| Number |
US-2011-10-09 |
| Issued by |
 United States of America |
| Issue date |
2011-06-14 |
| Effective date |
2011-06-17 |
| EASA approval number |
|
| ATA Chapter |
51 |
Approval Holder
/ Type Designation |
-
TEXTRON AVIATION INC.
-
150
-
150
-
150A
-
150B
-
150C
-
150D
-
150E
-
150F
-
150G
-
150H
-
150J
-
150K
-
150L
-
150M
-
A150K
-
A150L
-
A150M
-
152
-
172 (Skyhawk)
-
172
-
172A
-
172B
-
172C
-
172D
-
172E
-
172F
-
172G
-
172H
-
172I
-
172K
-
172L
-
172M
-
172N
-
172P
-
172Q
-
172RG
-
175
-
177 (Cardinal)
-
177RG (Cardinal RG)
-
180
-
180
-
180A
-
180B
-
180C
-
180D
-
180E
-
180F
-
180G
-
180H
-
180J
-
180K
-
182 (Skylane)
-
182
-
182A
-
182B
-
182C
-
182D
-
182E
-
182F
-
182G
-
182H
-
182J
-
182K
-
182L
-
182M
-
182N
-
182P
-
182Q
-
182R
-
R182
-
T182
-
TR182
-
185 (Skywagon)
-
185
-
185A
-
185B
-
185C
-
185D
-
185E
-
A185E
-
A185F
-
188 (AGwagon)
-
188
-
188A
-
188B
-
A188
-
A188A
-
A188B
-
T188C
-
206/U206 (Super Skywagon)
-
206
-
TU206A
-
TU206B
-
TU206C
-
TU206D
-
TU206E
-
TU206F
-
TU206G
-
U206
-
U206A
-
U206B
-
U206C
-
U206D
-
U206E
-
U206F
-
U206G
-
207 (Skywagon)
-
210 (Centurion)
-
210
-
210-5 (205)
-
210-5A (205A)
-
210A
-
210B
-
210C
-
210D
-
210E
-
210F
-
210G
-
210H
-
210J
-
210K
-
210L
-
210M
-
210N
-
210R
-
P210N
-
P210R
-
T210F
-
T210G
-
T210H
-
T210J
-
T210K
-
T210L
-
T210M
-
T210N
-
T210R
-
336
-
337 (Super Skymaster)
-
337
-
337A
-
337B
-
337C
-
337D
-
337E
-
337F
-
337G
-
337H
-
M337B
-
P337H
-
F150
-
F150F
-
F150G
-
F150H
-
F150J
-
F150K
-
F150L
-
F150M
-
FA150K
-
FA150L
-
FA150M
-
FRA150L
-
FRA150M
-
F152
-
F172
-
F172D
-
F172E
-
F172F
-
F172G
-
F172H
-
F172K
-
F172L
-
F172M
-
F172N
-
F172P
-
FP172D
-
F177RG
-
F182
-
F337
-
F337E
-
F337F
-
F337G
-
F337H
-
FT337E
-
FT337F
-
FT337G
-
FT337GP
-
FT337HP
-
FR172 (Reims Rocket)
-
FR172E
-
FR172F
-
FR172G
-
FR172H
-
FR172J
-
FR172K
-
P206/TP206 (Super Skylane)
-
P206
-
P206A
-
P206B
-
P206C
-
P206D
-
P206E
-
TP206A
-
TP206B
-
TP206C
-
TP206D
-
TP206E
-
R172 (Hawk XP)
-
R172E
-
R172F
-
R172G
-
R172H
-
R172J
-
R172K
-
T303 (Crusader)
-
T337
-
T337B
-
T337C
-
T337D
-
T337E
-
T337F
-
T337G
-
T337H
-
T337H-SP
|
| Revision |
Not applicable
|
| Correction |
FAA has approved Global AMOCs for AD 2011-10-09, as made public in SAIB CE-12-14 dated January 25, 2012. As these AMOC approvals meet the criteria of ED Decision 2004/04/CF, article 4, the alternative methods are automatically EASA approved and therefore valid for application on the affected aircraft registered in Europe. Copies of the FAA AMOC approval Letters, references L115W-11-804, L115W-11-986 and L115W-11-1109, are attached to this record.
|
| Supersedure |
This AD supersedes FAA AD 87-20-03 R2 dated September 5, 1990; and DGAC France AD (CN) 88-123 dated 3 October 1988.
|
| Publication(s) and related information |
Cessna Repair No. S-150-ATA25/01RD Rev.A dated August 3, 2011 [FAA AMOC approval L115W-11-804], Cessna Single Engine Service Bulletin SEB11-4, and Cessna Multi-Engine Service Bulletin MEB11-2, both dated December 12, 2011 [FAA AMOC approval L115W-11-1109]. For further information, or copies of related service information, contact the Cessna Aircraft Company, One Cessna Boulevard, P.O. Box 7704, Wichita, Kansas 67277, USA; telephone: +1 316-517-5650. |
| Remarks |
Cessna types 170, 190 and 195 are classified as Annex II of Regulation (EC) 1592/2002 and are therefore outside EASA scope. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu
|
