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.
N530TM is a 2000 Beech 400A (FJ44-3AP reference) in the FAA registry (aircraft page). Matched on type certificate model 400A.
RESULTS
29 ADs in effect may apply to N530TM
- In effect29
- Recurring2
- Superseded or removed2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.
Also show 2 superseded or removed N530TM’s registration record
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Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Airplanes
Applicability, as the AD words it
This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) airplanes identified in paragraphs (c)(1)(i), (c)(1)(ii), and (c)(1)(iii) of this AD. (i) Model 400 Beechjet airplanes having serial numbers RJ-1 through RJ-65, inclusive. (ii) Model 400A Beechjet airplanes having serial numbers RK-1 through RK-604, inclusive. (iii) Model 400T Beechjet airplanes having serial numbers TT-1 through TT-180, inclusive; and TX-1 through TX-13, inclusive. (2) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Mitsubishi Heavy Industries, Inc. Ltd.) Model MU-300 airplanes, having serial numbers A003SA through A093SA, inclusive.
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Beechcraft Corporation Airplanes
Applicability, as the AD words it
This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(5) of this AD. (1) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Mitsubishi Heavy Industries, Inc. Ltd.) Model MU-300 airplanes, serial numbers A003SA through A093SA inclusive. (2) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400 airplanes, serial numbers RJ-1 through RJ-65 inclusive. (3) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400A airplanes, serial numbers RK-1 through RK-604 inclusive. (4) Beechcraft Corporation (Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400T (T-1A) airplanes, serial numbers TT-1 through TT-180 inclusive. (5) Beechcraft Corporation Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400T (TX), serial numbers TX-1 through TX-13 inclusive.
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Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company; Beech Aircraft Corporation) Airplanes
Applicability, as the AD words it
This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Hawker Beechcraft Corporation (Type Certificate previously held by Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400A airplanes having serial numbers RK-45 and RK-49 through RK-353 inclusive. (2) Hawker Beechcraft Corporation (Type Certificate previously held by Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400A airplanes (marketed as Hawker 400XP airplanes) having serial numbers RK-354 through RK-594 inclusive.
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Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400A and 400T Airplanes
Applicability, as the AD words it
This AD applies to Hawker Beechcraft Corporation (Type Certificate previously held by Raytheon Aircraft Company; Beech Aircraft Corporation) airplanes, certificated in any category; as identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Model 400A airplanes having serial numbers RK-337 through RK-484, RK-486 through RK-570 inclusive, RK-572, RK-573, and RK-575 through RK-577 inclusive. (2) Model 400T airplane having serial number TX-13.
- AD 2009-07-02 One-time
Hawker Beechcraft Corporation Model MU-300-10 Airplanes and Model 400 and 400A Series Airplanes; and Raytheon (Mitsubishi) Model MU-300 Airplanes
We are issuing this AD to prevent sudden shifting of a flightcrew seat, which could impair the flightcrew's ability to control the airplane.
Applicability, as the AD words it
This AD applies to the airplanes specified in Table 1 of this AD, certificated in any category. Table 1--Applicability Manufacturer Model Serial Nos. Hawker Beechcraft Model 400 series RJ-1 through RJ-65 Corporation. airplanes. inclusive. Hawker Beechcraft Model 400A series RK-1 through RK-93 Corporation. airplanes. inclusive. Hawker Beechcraft Model MU-300-10 A1001SA through Corporation. airplanes. A1011SA inclusive. Raytheon (Mitsubishi): Model MU-300 A003SA through airplanes. A091SA inclusive.
- AD 2008-24-10 One-time Engine
Pratt & Whitney Canada Corp. JT15D-5; -5B; -5F; and -5R Turbofan Engines
We are issuing this AD to prevent engine flameouts of one or both engines caused by excessive moisture and freezing in the P3 servo during certain flight conditions.
Applicability, as the AD words it
This AD applies to the following Pratt & Whitney Canada Corp. (P&WC) turbofan engines with compressor air to HMU delivery tube, part number (P/N) 3119150-01 installed: (1) JT15D-5 turbofan engines, serial numbers (SNs) below and including SN PCE-100411. (2) JT15D-5 turbofan engines, SNs below and including SN PCE- JA0818. (3) All JT15D-5B turbofan engines. (4) All JT15D-5F turbofan engines. (5) JT15D-5R turbofan engines SNs below and including SN PCE- JG0104. (6) All JT15D-5 turbofan engines converted to model JT15D-5R by incorporation of P&WC Service Bulletin No. 7605. These engines are installed on, but not limited to, Hawker Beechcraft models 400, 400A, and 400T airplanes.
- AD 2007-24-01 One-time
Hawker Beechcraft Model 400A Series Airplanes
We are issuing this AD to prevent overheating of wire insulation and consequent fire or smoke in the airplane cabin.
Applicability, as the AD words it
This AD applies to Hawker Beechcraft Model 400A series airplanes, certificated in any category; as identified in Raytheon Service Bulletin SB 25-3758, dated June 2006.
- AD 2007-19-05 One-time
Hawker Beechcraft Model 400, 400A, and 400T Series Airplanes
We are issuing this AD to prevent failure of the attachment fasteners on the engine cowling panels, which could result in separation of a panel from the airplane, and consequent damage to airplane structure.
Applicability, as the AD words it
This AD applies to Hawker Beechcraft Model 400, 400A, and 400T series airplanes, certificated in any category; as identified in Raytheon Service Bulletin SB 54-3788, dated December 2006.
- AD 2006-21-02 One-time
Raytheon (Beech) Model 400, 400A, and 400T Series Airplanes; and Raytheon (Mitsubishi) Model MU-300 Airplanes
Applicability, as the AD words it
This AD applies to all Raytheon (Beech) Model 400, 400A, and 400T series airplanes; and Raytheon (Mitsubishi) Model MU-300 airplanes; certificated in any category.
- AD 2006-15-16 One-time
Raytheon (Beech) Model 400 and 400A Series Airplanes
We are issuing this AD to prevent over- voltage conditions of the DC starter generator due to the incompatibility between certain generator control units (GCUs), which could result in the loss of normal electrical power, damage to some electrical components, or blown fuses during flight, and consequent unrecoverable loss of some or all essential equipment.
Applicability, as the AD words it
This AD applies to the airplanes identified in Table 1 of this AD, certificated in any category. Table 1.--Applicability Raytheon (Beech) model-- Serials-- On which-- (1) 400 series airplanes: RJ-1 through RJ- Kit part number (P/N) 65 inclusive. 128-3004-1 P or 128- 3004-3 P has been incorporated (Lucas Aerospace/Goodrich Direct Current (DC) Starter Generator). (2) 400A series airplanes: RK-1 through RK- Kit P/N 128-3004-1 P 23 inclusive. or 128-3004-3 P has been incorporated (Lucas Aerospace/ Goodrich DC Starter Generator).
- AD 2004-22-02 One-time
Raytheon (Beech) Model MU-300-10, 400, 400A, and 400T Series Airplanes; and Raytheon (Mitsubishi) Model Beech MU-300 Airplanes
This AD was prompted by a report of fuel leaking from components in the spoiler mixer bay of several Raytheon (Beech) Model 400A series airplanes.
Applicability, as the AD words it
This AD applies to Raytheon (Beech) Model MU-300-10, 400, 400A, and 400T series airplanes; and Raytheon (Mitsubishi) Model Beech MU-300 airplanes; certificated in any category; as listed in Raytheon Service Bulletin SB 53-3486, dated June, 2003.
- AD 2004-08-15 One-time Appliance
Goodrich Avionics Systems, Inc. TAWS8000 Terrain Awareness Warning System
Applicability, as the AD words it
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 includes, but is not limited to, the following airplanes. Airplanes that are not in this list and have the TAWS installed through field approval or other methods are still affected by this AD: Company Models Cessna Aircraft Company: 421, 500, 501, 525, 525A, 550, 551, 650, and S550 DASSAULT AVIATION: Mystere-Falcon 20 series Gulfstream Aerospace LP: 1125 Westwind Astra Raytheon Aircraft Company: 100, 200, 300, 400A, and F90 Sabreliner Corporation: NA-265 The New Piper Aircraft Inc: PA-42-1000
- AD 2004-03-35 One-time
Raytheon Model Beech 400A and 400T Series Airplanes
To prevent intermittent sticking of the relays on the roll trim printed circuit board (PCB) in either the open or closed position, which could result in an out-of-trim condition that could require using considerable control wheel force to keep the wings level, and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model Beech 400A series airplanes having serial numbers RK-45, and RK-49 through RK-322 inclusive; and Model 400T series airplanes having serial numbers TT-1 through TT-180 inclusive, and TX-1 through TX-12 inclusive; certificated in any category.
- AD 2003-10-13 One-time
Raytheon Model Beech 400A and 400T Series Airplanes
To prevent leakage of oxygen from scored low-pressure oxygen tubing, which could result in lack of available oxygen for the flightcrew, possible explosion, or fire.
Applicability, as the AD words it
Model Beech 400A series airplanes, serial numbers RK-232 through RK-265 inclusive; and Model Beech 400T series airplane having serial number TX-10; certificated in any category.
- AD 2002-01-23 Recurring
Raytheon Model Beech 400, 400A, and 400T Series Airplanes; Model Beech MU-300-10 Airplanes; and Model Mitsubishi MU-300 Airplanes
To prevent failure of the engine mount and possible loss of the engine, and consequent loss of control of the airplane.
Applicability, as the AD words it
The following airplanes, certificated in any category: Table 1.--Applicability Model Serial Numbers Beech 400 series airplanes: RJ-1 through RJ-65 inclusive. Beech 400A series airplanes: RK-1 and subsequent. Beech 400T series airplanes: TT-1 through TT-180 inclusive. Beech 400T-1 airplanes: TX-1 through TX-11 inclusive. Beech MU-300-10 airplanes: A1001SA through A1011SA inclusive. Mitsubishi MU-300 airplanes: A003SA through A091SA inclusive.
- AD 2001-24-11 One-time
Raytheon Model Beech 400, 400A, and 400T Series Airplanes, Model Mitsubishi MU-300 Airplanes, and Model Beech MU-300-10 Airplanes
To prevent reduced controllability of the airplane due to loss of airspeed indication by ensuring that the flightcrew is advised of in-flight procedures in the event of loss of airspeed indication.
Applicability, as the AD words it
All Model Beech 400, 400A, and 400T series airplanes, Model Mitsubishi MU-300 airplanes, and Model Beech MU- 300-10 airplanes; certificated in any category.
- AD 2001-20-07 One-time
Raytheon Model Beech 400A Series Airplanes
To prevent electrical arcing or overheating of the ground connection in the aft fuselage area, which could result in a fire hazard due to ignition of fuel fumes during an engine start sequence.
Applicability, as the AD words it
Model 400A series airplanes, serial numbers RK- 78, RK-87 through RK-207 inclusive, certificated in any category.
- AD 2001-03-06 Recurring
Raytheon (Beech) Model MU-300, MU-300-10, 400, and 400A Series Airplanes
Applicability, as the AD words it
All Model MU-300, MU-300-10, 400, and 400A series airplanes, certificated in any category.
- AD 2000-25-04 One-time
Raytheon (Beech) Model MU-300, MU-300-10, 400, 400A, and 400T Series Airplanes
To prevent an asymmetric braking condition and a longer stopping distance due to sudden loss of normal braking to the left wheel, which could result in the airplane overrunning the runway surface.
Applicability, as the AD words it
Model MU-300, MU-300-10, 400, 400A, and 400T series airplanes; as listed in Raytheon Aircraft Service Bulletin SB 32-3300, dated December 1999; certificated in any category.
- AD 2000-09-12 One-time
Raytheon (Beech) Model 400A and 400T Series Airplanes
To prevent detachment or breakage of wires in the temperature switch assemblies of the wing ice protection system, which could result in the flightcrew not being advised of an over-temperature situation on the leading edge of the wing, and consequent structural damage to the wing.
Applicability, as the AD words it
Model 400A series airplanes, having serial numbers RK-01 through RK-188 inclusive; Model 400T (T-1A) series airplanes, having serial numbers TT-01 through TT-180 inclusive; and Model 400T (TX) series airplanes, having serial numbers TX-01 through TX-09 inclusive; certificated in any category.
- AD 2000-05-06 One-time
Raytheon (Beech) Model 400A and 400T Series Airplanes
To prevent failure of the engine fire extinguisher bottle to discharge, or discharge of the wrong engine fire extinguisher bottle.
Applicability, as the AD words it
Model 400A series airplanes, serial numbers RK-45 and RK-49 through RK-209 inclusive; Model 400T series airplanes (T- 1A), serial numbers TT-01 through TT-180 inclusive; and Model 400T series airplanes (TX), serial numbers TX-01 through TX-09 inclusive; certificated in any category.
- AD 99-21-26 One-time
Raytheon (Beech) Model 400, 400A, 400T, and MU-300-10 Airplanes
To prevent uncommanded nose-down pitch at certain flap settings during icing conditions.
Applicability, as the AD words it
All Model 400, 400T, and MU-300-10 airplanes; and Model 400A airplanes having serial numbers RK-1 through RK-107 inclusive; certificated in any category.
- AD 99-21-08 One-time
Raytheon (Beech) Model 400A Airplanes
To prevent chafing of the fuel drain tube assembly, which could result in fuel leakage from the fuel drain tube assembly and consequent risk of fire.
Applicability, as the AD words it
Model 400A airplanes, serial numbers RK-1 through RK-92 inclusive, certificated in any category.
- AD 98-06-30 One-time
Raytheon (Beech) Model 400, 400A, 400T, MU-300, and MU-300-10 Airplanes
To prevent cracking and consequent failure of the outflow/safety valves, which could result in rapid decompression of the airplane.
Applicability, as the AD words it
The following models and series of airplanes, certificated in any category, equipped with AlliedSignal outflow/ safety valves, as identified in AlliedSignal Aerospace Service Bulletin 103570-21-4012, Revision 1, dated May 30, 1995: Model of airplane Serial Nos. 400: RJ-1 through RJ-65 inclusive. 400A: RK-1 through RK-42 inclusive. 400T (military): TT-4 and TT-19. MU-300: S/N A001SA through A091SA inclusive. MU-300-10: A1001SA through A1011SA inclusive.
- AD 96-25-03 One-time
Raytheon (Beech) Model 400A, 400T (Military T-1A), and 400T (Military TX) Series Airplanes
To prevent loss of roller attach nuts and the flap roller, which could result in the loss of a flap when the airplane is subject to load limit conditions, and consequently lead to reduced controllability of the airplane.
Applicability, as the AD words it
Model 400A and 400T series airplanes; as listed in Beech Service Bulletin No. 2522, dated January 1994, and Raytheon Service Bulletin No. 2522, Revision 1, dated May 1996; certificated in any category.
- AD 95-25-06 One-time
Beech Model 400, 400A, and 400T (Military T-1A) Airplanes
To ensure that the standby instrument lighting system adequately illuminates the standby instrument, if normal electrical power is lost or is turned off as a result of a fire or smoke in the cockpit.
Applicability, as the AD words it
Model 400 airplanes, serial number RJ-61; 400A airplanes, serial numbers RK-1 through RK-80 inclusive; and 400T (military T-1A) airplanes, serial numbers TT-1 through TT-108 inclusive; certificated in any category.
- AD 95-25-05 One-time
Beech Model 400A Airplanes
To prevent reduced controllability of the airplane after takeoff.
Applicability, as the AD words it
Model 400A airplanes, serial numbers RK-1 through RK-96 inclusive, certificated in any category.
- AD 95-18-04 One-time
Beech Model 400 and 400A Airplanes
To prevent reduced controllability of the airplane.
Applicability, as the AD words it
Model 400 airplanes, serial RJ-61; and Model 400A airplanes, serials RK-1 through RK-77 inclusive, and RK-79 through RK-92 inclusive; certificated in any category.
- AD 94-01-06 One-time Appliance
Airworthiness Directives: Rockwell International, Collins Air Transport Division, Traffic Alert and Collision Avoidance System II Processors
To prevent collisions or near misses caused by incompatibility between the traffic alert and collision avoidance system (TCAS) II processors and the current air traffic control system.
Applicability, as the AD words it
Traffic Alert and Collision Avoidance System II processors that are installed on, but not limited to the following airplanes (all serial numbers), certificated in any category: General Aviation Airplanes Astra Model 1125 airplanes BAC Model 1-11 airplanes British Aerospace Model 125-800 airplanes Beech Models C90A, B200, 300, 350, and 400A airplanes Canadair Models CL-600, CL-600-2B16, CL-601, CL-601-1A, and CL-601- 3A airplanes Learjet Models 31, 55, and 60 airplanes Falcon Models 20, 50, 200, and 900 airplanes Gulfstream Models G2 and G3 airplanes British Aerospace Models HS-125-700 airplanes and Sabreliner Model 60 airplanes Air Transport Airplanes Aerospatiale Models ATR-42 and ATR-72 airplanes Airbus Industries Models A300B2, A-300B, and A-320 airplanes British Aerospace Models ATP and 146 airplanes Boeing Models 707, 727, 737, 747, 757, and 767 airplanes British Aerospace/Aerospatiale Model Concorde SST airplanes de Havilland DHC-7 and DHC-8 series airplanes McDonnell Douglas Models DC-8, DC-9, and DC-10, MD-80, and MD-11 airplanes Ilyushin Model IL-86 airplanes Lockheed Model L-1011 airplanes SAAB Models SF340A and SF340B airplanes and Shorts Models SD3-60-300 airplanes.
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.