Reims Aviation S.A. Airworthiness Directives

23 ADs indexed for Reims Aviation S.A. aircraft.

Models

F406 11 ADs F406 4 ADs 402B 3 ADs 402C 3 ADs 404 3 ADs 421B 3 ADs 421C 3 ADs 441 3 ADs 152 2 ADs 172N 2 ADs 172P 2 ADs 172Q 2 ADs 172RG 2 ADs 180K 2 ADs 182Q 2 ADs 182R 2 ADs 310R 2 ADs 335 2 ADs 340A 2 ADs 401 2 ADs 402 2 ADs 402A 2 ADs 414 2 ADs 414A 2 ADs 421 2 ADs 421A 2 ADs 425 2 ADs A152 2 ADs A185F 2 ADs F152 2 ADs F172N 2 ADs F172P 2 ADs F182Q 2 ADs FA152 2 ADs FR172K 2 ADs FR182 2 ADs R172K 2 ADs R182 2 ADs T182 2 ADs T303 2 ADs TR182 2 ADs 150 1 AD 150A 1 AD 150B 1 AD 150C 1 AD 150D 1 AD 150E 1 AD 150F 1 AD 150G 1 AD 150H 1 AD 150J 1 AD 150K 1 AD 150L 1 AD 150M 1 AD 172 1 AD 172A 1 AD 172B 1 AD 172C 1 AD 172D 1 AD 172E 1 AD 172F (USAF T-41A) 1 AD 172G 1 AD 172H (USAF T-41A) 1 AD 172I 1 AD 172K 1 AD 172L 1 AD 172M 1 AD 175 1 AD 175A 1 AD 175B 1 AD 175C 1 AD 177 1 AD 177A 1 AD 177B 1 AD 177RG 1 AD 180 1 AD 180A 1 AD 180B 1 AD 180C 1 AD 180D 1 AD 180E 1 AD 180F 1 AD 180G 1 AD 180H 1 AD 180J 1 AD 182 1 AD 182A 1 AD 182B 1 AD 182C 1 AD 182D 1 AD 182E 1 AD 182F 1 AD 182G 1 AD 182H 1 AD 182J 1 AD 182K 1 AD 182L 1 AD 182M 1 AD 182N 1 AD 182P 1 AD 185 1 AD 185A 1 AD 185B 1 AD 185C 1 AD 185D 1 AD 185E 1 AD 188 1 AD 188A 1 AD 188B 1 AD 206 1 AD 207 1 AD 207A 1 AD 208 1 AD 208B 1 AD 210 1 AD 210-5 (205) 1 AD 210-5A (205A) 1 AD 210A 1 AD 210B 1 AD 210C 1 AD 210D 1 AD 210E 1 AD 210F 1 AD 210G 1 AD 210H 1 AD 210J 1 AD 210K 1 AD 210L 1 AD 210M 1 AD 210N 1 AD 210R 1 AD 310P 1 AD 310Q 1 AD 336 1 AD 337 1 AD 337A 1 AD 337B 1 AD 337C 1 AD 337D 1 AD 337E 1 AD 337F 1 AD 337G 1 AD 337H 1 AD 340 1 AD 401A 1 AD 401B 1 AD 411 1 AD 411A 1 AD A150K 1 AD A150L 1 AD A150M 1 AD A185E 1 AD A188 1 AD A188A 1 AD A188B 1 AD F150F 1 AD F150G 1 AD F150H 1 AD F150J 1 AD F150K 1 AD F150L 1 AD F150M 1 AD F172D 1 AD F172E 1 AD F172F 1 AD F172G 1 AD F172H 1 AD F172K 1 AD F172L 1 AD F172M 1 AD F177RG 1 AD F182P 1 AD F337E 1 AD F337F 1 AD F337G 1 AD F337H 1 AD FA150K 1 AD FA150L 1 AD FR172E 1 AD FR172F 1 AD FR172G 1 AD FR172H 1 AD FR172J 1 AD FRA150L 1 AD FRA150M 1 AD FT337E 1 AD FT337F 1 AD FT337GP 1 AD FT337HP 1 AD M337B 1 AD P172D 1 AD P206A 1 AD P206B 1 AD P206C 1 AD P206D 1 AD P206E 1 AD P210N 1 AD P210R 1 AD P337H 1 AD R172E 1 AD R172F 1 AD R172G 1 AD R172H 1 AD R172J 1 AD T188C 1 AD T207 1 AD T207A 1 AD T210F 1 AD T310P 1 AD T310R 1 AD T337B 1 AD T337C 1 AD T337D 1 AD T337E 1 AD T337F 1 AD T337G 1 AD T337H 1 AD T337H-SP 1 AD TP206A 1 AD TP206B 1 AD TP206C 1 AD TP206D 1 AD TP206E 1 AD TU206A 1 AD TU206B 1 AD TU206C 1 AD TU206D 1 AD TU206E 1 AD TU206F 1 AD TU206G 1 AD U206 1 AD U206A 1 AD U206B 1 AD U206C 1 AD U206D 1 AD U206E 1 AD U206F 1 AD U206G 1 AD Various 1 AD

Recent ADs

2021-23-09

final rule

Airworthiness Directives; ASI Aviation (Type Certificate Previously Held by Reims Aviation S.A.) Airplanes

Unsafe Condition: An occurrence was reported where one pilot rudder control pedal of an F 406 aeroplane detached in flight. No change in aeroplane attitude occurred. The rudder was controlled using the co-pilot rudd...

Effective: Jan 10, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; ASI Aviation (Type Certificate Previously Held by Reims Aviation S.A.) Airplanes

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

2021-22-21

final rule

Airworthiness Directives; ASI Aviation (Type Certificate Previously Held by Reims Aviation S.A.) Airplanes

Unsafe Condition: failure of a circuit breaker (CB) switch, which could lead to smoke and/or burning smell in the cockpit, possibly resulting in reduced control of the aeroplane.

Effective: Jan 3, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; ASI Aviation (Type Certificate Previously Held by Reims Aviation S.A.) Airplanes

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

2016-19-15

final rule

Airworthiness Directives; REIMS AVIATION S.A. Airplanes

Unsafe Condition: Cracks found in the horizontal stabilizer rear attach structure and the vertical fin rear spar attach structure.

Effective: Nov 2, 2016 Category: aircraft Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; REIMS AVIATION S.A. Airplanes

Amdt-39-18328

final rule

Airworthiness Directives; REIMS AVIATION S.A. Airplanes

Unsafe Condition: Detachment of the pilot's rudder control pedal in flight.

Effective: Dec 28, 2015 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; REIMS AVIATION S.A. Airplanes

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

2015-16-07

final rule

Airworthiness Directives; REIMS AVIATION S.A. Airplanes

Unsafe Condition: Detachment of the pilot's rudder control pedal in flight.

Effective: Aug 18, 2015 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; REIMS AVIATION S.A. Airplanes

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

2013-06-04

final rule

Airworthiness Directives; REIMS AVIATION S.A. Airplanes

Unsafe Condition: Fretting (wear and/or chafing) found between the elevator pushrod assembly and the horizontal tail structure, which could cause the elevator pushrod to jam and could result in loss of control.

Effective: May 3, 2013 Category: aircraft Compliance: Within 4 months after May 3, 2013

Why matched: Airworthiness Directives; REIMS AVIATION S.A. Airplanes

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

2013-04-02

final rule

Airworthiness Directives; Reims Aviation S.A. Airplanes

Unsafe Condition: Improper material used in nose landing gear (NLG) attachment brackets, Part Number 6013119-1, could lead to failure of the NLG bracket with consequent damage to the airplane while landing.

Effective: Mar 28, 2013 Category: aircraft Compliance: Within 25 hours time-in-service (TIS) after March 28, 2013, or within the next 30 days after Marc...

Why matched: Airworthiness Directives; Reims Aviation S.A. Airplanes

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

2011-07-03

final rule

Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

Unsafe Condition: Cracks in rudder pulley brackets, Part Number 6015511-1, installed on Reims F406 airplanes with the optional 'Camera Hole' modification. This could result in the loss of rudder control on the airpl...

Effective: Apr 26, 2011 Category: aircraft Compliance: Within 10 hours time-in-service after February 13, 2007, for initial inspection. Repetitive inspe...

Why matched: Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

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

Amdt-39-16067

final rule

Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

Unsafe Condition: Leaks of the landing gear emergency blowdown bottle have been reported due to a design deficiency in the bottle head, potentially leading to insufficient internal bottle pressure and malfunction du...

Effective: Dec 4, 2009 Category: aircraft Compliance: Within 50 flight hours after the effective date of December 4, 2009.

Why matched: Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

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

2007-26-08 R1

final rule

Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

Unsafe Condition: Leaks of the landing gear emergency blowdown bottle have been reported due to a design deficiency in the bottle head, resulting in potential failure to maintain internal pressure and malfunction du...

Effective: Dec 4, 2009 Category: aircraft

Why matched: Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

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

2007-26-08

final rule

Airworthiness Directives; REIMS AVIATION S.A. Model F406 Airplanes

Unsafe Condition: Leaks of the landing gear emergency blowdown bottle have been reported, caused by a design deficiency in the bottle head, leading to leakage on the nut manometer. If uncorrected, this could result ...

Effective: Jan 31, 2008 Category: aircraft Compliance: Within 12 calendar months after January 31, 2008

Why matched: Airworthiness Directives; REIMS AVIATION S.A. Model F406 Airplanes

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

2007-11-04

final rule

Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

Unsafe Condition: Important corrosion found on the ailerons bearings, which, if left uncorrected, could result in the loss of roll control on the airplane.

Effective: Jun 26, 2007 Category: aircraft Compliance: Within the next 100 hours time-in-service or 3 months, whichever occurs first after the effective...

Why matched: Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

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

2007-10-02

final rule

Airworthiness Directives; REIMS AVIATION S.A. Model F406 Airplanes

Unsafe Condition: Corrosion on the bearings with propagation to the bracket-hinge of the rudder. This corrosion has been discovered after rudder removals. This condition, if left uncorrected, could result in the los...

Effective: Jun 13, 2007 Category: aircraft Compliance: Within 100 hours time-in-service (TIS) or 3 months after the effective date of this AD, whichever...

Why matched: Airworthiness Directives; REIMS AVIATION S.A. Model F406 Airplanes

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

2007-09-02

final rule

Airworthiness Directives; REIMS AVIATION S.A. Model F406 Airplanes

Unsafe Condition: Cracks have been discovered about the left and right rib at the connection of the center wing and the fuselage localized at fuselage station FS160.80. Cracks spreading in the rib could result in st...

Effective: May 31, 2007 Category: aircraft Compliance: Within the next 600 hours time-in-service or the next 12 months after the effective date of this ...

Why matched: Airworthiness Directives; REIMS AVIATION S.A. Model F406 Airplanes

2007-05-09

final rule

Airworthiness Directives; REIMS AVIATION S.A. Model F406 Airplanes

Unsafe Condition: unsafe condition on an aviation product.

Effective: Apr 11, 2007 Category: aircraft

Why matched: Airworthiness Directives; REIMS AVIATION S.A. Model F406 Airplanes

2007-02-12

final rule

Airworthiness Directives; Reims Aviation S.A. F406 Airplanes

Unsafe Condition: unsafe condition on an aviation product.

Effective: Feb 13, 2007 Category: aircraft

Why matched: Airworthiness Directives; Reims Aviation S.A. F406 Airplanes

2003-09-09 R1

final rule

Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Airplanes

Unsafe Condition: Chafing and/or arcing of the fuel boost pump wiring could result in arcing within the wing fuel storage system, leading to ignition of explosive vapor within the fuel storage system.

Effective: Jan 22, 2004 Category: aircraft Compliance: Initially within the next 25 hours time-in-service or 60 days after May 31, 2002, whichever occur...

Why matched: Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Airplanes

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

2001-23-07 Recurring

final rule

Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes; Correction

Unsafe Condition: Cracks in the canted rib upper cap in the center wing carry-through area.

Effective: Jan 7, 2002 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

2001-01-07 Recurring

final rule

Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes

Unsafe Condition: Cracks in the canted rib upper cap in the center wing carry-through area, which could result in structural failure of the wing with possible loss of control of the airplane.

Effective: Jan 7, 2002 Category: aircraft Compliance: Within the next 75 hours time-in-service (TIS) after January 7, 2002.

Why matched: Airworthiness Directives; Airbus Model A300 B2, A300 B4, A300 B4-600, A300 B4-600R, A300 F4-600R, and A310 Series Airplanes

98-04-28

final rule

Airworthiness Directives; Cessna Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414, 414A, 421B, 421C, 425, and 441 Airplanes.

Unsafe Condition: Flight in freezing rain, freezing drizzle, or mixed icing conditions may result in ice build-up on protected surfaces exceeding the capability of the ice protection system, or may result in ice for...

Effective: Mar 13, 1998 Category: aircraft Compliance: Within 30 days after the effective date of this AD (March 13, 1998).

Why matched: Airworthiness Directives; Cessna Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414, 414A, 421B, 421C, 425, and 441 Airplanes.

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