# N8690A: 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: 36916 - Year built: 2016 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 17, 2016 - Certificate issued: August 11, 2016 - Expires: August 31, 2029 - Mode S code: ABF29F - 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=8690A - Page: https://openairdocs.org/aircraft/N8690A 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 N8690A. ## FAA accident and incident reports None matched to N8690A. ## Service difficulty reports (91, 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 SWAA2026072106335](https://openairdocs.org/sdr/SWAA2026072106335), Jul 17, 2026: LIGHT. INOPERATIVE. CAPT. SIDE OWING EMER EXIT DOOR LIGHT INOP AFT DOOR_ OK TO CONT PER MEL 33-2-04 SP1B AUTH 329716. REPLACED LED LIGHT ASY IAW AMM 33-51-01. OPS CHKD GOOD. PLACAR - [SDR SWAA2026050494082](https://openairdocs.org/sdr/SWAA2026050494082), Apr 30, 2026: GIRT BAR. OUT OF ADJUST. AFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT (HOOK AND LOOP NOT SECURED) REMOVED, SECURED GIRT BAR HOOK AND LOOP, AND REINSTALLED IAW AMM 25-66-01. MT 725-61-0 - [SDR SWAA2026040987582](https://openairdocs.org/sdr/SWAA2026040987582), Apr 8, 2026: FLASHLIGHT. FAILED. RIGHT AFTER INBD FLASHLIGHTS DOES NOT TEST<[01] OK TO. CONT PER MEL 25-12-01 SP 1B C/W AUTHORIZATION 314060;[02] PERFORMED FUNCTIONAL TEST OF RIGHT AFT INBD FLA - [SDR SWAA2026031177487](https://openairdocs.org/sdr/SWAA2026031177487), Mar 7, 2026: FLASHLIGHT. NO TEST. FWD GALLEY EMERGENCY FLASHLIGHT DOES NOT TEST. REPOSTIONED FLASHLIGHT PER S. I P - [SDR SWAA2026011260097](https://openairdocs.org/sdr/SWAA2026011260097), Jan 10, 2026: ENGINE. BIRD INGESTION. POSSIBLE BIRDSTRIKE ON TAKEOFF SMELL OF SMOKE IN CABIN AND COCKPIT ALL ENGINE INDICATIONS NORMAL. COMPLIED WITH ODOR AND SMOKE CHECK IN CABIN AND COCKPIT PER HM - [SDR SWAA2025103029626](https://openairdocs.org/sdr/SWAA2025103029626), Oct 29, 2025: BATTERY PACK. NO TEST. THE LT EMERGENCY LIGHTING BATTERY PACK AT ROW 20 FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06. - [SDR SWAA2025071089669](https://openairdocs.org/sdr/SWAA2025071089669), Jul 8, 2025: COFFEEMAKER. ODOR. FO SIDE AFT COFFEE MAKER FA REPORTS BURNING SMELL WHEN ON SMELL GOES AWAY WHEN TURNED OFF<[01] R&R F/O SIDE AFT COFFEE MAKER PER AMM 25-30-01 - [SDR SWAA2025060276501](https://openairdocs.org/sdr/SWAA2025060276501), May 30, 2025: COMPENSATOR. FAULTY. AT CRUISE NOTICED #1 FUEL TANK DECREASING RAPIDLY (1200 LB IMBALANCE). DIVERTED TO PSP. NOTICED 2 UNITS LEFT AILERON TRIM. NO OVERWEIGHT LANDING. ON POST FLIGHT - [SDR SWAA2025052774706](https://openairdocs.org/sdr/SWAA2025052774706), May 24, 2025: FLASHLIGHT ASSY. MALFUNCTIONED. FWD GALLEY FLASHLIGHT INOP. INSPECTED PER AMM 25-64-00-200-802-NG-01, FLASHLIGHT CHECK WITH FLASHING OR PUSH TO TEST, LED INDICATOR. FOUND NORMAL. - [SDR SWAA2025052774059](https://openairdocs.org/sdr/SWAA2025052774059), May 22, 2025: COVER. DAMAGED. AFT R/H DOOR ESCAPE SLIDE COVER IS DENTED AT FWD UPPER CORNER<[01] REMOVED DAMAGED ESCAPE SLIDE COVER AND INSTALLED SERVICEABLE COVER PER AMM 25-66-01 AND MT 72 - [SDR SWAA2025052772146](https://openairdocs.org/sdr/SWAA2025052772146), May 18, 2025: BATTERY PACK. INOPERATIVE. ALL ASSOCIATED LIGHTS FOR EMERGENCY BATTERY PACK M1670 IS INOP<[01] AFTER DEEP CYCLE CHARGE FOUND ALL ASSOCIATED LIGHTS FOR EMERGENCY BATTERY PACK M1670 TESTED - [SDR SWAA2025052771085](https://openairdocs.org/sdr/SWAA2025052771085), May 14, 2025: SEAL. CRACKED. LT. HORIZONTAL STAB L/E UPPER FWD SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB SLIDE SEAL IAW AMM 53-31-31/401;[02] TASK C/W - [SDR SWAA2025052771084](https://openairdocs.org/sdr/SWAA2025052771084), May 14, 2025: SEAL. CRACKED. RT. HORIZONTAL STAB L/E FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB SLIDE SEAL IAW AMM 53-31-31/401;[02] TASK C/W - [SDR SWAA2025052770750](https://openairdocs.org/sdr/SWAA2025052770750), May 13, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241AF HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-0 - [SDR SWAA2025052770755](https://openairdocs.org/sdr/SWAA2025052770755), May 13, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232SF HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232SF WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025052770134](https://openairdocs.org/sdr/SWAA2025052770134), May 13, 2025: FLOORBEAM. CRACKED. 540 BREAK PANEL IS CRACKED AT RBL 1; WL 208.<[01] REMOVED AND REPLACED BS-540 BREAK PANEL RBL-1 TO RBL-25; WL-208 IAW SRM 51-40-02-0G-0 AND DWG#143A5240 - [SDR SWAA2025052770135](https://openairdocs.org/sdr/SWAA2025052770135), May 13, 2025: FLOORBEAM. CRACKED. 540 BREAK PANEL IS CRACKED AT LBL 1; WL 208.<[01] REMOVED AND REPLACED BS-540 BREAK PANEL LBL-1 TOLBL-25; WL-208 IAW SRM 51-40-02-0G-0 AND DWG#143A5240 - [SDR SWAA2025052770756](https://openairdocs.org/sdr/SWAA2025052770756), May 13, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241CF HAS AREAS OF PULLED STRANDS. CORRECT PANEL NUMBER IS 241EF.<[01] FLOOR PANEL 241EF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABR - [SDR SWAA2025052770865](https://openairdocs.org/sdr/SWAA2025052770865), May 13, 2025: PANEL. CRACKED. LT WING TRAILING EDGE SPANWISE PANEL BETWEEN SPOILER PANELS 5 AND 6 CRACKED IN UPPER RADIUS. (PN 115A2512-29)<[01] REMOVED AND REPLACED ANGLE P/N 115A2156-7 IAW - [SDR SWAA2025032408177](https://openairdocs.org/sdr/SWAA2025032408177), Mar 20, 2025: FLASHLIGHT. INOPERATIVE. FA FWD JUMP SEAT FLASHLIGHT INOP <[01]. RESEATED FWD FA FLASHLIGHT IN CRADLE PER SIP. OPS CHECKS GOOD. - [SDR SWAA2025011686657](https://openairdocs.org/sdr/SWAA2025011686657), Jan 16, 2025: LAMP. INOPERATIVE. L2 EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED L2 EMERGENCY EXIT LIGHT. OPS CHECK GOOD. ALL WORK PERFORMED PER AMM 33-51-04. - [SDR SWAA2025010382394](https://openairdocs.org/sdr/SWAA2025010382394), Jan 1, 2025: LIGHT. BROKEN. FWD EMERGENCY FO SIDE LIGHT ASSEMBLY BROKEN<[01] R&R EMERGENCY EXIT LIGHT ASSEMBLY OVER WING RH FWD SIDEWALL. OPS CK GOOD PER AMM 33-51-01. - [SDR SWAA2024091637771](https://openairdocs.org/sdr/SWAA2024091637771), Sep 14, 2024: TRIM MOTOR. FAULTY. STABILIZER TRIM INOP<[01] T/S PER FIM 22-15 TASK 821. CYCLED C/B & FAULT WAS INTERMITTENT. PER MOC REQUEST; R&R STAB TRIM MOTOR PER AMM 27-41-71. OPS CHECK GOOD - [SDR SWAA2024090333182](https://openairdocs.org/sdr/SWAA2024090333182), Aug 30, 2024: BATTERY. INOPERATIVE. FLIGHT ATTENDANT FORWARD FLASHLIGHT INOP<[01] OK FOR CONTINUE SERVICE PERMEL 25-12-01 SP1B;[02] REMOVED AND REPLACED BATTERY FOR FA FWD FLASHLIGHT PER AMM 25-64 - [SDR SWAA2024061301239](https://openairdocs.org/sdr/SWAA2024061301239), Jun 12, 2024: FLASHLIGHT. FAILED. FLIGHT ATTENDANT FORWARD JUMPSEAT FLASHLIGHT PRESS TO TEST BUTTON NOT WORKING.<[01] PROPERLY POSITIONED FLASHLIGHT IN HOLDER AND OPS CK GOOD PER AMM 25-64-00. - [SDR SWAA2024060698227](https://openairdocs.org/sdr/SWAA2024060698227), Jun 4, 2024: BATTERY PACK. INOPERATIVE. FWD O/W EMERGENCY EXIT LIGHTS INOP ON LEFT SIDE<[01] REPLACED EMERGENCY BATTERIES PACK; M1675 PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECT - [SDR SWAA2024060698229](https://openairdocs.org/sdr/SWAA2024060698229), Jun 4, 2024: BATTERY PACK. INOPERATIVE. CEILING EMERGENCY EXIT LIGHTS; SEVERAL LIGHTS INOP.<[01] REPLACED EMERGENCY BATTERIES PACK; M1672; M1673; PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERI - [SDR SWAA2024060698842](https://openairdocs.org/sdr/SWAA2024060698842), Jun 4, 2024: BATTERY PACK. INOPERATIVE. CEILING EMERGENCY EXIT LIGHTS; SEVERAL LIGHTS INOP.<[01] REPLACED EMERGENCY BATTERIES PACK; M1672; M1673; PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERI - [SDR SWAA2024060698228](https://openairdocs.org/sdr/SWAA2024060698228), Jun 4, 2024: BATTERY PACK. INOPERATIVE. O/W FWD AND AFT EMERGENCY EXIT LIGHTS INOP ON RT SIDE<[01] REPLACED EMERGENCY BATTERIES PACK; M1674; PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERIFIED - [SDR SWAA2024060697838](https://openairdocs.org/sdr/SWAA2024060697838), Jun 3, 2024: CONNECTOR. DISCONNECTED. DURING FWD CABIN RESTORATION; FOUND FWD GALLEY DOORWAY EMERGENCY EXIT SIGNS; UPPER AND LOWER; INOP.<[01] FOUND CONNECTOR D14812 NOT PROPERLY SEATED. RE-SEATED C - [SDR SWAA2024060684064](https://openairdocs.org/sdr/SWAA2024060684064), May 9, 2024: FLOORBEAM. DAMAGED. ELONGATED HOLE IN FWD FLANGE OF BS 887 FLOOR BEAM; RBL 4; WL 208. DAMAGE WAS FOUND TO A FLOOR PANEL ATTACH HOLE IN THE FWD FLANGE OF THE BS 887 FLOOR BEAM (146A - [SDR SWAA2024060683900](https://openairdocs.org/sdr/SWAA2024060683900), May 9, 2024: FLOORBEAM. CORRODED. CORROSION AROUND FITTING ON FLOOR BEAM BS 947; RBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947 RBL 50 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THIC - [SDR SWAA2024060683901](https://openairdocs.org/sdr/SWAA2024060683901), May 9, 2024: FLOORBEAM. CORRODED. CORROSION AROUND FITTING ON FLOOR BEAM BS 947; LBL 25 (MARKED)<[01] REMOVED DAMAGE ON BS 947 LBL 25 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THIC - [SDR SWAA2024060683904](https://openairdocs.org/sdr/SWAA2024060683904), May 9, 2024: FLOORBEAM. CORRODED. CORROSION AROUND FITTING ON FLOOR BEAM BS 947; LBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947 LBL 50 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THIC - [SDR SWAA2024060684067](https://openairdocs.org/sdr/SWAA2024060684067), May 9, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT AT BS 947 RBL 50 WL 208<[01] REMOVED DAMAGE ON BS 947-967 RBL 50 FLOOR SUPPORT UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS - [SDR SWAA2024060683902](https://openairdocs.org/sdr/SWAA2024060683902), May 9, 2024: FLOOR SUPPORT. CORRODED. CORROSION AROUND FITTING ON FLOOR SUPPORT BS 947+3; LBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947-967 LBL 50 FLOOR SUPPORT UPPER SURFACE IN AN AREA OF 1'X 1'; O - [SDR SWAA2024060783884](https://openairdocs.org/sdr/SWAA2024060783884), May 8, 2024: ATTACH ANGLE. CORRODED. FWD SERVICE DOOR MOPSILL THRESHOLD ATTACH ANGLE HAS CORROSION AT BS 305; 310; 315; 319 RBL 61 WL 208. INSTALLED NEW FWD SERVICE DOOR MOPSILL THRESHOLD ATTACH AN - [SDR SWAA2024060783886](https://openairdocs.org/sdr/SWAA2024060783886), May 8, 2024: ATTACH ANGLE. CORRODED. CORROSION ON FED MOPSILL THRESHOLD ATTACH ANGLE AT BS 340 LBL 63 WL 208. - [SDR SWAA2024060683588](https://openairdocs.org/sdr/SWAA2024060683588), May 8, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241XF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] AFT FLOOR PANEL 241XF UPPER SKIN AREA OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00 - [SDR SWAA2024060683601](https://openairdocs.org/sdr/SWAA2024060683601), May 8, 2024: SUPPORT. BROKEN. AFT CARGO BAY FORWARD BULKHEAD FLOOR TO BULKHEAD SUPPORT IS BROKE BS 727+4 LBL 10 TO RBL 10 WL156<[01] IF REPAIR REFERENCE 25-52-10-400-801-NG-01 WAS ORIGINALLY - [SDR SWAA2024060683593](https://openairdocs.org/sdr/SWAA2024060683593), May 8, 2024: FLOOR PANEL. DAMAGED. FWD FLOOR PANEL 221BF O/B AFT CORNER TANG IS MISSING.<[01] FLOOR PANEL 221BF AFT CORNER TANG HAS BEEN REPAIRED IAW SRM 53-00-50-2R-6. - [SDR SWAA2024060683882](https://openairdocs.org/sdr/SWAA2024060683882), May 8, 2024: CHANNEL. CRACKED. FWD ENTRY DOOR MOPSILL IS CRACKED AT BS 303 LBL 57 WL 208<[01] REMOVED AND REPLACED FWD ENTRY MOPSILL IAW SRM 51-40-02-0G-0 AND DWG 140A9810;[02] VERIFIED CORRE - [SDR SWAA2024061083267](https://openairdocs.org/sdr/SWAA2024061083267), May 7, 2024: PANEL. DEBONDED. R/H; AFT AWE; HEADER PANEL FWD SIDE BOTTOM CLIP IS DISBONDED<[01] CORRECTTION SHOULD BE (R/H; AFT OWE; HEADER PANEL FWD SIDE BOTTOM CLIP IS DISBONED);[02] BONDE - [SDR SWAA2024060683586](https://openairdocs.org/sdr/SWAA2024060683586), May 7, 2024: SCUFF PLATE. CRACKED. FORWARD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FWD CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1. - [SDR SWAA2024060683587](https://openairdocs.org/sdr/SWAA2024060683587), May 7, 2024: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1. - [SDR SWAA2024060683583](https://openairdocs.org/sdr/SWAA2024060683583), May 7, 2024: WEB. CORRODED. CORROSION FWD CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS440+5' TO BS490' RBL 26 WL156<[01] REMOVED DAMAGED SUB THRESHOLD WEB; LOCATED; - [SDR SWAA2024060683584](https://openairdocs.org/sdr/SWAA2024060683584), May 7, 2024: WEB. CORRODED. CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01] REMOVED DAMAGED SUB THRESHOLD WEB. LOCATED; DRI - [SDR SWAA2024060683594](https://openairdocs.org/sdr/SWAA2024060683594), May 7, 2024: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727H+19' TO BS787+1' LBL22 WL156<[01] REMOVED DAMAGED SECTIO - [SDR SWAA2024060683585](https://openairdocs.org/sdr/SWAA2024060683585), May 7, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727C TO BS767 RBL22 WL156<[01] CORROSION ON SUPPORT WAS - [SDR SWAA2024030457919](https://openairdocs.org/sdr/SWAA2024030457919), Mar 1, 2024: POWER SUPPLY. INOPERATIVE. AFT LH EMERGENCY POWER SUPPLY INOP<[01] R/R
01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)] All 91: https://openairdocs.org/aircraft/N8690A/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.