Airworthiness Directives; Allied Ag Cat Productions, Inc. Models G-164, G-164A, G-164B, G-164B With 73″ Wing Gap, G-164B-15T, G-164B-34T, G-164B-20T, G-164C, G-164D, and G-164D With 73″ Wing Gap Airplanes
Unsafe Condition: Corrosion in the rudder main tubular spar could result in failure of the rudder main spar tube, leading to loss of directional control.
Effective: Mar 17, 2011Category: aircraftCompliance: Within 5 years of the effective date of this AD for Models G-164, G-164A, and G-164B airplanes.
Why matched: Airworthiness Directives; Allied Ag Cat Productions, Inc. Models G-164, G-164A, G-164B, G-164B With 73'' Wing Gap, G-164B-15T, G-164B- 34T, G-164B-20T, G-164C, G-164D, and G-164D With 73'' Wing Gap Airplanes
Airworthiness Directives; Allied Ag Cat Productions, Inc. Model G-164 Series Airplanes
Unsafe Condition: Corrosion in the rudder main tubular spar could result in failure of the weld to the main spar tube, leading to loss of directional control.
Effective: Dec 19, 2008Category: aircraftCompliance: Initially inspect within the next 60 months after the last inspection required in AD 78-08-09 or ...
Why matched: Airworthiness Directives; Allied Ag Cat Productions, Inc. Model G-164 Series Airplanes
Airworthiness Directives; Allied Ag Cat Productions, Inc. (Type Certificate No. 1A16 Formerly Held by Schweizer Aircraft Corp.) G-164 Series Airplanes
Unsafe Condition: Turning the fuel shut-off valve clockwise past the 'ON' position, which could allow the fuel valve to be rotated to an unplacarded 'OFF' position, leading to reduced fuel flow and consequent loss o...
Effective: Sep 18, 2007Category: aircraftCompliance: Within the next 100 hours time-in-service after the applicable effective date (April 6, 1982 for ...
Why matched: Airworthiness Directives; Allied Ag Cat Productions, Inc. (Type Certificate No. 1A16 Formerly Held by Schweizer Aircraft Corp.) G-164 Series Airplanes
Airworthiness Directives; SCHWEIZER (GRUMMAN) All Model G-164 Series Airplanes
Unsafe Condition: Failure of the forward and aft elevator control system push-pull rods and end fittings due to corrosion and cracks.
Effective: Nov 24, 1989Category: aircraftCompliance: Within the next 30 calendar days after the effective date of this AD, and thereafter at intervals...
Why matched: Airworthiness Directives; SCHWEIZER (GRUMMAN) All Model G-164 Series Airplanes
Airworthiness Directives; SCHWEIZER (GULFSTREAM AMERICAN-GRUMMAN) Models G-164B, G-164C, and
G164D Airplanes
Unsafe Condition: Elongation of the aileron cable attach holes and dislodgement of P/N A1450-281 bushings from the aileron bellcrank.
Effective: Jul 5, 1982Category: aircraftCompliance: Within 25 hours time-in-service after the effective date of this AD and every 12 months thereafte...
Why matched: Airworthiness Directives; SCHWEIZER (GULFSTREAM AMERICAN-GRUMMAN) Models G-164B, G-164C, and
G164D Airplanes
Airworthiness Directives; Grumman Models G-164A and G-164B
Unsafe Condition: Looseness, wear, or corrosion of the bolts attaching the Elevator Control Horn, P/N A 1841-3, to the left and right side elevators, P/N A1201-5A and A1201-4A, could result in loss of elevator control.
Effective: Aug 29, 1979Category: aircraftCompliance: Within the next 25 hours in service or two weeks, whichever occurs first, unless already accompli...
Why matched: Airworthiness Directives; Grumman Models G-164A and G-164B
Airworthiness Directives; GRUMMAN G-164 S/N's 1 thru 400, G-164A S/N's 401 and up, G-164B S/N's 01B and up, G-164C S/N's 01C and up, certificated in all categories.
Unsafe Condition: Aileron balance cables (P/N A1860-101 and A1860-401) may contain broken wires at the wing root pulley, which could result in loss of aileron control.
Effective: Feb 28, 1979Category: aircraftCompliance: Within the next 50 hours in service after the effective date, unless already accomplished within ...
Why matched: Airworthiness Directives; GRUMMAN G-164 S/N's 1 thru 400, G-164A S/N's 401 and up, G-164B S/N's 01B and up, G-164C S/N's 01C and up, certificated in all categories.
Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B Aircraft
Unsafe Condition: Corrosion of the lower wing attachment fittings (P/N's A1050-1, -3, -4, -101, -102, -103, -104, -13, -19, -20, -411, -412 and 3050-13, -14, -15, -16) may lead to structural failure of the wing fitt...
Effective: Dec 20, 1978Category: aircraftCompliance: Within the next 25 hours in service and thereafter at intervals not to exceed 500 hours in servic...
Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B
Unsafe Condition: Rudder cables (P/N A1860-35, -36 for G-164 and G-164A; P/N A3860-1, -3 for G-164B) may fray in the cockpit floorboard and chafe strip area, leading to broken strands and potential failure.
Effective: Jul 7, 1977Category: aircraftCompliance: Within 20 hours' time in service after July 7, 1977, unless inspected within last 80 hours, and t...
Why matched: Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B
Airworthiness Directives; Grumman-American Model G-164B and G-164A
Unsafe Condition: Failure to install a warning placard adjacent to the parking brake handle and the absence of the alteration defined in Grumman American Aviation Corporation Service Bulletin No. 60 may result in th...
Effective: Jun 29, 1977Category: aircraftCompliance: before further flight (for placard installation) and within the next 50 hours in service (for the...
Why matched: Airworthiness Directives; Grumman-American Model G-164B and G-164A
Airworthiness Directives; Grumman Models G-164 and G-164A Airplanes
Unsafe Condition: Main landing gear strut failures associated with cracks and corrosion damage in Grumman American main landing gear struts P/N A1515-11, -12, A1530-11, -12, and Cessna struts P/N 0341109-1, -2.
Effective: Nov 30, 1976Category: aircraftCompliance: Within the next 100 landings after the effective date of this airworthiness directive, unless acc...
Why matched: Airworthiness Directives; Grumman Models G-164 and G-164A Airplanes
Airworthiness Directives; Grumman Model G-164 Airplanes
Unsafe Condition: Main landing gear strut failures associated with Frenco Co. P/N 1428 struts installed under STC SA647WE.
Effective: Oct 20, 1976Category: aircraftCompliance: Within the next 100 landings after the effective date of this airworthiness directive, unless acc...
Why matched: Airworthiness Directives; Grumman Model G-164 Airplanes
Airworthiness Directives; Grumman Models G-164 and G-164A Airplanes
Unsafe Condition: Failure of the elevator torque tube due to cracks where the inboard elevator rib is welded to the torque tube and between the two inboard blind rivets.
Effective: Dec 16, 1975Category: aircraftCompliance: Within specified intervals based on time in service as of April 22, 1966: (a) 25 hours' time in s...
Why matched: Airworthiness Directives; Grumman Models G-164 and G-164A Airplanes
Airworthiness Directives; Grumman Model G-164 Aircraft
Unsafe Condition: Loose rivets attaching the rod ends of the elevator forward pushrod assembly (P/N A1847-1 and A1847-3) may lead to failure of the assembly.
Effective: Oct 27, 1967Category: aircraftCompliance: Within the next 50 hours' time in service (for aircraft with ≥250 hours on effective date) or bef...
Why matched: Airworthiness Directives; Grumman Model G-164 Aircraft
Airworthiness Directives; Grumman Models G-164 and G-164A Airplanes
Unsafe Condition: Fouling of the control stick by the surface control lock and inadvertent locking of the right toe brake master cylinder during flight maneuvering.
Effective: Mar 24, 1967Category: aircraftCompliance: Within the next 25 hours' time in service after April 7, 1966 (for Model G-164, S/N 301-400) and ...
Why matched: Airworthiness Directives; Grumman Models G-164 and G-164A Airplanes