Cessna CitationJet airworthiness directives FAA ADs that may apply, with the official text
- In effect
- 17
- Recurring
- 2
- Superseded or removed2
- Latest2024-15-09
Cessna CitationJet: price, specs and every tail number · Look up ADs by N-number · AD burden by model, ranked
IN EFFECT
17 CitationJet ADs in effect, newest first
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.
- 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 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 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 2013-08-05 One-time
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.
Applicability, as the AD words it
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 One-time
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.
Applicability, as the AD words it
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 on various small and transport category airplanes, certificated in any category, including, but not limited, to the airplane models listed in Table 1 of this AD. Table 1.--Manufacturers/Airplane Models Manufacturer Airplane model(s) Airbus: A300. Avions Marcel Dassault-Breguet Aviation (AMD/BA).. Falcon 10. Boeing: 727, 737, 747. Bombardier (LearJet): 24, 35, 36, 55. British Aerospace (Operations) Limited: Jetstream Series 3101. Cessna: 208, 208B, 421C; 501, 525, 550, 560, 650, S550. Embraer: EMB-120. Dassault-Aviation: Mystere-Falcon 50, Mystere-Falcon 200. Gulfstream: G-I, G-1159A (G-III) Israel Aircraft Industries (IAI): 1124, 1125 Westwind Astra. McDonnell Douglas: DC-10. Piper: PA-31T2. Raytheon: 58; 1900D, 400; A36; BAe.125 Series 800A; HS.125 Series 600A/700A; Hawker 800-XP; 200, 300, 350; A200, B100, B200, B300, C90, C90A, C90B, E90, F90; MU-300-10. Sabreliner: 60 (NA-265-60). Twin Commander: 500-A, 695A. Viking Air Limited: DHC-6.
- AD 2008-12-01 One-time
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.
Applicability, as the AD words it
This AD applies to Model 525 airplanes, serial numbers 525- 0600 through 525-0662, that are certificated in any category.
- 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 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 2004-14-20 One-time
The Cessna Aircraft Company Model 525 Airplanes
Applicability, as the AD words it
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 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 2002-20-09 One-time Appliance
Rockwell Collins, Inc. AFD-3010 Adaptive Flight Display Units
Applicability, as the AD words it
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 display units are installed in, but not limited to, the following aircraft that are certificated in any category: (1) Bombardier Model CL-600-2A12 (CL-601) airplanes; (2) Cessna Model 525 and 525A airplanes; (3) Dassault Model Mystere-Falcon 20-F5 and Mystere-Falcon 50 airplanes; and (4) Raytheon Model 390 and Hawker 800XP airplanes. (b) Who must comply with this AD? Anyone who wishes to operate an aircraft equipped with one of the affected AFD-3010 adaptive flight display units must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to prevent premature failure of the Application Specific Integrated Circuit (ASIC) device, which could result in the AFD-3010 unit displaying erroneous primary flight and engine parameter information. Such failure could lead to the pilot using incorrect information when making critical flight safety decisions. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Actions Compliance Procedures (1) Inspect the AFD-3010 Within the next 14 In accordance with adaptive flight display days after November Rockwell Collins unit to determine the 12, 2002 (the Service Bulletin serial number. effective date of 12, Revision No. 2 this AD), unless (AFD-3010-31-12), already dated August 30, accomplished. 2002. (2) If the serial number of Prior to further In accordance with the AFD-3010 unit is listed flight after the Rockwell Collins as one of the affected inspection required Service Bulletin units specified in Rockwell in paragraph (d)(1) 12, Revision No. 2 Collins Service Bulletin of this AD, unless (AFD-3010-31-12), 12, Revision No. 2 (AFD- already dated August 30, 3010-31-12), dated August accomplished. 2002. 30, 2002, then inspect the MFP386 ASIC device to determine the date code. (i) If the date code on the MFP386 ASIC device is 0128, return the unit to the manufacturer for modification and install the modified ADF-3010 unit. (ii) If the date code on the MFP386 ASIC is other than 0128, no manufacturer modification is necessary. (3) Do not install, on any As of November 12, Not applicable. aircraft, an affected ADF- 2002 (the effective 3010 adaptive flight date of this AD). display that contains a MFP386 ASIC device with a date code of 0128. (e) Can I comply with this AD in any other way? You may use an alternative method of compliance or adjust the compliance time if: (1) Your alternative method of compliance provides an equivalent level of safety; and (2) The Manager, Wichita Aircraft Certification Office, approves your alternative. Submit your request through an FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Wichita Aircraft Certification Office. Note: This AD applies to each airplane identified in paragraph (a) of this AD, regardless of whether it has been modified, altered, or repaired in the area subject to the requirement
- AD 2001-23-17 One-time Appliance
GARMIN International GNS 430 Units
Applicability, as the AD words it
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 numbers 9630001, 96300002, 96300017, 96300028, 96300034, 96300040, 96300068, 96300104, 96300108, 96300122, 96300125, 96300130, 96300142, 96300149, 96300161, 96300165, 96300218, 96300222, 96300232, 96300269, 96300272, 96300308, 96300333, 96300340, 96300348, 96300354, 96300369, 96300372, 96300382, 96300394, 96300411, 96300413, 96300429, 96300437, 96300451, 96300484, 96300485, 96300489, 96300504, 96300506, 96300513, 96300522, 96300549, 96300563, 96300585, 96300587, 96300618, 96300621, 96300624, 96300628, 96300641, 96300653, 96300664, 96300713, 96300734, 96300756, 96300766, 96300781, 96300785, 96300786, 96300808, 96300831, 96300837, 96300842, 96300846, 96300866, 96300870, 96300872, 96300899, 96300916, 96300923, 96300925, 96300929, 96300941, 96300961, 96300984, 96300987, 96301021, 96301108, 96301130, 96301280, and 96301296 through 96303200. (2) Aircraft with the GNS 430 Unit Installation (other aircraft could have field approval installations): TC holder Airplane models Cessna Aircraft Company: 172, 182, 206, 208, 210, 401, 402, 404, 406, 411, 414, 414A, 421A, 421B, 421C, 425, 441, 500, 550, S550, 552, 560, 560XL, 501, 525, and 551. Mooney Aircraft: M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S, and M22. Raytheon Aircraft Company: Beech Models E33, F33, G33, E33A, F33A, E33C, F33C, 35, 35R, A35, B35, B35TC, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35TC, V35A, V35A-TC, V35B, V35B-TC, 36, A36, A36TC, 50, B50, C50, D50, D50A, D50B, D50C, D50E, E50, F50, G50, H50, J50, 60, A60, B60, 65-90, 65-A90, B90, C90, C90A, C90B, E90, F90, 100, A100, B100, 95-55, 95-A55, 95-B55, 95-C55, D-55, E55, 58, 58P, and 58TC. Socata: TBM 700. The New Piper Aircraft, Inc.. J3C-40, J3C-50, J3C-50S (Army L-4, L-4B, L-4H, and L-4J), J3C-65 (Navy NE-1 and NE-2), J3C-65S, J3F-50, J3F-50S, J3F-60, J3F-60S, J3F-65 (Army L-4D), J3F-65S, J3L, J3L-S, J3L-65 (Army L-4C), J3L-65S, J4, J4A, J4A-S, J4E (Army L-4E), J5A (Army L-4F), J5A-80, J5B (Army L-4G), J5C, AE-1, HE-1, PA-11, PA-11S, PA-12, PA-12S, PA-14, PA-15, PA-16, PA-16S, PA- 17, PA-18, PA-18A, PA-18A (Restricted), PA-18S, PA-18-"105" (Special), PA-18S- "105" (Special), PA-18-"125" (Army L- 21A), PA-18AS-"125", PA-18S-"125",
- AD 2001-02-13 One-time
The Cessna Aircraft Company Model 525 (CitationJet 1) Airplanes
Applicability, as the AD words it
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 airplanes must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to prevent this battery switch from failing while the airplane is in-flight, which is a latent failure. This could result in the pilot's inability to select "EMER" power or the inability to disconnect an overheated main ship's battery. On a battery overheat indication, the Airplane Flight Manual (AFM) instructs the pilot to disconnect the battery and, if the problem cannot be fixed, the pilot should immediately land the airplane. The main ship's battery that remains powered in an overheated condition may become hot enough to damage adjacent components and structure and may interfere with continued flight and a safe landing. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Action Compliance time Procedures (1) Inspect the airplane to During the next Not Applicable. determine whether a DC power phase check that battery switch, Eaton part occurs 30 number A3-205-01/P with a calendar days or manufacturer's date code of more after 9926 through 0039, is installed. February 28, 2001 (the effective date of this AD) or within the next 60 calendar days after February 28, 2001 (the effective date of this AD), whichever occurs first. (2) If, by inspecting the Prior to further Not Applicable. airplane, you can positively flight after the show that one of the affected inspection. DC power battery switches is not installed, then the replacement requirement of this AD does not apply. Make an entry into the aircraft records that shows compliance with this portion of the AD, in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (3) If, by inspecting the Prior to further In accordance with airplane, you find that one of flight after the the the affected DC power battery inspection, Accomplishment switches is installed or you unless already Instructions cannot positively show that one accomplished. section of Cessna of the affected DC power Service Bulletin battery switches is not SB525-24-20, installed, replace with a new dated November switch of the same part number 16, 2000. that has a manufacturer's date code of 0040 or later, or FAA- approved equivalent part number. (4) Do not install, on any As of February 28, Not Applicable. affected airplane, a DC power 2001 (the battery switch, Eaton part- effective date of number A3-205-01/P with a this AD). manufacturer's date code of 9926 through 0039.
- 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.
- AD 97-05-03 One-time Appliance
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.
Applicability, as the AD words it
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 Corporation: 525, 550, and 560 Dausault Aviation: Mystere-Falcon 20 and 50 Avions Marcel Dassault: Falcon 10 Gulfstream Aerospace: G-1159 (G-II) and G-1159A (G- III) Raytheon Corporate Jets: Hawker 800 Israel Aircraft Industries, Ltd: 1124 Sabreliner Corporation: NA-65 Learjet Inc: 35 Jetstream Aircraft Ltd: 4101
- AD 97-01-05 Recurring Engine
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.
Applicability, as the AD words it
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 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.
Applicability, as the AD words it
Model 525 airplanes (serial numbers 525-0001 through 525-0153), certificated in any category.
2 superseded or removed ADs
- 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 2003-21-07 Superseded by AD 2004-14-20
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.
Applicability, as the AD words it
This AD affects Model 525 airplanes, serial numbers 525- 0001, 525-0002, and 525-0004 through 525-0159, that are certificated in any category.
Radar reads the aircraft’s 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
CitationJet AD questions
Source: FAA final rules under 14 CFR part 39, from the Federal Register. The FAA’s Dynamic Regulatory System holds the official list.
How many airworthiness directives apply to the CitationJet?
19 FAA ADs published since 1995 name the Cessna CitationJet's type certificate model (525) in their applicability. 17 are still in effect as far as the Federal Register shows; the others were superseded by a later AD or removed. How many apply to one aircraft depends on its serial number, equipment and modifications.
Which CitationJet ADs are recurring?
2 of the ADs in effect require actions that repeat, such as inspections at set intervals, until a terminating action is done. They are marked Recurring above. One-time ADs are complied with once, but the compliance record stays with the aircraft.
What is the latest CitationJet airworthiness directive?
AD 2024-15-09, effective Oct 22, 2024: Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes. The list is refreshed from the Federal Register every weekday.
How do I know whether an AD applies to my CitationJet?
Read the AD's applicability paragraph, shown with each AD on this page, against the aircraft's serial number and its installed engines, propellers, parts and modifications. A certificated mechanic or inspector makes the determination and records the method of compliance in the maintenance records. The FAA's Dynamic Regulatory System holds the official list of ADs.
Why are engine and propeller ADs missing?
This page lists ADs whose applicability names the Cessna CitationJet airframe, plus appliance ADs that list it among the aircraft they can be installed on. Engine and propeller ADs name the engine or propeller model rather than the aircraft, so check them by the installed engine and propeller models.
Every AD on your CitationJet, tied to the logbook entry that closed it.
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.