Number |
US-97-18-02R1 |
Issued by |
United States of America |
Issue date |
2003-07-08 |
Effective date |
2003-06-26 |
EASA approval number |
|
ATA Chapter |
61 |
Approval Holder / Type Designation |
-
HARTZELL PROPELLER INC.
-
HA-A2V, HA-A2MV
-
HC-12V
-
HC-12V20-3
-
HC-12V20-7
-
HC-12V20-8
-
HC-12X
-
HC-12X20-1
-
HC-12X20-2
-
HC-12X20-3
-
HC-12X20-4
-
HC-12X20-5
-
HC-12X20-6
-
HC-12X20-7
-
HC-12X20-8
-
HC-12X20-9
-
HC-13X
-
HC-13X20-5
-
HC-13X20-6
-
HC-13X20-8
-
HC-82V
-
HC-82VF-2
-
HC-82VK-2
-
HC-82VL-2
-
HC-83V
-
HC-83V20-1
-
HC-83V20-2
-
HC-83VF-2
-
HC-83VF-3
-
HC-A2V, HC-A2MV
-
BHC-A2VF-1
-
BHC-A2VF-2
-
BHC-A2VF-3
-
HC-A2V20-1
-
HC-A2V20-2
-
HC-A2V20-3
-
HC-A2V20-4
-
HC-A2V20-5
-
HC-A2VF-1
-
HC-A2VF-2
-
HC-A2VF-3
-
HC-A2VF-6
-
HC-A2VK-1
-
HC-A2VK-2
-
HC-A2VK-3
-
HC-A2VL-1
-
HC-A2VL-2
-
HC-A2VL-6
-
HC-A3V, HC-A3MV
-
EHC-A3VF-2
-
HC-A3V20-1
-
HC-A3V20-2
-
HC-A3V20-3
-
HC-A3V20-5
-
HC-A3V21-2
-
HC-A3VF-1
-
HC-A3VF-2
-
HC-A3VF-3
-
HC-A3VF-4
-
HC-A3VF-5
-
HC-A3VF-7
-
HC-A3VK-1
-
HC-A3VK-2
-
HC-A3VK-4
-
PHC-A3VF-2
-
PHC-A3VF-3
-
PHC-A3VF-4
-
PHC-A3VF-5
-
PHC-A3VF-7
-
HC-D2V, HC-D2MV
-
HC-D2V20-1
-
HC-D2V20-2
-
HC-D2V20-3
-
HC-D2V20-4
-
HC-D2V20-5
-
HC-D2V20-6
-
HC-D2V20-7
-
HC-D2V20-8
-
HC-D2V20-9
-
HC-D2X
-
HC-D2X20-3
-
HC-D2X20-7
-
HC-D2X20-8
-
HC-D3V, HC-D3MV
-
HC-D3V20-5
-
HC-D3V20-6
-
HC-D3V20-8
|
Revision |
This AD revises FAA AD 97-18-02, dated August 27, 1997.
|
Correction |
This AD was republished to correct the omission of the (Part 39) Amendment number. In all other respects, the original document (AD 97-18-02 R1), as published on 26 June 2003, remains the same.
|
Supersedure |
None
|
Publication(s) and related information |
Hartzell SB No. HC-SB-61-217, Revision 1, dated July 11, 1997. Information on modifying the propellers may be found in Hartzell SB No.'s HC-SB-61-232, dated March 20, 1998, and HC-SB-61-233, dated April 17, 1998. Copies may be obtained from Hartzell Propeller Inc., One Propeller Place, Piqua, OH 45356-2634, ATTN: Product Support; telephone +1 (937) 778-4200, fax +1 (937) 778-4321. |
Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail:
ADs [at] easa.europa [dot] eu
|