# N8693A: 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: 36921 - Year built: 2016 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 28, 2016 - Certificate issued: September 8, 2016 - Expires: September 30, 2029 - Mode S code: ABF308 - 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=8693A - Page: https://openairdocs.org/aircraft/N8693A 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 (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA18CA209](https://openairdocs.org/ntsb/DCA18CA209), Jun 12, 2018: Boeing 737-8H4 (N8693A), Phoenix, AZ, no damage. Probable cause: a passenger bumping into a flight attendant who was holding a hot liquid. ## FAA accident and incident reports None matched to N8693A. ## Service difficulty reports (87, 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 SWAA2026081972945](https://openairdocs.org/sdr/SWAA2026081972945), Aug 15, 2026: HANDLE. LOOSE. LOOSE DOOR HANDLE ON AFT ENTRY DOOR. TIGHTENED ASD FWD DOOR ASSIST HANDLE IAW AMM 52-13-31-400-802 SECTION 3.G. - [SDR SWAA2026081996875](https://openairdocs.org/sdr/SWAA2026081996875), Aug 15, 2026: HANDLE. LOOSE. LOOSEN TWO DOOR HANDLES AT FWD ENTRY DOOR ON THE DOOR AND ON AFT DOOR LINER TIGHTENED DOOR HANDLES AT FWD ENTRY DOOR ON THE DOOR AND ON AFT DOOR LINER IAW AMM 5 - [SDR SWAA2026081828741](https://openairdocs.org/sdr/SWAA2026081828741), Aug 13, 2026: FUSE. INOPERATIVE. FWD OVERWING LH/RH EXIT LOCATOR SIGNS INOP REPLACED FUSE FOR FWD OVERWING LH/RH EXIT LOCATOR SIGNS IAW AMM 33-51-06-960-804. REPLACED FUSE AND PERFORMED GOOD OP - [SDR SWAA2026081839947](https://openairdocs.org/sdr/SWAA2026081839947), Aug 13, 2026: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHTS RIGHT AFT OWE AND RIGHT FUSELAGE JUST AFT OF FLAPS ARE INOP RELAMPED EXTERIOR EMERGENCY LIGHTS RIGHT AFT OWE AND RIGHT FUSELAGE JUST A - [SDR SWAA2026081868995](https://openairdocs.org/sdr/SWAA2026081868995), Aug 12, 2026: SWITCH. DISCONNECTED. EMERGENCY EXIT LIGHT INTEGRATED SWITCH ASSY DOES NOT OPERATE UPON FURTHER INVESTIGATION FOUND PIN 31 RECESSED ON D14372 INSERTED CONTACT INTO PIN 31 FULLY PER S - [SDR SWAA2026081987670](https://openairdocs.org/sdr/SWAA2026081987670), Aug 5, 2026: MEGAPHONE. DAMAGED. PORTABLE SAFETY MEGAPHONE DAMAGED WHILE REMOVING FROM G2 GALLEY. REMOVED AND REPLACED PORTABLE SAFETY MEGAPHONE IN G2 GALLEY IAW AMM INTRO SIP AND SWA DWG 25600 - [SDR SWAA2026081919226](https://openairdocs.org/sdr/SWAA2026081919226), Aug 4, 2026: SWITCH. INOPERATIVE. FUNCTIONAL CHECK, ALL EMERGENCY LIGHTS, OUTGOING, PERFORMED A GOOD OPS TEST OF ALL EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. FOUND EMERGENCY EXIT LIGHT INTEGRA - [SDR SWAA2026072442868](https://openairdocs.org/sdr/SWAA2026072442868), Jul 20, 2026: FLASHLIGHT. INOPERATIVE. ONE FWD FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD F/A OTBD FLASHLIGHT AMM 25-64-00-200-802-NG-01. - [SDR SWAA2026052105198](https://openairdocs.org/sdr/SWAA2026052105198), May 20, 2026: FLASHLIGHT. NO DISCREPANCY. FA FLASHLIGHT AFT FO SIDE HOUSING LIGHT IS NOT ILLUMINATING. OPS CHECK NORMAL IAW SIP. NO FURTHER ACTION REQUIRED. - [SDR SWAA2026042090459](https://openairdocs.org/sdr/SWAA2026042090459), Apr 17, 2026: FLASHLIGHT. INOPERATIVE. AFT FA FLASHLIGHT BATTERY DEAD. R & R AFTER FA FLASLIGHT & BATTERY IAW AMM 25-64-00. - [SDR SWAA2026042091113](https://openairdocs.org/sdr/SWAA2026042091113), Apr 17, 2026: BATTERY. INOPERATIVE. AFT FA FLASHLIGHT BATTERY DEAD. R & R AFTER FA FLASLIGHT & BATTERY REF AMM 25-64-00. - [SDR SWAA2026010959376](https://openairdocs.org/sdr/SWAA2026010959376), Jan 8, 2026: RETAINER. LOOSE. FWD ENTRY DOOR AFT GIRT BAR RETAINER CLIP LOOSE. REMOVED AND REPLACED RIVET AT FE DOOR AFT GIRT BAR RETAINER CLIP IAW SRM 51-40-02. - [SDR SWAA2025121953349](https://openairdocs.org/sdr/SWAA2025121953349), Dec 17, 2025: LENS. MISSING. EXIT SIGN COVER AT FWD SERVICE DOOR MISSING. INSTALLED THE LENS IAW AMM 33-51-01. - [SDR SWAA2025090309810](https://openairdocs.org/sdr/SWAA2025090309810), Aug 30, 2025: FLASHLIGHT. INOPERATIVE. FWD AND AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHTS INOP. R&R FWD AND AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT BATTERIES PER CMM 25-60-02. - [SDR SWAA2025081504794](https://openairdocs.org/sdr/SWAA2025081504794), Aug 14, 2025: FLASHLIGHT. NO TEST. OUTBOARD FLASHLIGHT WONT TEST. R & R THE BATTERY TO FWD OTBD FLASHLIGHT IAW SIP, OPS CHECKED GOOD. - [SDR SWAA2025081199183](https://openairdocs.org/sdr/SWAA2025081199183), Aug 7, 2025: SILL DRAIN. ODOR. TERRIBLE SMELL COMING FROM AFT GALLEY FLOOR DRAINS<[01] CLEANED AND FLUSHED AFT ENTRY AND AFT SERVICE DOOR SILL DRAINS REF AMM 38-31-00 - [SDR SWAA2025072494944](https://openairdocs.org/sdr/SWAA2025072494944), Jul 24, 2025: BATTERY. INOPERATIVE. F/A FWD EMERGENCY FLASHLIGHT, LEFT SIDE WILL NOT TEST. R & R THE BATTERY IAW AMM 25-64-00. - [SDR SWAA2025071788824](https://openairdocs.org/sdr/SWAA2025071788824), Jul 7, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT RT BATTERY PACK AT BS 565 IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK AT BS 565 IAW MM 33-51-06. CABIN EMERGENCY LIGHTS OPS CHECKED GOOD - [SDR SWAA2025071784707](https://openairdocs.org/sdr/SWAA2025071784707), Jun 24, 2025: ATTACH ANGLE. CRACKED. LEFT WING TRAILING EDGE; ATTACH ANGLE FROM DEFLECTION CONTROL RIB TO INTERCOSTAL WEB IS CRACKED. REMOVED CRACKED ANGLE PER SRM 51-40-02.;[02] ANGLE HAS BEEN REM - [SDR SWAA2025071784706](https://openairdocs.org/sdr/SWAA2025071784706), Jun 24, 2025: INTERCOSTAL. CRACKED. L/H WING TRAILING EDGE; INTERCOSTAL WEB INBD OF DEFLECTION CONTROL RIB IS CRACKED. REMOVED AND REPLACED INTERCOSTAL WEB PER SRM 51-40-02. - [SDR SWAA2025071784705](https://openairdocs.org/sdr/SWAA2025071784705), Jun 24, 2025: ANGLE. CRACKED. L/H WING TRAILING EDGE; ANGLE INBD OF INTERCOSTAL WEB AT DEFLECTION CONTROL RIB IS CRACKED. REMOVED CRACKED ANGLE INBD OF INTERCOSTAL WEB PER SRM 51-40-02. CRAC - [SDR SWAA2025071684592](https://openairdocs.org/sdr/SWAA2025071684592), Jun 23, 2025: ATTACH ANGLE. CRACKED. R/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT RBL 34. FABRICATED & MATCH DRILLED REPAIR PARTS PER SRM 57-10-10-2R-5. INITIAL AREA AND FASTENER HOLES RE - [SDR SWAA2025071684698](https://openairdocs.org/sdr/SWAA2025071684698), Jun 23, 2025: ATTACH ANGLE. CRACKED. CRACK FOUND AT L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE LBL 9. CUT OUT AND REMOVED BS 663 ATTACH ANGLE FROM APPROX LBL 18-LBL 5. ALL WORK DONE IAW SRM 57-10- - [SDR SWAA2025071783852](https://openairdocs.org/sdr/SWAA2025071783852), Jun 20, 2025: PANEL. PULLED. LH WING TRAILING EDGE PANEL 561BB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. ACCOMPLISHED REPAIR T - [SDR SWAA2025071783857](https://openairdocs.org/sdr/SWAA2025071783857), Jun 20, 2025: PANEL. DAMAGED. LH WING TRAILING EDGE PANEL 561AB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND AC - [SDR SWAA2025071783858](https://openairdocs.org/sdr/SWAA2025071783858), Jun 20, 2025: PANEL. PULLED. LH WING TRAILING EDGE PANEL 561CB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND AC - [SDR SWAA2024083031016](https://openairdocs.org/sdr/SWAA2024083031016), Aug 27, 2024: GIRT BAR. OUT OF ADJUST. FAS REPORT FWD ENTRY EMERG SLIDE GIRT BAR DIFFICULT TO ARM /INSERT INTO FLOOR RECEPTACLE<[01] ADJUSTED FWD ENTRY DOOR EMERGENCY SLIDE IAW AMM 25-66-01; OPS CHEC - [SDR SWAA2024081926825](https://openairdocs.org/sdr/SWAA2024081926825), Aug 16, 2024: FLASHLIGHT. INOPERATIVE. FWD GALLEY FLIGHT ATT FLASHLIGHT INOP FWD GALLEY FLIGHT ATT FLASHLIGHT INOP< - [SDR SWAA2024052989297](https://openairdocs.org/sdr/SWAA2024052989297), May 24, 2024: BATTERY PACK. INOPERATIVE. CABIN EMERGENCY LIGHT BATTERY PACK M2335 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M2335 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CA - [SDR SWAA2024052989293](https://openairdocs.org/sdr/SWAA2024052989293), May 23, 2024: BATTERY PACK. INOPERATIVE. CABIN EMERGENCY LIGHT BATTERY PACK M1694 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY M1694 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERI - [SDR SWAA2024052989294](https://openairdocs.org/sdr/SWAA2024052989294), May 23, 2024: BATTERY PACK. INOPERATIVE. CABIN EMERGENCY LIGHT BATTERY PACK M1675 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1675 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CA - [SDR SWAA2024052989295](https://openairdocs.org/sdr/SWAA2024052989295), May 23, 2024: BATTERY PACK. INOPERATIVE. CABIN EMERGENCY LIGHT BATTERY PACK M1676 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1676 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CA - [SDR SWAA2024053188344](https://openairdocs.org/sdr/SWAA2024053188344), May 21, 2024: WEB. CRACKED. R/H WING VERTICAL WEB LOCATED JUST INBOARD OF DEFLECTION RIB AT WS 278.5 IS CRACKED AT OUTBOARD HOLE.<[01] REMOVED CRACKED VERTICAL WEB PER SRM 51-40-02. DRILLE - [SDR SWAA2024053087383](https://openairdocs.org/sdr/SWAA2024053087383), May 18, 2024: FITTING. CRACKED. FWD CARGO AFT CORNER THRESHOLD FITTING IS CRACKED<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVAL/INSTALLATION - PERMA - [SDR SWAA2024053085707](https://openairdocs.org/sdr/SWAA2024053085707), May 14, 2024: SKIN. DELAMINATED. L/H O/B AFT FLAP HAS DELAMINATION AT I/B LOWER CORNER LOWER SURFACE.<[01] REMOVED L/H O/B AFT FLAP ASSY. REF AMM 27-51-22;[02] INSTALLED L/H O/B AFT FLAP. REF A - [SDR SWAA2024060384930](https://openairdocs.org/sdr/SWAA2024060384930), May 11, 2024: FUEL PANEL. CORRODED. FUELING STATION PANEL AT 621GB HAS SURFACE CORROSION.<[01] REMOVED AND REPLACED FUELING PANEL PER SOPM 20-50-01 AND MM 28-41-61;[02] VERIFIED. REMOVED AND REPLA - [SDR SWAA2024053183039](https://openairdocs.org/sdr/SWAA2024053183039), May 6, 2024: FLOORBEAM. CORRODED. AFT R/H LAV; O/B AFT FLOOR MOUNT AT STA 947 HAS AREA OF SURFACE CORROSION IN FLOOR BEAM. REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF L - [SDR SWAA2024053083040](https://openairdocs.org/sdr/SWAA2024053083040), May 6, 2024: MOUNT. CORRODED. AFT R/H LAV; O/B AFT MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION ON INTERCOSTAL. (MARKED)<[01] PRIOR TO BLENDING; DEPTH OF CORROSION IS .092'. REMAINING THI - [SDR SWAA2024053083245](https://openairdocs.org/sdr/SWAA2024053083245), May 6, 2024: FLOOR SUPPORT. CORRODED. INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 24 HAS SURFACE CORROSION.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SR - [SDR SWAA2024053182762](https://openairdocs.org/sdr/SWAA2024053182762), May 5, 2024: FLOORBEAM. CORRODED. AFT GALLEY FLOOR STRUCTURE WET AREA AT STA 986.5 APPROXIMATELY 18' I/B OF AFT SERVICE DOOR OPENING HAS SMALL AREA OF SURFACE CORROSION ON FLOOR BEAM FASTENER HO - [SDR SWAA2024053182761](https://openairdocs.org/sdr/SWAA2024053182761), May 5, 2024: MOUNT. CORRODED. AFT L/H LAV; O/B AFT FLOOR MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02. DAMAGE REMOVAL .041' OUT OF LIMITS PER SRM 53-70 - [SDR SWAA2024053082769](https://openairdocs.org/sdr/SWAA2024053082769), May 5, 2024: STRINGER CLIP. CRACKED. FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT FRAME RIVETS; STA 500I STR 25L.<[01] REMOVED DAMAGED STRINGER CLIP REF SRM 51-40-02.;[02] REMOVED L - [SDR SWAA2024053082770](https://openairdocs.org/sdr/SWAA2024053082770), May 5, 2024: STRINGER CLIP. CRACKED. FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT FRAME RIVETS; STA 500I STR 25R.<[01] REMOVED RH SIDE PLATE BAFFLE AND BULKHEAD LOWER CHORD TO FOM P - [SDR SWAA2024053082760](https://openairdocs.org/sdr/SWAA2024053082760), May 5, 2024: MOUNT. CORRODED. AFT GALLEY L/H FWD FLOOR MOUNT HAS POSSIBLE LIGHT CORROSION PRESENT AROUND LOWER O/B EDGE. REMOVED DAMAGE PER SRM 51-10-02. DAMAGE FOUND TO BE OUT OF LIMITS PER - [SDR SWAA2024053082765](https://openairdocs.org/sdr/SWAA2024053082765), May 5, 2024: MOUNT. CORRODED. AFT R/H LAV; I/B AFT FLOOR MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION. (MARKED)<[01] REMOVED AFT R/H LAV; I/B AFT FLOOR MOUNT AT STA 947 IAW SRM 51-40-02;[ - [SDR SWAA2024053082766](https://openairdocs.org/sdr/SWAA2024053082766), May 5, 2024: FLOOR SUPPORT. CORRODED. AFT GALLEY FLOOR STRUCTURE SUPPORT ANGLE AT STA 986.5 +8' APPROXIMATELY 12' I/B OF AFT SERVICE DOOR OPENING HAS SMALL AREA OF SURFACE CORROSION ON FASTENER HOLE - [SDR SWAA2024053182344](https://openairdocs.org/sdr/SWAA2024053182344), May 4, 2024: ANGLE. CORRODED. FWD CARGO STA 500D TO 500E AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES.<[01] BLENDED AREAS; REMOVED .010' MATERIAL; FOUND TO BE OUT OF - [SDR SWAA2024053182349](https://openairdocs.org/sdr/SWAA2024053182349), May 4, 2024: ANGLE. CORRODED. FWD CARGO STA 500E TO 500F AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES. BLENDED AREAS; REMOVED .023' MATERIAL; FOUND TO BE OUT OF LIMI - [SDR SWAA2024053189291](https://openairdocs.org/sdr/SWAA2024053189291), May 4, 2024: RIB. WORN. RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB IS WORN AT 2 FASTENER HOLES. TRIMMED OFF DAMAGED UPPER TAB FROM DEFLECTION CONTROL RIB IAW SRM 51-10-02 AND SRM - [SDR SWAA2024053182601](https://openairdocs.org/sdr/SWAA2024053182601), May 4, 2024: WEB. CORRODED. AFT CARGO THRESHOLD WEB HAS CORROSION IN AND AROUND NUTPLATE HOLES AT NUMEROUS LOCATIONS. REMOVED SURFACE CORROSION AROUND DISCREPANT NUTPLATE HOLE LOCATIONS PE All 87: https://openairdocs.org/aircraft/N8693A/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 N8693A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8693A before. - [Cancelled 1971-07-15](https://openairdocs.org/deregistered/N8693A-1971-07-15): Beech B35, S/N D-2238, built 1950. Owner: [Wilson Mill & Cabinet Co](https://openairdocs.org/faa-owner/WILSON%20MILL%20%26%20CABINET%20CO), [Santa Ana, CA](https://openairdocs.org/faa-place/CA/Santa%20Ana) ## 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.