# N8699A: 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: 36923 - Year built: 2016 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 1, 2016 - Certificate issued: October 6, 2016 - Expires: October 31, 2029 - Mode S code: ABF3DA - 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=8699A - Page: https://openairdocs.org/aircraft/N8699A 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 N8699A. ## FAA accident and incident reports None matched to N8699A. ## Service difficulty reports (93, 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 SWAA2026101218971](https://openairdocs.org/sdr/SWAA2026101218971), Oct 11, 2026: FILTER. ODOR. SEVERAL PAX SMELLED A SCORCHED ODOR AROUND ROW 27 ON THE RT SIDE OF THE ACFT. RAN PACKS WITH ENG BLEEDS RAN PACKS WITH APU BLEED NO SCORCHED ODOR NOTED. SLIGHT - [SDR SWAA2026101238616](https://openairdocs.org/sdr/SWAA2026101238616), Oct 11, 2026: HYDRAULIC SYSTEM. OVERSERVICED. SEVERAL PAX SMELLED A SCORCHED ODOR AROUND ROW 27 ON THE RIGHT SIDE OF THE AIRCRAFT. RAN PACKS WITH ENG BLEEDS RAN PACKS WITH APU BLEED NO ODOR NOTED. SLIGHT HY - [SDR SWAA2026031679121](https://openairdocs.org/sdr/SWAA2026031679121), Mar 12, 2026: ACCESS PANEL. DELAMINATED. WING-TO-BODY FAIRING PANEL 192BL LEADING EDGE DELAMINATION. APPLIED REPAIR PLIES PER SRM 51-70-05. REQIURES PAINT FINISH. PANEL 192BL REMOVED IAW SRM 51-40-02. - [SDR SWAA2026022473176](https://openairdocs.org/sdr/SWAA2026022473176), Feb 22, 2026: PANEL. DELAMINATED. PANEL 192 BL IS DELAMINATED ON FWD LEADING EDGE SKIN. COMPLIED WITH EA 26-153-00501. - [SDR SWAA2025101421498](https://openairdocs.org/sdr/SWAA2025101421498), Oct 5, 2025: FILLER. MISSING. EGPR DOOR CUT OUT REPAIR FILLER IS MISSING. REPLACED MISSING FILLER ON EXISTING EGPR DOOR CUT OUT REPAIR IAW B737-800 SRM 53-10-15-2R-4. - [SDR SWAA2025082204445](https://openairdocs.org/sdr/SWAA2025082204445), Aug 14, 2025: BATTERY PACK. INOPERATIVE. L/H OVERWING EMERGENCY LIGHT BATTERY PACK INOP AT. STA 565L<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06;[02] L/H OVERWING EMERGENCY LIGHTS OPS CHECKE - [SDR SWAA2025082298619](https://openairdocs.org/sdr/SWAA2025082298619), Aug 6, 2025: ANGLE. CRACKED. LH WING ANGLE CRACKED INBOARD OF MIDSPAN DEFLECTION CONTROL RIB<[01] REMOVED L/H WING ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB FOR REPLACEMENT.;[02] LOC - [SDR SWAA2025082298259](https://openairdocs.org/sdr/SWAA2025082298259), Aug 4, 2025: LENS. CRACKED. BULL NOSE TRIM ABOVE 28-29 ABC OVERHEAD BIN EMERGENCY LIGHT LENS COVER CRACKED.<[01] R/R LENS PER AMM 33-51-03;[02] 02 - INSPECTED PER [AMM 33-51-03-960-803-NG - [SDR SWAA2025082698537](https://openairdocs.org/sdr/SWAA2025082698537), Aug 3, 2025: SKIN. DAMAGED. FASTENER HOLE COMMON TO THE FUEL TANK AT STA.663 LBL 60 SHOWS INDICATION OF A DEFECT USING HFEC. (M). HFEC HOLE PROBE INSPECTION OF FASTENER HOLE COMMON TO THE - [SDR SWAA2025082296425](https://openairdocs.org/sdr/SWAA2025082296425), Jul 30, 2025: PANEL. CRACKED. PANEL 193AR HAS CRACK ON UPPER FWD EDGE.<[01] REMOVED PANEL 193AR TO F.O.M. PER AMM 53-51-21;[02] DISREGARD CORRECTIVE ACTION STATEMENT #1. SEE FAULT ID TTG8Q01 - [SDR SWAA2025082195573](https://openairdocs.org/sdr/SWAA2025082195573), Jul 26, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241DF DELAMINATED WITH NUMEROUS DENTS. INSTALLED A NEW FLOOR PANEL 241DF IAW AMM 53-21-00. - [SDR SWAA2025082294441](https://openairdocs.org/sdr/SWAA2025082294441), Jul 23, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED ON OUTBD SIDE OF FLEX JOINT @ LBL 34' HFEC VERIFIED.<[01] DAMAGE AT LBL 34 IS VERIFIED USING HFEC PER NDT PART 6; 51-0 - [SDR SWAA2025082294129](https://openairdocs.org/sdr/SWAA2025082294129), Jul 23, 2025: FITTING. CRACKED. R/H WING INBD TRAILING EDGE; UPPER SHELF PANEL INTERCOSTAL INBD OF DEFLECTION FITTING IS CRACKED<[01] REMOVED INTERCOSTAL WEB INBD OF R/H WING DEFLECTION CONTRO - [SDR SWAA2025082194119](https://openairdocs.org/sdr/SWAA2025082194119), Jul 23, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242CF DELAMINATED WITH NUMEROUS DENTS. INSTALLED FLOOR PANEL 242CF PER AMM 53-21-00. - [SDR SWAA2025082693633](https://openairdocs.org/sdr/SWAA2025082693633), Jul 22, 2025: PLATE. CRACKED. LEFT WING REAR SPAR, WAFFLE PLATE INBD OF NR 3 FLAP TRACK WAS CRACKED AT FASTNERS. REMOVED AND REPLACED LT WING REAR SPAR WAFFLE PLATE IAW SRM 51-40-02. - [SDR SWAA2025082293965](https://openairdocs.org/sdr/SWAA2025082293965), Jul 22, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED ON INBOARD SIDE OF FLEX JOINT @ RBL 9 AND SUSPECTED CRACK AT RBL 34<[01] ACCOMPLISHED HFEC SURFACE INSPECTION OF RBL 3 - [SDR SWAA2025082293628](https://openairdocs.org/sdr/SWAA2025082293628), Jul 21, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED ON INBOARD SIDE OF FLEX JOINT @ LBL 9.<[01] REMOVED RIVETS AT L/H STA 663 ATTACH ANGLE COMMON TO VAPOR BARRIER FROM LB - [SDR SWAA2025082292708](https://openairdocs.org/sdr/SWAA2025082292708), Jul 18, 2025: SKIN. DELAMINATED. RIGHT OUTBOARD TRAILING EDGE FLAP HAS DELAM ON INBD TRAILING CORNER AND SHARP BEVEL ON TRAILING EDGE AT FLAP CENTER.<[01] REMOVED R/H O/B AFT FLAP PER MM 27-51- - [SDR SWAA2025060276713](https://openairdocs.org/sdr/SWAA2025060276713), May 30, 2025: FLASHLIGHT. BROKEN. FWD F/A FLASHLIGHT WILL NOT TEST AND SEAL IS BROKEN. <[01] REMOVED & REPLACED FWD FA FLASHLIGHT ASSY IAW AMM 25-64-00; OPS CHECK GOOD. - [SDR SWAA2025032406289](https://openairdocs.org/sdr/SWAA2025032406289), Mar 18, 2025: PANEL. CRACKED. AFT CARGO COMPARTMENT PANEL 141FW HAS CRACKS AT LOWER EDGE <[01]. REMOVED AND FABRICATED PANEL PER AMM 25-52-01. PANEL WILL REQUIRE INSTALLATION.; [02] INSTALLE - [SDR SWAA2025021896389](https://openairdocs.org/sdr/SWAA2025021896389), Feb 15, 2025: BATTERY PACK. NO TEST. AFT FLASHLIGHT UNDER FLIGHT ATTENDANT'S JUMPSEAT DOES NOT TEST MOST TIMES; WHEN DOES LIGHT IS RED.<[01] R/R'D AFT R/H O/B EMERG FLASHLIGHT BATTERY PACK & RESEAL - [SDR SWAA2024121979440](https://openairdocs.org/sdr/SWAA2024121979440), Dec 19, 2024: SLIDE. OUT OF ADJUST. REF PREV LOG PAGE 2380351 'FORWARD ENTRY SLIDE FELL OUT OF CONTAINER'<[01] REMOVED FORWARD ENTRY DOOR SLIDE; FOUND SLIDE LATCH ASSY BROKEN. REF AMM 25-66-01 (MT - [SDR SWAA2024121979439](https://openairdocs.org/sdr/SWAA2024121979439), Dec 18, 2024: SLIDE. OUT OF ADJUST. FWD ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] COMPLIED WITH W/O 89269033
01 - REMOVED AND REPLACED PER [AMM 25-66-01-401-NG (DOOR-MOUNTED ESCAPE SYSTEM - R - [SDR SWAA2024082026422](https://openairdocs.org/sdr/SWAA2024082026422), Aug 16, 2024: BULB. INOPERATIVE. F.S.D. EMERGENCY EXIT FWD LIGHT HAS SEVERAL INOP BULBS<[01] RELAMPED THE F.S.D. EMERGENCY EXIT FWD LIGHT AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33- - [SDR SWAA2024081525679](https://openairdocs.org/sdr/SWAA2024081525679), Aug 14, 2024: BATTERY PACK. INOPERATIVE. INOP EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1676.<[01] REMOVED; REPLACED; AND PERFORMED A GOOD TEST AT BATTERY PACK M1676 IAW AMM 33-51-06-960-805.;[02] - [SDR SWAA2024081525680](https://openairdocs.org/sdr/SWAA2024081525680), Aug 14, 2024: BATTERY PACK. INOPERATIVE. INOP EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M2335.<[01] REMOVED; REPLACED; AND PERFORMED A GOOD TEST AT BATTERY PACK M2335 IAW AMM 33-51-06-960-805.;[02] - [SDR SWAA2024081525681](https://openairdocs.org/sdr/SWAA2024081525681), Aug 14, 2024: BATTERY PACK. INOPERATIVE. INOP EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1672.<[01] REMOVED; REPLACED; AND PERFORMED A GOOD TEST AT BATTERY PACK M1672 IAW AMM 33-51-06-960-805.;[02] - [SDR SWAA2024081921932](https://openairdocs.org/sdr/SWAA2024081921932), Jul 26, 2024: PANEL. CRACKED. ASD PANEL 844DZ IS CRACKED<[01] REMOVED GIRT BAR SEAL FROM PANEL 844DZ AND INSTALLED ON NEW PANEL 844DZ IAW SOPM 20-50-01 TORQUE REQUIREMENTS ACCOMPLISHED USING - [SDR SWAA2024081617891](https://openairdocs.org/sdr/SWAA2024081617891), Jul 26, 2024: SUPPORT. CRACKED. AED SURROUND STRUCTURE SUPPORT CLIP AT STGR 7L STA 1006 CRACKED. (MARKED)<[01] UPDATED 3 MEASUREMENTS;[02] REMOVED AND REPLACED AED SURROUND STRUCTURE SUPPORT C - [SDR SWAA2024081517889](https://openairdocs.org/sdr/SWAA2024081517889), Jul 26, 2024: ISOLATOR. DAMAGED. AFT SERVICE DOOR HAS 1 EA DAMAGED ISOLATOR AT BOTTOM AFT CORNER (MARKED).<[01] REMOVED AND REPLACED BOTH FWD AND AFT ASD BOTTOM CORNER ISOLATORS PER SRM 51-40-0 - [SDR SWAA2024081517191](https://openairdocs.org/sdr/SWAA2024081517191), Jul 26, 2024: ANGLE. CORRODED. CORROSION ON AFT CARGO BAY INTERCOSTAL ANGLE UNDER SHIELD BS 767+2 RBL 22 WL 156<[01] EVALUATED CORROSION ON INTERCOSTAL ANGLE BS 767+2 RBL 22 WL 156; FOUND TO - [SDR SWAA2024081517192](https://openairdocs.org/sdr/SWAA2024081517192), Jul 26, 2024: WEB. CORRODED. CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB BS 787+12 TO BS 827+4 RBL 28 WL 155<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 8 - [SDR SWAA2024081417190](https://openairdocs.org/sdr/SWAA2024081417190), Jul 26, 2024: SHIELD. CORRODED. CORROSION ON AFT CARGO BAY SHIELD BS 767+11 TO BS 767+16 RBL 22 WL 156<[01] EVALUATED CORROSION ON SHIELD BS 767+11 TO BS 767+16 RBL 22 WL 156; FOUND TO BE OUT - [SDR SWAA2024081317897](https://openairdocs.org/sdr/SWAA2024081317897), Jul 26, 2024: FLOORBEAM. CORRODED. CORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 947 LBL 50; LBL 25; RBL 25 CORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 947 LBL 50 LBL 25 RBL 25 WL208<[01] REMOV - [SDR SWAA2024081616408](https://openairdocs.org/sdr/SWAA2024081616408), Jul 25, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STRUCTURE AROUND FITTING BS 947.5; LBL 50<[01] REMOVED DAMAGED ON FLOOR SUPPORT (INTERCOSTAL) AT BS 947.5 LBL 50 WL 208 IN AN AREA OF - [SDR SWAA2024081616406](https://openairdocs.org/sdr/SWAA2024081616406), Jul 25, 2024: FLOORBEAM. CORRODED. SIGN OF CORROSION ON FLOORBEAM STRUCTURE AROUND FITTING BS 947.5; RBL 50<[01] CORROSION WAS FOUND TO BE ON FLOORBEAM BS 947.5 RBL 50 UPPER SURFACE. ALL DIMENSIO - [SDR SWAA2024081616409](https://openairdocs.org/sdr/SWAA2024081616409), Jul 25, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM STRUCTURE AROUND FITTING BS 947.5; RBL 25<[01] CORROSION WAS FOUND TO BE ON FLOORBEAM BS 947.5 RBL 25 UPPER SURFACE. ALL DIMENSIONS WILL - [SDR SWAA2024081617177](https://openairdocs.org/sdr/SWAA2024081617177), Jul 25, 2024: SUPPORT. CRACKED. BREAKER PANEL CRACKED AT BS 540 LBL1 WL 208.<[01] REMOVED AND REPLACED CRACKED BREAKER PANEL BS 540; LBL 1; WL 208 IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLAC - [SDR SWAA2024081617178](https://openairdocs.org/sdr/SWAA2024081617178), Jul 25, 2024: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT AT BS 396 LBL12 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 396 LBL 12 WL208 IAW SRM 51-40-02; BOEING DWG 143A5400 ID: 0184 REV: - - [SDR SWAA2024081617179](https://openairdocs.org/sdr/SWAA2024081617179), Jul 25, 2024: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT AT BS 390 LBL52 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 390 LBL 52 WL208 IAW SRM 51-40-02; BOEING DWG 143A5400 ID:0183 REV: - - [SDR SWAA2024081617180](https://openairdocs.org/sdr/SWAA2024081617180), Jul 25, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT AT BS 317 RBL11 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 312-328 RBL 11 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A54 - [SDR SWAA2024081617181](https://openairdocs.org/sdr/SWAA2024081617181), Jul 25, 2024: PLATE. CORRODED. CORROSION ON FED MOPSILL AROUND AFT GRIT BAR FITTING PLATE AT BS 345 LBL59 WL208<[01] EVALUATED CORROSION ON FED MOPSILL AROUND AFT GRIT BAR FITTING PLATE AT BS - [SDR SWAA2024081617189](https://openairdocs.org/sdr/SWAA2024081617189), Jul 25, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM AT FWD WET AREA BS328 RBL54; RBL55 WL208. MARKED<[01] REPAIRED DAMAGED ON FLOOR BEAM AT FWD WET AREA BS 328 RBL 54 RBL 55 WL 208 IAW SRM - [SDR SWAA2024081517182](https://openairdocs.org/sdr/SWAA2024081517182), Jul 25, 2024: ANGLE. CORRODED. CORROSION ON FED MOPSILL SCUFF PLATE ATTACH ANGLE BS 318; 338; 339 LBL60 WL208<[01] EVALUATED CORROSION ON FED MOPSILL SCUFF PLATE ATTACH ANGLE BS 318; 338; 339 - [SDR SWAA2024081517183](https://openairdocs.org/sdr/SWAA2024081517183), Jul 25, 2024: ANGLE. CORRODED. CORROSION ON FSD MOPSILL SCUFF PLATE ATTACH ANGLE AT BS 322 AND 331 RBL 59 WL208<[01] COMPLETED MEASURMENT TABLE;[02] DAMAGE OUT OF LIMITS PER SRM 53-10-15-1A-2 - [SDR SWAA2024081417184](https://openairdocs.org/sdr/SWAA2024081417184), Jul 25, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241GF HAS UPPER SURFACE DELAMINATION.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL; USING BMS - [SDR SWAA2024081417187](https://openairdocs.org/sdr/SWAA2024081417187), Jul 25, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 231GF HAS UPPER SURFACE DELAMINATION<[01] REMOVED AND REPLACED FLOOR PANEL 231GF PER AMM 53-21-00-400-801;[02] CORRECTED MEASUREMENT - [SDR SWAA2024081316400](https://openairdocs.org/sdr/SWAA2024081316400), Jul 25, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241D UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] AFT FLOOR PANEL 241D UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] JOB COMPLET - [SDR SWAA2024081316391](https://openairdocs.org/sdr/SWAA2024081316391), Jul 25, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221BF HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] 221BF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG - [SDR SWAA2024081316393](https://openairdocs.org/sdr/SWAA2024081316393), Jul 25, 2024: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221DF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] 221DF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND All 93: https://openairdocs.org/aircraft/N8699A/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 ## 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.