# N549AS: 2005 Boeing 737-8FH

- Status: Valid registration
- Airframe: [Boeing 737-8FH](https://openairdocs.org/model/boeing-737-8fh) (registry code 13844NA, 149 seats)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 30824
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 10, 2005
- Certificate issued: August 11, 2021
- Expires: August 31, 2028
- Mode S code: A6F96C
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=549AS
- Page: https://openairdocs.org/aircraft/N549AS

From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56 model are included.

## ADs that may apply (OpenAirDocs): 55 in force

### Matched by airframe (Boeing 737-8FH)

None in force.

### Matched by engine (CFM International CFM56 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2017-14-08](https://openairdocs.org/ad/2017-14-08): Turbine Engine Compressor Section · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Aug 18, 2017
- [AD 2017-05-09](https://openairdocs.org/ad/2017-05-09): Accessory Gearboxes · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Apr 13, 2017
- [AD 2016-14-10](https://openairdocs.org/ad/2016-14-10): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Aug 9, 2016
- [AD 2016-02-04](https://openairdocs.org/ad/2016-02-04): Turbine rear frames (TRFs) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Mar 1, 2016
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2013-14-06](https://openairdocs.org/ad/2013-14-06): Hydro-mechanical unit (HMU) fuel control · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Sep 3, 2013
- [AD 2012-02-03](https://openairdocs.org/ad/2012-02-03): Engine · CFM International CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3 and 8 more. Effective Mar 15, 2012
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-12-03](https://openairdocs.org/ad/2010-12-03): Fan blades · CFM International CFM56-3 and CFM56-3B. Effective Jul 13, 2010
- [AD 2010-09-14](https://openairdocs.org/ad/2010-09-14): Exhaust gas temperature (EGT) · CFM International CFM56-5B1/2P, CFM56-5B1/P, CFM56-5B2/2P and 16 more. Effective Jun 8, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-18-01](https://openairdocs.org/ad/2009-18-01): LP turbine rear frames · CFM International CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2/3 and 19 more. Effective Oct 1, 2009
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2007-24-04](https://openairdocs.org/ad/2007-24-04): Low pressure turbine (LPT) · CFM International CFM56-5C4/1. Effective Dec 6, 2007
- [AD 2007-03-15](https://openairdocs.org/ad/2007-03-15): Exhaust gas temperature (EGT) harness · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Mar 19, 2007
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2005-10-05](https://openairdocs.org/ad/2005-10-05): Air turbine starters · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 50 more. Effective Jun 14, 2005
- [AD 97-09-02 R3](https://openairdocs.org/ad/97-09-02-R3): High pressure turbine rotor (HPTR) front shafts · CFM International CFM56-5C2, CFM56-5C3/G and CFM56-5C4. Effective Oct 14, 2004
- [AD 2004-10-13](https://openairdocs.org/ad/2004-10-13): Service main fuel pumps · CFM International CFM56-3, CFM56-5, CFM56-5-A1/F and 4 more. Effective Jun 24, 2004
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-09-17](https://openairdocs.org/ad/2001-09-17): Fuel Manifold and CJ9L Harness · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 13 more. Effective May 14, 2001
- [AD 2001-04-06](https://openairdocs.org/ad/2001-04-06): Fan Disk · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Apr 4, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000
- [AD 2000-05-22](https://openairdocs.org/ad/2000-05-22): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 2, 2000
- [AD 99-06-16](https://openairdocs.org/ad/99-06-16): High Pressure Turbine Rotor (HPTR) Front Air Seal · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Apr 21, 1999
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998
- [AD 98-19-10](https://openairdocs.org/ad/98-19-10): Accessory Gearbox · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Sep 28, 1998
- [AD 98-12-32](https://openairdocs.org/ad/98-12-32): High Pressure Turbine Rotor Disks · CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective Jul 20, 1998
- [AD 98-10-11](https://openairdocs.org/ad/98-10-11): Accessory Gearbox · CFM International CFM56-3, CFM56-3B, CFM56-3C and 31 more. Effective Jun 3, 1998
- [AD 98-07-02](https://openairdocs.org/ad/98-07-02): Air/oil Seal · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Mar 30, 1998
- [AD 98-02-04](https://openairdocs.org/ad/98-02-04): Low Pressure Turbine Case · CFM International CFM56-5B1/2P, CFM56-5B2/2P, CFM56-5B3/2P and 1 more. Effective Mar 23, 1998
- [AD 89-23-06 R1](https://openairdocs.org/ad/89-23-06-R1): Magnetic Chip Detector · CFM International CFM56-2, CFM56-2A, CFM56-3 and 8 more. Effective Jan 28, 1998
- [AD 97-08-01](https://openairdocs.org/ad/97-08-01): Fan Disks · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Jun 23, 1997
- [AD 97-06-01](https://openairdocs.org/ad/97-06-01): High Pressure Compressor Rotor (HPCR) Stage 1-2 Spool · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 28 more. Effective Jun 3, 1997
- [AD 97-05-13](https://openairdocs.org/ad/97-05-13): Air Turbine Engine Starter · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Jun 3, 1997
- [AD 96-25-11](https://openairdocs.org/ad/96-25-11): Redesigned Fan Blades · CFM International CFM56-3B and CFM56-3C. Effective Jan 29, 1997

### Historical (superseded or no longer in force)

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2013-02-02](https://openairdocs.org/ad/2013-02-02) (historical): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Jan 28, 2013
- [AD 2009-01-01](https://openairdocs.org/ad/2009-01-01) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 22 more. Effective Dec 31, 2008
- [AD 97-09-02 R2](https://openairdocs.org/ad/97-09-02-R2) (historical): Low pressure turbine rotor (LPTR) · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 9 more. Effective Apr 29, 2003
- [AD 2003-02-04](https://openairdocs.org/ad/2003-02-04) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5 Series (all). Effective Feb 27, 2003
- [AD 97-09-02 R1](https://openairdocs.org/ad/97-09-02-R1) (historical): High Pressure Turbine rotor (HPTR) front shaft · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Sep 24, 2002
- [AD 2001-17-14](https://openairdocs.org/ad/2001-17-14) (historical): LPT Conical Supports · CFM International CFM56-5C4/1. Effective Sep 7, 2001
- [AD 2001-08-51](https://openairdocs.org/ad/2001-08-51) (historical): Fuel leakage · CFM International CFM56-5 Series (all)
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000
- [AD 99-08-16](https://openairdocs.org/ad/99-08-16) (historical): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 13, 1999
- [AD 97-09-02](https://openairdocs.org/ad/97-09-02) (historical): High/Low Pressure Turbine Rotor · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Jun 30, 1997

All 71: https://openairdocs.org/aircraft/N549AS/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014
- [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution  CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012
- [SAIB NE-06-02](https://openairdocs.org/saib/NE-06-02): . Issued Oct 18, 2005
- [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013
- [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations

None matched to N549AS.

## FAA accident and incident reports

None matched to N549AS.

## Service difficulty reports (137, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASAA2026061266770](https://openairdocs.org/sdr/ASAA2026061266770), Jun 12, 2026: DOOR. NO DISCREPANCY. FA REPORTS L1 DOOR DIFFICULT TO CLOSE& LATCH. ABNORMAL WHISTLING NOTED FROM TAKEOFF TO APPROXIMATLY 10,000. GROUNDED - YES. INSPECTED SEAL AND CLEANED REF 52-11
- [SDR ASAA2026042865763](https://openairdocs.org/sdr/ASAA2026042865763), Apr 28, 2026: LAMP. INOPERATIVE. L1 SLIDE EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED L1 SLIDE EMERGENCY LIGHT REF AMM 33-51-04.
- [SDR ASAA2025122363358](https://openairdocs.org/sdr/ASAA2025122363358), Dec 23, 2025: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1672 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1672, OPS CHECK GOOD REF B737 AMM 33-51-06.
- [SDR ASAA2025122363357](https://openairdocs.org/sdr/ASAA2025122363357), Dec 23, 2025: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M2335 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M2335, OPS CHECK GOOD REF B737 AMM 33-51-06.
- [SDR ASAA2025122363356](https://openairdocs.org/sdr/ASAA2025122363356), Dec 23, 2025: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1675 ARE INOPERATIVE. GROUNDED - YES. REMOVED, REPLACED AND OPS TEST PERFORMED SUCCESSFULLY OF THE M1675 S/N 1092
- [SDR ASAA2025122363355](https://openairdocs.org/sdr/ASAA2025122363355), Dec 23, 2025: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1670 ARE INOP. GROUNDED - YES. REMOVED & REPLACED POWER SUPPLY M1670 S/N 27170, OPS CHECK GOOD. REF B737 AMM 33-5
- [SDR ASAA2025121363119](https://openairdocs.org/sdr/ASAA2025121363119), Dec 13, 2025: FLOOR PANEL. DAMAGED. AFT WET AREA CABIN FLOOR PANEL P/N 147A5810-23 REQUIRES REPAIRED 4 EACH HOLES NEED TO PLUGGED . GROUNDED - YES. ACCOMPLSIHED PERMANENT REPAIR TO AFT WET AREA CA
- [SDR ASAA2025121363118](https://openairdocs.org/sdr/ASAA2025121363118), Dec 13, 2025: FLOOR PANEL. DAMAGED. AFT WET AREA CABIN FLOOR PANEL P/N 147A5810-28 (STA 986 SIDE) REQUIRES REPAIRED (PLUG OF DELETE HOLES) MARKED WITH TAPE. GROUNDED - YES. ACCOMPLISHED PERMANENT 
- [SDR ASAA2025113063086](https://openairdocs.org/sdr/ASAA2025113063086), Nov 30, 2025: SUPPORT. CORRODED. MAIN CABIN AFT WET AREA STA 986 AT RBL 32 HAS A WALL SUPPORT (PN: 147A5710) THAT HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT O
- [SDR ASAA2025113063085](https://openairdocs.org/sdr/ASAA2025113063085), Nov 30, 2025: SUPPORT. CORRODED. MAIN CABIN AFT WET AREA BS 986, LBL 32 HAS A WALL SUPPORT (PN:147A5710) THAT HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND FOUND OUT OF LIMITS O
- [SDR ASAA2025113063084](https://openairdocs.org/sdr/ASAA2025113063084), Nov 30, 2025: FLOOR SUPPORT. CORRODED. MAIN CABIN AFT WET AREA (SEC. 47) STA 947 TO STA 967 FLOOR SUPPORT AT RBL 16 HAS CORROSION ON THE UPPER SURFACE. GROUNDED - YES. REMOVED CORROSION ON FLOOR SUPP
- [SDR ASAA2025113063083](https://openairdocs.org/sdr/ASAA2025113063083), Nov 30, 2025: FLOOR SUPPORT. CORRODED. AFT WET AREA FLOOR SUPPORT, BS 967 - 986, LBL 14 HAD AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, OR
- [SDR ASAA2025112663082](https://openairdocs.org/sdr/ASAA2025112663082), Nov 26, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPOR BS 947-967, LBL 24 HAD SEVERAL AERAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON THE FLOOR SUPPORT BS 947-967, LBL 24, LOST .035" OF MATERIA
- [SDR ASAA2025112663081](https://openairdocs.org/sdr/ASAA2025112663081), Nov 26, 2025: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT BS 947-967 RBL 24 HAS SEVERAL AERAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON FLOOR SUPPORT AT BS 947-967, RBL 24, LOST .030" OF MATER
- [SDR ASAA2025112162749](https://openairdocs.org/sdr/ASAA2025112162749), Nov 21, 2025: BAFFLE. CRACKED. FWD CARGO PIT LT BAFFLE CRACKED BS 500 - 500A. GROUNDED - YES. REMOVED BAFFLE AT FWD CARGO BS 500-500A LT, RECEIVED BAFFLEP/N: 143A7510-17, P.O.# 1137749.1, LOC
- [SDR ASAA2025112062772](https://openairdocs.org/sdr/ASAA2025112062772), Nov 20, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL HAS COMPOSITE DAMAGE. GROUNDED - YES. EVALUATED PANEL FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS, REQUIRES FABRICATION OF NEW PANEL IAW SRM 53-00-50
- [SDR ASAA2025112062771](https://openairdocs.org/sdr/ASAA2025112062771), Nov 20, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL IS DELAMINATED. GROUNDED - YES. FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 143A5810-90, REV-.
- [SDR ASAA2025112062770](https://openairdocs.org/sdr/ASAA2025112062770), Nov 20, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL IS DELAMINATED. GROUNDED - YES. FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 143A5810-43, REV:-.
- [SDR ASAA2025112062769](https://openairdocs.org/sdr/ASAA2025112062769), Nov 20, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL IS DELAMINATED. GROUNDED - YES. FABRICATED NEW FLOOR PANEL IAW DWG 146A5810 SH 31 REV B, AND SRM 53-00-50-2R-0.
- [SDR ASAA2025112062768](https://openairdocs.org/sdr/ASAA2025112062768), Nov 20, 2025: FLOOR PANEL. DELAMINATED. FLOOR PANEL 146A5810-71 IS DELAMINATED. GROUNDED - YES. FABRICATED NEW FLOOR PANEL IAW DWG 146A5810 SH 71 REV-, AND SRM 53-00-50-2R-0.
- [SDR ASAA2025111562559](https://openairdocs.org/sdr/ASAA2025111562559), Nov 15, 2025: BAFFLE. CORRODED. AFT CARGO, RIGHT INTERCOSTAL BAFFLE HAS CORRODED ON THE TOP SURFACE, BS 747 - 767, S25 - S26R. GROUNDED - YES. EVALUATED BAFFLE AND FOUND TO BE OUT OF LIMITS DU
- [SDR ASAA2025111462748](https://openairdocs.org/sdr/ASAA2025111462748), Nov 14, 2025: BRACKET. CORRODED. AFT CARGO DOOR CUTOUT, FORWARD LOWER MAIN SILL, BRACKET ASSY HAS CORRODED IN RIGHT SIDE BS 787 - 794.37, S25R. GROUNDED - YES. EVALUATED AFT CARGO FWD LOWER MAI
- [SDR ASAA2025111163359](https://openairdocs.org/sdr/ASAA2025111163359), Nov 11, 2025: SKATE ANGLE. CRACKED. CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE CRACK AT BS 661.95 LBL+7. GROUNDED - YES. REPAIRED CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE IAW SRM 57-10-1
- [SDR ASAA2025111163354](https://openairdocs.org/sdr/ASAA2025111163354), Nov 11, 2025: ANGLE. CRACKED. CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE CRACK AT BS 661.95 RBL+9. GROUNDED - YES. REPAIRED CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE AT BS 661.95 RB
- [SDR ASAA2025111163080](https://openairdocs.org/sdr/ASAA2025111163080), Nov 11, 2025: FLOORBEAM. CORRODED. AFT WET AREAS BS 986.5 TEE CAP APPROX. BETWEEN RBL 24 TO RBL 58 HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 
- [SDR ASAA2025111163079](https://openairdocs.org/sdr/ASAA2025111163079), Nov 11, 2025: FLOORBEAM. CORRODED. AFT WET AREA STA 947.5 TEE CAP APPROX. BETWEEN LBL 24 TO RBL 24 HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 
- [SDR ASAA2025111163078](https://openairdocs.org/sdr/ASAA2025111163078), Nov 11, 2025: INTERCOSTAL. CORRODED. RIGHT AFT INTERCOSTAL AT BS 947.5 APPROX, RBL 51 HAS SEVERAL AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON INTERCOSTAL AT BS. 947 RBL 51, LOST .045" 
- [SDR ASAA2025111163077](https://openairdocs.org/sdr/ASAA2025111163077), Nov 11, 2025: INTERCOSTAL. CORRODED. LEFT AFT INTERCOSTAL AT BS 947.5, APPROX LBL 51 HAS SEVERAL AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON INTERCOSTAL AT BS 947-967 LBL 51, LOST .035
- [SDR ASAA2025111162747](https://openairdocs.org/sdr/ASAA2025111162747), Nov 11, 2025: TRANSITION PANEL. CORRODED. AFT CARGO PIT RT TRANSITION PANEL BS 727 - 767 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO 
- [SDR ASAA2025111162745](https://openairdocs.org/sdr/ASAA2025111162745), Nov 11, 2025: TRANSITION PANEL. CORRODED. FWD CARGO PIT LT TRANSITION PANEL BS 500 - 500I HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO
- [SDR ASAA2025111162583](https://openairdocs.org/sdr/ASAA2025111162583), Nov 11, 2025: WEB. CORRODED. AFT CARGO PIT THRESHOLD WEB HAS CORROSION. GROUNDED - YES. EVALUATED AFT CARGO THRESHOLD WEB, ORIGINAL THICKNESS .045, REMOVED .024, REMAINING .021, FOUND TO BE
- [SDR ASAA2025111162562](https://openairdocs.org/sdr/ASAA2025111162562), Nov 11, 2025: TRANSITION PANEL. CORRODED. AFT CARGO PIT LT TRANSITION PANEL BS 727 - 847 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL MATERIAL 0.040, REMOVED 0.040, REMANINING 0.000, FOUND 
- [SDR ASAA2025111162561](https://openairdocs.org/sdr/ASAA2025111162561), Nov 11, 2025: SUPPORT. CORRODED. FWD CARGO PIT, AFT BULKHEAD SUPPORT LOWER RAIL STA 500I HAS CORROSION. GROUNDED - YES. EVALUATED ORIG THICK=.071", REMOVED .071, REMAINING .000 100% MAT LOSS FO
- [SDR ASAA2025111162560](https://openairdocs.org/sdr/ASAA2025111162560), Nov 11, 2025: TRANSITION PANEL. CORRODED. FWD CARGO PIT RT TRANSITION PANEL STA 500A - STA 500I HAS CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS IS .040 REMOVED .040, REMAINING THICK
- [SDR ASAA2025111063087](https://openairdocs.org/sdr/ASAA2025111063087), Nov 10, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL 147A5810-186 HAS DAMAGED AND MISSING INSERTS. GROUNDED - YES. FABRICATED NEW FLOOR PANEL 147A5810-186 IAW B737-800 SRM 53-00-50-2R-0 AND DRAWING 147
- [SDR ASAA2025111062773](https://openairdocs.org/sdr/ASAA2025111062773), Nov 10, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL HAS DAMAGED INSERTS. GROUNDED - YES. REMOVED AND REPLACED 20EA DAMAGED INSERTS ON FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR ASAA2025100561351](https://openairdocs.org/sdr/ASAA2025100561351), Oct 5, 2025: POWER SUPPLY. INOPERATIVE. DURING T/C 78233008, FOUND RT AISLE EMERGENCY EXIT LT'S INOP. GROUNDED - YES. VERIFIED DISCREPANCY AND FOUND POWER SUPPLY M1671 TO BE INOP REF WDM 33-51-14. REM
- [SDR ASAA2025100561350](https://openairdocs.org/sdr/ASAA2025100561350), Oct 5, 2025: POWER SUPPLY. INOPERATIVE. DURING T/C 78233008, FOUND RH AFT OVERWING EXIT EMERGENCY LT INOP. GROUNDED - YES. VERIFIED DISCREPANCY AND FOUND POWER SUPPLY M1671 TO BE INOP REF WDM 33-51-14
- [SDR ASAA2025092060983](https://openairdocs.org/sdr/ASAA2025092060983), Sep 20, 2025: COVER. DETACHED. FA'S FOUND EMERGENCY SIGN COVER FELL OFF AT ROW 16 ABC. GROUNDED - YES. REINSTALLED EMERGENCY COVER REF AMM 33-51-01.
- [SDR ASAA2025091960984](https://openairdocs.org/sdr/ASAA2025091960984), Sep 19, 2025: COVER. MISSING. EMERGENCY EXIT LIGHT COVER AT 16A IS MISSING. GROUNDED - YES. REPLACED MISSING EMERGENCY EXIT LIGHT COVER AT 16A REF AMM 33-51-01-960-802.
- [SDR ASAA2025032856960](https://openairdocs.org/sdr/ASAA2025032856960), Mar 28, 2025: LENS. MISSING. LIGHTED PLACARD MISSING NEXT TO A/C LEFT AFT LAV. GROUNDED - YES. REPLACED LIGHT ASSYM INFRONT OF LAV FOR EMERGENCY EXIT AREA LIGHT IAW CMM 25-43-82. OPS TEST G
- [SDR ASAA2024121354546](https://openairdocs.org/sdr/ASAA2024121354546), Dec 13, 2024: LIGHT. NO DISCREPANCY. FA REPORTED EMERGENCY LIGHT ROW 16 ABC NOT ILLUMINATED. GROUNDED - YES. PERFORMED OPS-TEST OF EMER LTS FOR ROW 16 ABC/DEF: ALL LIGHTS @ THAT LOCATION WORKS: NO 
- [SDR ASAA2024090652349](https://openairdocs.org/sdr/ASAA2024090652349), Sep 6, 2024: HOUSING. BROKEN. EMERGENCY EXIT SIGN ON R1 DOOR FOUND DETACHED AND BROKEN. GROUNDED - YES. R1 DOOR EMERGENCY EXIT SIGN HOUSING & LENS REMOVED AND REPLACED REF AMM 33-51-01-960-8
- [SDR ASAA2024072451297](https://openairdocs.org/sdr/ASAA2024072451297), Jul 24, 2024: LAMP. INOPERATIVE. R1 DOOR EXTERNAL EMERGENCY & AFT LEFT WHEEL WELL EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED R1 DOOR EXTERNAL EMERGENCY LIGHT & AFT LEFT WHEEL WELL EMERGENCY
- [SDR ASAA2024031748496](https://openairdocs.org/sdr/ASAA2024031748496), Mar 17, 2024: OIL SYSTEM. LEAKING. FA'S REPORT ODOR OF MUST, MOLD, DIRTY SOCKS. SYMPTOMS INCLUDING HEADACHE, DIZZINESS, FATIGUE. CABIN AIR REPORTING FORM INCLUDED ODOR INCREASED DRAMATICALLY AT 4
- [SDR ASAA2023111447207](https://openairdocs.org/sdr/ASAA2023111447207), Nov 14, 2023: SKIN. CRACKED. L/H HORIZONTAL LOWER SKIN HAS 2 EA CRACKS AT STA 100.0 ONE 20 INCHES FROM T/E THE OTHER 29 INCHES FROM T/E. GROUNDED - YES. REPAIRED L/H HORIZONTAL LOWER SKIN C
- [SDR ASAA2023061343580](https://openairdocs.org/sdr/ASAA2023061343580), Jun 13, 2023: LAMP. INOPERATIVE. FLIGHT ATTENDANT REPORTS EMERGENCY EXIT LIGHT ABOVE SEAT 17F INOP. GROUNDED - YES. RELAMPED EMERGENCY EXIT LIGHT ABOVE SEAT 17F REF AMM 33-51-00.
- [SDR ASAA2022070338892](https://openairdocs.org/sdr/ASAA2022070338892), Jul 3, 2022: SIGN. INOPERATIVE. AFT GALLEY EXIT/SALIDA 4ER LIGHTS R/H SIDE INOP. GROUNDED - YES. RELAMPED AFT GALLEY EXIT/SALIDA SIGN REF B737-800 AMM 33-51-01. OPS CHK OK.
- [SDR ASAA2022070338891](https://openairdocs.org/sdr/ASAA2022070338891), Jul 3, 2022: LAMP. INOPERATIVE. EXTERIOR L1 DOOR ER LIGHT INOP. GROUNDED - YES. RELAMPED L1 SLIDE ER LT REF B737-800 AMM 33-51-04. OPS CHK OK.
- [SDR ASAA2022060838594](https://openairdocs.org/sdr/ASAA2022060838594), Jun 8, 2022: SIGN. INOPERATIVE. L2 DOOR EXIT SIGN INOP. GROUNDED - YES. RELAMPED IAW AMM B737-800 33-51-01. OPS NORMAL.

All 137: https://openairdocs.org/aircraft/N549AS/reports.md

## STCs that may be installed (OpenAirDocs) (37)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Boeing 737-8FH)

- [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series
- [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series
- [STC SA270NW](https://openairdocs.org/stc/SA270NW): Installation of modified seat. Aviation Technical Services. Lists 737 Series
- [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 737 Series
- [STC SA2607SO](https://openairdocs.org/stc/SA2607SO): Installation of coffee maker P/N 416-1001-29. B/E Aerospace Inc. Lists 737 Series
- [STC SA2608SO](https://openairdocs.org/stc/SA2608SO): Installation of rail assembly, P/N 416-0201-15. B/E Aerospace Inc. Lists 737 Series
- [STC SA3058SO](https://openairdocs.org/stc/SA3058SO): Installation of coffee maker 416-0001-23 and rail assembly 416-0201-5. B/E Aerospace Inc. Lists 737 Series
- [STC ST01476AT](https://openairdocs.org/stc/ST01476AT): Installation of coffee maker. B/E Aerospace Inc. Lists 737 Series
- [STC ST01778AT](https://openairdocs.org/stc/ST01778AT): Installation of espresso maker p/n 3510-0066-01. B/E Aerospace Inc. Lists 737 Series
- [STC SA629GL](https://openairdocs.org/stc/SA629GL): Installation of Grimes galley, Model 1545LW unit 2 and unit 4. B/E Aerospace. Lists 737 Series
- [STC ST01332AT](https://openairdocs.org/stc/ST01332AT): Installation of Galley Service Carts. Champ International, Inc. Lists 737 Series
- [STC ST09870SC](https://openairdocs.org/stc/ST09870SC): Installation of Mechanical Window Shades. Lou Martin & Associates. Lists 737 Series
- [STC ST00033AT](https://openairdocs.org/stc/ST00033AT): Installation of a single Mode S system and provisions for a TCAS II system. General Aerospace, Inc. Lists 737 Series
- [STC SA4532NM](https://openairdocs.org/stc/SA4532NM): Installation of Coltech, CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series
- [STC ST4532NM](https://openairdocs.org/stc/ST4532NM): Installation of Coltech CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series
- [STC ST00774NY](https://openairdocs.org/stc/ST00774NY): Installation of a passenger cabin Liquor/beverage service cart P/N E500170. (757-222) (767-222) (727-222) (737 SERIES 222, 291, 322, 522) (747-100 SERIES 238B). Driessen Aircraft Interior Systems USA, Inc. Lists 737 Series
- [STC ST02052AT](https://openairdocs.org/stc/ST02052AT): Installation of a single Collins GNLU910A flight management system, along with global navigation satellite system sensor. General Aerospace, Inc. Lists 737 Series
- [STC SA02034AT](https://openairdocs.org/stc/SA02034AT): Manufacture of tray carrier, P/N 2282-506. BFE Services. Lists 737 Series
- [STC ST01968AT](https://openairdocs.org/stc/ST01968AT): Manufacture of inserts for galley stowage. JK Aerospace, Inc. Lists 737 Series
- [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 737 Series
- [STC SA2534SO](https://openairdocs.org/stc/SA2534SO): Installation of window shades, acoustic panes and reveals. Magee Plastics Company. Lists 737 Series
- [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists 737 Series
- [STC SA00056LA](https://openairdocs.org/stc/SA00056LA): Installation of Weber Coffeemaker, P/N 870130-415. Monogram Systems. Lists 737 Series
- [STC SA6090NM](https://openairdocs.org/stc/SA6090NM): Installation of emergency vision assurance system (EVAS). VisionSafe Corporation. Lists 737 Series
- [STC SA370NW](https://openairdocs.org/stc/SA370NW): Removal of passenger interior, installation of cargo compartment liners and cargo tie down equipment. Western Metal Products. Lists 737 Series
- [STC SA2589CE](https://openairdocs.org/stc/SA2589CE): Install Bennetts Seat Converter Stowage Compartment on passenger seat(s). John's Aircraft and Upholstery. Lists 737 Series
- [STC SA1029NW](https://openairdocs.org/stc/SA1029NW): Installation of a cargo system. Western Metal Products. Lists 737 Series
- [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 737 Series
- [STC SA1052SO](https://openairdocs.org/stc/SA1052SO): Installation of GE battery P/N43B022RB36 in place of Marathon P/N CA-727-7, CA-727-20, or CA-27-20 batteries or SAFT P/N23180 batteries; or installation of GE battery P/N 43B020RB10 replacing Marathon P/N CA-727-7, CA-727-20 or CA-27-20 or SAFT P/N 23186 or 23180 batteries. General Electric Company. Lists 737 Series
- [STC SA1082NW](https://openairdocs.org/stc/SA1082NW) (historical): Installation of auxiliary fuel tanks in the aft cargo compartment. (737 series -2K9A). Rogerson ATS. Lists 737 Series

### Approved for the engine (CFM International CFM56 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC. Lists CFM56-7B20
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc. Lists CFM56-7B20
- [STC SE00032EN](https://openairdocs.org/stc/SE00032EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00033EN](https://openairdocs.org/stc/SE00033EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00034EN](https://openairdocs.org/stc/SE00034EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00035EN](https://openairdocs.org/stc/SE00035EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00822CH](https://openairdocs.org/stc/SE00822CH): Install AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines. AeroControlex Group TransDigm Inc. Lists CFM56-2

## Earlier aircraft with N549AS

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N549AS before.

- [Cancelled 2000-01-31](https://openairdocs.org/deregistered/N549AS-2000-01-31): Dassault-Breguet FALCON 10, S/N 87. Exported to Canada. Owner: [Asc Transportation Inc](https://openairdocs.org/faa-owner/ASC%20TRANSPORTATION%20INC), [Bethel, ME](https://openairdocs.org/faa-place/ME/Bethel)

## Related

- Other Boeing 737-8FH aircraft: https://openairdocs.org/model/boeing-737-8fh/aircraft.md
- The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md

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