# N8650F: 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: 36909
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 27, 2014
- Certificate issued: October 15, 2014
- Expires: October 31, 2027
- Mode S code: ABE3C8
- 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=8650F
- Page: https://openairdocs.org/aircraft/N8650F

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 N8650F.

## FAA accident and incident reports

None matched to N8650F.

## Service difficulty reports (165, 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 SWAA2026082179206](https://openairdocs.org/sdr/SWAA2026082179206), Aug 17, 2026: FAIRING. PULLED. NR 3 FLAP SUPPORT FAIRING HAS 2 PULLED RIVETS. HOLES OVERSIZED, REQUIRES FAIRING REPLACEMENT. REMOVED THE NR 3 FLAP TRACK FAIRING IAW AMM 27-51-18, REF WO 12852
- [SDR SWAA2026081049387](https://openairdocs.org/sdr/SWAA2026081049387), Aug 6, 2026: BATTERY. INOPERATIVE. AFT LEFT OTBD FA FLASHLIGHT WAS INOPERATIVE. REPORTED BY CREW. R & R THE AFT LT OTBD FA FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHKD GOOD.
- [SDR SWAA2026072182417](https://openairdocs.org/sdr/SWAA2026072182417), Jul 20, 2026: BATTERY. FAULTED. F/A REPORTS AFT ENTRY DOOR EMERGENCY LIGHTS ILLUMINATED IN FLIGHT AND THAN EXTINGUISHED. R & R AFTER BATTERY AND POWER SUPPLY IAW AMM 33-51-06, OPS CHKD GOOD.
- [SDR SWAA2026072155717](https://openairdocs.org/sdr/SWAA2026072155717), Jul 20, 2026: BATTERY. FAULTY. F/A REPORTS AFT ENTRY DOOR EMERGENCY LIGHTS ILLUMINATED IN FLIGHT AND THEN EXTINGUISHED. R & R AFT BATTERY AND POWER SUPPLY IAW AMM 33-51-06 OPS CK GOOD.
- [SDR SWAA2026072164458](https://openairdocs.org/sdr/SWAA2026072164458), Jul 14, 2026: INSERT. DAMAGED. DAMAGED INSERT LOCATED ON GIRT BAR PLATE AREA ON FLOOR PANEL 241ABF AT AFT GALLEY AREA (3EA). REPLACED INSERTS ON GIRT BAR PLATE FLOOR PANEL 241ABF IAW SRM 53-0
- [SDR SWAA2026072120112](https://openairdocs.org/sdr/SWAA2026072120112), Jul 14, 2026: INSERT. DAMAGED. DAMAGED INSERT LOCATED ON GIRT BAR PLATE AREA ON FLOOR PANEL 242UF AT AFT GALLEY AREA (3EA). REPLACED INSERTS ON GIRT BAR PLATE AREA ON FLOOR PANEL 242UF AT AFT
- [SDR SWAA2026072243189](https://openairdocs.org/sdr/SWAA2026072243189), Jul 2, 2026: WEB. CRACKED. CRACKED WEB, BS 500H - 500I, STR 26R IN THE FWD CARGO BAY. REPLACED WEB IAW SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-.
- [SDR SWAA2026072469644](https://openairdocs.org/sdr/SWAA2026072469644), Jun 27, 2026: WEB. CRACKED. CRACKED WEB BTWN BS 500G - 500H, STR 26R IN THE FWD CARGO BAY. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV-.
- [SDR SWAA2026072463067](https://openairdocs.org/sdr/SWAA2026072463067), Jun 27, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 232KF IN THE PASSENGER CABIN. REPAIRED FLOOR PANEL 232KF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7.
- [SDR SWAA2026072492560](https://openairdocs.org/sdr/SWAA2026072492560), Jun 27, 2026: ANGLE. CRACKED. CRACKED ANGLE BTWN BS 360 - 380, STR 27R - 28R. IN THE E & E BAY. REPLACED ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.
- [SDR SWAA2026072435186](https://openairdocs.org/sdr/SWAA2026072435186), Jun 27, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 231QF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 231QF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7, REPAIR 7.
- [SDR SWAA2026072470635](https://openairdocs.org/sdr/SWAA2026072470635), Jun 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-OG-0, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 140, R
- [SDR SWAA2026072454053](https://openairdocs.org/sdr/SWAA2026072454053), Jun 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, DWG 143A5400, SHEET 139, REV -, & DWG 143A5
- [SDR SWAA2026072454977](https://openairdocs.org/sdr/SWAA2026072454977), Jun 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE BTWN BS 380 - 400, RBL 41, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-OG-0, SRM 51-10-02, ITEM 9, AND DWG 143A5400, SHEET 140, 
- [SDR SWAA2026072421409](https://openairdocs.org/sdr/SWAA2026072421409), Jun 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, LBL 51, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-OG-0, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 140, R
- [SDR SWAA2026072446450](https://openairdocs.org/sdr/SWAA2026072446450), Jun 25, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500I, STR 28L. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 320, REV-, :
- [SDR SWAA2026072484385](https://openairdocs.org/sdr/SWAA2026072484385), Jun 25, 2026: SLIDE. WORN. WEAR ON ENTRY DOOR SCAPE SLIDE BOLTS AT AFT GALLEY AREA (2 EA). REPLACED ON ENTRY DOOR SCAPE SLIDE BOLTS AT AFT GALLEY AREA (2 EA) IAW B737-800 SOPM-20-50-01 RE
- [SDR SWAA2026072498032](https://openairdocs.org/sdr/SWAA2026072498032), Jun 25, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED REAR SPAR IFSS 177 AT LT WING. REPLACED ANGLE(BLOCK CLAMP) LOCATED REAR SPAR IFSS 177 AT LT WING IAW AMM 20-10-53-401 AND SOPM 20-50-01.
- [SDR SWAA2026072423919](https://openairdocs.org/sdr/SWAA2026072423919), Jun 25, 2026: BOLT. WORN. WEAR ON SERVICE DOOR SLIDE BOLTS. REPLACED THE SERVICE DOOR SLIDE BOLTS IAW MT 725-61-06.
- [SDR SWAA2026072479870](https://openairdocs.org/sdr/SWAA2026072479870), Jun 25, 2026: ANGLE. DAMAGED. ELONGATED HOLE ON ANGLE, REAR SPAR IFSS 185, LT WING. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & DWG 115A2510, SHEET 12, REV-.
- [SDR SWAA2026072497935](https://openairdocs.org/sdr/SWAA2026072497935), Jun 25, 2026: GLOWSTRIP. BROKEN. BROKEN PHOTOLUMINESCENT STRIP RT SIDE IN PASSENGER CABIN. REPLACED THE PHOTOLUMINESCENT STRIP RT SIDE IAW AMM-33-51-15-400-802.
- [SDR SWAA2026072425950](https://openairdocs.org/sdr/SWAA2026072425950), Jun 25, 2026: GLOWSTRIP. BROKEN. BROKEN PHOTOLUMINESCENT STRIP, LT SIDE IN THE PAX CABIN. REPLACED THE PHOTOLUMINESCENT STRIP IAW AMM-33-51-15-400-802, JOB CARD TTG8Q00EYU9C.
- [SDR SWAA2026072458815](https://openairdocs.org/sdr/SWAA2026072458815), Jun 25, 2026: WEB. CRACKED. CRACKED WEB, BTWN BS 500G - 500H, STRINGER 26L. REPLACED THE WEB IAW SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.
- [SDR SWAA2026072457579](https://openairdocs.org/sdr/SWAA2026072457579), Jun 24, 2026: FRAME. CRACKED. CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. PERFORMED TRIMMING OUT ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. I
- [SDR SWAA2026072458149](https://openairdocs.org/sdr/SWAA2026072458149), Jun 24, 2026: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW SRM 51-40-02-0G-0
- [SDR SWAA2026072403398](https://openairdocs.org/sdr/SWAA2026072403398), Jun 24, 2026: BOLT. WORN. WEAR ON FWD ENTRY DOOR ESCAPE SLIDE BOLTS AT FWD GALLEY AREA. REPLACED FWD ENTRY DOOR ESCAPE SLIDE BOLTS IAW SOPM-20-50-01, REV 40.
- [SDR SWAA2026072413423](https://openairdocs.org/sdr/SWAA2026072413423), Jun 24, 2026: PLATE. CRACKED. CRACKED SEAL PLATE FOR ACCESS PANEL 431, LT PYLON. REPLACED THE SEAL PLATE FOR ACCESS PANEL 431 IAW SRM 51-40-02-0G, AND DWG 313A2110, SHEET 24, REV -. EVALUATE
- [SDR SWAA2026072427780](https://openairdocs.org/sdr/SWAA2026072427780), Jun 23, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 500I, STR 26L. REPLACED THE TIE CLIP IAW SRM 51-40-02-0G-0, DWG 143A1234, SHEET 14, REV A, & DWG 143A1234, SHEET 46, REV -.
- [SDR SWAA2026072498431](https://openairdocs.org/sdr/SWAA2026072498431), Jun 23, 2026: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 500I AT LEVEL STR 26R AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED BS 500I AT LEVEL STR 26R AT FWD CARGO COMPA
- [SDR SWAA2026072453602](https://openairdocs.org/sdr/SWAA2026072453602), Jun 23, 2026: SEAL SEAT. CRACKED. CRACKED SEAL BLADE ON ACCESS PANEL 441AL, AT RT PYLON. REPLACED SEAL BLADE ON ACCESS PANEL 441AL IAW SRM 51-10-02-0G-0, PARAGRAPH 9, AND SRM 51-40-02-0G-0.
- [SDR SWAA2026072421175](https://openairdocs.org/sdr/SWAA2026072421175), Jun 23, 2026: WEB. CORRODED. CORROSION ON SHIELD WEB LOCATED BTW BS 492.4 - 500A, RBL 22, WL 156.1 IN THE FWD CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-40-02-0G-0, & DWG 143A0080, SHEET
- [SDR SWAA2026072402078](https://openairdocs.org/sdr/SWAA2026072402078), Jun 22, 2026: PLATE. CRACKED. CRACK CORRUGATED PLATE, ORSS 297, LT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.
- [SDR SWAA2026072477560](https://openairdocs.org/sdr/SWAA2026072477560), Jun 22, 2026: PLATE. DAMAGED. ELONGATED HOLE CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 215 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 215 AT LT WING IAW SRM 51-40-02 
- [SDR SWAA2026072492712](https://openairdocs.org/sdr/SWAA2026072492712), Jun 22, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 867 BTW STR 26L TO STR 27L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 149A8102, SHEET 19, REV A.
- [SDR SWAA2026072432896](https://openairdocs.org/sdr/SWAA2026072432896), Jun 22, 2026: FITTING. DAMAGED. ELONGATED HOLES ON FITTING ON TRAILING EDGE, ORSS 251, LT WING. REPLACED FITTING ON TRAILING EDGE AT LEVEL OFSS 251 AT LT WING IAW SRM 51-40-02.
- [SDR SWAA2026072219695](https://openairdocs.org/sdr/SWAA2026072219695), Jun 22, 2026: WEB. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BTW BS 747 TO BS 767 RBL 22 WL 156.1 AT AFT CARGO BAY. REPLACED WEB INTERCOSTAL LOCATED BS 747 - 767 RBL 22 WL 156.1 IAW SRM
- [SDR SWAA2026072409573](https://openairdocs.org/sdr/SWAA2026072409573), Jun 20, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE, ORSS 297 TRAILING EDGE RT WING. REPLACED CORRUGATED PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.
- [SDR SWAA2026072405744](https://openairdocs.org/sdr/SWAA2026072405744), Jun 20, 2026: SUPPORT BRACKET. ELONGATED. ELONGATED HOLE ON SUPPORT BRACKET LOCATED INTERNAL AREA KRUEGER FLAP 2 AT LT WING. REPLACED SUPPORT BRACKET LOCATED INTERNAL AREA KRUEGER FLAP 2 AT LT WING IAW 
- [SDR SWAA2026072419544](https://openairdocs.org/sdr/SWAA2026072419544), Jun 20, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE, ORSS 215, RT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02-0G-0, 51-10-02-0G-0, STEP 9, AND DWG 115A2781, SHEET 2, REV B.
- [SDR SWAA2026072460875](https://openairdocs.org/sdr/SWAA2026072460875), Jun 20, 2026: ANGLE. CRACKED. CRACKED ANGLE, ORSS 270 RT WING TE. REPLACED THE ANGLE IAW SRM 51-40-02 AND DWG 115A2930, SHEET 12, REV A.
- [SDR SWAA2026072471735](https://openairdocs.org/sdr/SWAA2026072471735), Jun 20, 2026: NUT PLATE. CORRODED. CORRODED RAIL NUT PLATE, OFSS 449 RT WING LE. REPLACED RAIL NUT PLATE AND FASTENERS IAW SRM 51-40-02-0G, AND DWG 112A4402, SHEET 40, REV A. CORROSION WAS NOT FO
- [SDR SWAA2026072405717](https://openairdocs.org/sdr/SWAA2026072405717), Jun 19, 2026: ANGLE. CRACKED. CRACKED ANGLE, FWD FACE BS 500G, STR 26R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, & 138, RE
- [SDR SWAA2026072422444](https://openairdocs.org/sdr/SWAA2026072422444), Jun 19, 2026: ANGLE. CRACKED. CRACKED ANGLE, LOCATED AT THE FWD FACE BS 500H, STR 26R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET
- [SDR SWAA2026072437174](https://openairdocs.org/sdr/SWAA2026072437174), Jun 19, 2026: ANGLE. CRACKED. CRACK ANGLE LOCATED AFT FACE BS 500G AT LEVEL STR 26L FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED AFT FACE BS 500G AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW 
- [SDR SWAA2026072493553](https://openairdocs.org/sdr/SWAA2026072493553), Jun 19, 2026: WEB. CRACKED. CRACKED WEB, BTWN BS 500A - 500B, STR 26R, IN THE FWD CARGO BAY. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV-.
- [SDR SWAA2026072474065](https://openairdocs.org/sdr/SWAA2026072474065), Jun 19, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26L FWD CARGO BAY, REPLACED THE ANGLE IAW SRM 51-40-02 AND DWG 143A7505, SHEET 139, REV-.
- [SDR SWAA2026072423185](https://openairdocs.org/sdr/SWAA2026072423185), Jun 19, 2026: ANGLE. CRACKED. CRACKED ANGLE, FWD FACE BS 500H, STR 26L IN FWD CARGO BAY. REPLACED THE ANGLE, LOCATED FWD FACE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.
- [SDR SWAA2026072422953](https://openairdocs.org/sdr/SWAA2026072422953), Jun 19, 2026: ANGLE. CRACKED. CRACKED ANGLE, AFT FACE BS 500H, STR 26R IN FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, AND 138, REV-
- [SDR SWAA2026072482237](https://openairdocs.org/sdr/SWAA2026072482237), Jun 19, 2026: GUSSET. CRACKED. CRACKED GUSSET ANGLE, BS 500I, STR 19R IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 256,
- [SDR SWAA2026072434343](https://openairdocs.org/sdr/SWAA2026072434343), Jun 19, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STR 25R. REPLACED ANGLE CLIP AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, & 138, REV-.

All 165: https://openairdocs.org/aircraft/N8650F/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

## 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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