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.
N83MP is a 2012 Hawker Beechcraft B200GT in the FAA registry (aircraft page). Matched on type certificate model B200GT.
RESULTS
3 ADs in effect may apply to N83MP
- In effect3
- Recurring0
- Superseded or removed3
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 N83MP’s registration record
- AD 2025-20-11 One-time
Textron Aviation Inc. Airplanes
This AD was prompted by a report of rudder control pushrod failure during a production ground run caused by sheared rivets off of a rudder control pushrod.
Applicability, as the AD words it
This AD applies to Textron Aviation Inc. Model airplanes, certificated in any category, identified in paragraphs (c)(1) through (4) of this AD. (1) Model B200GT, serial numbers (S/Ns) BY-335, BY-356, BY-443, BY-453, BY-454. (2) Model B200CGT, S/Ns BZ-4 through BZ-9. (3) Model B300, S/Ns FL-1173 through FL-1175 inclusive, FL-1177, FL-1181, FL-1184 through FL-1186 inclusive, FL-1189, FL-1193, FL- 1197 through FL-1202 inclusive, FL-1210, FL-1211, FL-1213, FL-1218, FL-1220 through FL-1222 inclusive, FL-1225, FL-1228 through FL-1230 inclusive, FL-1232, FL-1233, FL-1240 through FL-1242 inclusive, FL- 1244, FL-1245, FL-1249 through FL-1251 inclusive, FL-1253, FL-1257 through FL-1259 inclusive, FL-1262, FL-1265, FL-1266, FL-1269, FL- 1271, FL-1275, FL-1276, FL-1277, FL-1280, FL-1284, FL-1286, FL-1287, FL-1290, FL-1291, FL-1293, FL-1296, FL-1305, FL-1310, FL-1315 through FL-1317 inclusive, FL-1319, and FL-1320. (4) Model B300C, S/Ns FM-78 through FM-86, FM-88, FM-90 through FM-92 inclusive, FM-94, FM-96 through FM-107 inclusive, and FM-110.
- 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 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 2010-26-03 One-time
Hawker Beechcraft Corporation Models B200, B200GT, B300, and B300C Airplanes
This AD was prompted by reports of failures of the pneumatic supply tube for the tail deice system outside the area covered by AD 2008-07-10.
Applicability, as the AD words it
This AD applies to the following Hawker Beechcraft Corporation airplanes that are certificated in any category: Table 1--Affected Airplane Models and Serial Numbers Model Serial numbers B200: BB-1926, BB-1978, and BB-1988 through BB-2000. B200GT: BY-1 through BY-26. B300: FL-427, FL-493, and FL-500 through FL-573. B300C (C-12W): FM-14 through FM-18.
- AD 2008-07-10 Superseded by AD 2010-26-03
Hawker Beechcraft Corporation Models B200, B200GT, B300, and B300C Airplanes
We are issuing this AD to prevent collapsed pneumatic supply tubes, which could result in failure of the tail deice boots to operate.
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. B200: BB-1926, BB-1978, and BB-1988 through BB-2000. B200GT: BY-1 through BY-26. B300: FL-427, FL-493, and FL-500 through FL- 573. B300C: FM-14 through FM-18.
- AD 96-17-10 Superseded by AD 98-06-30
Beech Model 400, 400A, MU-300-10, and 2000 Airplanes, and Model 200, B200, 300, and B300 Series Airplanes
To prevent cracking and subsequent failure of the outflow/safety valves, which could result in rapid decompression of the airplane.
Applicability, as the AD words it
Model 400, 400A, MU-300-10, and 2000 airplanes, Model 200 and B200 series airplanes having a maximum altitude capability of greater than 31,000 feet, and Model 300 and B300 series airplanes; equipped with AlliedSignal outflow/safety valves, as identified in AlliedSignal Aerospace Service Bulletins 103570-21- 4012 and 103648-21-4022, both Revision 1, both dated May 30, 1995; certificated in any category.
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.