ADAA
Validity : S / N 1 - 9999 05-00-07Page 1
(CA) JUN 01
A.D.
(DGAC) SB or SL
SOCATA U.S. A.D. APPLICATION
SUBJECT Inspection Continuous
interval
Before In
progress
89-177 (A)
R3 SB 48/3 90-02-18
Amdt
39-6619 Fuel tanks 50 h
89-183 (A)
R1 SB 47/1 90-02-18
Amdt
39-6619 Fuel system
90-143 (A) SB 50/1 90-25-17
Amdt
39-6807 Oil cooler
91-031 (A) SB 57 91-15-10
Amdt
39-7074 Horizontal stabilizer balance weight Before
each
flight
91-143 (A)
R1 SB 58/1 Catches on cabin access doors 100 h
91-144 (A) SB 59 Propeller deicing electrical circuit
protection
91-145 (A) SB 60 Autopilot control system
91-160 (A) SB 49 Frame 0 : console side panel 50 h
91-246 (A) SB 61 Fuel tank outlet filter
92-152 (A)
R4 SB 10-072-78
R2 Exhaust system
92-225 (A)
R1 SB 10-067-28
R1 Fuel tanks air vent system
93-012 (A)
R2 SB 10-071-55
R3 Rudder balance weight
94-114 (A)
R1 SB 10-075-25
R1 Front seats
94-247 (A) SB 10-084-57 Wing rib, fuel tank area
1994-266 (A)
R3 SB 10-080-57
R3 98-18-13
Amdt
39-10729 Main landing gear 1000 h
and/or
1500
landings
95-084 (A) SB 10-091-57 Main landing gear
96-143 (A) SB 10-103-25 98-04-03
Arndt
39-10316 Upper attachment of front belts
97-032 (A) SB 10-105-32 Landing gear
1999-062 (A) SB 10-099-28 Fuel system : engine control panel
ADAA
Validity : S / N 1 - 9999 05 00 07Page 2
(EA) JUN 01
A.D.
(DGAC) SB or SL
SOCATA U.S. A.D. SUBJECT APPLICATION
Inspection Continuous
interval
Before In
progress
1999-319 (A) Verification of the presence of the vertical stabilizer forward junction doubler
1999-386 (A) SB 10-112-61 Propeller governor control (ATA 61)
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