| Number |
F-1972-060 |
| Issued by |
 France |
| Issue date |
1972-05-02 |
| Effective date |
1972-05-02 |
| EASA approval number |
|
| ATA Chapter |
27 |
Approval Holder
/ Type Designation |
-
TEXTRON AVIATION INC.
-
F150
-
F150F
-
F150G
-
F150H
-
F150J
-
FA150K
-
FA150L
-
FRA150L
-
F172
-
F177RG
-
FR172 (Reims Rocket)
-
FR172E
-
FR172F
-
FR172G
-
FR172H
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD 72-60 supersedes DGAC France AD 70-99 and AD 72-29.
|
| Publication(s) and related information |
Cessna Service Letter (SL) SE72-2, dated January 27, 1972, or (revised) March 24, 1972, or later FAA approved revision; or SL SE70-16, dated June 12, 1970, or SL SE72-17 Revision 1 dated January 12, 1973. |
| Remarks |
This AD is not the State of Design AD for US-manufactured (Cessna) aeroplanes - see FAA AD 72-03-03 R3; that AD can be used as (approximate) English translation for this AD, with regard to the technical instructions, NOT for Applicability or compliance times. This AD does not apply to Argentina-manufactured A182 aeroplanes, which are not validated in Europe. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu.
|
