# N8630B: 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: 42521
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 17, 2014
- Certificate issued: June 11, 2014
- Expires: June 30, 2027
- Mode S code: ABDC56
- 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=8630B
- Page: https://openairdocs.org/aircraft/N8630B

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 N8630B.

## FAA accident and incident reports

None matched to N8630B.

## Service difficulty reports (161, 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 SWAA2026101227160](https://openairdocs.org/sdr/SWAA2026101227160), Oct 8, 2026: COVER. LOOSE. OVERWING CEILING EXIT SIGN FELL OFF, SECURED OVERWING EXIT SIGN LENS COVERS IAW AMM 33-25-00.
- [SDR SWAA2026090918056](https://openairdocs.org/sdr/SWAA2026090918056), Sep 9, 2026: OVERHEAT SENSOR. FALSE ACTIVATION. NR 1 ENGINE OVERHEAT LIGHT CAME ON, STARTED QRH & THEN WENT OUT. PERFORMED FIM 26-10 TASK 811. NO DEFECTS FOUND AT THIS TIME. PERFORMED ENGINE FIRE DETECTION LO
- [SDR SWAA2026050695243](https://openairdocs.org/sdr/SWAA2026050695243), May 3, 2026: SIGN. DETACHED. EXIT SIGN OVER AT SEAT 15A FALLS OFF. SECURED EXIT SIGN PER MM 33-51-01.
- [SDR SWAA2026043093126](https://openairdocs.org/sdr/SWAA2026043093126), Apr 27, 2026: LIGHT. FAULTED. WALL LIGHT AT 6F IS FLASHING ON AND OFF. OK TO CONTINUE PER MEL 33-2-04; SP1B. REMOVED AND REPLACED IAW AMM 33-21-00-960-804-NG.
- [SDR SWAA2026042088598](https://openairdocs.org/sdr/SWAA2026042088598), Apr 13, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INTERIOR AND EXTERIOR DID NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACKS M2816; M1672 AND M1673 IAW AMM 33-51-06-960-805. TESTED OK.
- [SDR SWAA2026042088863](https://openairdocs.org/sdr/SWAA2026042088863), Apr 13, 2026: HANDLE. LOOSE. PAX CABIN AFT ENTRY DOOR FWD ASSISTANT HANDLE LOOSE. TIGHTENED PAX CABIN AFT ENTRY DOOR FWD ASSISTANT HANDLE IAW AMM 52-13-31-400-802, STEP 3.G.(2)(D).
- [SDR SWAA2026042088230](https://openairdocs.org/sdr/SWAA2026042088230), Mar 24, 2026: CIRCUIT BREAKER. BROKEN. BROKEN CIRCUIT BREAKER POSITION A9 AT P6-11 PANEL. REMOVED AND REPLACED CIRCUIT BREAKER ON P6-11 POSITION A9 IAW WDM 33-51-11-11 AND PERFORMED OPS TEST EMERGENC
- [SDR SWAA2026042080408](https://openairdocs.org/sdr/SWAA2026042080408), Mar 16, 2026: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED STA 360 AND BTW STR 27R TO STR 28R AT EQUIPMENT ELECTRONIC COMP. REPLACED SUPPORT ANGLE LOCATED BS 360 AND BTW STR 27R AND 28R AT EQ
- [SDR SWAA2026042091121](https://openairdocs.org/sdr/SWAA2026042091121), Mar 14, 2026: FRAME. CRACKED. CRACK FRAME LOCATED BS 312 BTW STR5L TO STR6L AT PASSENGER CABIN 2026-181127<[01] PERFORMED TRIMMING OUT ON FRAME BS 312 BTW STRINGER 5L & 6L AT PASSENGER CABIN
- [SDR SWAA2026042079742](https://openairdocs.org/sdr/SWAA2026042079742), Mar 14, 2026: FRAME. CRACKED. CRACK FRAME LOCATED BS 312 BTW STR5L TO STR6L AT PASSENGER CABIN. PERFORMED TRIMMING OUT ON FRAME BS 312 BTW STRINGER 5L & 6L AT PASSENGER CABIN. IAW EA M-22-15
- [SDR SWAA2026042079743](https://openairdocs.org/sdr/SWAA2026042079743), Mar 14, 2026: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS 277 STR10R AT PASSENGER CABIN . REPLACED TIE CLIP LOCATED BS277 STR10R AT PASSENGER CABIN IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-
- [SDR SWAA2026041679640](https://openairdocs.org/sdr/SWAA2026041679640), Mar 13, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 241KF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241KF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7.
- [SDR SWAA2026042079326](https://openairdocs.org/sdr/SWAA2026042079326), Mar 12, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 947.5, S-26L. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02, AND SRM-51-10-02-0G-0, ITEM 9, DWG 149A8103, SHEET 8, REV -.
- [SDR SWAA2026042091106](https://openairdocs.org/sdr/SWAA2026042091106), Mar 12, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 947.5, S-26L, REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02, AND SRM-51-10-02-0G-0, ITEM 9, DWG 149A8103, SHEET 8, REV -.
- [SDR SWAA2026041779080](https://openairdocs.org/sdr/SWAA2026041779080), Mar 12, 2026: NUT PLATE. CRACKED. CRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 334 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 334 AT LT WIN
- [SDR SWAA2026041679327](https://openairdocs.org/sdr/SWAA2026041679327), Mar 12, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 232SF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 232SF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7.
- [SDR SWAA2026042078740](https://openairdocs.org/sdr/SWAA2026042078740), Mar 11, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 663, RBL 31. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 111A1000; SHEET 330; REV A; DWG# 111A1000; SHEET 331, REV A & DWG 111A1322; SHE
- [SDR SWAA2026042078739](https://openairdocs.org/sdr/SWAA2026042078739), Mar 11, 2026: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS 540 AT LEVEL LBL 6 AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AIR CONDITIONING BAY I.A.W B737-
- [SDR SWAA2026042078741](https://openairdocs.org/sdr/SWAA2026042078741), Mar 11, 2026: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS 540 AT LEVEL RBL 6 AIR CONDITIONING BAYS. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS540 AT LEVEL RBL 6 AIR CONDITIONING 
- [SDR SWAA2026041778585](https://openairdocs.org/sdr/SWAA2026041778585), Mar 11, 2026: LENS. BROKEN. BROKEN EMERGENCY LIGHT LENS. REPLACED THE LENSES (2EA) IAW AMM 33-51-03-960-803, STEP 4.D. (1) THRU 4.D.(2).
- [SDR SWAA2026042078339](https://openairdocs.org/sdr/SWAA2026042078339), Mar 10, 2026: WEB. CRACKED. CRACKED FLOOR WEB BTW BS 270 TO BS 294.5 AT BL 0. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02 AND DWG 141A5400, SHEET 20, REV-.
- [SDR SWAA2026042091109](https://openairdocs.org/sdr/SWAA2026042091109), Mar 10, 2026: WEB. CRACKED. CRACKED FLOOR WEB BTW BS 270 TO BS 294.5 AT BL 0. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02 AND DWG 141A5400, SHEET 20, REV-.
- [SDR SWAA2026042078340](https://openairdocs.org/sdr/SWAA2026042078340), Mar 10, 2026: WEB. CRACKED. CRACKED FLOOR WEB BTW BS 312 TO BS 328 AT LBL 46. REPLACED FLOOR WEB BTW BS 312 TO BS 328 AT LBL 46 AT FWD GALLEY AREA IAW SRM 51-40-02 AND DWG 141A5400 SHEET 3
- [SDR SWAA2026042078581](https://openairdocs.org/sdr/SWAA2026042078581), Mar 10, 2026: ACCESS PANEL. CRACKED. CRACK SEAL BLADE ASSY ACCESS PANEL 333AB AT LT HORIZONTAL STAB. REPLACED SEAL BLADE ASSY ACCESS PANEL 333AB AT LT HORIZONTAL; IAW SRM-51-20-01-0G-0; CRACK LENGT
- [SDR SWAA2026041778580](https://openairdocs.org/sdr/SWAA2026041778580), Mar 10, 2026: LENS. MISSING. SIDEWALL PANEL 242ZAW EMERGENCY COVER LENS OVER WING HATCH MISSING. INSTALLED LENS IAW AMM 33-51-01-960-801, STEP 2, C, (1), (A), AND 2, C, (4).
- [SDR SWAA2026041678337](https://openairdocs.org/sdr/SWAA2026041678337), Mar 10, 2026: FLOOR SUPPORT. CORRODED. CORROSION FLOOR SUPPORT BTW BS 328 TO BS 344 AT LBL 22 AND WL 208.1 AT FWD GALLEY AREA. REPLACED FLOOR SUPPORT IAW SRM 51-10-02 ITEM 9 AND DWG 141A5730, SHEET 3
- [SDR SWAA2026042078168](https://openairdocs.org/sdr/SWAA2026042078168), Mar 9, 2026: ACCESS PANEL. MISSING. MISSING PANEL 832CZ ON EMERGENCY EXIT DOOR LINING PANEL. INSTALLED PANEL 832CZ ON EMERGENCY EXIT DOOR LINING PANEL IAW BOEING SOPM 20-50-12 REV 58.
- [SDR SWAA2026042078161](https://openairdocs.org/sdr/SWAA2026042078161), Mar 9, 2026: WEB. CORRODED. CORROSION BILGE AREA SHIELD WEB BTW BS 480 PLUS 12 INCHES AND BS 500A AT LEVEL STR 26R AND WL 156. REPLACED SHIELD WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, A
- [SDR SWAA2026042078163](https://openairdocs.org/sdr/SWAA2026042078163), Mar 9, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500F AFT FACE, STR 26R IN THE FWD CARGO COMPARTMENT. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV -.
- [SDR SWAA2026042078166](https://openairdocs.org/sdr/SWAA2026042078166), Mar 9, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G FWD FACE, STR 26R AT FWD CARGO COMPARTMENT. ANGLE WAS REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM 53-00-53-1A-2.
- [SDR SWAA2026042091110](https://openairdocs.org/sdr/SWAA2026042091110), Mar 9, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G FWD FACE, STR 26R AT FWD CARGO COMPARTMENT. THE ANGLE IS REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM 53-00-53-1A-2.
- [SDR SWAA2026042091111](https://openairdocs.org/sdr/SWAA2026042091111), Mar 9, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500F AFT FACE, STR 26R AT FWD CARGO COMPARTMENT. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 143A7505, SHEET 137, REV -.
- [SDR SWAA2026041778162](https://openairdocs.org/sdr/SWAA2026041778162), Mar 9, 2026: ANGLE. CRACKED. CRACKED ANGLE ON BS 500H, STR 26R AFT FACE. FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 143A7505, SHEET 137, REV -.
- [SDR SWAA2026041678157](https://openairdocs.org/sdr/SWAA2026041678157), Mar 9, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE BTWN BS 500A + 10 - BS 500F + 9 INCHES, STR 26L, WL 156. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550.
- [SDR SWAA2026041678160](https://openairdocs.org/sdr/SWAA2026041678160), Mar 9, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE BTWN BS 500D + 12 & BS 500I, STR 26R, WL 156. REPLACED SUPPORT ZEE; TAPER FILLERS (2E/A) AND FASTENERS IAW SRM 51-40-02, DWG 143A7500 SHEET
- [SDR SWAA2026041678159](https://openairdocs.org/sdr/SWAA2026041678159), Mar 9, 2026: SUPPORT. CORRODED. CORROSION SUPPORT ZEE BTWN BS 500A & BS 500D + 12, STR 26R, WL 156. REFER TO FAULT TTG8Q01AW516, THE SUPPORT ZEE WAS REPLACED.
- [SDR SWAA2026041678158](https://openairdocs.org/sdr/SWAA2026041678158), Mar 9, 2026: SUPPORT. CORRODED. CORROSION SUPPORT ZEE BTW BS 500F PLUS 9 INCHES AND BTW BS 500I AT LEVEL STR 26L AND WL 156 AT FWD CARGO BAY. (6 EA). REFER TO FAULT TTG8Q01AW4T5 SUPPORT ZEE WA
- [SDR SWAA2026042077663](https://openairdocs.org/sdr/SWAA2026042077663), Mar 8, 2026: FLOOR SUPPORT. CORRODED. CORROSION FLOOR SUPPORT BTW BS 947 TO BS 967 AT LBL 51 AND WL 208.1. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 147A5650, SHEET 55, REV A.
- [SDR SWAA2026042077664](https://openairdocs.org/sdr/SWAA2026042077664), Mar 8, 2026: FLOOR SUPPORT. CORRODED. CORROSION FLOOR SUPPORT BTW BS 947 TO BS 967, RBL 51, WL 208.1. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A5650, SHEET 71, REV A
- [SDR SWAA2026042077662](https://openairdocs.org/sdr/SWAA2026042077662), Mar 8, 2026: ANGLE. CRACKED. CRACKED ANGLE, TRAILING EDGE, ORSS 270, RT WING REPLACED THE ANGLE DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS FOR CRACK ON SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1. L
- [SDR SWAA2026041677665](https://openairdocs.org/sdr/SWAA2026041677665), Mar 8, 2026: FLOORBEAM. CORRODED. CORRODED FLOORBEAM, BS 986, RBL 44, WL 208.1. PERFORMED A PERMANENT REPAIR TO THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
- [SDR SWAA2026042077548](https://openairdocs.org/sdr/SWAA2026042077548), Mar 7, 2026: HANDLE. DETERIORATED. DETERIORATED ASSIST HANDLE AND NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA. REPLACED ASSIST HANDLE AND NUT ON FORWARD ENTRY DOOR LINING AT FORWARD G
- [SDR SWAA2026042091105](https://openairdocs.org/sdr/SWAA2026042091105), Mar 7, 2026: NUT. DETERIORATED. DETERIORATED ASSIST HANDLE AND NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (1 EA) 2026-180950<[01] REPLACED ASSIST HANDLE AND NUT ON FORWARD ENTRY D
- [SDR SWAA2026042076912](https://openairdocs.org/sdr/SWAA2026042076912), Mar 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS T500H, STR 26L. REPLACED ANGLE-CLIP AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -.
- [SDR SWAA2026042076904](https://openairdocs.org/sdr/SWAA2026042076904), Mar 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 143A7505, SHEET 138, REV -.
- [SDR SWAA2026042076913](https://openairdocs.org/sdr/SWAA2026042076913), Mar 5, 2026: SUPPORT ANGLE. CRACKED. CRACKED ANGLE, BS 400, STR 26L. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV -.
- [SDR SWAA2026042076902](https://openairdocs.org/sdr/SWAA2026042076902), Mar 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26R FWD CARGO COMPARTMENT. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 143A7505, SHEET 137, REV -.
- [SDR SWAA2026042091112](https://openairdocs.org/sdr/SWAA2026042091112), Mar 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR26R FWD CARGO COMPARTMENT. THE ANGLE WAS REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM 53-00-53-1A-2. CRACK LENGTH IS:0.86
- [SDR SWAA2026041777111](https://openairdocs.org/sdr/SWAA2026041777111), Mar 5, 2026: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN IAW AMM 33-51-15-960-801.
- [SDR SWAA2026041776911](https://openairdocs.org/sdr/SWAA2026041776911), Mar 5, 2026: GUSSET. CRACKED. CRACK GUSSET ANGLE LOCATED BS 500I, STR 19R AT FWD CARGO BAY. REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 I

All 161: https://openairdocs.org/aircraft/N8630B/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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