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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