# N8651A: 2014 Boeing 737-8H4

- Status: Valid registration
- Airframe: [Boeing 737-8H4](https://openairdocs.org/model/boeing-737-8h4) (registry code 138440A, 143 seats)
- Engine: [CFM International CFM56-7B27E series](https://openairdocs.org/engine/cfm-international-cfm56-7b27e-series) (registry code 13078)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 36920
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 16, 2014
- Certificate issued: October 30, 2014
- Expires: October 31, 2027
- Mode S code: ABE3E6
- Registered owner: [Southwest Airlines Co](https://openairdocs.org/faa-owner/SOUTHWEST%20AIRLINES%20CO)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: Corporation
- Owner's area on the map: 32.8326° N, 96.8491° W: Placed by OpenAirDocs at the center of ZIP code 75235, 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=8651A
- Page: https://openairdocs.org/aircraft/N8651A

From the FAA registry file of October 24, 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 CFM56-7B27E model are included.

## ADs that may apply (OpenAirDocs): 6 in force

### Matched by airframe (Boeing 737-8H4)

None in force.

### Matched by engine (CFM International CFM56-7B27E 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 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 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 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

### 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 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

## Information bulletins (advisory) (1 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-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011

## NTSB investigations

None matched to N8651A.

## FAA accident and incident reports

None matched to N8651A.

## Service difficulty reports (181, 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 SWAA2026081704440](https://openairdocs.org/sdr/SWAA2026081704440), Jul 20, 2026: ANGLE. CRACKED. CRACK ON ANGLE FWD FACE BS 500E, STR 26R. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7505, SHEET 151, REV-.
- [SDR SWAA2026081724384](https://openairdocs.org/sdr/SWAA2026081724384), Jul 18, 2026: WEB. CRACKED. CRACKED WEB, BS 400 - 420, STR 26L IN FWD CARGO BAY. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 151, REV-.
- [SDR SWAA2026081789106](https://openairdocs.org/sdr/SWAA2026081789106), Jul 14, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE T-E, IRSS 213, LT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 115A2713, SHT 6, REV A, & DWG: 115A20
- [SDR SWAA2026081744521](https://openairdocs.org/sdr/SWAA2026081744521), Jul 14, 2026: WEB. CRACKED. CRACKED WEB, ORSS 275, LT WING T/E. REPLACED THE WEB, IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 16, REV-.
- [SDR SWAA2026081783357](https://openairdocs.org/sdr/SWAA2026081783357), Jul 13, 2026: SEAT TRACK. CORRODED. CORROSION ON UPPER FLANGE OF SEAT TRACK, RBL 24.75, BTWN BS 867 - 887, WL 208.1. PERFORMED A PERMANENT REPAIR IAW SRM 53-00-522R-5, REPAIR 5, FIGURE 202, SHTS 1
- [SDR SWAA2026081746486](https://openairdocs.org/sdr/SWAA2026081746486), Jul 13, 2026: STRAP. CORRODED. CORRODED TEE STRAP, BS 887, BTWN STRINGERS 27L - 25R, AFT CARGO BAY. REPLACED THE TEE STRAP IAW SRM 51-40-02-0G, SRM 51-10-02, ITEM 9, DWG 146A7500, SHEET 236, 
- [SDR SWAA2026081737204](https://openairdocs.org/sdr/SWAA2026081737204), Jul 13, 2026: SUPPORT CHANNEL. CORRODED. CORROSION ON SUPPORT ZEE, BTWN BS 500A - 500D + 10 INCHES, RBL 21, WL 156 IN THE FWD CARGO BAY. REPAIRED SUPPORT CHANNEL IAW SRM 53-00-53-2R-5, REPAIR 5, & EA M
- [SDR SWAA2026081768901](https://openairdocs.org/sdr/SWAA2026081768901), Jul 13, 2026: WEB. CORRODED. CORRODED SHIELD WEB, BS 847 - 867, WL 156, RBL 21. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A0081, SHEET 49, REV A.
- [SDR SWAA2026081780982](https://openairdocs.org/sdr/SWAA2026081780982), Jul 13, 2026: FITTING. CRACKED. CRACKED FITTING, BS 947.5, STR 26L IN THE AFT CARGO BAY. REPLACED THE FITTING IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
- [SDR SWAA2026081721686](https://openairdocs.org/sdr/SWAA2026081721686), Jul 13, 2026: WEB. CORRODED. CORRODED SHIELD WEB BTWN BS 767 - 794.3, WL 156, RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 
- [SDR SWAA2026081786066](https://openairdocs.org/sdr/SWAA2026081786066), Jul 13, 2026: WEB. CORRODED. CORRODED WEB, BS 747 - 767, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 236, REV -, & DWG 
- [SDR SWAA2026081796776](https://openairdocs.org/sdr/SWAA2026081796776), Jul 13, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, AFT FACE OF PRESSURE BULKHEAD BS 727, RBL 3, IN THE AFT CARGO BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9,
- [SDR SWAA2026081736647](https://openairdocs.org/sdr/SWAA2026081736647), Jul 13, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 241KF IN PAX CABIN. REPAIRED THE FLOOR PANEL 241KF IAW SRM 53-00-50-2R-7, REPAIR 7.
- [SDR SWAA2026081754292](https://openairdocs.org/sdr/SWAA2026081754292), Jul 12, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 380 - 400, LBL 50, PAX CABIN. REPLACED WITH A NEW ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHT 183, REV-.
- [SDR SWAA2026081713353](https://openairdocs.org/sdr/SWAA2026081713353), Jul 12, 2026: ANGLE. CRACKED. CRACKED ANGLE BTWN BS 380 - 400, RBL 41, IN PAX CABIN. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A5400, SHT 140, REV-.
- [SDR SWAA2026081766876](https://openairdocs.org/sdr/SWAA2026081766876), Jul 12, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 380 - 400, LBL 13. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 182, SHEET 184, REV -.
- [SDR SWAA2026081709513](https://openairdocs.org/sdr/SWAA2026081709513), Jul 12, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 380 - 400, BL 0 IN THE PAX CABIN. REPLACED ANGLE & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 154, REV- .
- [SDR SWAA2026081746886](https://openairdocs.org/sdr/SWAA2026081746886), Jul 12, 2026: BRACKET. CRACKED. CRACKED BRACKET ON ACCESS PANEL 834DZ IN PAX CABIN. REPLACED THE BRACKET ON ACCESS PANEL 834DZ IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
- [SDR SWAA2026081768736](https://openairdocs.org/sdr/SWAA2026081768736), Jul 12, 2026: WEB. CRACKED. CRACKED WEB, BS 500G - 500H, STR 26R. REPLACED THE WEB & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHT 151, REV-.
- [SDR SWAA2026081751933](https://openairdocs.org/sdr/SWAA2026081751933), Jul 12, 2026: ANGLE. CRACKED. CRACKED ANGLE FLOOR STRUCTURE BTWN BS 380 - 400, RBL 10. REPLACED THE ANGLE IAW SRM 51-40-02, & SRM 51-10-02, ITEM 9, DWG 143A5400, SHT 139, REV-, & DWG 143A540
- [SDR SWAA2026081744181](https://openairdocs.org/sdr/SWAA2026081744181), Jul 11, 2026: ANGLE. ELONGATED. ELONGATED HOLE ON ANGLE IN UPPER AREA AT ACCESS PANEL 324AAL T/E AT VERTICAL STAB. REPLACED ANGLE LOCATED UPPER AREA AT LEVEL ACCESS PANEL 324AAL TRAILING EDGE 
- [SDR SWAA2026081794996](https://openairdocs.org/sdr/SWAA2026081794996), Jul 10, 2026: NUT PLATE. CRACKED. CRACKED RAIL NUT PLATE, INTERNAL CAVITY, LEADING EDGE OF SS 570 RT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 112A4402, SHT 40,
- [SDR SWAA2026081726891](https://openairdocs.org/sdr/SWAA2026081726891), Jul 10, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE ON ACCESS PANEL 651FB, RT WING. REPLACED SUPPORT ANGLE ON ACCESS PANEL 651FB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02.
- [SDR SWAA2026081746948](https://openairdocs.org/sdr/SWAA2026081746948), Jul 10, 2026: BRACKET. CRACKED. CRACKED BRACKET ON ACCESS PANEL 551FB, LT WING. EVALUATED AND DID NOT FIND ALLOWABLE DAMAGE IN SRM 57-41-02-1A-2, ALLOWABLE DAMAGE 2, BRACKET MUST BE REPLACED. 
- [SDR SWAA2026081725572](https://openairdocs.org/sdr/SWAA2026081725572), Jul 10, 2026: WEB. CRACKED. CRACKED WEB, LEADING EDGE INTERNAL CAVITY, SS 308 + 23 INCHES, LT WING. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 116A5440, SHEET 50, REV B
- [SDR SWAA2026081744212](https://openairdocs.org/sdr/SWAA2026081744212), Jul 9, 2026: CROSSBEAM. CRACKED. CRACKED BRAKE PANEL ON FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO LBL 24.75. REPLACED BRAKE PANEL ON FLOOR STRUCTURE IAW SRM 51-10-02, ITEM 9, AND DWG 143A
- [SDR SWAA2026081733855](https://openairdocs.org/sdr/SWAA2026081733855), Jul 9, 2026: CROSSBEAM. CRACKED. CRACK BRAKE PANEL ON FLOOR STRUCTURE, BS 540 BTW BL 0 - RBL 24.75 IN PASSENGER CABIN. REPLACED BRAKE PANEL AND FASTENERS ON FLOOR STRUCTURE IAW SRM 51-10-02, IT
- [SDR SWAA2026081713354](https://openairdocs.org/sdr/SWAA2026081713354), Jul 7, 2026: FRAME. CORRODED. CORRODED FRAME, BS 303.9, BTWN STR 16L - 17L, WL 210. REPAIRED THE FRAME IAW EA 26-153-01946-WIP1, & EA 26-153-01946.
- [SDR SWAA2026081794249](https://openairdocs.org/sdr/SWAA2026081794249), Jul 7, 2026: WEB. CRACKED. CRACKED WEB, BS 277 - 294.5, BL 0 IN THE FWD GALLEY. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 20, REV-.
- [SDR SWAA2026081778665](https://openairdocs.org/sdr/SWAA2026081778665), Jul 7, 2026: WEB. CRACKED. CRACKED WEB, BS 312 - 328, RBL 31. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 141A5400, SHT 39, REV-.
- [SDR SWAA2026081712281](https://openairdocs.org/sdr/SWAA2026081712281), Jul 7, 2026: WEB. CRACKED. CRACK WEB, BS 344 - 360, BL 0 IN THE FWD GALLEY AREA. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 32, REV-.
- [SDR SWAA2026081790900](https://openairdocs.org/sdr/SWAA2026081790900), Jul 7, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT, BS 312 - 328, LBL 45, IN THE FWD GALLEY AREA. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 141A5400, SHT 26, REV-
- [SDR SWAA2026081746099](https://openairdocs.org/sdr/SWAA2026081746099), Jul 7, 2026: STIFFENER. CORRODED. CORRODED STIFFENER, BS 328 - 344, LBL 12, WL 208.1 IN THE FWD GALLEY AREA. REPLACED THE STIFFENER IAW SRM 51-40-02, SRM 51-10-02, PARA 9, & DWG 141A5400, SHEET 
- [SDR SWAA2026081767691](https://openairdocs.org/sdr/SWAA2026081767691), Jul 7, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 867 BTWN STR 26 - 27L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
- [SDR SWAA2026081786719](https://openairdocs.org/sdr/SWAA2026081786719), Jul 7, 2026: STIFFENER. CORRODED. CORRODED STIFFENER, BTWN BS 312 - 328, LBL 12, WL 208.1 IN THE FWD GALLEY. REPLACED STIFFENER IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DWG 141A5400, SHT 2
- [SDR SWAA2026081796739](https://openairdocs.org/sdr/SWAA2026081796739), Jul 7, 2026: ANGLE. CRACKED. CRACKED ANGLE BTWN BS 291.5 & 294.5, STR 17R AT FWD GALLEY. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 141A8310, SHEET 33, REV- .
- [SDR SWAA2026081743735](https://openairdocs.org/sdr/SWAA2026081743735), Jul 6, 2026: STIFFENER. CORRODED. CORRODED FLOOR STRUCTURE STIFFENER BTW BS 947.5 & 967, LBL 25, WL 208.1 IN THE AFT GALLEY AREA. REPLACED THE STIFFENER IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, &
- [SDR SWAA2026081783395](https://openairdocs.org/sdr/SWAA2026081783395), Jul 6, 2026: SUPPORT ANGLE. CRACKED. CRACK CARGO LINER SUPPORT ANGLE ON STA 867 AND RBL 53 AT AFT CARGO COMPARTMENT. REPAIRED CARGO LINER SUPPORT ANGLE IAW SRM 51-70-11-2R-0, REPAIR GENERAL.
- [SDR SWAA2026081779140](https://openairdocs.org/sdr/SWAA2026081779140), Jul 6, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561AB, LT WING. REPAIRED ACCESS PANEL 561AB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026081799058](https://openairdocs.org/sdr/SWAA2026081799058), Jul 6, 2026: FLOOR SUPPORT. CORRODED. CORRODED FLOOR SUPPORT, BTWN BS 947.5 + 4 INCHES, LBL 19, WL 208.1 IN THE AFT GALLEY AREA. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 
- [SDR SWAA2026081738695](https://openairdocs.org/sdr/SWAA2026081738695), Jul 6, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026081792024](https://openairdocs.org/sdr/SWAA2026081792024), Jul 6, 2026: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 193AL. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-2, REPAIR 2.
- [SDR SWAA2026081795975](https://openairdocs.org/sdr/SWAA2026081795975), Jul 6, 2026: SUPPORT ANGLE. CRACKED. CRACKED CARGO LINER SUPPORT ANGLE, BS 887, RBL 53, IN AFT CARGO BAY. REPAIRED THE SUPPORT ANGLE IAW SRM 51-70-11-2R-0, REPAIR GENERAL.
- [SDR SWAA2026081771499](https://openairdocs.org/sdr/SWAA2026081771499), Jul 6, 2026: ACCESS PANEL. CRACKED. ELONGATED HOLES ON LT WING ACCESS PANEL 561BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026081767654](https://openairdocs.org/sdr/SWAA2026081767654), Jul 6, 2026: WEB. CRACKED. CRACKED WEB, BS 887 - 867, LBL 22 CEILING AREA IN THE AFT CARGO BAY. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, & DWG 149A8100, SHEET 1, REV -.
- [SDR SWAA2026081770746](https://openairdocs.org/sdr/SWAA2026081770746), Jul 6, 2026: FLOOR SUPPORT. CORRODED. CORROSION INTERCOSTAL FLOOR SUPPORT LOCATED BS947.5 + 4 INCHES, LBL 30, WL 208.1. REPLACED THE SUPPORT IAW SRM 51-40-02, & DWG 147A5650, SHT 55, REV A.
- [SDR SWAA2026081781900](https://openairdocs.org/sdr/SWAA2026081781900), Jul 6, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 193AL AT LOWER FUSELAGE. REPAIRED HOLES ON ACCESS PANEL 193AL AT LOWER FUSELAGE IAW SRM 51-70-05-2R-10 REPAIR 10.
- [SDR SWAA2026081706101](https://openairdocs.org/sdr/SWAA2026081706101), Jul 5, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661AB, RT WING. REPAIRED THE ACCESS PANEL 661AB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026081733965](https://openairdocs.org/sdr/SWAA2026081733965), Jul 5, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661CB ON RT WING. REPAIRED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026081735839](https://openairdocs.org/sdr/SWAA2026081735839), Jul 5, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON RT WING ACCESS PANEL 661BBN. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.

All 181: https://openairdocs.org/aircraft/N8651A/reports.md

## STCs that may be installed (OpenAirDocs) (31)

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 737-8H4)

- [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 CFM56-7B27E series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC

## Earlier aircraft with N8651A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8651A before.

- [Cancelled 1951-09-07](https://openairdocs.org/deregistered/N8651A-1951-09-07): Beech A35, S/N D-2061. Owner: [Neon Products Inc](https://openairdocs.org/faa-owner/NEON%20PRODUCTS%20INC), [Kokomo, IN](https://openairdocs.org/faa-place/IN/Kokomo)

## Related

- Other Boeing 737-8H4 aircraft: https://openairdocs.org/model/boeing-737-8h4/aircraft.md
- The CFM International CFM56-7B27E series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b27e-series.md

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