True Flight Holdings LLC Airworthiness Directives

26 ADs indexed for True Flight Holdings LLC aircraft.

Models

Recent ADs

2022-03-15

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...

Effective: Mar 21, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2021-14-12

final rule

Airworthiness Directives; True Flight Holdings LLC Airplanes

Unsafe Condition: cracks, buckles, corrosion, delamination, rust, and previous repair of the horizontal stabilizers could result in reduced structural integrity and lead to loss of control of the airplane.

Effective: Jul 27, 2021 Category: aircraft Compliance: Within 25 hours time-in-service or before the next 100 hour or annual inspection, whichever occur...

Why matched: Airworthiness Directives; True Flight Holdings LLC Airplanes

2006-12-07

final rule

Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies

Unsafe Condition: Cracks in the cylinder assemblies and possible engine failure caused by separation of a cylinder head.

Effective: Jul 11, 2006 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

95-19-15 R1

final rule

Airworthiness Directives; Tiger Aircraft LLC Models AA-5, AA-5A, AA-5B, and AG-5B Airplanes

Unsafe Condition: Wing attach shoulder bolt failure due to fretting, scoring, wear, enlarged or elongated mounting holes, or excessive wing to center spar clearance.

Effective: Oct 3, 2005 Category: aircraft Compliance: before further flight

Why matched: Airworthiness Directives; Tiger Aircraft LLC Models AA-5, AA-5A, AA-5B, and AG-5B Airplanes

2005-01-19

final rule

Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...

Effective: Feb 23, 2005 Category: aircraft Compliance: Within 12 months of the effective date (February 23, 2005).

Why matched: Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

89-18-08

final rule

Airworthiness Directives; GULFSTREAM AEROSPACE CORPORATION Models AA-5, AA-5A, AA-5B, and GA-7 Airplanes

Unsafe Condition: Fuel tank/fuel system contamination caused by deterioration of fuel tank access cover sealant.

Effective: Sep 21, 1989 Category: aircraft Compliance: within the next 25 hours time-in-service after the effective date of this AD, unless already acco...

Why matched: Airworthiness Directives; GULFSTREAM AEROSPACE CORPORATION Models AA-5, AA-5A, AA-5B, and GA-7 Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

85-21-02

final rule

Airworthiness Directives; GULFSTREAM AEROSPACE Models AA-1, AA-1A, AA-1B and AA-1C Airplanes

Unsafe Condition: Failure of the seat belt attachment bracket (Part Number 60152-2) in a minor crash.

Effective: Oct 28, 1985 Category: aircraft Compliance: within 25 hours time-in-service after the effective date of this AD unless already accomplished b...

Why matched: Airworthiness Directives; GULFSTREAM AEROSPACE Models AA-1, AA-1A, AA-1B and AA-1C Airplanes

81-24-03

final rule

Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model AA5, AA5A and A5B Series Airplanes

Unsafe Condition: Broken wires in carburetor airbox screens can cause filter material to enter the induction system and carburetor throat, leading to engine power loss.

Effective: Nov 16, 1981 Category: aircraft Compliance: Within specified intervals based on time in service: for airplanes with 400+ hours at effective d...

Why matched: Airworthiness Directives; GULFSTREAM AMERICAN CORPORATION Model AA5, AA5A and A5B Series Airplanes

81-15-03

final rule

Airworthiness Directives; BRACKETT AIRCRAFT COMPANY, INC. Brackett Aircraft Specialties, Inc.: Applies to Brackett Aircraft Company, Inc., Engine Inlet Air Filters

Unsafe Condition: Failure of the aluminum air filter retainer screen or gaskets could result in ingestion of the screen, filter element, and/or gasket particles into the carburetor throat, causing partial or complet...

Effective: Jul 20, 1981 Category: appliance Compliance: Within 25 hours of time in service after the effective date of this AD

Why matched: Airworthiness Directives; BRACKETT AIRCRAFT COMPANY, INC. Brackett Aircraft Specialties, Inc.: Applies to Brackett Aircraft Company, Inc., Engine Inlet Air Filters

79-22-04

final rule

Airworthiness Directives; Gulfstream American Corporation (GAC) Model AA-5, AA-5A, AA-5B, Airplanes

Unsafe Condition: Possible aileron oscillation due to loose rivets, damage, delamination, wear, damage, insecure mounting of aileron bearings and stops, improper rigging and cable tension, or worn and loose joints i...

Effective: Nov 9, 1979 Category: aircraft Compliance: within 25 hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; Gulfstream American Corporation (GAC) Model AA-5, AA-5A, AA-5B, Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

79-16-02

final rule

Airworthiness Directives; INDIANA MILLS AND MANUFACTURING, INC.: Applies to Model IMM 111040-1, -2, -3, -4 and -8 Safety Belt Assemblies

Unsafe Condition: The push-button release mechanism of the safety belt assemblies may not meet the required release force standards (2.5 to 8 pounds) as specified in FAA TSO-C22f Section 4.3.2.2.

Effective: Aug 2, 1979 Category: appliance Compliance: within 120 days from the effective date of the AD

Why matched: Airworthiness Directives; INDIANA MILLS AND MANUFACTURING, INC.: Applies to Model IMM 111040-1, -2, -3, -4 and -8 Safety Belt Assemblies

78-13-04

final rule

Airworthiness Directives; Grumman American Aviation Corporation Model AA-1, AA-1A, AA-1B Airplanes

Unsafe Condition: Failure of the fuel measurement gauge float and associated components could lead to inaccurate fuel quantity indication, increasing the risk of unintentional fuel exhaustion in flight.

Effective: Jun 30, 1978 Category: aircraft Compliance: within next 200 hours in service after the effective date of this AD

Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA-1, AA-1A, AA-1B Airplanes

77-08-03

final rule

Airworthiness Directives; Grumman American Aviation Corporation Model AA- 5A, and Model AA-5B, Airplanes

Unsafe Condition: Faulty altitude, airspeed, and vertical speed indications from the alternate static source valve Gerdes part number A-1390 due to contamination or lack of lubrication.

Effective: Apr 19, 1977 Category: aircraft Compliance: Prior to further flight under Instrument Flight Rules (IFR) or night flight, or within the next 2...

Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA- 5A, and Model AA-5B, Airplanes

77-07-04

final rule

Airworthiness Directives; Grumman American Aviation Corporation Model AA-5 and AA-5A Airplanes

Unsafe Condition: Failure of the carburetor heat valve assembly due to cracks in the bend radius of Configuration A.

Effective: Apr 11, 1977 Category: aircraft Compliance: Within 10 hours of flight after the effective date of this AD

Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA-5 and AA-5A Airplanes

76-22-09

final rule

Airworthiness Directives; Grumman American Model AA-5A and AA-5B Airplanes

Unsafe Condition: Use of certain Stewart Warner oil coolers with model number 10568B (serial 101-579) or 10578B (serial 101-634) or illegible markings may be defective.

Effective: Nov 10, 1976 Category: aircraft Compliance: before further flight

Why matched: Airworthiness Directives; Grumman American Model AA-5A and AA-5B Airplanes

76-17-03

final rule

Airworthiness Directives; Grumman American Aviation Corporation Model AA1, AA1A, AA1B, AA5, AA-5A, AA-5B Airplanes

Unsafe Condition: Delaminations in bonded skins

Effective: Aug 30, 1976 Category: aircraft Compliance: within the next 25 flight hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; Grumman American Aviation Corporation Model AA1, AA1A, AA1B, AA5, AA-5A, AA-5B Airplanes

76-04-05

final rule

Airworthiness Directives; Grumman American Model AA-5B Airplanes

Unsafe Condition: Failure of the carburetor mixture control wire.

Effective: Feb 25, 1976 Category: aircraft Compliance: within the next 20 hours' time in service after the effective date of this Airworthiness Directive

Why matched: Airworthiness Directives; Grumman American Model AA-5B Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

76-01-02

final rule

Airworthiness Directives; Grumman American Model AA-5, AA-5A and AA-5B Airplanes

Unsafe Condition: Failure of the upper engine cowl due to cracks in the hinge assembly adjacent to the forward and aft attach brackets.

Effective: Feb 25, 1976 Category: aircraft Compliance: Within the next 15 hours' time in service after January 12, 1976 for Model AA-5B airplanes, and w...

Why matched: Airworthiness Directives; Grumman American Model AA-5, AA-5A and AA-5B Airplanes

75-09-07

final rule

Airworthiness Directives; Grumman American Model AA-1, AA-1A, and AA-1B Airplanes

Unsafe Condition: Mixture control wire failures due to kinking or misrigging.

Effective: Apr 25, 1975 Category: aircraft Compliance: within the next 50 hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; Grumman American Model AA-1, AA-1A, and AA-1B Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

72-06-02

final rule

Airworthiness Directives; Grumman-American Aviation Corporation Models AA-1, AA-1A, AA-1B and AA-5 Airplanes

Unsafe Condition: Worn and broken rudder aileron and elevator control cables and pulleys control cables may result in loss of control.

Effective: Aug 29, 1974 Category: aircraft Compliance: prior to the next flight after the effective date of this A.D. unless already accomplished within...

Why matched: Airworthiness Directives; Grumman-American Aviation Corporation Models AA-1, AA-1A, AA-1B and AA-5 Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

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