# N8623F: 2013 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: 36731
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 19, 2013
- Certificate issued: January 30, 2014
- Expires: January 31, 2030
- Mode S code: ABD90C
- 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=8623F
- Page: https://openairdocs.org/aircraft/N8623F

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 N8623F.

## NTSB investigations on N8623F not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA79FA125](https://openairdocs.org/ntsb/MIA79FA125), Sep 19, 1979: Hughes 369HS (N8623F), Jacksonville, FL, destroyed, 1 fatal

## FAA accident and incident reports

None matched to N8623F.

## Reports on N8623F not matched to an aircraft (1)

They name N8623F, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 19790919036649A](https://openairdocs.org/incident/19790919036649A), Sep 19, 1979: Hughes 369HS (N8623F), Duval, FL, Destroyed. Helicopter observed to rock during hover, then spin into ground. Possible pilot incapacitation.

## Service difficulty reports (194, 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 SWAA2026082442664](https://openairdocs.org/sdr/SWAA2026082442664), Aug 20, 2026: COVER. MISSING. AFTER WINDSCREEN EMERGENCY EXIT SIGN LIGHT COVER MISSING CAPTAINS SIDE. CAPTAIN HELD OFF BOARDING. R & R AFT EMER LIGHT COVER IAW AMM 33-51-01.
- [SDR SWAA2026081046552](https://openairdocs.org/sdr/SWAA2026081046552), Aug 6, 2026: RIVET. MISSING. FA REPORTED FWD GALLEY DOOR GIRT BAR DIFFICULT TO LATCH ONTO DOOR. FOUND AFT GIRT BAR RETAINING BRACKET ON SLIDE BUSTLE RIVET MISSING. SECURED RETAINING BRACKET
- [SDR SWAA2026071559853](https://openairdocs.org/sdr/SWAA2026071559853), Jul 11, 2026: LENS. MISSING. CABIN FWD EMERGENCY LIGHT COVER MISSING. INSTALLED NEW LENS COVER IAW AMM 33-51-03.
- [SDR SWAA2026061110084](https://openairdocs.org/sdr/SWAA2026061110084), Jun 7, 2026: MEGAPHONE. INOPERATIVE. MEGAPHONE IS INOPERATIVE. R & R MEGAPHONE. OPS CHECK GOOD AT THIS TIME. R & R THE MEGAPHONE. OPS CHECK GOOD IAW AMM 25-64-00.
- [SDR SWAA2026033083815](https://openairdocs.org/sdr/SWAA2026033083815), Mar 27, 2026: LENS. MISSING. LT. FWD OVERWING EMERGENCY EXIT LOWER LIGHTED EXIT SIGN MISSING LENS.<[01] INSTALLED LOWER LIGHTED EXIT SIGN LENS ON LT. FWD EMERGENCY EXIT IAW AMM 33-51-01.
- [SDR SWAA2026032079473](https://openairdocs.org/sdr/SWAA2026032079473), Mar 13, 2026: FLOOR PANEL. CRACKED. FLOOR PANEL 221GF CRACKED AT FWD LT CORNER. REPAIRED FLOOR PANEL 221GF CRACKED AT FWD L/H CORNER IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026012062751](https://openairdocs.org/sdr/SWAA2026012062751), Jan 19, 2026: COVER. DISLODGED. AFT LT ESCAPE SLIDE COVER DISPLACED. SECURED AFT LT SLIDE COVER IAW AMM 25-66-01. AC OK FOR SERVICE.
- [SDR SWAA2026010658252](https://openairdocs.org/sdr/SWAA2026010658252), Jan 4, 2026: SLIDE. UNPACKED. ESCAPE SLIDE FWD SERVICE DOOR NEEDS REPACKING. PERFORMED INSPECTION OF FWD GALLEY SERVICE DOOR ESCAPE SLIDE PER AMM 25-66-01. FOUND NO DEFECTS. OK FOR SERVICE.
- [SDR SWAA2025112029146](https://openairdocs.org/sdr/SWAA2025112029146), Oct 28, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500I, STR 28R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7902, SHEET 301, REV A.
- [SDR SWAA2025112029147](https://openairdocs.org/sdr/SWAA2025112029147), Oct 28, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 500I & STR 28L AT FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02 AND DWG 143A7902, SHEET 301, REV A.
- [SDR SWAA2025112829141](https://openairdocs.org/sdr/SWAA2025112829141), Oct 27, 2025: RIB. CRACKED. CRACK RIB LOCATED LE STA 123.85 ACCESS PANEL 341B AT RT HORIZONTAL STAB. REPLACED RIB LOCATED LE STA 123.85 ACCESS PANEL 341B AT RT HORIZONTAL STAB IAW SRM 51-1
- [SDR SWAA2025112029148](https://openairdocs.org/sdr/SWAA2025112029148), Oct 27, 2025: ANGLE. CRACKED. CRACKED ANGLE ON ACCESS PANEL 844DZ RT SIDE AFT GALLEY DOOR. REPLACED THE ANGLE IAW SRM 51-40-02, AND 51-10-02, ITEM 9.
- [SDR SWAA2025112029145](https://openairdocs.org/sdr/SWAA2025112029145), Oct 27, 2025: ANGLE. CRACKED. CRACK ON ANGLE ON ACCESS PANEL 844DZ, LT SIDE, GALLEY DOOR. REPLACED ANGLE IAW SRM 51-40-02, AND 51-10-02, ITEM 9.
- [SDR SWAA2025112029143](https://openairdocs.org/sdr/SWAA2025112029143), Oct 27, 2025: SUPPORT BEAM. CRACKED. CRACK SUPPORT BEAM NR 4 LOCATED FWD GALLEY SERVICE DOOR. REPLACED BEAM 4 LOCATED FWD GALLEY SERVICE DOOR AT PASSENGER CABIN IAW SRM 51-40-02 SRM 51-10-02 ITEM 9
- [SDR SWAA2025112032981](https://openairdocs.org/sdr/SWAA2025112032981), Oct 27, 2025: BALANCE ARM. OUT OF TOLERANCE. DURING WEIGHT AND BALANCE PROCEDURE OF RT ELEVATOR FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BA
- [SDR SWAA2025112032980](https://openairdocs.org/sdr/SWAA2025112032980), Oct 27, 2025: BALANCE ARM. OUT OF TOLERANCE. DURING WEIGHT AND BALANCE PROCEDURE OF LT ELEVATOR FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BA
- [SDR SWAA2025112029022](https://openairdocs.org/sdr/SWAA2025112029022), Oct 27, 2025: RIB. CRACKED. CRACK RIB LOCATED LE HSS 105.26 LT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, SHEET 19, REV-, DUE TO NO ALLOWABLE D
- [SDR SWAA2025112028839](https://openairdocs.org/sdr/SWAA2025112028839), Oct 26, 2025: FLOORBEAM. CRACKED. CRACK ON THE FLOORBEAM, BS 540 BTW BL 0 TO RBL 24.75, WL 208.1. REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 143A0060, SHEET 6
- [SDR SWAA2025112828448](https://openairdocs.org/sdr/SWAA2025112828448), Oct 25, 2025: BRACKET. CRACKED. CRACK ON BRACKET TRAILING EDGE LOCATED ORSS273 AT RT WING. REPLACED THE BRACKET TRAILING EDGE LOCATED ORSS273 AT RT WING IAW SRM 51-10-02-0G; SRM 51-40-02-0G-0 
- [SDR SWAA2025112628445](https://openairdocs.org/sdr/SWAA2025112628445), Oct 25, 2025: SUPPORT. CORRODED. CORROSION ON SUPPORT ZEE LOCATED BTW BS 500E TO BS 500I LBL 22 WL 156.1AT FWD CARGO COMPARTMENT, 12 POINTS. FAULT RESOLVED ON FAULT TTG8Q016272L.
- [SDR SWAA2025112628455](https://openairdocs.org/sdr/SWAA2025112628455), Oct 25, 2025: SUPPORT. CORRODED. CORROSION ON SUPPORT ZEE LOCATED BTW BS 500 TO BS 500E LBL 22 WL 156.1, AT FWD CARGO COMPARTMENT,12 POINTS. THE DAMAGE WAS REPAIRED IAW SRM 53-00-53-2R-5 AND EA
- [SDR SWAA2025112028452](https://openairdocs.org/sdr/SWAA2025112028452), Oct 25, 2025: WEB. CORRODED. CORROSION ON SHIELD WEB, BTW BS 492.4 - 500A, RBL 23, WL 208.1. REPLACED SHIELD WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A0080, SHEET 39, REV-.
- [SDR SWAA2025112028454](https://openairdocs.org/sdr/SWAA2025112028454), Oct 25, 2025: SUPPORT. CORRODED. CORROSION ON SUPPORT ZEE, BTW BS 500E - 500I, RBL 22, WL 156.1. FWD CARGO COMPARTMENT. FAULT RESOLVED ON FAULT TTG8Q0161PAR.
- [SDR SWAA2025112028446](https://openairdocs.org/sdr/SWAA2025112028446), Oct 25, 2025: SUPPORT. CORRODED. CORROSION ON SUPPORT ZEE, BTW BS 500A - 500E, RBL 22, WL 156.1. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR5) AND EA M-22-153 -01550.
- [SDR SWAA2025112028453](https://openairdocs.org/sdr/SWAA2025112028453), Oct 25, 2025: TIE CLIP. CRACKED. CRACK ON TIE CLIP, BS 500I, STRINGER 26R, WL 156.1. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A1234, SHEET 13, REV A.
- [SDR SWAA2025112028579](https://openairdocs.org/sdr/SWAA2025112028579), Oct 25, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE BTW BS 380 TO BS 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 138, REV
- [SDR SWAA2025112028578](https://openairdocs.org/sdr/SWAA2025112028578), Oct 25, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 142,
- [SDR SWAA2025112028576](https://openairdocs.org/sdr/SWAA2025112028576), Oct 25, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 49 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 1
- [SDR SWAA2025112028577](https://openairdocs.org/sdr/SWAA2025112028577), Oct 25, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHEET 154, REV -, M
- [SDR SWAA2025112028573](https://openairdocs.org/sdr/SWAA2025112028573), Oct 25, 2025: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 867, BTW STR 2R TO STR 3R. REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND 
- [SDR SWAA2025112028574](https://openairdocs.org/sdr/SWAA2025112028574), Oct 25, 2025: FRAME. CRACKED. CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR FRAME IAW EA M-22-153-01244.
- [SDR SWAA2025112028190](https://openairdocs.org/sdr/SWAA2025112028190), Oct 24, 2025: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BTW BS 500A - 500B, STRINGER 26R. REPLACED THE WEB - INTERCOSTAL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV -.
- [SDR SWAA2025112028195](https://openairdocs.org/sdr/SWAA2025112028195), Oct 24, 2025: NUT. DETERIORATED. DETERIORATED CAM NUT ON AFT GALLEY SERVICE DOOR HANDLE. REPLACED CAM NUT IAW AMM 52-41-11-400-801, STEP 3.F (5), ITEM (I) THRU 3.F (5), ITEM (N).
- [SDR SWAA2025112028188](https://openairdocs.org/sdr/SWAA2025112028188), Oct 24, 2025: ANGLE. CRACKED. CRACK ON ANGLE AFT FACE BS 500H, STRINGER 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-. MEASUREMENT OF CRAC
- [SDR SWAA2025112028189](https://openairdocs.org/sdr/SWAA2025112028189), Oct 24, 2025: ANGLE. CRACKED. CRACK ON ANGLE CLIP FWD FACE, BS 500H, STRINGER 26R. REPLACED THE ANGLE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505 SHEET 139, REV-. MEASUREME
- [SDR SWAA2025112028193](https://openairdocs.org/sdr/SWAA2025112028193), Oct 24, 2025: ANGLE. CRACKED. CRACK ON ANGLE CLIP AFT FACE, BS 400 STRINGER 26L. MEASUREMENT OF CRACK IS L: 0.530 INCHES. REPLACED THE ANGLE CLIP IAW SRM 51-40-02-0G, SRM 51-10-02-0G, PARAGR
- [SDR SWAA2025112028194](https://openairdocs.org/sdr/SWAA2025112028194), Oct 24, 2025: ANGLE. CRACKED. CRACK ON ANGLE CLIP FWD FACE, BS 500H, STRINGER 26L. REPLACED THE ANGLE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-. MEASUREM
- [SDR SWAA2025112028191](https://openairdocs.org/sdr/SWAA2025112028191), Oct 24, 2025: ANGLE. CRACKED. CRACK GUSSET ANGLE, BS 500I, STRINGER 21L. REPLACED THE GUSSET ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7902, SHEET 256, REV B. REJ
- [SDR SWAA2025112028187](https://openairdocs.org/sdr/SWAA2025112028187), Oct 24, 2025: ANGLE. CRACKED. CRACKED GUSSET ANGLE, BS 500I, STRINGER 19R IN THE FWD CARGO BAY. MEASUREMENT OF THE CRACK IS L: 0.9235 INCHES. . REPLACED GUSSET ANGLE IAW SRM 51-10-02, ITEM 9
- [SDR SWAA2025112028192](https://openairdocs.org/sdr/SWAA2025112028192), Oct 24, 2025: ANGLE. CRACKED. CRACK ON THE ANGLE LOCATED AFT FACE BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEP 9, SRM 51-40-02, AND DWG 143A7505, SHE
- [SDR SWAA2025112028186](https://openairdocs.org/sdr/SWAA2025112028186), Oct 24, 2025: ACCESS PANEL. CRACKED. CRACKED SEAL - BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER. REPLACED BLADE LOCATED ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW SRM 51-40-02.
- [SDR SWAA2025112027629](https://openairdocs.org/sdr/SWAA2025112027629), Oct 23, 2025: WEB. CORRODED. CORROSION WEB - INTERCOSTAL BTW BS 747 - 767, STR 25R, WL 156.4. REPLACED THE WEB - INTERCOSTAL IAW 51-40-02, AND DWG 146A7502, SHEET 50, REV-.
- [SDR SWAA2025112027440](https://openairdocs.org/sdr/SWAA2025112027440), Oct 23, 2025: WEB. CRACKED. CRACK ON WEB BTW BS 927 TO BS 947.5, STRINGER 25R. REPLACED THE WEB IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G, AND DWG 147A7500, SHEET 20, REV -.
- [SDR SWAA2025112027447](https://openairdocs.org/sdr/SWAA2025112027447), Oct 23, 2025: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE, BTW BS 767 - 792, RBL 21, WL 156.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A8123, SHEET 16, R
- [SDR SWAA2025112027446](https://openairdocs.org/sdr/SWAA2025112027446), Oct 23, 2025: WEB. CORRODED. CORROSION ON THE SHIELD WEB BS 767 - 792, RBL 21, WL 156.1. REPLACED THE SHIELD WEB IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 146A0081, SHEET 49, REV A.
- [SDR SWAA2025112027178](https://openairdocs.org/sdr/SWAA2025112027178), Oct 23, 2025: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTINGS HARDWARE AND SHIMS ENTRY AND SERVICE DOOR. REPLACED GIRT BAR FITTINGS HARDWARE AND SHIMS ENTRY AND SERVICE DOOR AT AFT GALLEY ARE
- [SDR SWAA2025112027177](https://openairdocs.org/sdr/SWAA2025112027177), Oct 23, 2025: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTING HARDWARE AND SHIMS FWD ENTRY AND SERVICE DOOR. REPLACED GIRT BAR FITTING HARDWARE AND SHIMS. INSTALLATION WILL BE ACCOMPLISHED ON 
- [SDR SWAA2025112027438](https://openairdocs.org/sdr/SWAA2025112027438), Oct 23, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BS 867, STRINGER 26L, WL 156.1. REPLACED THE ANGLE IAW SRM 51-10-02-0G, SRM 51-40-02-0G-0, AND DWG 149A8102, SHEET 19, REV A. MEASURE OF 
- [SDR SWAA2025112027638](https://openairdocs.org/sdr/SWAA2025112027638), Oct 23, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE, BTW BS 727F - 767, STRINGER 25R, WL 156.4. REPLACED SUPPORT ZEE IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, SRM 53-00-53-2R-6, REPAIR 6
- [SDR SWAA2025112027172](https://openairdocs.org/sdr/SWAA2025112027172), Oct 23, 2025: SCUFF PLATE. CRACKED. CRACK ON FWD CORNER OF SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.

All 194: https://openairdocs.org/aircraft/N8623F/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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