AD 76-13-10

Airworthiness directive · Landing Gear Strut · Allied Ag Cat Productions G-164 and G-164A

Effective
November 30, 1976
Models
G-164, G-164A
Data sheet
TCDS1A16
Registered aircraft
272 matched by model
Product
Aircraft · Small airplane
Amendment
39-2777

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

76-13-10 GRUMMAN AMERICAN: Amendment 39-2657 as amended by Amendment 39-2777. Applies to Model G-164 and G-164A Ag-Cat Airplanes, S/N 1 through 1064, certificated in all categories.

Compliance required as indicated.

To prevent possible hazards associated with main landing gear strut failures, accomplish the following:

(a) For airplanes equipped with Grumman American main landing gear struts P/N A1515-11, -12, P/N A1530-11, -12, and Cessna struts P/N 0341109-1, -2:

(1) Within the next 100 landings after the effective date of this airworthiness directive, unless accomplished within the last 4400 landings, remove the gear struts and inspect the struts for cracks using dye penetrant or magnetic particle inspection procedures or with an FAA approved equivalent inspection procedure.

(2) Repeat the inspections of paragraph (a)(1) at intervals not to exceed 4500 landings.

(3) Inspect the struts for cracks and corrosion damage using dye penetrant inspection procedures,at each 1000 landings following the inspections specified in paragraph (a)(1) and (a)(2). This inspection can be conducted without removing the gear struts from the aircraft.

(b) Replace cracked or corroded parts prior to further flight with unused struts, Grumman American P/N A1530-33, -34 or with FAA approved equivalent parts.

(c) For the purpose of complying with this airworthiness directive, subject to the acceptance by the assigned FAA maintenance inspector, the number of landings may be determined by dividing each airplane's hours' time in service by the operator's fleet average time for takeoff to landing for the airplane type.

(d) Equivalent inspections and parts must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

(e) Upon submission of substantiating data by an owner or operator through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region, may adjust the compliance time in this AD. Grumman American Aviation Corporation Service Note No. 13 covers this same subjects.

Amendment 39-2657 was effective July 7, 1976.

This Amendment 39-2777 is effective November 30, 1976.

Affected TCDS · 1

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

Registered aircraft · 272

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
  • Grumman Acft ENG Cor-Schweizer150 aircraft
  • Grumman115 aircraft
  • Grumman American Avn.6 aircraft
  • Schweizer1 aircraft
By year built
19392005
Registered aircraft by year built: 219 aircraft
19391
19592
19606
19611
196213
19635
19646
19658
19664
19676
19686
196916
19707
197111
197223
197318
197431
197529
197620
19775
20051

53 with no year recorded

By model

Aircraft

See all 272 aircraft

NTSB investigations that cite this AD · 1

Their narratives or probable cause name AD 76-13-10, often to say whether the aircraft complied with it.