ADAA
Validity : S / N 1 - 9999 05-00-05Page 1
(EA) JUN 01
SIL SUBJECT VALIDITY
No. ATA
SIL 10-012 32 MICHELIN tires
SIL 10-013 00 SOCATA fleet follow-up
ADAA
Validity : S / N 1 - 9999 05 00 05Page 2
(EA) JUN 01
SOCATA TECHNICAL INSTRUCTIONS
TI SUBJECT VALIDITY SB r L
No.o (* S)
KIT No.
(OPT 10) ATA (1)
9074 F / E New voltage regulator LAMAR BOO 371-5
9075 F / E New starter relay RBM 70 112 225 5
9082 F / E Reinforcement of frame 1 in wing attachment zone for aircraft TB20
9085 F Locking improvement of access doors
9086 F / E Change of rear flight control supports at
frame 9 S / N 1 - 450
9087 F / E Elevator tab actuator housing for cable-type control S / N 275 - 340
9088 F / E Improvement of fuel pump drainage SB 22
9090 * L.H. wing tip - Spare parts from S / N 275 to 425
9091 R.H. wing tip - Spare parts from S / N 275 to 425
9092 F / E Reinforcement of frame 4 S / N 1 - 433
9093 * Locking improvement of oil inspection door
9097 * Addtion of centering rings on upper cowl
9098 * Addtion of centering pins on lower cowl
9099 * Manual control of intake air box flap
9100 F / E Friction plate on flaps Superseded by OPT10 9100 Amdt. 1
9100
Amdt. 1 F / E Friction plate on wing flaps S / N 1 - 478
9101 * Sound proofing improvement
9104 * Trim control attachment on elevator tab levers SB 24
9106 * Additional equipment for trim control
attachment on elevator tab levers SB 24
9111 F / E Installation of radio master switch
9114 F / E Engine controls panel RICHARD & PEKLY S / N 275 - 524
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飞机维护手册 05 时间限制维护检查 1(24)
