Rockwell International Airworthiness Directives

37 ADs indexed for Rockwell International aircraft.

Models

Recent ADs

2011-07-13

final rule

Airworthiness Directives; CPAC, Inc. (Type Certificate Formerly Held by Commander Aircraft Corporation, Gulfstream Aerospace Corporation, and Rockwell International) Models 112, 112B, 112TC, 112TCA, 114, 114A, 114B, and 114TC Airplanes

Unsafe Condition: Cracking of the elevator spar, which could lead to structural failure and separation of the elevator from the airplane, resulting in loss of control.

Effective: Apr 4, 2011 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; CPAC, Inc. (Type Certificate Formerly Held by Commander Aircraft Corporation, Gulfstream Aerospace Corporation, and Rockwell International) Models 112, 112B, 112TC, 112TCA, 114, 114A, 114B, and 114TC Airplanes

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

2005-12-51

final rule

Airworthiness Directives; Rockwell International (Aircraft Specification No. A-2-575 Previously Held by North American and Recently Purchased by Boeing) Models AT-6 (SNJ-2), AT-6A (SNJ-3), AT-6B, AT-6C (SNJ-4), AT-6D (SNJ-5), AT-6F (SNJ-6), BC-1A, SNJ-7, and T-6G Airplanes; and Autair Ltd. (Aircraft Specification No. AR-11 Previously Held by Noorduyn Aviation Ltd.) Model Harvard (Army AT-16) Airplanes

Unsafe Condition: Fatigue cracks in the inboard and outboard, upper and lower wing attach angles (except for the nose angles) of both wings.

Effective: Jun 23, 2005 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Rockwell International (Aircraft Specification No. A-2-575 previously held by North American and recently purchased by Boeing) Models AT-6 (SNJ-2), AT-6A (SNJ-3), AT- 6B, AT-6C (SNJ-4), AT-6D (SNJ-5), AT-6F (SNJ-6), BC-1A, SNJ-7, and T-6G Airplanes; and Autair Ltd. (Aircraft Specification No. AR-11 previously held by Noorduyn Aviation Ltd.) Model Harvard (Army AT-16) Airplanes

94-02-02

final rule

Airworthiness Directives: Rockwell International/Collins Air Transport Division DME-700 Distance Measuring Equipment

Unsafe Condition: The DME-700 units may fail to process and update distance outputs and establish a continuous restart mode upon power application, leading to navigational errors.

Effective: Feb 21, 1994 Category: appliance Compliance: within the next 12 calendar months after the effective date of this AD

Why matched: Airworthiness Directives: Rockwell International/Collins Air Transport Division DME-700 Distance Measuring Equipment

94-01-06

final rule

Airworthiness Directives: Rockwell International, Collins Air Transport Division, Traffic Alert and Collision Avoidance System II Processors

Unsafe Condition: Incompatibility between TCAS II processors and the current air traffic control system could cause collisions or near misses due to unresolved non-crossing resolution advisories (RAs).

Effective: Feb 4, 1994 Category: appliance Compliance: Prior to December 31, 1994

Why matched: Airworthiness Directives: Rockwell International, Collins Air Transport Division, Traffic Alert and Collision Avoidance System II Processors

93-04-02

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL/COLLINS AVIATION DIVISION TDR-94D Mode S Transponders, P/N CPN 622-9210-002

Unsafe Condition: Failure of TDR-94D Mode S transponders could cause a mid-air collision or a near-miss situation.

Effective: Mar 26, 1993 Category: appliance Compliance: Within 10 calendar days after effective date (March 26, 1993) for placard installation; within 6 ...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL/COLLINS AVIATION DIVISION TDR-94D Mode S Transponders, P/N CPN 622-9210-002

92-11-09

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL/COLLINS AIR TRANSPORT SYSTEMS TPR-720 Air Traffic Control Radar Beacon System/Mode S Transponders, Part Numbers (P/N) 622-7878-020, and P/N 622-7878-120, installed

Unsafe Condition: Loss of the ability to track aircraft positions by radar in high density air traffic areas due to transponder malfunction.

Effective: May 28, 1992 Category: appliance Compliance: Within the next 6 calendar months after the effective date of this AD

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL/COLLINS AIR TRANSPORT SYSTEMS TPR-720 Air Traffic Control Radar Beacon System/Mode S Transponders, Part Numbers (P/N) 622-7878-020, and P/N 622-7878-120, installed

86-25-01

final rule

Airworthiness Directives; COLLINS AVIONICS DIVISION/ROCKWELL INTERNATIONAL: Applies to Model 51RV-4 VOR-ILS Navigation Receivers, Part Number 622-3255-XXX, Serial Number 5960 thru and including 7277

Unsafe Condition: Deviation output signal oscillation that may cause undetected erroneous VOR and ILS localizer deviation display, flight director commands, and/or autopilot tracking.

Effective: Jan 6, 1987 Category: appliance Compliance: Within three calendar days and 30 calendar days after the effective date of this AD (January 6, 1...

Why matched: Airworthiness Directives; COLLINS AVIONICS DIVISION/ROCKWELL INTERNATIONAL: Applies to Model 51RV-4 VOR-ILS Navigation Receivers, Part Number 622-3255-XXX, Serial Number 5960 thru and including 7277

86-22-10

final rule

Airworthiness Directives; COLLINS AVIONICS DIVISION/ROCKWELL INTERNATIONAL: Applies to Collins Model DME-42, P/N 622-6263-002, Distance Measuring Equipment

Unsafe Condition: Display of erroneous DME-42 information

Effective: Nov 17, 1986 Category: appliance Compliance: within the next 25 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; COLLINS AVIONICS DIVISION/ROCKWELL INTERNATIONAL: Applies to Collins Model DME-42, P/N 622-6263-002, Distance Measuring Equipment

85-22-10

final rule

Airworthiness Directives; COLLINS AVIONICS DIVISION/ROCKWELL INTERNATIONAL: Applies to the following Flight Director Indicators and Horizontal Situation Indicators

Unsafe Condition: Internal gear slippage that may result in erroneous display of pitch and/or roll command and roll pointer displays in flight director indicators or course and/or heading displays in horizontal situ...

Effective: Dec 31, 1985 Category: appliance Compliance: Prior to further flight or use, within 25 hours time-in-service after the effective date, and rep...

Why matched: Airworthiness Directives; COLLINS AVIONICS DIVISION/ROCKWELL INTERNATIONAL: Applies to the following Flight Director Indicators and Horizontal Situation Indicators

82-26-02

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA 265-65, and NA 265-60 Series Airplanes

Unsafe Condition: Possible inadvertent cabin pressure loss due to fatigue failure of interior pressure panel P/N 306-312005-3.

Effective: Apr 13, 1983 Category: aircraft Compliance: Prior to the next flight for initial inspection and crack replacement. Within the next 150 flight...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA 265-65, and NA 265-60 Series Airplanes

80-04-11 R2

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA 265-60 and NA 265-80 Airplanes

Unsafe Condition: Structural failure of the airframe due to deviations from the supplemental type design in areas modified by The Raisbeck Group STC's SA687NW or SA847NW, including plugged holes, oblong or irregular...

Effective: Apr 13, 1983 Category: aircraft Compliance: Before further flight and before accumulation of 2000 flight hours time in service after modifica...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA 265-60 and NA 265-80 Airplanes

82-27-10

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA 265-65 Airplanes

Unsafe Condition: Failure of the horizontal stabilizer trim actuator and loss of longitudinal trim capabilities.

Effective: Jan 19, 1983 Category: aircraft Compliance: Within the next 25 flight hours, within the next 25 flight hours and every 25 flight hours therea...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA 265-65 Airplanes

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

82-10-02 R1

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA-265-60 and NA-265-65, Airplanes

Unsafe Condition: Flap screwjack actuator malfunction due to bearing failure.

Effective: Sep 13, 1982 Category: aircraft Compliance: Within the next 50 hours time-in-service after the effective date of this AD and within each addi...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA-265-60 and NA-265-65, Airplanes

81-13-04

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA-265-60, NA- 265-70, and NA-265-80 Airplanes

Unsafe Condition: The MLG shock strut trunnion may have an inside diameter exceeding 2.948 inches due to wear, which could result in structural failure of the main landing gear outer cylinder.

Effective: Jul 30, 1981 Category: aircraft Compliance: Prior to next flight

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA-265-60, NA- 265-70, and NA-265-80 Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

81-14-09

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA-265-40 and NA-265-60 Airplanes

Unsafe Condition: Cabin depressurization due to potential cracking of the door stop (beam) as a result of fatigue.

Effective: Jul 13, 1981 Category: aircraft Compliance: Within the next 600 hours additional time-in-service or within the next 12 months, whichever occu...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA-265-40 and NA-265-60 Airplanes

80-26-01

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA265-40 and -60 Series Airplanes

Unsafe Condition: Inadvertent cabin depressurization due to cracks in the fuselage structure below the cabin entrance door and adjacent areas.

Effective: Jan 19, 1981 Category: aircraft Compliance: Within the next 600 hours' additional time in service or within the next 12 months from the effec...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA265-40 and -60 Series Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

80-01-07 R1

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA 265-60 and NA 265-80 Airplanes

Unsafe Condition: Failure of the wing flap support structure due to cracks or fatigue in airplanes equipped with the Raisbeck Mark Five modification under STC SA687NW or SA847NW.

Effective: Jun 3, 1980 Category: aircraft Compliance: On or before 430 landings after modification; on or before 10 further landings or prior to 100 la...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA 265-60 and NA 265-80 Airplanes

80-03-05 R1

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA-265-70 and NA-265-80 Series Airplanes

Unsafe Condition: Elevator trailing edge delamination

Effective: May 29, 1980 Category: aircraft Compliance: Within 15 hours' time in service or 10 days from the effective date of this AD, whichever occurs ...

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA-265-70 and NA-265-80 Series Airplanes

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

80-08-07

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA265-40, -60, and -70 Series Airplanes

Unsafe Condition: Adverse flight characteristics resulting from elevator delamination

Effective: Apr 21, 1980 Category: aircraft Compliance: Compliance required as indicated, unless already accomplished

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA265-40, -60, and -70 Series Airplanes

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

79-17-01

final rule

Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA-265-60 Airplanes

Unsafe Condition: Flutter caused by the accumulation of undrained water in the elevators.

Effective: Aug 15, 1979 Category: aircraft Compliance: within 30 days or 30 flight hours, whichever occurs first

Why matched: Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA-265-60 Airplanes

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

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