Cessna Citation M2 series airworthiness directives

• AD 2024-15-09

  Effective 2024-10-22

  Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes

  This AD was prompted by a report of the potential for a failure of the ATLAS system in which a loss of load alleviation would be un- annunciated.

  This AD applies to Textron Aviation Inc. (type certificate previously held by Cessna Aircraft Company) Model 525, 525A, and 525B airplanes, all serial numbers (S/Ns), certificated in any category, with Tamarack active technology load alleviation system (ATLAS) winglets installed in accordance with Supplemental Type Cer...

• AD 2020-24-06

  Effective 2020-12-28

  Textron Aviation, Inc., (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes

  This AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

  This AD applies to Textron Aviation, Inc. (type certificate previously held by Cessna Aircraft Company) Models 525, 525A, and 525B airplanes, certificated in any category, with Tamarack active load alleviation system (ATLAS) winglets installed in accordance with Supplemental Type Certificate SA03842NY.

• AD 2019-08-13

  Effective 2019-05-24 · superseded or removed

  Textron Aviation, Inc. Airplanes

  This AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

  This AD applies to Textron Aviation, Inc. (type certificate previously held by Cessna Aircraft Company) Models 525, 525A, and 525B airplanes, certificated in any category, with Tamarack active load alleviation system (ATLAS) winglets installed in accordance with Supplemental Type Certificate (STC) SA03842NY.

• AD 2014-18-01

  Effective 2014-10-14

  Rockwell Collins, Inc. Transponders

  This AD was prompted by instances where the TDR-94 and TDR-94D Mode S transponders did not properly respond to Mode S Only All-Call interrogations when the airplane transitioned from a ground to airborne state.

  (1) This AD applies to the following Rockwell Collins, Inc. part number (P/N) Mode S transponders that are known to be installed on but not limited to the airplanes listed in paragraphs (c)(2)(i) through (c)(2)(xiv) of this AD, except for those airplanes listed in paragraphs (c)(3)(i) through (c)(3)(vi) of this AD, tha...

• AD 2013-08-05

  Effective 2013-05-30

  Cessna Aircraft Company Airplanes

  This AD was prompted by reports of smoke and/or fire in the tailcone caused by brushes wearing beyond their limits on the A/C motor.

  This AD applies to Cessna Aircraft Company Model 525 airplanes, serial number (S/N) 525-0001 through 525-0558 and 525-0600 through 525-0701, that (1) are equipped with part number (P/N) 1134104-1 or 1134104-5 air conditioning (A/C) compressor motor; and (2) are certificated in any category.

• AD 2006-16-18

  Effective 2008-07-18

  Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes

  We are issuing this AD to prevent a bearing error, which could lead to an airplane departing from its scheduled flight path, which could result in a reduction in separation from, and a possible collision with, other aircraft or terrain.

  This AD applies to Sandel Avionics Incorporated (Sandel) Model ST3400 terrain awareness warning system/radio magnetic indicator (TAWS/RMI) units approved under Technical Standard Order(s) C113, C151a, or C151b; as identified in Sandel ST3400 Service Bulletin SB3400-01, Revision B, dated September 15, 2004; as installed...

• AD 2008-12-01

  Effective 2008-07-16

  Cessna Aircraft Company Model 525 Airplanes

  We are issuing this AD to detect and correct missing firewall sealant between the aft firewall assembly and seal assembly, which could result in failure of the fire extinguishing system to prevent the spread of fire through the firewall gap.

  This AD applies to Model 525 airplanes, serial numbers 525- 0600 through 525-0662, that are certificated in any category.

• AD 2008-03-10

  Effective 2008-03-11

  Cessna Aircraft Company Models 525, 525A, and 525B Airplanes

  We are issuing this AD to detect and correct any damage from corrosion on the airplane structure.

  This AD applies to the following airplane models and serial numbers that have a cockpit mounted pilot relief tube installed and are certificated in any category: Models Serial No. (1) 525: 0001 through 0637. (2) 525A: 0001 through 0347. (3) 525B: 0001 through 0152.

• AD 2005-17-11

  Effective 2005-10-07

  The Cessna Aircraft Company Models 525, 525A, and 525B Airplanes

  This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. 525: 525-0001 through 525-0600. 525A: 525A-0001 through 525A-0234. 525B: 525B-0001 through 525B-0035.

• AD 2004-14-20

  Effective 2004-08-23

  The Cessna Aircraft Company Model 525 Airplanes

  This AD affects Model 525 airplanes with the following serial numbers that are certificated in any category: (1) Group 1 (maintains the actions from AD 2003-21-07): 525- 0001, 525-0002, and 525-0004 through 525-0159. (2) Group 2: 525-0160 through 525-0359.

• AD 2004-08-15

  Effective 2004-06-07

  Goodrich Avionics Systems, Inc. TAWS8000 Terrain Awareness Warning System

  This AD affects all airplane models and serial numbers, certificated in any category, that incorporate a Goodrich TAWS8000 terrain awareness warning system (TAWS), part number (P/N) 805- 18000-001, with "Mod None", "Mod A", or "Mod B" hardware installed. This list of airplanes that have the TAWS8000 TWAS installed incl...

• AD 2003-21-07

  Effective 2003-10-22 · superseded or removed

  The Cessna Aircraft Company Model 525 Airplanes

  We are issuing this AD to correct this single-point failure in the electric pitch trim system, which will result in a runaway pitch trim condition where the pilot could not disconnect using the control wheel autopilot/trim disconnect switch.

  This AD affects Model 525 airplanes, serial numbers 525- 0001, 525-0002, and 525-0004 through 525-0159, that are certificated in any category.

• AD 2002-20-09

  Effective 2002-11-12

  Rockwell Collins, Inc. AFD-3010 Adaptive Flight Display Units

  This AD applies to AFD-3010 adaptive flight display units, part numbers 822-1084-012/- 108/-202/-206/-302/-304/-402/-404/-406 (serial numbers as specified in Rockwell Collins Service Bulletin 12, Revision No. 2, AFD-3010- 31-12, dated August 30, 2002), that are installed in aircraft. These AFD-3010 adaptive flight disp...

• AD 2001-23-17

  Effective 2001-12-28

  GARMIN International GNS 430 Units

  This AD applies to the GNS 430 units that are specified in paragraph (a)(1) of this AD and are installed on aircraft. These GNS 430 units are installed in, but not limited to, aircraft that are certificated in any category and presented in paragraph (a)(2) of this AD: (1) GNS 430 Units, part number 011-00280-00: serial...

• AD 2001-02-13

  Effective 2001-02-28

  The Cessna Aircraft Company Model 525 (CitationJet 1) Airplanes

  This AD applies to Model 525 (CitationJet 1) airplanes, serial numbers 525-0360 through 525-0400, that: (1) incorporate a direct current (DC) power battery switch, Eaton part number A3-205-01/P; and (2) are certificated in any category. (b) Who must comply with this AD? Anyone who wishes to operate any of the above air...

• AD 99-07-04

  Effective 1999-05-24

  Williams International, L.L.C. FJ44-1A Turbofan Engines

  To prevent high pressure turbine (HPT) disk rim failure, which could result in an uncontained engine failure and damage to the aircraft.

  Williams International, L.L.C. FJ44-1A turbofan engines, installed on but not limited to Cessna 525 series aircraft.

• AD 97-05-03

  Effective 1999-04-20

  AlliedSignal Avionics, Inc. Models GNS- Xls and GNS-Xl Flight Management Systems

  To prevent deviation from an intended flight path during a non- precision approach to an airport caused by inaccurate information from the GPS flight management system.

  Models GNS-Xls and GNS-Xl global positioning systems (GPS), part numbers (P/N) 17960-0102-XXXX and P/N 18355- 0101-XXXX, respectively, installed on, but not limited to the following aircraft, certificated in any category: Manufacturer Models British Aerospace, Ltd. (BAe): 146-100A and 146-200A Cessna Aircraft Corporati...

• AD 97-01-05

  Effective 1997-01-21 · recurring

  Williams International, L.L.C. Model FJ44-1A Turbofan Engines

  To prevent possible high pressure turbine (HPT) disk blade retention post separations and the release of their retained turbine blades, subsequent loss of engine power, and possible high disk speed uncontained liberation of disk posts and the turbine blades, which could cause aircraft damage.

  Williams International L.L.C. Model FJ44-1A turbofan engines, with serial numbers 1001-1179, 1196, and 1197, installed on, but not limited to, Cessna Citation Model 525 aircraft.

• AD 97-01-02

  Effective 1997-01-15 · recurring

  Cessna Aircraft Company Model 525 Airplanes

  To prevent main landing gear (MLG) collapse caused by trunnion bearing failure, which could result in loss of control of the airplane during landing operations.

  Model 525 airplanes (serial numbers 525-0001 through 525-0153), certificated in any category.

Cessna Citation M2 series: price, specs and every tail

AD data from the Federal Register and the FAA. Data: Radar, FAA aircraft registry file of 2026-10-09.