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9132
48 28-20 Fuel tanks M 89-177 (A) Superseded by SB
48 / 1 
48 / 1 28-20 Fuel tanks M 89-177 (A)
R1 Superseded by SB 48 / 2 
48 / 2 28-20 Fuel tanks M 89-177 (A)
R2 Superseded by SB 48 / 3 
48 / 3 28-20 Fuel tanks M 89-177 (A)
R3 From S / N 1 to 1037 9154
9155
49 53-20 Attachment of console side on frame n° 0 M 91-160 (A) From S / N1 to 1286 9152
9172
50 79-20 Engine oil system M  Superseded by SB 50 / 1 
50 / 1 79-20 Engine oil system M 90-143 (A) All 
51 71-60 Carburator air bleed on engine cowling M 90-240 (A) N / A 
52 52-40 Fuel tanks tight doors R  From S / N1 to 1173 
53 31-50 Warning lights panel connectors R  From S / N 1 to 947 except from 823 to 849 and 888 
54 79-20 Engine oil circuit R  N / A 
55 71-60 Engine air inlet filter M 90-229
(AB) R2 All 
10-056 32 Main gear door hinge R  From S / N1 to 1480 except 1478 9175
57 55-10 Attachment of horizontal stabilizer balance weight M 91-031 (A) From S / N 1 to 1030 inclusive 
58 52-10 Catches on cabin access doors M 91-143 (A) Superseded by SB 58 / 1 
Not applicable
F Facultative
M Mandatory
R Recommended
TI or KIT at the latest revision
ADAA
Validity : S / N 1 - 9999 05-00-03Page 5
(EA) JUN 01
 

SB SUBJECT CL
* A.D.
(DGAC) VALIDITY TI or KIT
(OPT (1 0)
No. (**)
No.
(SB 1 0) ATA     
58 / 1 52-10 Catches on cabin access doors M 91-143 (A)
R1 Aircraft which cat
ches last inspection
occured for more
than 100 operating hours ago or which have totalized more than 100 hours since delivery date 
59 30-60 Propeller deicing electrical circuit protection M 91-144 (A) From S / N 948 to 1176, plus from 823 to 849 and 888 except 958,964 and 1124 equipped with OPT C522 20M "Propeller deicing" 9174
60 22-10 Autopilot control system M 91-145 (A) Aircraft equipped
with one of the following options : From S / N 275 to 947 except 823 to 849 and 888, OPT No. 066800 M, 066810 M,066900 M and 067000 M.
From S / N 948 to 1222 plus 823 to 849 and 888, OPT No. G66800 M,
G66900 M and
G67000 M. 
61 28-20 Fuel tanks outlet filter M 91-246 (A) From S / N 1038 to
　
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