AD 76-04-01

Airworthiness directive · Main Gear Extension · Cessna 210, 210A, 210B and 2 more

Effective
January 27, 1977
Models
210, 210A, 210B, 210C, 210D
Data sheet
TCDS3A21
Registered aircraft
554 matched by model
Product
Aircraft · Small airplane
Amendment
39-2810

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

76-04-01 CESSNA: Amendment 39-2517 as amended by Amendment 39-2556, 39-2686 and 39-2767 is further amended by Amendment 39-2810. Applies to Models 210 through 210D (Serial Numbers 57001 thru 57575 and 21057576 thru 21058510) airplanes on which are installed Electrol manufactured main gear rotary actuator assemblies, Cessna P/Ns 1280102-1 and -2 (Electrol P/Ns EA 1471-1 and -2) or Cessna P/Ns 1280501-1 and -2 (Electrol P/Ns EA 1614-1 and -2). This AD does not apply to those airplanes on which Cessna P/Ns 1280511-3/4 and 1298100-1/2 actuator assemblies are installed.

Compliance: Required as indicated, unless already accomplished in accordance with this AD, previous maintenance or AD 71-24-07.

To decrease the possibility of main gear extension failure, accomplish the following:

On or before April 1, 1977, or within 100 hours' time in service after February 26, 1976, whichever occurs later, install Cessna Kits 1209005-1 R/L in accordance with Cessna Service Letter SE75-21 dated October 3, 1975, or later approved revisions, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

NOTE 1) The landing gear actuator assemblies having Cessna P/Ns and manufactured by Electrol can be identified by using an inspection mirror through the inspection plate located forward of the strut doors to read the actuator nameplate.

NOTE 2) A significant savings of manhours will result if compliance with this AD and the modifications and/or inspections required by AD 76-14-07 (Amendment 39-2670 - landing gear saddle fittings) are accomplished at the same time.

NOTE 3) It is imperative that Cessna P/N 1209005-1 R/L Kits be ordered from the manufacturer immediately to assure that a sufficient supply of kits will be available to allow modification of all affected aircraft on or before April 1, 1977.

Amendment 39-2517 superseded AD 71-24-07, Amendment 39-1345.

Amendment 39-2517 became effective February 26, 1976.

Amendment 39-2556 became effective March 26, 1976.

Amendment 39-2686 became effective August 12, 1976, and replaces Amendments 39-2517 and 39-2556.

Amendment 39-2767 became effective November 2, 1976, and supplements Amendment 39-2686. Amendment 39-2686 in turn replaced Amendments 39-2517 and 39-2556.

This amendment, 39-2810, becomes effective January 27, 1977, and supplements Amendments 39-2686 and 39-2767.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 554

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Cessna554 aircraft
By year built
19581981
Registered aircraft by year built: 427 aircraft
19581
195915
1960133
196150
196285
196359
196479
19762
19772
19811

127 with no year recorded

By model

Aircraft

See all 554 aircraft

NTSB investigations that cite this AD · 2

Their narratives or probable cause name AD 76-04-01, often to say whether the aircraft complied with it.