Airworthiness Directive Lookup Free FAA AD search by N-number, make or model
Find the FAA airworthiness directives that may apply to an aircraft: 12,857 ADs from the Federal Register since 1995, through Oct 1, 2026, each with its applicability text and the official document. Free, no account.
Showing ADs for the Cessna Citation CJ3. Matched on type certificate model 525B.
RESULTS
9 ADs in effect may apply to Cessna Citation CJ3
- In effect9
- Recurring0
- Superseded or removed2
Informational only. These are FAA airworthiness directives whose published applicability names this make and model. Whether an AD applies to a particular aircraft depends on its serial number, installed engines, propellers, parts and modifications, and some ADs listed here will not apply. This list is not the official AD record and not a compliance determination: confirm applicability and compliance against the FAA’s Dynamic Regulatory System and the aircraft’s records with a certificated mechanic or inspector. Covers ADs published in the Federal Register since 1995, through Oct 1, 2026; older ADs, and engine, propeller and appliance ADs that do not name the aircraft, are not included.
Show only ADs in effect Every Cessna Citation CJ3 AD on one page
- AD 2026-03-06 One-time
Textron Aviation, Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes
This AD was prompted by the manufacturer's revision of the aircraft maintenance manual (AMM) to introduce more restrictive inspection intervals.
Applicability, as the AD words it
This AD applies to all Textron Aviation, Inc. (Type Certificate previously held by Cessna Aircraft Company) Model 525B airplanes, certificated in any category.
- AD 2024-15-09 One-time
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.
Applicability, as the AD words it
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 Certificate No. SA03842NY.
- AD 2021-05-17 One-time Appliance
Rockwell Collins, Inc. Flight Display System Application
This AD was prompted by a conflict between the traffic collision avoidance system (TCAS) primary display indications and aural alerts during a resolution advisory (RA) scenario.
Applicability, as the AD words it
This AD applies to Rockwell Collins, Inc., (Rockwell Collins) Flight Display System Application FDSA-6500 part numbers (P/Ns) 810- 0234-1H0001, 810-0234-1H0002, 810-0234-1H0003, 810-0234-2H0001, 810- 0234-2C0001, 810-0234-2C0002, and 810-0234-4B0001. These applications are installed on, but not limited to, Bombardier Inc. Model CL-600-2B16 (604 variant) airplanes and Textron Aviation Inc. Models 525B, B200, B200C, B200CGT, B200GT, B300, B300C, and C90GTi airplanes, certificated in any category.
- AD 2020-24-06 One-time
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.
Applicability, as the AD words it
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 2019-12-09 Superseded by AD 2021-05-17 Appliance
Rockwell Collins, Inc. Flight Display System Application
This AD was prompted by a conflict between the traffic collision avoidance system (TCAS) primary display indications and aural alerts during a resolution advisory (RA) scenario.
Applicability, as the AD words it
This AD applies to Rockwell Collins, Inc. (Rockwell Collins) Flight Display System Application FDSA-6500 part numbers 810-0234- 1H0001, 810-0234-1H0002, 810-0234-1H0003, 810-0234-2H0001, 810-0234- 2C0001, 810-0234-2C0002, and 810-0234-4B0001. These appliances are installed on, but not limited to, Bombardier Inc. Model CL-600-2B16 (604 variant) airplanes and Textron Aviation Inc. Models 525B, B200, B200C, B200CGT, B200GT, B300, B300C, and C90GTi airplanes, certificated in any category.
- AD 2019-08-13 Superseded by AD 2020-24-06
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.
Applicability, as the AD words it
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 One-time Appliance
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.
Applicability, as the AD words it
(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, that have been modified in-production or in-service: (i) TDR-94: CPN 622-9352-008, 622-9352-108, 622-9352-308, 622- 9352-408; and (ii) TDR-94D: CPN 622-9210-008, 622-9210-108, 622-9210-308, 622- 9210-408. (2) The products listed in paragraphs (c)(1)(i) and (c)(1)(ii) of this AD may be installed on but not limited to the following airplanes featuring weight-on wheels input to the transponder, certificated in any category: (i) ATR42 and ATR72; (ii) Bombardier (Canadair) CL-600-2B16 (604 Variant); (iii) Bombardier CL-600-2B19 (RJ100 and RJ200); (iv) Cessna 525, serial numbers (S/N) 525-0600 through 525-0684 (CJ1); (v) Cessna 525A, S/N 525A-0300 through 525A-0438 (CJ2); (vi) Cessna 525B, S/N 525B-0001 through 525B-0293 (CJ3); (vii) Cessna 560, S/N 560-0751 through 560-0802 (Citation Encore); (viii) Cessna 560XL, S/N 560-6001 and subsequent; (ix) Dassault Aviation Mystere-Falcon 50; (x) Dassault Aviation Mystere-Falcon 900; (xi) Dassault Aviation Falcon 2000; (xii) Dassault Aviation Falcon 2000EX; (xiii) Piaggio Aero Industries P.180 (Avanti and Avanti II); and (xiv) SAAB 2000. (3) This AD action does not apply to the excepted airplane models, identified in paragraphs (c)(3)(i) through (c)(3)(vi) of this AD, that have been modified in-production or in-service. They do not have the unsafe condition described in this AD. (i) Dassault airplanes that have been modified in-service or in- production following the applicable Dassault Aviation service information as listed in table 1 of paragraph (c)(3)(i) of this AD. Table 1 of Paragraph (c)(3)(i) of This AD: Excepted Dassault Airplanes Airplane models Service bulletin Modification(s) Mystere-Falcon 50: F50-457: M2966 and M2968 Mystere-Falcon 900: F900-354: M3896 Falcon 900EX: F900EX-239: M3896 Falcon 2000: F2000-312: M2624 and M2632 Falcon 2000EX: F2000EX-043: M2624 (ii) Model ATR 42 airplanes or ATR 72 airplanes that had P/N 622-9210-108 transponders installed in production using ATR modification 05614 or installed in-service using ATR Service Bulletin ATR42-34-0167 or ATR Service Bulletin ATR72-34-1094, as applicable. (iii) SAAB Model 2000 airplanes that had P/N 622-9210-008 transponders installed in production using SAAB modifications 6231, 6243, and 6249 or installed in-service using SAAB Service Bulletins 2000-34-066, 2000-34-072, and 2000-34-076. (iv) Bombardier Aerospace (Canadair) airplanes Model CL-600-2B16 (604 Variant) that had P/N 622-9210-008 transponders installed and incorporated the corrective actions recommended in the Bombardier Advisory Wire AW 604-34-0078 using the instructions in Bombardier Aerospace Service Bulletin 604-34-054 (drawing 604-70482 Engineering Order, Revison D-1) or using a service request for product support. Bombardier Aerospace (Canadair) airplanes Model CL-600-2B19 (RJ100 and RJ200) that had P/N 622-9210-008 transponders installed in production using Bombardier Aerospace Modification TC601R16789 or in service using Bombardier Aerospace Service Bulletin 601R-34-142 (Modification TC601R16790). (v) Cessna Aircraft Company Models 525, 525A, and 525B airplanes that had P/N 622-9352-008 transponders installed in production using Cessna Engineering Change Records (ECRs) 55298, 58654, and 59567; and Model 525B airplanes that had P/N 622-9352-008 transponders installed in service using Cessna Aircraft Company Service Bulletin SB525B-34-03 or SB525B-34-08. Cessna Aircraft Company Models 525, 525A, 525B, 560, and 560XL airplanes that had P/N 622-9210-008 transponders installed in production using Cessna ECRs 55298, 58654, 59567, 56135, and 58032; and Model 525B airplanes that had P/N 622- 9210-008 transponders installed in service using Cessna Service Bulletin SB525B-34-03 or SB525B-34-08. (vi) Piaggio Aero Industries Model P.180 (Avanti) airplanes that had P/N 622-9210-008 transponders installed in production using Piaggio modification 80-0773 or in service using Piaggio Service Bulletin SB-80-0227. Piaggio Aero Industries Model P.180 (Avanti II) airplanes that had P/N 622-9210-008 transponders installed in production using Piaggio modification 80-0588 and 80-0598.
- AD 2008-03-10 One-time
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.
Applicability, as the AD words it
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 2007-23-16 One-time
Cessna Aircraft Company, Model 525B Airplanes
We are issuing this AD to correct an incorrect wiring installation and to provide short-circuit protection for all wiring from the aircraft power distribution system.
Applicability, as the AD words it
This AD applies to Model 525B, serial numbers 0001 through 0013 airplanes, that are certificated in any category.
- AD 2005-17-11 One-time
The Cessna Aircraft Company Models 525, 525A, and 525B Airplanes
Applicability, as the AD words it
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 99-07-04 One-time Engine
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.
Applicability, as the AD words it
Williams International, L.L.C. FJ44-1A turbofan engines, installed on but not limited to Cessna 525 series aircraft.
Radar reads the logbooks and ties each AD to the entries that show how and when it was complied with, with recurring ADs due by date and hours.
QUESTIONS
AD lookup questions
Sources: FAA final rules under 14 CFR part 39, from the Federal Register; make and model from the FAA aircraft registry. The FAA’s Dynamic Regulatory System holds the official AD list.
What is an airworthiness directive (AD)?
An airworthiness directive is a legally enforceable rule the FAA issues under 14 CFR part 39 when it finds an unsafe condition in an aircraft, engine, propeller or appliance that is likely to exist in others of the same design. It says which products it applies to and what must be done, and by when: an inspection, a part replacement, a modification or a limitation. No one may operate a product to which an AD applies except in accordance with it.
How do I look up the ADs for my aircraft?
Type the N-number, or the make and model, into the box above. Radar finds the aircraft's make and model in the FAA registry and lists every AD published in the Federal Register whose applicability names it, newest first, with the AD's own applicability text and a link to the official document. The FAA's Dynamic Regulatory System (drs.faa.gov) holds the official list.
Does every AD in the results apply to my aircraft?
Not necessarily. An AD can be limited to serial number ranges, to aircraft with certain parts or modifications installed, or to a configuration. The results are ADs that may apply because they name the make and model. A certificated mechanic or inspector determines applicability against the aircraft's serial number and records, and records how each applicable AD was complied with.
What is the difference between a recurring and a one-time AD?
A one-time AD is complied with once, for example by replacing a part. A recurring (repetitive) AD requires an action again at an interval, such as an inspection every 100 hours or every 12 months, until a terminating action ends it. Radar marks an AD Recurring when its text requires repetitive actions; always read the AD for the intervals.
What does superseded mean?
When the FAA replaces an AD with a new one, the old AD is superseded: its requirements are carried into, or replaced by, the new AD. Results show the ADs in effect by default; superseded and removed ADs can be shown for the history.
Where does this data come from?
The Federal Register, where the FAA publishes every AD as a final rule. Radar reads each one from the Federal Register API (12,857 ADs since 1995) and refreshes the list every weekday. Make and model come from the FAA aircraft registry. ADs issued before 1995 are not in the Federal Register's online edition and are not included.
Are engine and propeller ADs included?
Only when their applicability names the aircraft. Most engine and propeller ADs name the engine or propeller model, so check those by the installed engine and propeller models. Appliance ADs that list the aircraft among those the appliance can be installed on are included and marked Appliance.
Know which ADs apply, and where each one was signed off.
Radar reads every logbook page, typed or handwritten, and builds one searchable record per tail: times, inspections, ADs and components, each tied to the page it came from.