Beechcraft 390 (certified family) airworthiness directives FAA ADs that may apply, with the official text
- In effect
- 21
- Recurring
- 4
- Superseded or removed2
- Latest2017-18-11
Beechcraft 390 (certified family): price, specs and every tail number · Look up ADs by N-number · AD burden by model, ranked
IN EFFECT
21 Beechcraft 390 (certified family) 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 2017-18-11 One-time
Textron Aviation Inc. Airplanes
This AD was prompted by reports of hydraulic fluid loss from the engine driven pumps (EDPs) on three different airplanes.
Applicability, as the AD words it
This AD applies to Textron Aviation Inc. (type certificate previously held by Beechcraft Corporation) Model 390 airplanes; serial numbers RB-4 through RB-295; certificated in any category.
- AD 2010-17-15 One-time
Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes
We are issuing this AD to detect and replace starter generators with deficient armature insulating materials.
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-4 through RB-257, RB-259 through RB-265, RB-268, and RB-269, that are certificated in any category.
- AD 2010-10-10 One-time
Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes
We are issuing this AD to detect and correct improper installation of the MOV and spark gap wiring, which could result in overload of the MOV in a lightning strike and allow electrical energy to continue to the essential bus and disable equipment that receives power from the essential bus.
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-4 through RB-248, that are certificated in any category.
- AD 2008-23-13 One-time
Hawker Beechcraft Corporation Model 390 Airplanes
We are issuing this AD to prevent hydraulic fluid leaking from the left and right hydraulic fluid pump and to prevent the flow of hydraulic fluid into the engine compartment.
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-4 through RB-224, that are certificated in any category.
- AD 2008-22-11 Recurring
Hawker Beechcraft Corporation Model 390 Airplanes
We are issuing this AD to prevent leakage of hydraulic fluid from the pump output hose within the engine compartment, which could cause an in-flight fire.
Applicability, as the AD words it
This AD applies to the following Model 390 airplanes that are certificated in any category: (1) Serial numbers RB-1 and RB-4 through RB-209 equipped with hose kit 390-5805-0001 installed during compliance with Hawker Beechcraft Mandatory Service Bulletin 29-3800, dated May 2007); and (2) Serial numbers RB-210 though RB-239.
- AD 2008-21-04 One-time
Hawker Beechcraft Corporation Model 390 Airplanes
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-1 and RB-4 through RB-238, that are certificated in any category.
- AD 2008-16-02 Recurring
Hawker Beechcraft Corporation Model 390 Airplanes
We are issuing this AD to correct potentially inadequate stall warning with loss of stick pusher function.
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-4 through RB-204, that are certificated in any category.
- AD 2007-20-07 One-time
Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes
We are issuing this AD to detect improperly shimmed starter-generators, which could result in premature starter-generator failure.
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-1 and RB-4 through RB-149, that are certificated in any category.
- AD 2007-12-21 Recurring
Hawker Beechcraft Corporation (Type Certificate No. A00010WI Previously Held by Raytheon Aircraft Company) Model 390 Airplanes
We are issuing this AD to prevent failure of the hydraulic pump outlet tube and consequent leaking of hydraulic fluid.
Applicability, as the AD words it
This AD affects the following Model 390 airplanes that are certificated in any category: (1) Serial numbers RB-1 through RB-49 that have Field Service Kit 390-9100 installed; and (2) Serial numbers RB-50 through RB-209.
- AD 2006-18-16 Recurring
Raytheon Aircraft Company Model 390 Airplanes
Applicability, as the AD words it
This AD affects Model 390 airplanes, serial numbers RB-1 and RB-4 through RB-139, that are certificated in any category.
- AD 2005-25-07 One-time
Raytheon Aircraft Company, Model 390, Premier 1 Airplanes
Applicability, as the AD words it
This AD applies to the following airplane models and serial numbers that are certificated in any category: (1) Group 1: Raytheon Aircraft Company, Model 390, Premier 1 Airplanes, serial numbers RB-1, RB-4 through RB-101, RB-103 through RB-119, and RB-121, that have not replaced the plastic cover over the compressor motor module with a metallic one (part number (P/N) 390-555015-0001 or FAA-approved equivalent part number). (2) Group 2: Raytheon Aircraft Company, Model 390, Premier 1 Airplanes, serial numbers RB-1, RB-4 through RB-101, RB-103 through RB-119, and RB-121, that have installed the metallic cover (P/N 390- 555015-0001 or FAA-approved equivalent part number). (3) Group 3: Raytheon Aircraft Company, Model 390, Premier 1 Airplanes, serial numbers RB-120 and RB-122 through RB-129.
- AD 2005-19-07 One-time
Raytheon Aircraft Company Model 390 Airplanes
Applicability, as the AD words it
This AD affects the following serial-numbered Model 390 airplanes that are certificated in any category: Serial Numbers (1) RB-1 (2) RB-4 through RB-36 (3) RB-38 through RB-41 (4) RB-43 through RB-67 (5) RB-69 through RB-80 (6) RB-82 through RB-84 (7) RB-87 through RB-94 (8) RB-96 through RB-101 (9) RB-103 through RB-115 (10) RB-117 through RB-119 (11) RB-121
- AD 2005-18-22 One-time
Raytheon Aircraft Company Model 390 Premier 1 Airplanes
Applicability, as the AD words it
This AD affects Model 390 airplanes that: (1) Incorporate a serial number of RB-1, RB-4 through RB-84, RB- 87 through RB-90, RB-92 through RB-96, RB-98 through RB-101, and RB- 103 through RB-107; and (2) Are certificated in any category.
- AD 2004-25-15 One-time
Raytheon Aircraft Company, Model 390, Premier 1 Airplanes
Applicability, as the AD words it
This AD affects the following airplane model and serial numbers that are certificated in any category: Model 390 Premier I, Serials RB-1, RB-4 through RB-84, RB-87 through RB-90, RB-92 through RB-96, RB-99 through RB-101, and RB-103 through RB-106.
- AD 2004-15-01 One-time
Raytheon Aircraft Company Model 390 Airplanes
Applicability, as the AD words it
This AD affects Model 390 airplanes, serial numbers RB-1, RB-4 through RB-84, RB-87, RB-89, RB-90, RB-93 through RB-96, RB-99 through RB-101, and RB-103; that are certificated in any category:
- AD 2003-10-05 One-time
Raytheon Aircraft Company Model 390 Airplanes
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-18 through RB-24, that are certificated in any category. (b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to require the use of necessary flight information to prevent runway overruns based on insufficient wheel braking if the lift dump spoilers do not operate after landing touchdown. This could result in reduced or loss of control of the airplane. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Actions Compliance (1) Incorporate information into the Within the next 5 hours time-in- FAA-approved Airplane Flight Manual service (TIS) after May 30, (AFM) that would add requirements for 2003 (the effective date of "Landing Performance for Operation of this AD). the Airplane with Lift Dump Inoperative." Accomplish this action by inserting Raytheon Temporary Change to the FAA Approved Airplane Flight Manual P/N 390-590001-0003BTC5A1, revised March 24, 2003. (2) The owner/operator holding at least Within the next 5 hours TIS a private pilot certificate as after May 30, 2003 (the authorized by section 43.7 of the effective date of this AD). Federal Aviation Regulations (14 CFR 43.7) may incorporate into the AFM the information specified in paragraph (d)(1) of this AD. Make an entry into the aircraft records showing compliance with this portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (e) Are special flight permits authorized for this AD? Special flight permits are not authorized for this AD. On July 10, 2002, FAA published a new version of 14 CFR part 39 (67 FR 47997, July 22, 2002), which governs FAA's AD system. Part of this amendment to 14 CFR part 39 authorized special flight permits for all ADs, unless specified otherwise. Because the owner/operator holding an appropriate pilot's license may accomplish the action of this AD and the compliance time is 5 hours TIS after the AD effective date, FAA has determined that special flight permits are not necessary for this AD. (f) Can I comply with this AD in any other way? To use an alternative method of compliance or adjust the compliance time, follow the procedures in 14 CFR 39.19. Send these requests to the Manager, Wichita Aircraft Certification Office (ACO). For information on any already approved alternative methods of compliance, contact Derek Morgan, Flight Test Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4172; facsimile: (316) 946-4107. (g) Are any service bulletins incorporated into this AD by reference? Actions required by this AD must be done in accordance with Raytheon Temporary Change to the FAA Approved Airplane Flight Manual P/N 390-590001-0003BTC5A1, revised March 24, 2003. The Director of the Federal Register previously approved this incorporation by reference under 5 U.S.C. 552(a) and 1 CFR part 51 as of April 7, 2003 (68 FR 16205, April 3, 2003). You can get copies from Raytheon Aircraft Company, 9709 E. Central, Wichita, Kansas 67201-0085; telephone: (800) 429-5372 or (316) 676-3140. You may view this information at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (h) When
- AD 2003-09-10 One-time
Raytheon Aircraft Company Model 390 Airplanes
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-1 through RB-64, that are certificated in any category. (b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to prevent moisture from entering the aft power distribution box through the aft ram air duct, which could result in electrical power failure. Such failure could lead to loss of all attitude display information during flight. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Actions Compliance Procedures (1) Remove the aft power Within the next 10 In accordance with distribution box and: hours time-in- Raytheon Aircraft (i) Inspect the left-hand service (TIS) after Mandatory Service and right-hand generator May 13, 2003 (the Bulletin SB 24- relays and the battery tie effective date of 3606, Issued: relay to determine if they this AD), unless April, 2003. are part number SM400D79 already (or FAA-approved equivalent accomplished. part number);. (ii) Replace part number SM400D79 with part number SM400D79-1 relays (or FAA- approved equivalent part number);. (iii) Inspect the essential bus relay to determine if it is part number SM150D22 (or FAA-approved equivalent part number); and (iv) Replace part number SM150D22 relay with part number SM150D22-1 relay (or FAA-approved equivalent part number) (unless already accomplished in accordance with Raytheon Aircraft Mandatory Service Bulletin SB 24-3544, Issued: November, 2002) (2) Remove and modify the Within the next 10 In accordance with aft ram air duct. If the hours TIS after May Raytheon Aircraft procedures in Raytheon 13, 2003 (the Mandatory Service Aircraft Mandatory Service effective date of Bulletin SB 24- Bulletin SB 24-3544, this AD), unless 3606, Issued: Issued: November, 2002, already April, 2003, and have already been accomplished. Raytheon Aircraft accomplished, only the Mandatory Service procedures specified in Bulletin SB 24- Raytheon Aircraft Mandatory 3544, Issued: Service Bulletin SB 24- November, 2002. 3606, Issued: April, 2003, Issued: April, 2003, need be accomplished. (3) Only install part number As of May 13, 2003 Not applicable. SM400D79-1 (left-hand and (the effective date right-hand generator relays of this AD). and battery tie relay) (or FAA-approved equivalent part number); and part number SM150D22-1 (essential bus relay) (or FAA-approved equivalent part number). (e) Can I comply with this AD in any other way? To use an alternative method of compliance or adjust the compliance time, follow the procedures in 14 CFR 39.19. Send these requests to the Manager, Wichita Aircraft Certification Office (ACO). For information on any already approved alternative methods of compliance, contact Bryan Easterwood, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4132; facsimile: (316) 946-4107. (f) Are any service bulletins incorporated into this AD by reference? Actions required by this AD must be done in accordance with Raytheon Aircraft Mandatory Service Bulletin SB 24-3606, Issued: April, 2003, and Raytheon Aircraft Mandatory Service Bulletin SB 24-3544, Issued; November,
- AD 2003-07-09 One-time
Raytheon Aircraft Company Model 390 Airplanes
Applicability, as the AD words it
This AD applies to Model 390 airplanes with the following serial numbers and are certificated in any category: (1) RB-4 through RB-17. (2) RB-25 through RB-59. (3) RB-64. (b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to require the use of necessary flight information to prevent runway overruns based on insufficient aerodynamic and wheel braking if the lift dump spoilers do not operate after landing touchdown. This could result in reduced or loss of control of the airplane. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Actions Compliance (1) Incorporate information into the FAA- Within the next 5 hours approved Airplane Flight Manual (AFM) that time-in-service (TIS) would add requirements for "Landing after April 7, 2003 (the Performance for Operation of the Airplane effective date of this with Lift Dump Inoperative." Accomplish AD). this action by inserting Raytheon Temporary Change to the FAA Approved Airplane Flight Manual P/N 390-590001-0003BTC5A1, revised March 24, 2003. (2) The owner/operator holding at least a Within the next 5 hours private pilot certificate as authorized by TIS after April 7, 2003 section 43.7 of the Federal Aviation (the effective date of Regulations (14 CFR 43.7) may incorporate this AD). into the AFM the information specified in paragraphs (d)(1) of this AD. Make an entry into the aircraft records showing compliance with this portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (e) Are special flight permits authorized for this AD? Special flight permits are not authorized for this AD. On July 10, 2002, FAA published a new version of 14 CFR part 39 (67 FR 47997, July 22, 2002), which governs FAA's AD system. Part of this amendment to 14 CFR part 39 authorized special flight permits for all ADs, unless specified otherwise. Because the owner/operator holding an appropriate pilot's license may accomplish the action of this AD and the compliance time is 5 hours TIS after the AD effective date, FAA has determined that special flight permits are not necessary for this AD. (f) Can I comply with this AD in any other way? To use an alternative method of compliance or adjust the compliance time, follow the procedures in 14 CFR 39.19. Send these requests to the Manager, Wichita Aircraft Certification Office (ACO). For information on any already approved alternative methods of compliance, contact Derek Morgan, Flight Test Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4172; facsimile: (316) 946-4407. (g) Are any service bulletins incorporated into this AD by reference? Actions required by this AD must be done in accordance with Raytheon Temporary Change to the FAA Approved Airplane Flight Manual P/N 390-590001-0003BTC5A1, revised March 24, 2003. The Director of the Federal Register approved this incorporation by reference under 5 U.S.C. 552(a) and 1 CFR part 51. You can get copies from Raytheon Aircraft Company, 9709 E. Central, Wichita, Kansas 67201-0085; telephone: (800) 429-5372 or (316) 676-3140. You may view this information at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capit
- 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 2002-19-04 One-time
Raytheon Aircraft Company Model 390 Airplanes
Applicability, as the AD words it
This AD applies to Model 390 airplanes, serial numbers RB-4 through RB-15, RB-19 through RB-32, and RB-34 through RB-40, that are certificated in any category. (b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to correct the air gap clearance between the fuel probe and the adjacent wing fuel tank access panel, which could result in arcing between the two conductive materials in the event of a lightning strike. This could serve as an ignition source inside the fuel tank and result in fire or explosion. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Actions Compliance Procedures (1) Replace the existing Within the next 50 In accordance with upper and lower fuel probe hours time-in- Raytheon Aircraft brackets with new upper and service after Mandatory Service lower fuel probe brackets, October 4, 2002 Bulletin SB 28- part numbers 390-920304-001/ (the effective date 3537, Rev. 1, 002 (upper) and 390-920305- of this AD). Revised: August, 001/002 (lower), or FAA- 2002. approved equivalent part numbers. (2) Do not install upper and As of October 4, Not applicable. lower fuel probe brackets 2002 (the effective that are not part numbers date of this AD). 390-920304-001/002 (upper) and 390-920305-001/002 (lower), or FAA-approved equivalent part numbers.
- AD 2002-11-02 One-time
Raytheon Aircraft Company Model 390 Airplanes
Applicability, as the AD words it
This AD applies to the following airplanes that are certificated in any category: Model Serial Nos. 390: RB-4 through RB-14, RB-20 through RB- 22, RB-24 through RB-32, and RB-34. (b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD. (c) What problem does this AD address? The actions specified by this AD are intended to prevent ice formation on the wing leading edges and the upper and lower wing surfaces during flight in icing conditions. Ice formation on the wings could cause symmetric or asymmetric loss of lift, degradation of handling qualities, and increased drag of the airplane. (d) What must I do to address this problem? To address this problem, you must accomplish the following actions: Actions Compliance Procedures Insert page 2 (Limitations Within the next 15 Incorporating the Section) and page 3 calendar days after AFM revisions, as (Abnormal Procedures June 14, 2002 (the required by this Section) of Raytheon effective date of AD, may be Temporary Change, Part this AD). performed by anyone Number (P/N) 390-590001- who holds at least 0003BTC1, dated April 29, a private pilot 2002, into the FAA-approved certificate, as Airplane Flight Manual authorized by (AFM). section 43.7 of the Federal Aviation Regulations (14 CFR 43.7. You must make an entry into the aircraft records that shows compliance with this AD, in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). (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 (ACO), approves your alternative. Submit your request through an FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Wichita ACO. 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 requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/ operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD. The request should include an assessment of the e
2 superseded or removed ADs
- AD 2006-26-08 Superseded by AD 2007-12-21
Raytheon Aircraft Company Model 390 Airplanes
We are issuing this AD to prevent failure of the hydraulic pump outlet tubes and consequent leaking of hydraulic fluid.
Applicability, as the AD words it
This AD applies to Model 390 airplanes, all serial numbers, that are certificated in any category:
- AD 2006-02-51 Superseded by AD 2006-26-08
Raytheon Aircraft Company Model 390 Airplanes
We are issuing this AD to prevent failure of the hydraulic tube assembly and the clamp and consequent leaking of hydraulic fluid.
Applicability, as the AD words it
This AD affects the following Model 390 airplanes that are certificated in any category: (1) Serial numbers RB-1 through RB-49 that are equipped with Kit 390-9100 that incorporates part number (P/N) 390-580035-0001 (or FAA-approved equivalent part number); (2) Serial numbers RB-50 through RB-141; and (3) Serial numbers RB-143 through RB-148.
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
Beechcraft 390 (certified family) 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 Beechcraft 390 (certified family)?
23 FAA ADs published since 1995 name the Beechcraft 390 (certified family)'s type certificate model (390) in their applicability. 21 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 Beechcraft 390 (certified family) ADs are recurring?
4 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 Beechcraft 390 (certified family) airworthiness directive?
AD 2017-18-11, effective Oct 16, 2017: Textron Aviation Inc. Airplanes. The list is refreshed from the Federal Register every weekday.
How do I know whether an AD applies to my Beechcraft 390 (certified family)?
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 Beechcraft 390 (certified family) 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 Beechcraft 390 (certified family), 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.