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.
N817RA is a 2002 Cessna Citation X in the FAA registry (aircraft page). Matched on type certificate model 750.
RESULTS
17 ADs in effect may apply to N817RA
- In effect17
- Recurring2
- Superseded or removed6
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Also show 6 superseded or removed N817RA’s registration record
- AD 2013-04-03 One-time
Cessna Aircraft Company Airplanes
This AD was prompted by reports of loss of displayed airspeed.
Applicability, as the AD words it
This AD applies to The Cessna Aircraft Company Model 750 airplanes, certificated in any category, serial numbers 0001 through 0245 inclusive.
- AD 2012-18-16 One-time
The Cessna Aircraft Company Airplanes
This AD was prompted by reports of direct current (DC) generator overvoltage events.
Applicability, as the AD words it
This AD applies to The Cessna Aircraft Company Model 750 airplanes, certificated in any category, having serial numbers - 0222, -0225 through -0306 inclusive, and -0308.
- AD 2011-03-16 One-time
The Cessna Aircraft Company Model 750 Airplanes
Applicability, as the AD words it
This AD applies to The Cessna Aircraft Company Model 750 airplanes, certificated in any category, having serial numbers - 0222, and -0225 and subsequent.
- AD 2010-20-10 One-time
The Cessna Aircraft Company Model 750 Airplanes
Applicability, as the AD words it
This AD applies to The Cessna Aircraft Company Model 750 airplanes, certificated in any category, as identified in Cessna Service Bulletin SB750-27-62, Revision 3, dated August 21, 2009.
- AD 2007-24-05 One-time Engine
Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan Engines
We are issuing this AD to prevent an in-flight engine shutdown due to loss of engine oil from the starter shaft seal and possible loss of the airplane.
Applicability, as the AD words it
This AD applies to Rolls-Royce Corporation (RRC) (formerly Allison Engine Company, Inc.) AE 3007A and AE 3007C series turbofan engines. These engines are installed on, but not limited to, Cessna Aircraft Company 750 series, and Empresa Brasileira de Aeronautica S. A. (EMBRAER) EMB-135 and EMB-145 series airplanes.
- AD 2007-11-17 One-time
Cessna Model 500, 501, 550, 551, S550, 560, 560XL, and 750 Airplanes
Applicability, as the AD words it
This AD applies to Cessna Model 500, 501, 550, 551, S550, 560, 560XL, and 750 airplanes, certificated in any category; as identified in the service bulletins specified in Table 1 of this AD. Table 1.--Cessna Service Bulletins Cessna Service Bulletin Revision Date Cessna model SB500-26-02, including Service 1: July 7, 2005: 500/501 airplanes. Bulletin Supplemental Data, dated April 1, 2005. SB500-26-02: Original: April 1, 2005: 500/501 airplanes. SB550-26-05: Original: April 1, 2005: 550/551 airplanes. SB560-26-01: Original: April 1, 2005: 560 airplanes. SB560XL-26-02: 1: December 22, 2004: 560XL airplanes. SB750-26-05: Original: November 24, 2004: 750 airplanes. SBS550-26-02: Original: April 1, 2005: S550 airplanes.
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Cessna Model 750 Airplanes
Applicability, as the AD words it
This AD applies to Cessna Model 750 airplanes, certificated in any category, serial numbers -0001 through -0256 inclusive.
- AD 2002-23-05 One-time
Cessna Model 750 Airplanes
To prevent overloading of certain airplane electrical wiring and circuits, which could result in a fire.
Applicability, as the AD words it
Model 750 airplanes, serial numbers-0001 through- 0100 inclusive; certificated in any category.
- AD 2001-25-05 One-time Engine
Rolls-Royce Corporation (Formerly Allison Engine Company) AE 3007 Series Turbofan Engines
To prevent low-cycle fatigue (LCF) failure of cone shafts, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Rolls-Royce Corporation (formerly Allison Engine Company) models AE 3007A, AE 3007A1, AE 3007A1/1, AE 3007A1/2, AE 3007A1/3, AE 3007A1P, and AE 3007C turbofan engines, with compressor cone shafts, part numbers (P/N's) 23050728 and 23070729, installed. These engines are installed on but not limited to EMBRAER EMB-135 and EMB-145 series and Cessna 750 series airplanes.
- AD 2001-19-03 Engine
Rolls-Royce Corporation (Formerly Allison Engine Company) Model AE 3007A and AE 3007C Turbofan Engines
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Rolls-Royce Corporation (formerly Allison Engine Company) Model AE 3007A and AE 3007C turbofan engines with HPT 1st to 2nd stage turbine spacer P/N 23058369 installed. These engines are installed on, but not limited to Empresa Brasileira de Aeronautica S.A. (EMBRAER) EMB-145, and Cessna 750 series airplanes.
- AD 2001-17-31 One-time Engine
Rolls-Royce Corporation (Formerly Allison Engine Company) AE 2100 Turboprop and AE 3007 Turbofan Series Engines
To detect and prevent early development of cracks due to low cycle fatigue of the 2nd stage HPT wheel in the aft bore face that can lead to wheel failure, power loss, and possible damage to the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Rolls-Royce Corporation (formerly Allison Engine Company) models AE 2100A and AE 2100C turboprop engines with high pressure turbine (HPT) wheel part number (P/N) 23050912 installed; AE 2100A turboprop engine with turbine wheel P/N 23063462 serial number (SN) MM14062 installed; AE 2100A, AE 2100C, AE 2100D3 turboprop and AE 3007A, and AE 3007C turbofan engines with 2nd stage HPT wheels with SN's before MM183060. These engines are installed on but not limited to Embraer EMB-145, Cessna 750, SAAB 2000, and Industi Pesawat Terbang Nusantara (IPTN) N-250 series airplanes.
- AD 2001-07-04 One-time
Cessna Model 750 Airplanes
To prevent jamming of the roll control system (ailerons and spoilers), which could result in reduced controllability of the airplane.
Applicability, as the AD words it
Model 750 airplanes, having manufacturer's serial numbers -0001 through -0102 inclusive, certificated in any category.
- AD 2000-18-06 One-time Engine
Allison Engine Company AE 3007A and 3007C Series Turbofan Engines
To prevent an uncommanded in-flight engine shutdown and the potential for an in-flight dual-engine shutdown.
Applicability, as the AD words it
This AD is applicable to Allison Engine Company Models AE 3007A, AE 3007A1/1, AE 3007A1/2, AE 3007A1, AE 3007A1/3, AE 3007A1P, AE 3007A3, and AE 3007C turbofan engines with full authority digital electronic controls (FADEC's) that have the following hardware serial numbers (SN's) installed: Engine model FADEC hardware SN AE 3007C: BX55758, BX55760, BX55761, BX55763 through BX55765, BX55767, and BX61001 through BX61069, unless the FADEC has been repaired and marked as provided in paragraphs (f) and (g) of this AD. AE 3007A, AE 3007A1/1, AE 3007A1/2, BX56348, BX56361 through AE3007A1/3, AE 3007A1, AE 3007A1P, AE BX56364, BX56374, BX56376, 3007A3. BX56392 through BX56395, BX59006, BX59007, BX59013, BX59014, BX59041, BX59050, BX59062, BX59064 through BX59066, BX59075 through BX59078, BX60000 through BX60145, BX60172 through BX60239, BX60265 through BX60287, BX60301, BX60303, BX60311, BX60381 through BX60384, unless the FADEC has been repaired and marked as provided in paragraphs (f) and (g) of this AD. These engines are installed on, but not limited to Embraer Model EMB-145, EMB-145ER, EMB-145MR, EMB-145LR, EMB-135ER, EMB-135LR, and Cessna 750 airplanes.
- AD 2000-13-01 One-time Engine
Allison Engine Company, Inc. AE 3007A and AE 3007C Series Turbofan Engines
To prevent an uncontained turbine wheel failure, which could result in damage to the airplane.
Applicability, as the AD words it
Allison Engine Company, Inc. AE 3007A and AE 3007C series turbofan engines, installed on, but not limited to, Cessna Aircraft Company 750 series airplanes and Empresa Brasileira de Aeronautica S.A. (Embraer) EMB-145 series airplanes.
- AD 2000-11-22 One-time Engine
Allison Engine Company AE 3007A and AE 3007C Series Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
Allison Engine Company AE 3007A, AE 3007A1/1, AE 3007A1/2, AE 3007A1/3, AE 3007A1, AE 3007A3, AE 3007A1P and AE 3007C series turbofan engines, installed on but not limited to EMBRAER EMB-135 and EMB-145 series and Cessna 750 series airplanes.
- AD 98-11-32 Recurring Engine
Allison Engine Company AE 3007A and AE 3007C Series Turbofan Engines
To prevent No. 4 bearing failure due to excessive bearing wear, which can result in an inflight engine shutdown.
Applicability, as the AD words it
Allison Engine Company AE 3007A and AE 3007C series turbofan engines with No. 4 bearing, Part Number (P/N) 23062504, installed on but not limited to EMBRAER EMB-145 and Cessna 750 series aircraft.
- AD 98-05-02 Recurring
Cessna Model 750 Airplanes
To prevent the possibility of the accumulation of ice on the aileron feel cartridge assembly shaft, which could result in jamming of the aileron control circuit, and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model 750 airplanes, serial numbers 0001 through 0053 inclusive; 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.