# N8687A: 2016 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/F series](https://openairdocs.org/engine/cfm-international-cfm56-7b27e-f-series) (registry code 13100) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 33937 - Year built: 2016 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 16, 2016 - Certificate issued: July 12, 2016 - Expires: July 31, 2029 - Mode S code: ABEFDD - 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=8687A - Page: https://openairdocs.org/aircraft/N8687A 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/F 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/F 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 N8687A. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20190118008189I](https://openairdocs.org/incident/20190118008189I), Jan 18, 2019: Boeing 737-8H4 (N8687A), Omaha, NE, Minor damage. On flight from las to oma, oma METAR was reporting light freezing drizzle and breaking action of 5-5-5 or wet good. Crew landed normally and was at taxi speed.… ## Service difficulty reports (88, 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 SWAA2026081014795](https://openairdocs.org/sdr/SWAA2026081014795), Aug 3, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1695 ARE INOPERATIVE. REPLACED THE BATTERY PACK M1695 AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06- - [SDR SWAA2026080716825](https://openairdocs.org/sdr/SWAA2026080716825), Aug 1, 2026: NUT. BROKEN. UPON INSTALLATION OF G1, ASSIST HANDLE RETAINING NUT FOUND BROKEN UPON INSTALLATION OF G1 ASSIST HANDLE RETAINING NUT FOUND BROKEN. REPLACED BROKEN NUT ON G1 AS - [SDR SWAA2026020266359](https://openairdocs.org/sdr/SWAA2026020266359), Jan 30, 2026: LENS. DETACHED. OVERHEAD CIELING EXIT LIGHT LENS FELL OFF. R & R LIGHT ASSY REF AMM 33-51-01 - [SDR SWAA2026010557567](https://openairdocs.org/sdr/SWAA2026010557567), Jan 1, 2026: LENS. MISSING. EMERGENCY EXIT SIGN MID CABIN NOT IN PLACE, NEEDS TO BE INSTALLED. INSTALLED MID CABIN EXIT SIGN LENS PER AMM 33-51-02 - [SDR SWAA2025120140999](https://openairdocs.org/sdr/SWAA2025120140999), Nov 29, 2025: LIGHT. BROKEN. CENTER AISLE EXIT LIGHT BROKEN. REINSTALLED MID CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01. ACFT OK FOR SERVICE. - [SDR SWAA2025120140801](https://openairdocs.org/sdr/SWAA2025120140801), Nov 29, 2025: ACM. SEIZED. LEFT ACM LIGHT ILLUMANTED FOLLOWED BY AN ODOR IN THE FLIGHT DECK. OK TO CONTINUE IAW MEL 21-1-01, SP1, AUTH 295231, FOUND LT ACM DAMAGED & SEIZED. R & R LT ACM - [SDR SWAA2025102125446](https://openairdocs.org/sdr/SWAA2025102125446), Oct 18, 2025: LENS. DETACHED. EMERGENCY EXIT SIGN FROM THE CENTER CABIN CEILING FELL OFF. RESURCURED CENTER CABIN EMERGENCY EXIT SIGN COVER REF. SIP. - [SDR SWAA2025102025244](https://openairdocs.org/sdr/SWAA2025102025244), Oct 17, 2025: BATTERY. INOPERATIVE. AFT LH OB EMERGENCY FLASHLIGHT INOP. R & R THE EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00. - [SDR SWAA2025092316604](https://openairdocs.org/sdr/SWAA2025092316604), Sep 20, 2025: GIRT BAR. OUT OF ADJUST. FORWARD SERVICE DOOR GIRT BAR EXTENDED MORE THAN NORMAL. ADJUSTED FWD SERVICE DOOR GIRT BAR PER AMM 25-66-01. - [SDR SWAA2025082708038](https://openairdocs.org/sdr/SWAA2025082708038), Aug 25, 2025: SIGN. DETACHED. OVERHEAD EXIT SIGN BETWEEN ROWS 15 AND 16 FELL FROM CEILING. REINSTALL OVERHEAD EXIT SIGN AS PER AMM 33-51-00. REINSTALLED OVERHEAD EXIT SIGN IAW AMM 33-51-01. - [SDR SWAA2025052771563](https://openairdocs.org/sdr/SWAA2025052771563), May 16, 2025: BATTERY PACK. INOPERATIVE. LEFT OVER WING HATCH EMERGENCY LIGHTS INOP. R&R EMERGENCY LIGHT BATTERY PACK AT M1694 IAW AMM 33-51-06. - [SDR SWAA2025052770777](https://openairdocs.org/sdr/SWAA2025052770777), May 13, 2025: LENS. MISSING. FWD LAVATORY EMERGENCY FLOOR PROXIMITY EXIT INDICATOR LIGHT LENS COVER LOCKING TAB ON THE BASE MISSING. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY; OPS CHECK - [SDR SWAA2025052867661](https://openairdocs.org/sdr/SWAA2025052867661), May 6, 2025: FAIRING. DEBONDED. LEFT WING #3 TRAILING EDGE FLAP AFT SUPPORT FAIRING TAILCONE HAS ELONGATED FASTENERS HOLES.<[01] REMOVED AND INSTALLED SERVICEABLE LEFT WING #3 TRAILING EDGE FL - [SDR SWAA2025052864520](https://openairdocs.org/sdr/SWAA2025052864520), Apr 26, 2025: COWL DOOR. CRACKED. #1 ENGINE INBOARD FAN COWL; PANEL 414; WEB AFT OF OIL SERVICE DOOR CRACKED. REMOVED AND REPLACE #1 ENG I/B FAN COWL IAW AMM 71-11-02. - [SDR SWAA2025052864522](https://openairdocs.org/sdr/SWAA2025052864522), Apr 26, 2025: COWL DOOR. CRACKED. #2 ENGINE OUTBOARD FAN COWL; PANEL 424; WEB AFT OF THE OIL SERVICE DOOR CRACKED.<[01] REMOVED AND REPLACED #2 ENGINE OUTBOARD FAN COWL PER AMM 71-11-02 AND MT# - [SDR SWAA2025052764525](https://openairdocs.org/sdr/SWAA2025052764525), Apr 26, 2025: SEAL. CRACKED. TAIL PANEL 333AT BLADE SEAL CRACKED. REMOVED AND INSTALLED NEW SEAL PER. SRM 51-40-02. - [SDR SWAA2025052764523](https://openairdocs.org/sdr/SWAA2025052764523), Apr 26, 2025: SEAL. CRACKED. PANEL 343AT METAL BLADE SEAL CRACKED. REMOVED AND INSTALLED NEW SEAL PER. SRM 51-40-02. - [SDR SWAA2025052764531](https://openairdocs.org/sdr/SWAA2025052764531), Apr 26, 2025: SEAL. CRACKED. TAIL PANEL 323BL SLIDER SEAL CRACKED. REMOVED AND REPLACED SLIDER SEAL I.A.W SRM 51-40-02. REMOVED AND REPLACED SLIDER SEAL I.A.W SRM 51-40-02. - [SDR SWAA2025052864261](https://openairdocs.org/sdr/SWAA2025052864261), Apr 25, 2025: SKIN. DELAMINATED. R/H O/B AFT FLAP LOWER INBD CORNER HAS PREVIOUS REPAIR THAT HAS DELAMED. REMOVED PREVIOUS REPAIR;,NO ADDITIONAL DAMAGE NOTED PER SRM 57-53-01-2R-14, ACCOMPLISHE - [SDR SWAA2025052764264](https://openairdocs.org/sdr/SWAA2025052764264), Apr 25, 2025: BRACKET. CRACKED. NUMBER 2 PYLON; LOWER AFT FAIRING CRACKED AT THE AFT 'V' SHAPE FITTING BRACKET THAT THE HYDRAULIC LINES PASS THROUGH. REMOVED DAMAGED #2 PYLON AFT FITTING BRACK - [SDR SWAA2025052153379](https://openairdocs.org/sdr/SWAA2025052153379), Apr 25, 2025: PANEL. DAMAGED. PANEL 561BB HAS ONE FASTENER HOLE THAT IS ELONGATED AND ALSO HAS COUNTER SINK DAMAGE.<[01] REPAIRED DAMAGED AREA PER SRM 51-70-08-0G-0.;[02] C/W INSPECTION - [SDR SWAA2025052753370](https://openairdocs.org/sdr/SWAA2025052753370), Apr 24, 2025: ANGLE. CRACKED. CRACK FOUND ON VAPOR BARRIER ATTACH ANGLE RBL 34; STA 663<[01] REMOVED FASTENERS AND MATCH-DRILLED REPLACEMENT ANGLE PER SRM 51-40-02;[15] REMOVED AND REPLACED - [SDR SWAA2025052753374](https://openairdocs.org/sdr/SWAA2025052753374), Apr 24, 2025: SKIN. DELAMINATED. LEFT OUTBOARD AFT FLAP HAS A HUGE DELAMINATION ON THE UPPER INBOARD SURFACE. (MARKED)<[01] OK TO INSTALL AFT FLAP;[02] REMOVED AND REPLACED LEFT OUTBOARD AFT FL - [SDR SWAA2025052853315](https://openairdocs.org/sdr/SWAA2025052853315), Apr 22, 2025: HANDLE. LOOSE. FWD ENTRY DOOR INNER HANDLE IS LOOSE. REMOVED AND REPLACED INTERIOR HANDLE BOLTS (2) EA IAW AMM 52-11-31. REMOVED AND REPLACED INTERIOR HANDLE BOLTS (2) EA IAW - [SDR SWAA2025052853356](https://openairdocs.org/sdr/SWAA2025052853356), Apr 22, 2025: HANDLE. OUT OF ADJUST. FORWARD ENTRY DOOR EXTERIOR HANDLE WILL NOT RETRACT WHEN DOOR IS CLOSED. ADJUSTED DOOR IAW AMM 52-11-00. INSPECTED WORK PERFORMED - [SDR SWAA2025040921923](https://openairdocs.org/sdr/SWAA2025040921923), Apr 6, 2025: FLASHLIGHT. FAILED. RIGHT HAND AFT INBOARD EMERGENCY FLASHLIGHT NOT TESTING. OK TO CONTINUE PER MEL 25-12-01; SP1B; AUTHORIZATION #245910 RIGHT HAND AFT INBOARD EMERGENCY FLASHLIGH - [SDR SWAA2025040822082](https://openairdocs.org/sdr/SWAA2025040822082), Apr 5, 2025: FLASHLIGHT. NO TEST. CREW REPORTS RH AFT IB EMERGENCY FLASHLIGHT NOT TESTING<[01] REMOVED AND REPLACED RH AFT IB EMERGENCY FLASHLIGHT PER AMM 35-55-00 - [SDR SWAA2024102150426](https://openairdocs.org/sdr/SWAA2024102150426), Oct 17, 2024: FUEL FILTER. CONTAMINATED. AT APPROX 500 AGL # 2 FILTER BYPASS LIGHT ILLUMINATED<[01] PERFORMED FIM 73-05 TASK 801 THRU STEP 2.D.1.B. FOUND METAL CONTAMINATION IN FUEL FILTER. FILTER SENT - [SDR SWAA2024091135091](https://openairdocs.org/sdr/SWAA2024091135091), Sep 7, 2024: PANEL. CRACKED. CRACK ON PANEL 194 FL; EDGE OF APU DRAIN MAST HOLE. CRACK ON PANEL 194 FL EDGE OF APU DRAIN MAST HOLE.<[01] ACCOMPLISHED PERMANENT REPAIR PER.SRM.53-60-70-2R-1 - [SDR SWAA2024091135180](https://openairdocs.org/sdr/SWAA2024091135180), Sep 7, 2024: PANEL. DELAMINATED. PANEL 194GL HAS DELAM 10IN. L X 1.25W EXTENDING 4IN.12IN. AFT OF PANEL L/E AND 13IN. UP FROM PANEL LOWER EDGE. PANEL 194GL HAS DELAM 10IN. L X 1.25W EXTENDING 4 - [SDR SWAA2024082628698](https://openairdocs.org/sdr/SWAA2024082628698), Aug 21, 2024: PANEL. CRACKED. A CRACK ON THE EDGE OF THE HOLE WHERE THE APU DRAIN MAST LINE GO THROUGH ON PANEL 194FL.<[01] ACCOMPLISHED EA 24-153-02300 - [SDR SWAA2024082328697](https://openairdocs.org/sdr/SWAA2024082328697), Aug 21, 2024: DRAIN MAST. MISSING. APU FUEL DRAIN MAST MISSING<[01] ADDED PART INFORMATION;[02] INSTALLED APU DRAIN MAST PER AMM 28-25-07 - [SDR SWAA2024052988739](https://openairdocs.org/sdr/SWAA2024052988739), May 22, 2024: SKIN. CRACKED. FOUND POWER RECEPTACLE LOWER SKIN EDGE CRACKED<[01] ACCOMPLISHED REPAIR PER SRM 51-40-02-0G-0 SRM 53-10-15-2R-4 REPAIR 4 IPC 52-48-51-02B DWG 141A3722;[02] VERI - [SDR SWAA2024052987971](https://openairdocs.org/sdr/SWAA2024052987971), May 20, 2024: BATTERY PACK. INOPERATIVE. SEVERAL PAX CABIM EMERGENCY LIGHTS INOP<[01] PERFORMED T/S OF EMERGENCY LIGHTS FOUND M1676; M1670; M1671; AND M1673 DEFECTS; REF. TO B 737 FIM TASK 33-50-TASK 8 - [SDR SWAA2024052986487](https://openairdocs.org/sdr/SWAA2024052986487), May 16, 2024: FLOOR PANEL. INSTALLED. INSPECTION REJECTION: FAILURE TO BE ACCOMPLISHED (NDT) HFEC PROCEDURE OF THE TRIMMED EDGE FOR FREE CRACK CONDITION INDICATED PER EA M-21-153-00734 REF: TTG8Q00T - [SDR SWAA2024052983358](https://openairdocs.org/sdr/SWAA2024052983358), May 7, 2024: SCUFF PLATE. CRACKED. FOUND AFT CARGO AFT SCUFF PLATE AFT CORNER HAS A CRACK. REPAIRED AFT CARCO AFT SCUFF PLATE. - [SDR SWAA2024052882230](https://openairdocs.org/sdr/SWAA2024052882230), May 4, 2024: FLOOR PANEL. DELAMINATED. FWD WET AREA FLOOR PANEL DELAMINATED PART # 141A5810-464<[01] LATE ENTRY: RECEIVED NEW FLOOR PANEL PN# 141A5810-464 INSTALLATION WAS ACCOMPLISHED 5/16/2024 ON # - [SDR SWAA2024052981709](https://openairdocs.org/sdr/SWAA2024052981709), May 2, 2024: FLOOR SUPPORT. CRACKED. FWD CABIN FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACKED AT FASTENER HOLES BL 0 BETWEEN BS 380 & 400. REMOVED AND INSTALLED NEW ANGLE SUPPORT UPPER CAP AT FWD CABI - [SDR SWAA2024052981701](https://openairdocs.org/sdr/SWAA2024052981701), May 2, 2024: FLOOR SUPPORT. CRACKED. FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACK AT LBL 13 BETWEEN STA 380 AND STA 400. REMOVED AND INSTALLED NEW FLOOR SUPPORT INTERCOSTAL UPPER CA - [SDR SWAA2024052981710](https://openairdocs.org/sdr/SWAA2024052981710), May 2, 2024: FLOOR PANEL. DELAMINATED. FWD CABIN WET AREA FLOOR PANEL 221GF TOP LAYER DELAMITED AND FWD O/B CORNER BROKEN. FAULT WAS RESOLVED ON ANOTHER FAULT; REF TO TTG8Q00T3U69. FOR INSTALLATION R - [SDR SWAA2024052981935](https://openairdocs.org/sdr/SWAA2024052981935), May 2, 2024: FLOOR SUPPORT. CRACKED. MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL 1. REMOVED AND INTALLED NEW SUPPORT BREAK AT MAIN CABIN CENTER SECTION FLOOR PER SRM 51-40- - [SDR SWAA2024052981940](https://openairdocs.org/sdr/SWAA2024052981940), May 2, 2024: FLOOR SUPPORT. CRACKED. MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL 1. REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK AT STA 540 RBL 1 REF. - [SDR SWAA2024052981700](https://openairdocs.org/sdr/SWAA2024052981700), May 2, 2024: FLOORBEAM. CORRODED. CORROSION SPOT FOUND AT FWD CABIN WET AREA FLOOR SUPPORT BEAM TOP SURFACE
STA 294.5 RBL 13 MKD DOT<[01] STEP 14 FABRICATED ANGLES NOT HEAT TREATED;[02] CORRE - [SDR SWAA2024052981943](https://openairdocs.org/sdr/SWAA2024052981943), May 2, 2024: FLOORBEAM. CORRODED. AFT WET AREA FLOOR BEAM SUPPORT STA 947.5 ;RBL50 AFT OUTBOARD FITTING SUPPORT GALLEY;AT INBOARD POSITION HAS CORROSION.<[01] ACCOMPLISHED REPAIR AT AFT WET AREA - [SDR SWAA2024052981951](https://openairdocs.org/sdr/SWAA2024052981951), May 2, 2024: RETAINER. CRACKED. LEFT HORIZONTAL STAB UPPER PANEL 333AT BLADE SEAL RETAINER CRACK.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STAB UPPER PANEL 333AT BLADE SEAL RETAINER AS PER SR - [SDR SWAA2024052981952](https://openairdocs.org/sdr/SWAA2024052981952), May 2, 2024: RETAINER. CRACKED. RIGHT HORIZONTAL STAB PANEL 343AT BLADE SEAL RETAINER CRACK.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB PANEL 343AT BLADE SEAL RETAINER REF.&NBSP;&NBSP;&NB - [SDR SWAA2024052981706](https://openairdocs.org/sdr/SWAA2024052981706), May 2, 2024: WEB. CRACKED. LEFT WING DEFLECTOR RIB CONTROL FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER WEB CRACKED @ O/B END. REMOVED AND INSTALLED NEW WEB RETAINER AT LEFT WING DEFLE - [SDR SWAA2024052981435](https://openairdocs.org/sdr/SWAA2024052981435), May 1, 2024: PLATE. CORRODED. CORROSION AT AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB PLATE. COMPLETED INSTALLATION OF NEW LOWER SILL WEB AT AFT CARGO COMPARTMENT DOOR CUTOUT PER SRM 5 - [SDR SWAA2024052981437](https://openairdocs.org/sdr/SWAA2024052981437), May 1, 2024: CHANNEL. CORRODED. AFT CARGO COMPARTMENT L/H SIDE FLOOR SUPPORT Z CHANNEL CORRODED S-26L FROM STA 727E STA 807. REMOVED; RECEIVED AND INSTALLED NEW SUPPORT Z CHANNEL AT AFT CARGO - [SDR SWAA2024052981440](https://openairdocs.org/sdr/SWAA2024052981440), May 1, 2024: STRAP. CORRODED. AFT CARGO BAY FLOOR SUPPORT STRAP FASTENER HOLE AT S26R BS 887. REMOVED CORROSION AT AFT CARGO BAY FLOOR SUPPORT STRAP FASTENER HOLE AT S26R BS 887 IAW SRM 51-1 All 88: https://openairdocs.org/aircraft/N8687A/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/F 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 N8687A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8687A before. - [Cancelled 1978-01-23](https://openairdocs.org/deregistered/N8687A-1978-01-23): Beech A35, S/N D-2097. Owner: [Kenyon Dale L](https://openairdocs.org/faa-owner/KENYON%20DALE%20L), [Richland, WA](https://openairdocs.org/faa-place/WA/Richland) ## Related - Other Boeing 737-8H4 aircraft: https://openairdocs.org/model/boeing-737-8h4/aircraft.md - The CFM International CFM56-7B27E/F series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b27e-f-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.