annunciator 油封 preservation
% h' g3 v. Q! a* r" E9 w行李架 luggage-rack 油箱 fuel tank# A. W4 j' n! ^: y
行李箱 stowage 游动梁 walk beam
, Q8 g s. G( U V& V$ ]! l5 _修边 reform 雨刮 wiper
1 j9 {' u$ v5 h$ c$ j修理 repair 语音记录器 voice recorder. W- d& y; c" _2 Q0 f; m
锈蚀 rust 预冷器 precooler) [, [) R' w, h0 U e; A5 G
循环 cycle 预位 ARM
/ k. P- G9 a$ M Y% H5 {' B+ @压紧 gland 原厚度 original thickness
9 ~3 n" I" u! \( _% C6 _! q压力通风系统 plenum system 原来 originally
: d1 `9 M+ ~$ ~ k8 } |4 @7 L7 L压条 cover 阅读灯 reading light
3 N8 W( b8 I0 q7 H$ y严重的 serious 允许损伤 allowable damage+ q/ M1 C9 ^3 |- O0 A
阳极化 anodize 杂志袋 literature container/ s: [$ T1 _' C$ H
氧气 oxygen 载荷调整 preload adjust7 s6 e2 M9 X; j ]) l9 R
氧气面罩 oxygen mask 再循环 recirculation6 M( Y2 E/ ^+ |! H0 X0 k
液压 HYD 在位 be in place* F& B, F! K' R( g; D
液压泵 HYD PUMP 脏 dirty
+ |% v( B7 F. q, E b液压管 HYD duct 增压 pressurization" t9 K" V7 r7 S6 V5 ]5 ?* n
液压系统 hydraulic system 增压泵 boost pump
' d- o+ B( e! E6 G7 G) C液压油管组件 TUBE ASSY 粘贴 bond+ G {0 m# `7 t3 s2 s; T6 i
液压油箱 hydraulic reservior 照明 illuminate
6 M; ^' p X# e% R, J3 a$ P9 c移到 move to 遮阳板 shade
& L4 u: u, a1 W) J$ Q8 C+ E$ J真空泵 vacuum pump 自动刹车 autobrake
# x l) h4 A5 Y& s- ^" n拯救 salvation 自动油门 auto thrust( ^1 Y# {0 `: w1 z* I: }8 C# c
整流罩 fairing 自锁螺帽 jam nut; f4 L, ^! O1 ~/ f
整流锥 spinner 自由移动 move freely w2 w& N- m9 J2 Q3 _! @
整形 rework 总管 manifold8 Z+ C) l9 @7 M
正常 normal 纵梁 longeron, v$ u; `8 a; C
正常位置 normal position 纵向 longitudial
8 ~) e5 |1 Y! t8 J正驾驶员座椅 captain's seat 阻力支柱 drag strut
2 j3 C1 q& o+ a [之间 between 组件 assembly,pack; z( q: M+ E4 j
支撑架 bracket 组件(电气) unit& d( T' g0 a! ^0 d# Z9 V0 m/ h
支撑座 support mount 组件(机械) assy
3 d; E: d7 v9 Q! m7 f8 N: `' J) Q支架 bracket 最薄 min thickness
% }! Y6 u6 h5 H: l$ H0 B支拄 support 作动筒 actuator4 W Z1 n2 \0 \
止动固定块 stop block 坐垫 cushion2 E5 x3 V( M& K7 {9 Y8 k
止动块 atopper 座椅 seat! c1 e2 e! \/ t4 k4 U
指点信标 marker beacon antenna 注意 caution
2 H2 N5 q5 J# Y! s8 ?指示 indication 转接器 adapter6 G4 t; u- d+ G6 Z
制作 fabricate 转弯灯 runway turnoff light# H7 I j; t2 b/ R4 z
中厕所 mid lav 转向 turn z) f- ?* q% ?* d. s- f
中间,中央 center 装饰条 trim strip
& o9 ?' s7 f: T- L3 F; K' l# E周围 around 准备 prepare
' D) H* m2 O! W$ h2 {) q轴 shaft 着陆灯 landing light
, N% y5 H6 o1 M* m- W/ `9 x/ H轴承 bearing 自动关闭 auto close
6 S' \# V/ o% q' u' u8 Y( G主轮 main wheel 助推机构扳机 power assist trigger5 @7 z, L: R3 N9 |( Y% r3 A# I% L
3 F* d1 s& p5 j. j
7 V9 [- Y) a5 a
, G7 \9 P ]6 C) y
, @; O, G6 ^) [1 \9 u6 T2 `' ?
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1 d) g' a8 z& K% R( g4 s% b# }6 P
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) Z9 \7 B. i2 h0 r
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8 H$ f9 @6 c9 E8 O7 a$ ?4 t) X. w
, [- j& Z( h5 ]( g2 B
* B. j0 M$ X+ h4 Q3 E
0 _& H, {" U( f# q. a
$ A/ _/ C. \ P! g( x
5 v- e* z _0 g) k& ~$ W% j7 y) X& c! P2 j( C9 k
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6 J- j ]3 |" T O/ r P
* L2 S3 T+ o3 R+ C
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3 P2 v- Z+ ]3 i- \# W' C
! D( M! p# k7 w2 aCategories of Defect
6 Y1 {# B7 K" W" t2 i9 O Categories of defect depends on experience of maintenance practice .In this manual, the default
8 r |- w- d' c 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. 3 V+ C1 X; y8 X1 y5 a$ _5 ~' f7 S
缺陷分类
' k; A/ V+ Q* C, q' b" F. m 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。1 i( q! c; V" B& ~
! R! F( x6 a$ K$ \' e
1. Common Structure Defects Terms5 F" F3 ~1 I: r, M8 T% @6 f5 ]
结构缺陷术语
U3 h5 W1 _$ U% N* b- J - u8 h( O( i7 Y/ `) q4 X W" ?
凹坑(1) dent % w/ L4 k `0 f$ l/ V0 f# z# c
凹槽(2) notch1 e( E" k" a F0 I+ Z
变形(3) deform
) S0 v5 v# H7 M. {5 q划痕(4) nick7 i; u; L! f( E9 {% O2 r8 D7 F
点腐蚀(5) pitting$ `7 W) ^* b8 P2 ?1 P' k
断裂(6) broken: x+ t; u$ f4 z8 _" Y2 w3 V2 A
腐蚀(7) corrode+ J; ~4 W1 G; y, T1 b- A3 H
划伤(8) scratch6 @ V( C3 P1 n3 ?& U
裂纹(9) crack' q' c/ U7 x! t. Q' c
毛刺(10) butt% b6 A* G* ~ r# s6 n
磨损(11) chafe+ J9 N8 b4 h F2 @, b7 t& ^
凸起(12) protrude* i9 O# M* l. O1 M F
凹陷(13) sag+ [" X3 A& E1 W' y
粗糙(14) rough( h7 @7 S9 x1 O) Y" I
漆层剥落(15) finish missing
. Y* B$ K( ~# G& r5 }3 e% L褪色(16) fade
7 M* B, z$ I2 R积水(17) entrapped water2 j- m2 O; j7 ^! u; ^, ]
2 y9 f& Q) R2 Z8 ]8 X
2. Common material defect terms4 w9 ~0 g. R( |& V& ^/ U! m
材料缺陷术语9 ^! D' q8 j) F8 f! ]
Material is divided in two categories: metallic and non-metallic.8 p/ X5 f% u! ?4 W
材料分为两类:金属材料及非金属材料
. q1 x5 c8 N( T- a( L* N" D5 Z
0 B! V' e* `+ n- ^9 g6 d6 i+ n" } 1)Common metallic defect: 0 |8 T9 f* ^: Z I1 b/ A$ n, T E
一般性金属材料缺陷:3 H. w+ z: v: L% B
; C0 ?$ N3 p; n0 X" Z- {, o 氧化(18) oxidize 5 @: L! F2 ~0 B _9 v6 D
划伤(8) scratch: b8 Q% n0 B: r) H/ h
扭曲(19) distort" e' C8 W8 N' a7 [
跷起(20) not in contour- e' h- K& G( B0 _1 o
穿孔(21) puncture- F- u; x9 _7 d& R' X+ @
碎屑(22) chip) k% V- P* a3 F, k+ q
腐蚀(7) corrode
& o7 U% A& Z& u 磨损(11) chafe
5 P3 p1 I# i2 w0 R. r+ Z- j$ b4 {变形(3) deform* h6 N: e! ~5 y; r |. g1 N
风蚀/风化(23) erode- G2 n3 A* |) L* S* \ E
裂纹(9) crack
1 {$ @9 z- }5 N/ z 2) Common non-metallic defect:; b* A' d6 a: C/ a* P
一般性非金属材料缺陷:/ E/ s8 c. n5 Q: E, N; U
% G7 C. x5 Z5 p/ r1 N
发霉(24) mildew
! Z/ x* C, {6 Z/ [+ H分层(25) delaminate
+ h" u5 F1 O6 G: o; Z风蚀/风化(23) erode! w9 L1 o, G, f: e
裂纹(9) crack1 C+ s! G9 A$ c4 [6 l& K7 ~2 w
老化(26) deteriorate
6 z+ ?2 I8 G/ f9 {" c起皱(27) wrinkle
- S* b* Y! y: J# _受潮(28) saturated
- f4 c0 N( y) O/ W$ \! x撕裂(29) tear: G( Q" O( {; _/ y+ d
穿孔(21) puncture" z- V! @) W" j( G2 m7 w& d, b
变色(16) fade% N0 L( L4 p( Q9 _* G& L; S0 o$ z
陈旧(30) worn9 w: R% S k; P+ u% l) J
脱胶(31) adhere! ^0 v* k3 O7 U) i( O4 J$ l
% R& D$ j, y% h5 ~# e
3. Common part component defect terms
) V) H/ u G" R- N6 h+ r 设备及零部件缺陷术语/ M0 O- _/ @/ c) u4 ~5 M0 F: b3 Z
Common part and component including : Plumbing, Wiring, Mechanical linkage, Fastener and Miscellaneous.8 U9 `, c( `% _5 d
设备及零部件分为:管路、线路、传动机构、紧固件及其他。) R! u4 X; B2 h2 c
& G7 c$ ~8 N3 B" c4 E! B1) Plumbing defect 管路缺陷5 s( g9 N3 p- [
7 q4 J" T7 z6 V* f& ^. }9 `
凹坑(1) dent + j$ j7 R: P5 _' q
爆裂(32) burst
) m- u) ]2 ^# t$ \擦伤(11) chafe5 N y! r& [3 y5 U! d. y
滑丝(33) cross thread2 A& G# D7 L5 I3 v% `# T
扭曲(34) twist
, L: @- Z) c; g渗漏(35) leak
2 y( e" `# I8 V6 l堵塞(36) obstruct
/ y1 o# ~6 \- x8 d5 I7 ]+ H 9 {8 y3 [) K9 d6 @* x5 @0 w0 k( v
2) Wiring defect 线路缺陷8 b# E6 n2 q& Y
4 W" F8 H0 D/ _9 s9 ]
腐蚀(7) corrode
$ r, R4 b8 t/ u0 ~/ n+ @" i磨损(11) chafe, ^0 @5 Y' v6 b1 M: U
相碰(37) contact
5 J0 u# q4 {7 {5 f断丝(38) fray
* H; u. g8 d$ T" M8 X熔断(39) fused5 M* x4 Y( V; h- }
弯曲(40) bend
2 v3 a' B3 s& H# ^; E. [ ! p1 L; a3 r3 S' g* m) ~
3) Mechanical linkage defect 传动机构缺陷
4 J8 p0 [* z ]* c3 U
( e! m; T2 R' \- ?断丝(38) fray - X! A: p- l+ e
松弛( ) slack
a/ g W* t: m3 e, g" T9 u扭结(34) twist
4 N3 \9 _5 f# t/ J磨损(11) chafe
1 f1 w& _! r" c! b脱开(41) disconnect% Q$ d! d) O5 m- E
3 f" M) v% w3 J. l. f4) Fastener defect 紧固件缺陷
, S# p$ m8 x: c+ b, v; X8 W & b' |! g. ^1 Y' U! u# b
丢失(42) missing' J5 `6 ?& Q$ _* u+ T- C
松动/松脱(43) loose
* Z( b: O, M9 X: G2 ^8 u# m7 \+ C 腐蚀(7) corrode
! r8 a* j$ J2 g4 O' L |! B 磨损(11) chafe7 j: f7 v3 y+ @, R2 ^- ], v. X" `
未关(扣)紧(44) not secure" \1 N, z2 H- }# a% t
c0 x4 ^7 k2 t3 g* {* U5 g) C
5) 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. % R( h' l8 Q" }8 T/ r v
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。
7 e# d( x# ~) Y1 n1 X' w* N& V / k6 e4 P0 H4 i: u6 I! m
a). Sealant 封严9 |2 w2 d+ W0 V; |! I
2 N2 u" J, A/ _% x7 i- x& A 脱胶(31) adhere) V. E2 J. J% _0 e# c1 U$ p; ]
老化(26) deteriorate# e8 y2 t- w% `! i7 r; \: E4 o
不均匀(45) inconsistent
( i) E$ e$ i+ w+ b# }+ q
1 T, \+ C+ h& B" s b). Wheel Assembly 轮胎1 Q5 J* M5 g s* X
见线(46) exposed cords- P5 h6 j2 T4 m) g ]6 J& v
磨平(47) bald
+ ]+ Z8 ]1 B* ? 扎伤(21) puncture
# ~" s/ r; s; n. C+ Z 气压不足(48) insufficient-air-pressure
/ g, \7 ~8 K6 M7 V5 n0 o3 m ; C4 W( l9 K% m
c). Life Limited Parts 时寿件 : \+ Z8 t8 n0 C& N) K
( w0 v; g& m$ {' W1 \
过期(49) expire
1 [1 e# B# L# ^& Z7 | 3 P/ X. u+ ]# D/ W
d). Placard and Marking 标牌/标识
+ P4 k8 J; H; e
9 N( M, `5 T: N# l1 O* F 模糊(50) illegible
8 d* P7 ?+ Y' ^( y2 \ 缺损(51) damage
0 B3 s0 Z+ H. R3 O& ^4 E 丢失(42) missing/ B8 I0 h1 j+ c% S+ P' b
翘起(52) lifting ) F0 W# b! N( Z
. j6 s, [- w3 ee). Slide/life Vest 滑梯/救生衣* o; ^2 p6 ?' C0 Z% t: C) \
, q) \% E% J1 j$ @2 I* v% g- b
散包(53) not properly packed4 X( a, f- Q8 D4 o5 t1 s
变形(54) not properly sealed
( S+ F% }" v: M3 M0 j6 V/ V. }0 W3 w1 @1 T 9 {7 A8 O- k3 ?
4.general defect terms 一般性缺陷术语6 k6 x( C. n( h1 T* V- ]
8 ]1 l3 H6 d6 w( \' {: S
脏(55) dirty& `, z% |& U) X' j
陈旧(30) worn3 s6 t1 G, B* y" I* p8 V
断裂(56) fracture
8 z, B6 c$ m6 s! T; r- g 磨损(11) chafe 1 D$ E* L1 l- _0 m) L
超标(57) exceed-the-limit; N/ o! N% G6 ` S# B* W* Y6 c
丢失(42) missing
6 R* z7 |7 X6 ~% J# V! r! l 腐蚀(7) corrode8 _2 ^- Q/ g7 t0 t5 a4 Y7 d
裂纹(9) crack8 I# d2 {+ ]$ N- H) p1 Q
空行程/无效行程(58) backlash
$ {, Z: k8 H7 S9 V g; B; T 卡阻/阻塞(59) block% Y; h5 `) e w% n
鼓起(60) bulge0 o' d0 B. R$ \; l
污染(61) contaminate0 @, N( O0 A. i6 K4 d& w
不一致(62) disagree" s. |7 q8 Z6 T) L a* Z! b
(电池/气瓶)被释放(63) discharge
2 o" h, D* ~( R. e4 q 装错(64) dislocate( t: Z* w5 I* T- K" z& D
失效(65) fail4 D& R3 g6 j/ n- w' Z( y8 e
摆动(66) fluctuate
; D& u+ v+ u# y- d 抖动(67) flutter2 q% o3 f" _3 v: {( I5 D
不够/不足(68) insufficient
- f$ F$ x5 p4 a$ n% t' C7 y 不工作(69) inoperative" `1 s/ v- D2 |+ [
(不)亮(70) (not) illuminate
, Z, c G, t, \1 ]: @ 干扰(71) interfere
1 x1 F3 m, z9 \3 m! P/ F7 | 扭结/缠结(72) kink
* ~1 y! s! _6 v6 j 走向错误(73) misrouted
# a5 p+ h; }/ Z' B# D! i( o# t0 R 漏装(74) not installed9 J7 x& z8 ?! S# H
相磨(75) rubbing
9 j1 }% s( W8 h( }2 s7 M1 Y: r 干涩/缺乏润滑(76) un-lubricated, E8 X3 ~$ z" I6 P9 g' y
不能复位(77) will-not-reset9 c" y5 J7 K3 T0 x! n' e8 y( }. f$ E
& P$ b- F. ?. e U (1) dent: 凹坑( j, [6 }3 z& L% H/ t$ S" S( X
A depression in a surface caused by pressure or impact.0 y( X+ C6 q; v4 k$ D$ U3 v
受压力或冲击造成表面的下陷。5 y% Y- D0 Z5 j! a
For example: Left horizontal stabilizer outboard leading edge at WL 368.25 dented approximately 2 inches in diameter.(Area marked in red)" b# I$ R2 A/ A$ P5 T2 @
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)。
6 n0 ?5 U+ {% Y/ s! p 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---5 S, s9 Z! _( n# d' u
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。- i& a. o2 f5 Y- Q8 n5 K: y- T7 \
: u' N' T2 J- Z" \/ V9 F
(2) notch: 凹槽
1 e% I* F" h6 _& {5 u9 J A “V” shaped cut or protrusion) ~4 P. k0 `8 ?
V字形的切口或者突起
, D( q$ M$ m& k# @9 j For example: Forward L1 entry door number 1 floor panel has a 1-inch notch 6 inches from the forward right edge.
( R+ G" y7 t* p/ Q. _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$ G8 k( o4 F+ d3 G. o
槽。* p5 g m8 Q) X% V4 T$ k
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---.
, M* ?7 g( {6 z# s0 B' g 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。. [" ]& T9 T+ i
8 M' v- T$ ]9 b3 L- H' k1 F+ g- L
(3) deform: 变形" J, s# R/ { j% E
To misshape the original form8 E) U! G s+ e/ F6 n
原有的形状发生变化
( T; p. B3 [- R% y4 B/ g/ AFor example: Left wing number 2-fuel access door is deformed.& d) W+ e7 K4 u8 F# I0 e$ M, z) K
左大翼二号油箱盖板变形。0 s2 J$ v( p: ~9 p# O! A+ K5 @
Replaced number 2 deformed access door in accordance with AMM--- Carried out fuel leak check in accordance with AMM--- with no defects noted.
$ g" P% [1 N2 g4 F 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。4 S! @1 \! ^3 b7 M
) ^$ Y. J& v; K5 p) W2 _2 o# t
(4) nick: 划痕
0 z' L% I, Q( j7 ] A shallow notch, cut, or indentation on a surface.0 V$ c7 R. J5 _: [( F' m
表面上的较浅的刻槽、刻痕或缺口。
8 Y7 w( q: [1 R9 j8 @! |; U) f For example: Right environmental control system (ECS) access door, after right corner has 4 nicks on external surface . Area marked in red.
8 W. p9 P g N7 v7 ^2 D 右空调舱门右后角表面有四条刻痕(已用红笔标出)。
0 Y' M" X: Z8 p$ P$ U 7 Y G h- Z6 ]
Detailed inspection carried out with reference to SRM---no delamination3 t: u4 o7 C Y, r2 x
noted. Carried out permanent repair by filling nicks with fiberglass and epoxy
* O/ P( ?0 k; y& M% hresin BMS-387 with reference to SRM---.; M' v4 X) \+ v( D& E% v. I
根据SRM—详细检查该区域,没有发现分层。按照SRM—进行永久性修' {1 }7 }& |5 w( M$ Z
理,使用玻璃纤维及环氧树脂BMS-387填平刻痕。
4 s& z( q1 m4 q6 }/ F) X! h
! W% a% E# i2 K9 j5 j$ K" B# Y F; \(5) pitting: 点腐蚀/砂眼
6 e1 s: C' a4 _& k" W4 C4 _2 v Small cavities, depressions or scars on a surface.) {/ M# i2 r! h n1 b
表面上的较小的空穴,凹陷或凹痕。
! B2 h) G3 ~) m% y1 VFor example: Left main landing gear number 1 brake aluminum hydraulic line has pitting.
5 n3 u8 C& U( c 左起落架一号刹车铝液压管发现点腐蚀。
+ w& O5 H! {9 r0 G* ^# {+ f) W3 c Replaced left main landing gear number 1 brake aluminum hydraulic line with6 w4 d+ w* U2 V( [/ o: p* M6 Y
serviceable hydraulic line in accordance with AMM---
% b. ~. k6 H+ x% F- H1 G 根据AMM—更换左起落架一号刹车铝液压管。
* v1 P! I6 G3 Z" z) n1 D r$ K ) x9 d9 j& C+ y G0 o5 J% a$ L
(6) broken: 断裂
# \9 q; C- E2 O! U. _& f" E) R Forcibly separated into two or more pieces.
4 {; I1 G3 S( q$ ? 被分成两半或更多块/ r3 _' \1 x+ k- v
For example: Flight deck entrance door has broken door latch and will not lock. X4 V/ y. @) y# C$ F2 w
驾驶舱门锁销断裂,锁不上。8 z7 @2 X- R* ]$ e
Replaced broken door latch on flight deck entrance door in accordance with AMM--- Operational and functional check good.
( y3 F5 o- A5 u" h/ x( f 根据AMM—更换驾驶舱门锁销,操作检查正常。
3 p# s& y; w+ z7 y5 T & a/ \3 G L4 C7 a4 c
(7) corrode: 腐蚀4 D- R z, c# D
To dissolve or wear away gradually by chemical action.
5 W3 M9 T* p* f7 i6 \ U2 I 氧化或化学污染造成金属表面逐见破坏的化学反应。# @: M/ m& @) e/ }. w
For example: Floor beam at body station 360 and wbl 25.1 has moderate corrosion 2 inches in length and 1 inch in diameter.8 c( i. q/ L3 y% X, f
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)。) h3 c) y3 \" q+ T1 z: e9 s
Removed corroded area by grinding and polishing in accordance with SRM---. NDT revealed remaining thickness out of limit. Carried out permanent floor beam repair in accordance with attached Boeing TELEX 530092-23 and attached Gameco engineering order 53-099-84.
4 G8 H: B8 f: Y) G$ ]9 K% v 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。
- H0 p7 u+ W3 i$ C/ j- L4 ^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。
( s, @1 R2 {4 @, Z! D2 d! m1 m1 d, @
8 Q; M* O/ U7 R/ d' ~ (8) scratch: 划伤5 ]9 d) w1 y3 `4 d2 C, O! }
A thin shallow cut or mark on a surface3 A# {$ \ d! N5 w7 M4 Z( N
表面的薄而浅的切口或痕迹。- T& S: u$ e5 w5 M& [
For example: Left cabin external windows numbered 12, 16, 17, 21 and 27 are scratched (obstructing view)
2 m/ _" ]# N, ^* o, K 左客舱外部12#、16 #、17#、21#、27#窗户被划伤(阻碍视线)。
9 a$ T5 `- }0 X0 o6 Z& S3 |; e 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.
/ Y$ J2 ~0 e. d& g l+ Y 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$ O+ F- n, N4 X0 T4 w( j0 |4 k
/ S) Z& E1 ]% b" z$ V5 E, `1 V(9) crack: 裂纹/龟裂
9 j; Q+ Y+ L0 ~8 l5 T) V* s To break apart without dividing into two parts.5 X5 e! l/ D, m* k8 e. c
裂开但没有分成两部分的破裂。
% L: x/ a3 g. v( i/ s! v For example: Number 2 engine fuel control cable located at Body Station 360 and Water
2 t) W% f) s' l+ v2 l! z+ bBody Line 25.7 has cracked turnbuckle.1 ^8 c& @( G5 n) f) P4 U
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。4 F- f- T2 \" u4 F$ t; n" I
Replaced cracked turnbuckle with new turnbuckle in accordance with! q5 a7 L, ?; z/ w* i7 }
AMM--- Travel and functional check carried out in accordance with AMM---,
- C! V& Z; n& f+ E! S, F# Pno defects noted.
3 p% x; z5 b( B) w4 }2 I$ I% d根据AMM—更换有裂纹的松紧螺套。按照AMM的要求进行行程及功能测试,检查正常。9 z' t& D9 P5 l
! k [+ V8 d; Q(10) burr: 毛刺
* Q* W2 P% H' |. j0 BA rough edge remaining on metal or other material after it has been cut or drilled
7 ^: O C5 x! i8 N! U Y' K' e被切割或钻孔后留在金属或其他材料上的粗糙的边缘. h/ ~3 p n% }) X% x, p, W
For example: External fuselage repair at body station 727 and stringer 9R~11R has burrs at( P9 X! Z: s3 M! k1 c
all drill holes.. o, d6 \" F' }1 k' Z- [: n
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。4 g0 p1 j) D; U6 Q
Removed burrs with rotary file in accordance with standard practices and
% _0 x2 r3 ?' ~, I! Y7 ?SRM---.
5 ~$ A$ i& [4 x% M6 W9 V8 D 根据标准施工手册及结构修理手册—的要求打磨去除毛刺。2 q& k1 c3 a' x- G( l0 [
6 @4 I* @2 Q0 M: @% Z8 A# y(11) chafe: 擦伤8 L/ G* G: Q$ L) E5 e3 F& K3 |
To wear away by rubbing.
+ ?6 ]7 {1 p' U/ c( L因为摩擦而损坏。
, i( E4 B1 U! }+ S% T) aFor example: Forward cargo compartment after corner threshold chafed by cargo door.
Z$ u0 z' _! l& Y0 ^) R 前货舱门槛的后下角因与货舱门相磨导致擦伤。0 [8 V! }+ v. Z& O
Forward cargo door upper support bracket worn. Replaced support bracket in
% c: D! T" E3 a3 J8 A- Iaccordance with AMM---eliminated chafing.
! L3 k4 R3 [1 [ H' P: n( ^* m& p) Y检查发现前货舱门上支架磨损,根据AMM—更换该支架。
+ W1 \/ L7 `; g+ O7 j6 U' s " g! ^7 H1 x$ y ^5 T$ j5 v
(12) protrude: 凸起/突出
8 j$ q( h; Y, u+ J# t9 ^9 U+ W7 rTo push outward.( [! s% B* d3 G$ ~4 K% ]5 o9 ~: M; w
向外伸出。4 [# c$ `' o, I, _2 m! X% d
For example: Forward external fuselage servicing doorstop is protruding through access
% g& y& Y# y3 l. [door.
8 ?9 A: Z( J1 J( ~' J 前外机身勤务门止动点凸起。
! H1 \, P( F4 V% {9 A" H. ? Repaired forward external fuselage servicing access door to original contour with reference to SRM---. Adjusted doorstop to eliminate protrusion in accordance with AMM---.: C: M& U: a3 a2 K/ T/ Q
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。
0 Q# U# k9 t! X4 t: L: y
( T& Y& T2 b( {, V) c* P6 Z(13) sag: 凹陷
5 V$ F( F, c! v' Y( E/ c3 HTo sink, droop, or settle from pressure or weight.$ H; m) _- |7 g# @
因压力或重力而下沉,下垂或下陷。$ @& Q* v' f( u; T3 ]
For example: After cargo compartment overhead ceiling panels are sagging.9 ?( i1 N3 ]4 w n# `! _2 z
后货舱天花板凹陷。9 x) e' t9 ?3 H. e d: s
Detailed inspection revealed ceiling panel screw holes worn. Replaced k4 M! v/ L# ?6 [& W
unserviceable sagging ceiling panels with new as referenced in AMM---.
$ `( W! Y& d/ j" A& W4 M. R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
$ v/ J" h+ q! l! v! F, C板。+ |* u' h5 H8 n [8 E( H P
* y2 Q: o8 _3 ]0 t) Y9 B5 V
(14) rough: 粗糙4 K2 W2 G5 Y3 I& \4 V8 Y
Having a bumpy, uneven surface.
3 ?" o# r1 |6 M& `表面不平坦,有起伏。% W5 E" Q( ~5 h* ]& a1 K3 Y5 {
For example: The protective finish is rough at the number 1 engine inboard pylon.
# {6 j$ }: g- ~6 [* z7 H0 L 一号发动机吊架内部的保护层粗糙。
0 o: s4 C: [6 w- N Removed rough protective finish at the number 1 engine inboard pylon in
. G& H8 N% Q D. r; waccordance with SRM---. Applied 2 coats of enamel to restore protective, Q& h# F( R$ `. ]7 Y1 j
finish with reference to SRM---.% L$ O( f7 U4 v T | C
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。
4 N7 Q) ?3 a& P) q + Y1 Q* I* B$ `+ f: e2 h# X
(15) finish (missing): 漆层(剥落)8 m; x& T$ U% b( @& j; M- G
To protective material used in surfacing and finishing flake off. [, ?* g/ @6 Q8 C+ 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。
( {/ l, ]6 G4 E" k' t0 [7 y5 VFor example: Fuselage skin protective finish at pilots and copilots number 1 and number 2& f7 d" J' o* \8 t) X( i
windows missing.
& v" E/ ~1 |0 w% H正副驾驶1号和2号窗上的机身蒙皮保护漆层剥落。
1 N( O* S/ {# u* @Prepared affected area of fuselage skin at pilots and copilots number 1 and
, K) V6 s2 e" l; P8 lnumber 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.
# ?- u O9 A O- E1 n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。
7 o m2 U! q1 R0 n4 A / Q* U% s" ^" E& T' N' O4 A
(16) fade: 褪色/变色
* F I: b5 v' Q1 V k: |7 nTo lose original brightness or color.: e1 F# Q3 W. G+ V; F! D P
失去原有的光泽或颜色。5 M0 ?5 ~) M& g# m! R" A* {
For example: Number 1 and number 2 engine intake cowling chrome is faded.
& h3 i0 A$ {; I; ]- A& {; n( v, X 1 号和2号发动机进气道的铬层褪色。
' p7 ]5 l9 {3 z/ Q" x' \# j- I Polished number 1 and number 2 engine intake cowling chrome with reference" v8 y. q4 ]) H: J$ o' u
to SRM---.
- O1 \- x7 {- g( W' r9 L, {0 c, S( t 根据结构修理手册,对1号和2号发动机进气道铬层进行抛光。
7 {& o9 e a) x8 O) a& }/ @ # x9 i* y6 I$ b7 c( I& @6 y
(17) entrapped (water): 积/含(水)
& y5 i0 Y& b( E% n) i9 u* p+ O4 r; mTo collect in an area.
5 v7 R# j; M; B水或水汽在某区域内聚集。
5 u. \0 H2 g6 Y2 DFor example: After cargo compartment forward bilge area at body station 840 has entrapped
# R$ a6 s4 J' i- H8 j- W6 e( Vpotable water.( j/ \$ W1 b6 E2 A' b+ @
后货舱在机身战位840处的前部区域有积水。5 V7 d5 f, b/ Y. X# y9 v- G5 S' Y
Detailed inspection found pressure drain valve clogged. Removed,cleaned and reinstalled pressure drain valve in accordance with AMM--- Removed residual entrapped potable water.% S& G- m0 M" V- Q& J3 L
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。. D" T @1 F6 n: B& k
# _7 G5 b5 l, _- k, r8 O$ L k$ |
(18) oxidize: 氧化
& t+ R4 [# E% i; e, \; l4 U- h& `# SThe containing of oxygen usually caused by natural elements.5 ^: E6 [3 D3 G( b! u/ A8 l
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。
) ^, _" s* v7 _For example: E-3 rack lower after corner is heavily oxidized.3 |- s, p& o2 o! Y( y% \; {9 E7 x9 T M
E-3架后下角氧化严重。! ~3 ]6 m. p! }+ E) T) b
Removed oxidation at the corner of E-3 rack in accordance with SRM---.
5 {+ a7 q( `/ ~# B% A' W& x 根据SRM—去除E-3架后下角的氧化。
7 N, K8 c( k2 w* Q $ {$ W, [0 e; _4 ^9 N
(19) distort: 扭曲+ ?! ]. \' \! E* k+ y" D. k- ^/ ]
To twist out of a proper or natural state./ g, L7 Z; L+ T% H1 y# P M
因受到扭力而导致原有的形状发生改变。
) n8 ~1 r- i' b% _0 HFor example: Access panel 2145J to left wing number 3 slat actuator distorted.7 {# Z, v/ E, S2 d6 Q% }
左大翼3号缝翼作动筒的接近面板2145J扭曲。
- D- K- w3 u C4 B! Q Replaced access panel 21458 with new panel in accordance with standard8 Q! y7 ]" @% z0 w. j% f- e
practices and AMM---. Original panel declared scrap, tagged panel as much
$ ?9 Y" P# q! C, N( |: [and routed to MSC to return to customer.
: I# P4 B- |( Y+ 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。
! _* S4 Z2 t4 Y
: o8 {" b% L) c: u" ~5 v* G2 X(20) (not in) contour: 外形/轮廓翘起
6 q- g0 U% g, q9 Y" O2 b: T$ pA shape or outline is deformed.
& ?1 a( `& g3 H- f形状或外形轮廓变形。2 n0 f! I) W$ Z: h
For example: After lower corner of after fuselage external servicing door is not in contour& y* j8 N: z! S& L3 X B
with the fuselage.
6 d$ L6 l- x6 G9 e- L( ^" ^+ g后机身外勤务门后下角翘起。
$ W( x, U, Q7 ~. \0 N/ y. K% ZAdjusted after fuselage external servicing door to contour of fuselage in/ |% O5 s. S0 S2 Y9 S" m
accordance with AMM---.: N! [ b! U1 x5 T5 y
根据AMM—调节后机身外勤务门正常。
5 l) @; M- e% Y) O % s2 K! @6 ^2 R: y: N+ {
(21) puncture: 穿孔/扎伤
/ C! c$ K+ ]$ y+ |9 GTo pierce with a pointed object.
1 X# [5 e% F4 B& L2 m被尖锐的物体刺穿。
! a5 [! Y' d- u0 ~* a5 J# d# ?) FFor example: Number 4 tire is punctured.+ [) E8 Y! W$ d/ X/ H
四号轮胎扎伤。; f. G6 M% Y/ O) ^: I# p
Replaced number 4 punctured tire with serviceable wheel assembly in
* M* a+ S, X2 C! Paccordance with AMM---. Pressure check normal.
/ e8 L! N' z' n9 a8 j 根据AMM—更换四号轮胎,检查压力正常。% O$ ]2 f1 o2 |+ Q
5 Y& [; `; R% \" H# R
(22) chip: 碎屑1 n% ^5 d" W$ V7 d7 U
A small piece broken and missing from a surface.. ^$ o- ~: s6 Z8 M4 \
从表面剥落的小碎片。
8 L- L; Q% Z# v( s, SFor example: Starter magnetic chip detector has evidence of metal chips.
_+ C) s5 V. T" r1 C 起动机磁性堵塞上发现有明显的金属屑。% {8 k5 X3 \+ X. z5 s: a+ \
Removed metal chips from starter MCD. Drained and replaced oil, operation+ p0 D/ S9 p1 O6 X# ]
and leak check good in accordance with AMM---. Reinspect next “A” check as
) N- J* d* S3 E per attached EO 80-003-1.* j& o+ k: S0 u( ?9 f( g% v9 i
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。$ m, }6 [, _; f" P
, [8 s# L# v0 v4 m
(23) erode: 风蚀/风化
2 C; E8 u; H& n) wTo wear a surface away by weathering, abrasion, or foreign particle.
7 j) [; v8 d- @( W, q因天气或外来颗粒等原因导致表面被磨蚀。
+ Y& k' ^9 x1 YFor example: Number 1 engine intake cowling eroded 360 degrees, 2 inches in width from* w' w4 ?( A v
center of forward leading edge.! K0 a8 @5 F. S% @$ Z! M- l
一号发动机进气道周边风蚀(2英寸宽)。' B" m( A7 `. G5 p& A
Removed erosion by polishing surface with reference to SRM---. NDT$ \8 d% D; T- P
inspection revealed 0.02 inches of material removed, remaining material 0.23
8 h7 t; k7 p- C8 \5 Tof an inch within limits to SRM---.
! [* J3 G; j9 ^: c: v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: b( {$ e( J; C& P
少0.02英寸,尚余0.23英寸,在SRM—规定的范围内。
/ k" N1 f% S6 s8 j7 N. t2 {: C3 C , S( T6 p# ~4 c# Q, E; w* t
(24) mildew: 发霉# N7 f' M4 ?( D4 A" ]7 l1 B2 S1 o3 N
A fungus growth.$ i8 W2 ~* V9 n
有机质滋生霉菌而变质,常见白色的生长物。
! \/ m. w7 v3 }8 rFor example: Forward cargo compartment insulation blankets in after floor area are moist# A0 @9 y- ^' e n8 Z8 O0 H! G3 H% a
and have mildew.; o! A7 u. \& R
前货舱后部区域隔热棉潮湿发霉。7 t* k6 i* N+ U5 }& g
Eliminated mildew and moisture of forward cargo compartment insulation
' C# {) }. E9 x0 E, Xblankets in after floor area by fabricating and installing new in accordance with% Q% S; l" W% W* J; S3 S
SRM--- and AMM---.$ \+ c {* e2 F4 V* R
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
2 |, ]. B& W' l; p4 C发霉的隔热棉。
- Z4 H) i+ g; x4 [
7 P! N+ `: o6 Y: o3 K" X H3 w4 t(25) delaminate: 分层. u6 n- s5 C7 @' t+ }8 D4 `
The act of separating into layers.' y& _- o! v; r9 P& ]2 O( g9 l
压合在一起的材料互相脱离或分开。2 k7 Z% k8 S' V" e3 S; F
For example: Nose radome delaminated from impact of “bird-strike”.
) e! p' Z7 E i+ \, w6 I 前雷达罩因鸟撞导致分层。
0 o; U W3 J& F$ u Removed delaminated core section and replaced with new with reference to
& @/ P. i2 `' G" K# eSRM--- impact test carried out. Nose radome OK for service.
# Q2 J! H9 l5 Y& R6 \根据SRM—更换分层的核心部分并进行冲击测试,检查正常。
7 Y8 J" Q3 m7 e" y; U1 Z % X% d; Z. a) ?3 U
(26) deteriorate: 老化
! E( j6 v4 G! Q9 r7 bThe diminish or impair in quality, character, or value.
9 E5 i8 U. S; {! k+ Q3 ^) Y" u橡胶、塑料等高分子化合物,在光、热、空气、机械力等的作用下,变得黏软或硬脆。
8 B7 d! s8 d6 K, O C- kFor example: Number 2 engine to pylon fire seal deteriorated.$ ?" c0 w5 S# k0 O
二号发动机吊架防火封严老化。4 Y W! t( ?: @; _$ H7 B
Replaced number 2 engine to pylon deteriorated fire seal with new seal in* h/ K( y7 z2 z2 P4 x
accordance with AMM---.* V, x# j+ z+ |
根据AMM—更换二号发动机吊架防火封严。
, ]: h+ a0 O0 h4 g 2 z8 z' E+ i' N! F( f
(27) wrinkle: 起皱
: N% ]' f, ^$ ?$ J JA furrow, ridge or crease on a normally smooth surface.
; I5 R9 z; M1 \! T( e6 k正常的平滑的表面上出现的皱纹,或折痕。# L' ~" @/ b% t4 b) M
For example: Forward galley wall at flight deck entrance has areas of wrinkled wallpaper.5 q: H# i. ~8 T/ _& f5 y9 ~6 c6 ~
驾驶舱门过道的前厨房墙纸起皱。% x# r6 D9 B8 ?1 o
Eliminated wrinkled wallpaper at forward galley wall at flight deck entrance by: W. t4 A+ q: c
replacing with new in accordance with standard practices and AMM---.9 d/ p$ X8 ]) g4 o5 i' C
根据AMM—更换驾驶舱门过道的前厨房墙纸。
V8 ?+ ~/ X) A% q, ]4 H# k1 Z. M- h 3 _( c* }- q5 j0 O# I1 y4 z2 v5 o
(28) saturated: 受潮
6 a$ F0 o$ {/ C0 A* GSoaked with moisture.- Q% ?. s" T) S; U" x
物体吸收了水分的状态。! W6 z7 [6 V. y- a& q
For example: After cabin floor carpet between lavatories B and C is saturated with water.' _' d( q; k' A- e1 D1 I
后客舱厕所B和厕所C之间过道的地毯受潮。
! E( C1 P9 l. l+ n7 |) _ Eliminated saturation of after cabin floor carpet between lavatories B and C by& Q6 H- T/ g' i+ l3 P; h8 M
replacing with new in accordance with standard practices and AMM---.; j1 d! v8 Y0 L3 n8 F4 y
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。
% u9 A2 f ]% \/ k! j2 @ ; N, {2 ^, f( I3 `3 y0 M
(29) tear: 撕裂
/ K% k8 e# K7 U" Y0 j) MTo pull apart resulting in a tip.3 K) `; i1 V" {3 P, k3 ?
裂开后分离。
" N* K& i/ g, w# j9 h& t9 nFor example: Number 8R window shade in main cabin has a tear.: _. S' s- A3 x/ g7 D; I5 B
客舱8R窗户遮光板撕裂。$ ^: G7 b" R$ K; f1 t# \
Replaced number 8R window shade with serviceable window shade in
* ?$ X/ d7 @- t3 x/ }" @accordance with AMM---.
0 R X* O9 U& }! m根据AMM—更换客舱8R窗户遮光板
n6 ?0 {0 N' q5 E 2 X- a9 ]2 I) G, g" C5 P! ]6 F
(30) worn: 磨损/陈旧8 J5 k% l- R6 }/ |; k/ Z2 [
Unserviceable due to excessive wear.; X! r: D4 }% f% }
由于过度磨损而不可用。
. D1 s3 f4 A" e1 {. D* ?6 `For example: R1 service door upper guide and door latch on doorframe is worn.1 y3 [+ @6 ^, w' ^% [ G- P& C
R1服务门上导轨和门框的门闩陈旧并且磨损。' T) Z5 G$ c5 |! p$ Y- }2 l k
Replaced worn upper guide and door latch on doorframe in accordance with7 a- Q3 y! x- p6 k A4 Y4 ]% {! l
AMM---. Operational and functional check good." ^1 v- ^% _5 O3 g3 |
根据AMM—更换上导轨门框的门闩,功能测试,操作检查正常。1 d1 i* M3 y, g; W# R: S/ e
$ `) \ k9 ~+ c5 w7 i(31) be not adhered: 脱胶1 ~) }. K' G8 K" B% @+ g
Unsecured and not positioned in place by glue or sealant.
$ U0 f$ E: Q: \6 o因附着力减弱导致脱开。 l6 H0 k' _4 v2 h' x4 S/ l t
For example: Left emergency exit hatch external “EMERGENCY EXIT” placard is not0 M. `! m/ A* a' a* k, m$ O/ m( x8 a
adhered in place.4 x6 n/ m# |/ A1 i
左紧急出口舱门口盖“EMERGENCY EXIT”标牌脱胶。3 J, e. ^0 w" s( V2 P; R
Resealed left emergency exit hatch external “EMERGENCY EXIT” placard in& @ P6 B# h4 m5 K
accordance with standard practices and AMM---.* a0 t. E; @5 n" s* G
根据标准施工手册及AMM—重粘左紧急出口舱门口盖“EMERGENCY
2 j! O, w R5 x- P nEXIT”标牌
* h: A! g8 _5 f4 Y# J6 p , m' K3 n6 ^/ s- f
(32) burst: 爆裂
* c* M" Q5 C) M5 i! `. `To open and suddenly come apart from internal pressure.
4 ^5 E/ G4 z: O2 _/ X因为内部的压力突然炸破或剧烈的爆开。
! V. i, M Q0 @+ G( Z8 pFor example: “A” system hydraulic pressure line located in forward left wheel well burst
& R) `: b- T8 |during landing gear functional check.
1 [5 X! s0 i3 d" ^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。( e8 D; E) P, `
Detailed inspection of “A” system hydraulic pressure line,revealed grommet
5 X y' z! H) f: o4 wof retaining clamp missing resulting in chafing. Installed new “A” system
2 p' d8 X% i& S2 I9 H2 k+ y) Hhydraulic pressure line and clamp in accordance with AMM---. Operational
0 J6 z5 a: ?) W! i and leak check good.
6 r h, o0 h1 i( p 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
9 P, C3 d, w7 U1 j' 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2 t3 j1 s2 s5 @. d
漏。
4 N. y- K% c9 \8 C, B+ v! t ; P) g0 S! w9 n a1 I
(33) cross-thread (pertain to plumbing) 滑丝(限于管路)
( C# t( h$ ?. l2 O" E, [# E7 B8 A9 v$ KTo damage threads to an unserviceable condition.
8 Q4 {/ o% T2 z3 f螺纹损坏后不可用。
5 A7 x. X/ T5 |& x5 ^For example: Left wing number 1 ground spoiler actuator hydraulic pressure line has
/ R4 @1 ^8 g4 y, fcross-threads at “B” nut.
( j% o3 G0 j# O& Y* U7 p左大翼一号地面扰流板作动筒液压管B螺母滑丝。
1 a, o3 j, j, W& SInstalled serviceable hydraulic pressure line at left wing number 1 ground; _( _. W5 c7 {. ~8 D/ Q+ m4 w
spoiler actuator in accordance with AMM---. Operational and leak check good.
* `* P$ m: Q7 H9 `( G" t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,$ |) h' i l* Q) G9 \4 Y Y* y
无渗漏。( D& W5 ~- j. G4 Q% q. B" H
; G: N' n. x# z# i! K A$ C! S' Y
(34) twist: 扭结/弯曲8 h( D# L+ a3 d. Z
To alter the normal aspect resulting from torsional stress or strain.: w$ U+ ~" [8 f h9 ?( @
因为扭曲的压力或者张力导致改变了正常的面貌。
$ b* c: ]0 v, |- e& G! eFor example: Right environmental control system intake door linkage twisted along routing
. a& u( p% |& v* a% G0 k# x- Rto exhaust louver., H% V/ _& K: P0 ~8 S" w
右空调系统进气门传动连杆朝排气口的方向弯曲。
3 n" f& V# b( f$ O& e. KDetailed inspection found broken bolt at eyelet connected to exhaust louver.2 o0 K" S+ ?* a9 S, @" P$ j
Replaced broken bolt with new and reattached eliminating twisting with5 G% y& O% s5 L i8 U
reference to AMM---. Operational and functional check good.
, L" l2 X" P4 O" _" P) o$ p3 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
2 X1 m% _* k1 |; u常。
3 X1 s( Z# U1 `, f' q 3 l! r' [# b- E( y3 Q
(35) leak: 渗漏2 D1 {6 i0 L: Q2 X' }% [
The escape of a liquid or air in a system.5 s! o) ]7 e' F/ j5 u$ H
系统里的液体或空气逃逸出来。
* i ?4 p: [( ^% C ?/ }' N* r k6 mFor example: With reference to routine task card 37-265-1 pilots pitot static probe test failed o9 H3 d3 M; \3 J4 O
due to leak in the system.
2 E$ N# L& }+ P. i; {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。
2 E" ^0 X+ R- Z4 l8 w/ IDetailed inspection found loose connection at pilots static port. Removed “B”; I1 J' x7 ^! S' f3 s* d3 m# J6 @
nut and inspected with no defects noted. Reassembled connection and leak
7 S9 S+ O% H$ s5 ` check good with reference to AMM---.2 c- k6 |7 H6 {1 y 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4 @# M( c& @5 m5 u/ _0 h0 s* E- Y
陷,根据AMM—重装接头,渗漏测试检查正常。
+ v8 w& g7 K1 Q' X 2 y% G9 ~( j: n$ X# E
(36) obstruct: 堵塞
m$ e! ^! e, x3 X1 {/ t/ ?5 _Blockage by foreign matter.. R& j3 y8 V% [: U" I
外物妨碍管道的通畅。1 Y) g2 v& y+ L6 A r" v. C
For example: After lavatory service panel inoperative, suspect obstruction." f* l; R9 d' E; V
后厕所勤务面板失效,怀疑有堵塞。
$ e8 {0 Z! U# s1 a Detailed inspection revealed drain system plumbing obstructed with foreign matter. Cleared foreign matter from drain system plumbing, operation check good in accordance with AMM---.8 V8 X0 a/ _2 b* U9 D( X" F
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。4 b$ @4 L, E. R4 _+ {/ U0 `
( ` V, X6 C2 {
(37) contact: 相碰 ' T+ U" O+ b( X) B
Touching of two surfaces or objects.
( z7 o. _2 L y两个表面或物体的相碰或搭接。7 ?( x8 [9 G6 f4 {( ~2 t0 d& j. m
For example: Left wing trailing edge has aileron control cable contacting pulley bracket at. ? M) t( H* Q$ D- s0 q. U* V2 a4 U
WB Station 245.9.7 d( o5 m+ b- E+ ^ q
左大翼后缘在WB位置245.9处副翼控制钢索和滑轮架相碰。
_/ I( I6 J( `8 h# ?4 j `Detailed inspection revealed pulley bearing worn beyond limits. Replaced with
1 J7 R5 R0 M t5 ?2 }new pulley in accordance with AMM--- travel and clearance check OK.
2 Q! m$ f+ g# I; Z4 _* x; A7 }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
! o. j6 e+ x% H- _' o# x间隙正常。4 X, ?' x! _% Q) C! N5 a# r9 O p! ~
; b* _/ W E, c' D* p0 Z
(38) fray: 断丝/磨损
, v' P4 _- d, K+ Y! T( fTo wear away by rubbing.4 J4 i/ Q5 T8 @, I+ M, |0 [7 e% E
因相磨或反复拉伸导致的损耗。
0 W5 u, N! e+ ]6 BFor example: The lanyard attached to the after end of the right access door to the APU
) }. a& {& N2 M. w( @3 ?compartment is frayed.
- X: A. w+ }3 D右APU舱门后端系留绳断丝。
- w1 a: r" w5 _( Q* MRemoved and replaced frayed lanyard in accordance with AMM---.
h4 {9 h" b; Z& Y. k: E* Z! Z A) w& k根据AMM—更换系留绳。' B2 n+ J- Z& i2 U
* Z7 K; l( B+ j4 @) C9 B; G
(39) fused: 熔断
7 V8 b7 a v0 I/ \6 ~To become united by melting from heat.: j. E% ?, z: k
因为高热而融化连接在一起。
0 |1 h" _ F% zFor example: After galley coffee maker inoperative. Detailed inspection of after galley coffee
1 i$ O# u7 H5 o5 e0 N% ~maker revealed thermostat wire D34768 fused to temperature controller wire G, @, L6 {' I6 e
E57689.
: m0 W1 _' U8 u0 N- F# k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
* q, {( k2 u" h- J, N6 f: f# R置导线D34768与温度控制器导线E57689熔断在一起。+ ^, M4 {. C! O$ t1 t$ ~! E
Replaced wiring with new, operational and functional check good with; d: m( G! `6 W1 @9 t
reference to OHM---.. r |, i& ^8 `: w; o
根据OHM—更换线路,功能测试正常。
$ R9 Q4 F L; T( i2 s
, ^8 q; `; x7 m$ J4 T0 n(40) bend: 弯曲
% L$ a2 `+ U8 h" H2 ^Altered from straightness or original position.
6 ~9 Q0 c: R1 G* J+ T/ H" Z- j' s! v1 y改变平直或者原有的形状。
, ?9 r% H% c% R6 PFor example: Forward electronic bay door left hinge bent.
% p( S( m- D% w3 x4 { 前电子舱门左铰链弯曲。$ H/ v. u* Y: o7 U& a
Replaced left hinge with serviceable hinge on forward electronic bay door with# c# I8 q: e6 N: p b
reference to AMM---operational and pressure check good..
- P* a3 j7 K: y' y) k W& v根据AMM—更换前电子舱门左铰链,功能检查正常。1 Y, Z$ v4 Q, L) Z8 p
) ^' D6 W' s; ^3 q) w- [( k1 X
(41) disconnect: 脱开! K; r; k! T7 Q" L
Not joining resulting in failure.
7 Y0 o1 i% V; O. ?4 J @% Q6 K因没有连接而失效。/ c7 x/ I ^& L) }0 z) R
For example: Left environmental control system pack temperature control has disconnected, u; T0 q2 @$ [/ N2 l! ~2 D" G
cannon plug.
1 I) [( F* S0 p3 ?; ^4 Y3 P左空调系统组件温度控制插头脱开。
# f/ v; \2 u# g% h; R) t& R* QReinstalled left environmental control system pack temperature controllers& Z; o1 X9 t, F: {3 S% J) A9 _- j
cannon plug, operational and functional check good with reference to AMM---.
8 c0 {3 c) ~6 u$ M) f, M/ _8 S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
# I7 r" K" C3 i1 W5 j; O. v' z查正常。
7 c( Q" E! K2 g- E" k! C
4 g0 q0 @- ]$ T8 k# F(42) missing: 丢失, E) X. z- Q9 @! o
Not present.
& a6 F( h9 y/ I) w0 T 不在位。) ~/ k, \' ]0 j
For example: L1 entry door has 3 each door stop pads missing at the after middle section of
- g2 \, Z+ T2 N; b' pthe door frame.0 B8 I+ O$ q/ G7 j( p4 Q
左1号登机门后门框中间位置有3个止动钉丢失。
2 p4 D- d+ `( b4 W. pInstalled 3 each door stop pads at the after middle section of the L1 entry door
: f# v5 i! F5 Y# L- m+ Nframe in accordance with AMM---.
( P7 n2 G, W r$ {! [0 b, J根据AMM—安装左1号登机门后门框中间位置的3个止动钉。6 w9 ]* `6 W7 E. E
+ b! k% t. i7 k0 R8 o& p3 I- z
(43) loose: 松动/松脱
# m5 a( n" ~1 q4 ^; ]# f6 ~Not secure.+ e1 V4 U8 \. M3 k
没有紧固;活动
" z0 P8 E4 w+ Q* }For example: Forward right wing to body fairing has several loose screws.2 M+ Q% t6 N# l, D) P
右大翼机身整流罩前部有几颗螺钉松动。
0 r+ m% [# N' [4 L Found 17 screws loose. Tightened loose screws with reference to AMM---.0 M" o0 b) C1 |8 l2 r Y! Z) {2 ?
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。' S6 \" j% i& U
$ a0 H m* \9 b' B4 B+ d
(44) not secure: 未关(扣、夹、卡)紧3 B/ H$ C4 e" F# s
Not fastened, to make firm or tight.$ _4 `6 x; P. E! h6 z; L
没有扣紧,(使)紧密。 P( _! w( F) n$ v
For example: Number 1 engine cowling; number 3 latch is not secure.
7 t( {: o B7 n: v 一号发动机整流罩的三号锁扣未扣紧。 . a* |! ^, R! A+ P& P8 N
Number 1 engine cowling; number 3 latch has damaged hook. Replaced
+ R4 S. N$ _% h1 i w( u' ?& Y# k8 fnumber 3 latch with new part in accordance with AMM---. Operation check
1 e7 i& ~9 W# ]5 H/ iOK.- V4 @/ f) ^ H9 C. X. {
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,& O0 S4 E0 r9 l1 e. n! {
操作检查正常。- i: \; U$ l6 R6 N, m* A
* }+ w9 V6 l% C- E/ a, a(45) inconsistent: 不均匀
$ N* p# t4 v- C3 _Not in agreement, erratic' j( V: ^- c5 r) Y5 J# E+ E+ C
缺乏连续性。
8 I+ r7 X/ v1 n. C: n SFor example: Left wing-to-body fairing seal is inconsistent in relation to fuselage.+ H; M1 X- {: c' m& H8 P' w
左大翼-机身整流罩封严胶不均匀。( g6 B) y8 f6 g2 U b& K
Re-sealed the left wing-to-body in accordance with standard practices and3 g6 ~7 y* \8 `& F
AMM---.
1 l* l1 Z B7 x$ B9 u3 S 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。
0 N/ m4 `/ V# a9 {4 n% V 3 _4 p2 X6 B9 d* y
(46) exposed cords: 见线
+ Q0 q: I+ R: P$ i \0 fVisual tire cords.* c' Y% e* T$ l: L% R
轮胎编织线裸露。
7 j) \7 `( u/ n; b6 t" aFor example: Number 3 tire has exposed cords.
4 K8 `( I) k) t' h% M 三号轮胎见线。# |" y$ ~, t1 G3 C
Replaced number 3 tire with exposed cords with serviceable wheel assembly in! c* e3 _- a, P: i1 z6 C: ?' T( n' U
accordance with AMM---. Pressure check normal./ U) T1 O8 R* W. x$ j( E
根据AMM—更换三号轮胎,检查压力正常。- Z& G1 H, w. p. Q
2 ~: ? u# g! G
(47) bald: 磨平
) b: O3 Y! T! W) eLacking a natural or usual covering.3 ~9 V' V( I& O
轮胎表面排水槽由于磨损而消失。& L* Y& G0 p' d- Y5 k. P3 f2 E
For example: Number 3 tire is bald and requires change prior to flight for no serviceable
8 |* T2 D& Y- W. n3 d3 @spare at scheduled flight sector out stations.
8 O& }+ d' d, k$ q4 _3 A- t& X9 L三号轮胎磨平,因下一航站没有备件,请在航前更换。! S5 l- X# B# h5 _5 ~
Replaced number 3 tire with serviceable wheel assembly in accordance with
" g6 `, g n( e; @AMM---. Pressure check normal./ M7 N C1 V x3 j
根据AMM—更换三号轮胎,检查其压力正常。
' d+ U# q+ j* {, ~2 g ! s: p6 S. p3 k
(48) insufficient-air-pressure: 气压不足
& w$ }6 X9 M3 UAir pressure does not meet manufacturers requirements.
# p1 e- r# [1 D0 N5 _- U空气压力没有符合生产厂家的要求。- S& F3 G8 S* b5 r! I. r
For example: Number 1 tire has insufficient-air-pressure.
" b! _. M6 Q0 u. s0 z7 a9 G 一号主轮气压不足。
7 w- R! A& q+ S7 L- T3 M7 @" y Measuring air pressure revealed 5 psi. Air pressure required within limit as" j" ^' y0 b# p" C
called out in AMM---. Serviced number 1 tire with Nitrogen as referenced in' d# Y: w D2 e
AMM---. OK for service.' \8 G" D$ G2 ^* R' y
测量一号主轮气压为5PSI,根据AMM—对一号主轮充氮气至要求。: K& {: s3 K0 s) A, l
8 `. N2 d" G( @8 y; }
(49) expire: 过期
* ~' g9 B# o$ v C9 H. JTo come to an end or terminate. x0 P8 v. {! Q0 D
超过时限、期限。8 d8 y3 ]3 N7 ?/ N9 a+ n
For example: 2 each life vests located at L2 entry door flight crew station expired.
) V" @ k5 C( n. }: Y& s9 X 位于左2号登记门机组人员位置的两个救生衣过期。1 g4 n6 p# n* w, h! H$ i. c0 f& S
Replaced 2 each life vests located at L2 entry door flight crew station with
' p+ H7 x* A7 D7 V9 {0 rserviceable life vests due at 9-2005 with reference to FAR 121.6.5 B, K) J5 V/ Z* o5 w
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
}& A- d2 u( H衣。. b4 F) ^. [( t3 ^% N3 I8 d
5 V! a' a! ^1 K0 r; n! u. J9 E$ ?2 H
(50) illegible: 模糊& D+ Y, `' e# z' F+ P
Not capable of being read or deciphered.
% g# r7 ~5 a2 z5 P8 P难以辨认的,无法读出或解释的。) p7 F9 }5 t$ R* l; n( P5 s( z
For example: Left over wing external emergency exit hatch “EMERGENCY EXIT” placard
/ m! r8 r6 w) Y% V' u j& }3 `0 J' |" Sis illegible.
4 M; ~+ R% H" E3 U$ F+ n* G% [& P左翼上紧急出口舱盖处的“EMERGENCY EXIT”(紧急出口)的标牌模糊。
& t) S; J* B7 YRemoved and replaced left over wing external emergency exit hatch
" H$ F8 }1 X+ [8 N8 ]“EMERGENCY EXIT” placard with new in accordance with AMM---. f9 N. g' c6 f8 ?
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。
- z H# b3 |# V7 a+ |5 C2 {: {" v
5 U6 [- ?4 n# p$ ?7 ?+ ?(51) damage: 破损/缺损
* k# R0 J! T. W! ? Q, {Not useful or functional.
8 m* i, \% l' h/ ^不能用或者功能失效。
% L! _* @, f, _, {2 _For example: Left wheel well landing gear door “NO-STEP” placard damaged.3 A- L$ M$ y' ~5 a
左起落架门的“NO-STEP”标牌缺损。
+ r' w+ ]+ X" R Replaced damaged placard “NO-STEP” at left wheel well landing gear door.
% k9 r' Y8 n) U3 g; l( z% I 更换左起落架门的“NO-STEP”标牌。6 n( i) x( I( X' n4 T
. v' q4 X: d5 Z9 w(52) lifting: 翘起
' o @2 s- C9 B& y3 b4 I) ?; _To become raised, not intact.
% r2 V2 z* Z9 \$ \" O没有紧固;活动
/ S. {5 }9 P, m2 P P6 E) O! FFor example: R2 service door escape slide operation placard is lifting.3 I: d' V/ \" `" `0 t( W
右2号服务门逃生滑梯操作标牌翘起。7 _ J/ }, Y5 g- L' P" M, X6 L3 k
Removed lifting R2 service door escape slide operation placard, cleaned and' X# W7 ^# B5 v3 \- L5 ^4 Z4 |5 E2 B
re-adhered to in accordance with AMM---.
, i4 c" B1 O) ~) N. 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
( T# a w/ i9 _该标牌粘好。! q4 k# ]" S/ w4 `6 [2 A2 I, ^: w
4 M2 v0 R6 N) t7 d
(53) not properly sealed: 变形/密封不佳
* ?+ {! M( t3 n: a J: h# GRetaining package torn exposing contained contents.; T5 v, \ I# o- |1 y* v5 Y
固定的包装撕裂而露出里面的东西。0 B$ o$ J) y4 {+ j, {0 E
For example: L1 entry door flight crew station portable breathing equipment not properly9 o& }& c/ R: `
sealed.
2 |2 i1 F( O8 d- ~" M& g, s! E+ A左一号登记门机组手提防烟设备变形。
`7 R) @0 r3 v$ I$ c( X oReplaced not properly sealed portable breathing equipment with serviceable
- O2 b- X# z( u! V9 L6 K$ Oportable breathing equipment with reference to FAR 121.25 as required for8 P) j% I, j# y( y
dispatch . Tagged and routed unserviceable PBE to MSC to return to customer.% Q+ a2 F8 D# f) M+ ?
根据FAR 121.25放行要求,更换变形的手提防烟设备。旧件挂牌送航材处
& s% q% {4 e9 w6 P理。; J8 m0 w& h& C" k+ C$ ]$ G
/ j, p! b5 o. m+ a0 Z8 v+ t! i* g(54) not properly packed: (滑梯)散包( e5 _0 F* q# o( n& F
The condition of a released slide.
( d" V( f% X: C7 C: z滑梯包散开的状态。9 a% s! S* p6 V, g; A, L
For example: With reference to reliability work order and task card 25-456-01, replace R2. F$ h! K6 ]" z( M4 D
service door escape slide, provided escape slide from workshop S/N 4321 is not
; m# E; k H4 l6 S3 X$ Sproperly packed.- T1 X' i/ i* e6 j6 z+ ?
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
$ G' `# Q3 c, X/ i+ E9 m3 Q7 [车间提供的(S/N 4321)件已经散包。7 ]$ e% m& L; T4 w7 ~5 L# P0 j
Tagged and routed emergency escape slide S/N 4321 to MSC to be re-pack in* @5 _! r' }0 s; s( _
workshop. Obtained serviceable emergency escape slide S/N 8765 and installed
- ~) p* y" k; X! A, @( fat the R2 service door position with reference to task card 25-456-01 and1 }. w! ?2 d3 R
AMM---.
: s! P! E+ [+ g4 i3 ^; x/ O4 ~7 j 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
2 S: q6 I: E7 Z! s% l# B25-456-01及AMM—在右2号服务门安装序号为8765的紧急滑梯。
* v' L! m6 ~ U$ Q9 J+ s/ M4 e) ]& j1 a
3 {( a2 p9 y# r5 g7 l5 m8 J(55) dirty: 脏: p0 Q$ Q0 Q- o3 P( ^% }( k
Unclean, soiled with dirt, grease etc., Y$ \7 ]0 K( n6 T( X8 q C8 f
不干净,有灰尘或油渍。
7 e8 t$ q m; a- ^' CFor example: Flight deck external window are dirty., x I2 f% P+ H2 t4 R
驾驶舱外层玻璃脏。
- p" o9 @8 D# K+ k k& F) Z Cleaned dirt from flight deck external window in accordance with AMM---.
9 U G' ]( ] t, j, ^根据AMM—对驾驶舱外层玻璃进行清洁。
! M( L3 Q; A/ \0 V
( V A! K- }- c- B2 y(56) fracture: 断裂
* w* N$ w% w& `6 H$ Z- j6 pA break, rupture or crack.
) }0 q& F2 k9 ^6 g `& g! Z破碎,破裂或裂缝。6 [ {: X& N% O2 L% B: }" N x- ?
For example: Reference Gameco routine task card 53-004-12, NDT X-Ray inspection at right- L9 v" u. o1 a) Q1 h
wing emergency exit hatch frame revealed 4 inch fracture at forward lower sill.
! F, I+ L$ t5 j" x' ?参考Gameco例行工卡53-004-12,NDT进行的X光检查中,发现右翼紧! Y" H; W) r9 T( ]' H7 N5 Y+ k
急出口舱门框前下角断裂(长约4英寸)。6 r2 z2 F: Y) G
Repaired fracture with permanent repair in accordance with SRM---, attached6 t3 N! M( L9 Y7 W/ m
Gameco engineering order 53078-4, and attached Boeing TELEX 53-0987-1.
' S: {# Y0 K6 [. Z" S0 tApplied protective finish in accordance with reference to SRM---.
/ Y8 o( o; L$ j根据SRM---,Gameco 工程指令53078-4及波音电传 53-0987-1,对断裂进$ }1 V& G* s* N6 r% y
行修理。参考SRM—进行保护漆层的恢复。0 M: c' |2 h: [9 b# n6 E6 Q
9 ]) O; [& d$ H# o" O
(57) exceed-the-limit: 超标; w5 ^# C3 ]+ M
Does not meet manufacturers specifications.
( o5 A; K0 n; R+ y超出生产厂家的技术标准或规格要求的范围。7 S, t" B r8 q
For example: Reference routine task card 32-098-01 landing gear functional check, nose
+ t9 c3 b A- I+ m ulanding gear doors faired to fuselage skin exceed-the-limit during functional
) `5 Y6 I9 F6 R7 a6 Ocheck.0 P: R0 [$ m% f# D. x- F) m4 t, F" o
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
$ m& A% s q5 p: x' H( P8 K架门与机身蒙皮间隙超标。
. Q8 Z3 k* _: u) i) iAdjusted push-pull control rods at nose landing gear doors to obtain proper1 C6 x# {3 q2 |% U6 t3 N
fairing to fuselage skin in accordance with AMM---. Clearance and functional
+ f' e4 T* ?5 [7 m1 ^6 Acheck good in accordance with routine task card 32-098-01.
4 f1 i3 P9 \6 T" M- N" K3 g6 A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
/ K/ Y/ d( p0 {( Q& V7 N进行功能测试,检查正常。
m4 B& x& ]6 ]5 k" l0 e
3 }0 I3 S/ O' ~- ](58) backlash: 空行程/无效行程: s7 T* x3 Y0 D8 G7 `1 A
To measure play resulting from loose connections between gears or other mechanical2 ^' e% |. f* l2 M2 o
elements.
& A5 m9 b, p' ?0 m& R+ }4 n传动装置或者其他机械元件之间连接的松动而导致的空隙。5 o' E6 B. |( Y- d. o* C" f
For example: Horizontal stabilizer jackscrew clutch failed backlash test with reference to7 _0 `- @+ j% [, b8 j3 u
routine task-card 27-0345-01.
- U/ h$ ]6 N( P按例行工卡27-0345-01进行测试,水平安定面蜗杆离合器有空行程。9 `) J: b$ I! M9 s4 n9 r/ d# v: ]
Removed horizontal stabilizer jackscrew clutch. Detailed inspection revealed2 ~/ M- ]' F6 e0 [ V% s
worn clutch plates. Tagged and routed unserviceable clutch unit to MSC for- I- j' _% f1 A/ _; W$ L2 H
return to customer. Installed serviceable horizontal stabilizer jackscrew clutch
; x) h* d! D3 J+ S9 tin accordance with AMM---backlash and operational check good.
$ E* H) F" S% u& d! o; ` 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
, G; X3 v. e3 p8 ^# b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。
) ~# N H6 j- i* m5 ~, P! r9 L 8 b+ w4 x# v* B; }8 U2 ?2 E
(59) block: 卡阻/阻塞
L! C5 e9 m6 M! a9 _6 B" d" ^" pThe act of obstructing.$ v, h3 t% F0 e# L+ |& H
通道堵塞:运动部件的动作不顺畅。
) I2 R& Y6 c4 B6 L; oFor example: Forward cargo compartment door forward actuator is blocked when opening8 q1 _1 o; m% h$ {( r* S
the door.
# d, j; `* y9 Y: m# W前货舱门在打开时有卡阻。' C# B7 |$ i) a4 V
Detailed inspection revealed there was a dent on the actuator rod. Replaced the
1 y* v$ f) |5 ]6 M; l5 |/ ginoperative actuator in accordance with AMM---. Operational and functional: t$ K* E: V% g& ^: |% D3 x' F
check good.' M; L, [+ B* b$ u0 m
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,
% x2 i& S, B: D" C7 h$ K- G" A, ^操作检查正常。
) Z/ V$ U% o5 t/ q' Q) |) t5 y 7 @$ {; I- R" R) g& I
(60) bulge: 鼓起
8 E5 U% c: c1 ]8 S) @3 yAn outward curve or swelling./ c. p% U( `1 S' o) T4 j( F
向外凸起。
0 z7 X$ B' Q# G1 ~% t( W0 K* l% k' U, rFor example: Forward cabin lavatory floor panel is bulging.
6 \2 t5 P' E6 I- M% Q$ f; E 前货舱厕所过道地板鼓起。9 z$ E: I1 O" J: Q
Removed forward cabin lavatory floor panel, no defects noted. Re-adhered& a" ?) H3 P. E R
forward cabin lavatory floor panel and eliminated bulging in accordance with0 _4 P; R. {, I8 v% H
standard practices and AMM---.
/ ?4 r7 W, R( \- _: K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
; ~$ E% H2 i5 f) {3 l3 IAMM—重新粘接该地板。. w+ f C7 H5 u) j3 R$ H
0 h+ C+ j) w% E3 `. [# s8 }
(61) contaminate: 污染
, g: J' O/ |# j* O+ j9 w, eImpure mixture.
$ J! J+ _, t( k" a( y; p有不纯的杂质或异物。/ \. j5 |$ A; u/ L
For example: Fuel sample reveals positive contamination of microorganism growth.8 P! Y. g# e/ A4 M7 z( W
燃油样品检查发现有微生物污染。0 g; g: ?$ m1 ~: V0 {" r
Treated fuel tank with biocides with reference to attached Engineering Order
6 g8 a- W& R% {% p/ RG2009619.6 {/ |2 v" x6 C) c7 h+ x8 r8 E1 z# A
根据工程指令G2009619,使用杀菌剂对油箱进行杀菌处理。
4 _/ |& [1 |) `4 f$ G3 R2 M6 I
5 `. E" _9 _4 K) n$ B2 ~(62) disagree: 不一致
$ g3 e+ [0 C% lFail to be in agreement.% ?$ W+ \9 p9 G) j4 y* j8 ~
对应关系不正确。: E. }5 y8 R5 P) d
For example: Flap control lever disagrees with flap indication gauge through all detents.
q" y# R p8 s& l 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 z$ W6 L5 Y6 F% G% t+ ]
Adjusted left and right wing flap indicators in accordance with AMM---.
$ E0 j( I( w& p. [0 `Operational check good through all detents.
1 O2 I: z# _8 F. t% \- M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
) |) h5 N* S$ I$ P. x$ O7 _表指示一致。" O+ w3 a2 ]% p. f1 F6 S. r* Y* c
; f: c3 ?/ f/ C; [2 r2 G; m w* R# l
(63) discharge: (电池/气瓶)被释放
9 D/ _& }" Q, q7 B2 hTo relieve retained contents to an empty state.3 `* U' Q- P3 b# L
放出;腾空
* P- m# M0 ]5 t4 {- qFor example: R2 service door assist accumulator discharged.* d, M0 `& K f4 q4 R0 U
右二号服务门助推气瓶被释放。' Q$ ~) D/ H! N
R2 service door assist accumulator detailed inspection revealed damaged- G$ L% w% g [4 _, ?
pressure gauge. Replaced pressure gauge, serviced with dry air as called out in: S( o$ K# ]) @4 T2 ~- {' `
AMM---leak check good.
% S5 ^( L" ^% Q. m/ R: 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
( X9 p2 f a) H压力表,对助推气瓶进行勤务,渗漏检查正常。7 q; I* u" t) V# M
) Z$ m& d# }- M(64) dislocated: 装错2 o* s- }6 x# X( G' ~# `5 N
Not in proper relationship with joining part.5 K0 ?1 h& }. Z; z
零部件没有安装在正确的位置。0 x! w8 |3 f" v& N2 r; d
For example: Forward cargo door pressure seal is dislocated from retaining track along after
3 G7 I- w* }; @' j7 _, d7 b5 Y& land bottom section of door.3 R4 M7 q+ p# u( i; l9 I8 p
前货舱门后底部固定轨道的压力封严条装错。
) B# @1 A% T5 y6 I+ Y$ ]0 gDetailed inspection revealed pressure seal retainer damaged along after and
; X% o0 b- @! Pbottom section of forward cargo door. Replaced affected section of pressure0 ]& I- }! J6 q+ Q+ v1 \
seal retainer and reinstalled original pressure seal in accordance with AMM---." e& D: ^# ^$ F# y' W4 v2 v5 D
Operational and pressure check good.
; J. j2 l- |6 x7 t1 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( r( X. m$ A" d; B* I4 R
该安装槽并重装封严条,操作并增压检查正常。
4 J+ J7 e, @5 b; ^/ S! P ' w0 R3 w7 S4 _: e: d* o
(65) fail: 失效- m: P* b4 l5 A
Note: must have detailed description of failure.$ M* R0 g1 v9 N, A/ A8 F: o r$ }" n
注:如用此术语,必须给出故障失效的具体描述。; B2 r9 W+ O" s/ ]( d% e- N
To perform ineffectively or inadequately.
: O7 m8 |+ B: v9 A/ C! h& ?不能执行或不能完全执行原有的功能。, D/ d* |% o0 c- H5 I/ E
For example: 13F seat actuator failed to adjust.
' g5 ^9 r" p- P: p# _% D 第13排F座椅作动筒失效,不能调节。
7 P. w' Z+ O2 h) ^3 k7 A Replaced 13F seat actuator with new part, functional check good.
; Q- k; I7 c( w9 w/ h 根据AMM—更换第13排F座椅作动筒,功能测试正常。
8 X5 h+ a6 N' z, y
: W$ L) C4 [) i* u(66) fluctuate: 摆动) x1 T$ G9 f/ {/ J
To continually change or vary in an irregular way.1 n' m9 o1 ] F
无规律连续的起伏不定,变化。
6 R/ J3 w* F+ e& ?( dFor example: During engine run the number 1 engine oil pressure gauge fluctuates./ B. L! C! F" e# v' ^& X, ^' }2 P: T
试车时,一号发动机滑油压力表指示摆动。
w$ F6 K2 a0 H4 [3 N Replaced the number 1 engine oil pressure gauge in accordance with AMM---. Carried out engine run, oil pressure gauge normal.
6 v, H7 c( X5 n4 t' V6 ` 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。
3 C2 |" T# [ m2 o s; A
/ S# w& K/ c% e- r' Z) ](67) flutter: 抖动7 t& y; i8 f: B) O# L
A rapid waiving or flapping movement.% G5 g+ K, m. U
快速的摇动或者上下振动。
6 a* ~$ X% C3 ?! B% GFor example: Pilot report on flight logbook page 908701 fluttering sound from left side of. r6 d9 V8 o% @: E; G" L
airplane during descend beginning at 11000 feat.
9 A [- A" l+ l3 }. Y9 C) x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
9 x# n/ S6 a9 N( |3 E) ?- q) I# @侧有抖动的声音。$ o+ t3 n! g! O. h
Investigated fluttering sound from left side of aircraft as squawked on page
! S- f" ?3 L3 ]9 {6 j3 c8 J908701 of flight logbook. Found number 3 flight spoiler actuator leaking.7 L7 A! P: W: R8 D8 ? w
Replaced number 3 flight spoiler actuator in accordance with AMM---1 t$ S, |% @6 p' t6 {! k8 M0 w: [
operational, leak, functional check good. Flight crew briefed prior to flight.
$ J' \- h3 J U) a4 d5 J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。
8 T! h6 @$ ^* q
, V" Z8 O2 `; L: K" E: H& _0 \( l' a(68) insufficient: 不够/不足) I% r0 T( V# K: E8 r- t1 ~
Not sufficient, inadequate.
) @3 d( i+ P* {9 z! @达不到所要求的数量,数目。
& `0 Z* U4 i# y& N( b; L6 yFor example: Left main landing gear alternate extension control cable has insufficient+ O$ J2 V9 T5 h- f6 o" Z5 m
lubrication.
/ H D0 U0 c) R4 m3 D2 _7 u左主起落架备用控制钢索润滑不足。" Z5 O3 P8 ^' W# W; S" l
Lubricated left main landing gear alternate extension control cable with7 z. g0 @' s; m, {% Z
Aero-shell 12 grease as called out in AMM---.$ V* L5 A3 t$ G$ ` Y2 w, G5 q5 Z
根据AMM—用Aero-shell 12润滑左主起落架。8 T5 H! s( R+ a7 a% L; N
! a8 B) }1 ?8 @(69) inoperative: 不工作6 @$ Z: m6 M- M) v
Not working.) ?) c) P3 m' v( {2 D. w
不能正常的发挥功能,作用。0 R% Y* a# A/ ^; ?4 Q
For example: Forward electronics bay door indication light in flight deck is inoperative.
; ?. z' {: \! ~1 s' g 驾驶舱前电子舱门指示灯不工作。- v7 X$ O% \# Z# I+ o# P
Detailed inspection revealed 2 each bulb filaments fused in electronics bay
7 k, A5 r7 U- m9 {( I: u" m6 m" zdoor indicator. Replaced 2 each bulbs in accordance with AMM--- operational8 F7 o6 i8 D& p! Q5 U. c7 q9 k
check good.
/ `' d. V0 s6 s; h. H0 o& i" N2 l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- Q# [1 \" u8 a/ \
这两个灯泡,操作检查正常。
3 G' j( m3 Q* w1 p0 z
0 K) w1 Z* V( c5 a v(70) (not) illuminate: (不)亮/ H* T$ A3 h; o; _3 L
Not brighten with light.
1 o9 Q p/ ~2 Y" h3 E$ `% e+ ~5 R不照明,不发光。
/ P; I4 O% y9 p) MFor example: Passenger reading light at cabin rows 12AB, 14C, and 17AD, will not
5 `1 j- Y" B1 u% ^illuminate.0 _0 L" _7 }9 M) ?/ v" _+ ~
12AB, 14C, 和 17AD座位的旅客阅读灯不亮。
& i7 E* Y7 | R5 |! ^) T9 ZReplaced passenger reading light bulbs at cabin rows 12AB, 14C, and 17AD in
( ]' c% n5 n- \$ ^1 caccordance with AMM--- operational check good.* n' [3 f5 r6 Z1 v' L! _/ x a
根据AMM—更换12AB, 14C, 和 17AD座位的旅客阅读灯,操作检查正
: Q$ Y/ v+ c) H# S' |6 x常。9 J. c) \9 X2 I, F# x
' W7 C, ^5 i! N' c8 u- B# X1 q3 t(71) interfere: 干扰% ~+ c/ m% N( F& H+ A8 C0 o$ s
To come between so as to be a hindrance or an obstacle.
u) ?9 V" r) f4 P妨碍无线电设备正常接受信号的电磁振荡。! K: W1 p) }& B @9 v9 }
For example: Functional check L VHF radio revealed interference static and abnormal noise.
2 }! q- s4 j1 p( n8 ^ 功能检查左VHF设备发现其工作有干扰及静电噪音。
: E) x0 k/ |$ a9 M3 g Replaced L VHF radio in accordance with AMM--- and tagged and routed the: f) |* d0 Y* ~
removed part to MSC.3 C2 I6 [0 y( X6 ~- }, t
根据AMM—更换左VHF设备,旧件挂牌送航材。7 r' Q5 Y( R$ ]8 Z9 T
: }7 P! q0 g7 v(72) kink: 扭结/缠结
0 |4 R' L, C& K/ O4 l' |A tight curl or sharp twist.4 p2 v$ m- ^+ h
(钢索,条壮物)缠绕在一起。1 ?! U( S! A/ n3 x& s
For example: Right wing inboard flap control cable at control mechanism located in after; r. {+ ~( b, y [
right wheel well is incorrectly routed and kinked.
* I) u/ ?- Q8 F* i- Q8 \- S" c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。
: S5 l4 X' Y; f. x' P# AReplaced with new flap control cable from Body Station 760 to flap control3 b9 ~2 r3 ?$ Q; v" V
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.5 Y& N7 t2 K# a- p+ M
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。. c( t% `2 o! W! Q' j
K; Y! Q/ t0 V: y
(73) misrouted: 走向错误
8 Y. w; }9 v( a2 j( }7 F4 a& q8 L+ BNot properly aligned through a course of travel.: y/ r) J3 v9 H
在行程中没有正确对折。7 U/ X$ ]$ i& X. s( E( b$ D q
For example: Left main landing gear manual extension cable is misrouted through pulley attached bulkhead in the left wheel well.1 F# B5 N& y3 L6 P) r8 p
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
3 K& l& B/ m, z+ ~9 M6 k5 H 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.
/ w2 X4 ?9 a- ^1 p: R 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
4 z$ s4 |9 d! L7 w" x8 p. C! Q) l9 N该滑轮重新安装,功能测试,检查正常。
0 u/ f9 g7 \& `# m4 X/ R5 d' \
! ]6 N1 O7 e2 R p(74) not installed: 漏装
; {7 ^7 O" Y7 S# S: c- pMissing.. W8 j7 y, `+ j) S$ G
根据要求本应安装的零部件未安装。+ G% x: f5 ^. R, F( S
For example: Life vests not installed at L1 entry door flight crew station.
0 X2 p( u/ V5 A L1登机门飞行机组位置救生衣未安装。' Z* i, R3 z1 T5 b. \& Y$ i
Installed required life vests at L1 entry door flight crew station.
4 p; h9 s1 I8 C$ @$ `! ? 在L1登机门飞行机组位置安装救生衣。. l# W4 I6 \( _# V0 W
( o+ R6 [9 }& A. C; t2 f7 j(75) rubbing: 相磨
! y8 v2 ?7 l, lMaking contact with an unrelated surface
/ F# w# |% f! c& o1 i: u; e相对运动的两个物体表面因接触而导致磨损。
0 E; {6 G" n! oFor example: Wire harness for cabin PSU’s running through floor beam at body station 360& }7 a8 ]7 e e( ~
and wbl 21.52 is rubbing against floor beam cutout.; x: e; M3 ]5 t
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
7 r V* c$ r A- y板梁时与地板梁切口相磨。) s$ H6 @1 b+ L1 E8 z. ^6 C* q
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---. ; z T5 K, m# v" Y! b( H
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,
: j* I; { t: I! i* Z' Z( V+ q根据标准施工手册及AMM—更换并调节该处的安装夹,消除导线束与该
) c* ^& U _9 a+ u. e% y$ Y/ n处地板梁切口相磨的情况。/ q* a* F% c9 F1 d
y1 B, x% P# f# i3 y# X(76) un-lubricated: 干涩/缺乏润滑
9 y3 R+ y# @3 ~9 o: jWithout lubrication resulting in friction, heat and wear.
1 N. n2 i- k5 t* C没有润滑而导致相磨,发热和磨损。) k; d% ?! Y& X1 v9 a) I
For example: After aircraft wash, all 3 landing gears were found un-lubricated.
( h: m) \, O4 r 洗飞机后,发现三个起落架都缺乏润滑。
$ z* T8 V% k% f4 u Lubricated all 3 landing gears with aero shell 17 grease with reference to
5 Q2 ~ D& Z q3 JAMM---.6 o& W: J( N) w ^; k
根据AMM—润滑三个起落架。5 ? E+ E4 r) B1 T9 f
: m. m9 O6 ]0 i E3 t% u! ]
(77) will-not-reset: 不能复位4 i- x4 `6 d; ]+ o7 [
Will not return to its operating(original) position.
4 { Y: U* @- I/ z, {) Z' _不能回到原来的位置。0 n5 K, c' ~# P, `: O B
For example: APU circuit breaker will-not-reset." T+ t+ K' L" k, T1 |0 v" Y
APU跳开关不能复位。
$ f. |# f2 K- q/ D Detailed inspection found APU circuit breaker faulty. Replaced APU circuit
( o; P( l0 X; D, g2 c& vbreaker in accordance with AMM---.Operational check good.9 j' T. N4 q" z4 Z. ~ O5 J6 t
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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