N / A Not applicable
CI F Facultative
M Mandatory
R Recommended
(**) TI or KIT at the latest revision
ADAA
Validity : S / N 1 - 9999 05-00-03Page 12
(EA) JUN 01
 

SB SUBJECT C L
* A.D.
(DGAC) VALIDITY TI or KIT
(OPT 1 0)
No. (**)
No
(SB 1 0) ATA     
10-107 32 Landing gear electrohydraulic
generator R  Aircraft equipped
with "0 I LDYN E 
COMMERCIAL HYDRAULICS"
generator, P / N
TB20 61267000,
S / N 1676, 1677, 1699,1700,1707 to 1709,1716,1723 to 1730,1746 to 1800, 1802, 1803 and
1808, as well as aircraft on which the SL 10-036-32 has been applied 9230
10-108 73 TB 200 fuel flowmeter pipe M 1999-061
(A) Superseded by SB 10-108-73 Amdt. 1 
10-108 Amdt. 1 73 TB 200 fuel flowmeter pipe M 1999-061
(A) R1 N / A 
10-109 00 Technical documentation R  Superseded by SB 10-109-00 Amdt. 1 
10-109 Amdt. 1 00 Technical documentation R  Superseded by SB 10-109-00 Amdt. 2 
10-109
Amdt. 2 00 Technical documentation R  Superseded by SB 10-109-00 Amdt. 3 
10-109
Amdt. 3 00 Technical documentation R  Superseded by SB 10-109-00 Amdt. 4 
10-109
Amdt. 4 00 Technical documentation R  All 
10-110 55 Change of horizontal stabilizer
fitting material F  S / N 480 to 1864, 1867 to 1869
S / N 1 to 480 with kit OPT10 909600 or OPT10 910300 
10-111 78 Low noise exhaust F  Superseded by SB 10-111-78 Amdt. 1 
10-111
Amdt. 1 78 Low noise exhaust F  Superseded by SB 10-111-78 Amdt. 2 

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 13
(EA) JUN 01
 

SB SUBJECT C L
* A.D.
(DGAC) VALIDITY TI or KIT
(OPT 10)
No. (**)
No
(SB 10) ATA     
10-111
Amdt. 2 78 Low noise exhaust F  From S / N 1 
10-112 61 Propeller governor control M 1999-386
(A) S / N 1899, 1904 to 1909 
10-113 32 Main landing gear shock-absorber R  N / A 
　
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