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2010-09-24
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Airworthiness Directives; de Havilland Model DHC-8-301, -311, and -315 Series Airplanes
Rules and Regulations
D09002ee1be045d38
D09002ee1be045de1
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
originator
org
United States Government Agency or Subagency
This amendment supersedes an existing airworthiness directive (AD), applicable to certain de Havilland Model DHC-8-301,--311, and-- 315 series airplanes, that currently requires modification of the airspeed limitations placard and revision of the Airplane Flight Manual to specify operating at lower airspeeds when the airplane is operating at full flaps. That action also provides for the optional termination of the requirements of the AD for certain airplanes. That action was prompted by a report that incorrect rivets were installed on the outboard flaps assemblies of these airplanes. The actions specified by that AD are intended to prevent structural failure of the outboard flaps of the wings due to the installation of incorrect rivets in the flap assemblies, which could result in reduced controllability of the airplane. This new amendment requires the installation of the previously optional terminating modification on certain airplanes. DATES: Effective August 6, 1996.
61 FR 34368
https://www.govinfo.gov/app/details/FR-1996-07-02/96-16807
96-16807
fr02jy96-2
RIN 2120-AA64
4910-13-U
Docket No. 95-NM-268-AD
Amendment 39-9685
AD 96-14-03
https://www.govinfo.gov/app/details/FR-1996-07-02/96-16807
https://www.govinfo.gov/content/pkg/FR-1996-07-02/html/96-16807.htm
https://www.govinfo.gov/content/pkg/FR-1996-07-02/pdf/96-16807.pdf
3 p.
34368
34370
61 FR 34368
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; de Havilland Model DHC-8-301, -311, and -315 Series Airplanes; Federal Register Vol. 61, Issue
RULE
96-16807
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
1996-08-06
Docket No. 95-NM-268-AD
Amendment 39-9685
AD 96-14-03
4910-13-U
96-16807
Final rule.
This amendment supersedes an existing airworthiness directive (AD), applicable to certain de Havilland Model DHC-8-301,--311, and-- 315 series airplanes, that currently requires modification of the airspeed limitations placard and revision of the Airplane Flight Manual to specify operating at lower airspeeds when the airplane is operating at full flaps. That action also provides for the optional termination of the requirements of the AD for certain airplanes. That action was prompted by a report that incorrect rivets were installed on the outboard flaps assemblies of these airplanes. The actions specified by that AD are intended to prevent structural failure of the outboard flaps of the wings due to the installation of incorrect rivets in the flap assemblies, which could result in reduced controllability of the airplane. This new amendment requires the installation of the previously optional terminating modification on certain airplanes. DATES: Effective August 6, 1996.
Effective August 6, 1996.
Franco Pieri, Aerospace Engineer, Airframe Branch, ANE-171, FAA, New York Aircraft Certification Office, Engine and Propeller Directorate, 10 Fifth Street, Third Floor, Valley Stream, New York 11581; telephone (516) 256-7526; fax (516) 568-2716.
Federal Register
Vol. 61, no. 128
Office of the Federal Register, National Archives and Records Administration
1996-07-02
continuing
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351 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-1996-07-02
P0b002ee180a1e600
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr02jy96
https://www.govinfo.gov/app/details/FR-1996-07-02
https://www.govinfo.gov/content/pkg/FR-1996-07-02/pdf/FR-1996-07-02.pdf
fdlp
34367
34711
DGPO
2010-09-24
2023-05-06
FR-1996-07-02
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FR
FR-1996-07-02
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