# N8649A: 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: 42527 - Year built: 2014 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 23, 2014 - Certificate issued: October 8, 2014 - Expires: October 31, 2027 - Mode S code: ABE147 - 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=8649A - Page: https://openairdocs.org/aircraft/N8649A 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 N8649A. ## FAA accident and incident reports None matched to N8649A. ## Service difficulty reports (146, 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 SWAA2026072808960](https://openairdocs.org/sdr/SWAA2026072808960), Jul 11, 2026: WEB. CRACKED. CRACKED WEB, BTW BS 500F - 500G, RBL 25 IN THE FWD CARGO BAY. REPAIRED WEB IAW SRM 53-30-53-2R-1. - [SDR SWAA2026072896745](https://openairdocs.org/sdr/SWAA2026072896745), Jul 2, 2026: WEDGE. DEBONDED. DEBONDED WEDGE PANEL ON RT INBD MAIN FLAP AT RT WING. REPAIR ACCOMPLISHED IAW SRM 57-53-01-2R-18, REPAIR 18. - [SDR SWAA2026072802495](https://openairdocs.org/sdr/SWAA2026072802495), Jul 2, 2026: PANEL. DEBONDED. DEBONDED WEDGE PANEL ON LT INBOARD MAIN FLAP AT LT WING. REPLACED WEDGE PANEL ON LT INBOARD MAIN FLAP AT LT WING FOR REMOVAL AND INSTALLATION SEE TTG8Q01D0DSC. - [SDR SWAA2026072858158](https://openairdocs.org/sdr/SWAA2026072858158), Jul 1, 2026: WEB. CRACKED. CRACKED WEB, BS 500A, RBL 21, FWD CARGO BAY. INSTALLED A NEW WEB AND FASTENERS IAW SRM 51-40-02-0G, AND DWG 143A7505, SHEET 137, AND 138, REV -. - [SDR SWAA2026072859565](https://openairdocs.org/sdr/SWAA2026072859565), Jul 1, 2026: WEB. CRACKED. CRACKED WEB, TRAILING EDGE ORSS 275, RT WING. REPLACED THE WEB IAW SRM 51-10-02, I?TEM 9, SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV -. - [SDR SWAA2026072877221](https://openairdocs.org/sdr/SWAA2026072877221), Jun 30, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, LOWER HINGE PANEL 834DZ AT AFT ENTRY DOOR L2. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 411A2119, SH - [SDR SWAA2026072861022](https://openairdocs.org/sdr/SWAA2026072861022), Jun 30, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A1110, SHEET 55, REV -. - [SDR SWAA2026072872342](https://openairdocs.org/sdr/SWAA2026072872342), Jun 29, 2026: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 140BF AT AFT CARGO BAY. REPLACED FLOOR PANEL IAW SRM 51-10-02, ITEM 9, AND DWG 453A2610, SHEET 20, REV E. - [SDR SWAA2026072817982](https://openairdocs.org/sdr/SWAA2026072817982), Jun 29, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500I - 520, BL 0. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 139, REV-. - [SDR SWAA2026072823655](https://openairdocs.org/sdr/SWAA2026072823655), Jun 29, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500I, STR 28R, FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 143A7902, SHEET 320, REV -. - [SDR SWAA2026072898408](https://openairdocs.org/sdr/SWAA2026072898408), Jun 29, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500I, STR28L. FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 143A7902, SHEET 320, REV -. - [SDR SWAA2026072866567](https://openairdocs.org/sdr/SWAA2026072866567), Jun 27, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET ON ACCESS PANEL 834DZ ON THE AFT ENTRY DOOR. FAULT RESOLVED ON OTHER FAULT SEE FAULT TTG8Q01CZAL5 FAULT. - [SDR SWAA2026072895026](https://openairdocs.org/sdr/SWAA2026072895026), Jun 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 867, STRINGERS 2 - 3R UPPER POSITION AT PASSENGER CABIN. REPLACED SUPPORT ANGLE & FASTENERS BS 867 S2R - 3R UPPER POSITION AT PASSENGE - [SDR SWAA2026072895182](https://openairdocs.org/sdr/SWAA2026072895182), Jun 26, 2026: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS945 AT LEVEL STR26L AT AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMEN - [SDR SWAA2026072850681](https://openairdocs.org/sdr/SWAA2026072850681), Jun 26, 2026: SHIELD. CORRODED. CORROSION SHIELD WEB, BTW BS 492.4 - 500A, RBL 21 IN THE FWD CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-10-02, ITEM 9, AND DWG 143A0080, SHEET 39, REV-. - [SDR SWAA2026072849693](https://openairdocs.org/sdr/SWAA2026072849693), Jun 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500A, RBL 21, AFT SIDE FWD CARGO BAY. REPLACED CLIP AND FASTENERS, BS 500A, RBL 21 AFT SIDE FWD CARGO BAY IAW SRM 51-40-02-0G, AND DWG 143A750 - [SDR SWAA2026072825880](https://openairdocs.org/sdr/SWAA2026072825880), Jun 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, RBL 21 AFT SIDE FWD CARGO BAY, REPLACED THE ANGLE, BS 500H, RBL 21, AFT SIDE FWD CARGO BAY IAW SRM 51-10-02, ITEM 9, AND DWG 143A7505, S - [SDR SWAA2026072811304](https://openairdocs.org/sdr/SWAA2026072811304), Jun 24, 2026: GUSSET. CRACKED. CRACKED GUSSET ANGLE LOCATED BS 500I, S19R AT FWD CARGO BAY. REPLACED GUSSET AND FASTENERS LOCATED BS 500, IS 19R AT FWD CARGO BAY IAW SRM 51-40-02, AND SRM 51- - [SDR SWAA2026072810778](https://openairdocs.org/sdr/SWAA2026072810778), Jun 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, LOCATED BS 500H, LBL21 AFT SIDE FWD CARGO BAY. REPLACED THE ANGLE, LOCATED BS 500H, LBL21 AFT SIDE FWD CARGO BAY IAW SRM 51-10-02, ITEM 9, AND DW - [SDR SWAA2026072890761](https://openairdocs.org/sdr/SWAA2026072890761), Jun 24, 2026: ANGLE. CRACKED. CRACK ANGLE LOCATED BS500G AND RBL21 FWD SIDE FWD CARGO COMPARTMENT. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026072830949](https://openairdocs.org/sdr/SWAA2026072830949), Jun 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, LBL 21, FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 138, REV-. - [SDR SWAA2026072877858](https://openairdocs.org/sdr/SWAA2026072877858), Jun 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, RBL 21 FWD SIDE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 139, REV -. - [SDR SWAA2026072821886](https://openairdocs.org/sdr/SWAA2026072821886), Jun 24, 2026: ANGLE. CRACKED. CRACK ANGLE, BS 500H, LBL 21 FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET:139, REV-. - [SDR SWAA2026072800023](https://openairdocs.org/sdr/SWAA2026072800023), Jun 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 400 LBL 21 IN FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2026072827428](https://openairdocs.org/sdr/SWAA2026072827428), Jun 24, 2026: ACCESS PANEL. CORRODED. CORROSION ON BRACKET OF ACCESS PANEL 191CR AT LOWER FUSELAGE. REPLACED BRACKET OF ACCESS PANEL 191CR AT LOWER FUSELAGE IAW SRM 51-10-02, I?TEM 9, SRM 51-40-02, - [SDR SWAA2026072863129](https://openairdocs.org/sdr/SWAA2026072863129), Jun 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500F, RBL 21 FWD SIDE FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026072823313](https://openairdocs.org/sdr/SWAA2026072823313), Jun 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500F, RBL21 AFT SIDE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026072898032](https://openairdocs.org/sdr/SWAA2026072898032), Jun 23, 2026: HANDLE. DETERIORATED. DETERIORATED ENTRY DOOR ASSIST HANDLE NUT AT FWD GALLEY AREA (4 EA). REPLACED ENTRY DOOR ASSIST HANDLE NUT AT FWD GALLEY AREA (4EA) IAW AMM 52-11-31-400-802 STE - [SDR SWAA2026072843184](https://openairdocs.org/sdr/SWAA2026072843184), Jun 23, 2026: PLATE. CRACKED. CRACKED PLATE ATTACH ON FWD ENTRY DOOR LINING AT FWD GALLEY AREA. REPLACED THE PLATE ATTACH ON FWD ENTRY DOOR LINING AT FWD GALLEY AREA IAW SOPM 20-50-12, REV 5 - [SDR SWAA2026072872781](https://openairdocs.org/sdr/SWAA2026072872781), Jun 22, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9. - [SDR SWAA2026072894889](https://openairdocs.org/sdr/SWAA2026072894889), Jun 19, 2026: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM LOCATED BS986.5 RBL43 AND WL208.1. PERFORMED PERMANENT REPAIR ON FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6. - [SDR SWAA2026072857150](https://openairdocs.org/sdr/SWAA2026072857150), Jun 19, 2026: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM LOCATED BS947.5 LBL4 AND WL208.1 AT AFT GALLEY AREA. PERFORMED REPAIR ON FLOORBEAM LOCATED AT BSTA 947.5 - BTW LBL50 TO RBL20 AND WL208.1 - [SDR SWAA2026072811416](https://openairdocs.org/sdr/SWAA2026072811416), Jun 18, 2026: STRAP. CORRODED. CORROSION ON LOWER ATTACH STRAP LOCATED AT OSS 422 LEADING EDGE AT RH WING. PERFORMED REPAIR CATEGORY A ON LOWER ATTACH STRAP LOCATED AT OSS 422 LEADING EDGE AT - [SDR SWAA2026031178354](https://openairdocs.org/sdr/SWAA2026031178354), Mar 10, 2026: COVER. OUT OF ADJUST. L1 DOOR SLIDE COVER OUT OF PLACE. REPOSITIONED LANYARD COVER AND INSPECTED SLIDE IAW MM 25-66-00, NO FURTHER DEFECTS NOTED. - [SDR SWAA2025101523814](https://openairdocs.org/sdr/SWAA2025101523814), Oct 12, 2025: POWER SUPPLY. INOPERATIVE. M1694 & M1695 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACKS INOPERATIVE. R & R M1694 & M1695 POWER SUPPLIES AND ASSOCIATED BATTERY PACKS IAW MM 33-51-06. OPS C - [SDR SWAA2025101524696](https://openairdocs.org/sdr/SWAA2025101524696), Oct 12, 2025: BATTERY PACK. INOPERATIVE. M1694 & M1695 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACKS INOPERATIVE. R & R M1694 & M1695 POWER SUPPLIES AND ASSOCIATED BATTERY PACKS IAW MM 33-51-06. OPS C - [SDR SWAA2025062584582](https://openairdocs.org/sdr/SWAA2025062584582), Jun 23, 2025: MEGAPHONE. BROKEN. FWD GALLEY MEGAPHONE FELL AND HANDLE BROKE<[01] REPLACED MEGAPHONE IAW AMM 25-64-00. - [SDR SWAA2025052272862](https://openairdocs.org/sdr/SWAA2025052272862), May 20, 2025: SEAT. INOPERATIVE. PASSENGER CABIN SEAT 13F RECLINE FUNCTIONS AND SHOULD BE INOP DUE TO EMERGENCY EXIT ROW <[01]. LOCKED OUT 13F RECLINE CABLE/HYDORCK PER CMM 25-22-46. - [SDR SWAA2024111960582](https://openairdocs.org/sdr/SWAA2024111960582), Nov 15, 2024: FUEL SYS. ERRATIC. HAD 200 LB FUEL IMBALANCE ON #1 TANK. REBALANCED FUEL AND WITHIN 18 MIN; HAD A 500 LBS IMBALANCE. THEN RAPIDLY DROPPED TO 1800LBS. UPON FINAL APPROACH; #1 FUEL - [SDR SWAA2024091134939](https://openairdocs.org/sdr/SWAA2024091134939), Sep 7, 2024: LATCH. LOOSE. L1 DOOR LIFE RAFT GIRT BAR LATCHES ARE LOOSE.<[01] REMOVED & REINSTALLED L1 DOOR LIFE RAFT GIRT BAR LATCHES PER AMM 25-66-02-000-801 & AMM 25-66-02-400-801.;[02 - [SDR SWAA2024091134453](https://openairdocs.org/sdr/SWAA2024091134453), Sep 5, 2024: BATTERY PACK. NO TEST. BATTERY PACK M2335 FAILS TEST<[01] REMOVED AND REPLACED BATTERY PACK M2335 AND PERFORMED GOD OPERATIONAL CHECK IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIV - [SDR SWAA2024091129619](https://openairdocs.org/sdr/SWAA2024091129619), Aug 23, 2024: ANGLE. CRACKED. LT WING UPPER T/E FIX PANEL BETWEEN #5 AND #6 SPOILERS; SUPPORT BEAM ATTACHMENT ANGLE TO DEFLECTION CONTROL RIB CRACK.<[01] REMOVED; REPLACED; AND INSTALLED A N - [SDR SWAA2024091129620](https://openairdocs.org/sdr/SWAA2024091129620), Aug 23, 2024: RIB. CRACKED. LT WING T/E ANGLE RIB CRACK AT ORSS 261+13.<[01] REMOVED AND REPLACED LT WING T/E ANGLE RIB AT ORSS 261+13 IAW SRM 51-40-02.;[02] REMOVED AND REPLACED LT WING T - [SDR SWAA2024091129317](https://openairdocs.org/sdr/SWAA2024091129317), Aug 22, 2024: SUPPORT. CRACKED. CRACKED PANEL BREAK AT PASSENGER CABIN BS540 RBL1 WL208.<[01] ALL STEPS COMPLETED REMOVED FLOOR PANEL 231UF PER AMM 53-21-00-000-801 REMOVED CRACKED PANEL BREAK - [SDR SWAA2024091129318](https://openairdocs.org/sdr/SWAA2024091129318), Aug 22, 2024: SUPPORT. CRACKED. CRACKED PANEL BREAK AT PASSENGER CABIN BS540 LBL1 WL208.<[01] ALL STEPS COMPLETED REMOVED CRACKED PANEL BREAK AT PASSENGER CABIN BS 540 LBL1 WL208 PER SRM 51-40 - [SDR SWAA2024091128739](https://openairdocs.org/sdr/SWAA2024091128739), Aug 22, 2024: SKIN. DEBONDED. #4 AFT FLAP LOWER SKIN IS DISBONDED ON I/B SIDE.<[01] CORRECTED SUB-STEP 4;[02] REMOVED AND REPLACED R/H O/B AFT FLAP IAW AMM 27-51-22-400-801 AND AMM 27-51-22- - [SDR SWAA2024091131587](https://openairdocs.org/sdr/SWAA2024091131587), Aug 21, 2024: SEAT. OUT OF ADJUST. PASSENGER SEAT HYDRAULIC LOCK REQUIRES ADJUSTMENT ON SEATS 2A; 3C; 4A; 5C; 6C; 7A; 11C; 12BC<[01] ADJUSTED PASSENGER SEAT HYDRAULIC LOCK ON SEATS 2A; 3C; 4A; 5C - [SDR SWAA2024091131953](https://openairdocs.org/sdr/SWAA2024091131953), Aug 21, 2024: SEAT. OUT OF ADJUST. PASSENGER SEAT HYDRAULIC LOCK REQUIRES ADJUSTMENT ON SEATS 7DF; 8DF; 9F; 10DF; 11F; 12DE<[01] ADJUSTED PASSENGER SEAT HYDRAULIC LOCK ON SEATS 7DF; 8DF; 9F; 10DF - [SDR SWAA2024091128241](https://openairdocs.org/sdr/SWAA2024091128241), Aug 21, 2024: SKIN. DEBONDED. PANEL 192AL OUTER SKIN HAS AN AREA OF DISBOND NEAR FWD EDGE OF PANEL. (MARKED)<[01] 04 - REPAIRED PER [SRM 51-70-05-2R-2-B00319 (REPAIR 2 - REPAIR OF DAMAGE THA - [SDR SWAA2024061300752](https://openairdocs.org/sdr/SWAA2024061300752), Jun 12, 2024: BATTERY PACK. INOPERATIVE. CEILING EMERGENCY LIGHTS AT ROWS 6-14 DEF INOP<[01] REMOVED AND REPLACED POWER PACK CHARGER ASSY IAW AMM 33-51-51 AT ROWS 6-14 DEF OPS CHECK GOD. All 146: https://openairdocs.org/aircraft/N8649A/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 N8649A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8649A before. - [Cancelled 1958-06-30](https://openairdocs.org/deregistered/N8649A-1958-06-30): Beech A35, S/N D-2125. Owner: [Frawley James R](https://openairdocs.org/faa-owner/FRAWLEY%20JAMES%20R), [Alhambra, CA](https://openairdocs.org/faa-place/CA/Alhambra) ## 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.