N / A Not applicable
(*) F Facultative
M Mandatory
R Recommended
(**) TI or KIT at the latest revision
ADAA
Validity : S / N 1 - 9999 05-00-03Page 14
(EA) JUN 01
SOCATA SERVICE LETTERS
SL SUBJECT VALIDITY TI or KIT
(OPT 10)
No. (*)
No. ATA
5 / Equipment warranty
11 / Parking brake hydraulic fluid tank all models TB9 - TB10 - TB20 Up to S / N 364
13 / Prevention or repair of cracks on TB20 flaps actuator support S / N 275 to 433
14 / Repercussion of TB10 fatigue tests on TB9, TB10, TB20 and TB21 airplanes Superseded by SL 14 / 1
14 / 1 / Repercussion of TB10 fatigue tests on TB9, TB10, TB20 and TB21 airplanes Superseded by SL 10-14 / 2
10-14 / 2 / Repercussion of TB10 fatigue tests on TB9, TB10, TB20 and TB21 airplanes Cancelled
Content included in
Maintenance Manual
15 / Hole for water draining off under wings on TB20 aircraft From S / N 434 except 444
17 / Engine air substitutive intake (alternate air) on TB20 aircraft S / N 1 to 444
18 / TB aircraft battery TB (CN 85.130)
19 / Bearing plates riveted on R.H. and L.H. flaps S / N 1 to 485 9100
20 71 Engine mounts - monitoring improvement Aircraft having an
engine mount with the riveted manufacturer plate
21 49 Magnetos selector - modification of a lug S / N 1 to 587
24 51 Water discharge holes under fuselage rear section S / N 1 to 771 except 656
25 12 Cancelled Replaced by SB 41
26 24 Landing gear microswitch attachment S / N 1 to 790
27 52 Catches on access doors Superseded by SB 58
28 28 Fuel selector S / N 731 to 750 except 744
29 78 Burnt gases discharge Superseded by SL
10-029 / 1-78
10-029 / 1 78 Burnt gases discharge Superseded by SB
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