Number |
F-1999-053R1 |
Issued by |
France |
Issue date |
1999-03-10 |
Effective date |
1999-02-20 |
EASA approval number |
|
ATA Chapter |
71 |
Approval Holder / Type Designation |
-
CEAPR
-
DR 200
-
DR 220
-
DR 253
-
DR 300
-
DR 315
-
DR 340
-
DR 360
-
DR 380
-
DR 400
-
DR 400/100
-
DR 400/120
-
DR 400/120 A
-
DR 400/120 D
-
DR 400/125
-
DR 400/125 i
-
DR 400/140
-
DR 400/140 B
-
DR 400/160
-
DR 400/160 D
-
DR 400/180
-
DR 400/180 R
-
DR 400/180 S
-
DR 400/2+2
-
DR 400/200 R
-
DR 400/500
-
DR 400/NGL
-
DR 400/RP
-
HR 100
-
HR 100/200
-
HR 100/200 B
-
HR 100/210
-
HR 100/210 D
-
HR 100/250 TR
-
HR 100/285
-
HR 100/285 C
-
R 1180
-
R 3000
-
R 3000/100
-
R 3000/120
-
R 3000/120 D
-
R 3000/140
-
R 3000/160
-
R 3000/160 S
-
R 3000/180
|
Revision |
This Revision 1 replaces DGAC France AD 1999-053(A) dated February 10, 1999.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Avions ROBIN Service Bulletin No. 161 dated January 26, 1999. |
Remarks |
CAA New Zealand AD DCA/R2000/25 has been issued to take over the requirements of this AD for HR200/R2000 aeroplanes. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|