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98-23-13

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745, 745D, and 810 Series Airplanes

Unsafe Condition: Cracking of the eye end fittings of the outboard engine lower support could result in reduced structural integrity of the engine nacelle support structures.

Effective: Dec 17, 1998 Category: aircraft Compliance: Within 3 months after the effective date of this AD for Model Viscount 744, 745, and 745D series ...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745, 745D, and 810 Series Airplanes

98-12-17

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745, 745D, and 810 Series Airplanes

Unsafe Condition: Cracking and corrosion of engine nacelle subframe structure components could result in reduced structural integrity, engine separation from the airframe, and reduced controllability of the airplane.

Effective: Jul 1, 1998 Category: aircraft Compliance: Within 100 flight hours after the effective date of this AD or prior to the accumulation of the n...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745, 745D, and 810 Series Airplanes

95-22-08

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

Unsafe Condition: Reduced structural capability of the fuselage pressure vessel due to fatigue and corrosion in components of the fuselage pressure vessel.

Effective: Nov 27, 1995 Category: aircraft Compliance: Required as indicated, unless accomplished previously. Actions must be done at the later of speci...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

95-19-11

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

Unsafe Condition: Fatigue cracking of certain fittings in the tailplane spar could result in structural degradation of the attachment of the horizontal stabilizer to the fuselage.

Effective: Oct 20, 1995 Category: aircraft Compliance: Within 3,000 landings or 3 years after the effective date of this AD, whichever occurs first (for...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

95-15-02

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

Unsafe Condition: Fatigue cracking of the engine 'W' frame socket fittings inspection holes, which could lead to separation of the engine from the airframe due to fastener failure.

Effective: Aug 23, 1995 Category: aircraft Compliance: Within 12 months after the effective date of this AD, with engine removal and follow-on actions n...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

95-15-08

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

Unsafe Condition: Cracking or corrosion of the main spar forward booms or the upper root joint attachment fitting could lead to failure of the tailplane assemblies.

Effective: Aug 23, 1995 Category: aircraft Compliance: Prior to the accumulation of 8 years of service since date of manufacture or within 18 months aft...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

95-14-08

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

Unsafe Condition: Fatigue cracking of the undercarriage bracing of the nose wheel could result in failure of the structure and fittings, and subsequent collapse of the nose landing gear.

Effective: Aug 18, 1995 Category: aircraft Compliance: Prior to the accumulation of 2,050 landings after the effective date of this AD, or within 12 mon...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes

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

95-03-04

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Series Airplanes

Unsafe Condition: Fatigue cracking in the pivot pins that attach both nose wheel steering actuators to the steering head assembly could result in loss of nose wheel steering capability.

Effective: Mar 20, 1995 Category: aircraft Compliance: Prior to the accumulation of 1,100 landings after the effective date of this AD, or within 14 mon...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Series Airplanes

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

94-26-16

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Series Airplanes

Unsafe Condition: Damage, corrosion, or cracking of taper plugs (P/N 60216-1017) and split bushings (P/N 60216-1019) of the engine mount due to corrosion effects could lead to failure of the engine mount attachment ...

Effective: Mar 1, 1995 Category: aircraft Compliance: No later than 12 months after the effective date of this AD (March 1, 1995). Repeat inspections a...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Series Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

94-26-14

final rule

Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Series Airplanes

Unsafe Condition: Cracking in the chassis top strut support intercostal in the side bracing structure inside the wing due to metal fatigue, which could lead to failure of the chassis side bracing structure and reduc...

Effective: Feb 3, 1995 Category: aircraft Compliance: Within 6 months after the effective date of this AD (February 3, 1995). Repeat inspections at int...

Why matched: Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Series Airplanes

92-22-03

final rule

Airworthiness Directives; BRITISH AEROSPACE Viscount Model 744, 745D, and 810 Series Airplanes

Unsafe Condition: Structural failure of the rear pressure bulkhead and associated decompression of the passenger cabin due to corrosion, cracks, and damage.

Effective: Dec 3, 1992 Category: aircraft Compliance: Within 90 days after the effective date of this AD, and repeat inspections at intervals not to ex...

Why matched: Airworthiness Directives; BRITISH AEROSPACE Viscount Model 744, 745D, and 810 Series Airplanes

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

92-14-06

final rule

Airworthiness Directives; BRITISH AEROSPACE Model Viscount 810 Series Airplanes

Unsafe Condition: Loss of elevator structural integrity and reduced controllability of the airplane due to skin quilting, corrosion, and delamination on the elevator lower skins.

Effective: Aug 20, 1992 Category: aircraft Compliance: Within 60 days after the effective date of this AD

Why matched: Airworthiness Directives; BRITISH AEROSPACE Model Viscount 810 Series Airplanes

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

92-11-05

final rule

Airworthiness Directives; BRITISH AEROSPACE Viscount Models 744, 745D and 810 Series Airplanes

Unsafe Condition: Reduced structural integrity of the engine mount attachment to the wing and wing structure due to improper fastener edge distance on the upper boom of the wing rib at wing station 257, left and right.

Effective: Jul 9, 1992 Category: aircraft Compliance: Within 100 landings or within 4 months after the effective date of this AD, whichever occurs earlier

Why matched: Airworthiness Directives; BRITISH AEROSPACE Viscount Models 744, 745D and 810 Series Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

92-09-04

final rule

Airworthiness Directives; BRITISH AEROSPACE All Viscount Model 744, 745D, and 810 Series Airplanes

Unsafe Condition: Failure of one or more of the landing gears due to obstructions, burrs, damaged plating, or damaged bores in the shuttle valve elbow connections, shuttle, and retraction jack assemblies.

Effective: Jun 2, 1992 Category: aircraft Compliance: Within 500 hours time in-service or within 6 months after the effective date of this AD, whicheve...

Why matched: Airworthiness Directives; BRITISH AEROSPACE All Viscount Model 744, 745D, and 810 Series Airplanes

91-26-01

final rule

Airworthiness Directives; BRITISH AEROSPACE Viscount Model 744, 745D, and 810 Series Airplanes

Unsafe Condition: Corrosion of the mild steel balance weights and the forward face of the leading edge members could reduce controllability of the airplane.

Effective: Mar 23, 1992 Category: aircraft Compliance: Within 180 days after the effective date of this AD, and thereafter at intervals not to exceed 4 ...

Why matched: Airworthiness Directives; BRITISH AEROSPACE Viscount Model 744, 745D, and 810 Series Airplanes

91-18-06

final rule

Airworthiness Directives; BRITISH AEROSPACE Viscount Model 744, 745D, and 810 Series Airplanes

Unsafe Condition: Cracks in the wing flap guide rails and corrosion at the abutment face of flap guide rails and flap end ribs on landing flaps could reduce structural integrity of the landing flaps.

Effective: Sep 23, 1991 Category: aircraft Compliance: Within 180 days after the effective date of this AD, or prior to the accumulation of 500 landings...

Why matched: Airworthiness Directives; BRITISH AEROSPACE Viscount Model 744, 745D, and 810 Series Airplanes

91-14-16

final rule

Airworthiness Directives; British Aerospace Viscount Model 744 and 745D Series Airplanes and Model 810 Series Airplanes

Unsafe Condition: Reduced structural integrity of the wings due to an incorrectly manufactured shear pin, Part No. 80203-3009, in the upper break-joint.

Effective: Aug 9, 1991 Category: aircraft Compliance: Within 200 hours time-in-service or within 90 days after the effective date of this AD, whichever...

Why matched: Airworthiness Directives; British Aerospace Viscount Model 744 and 745D Series Airplanes and Model 810 Series Airplanes

91-14-18

final rule

Airworthiness Directives; BRITISH AEROSPACE Viscount Model 744, 745D, and 810 Series Airplanes

Unsafe Condition: Reduced structural integrity of the wings due to corrosion along the total length of the top surface of the left and right wing spar upper boom.

Effective: Aug 6, 1991 Category: aircraft Compliance: Within 180 days after the effective date of this AD, and thereafter at intervals not to exceed 18...

Why matched: Airworthiness Directives; BRITISH AEROSPACE Viscount Model 744, 745D, and 810 Series Airplanes

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

91-11-12

final rule

Airworthiness Directives; British Aerospace Viscount Model 810 Series Airplanes

Unsafe Condition: In-flight separation of an entrance or emergency door from the airplane and subsequent decompression of the passenger cabin due to incorrectly machined door operating torque shaft coupling sleeves.

Effective: Jul 1, 1991 Category: aircraft Compliance: Within 90 days after the effective date of this AD

Why matched: Airworthiness Directives; British Aerospace Viscount Model 810 Series Airplanes

88-14-04

final rule

Airworthiness Directives; BRITISH AEROSPACE Model 700 and 800 Series Airplanes

Unsafe Condition: Corrosion of the wing upper surface and main spar upper cap could lead to structural failure of the wing.

Effective: Sep 6, 1988 Category: aircraft Compliance: Within 7 days after the effective date of this AD, and thereafter at intervals not to exceed 12 m...

Why matched: Airworthiness Directives; BRITISH AEROSPACE Model 700 and 800 Series Airplanes

87-23-03

final rule

Airworthiness Directives; BRITISH AEROSPACE Model 700, 800, and 810 Series Airplanes

Unsafe Condition: Failure of the wing due to cracking.

Effective: Dec 9, 1987 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; BRITISH AEROSPACE Model 700, 800, and 810 Series Airplanes

87-22-04

final rule

Airworthiness Directives; BRITISH AEROSPACE Model 700 and 800 Series Airplanes

Unsafe Condition: Failure of landing gear ram feet

Effective: Nov 13, 1987 Category: aircraft Compliance: Within 30 days or 120 landings after the effective date of this AD, whichever occurs first

Why matched: Airworthiness Directives; BRITISH AEROSPACE Model 700 and 800 Series Airplanes

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

86-16-09

final rule

Airworthiness Directives; BRITISH AEROSPACE VISCOUNT Model 800 Series Airplanes

Unsafe Condition: Nose landing gear collapse as a result of a faulty hydraulic cut out valve (Part Number AIR 41916).

Effective: Sep 8, 1986 Category: aircraft Compliance: Within the next 1,000 hours time-in-service or nine months after the effective date of this AD, w...

Why matched: Airworthiness Directives; BRITISH AEROSPACE VISCOUNT Model 800 Series Airplanes

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

84-07-03 R1

final rule

Airworthiness Directives; BRITISH AEROSPACE Model 700 Series and 800 Series Airplanes

Unsafe Condition: Collapse of the nose landing gear

Effective: Mar 24, 1986 Category: aircraft Compliance: Within the next six months after the effective date of this AD, unless previously accomplished wi...

Why matched: Airworthiness Directives; BRITISH AEROSPACE Model 700 Series and 800 Series Airplanes

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

86-02-05

final rule

Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes

Unsafe Condition: Nose landing gear collapse as a result of a faulty hydraulic cut out valve (Part Number AIR 41916).

Effective: Feb 3, 1986 Category: aircraft Compliance: Within the next 1000 hours time-in-service or nine months after the effective date of this AD, wh...

Why matched: Airworthiness Directives; BRITISH AEROSPACE Model 700 Series Airplanes

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