# N8628A: 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: 42384 - Year built: 2014 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 24, 2014 - Certificate issued: May 19, 2014 - Expires: May 31, 2027 - Mode S code: ABD9B6 - 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=8628A - Page: https://openairdocs.org/aircraft/N8628A 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 N8628A. ## FAA accident and incident reports None matched to N8628A. ## Service difficulty reports (168, 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 SWAA2026090815076](https://openairdocs.org/sdr/SWAA2026090815076), Sep 4, 2026: LIGHT. BROKEN. CABIN AISLE EMERGENCY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT HOUSING IAW AMM 33-51-01, OPS CHKD GOOD. - [SDR SWAA2026041487311](https://openairdocs.org/sdr/SWAA2026041487311), Apr 7, 2026: BATTERY PACK. INOPERATIVE. TROUBLESHOOT VARIOUS EMERGENCY LIGHTS INOPERATIVE THROUGHOUT CABIN. REMOVED AND REPLACED THREE BATTERY PACKS, OPS CHECKED GOOD IAW AMM 33-51-06-960-805. - [SDR SWAA2026041386161](https://openairdocs.org/sdr/SWAA2026041386161), Apr 3, 2026: FITTING. LOOSE. L1 DOOR FWD GIRT BAR FITTING NOT SECURED. SECURED L1 DOOR FWD GIRT BAR FITTING IAW BOEING AMM 25-66-02-400-801TO: T8929K. VERIFIED SECURED L1 DOOR FWD GIRT BAR - [SDR SWAA2026030976279](https://openairdocs.org/sdr/SWAA2026030976279), Mar 3, 2026: SEAT. OUT OF ADJUST. PAX CABIN AT SEAT ROW 14D MUST BE NOT RECLINE. PERFORMED ADJUSTMENT ON HYDRAULIC LOCK STROKE ON SEAT ROW 14D AT PAX CABIN IAW CMM 25-22-46-3500, REV 9. FITS AND - [SDR SWAA2026030968411](https://openairdocs.org/sdr/SWAA2026030968411), Feb 6, 2026: STRAP. CORRODED. CORRODED STRAP, BS 807 - 827, RBL 20, WL 156. REPLACED THE STRAP IAW SRM 51-10-02, ITEM 9, & DWG 149A0081, SHEET 49, REV A. - [SDR SWAA2026030968412](https://openairdocs.org/sdr/SWAA2026030968412), Feb 6, 2026: WEB. CORRODED. CORRODED SHIELD WEB CUTOUT STRUCTURE, BS 767 - 794, RBL 21, WL 156. REPLACED THE SHIELD WEB IAW SRM 51-10-02 ITEM 9, & DWG 146A0081, SHEET 49, REV A. - [SDR SWAA2026030968415](https://openairdocs.org/sdr/SWAA2026030968415), Feb 6, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 867, S26 - 27L. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 149A8102, SHEET 19, REV A. - [SDR SWAA2026030968011](https://openairdocs.org/sdr/SWAA2026030968011), Feb 5, 2026: DOOR FRAME. CRACKED. CRACKED DOOR FRAME, BS 312, STR 5L - STR 6L. PERFORMED A REPAIR ON THE DOOR FRAME IAW EA NM-22-153-01244, REV B. - [SDR SWAA2026030968012](https://openairdocs.org/sdr/SWAA2026030968012), Feb 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500I, LBL 7. REPLACED THE ANGLE IAW SRM 51-40-02-0G, & DWG 143A7902, SHEET 320, REV -. - [SDR SWAA2026030968013](https://openairdocs.org/sdr/SWAA2026030968013), Feb 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, DOOR CUT OUT, BS 309, STR 8L. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 141A8220, SHEET 21, REV A. - [SDR SWAA2026030968014](https://openairdocs.org/sdr/SWAA2026030968014), Feb 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500I, RBL 7. REPLACED THE ANGLE IAW SRM 51-40-02-0G, & DRAWING 143A7902, SHEET 320, REV -. - [SDR SWAA2026030968010](https://openairdocs.org/sdr/SWAA2026030968010), Feb 5, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE, BS 360 SUPPORT STRUCTURE OF OXYGEN BOTTLE. REPLACED SUPPORT ANGLE LOCATED ON BS 360 SUPPORT STRUCTURE OF OXYGEN BOTTLE IAW SRM 51-40-01 - [SDR SWAA2026030967382](https://openairdocs.org/sdr/SWAA2026030967382), Feb 3, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BS 500 - 500E, LBL 22, WL 156. THE DAMAGE WAS REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EA M-22-153-01550. - [SDR SWAA2026030967251](https://openairdocs.org/sdr/SWAA2026030967251), Feb 3, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BS 500E - 500I, LBL22, WL 156. 6. REPAIRED THE SUPPORT ZEE IAW SRM 53-00-53-2R-5. - [SDR SWAA2026030967241](https://openairdocs.org/sdr/SWAA2026030967241), Feb 3, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 380 - 400, RBL 10. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G, & DWG 143A5400, SHEET 182, REV-. - [SDR SWAA2026030967245](https://openairdocs.org/sdr/SWAA2026030967245), Feb 3, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 137, REV-. - [SDR SWAA2026030967246](https://openairdocs.org/sdr/SWAA2026030967246), Feb 3, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500F, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2026030967247](https://openairdocs.org/sdr/SWAA2026030967247), Feb 3, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, & DRAWING 143A7505, SHEET 137, REV -. - [SDR SWAA2026030967248](https://openairdocs.org/sdr/SWAA2026030967248), Feb 3, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STR 26RL REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2026030967379](https://openairdocs.org/sdr/SWAA2026030967379), Feb 3, 2026: ANGLE. CRACKED. CRACKED ANGLE BS 500A, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2026030967244](https://openairdocs.org/sdr/SWAA2026030967244), Feb 3, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, S26L, REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2026030967381](https://openairdocs.org/sdr/SWAA2026030967381), Feb 3, 2026: ANGLE. CRACKED. CRACK GUSSET ANGLE, BS 500I, STR 21L. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02-0G, AND DWG 143A7902. SHEET 256, REV B. - [SDR SWAA2026030967385](https://openairdocs.org/sdr/SWAA2026030967385), Feb 3, 2026: ANGLE. CRACKED. CRACKED GUSSET ANGLE, BS 500I, STR 19R. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02, & DWG 143A7902, SHEET 256, REV B. - [SDR SWAA2026030967384](https://openairdocs.org/sdr/SWAA2026030967384), Feb 3, 2026: ANGLE. CRACKED. CRACKED ANGLE TRAILING EDGE MLG BAY AT LT WING. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A2510, SHEET 12, REV-. - [SDR SWAA2026030967242](https://openairdocs.org/sdr/SWAA2026030967242), Feb 3, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE LOCATED BETWEEN BS380 - 400, LBL 13. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G AND DRAWING 143A5400, SHEET 182, REV -. - [SDR SWAA2026030967243](https://openairdocs.org/sdr/SWAA2026030967243), Feb 3, 2026: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BETWEEN BS 380 - 400 AND LBL52. REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 380 - 400 AND LBL52 IAW SRM 51-40-02-0G, AND DRAWING 143A5 - [SDR SWAA2026030667252](https://openairdocs.org/sdr/SWAA2026030667252), Feb 3, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 231PF AT PASSENGER CABIN 2026-93281<[01] TOOL USED: CALIPER P/N: 500-752-20. S/N: B21038258; DUE DATE: 06-NOV-26.;[02] TOOL USED: HOT BO - [SDR SWAA2026030667383](https://openairdocs.org/sdr/SWAA2026030667383), Feb 3, 2026: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS500A TO BS500E; RBL22 AND WL156 AT FWD CARGO COMPARTMENT 2026-93282<[01] TOOL USED ON Ï¿½TEM 4: EDDY CURRENT FLAW DETECT - [SDR SWAA2026030667249](https://openairdocs.org/sdr/SWAA2026030667249), Feb 3, 2026: TIE CLIP. CRACKED. CRACK ON TIE CLIP FLOOR STRUCTURE LOCATED BETWEEN BS500I AND STR26R AT FWD CARGO COMPARTMENT 2026-93269<[01] REPLACED TIE CLIP FLOOR STRUCTURE LOCATED BETWEEN B - [SDR SWAA2026030667250](https://openairdocs.org/sdr/SWAA2026030667250), Feb 3, 2026: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS500E TO BS500I; RBL22 AND WL156 AT FWD CARGO COMPARTMENT 2026-93268<[01] TOOL USED ON Ï¿½TEM 4: EDDY CURRENT FLAW DETECT - [SDR SWAA2026030667380](https://openairdocs.org/sdr/SWAA2026030667380), Feb 3, 2026: WEB. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500A TO BS500B AND STR26R FWD CARGO COMPARTMENT 2026-93285<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWE - [SDR SWAA2026030667253](https://openairdocs.org/sdr/SWAA2026030667253), Feb 3, 2026: LANYARD. WORN. WORN EMERGENCY EXIT HATCH LIFE LINE RH SIDE AT PASSENGER CABIN 2026-93265<[01] REPLACED EMERGENCY EXIT HATCH LIFE LINE RH SIDE AT PASSENGER CABIN I.A.W. B737-80 - [SDR SWAA2026030966766](https://openairdocs.org/sdr/SWAA2026030966766), Feb 2, 2026: CROSSBEAM. CRACKED. CRACKED FLOOR STRUCTURE LOCATED BS 540, BL 0 - LBL 24. REPLACED FLOOR STRUCTURE IAW SRM 51-10-02, ITEM 9, & DWG 143A0060, SHEET 64, REV-. - [SDR SWAA2026030966984](https://openairdocs.org/sdr/SWAA2026030966984), Feb 2, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 867, S2 - 3R. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0 AND DWG 146A7901, SHEET 66, REV A. - [SDR SWAA2026030966769](https://openairdocs.org/sdr/SWAA2026030966769), Feb 2, 2026: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 217 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 217 AT RT WING IAW SRM 51-10-02 ITEM 9 - [SDR SWAA2026030966764](https://openairdocs.org/sdr/SWAA2026030966764), Feb 1, 2026: WEB. CRACKED. CRACKED WEB, BS 312 - 328, RBL 33. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, & DWG 141A5400, REV -, SHEET 39. - [SDR SWAA2026030966578](https://openairdocs.org/sdr/SWAA2026030966578), Feb 1, 2026: ACCESS PANEL. CRACKED. CRACK EXTERNAL SKIN ACCESS PANEL 191CR AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191CR AT LOWER FUSELAGE IAW SRM 51-70-04-2R-2 REPAIR 2. - [SDR SWAA2026030966576](https://openairdocs.org/sdr/SWAA2026030966576), Jan 31, 2026: FLOORBEAM. CORRODED. CORRODED FLOORBEAM, BS 986.5, RBL 43, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM-53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4, FIG 205. - [SDR SWAA2026030966425](https://openairdocs.org/sdr/SWAA2026030966425), Jan 31, 2026: FLOOR SUPPORT. CORRODED. CORRODED FLOOR SUPPORT, BS 947.5 - 967, LBL 24, WL 208.1. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 147A5650, SHEET - [SDR SWAA2026030966426](https://openairdocs.org/sdr/SWAA2026030966426), Jan 31, 2026: ANGLE. CORRODED. CORRODED ANGLE, FLOOR STRUCTURE BS 992.8, RBL 31, WL 208.1. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 147A5700, SHEET 123, REV A. - [SDR SWAA2026030966090](https://openairdocs.org/sdr/SWAA2026030966090), Jan 30, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL, BS 277 - 294.5, BL 0. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 20, REV-. - [SDR SWAA2026030966259](https://openairdocs.org/sdr/SWAA2026030966259), Jan 30, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 727, RBL 24.5 AND LBL 24.5, WL 156. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9. - [SDR SWAA2026030964779](https://openairdocs.org/sdr/SWAA2026030964779), Jan 27, 2026: SCUFF PLATE. CRACKED. CRACKED AFT CORNER SCUFF PLATE IN THE FWD CARGO BAY, REPAIRED THE SCUFF PLATE IAW. SRM 53-30-15-2R-1, REPAIR 1. - [SDR SWAA2026030665125](https://openairdocs.org/sdr/SWAA2026030665125), Jan 27, 2026: STRAP. CRACKED. CRACK ON STRAP LOCATED BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT 2026-93094<[01] REPLACED STRAP LOCATED BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT IAW B7 - [SDR SWAA2026030665126](https://openairdocs.org/sdr/SWAA2026030665126), Jan 27, 2026: STRAP. CRACKED. CRACK ON STRAP LOCATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT 2026-93096<[01] REPLACED STRAP LOCATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-800 - [SDR SWAA2026030664436](https://openairdocs.org/sdr/SWAA2026030664436), Jan 25, 2026: SCUFF PLATE. CRACKED. CRACK ON FWD SCUFT PLATE AT AFT CARGO COMPARTMENT 2026-93021<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30; S/N:A23272210; DUE DATE: 26/MAR/26.;[02] ON STEP 4: - [SDR SWAA2025120943349](https://openairdocs.org/sdr/SWAA2025120943349), Dec 6, 2025: LIGHT. FAULTED. LEFT FWD OVERWING EMERGENCY EXIT LIGHT FLICKERING. PERFORMED PHASE 2 DATA LOAD. OP CHECK GOOD IAW AMM 23-42-03. - [SDR SWAA2025112639318](https://openairdocs.org/sdr/SWAA2025112639318), Nov 23, 2025: SLIDE. DISLODGED. L2 DOOR SLIDE OUT OF CONTAINER. REPACKED L2 DOOR SLIDE IAW MT 725-61-06. ACFT OK FOR SERVICE. - [SDR SWAA2025112037078](https://openairdocs.org/sdr/SWAA2025112037078), Nov 20, 2025: BATTERY PACK. INOPERATIVE. AFTER L ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK BATTERY M1673 IAW MM 33-51-06, ALL 3 EMERGENCY LIGHT POWERED BY BATTERY PACK M1673 OPS C - [SDR SWAA2025082909604](https://openairdocs.org/sdr/SWAA2025082909604), Aug 28, 2025: SLIDE. UNPACKED. CREW REPORTED AFT ENTRY DOOR SLIDE IS IN CONTACT WITH THE FUSELAGE WHEN CLOSING THE DOOR. REPACKED AFTER ENTRY DOOR SLIDE IAW MT725-61-06 All 168: https://openairdocs.org/aircraft/N8628A/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 N8628A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8628A before. - [Cancelled 1996-01-16](https://openairdocs.org/deregistered/N8628A-1996-01-16): Enstrom 280FX, S/N 2069. Exported to Mexico. Owner: [Beech Transportation Inc DBA](https://openairdocs.org/faa-owner/BEECH%20TRANSPORTATION%20INC%20DBA), [Eden Prairie, MN](https://openairdocs.org/faa-place/MN/Eden%20Prairie) - [Cancelled 1970-07-15](https://openairdocs.org/deregistered/N8628A-1970-07-15): Beech D18S, S/N A-543. Exported to Bahamas. Owner: [Leasing Consultants Inc](https://openairdocs.org/faa-owner/LEASING%20CONSULTANTS%20INC), [Quenns, NY](https://openairdocs.org/faa-place/NY/Quenns) ## 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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.