# N8692F: 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: 33942
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 16, 2016
- Certificate issued: August 31, 2016
- Expires: August 31, 2029
- Mode S code: ABF2EA
- 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=8692F
- Page: https://openairdocs.org/aircraft/N8692F

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 N8692F.

## FAA accident and incident reports

None matched to N8692F.

## Service difficulty reports (81, 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 SWAA2026021169785](https://openairdocs.org/sdr/SWAA2026021169785), Feb 11, 2026: UNKNOWN. ODOR. VERY STRONG BURNING METAL ODOR IN THE AFT GALLEY, NO SMOKE. COFFEE POT WAS NOT ON. ODOR CAME ON STRONG & THEN DECREASED. PERFORMED AN INSPECTION IAW AMM 05-51-5
- [SDR SWAA2026012964893](https://openairdocs.org/sdr/SWAA2026012964893), Jan 26, 2026: LIGHT. DETACHED. LAST EMERGENCY LIGHTING STRIP ON LEFT SIDE REMOVED. APPROX 3 FEET LONG. REINSTALLED PHOTOLUMINSCENT STRIP IAW MM33-51-15
- [SDR SWAA2025112036811](https://openairdocs.org/sdr/SWAA2025112036811), Nov 19, 2025: PUMP. LEAKING. LOSS OF A HYDRAULICS QUANTITY ZERO R & R SYSTEM A EMDP PUMP IAW AMM 29-11-21-000 IAW SUB TASK 729-PRD-01-01.
- [SDR SWAA2025112037150](https://openairdocs.org/sdr/SWAA2025112037150), Nov 19, 2025: ACTUATOR. LEAKING. LOSS OF A HYDRAULICS, QUANTITY ZERO. R & R SYSTEM A ED PUMP IAW AMM 29-11-21-000 IAW SUB TASK 729-PRD-01-01. REMOVED & REPLACED THE NR 1 OTBD GROUND SPOILER ACT
- [SDR SWAA2025061780646](https://openairdocs.org/sdr/SWAA2025061780646), Jun 11, 2025: LAMP. INOPERATIVE. RIGHT AFTER SERVICE DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED RIGHT AFT SERVICE DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04.
- [SDR SWAA2025061779898](https://openairdocs.org/sdr/SWAA2025061779898), Jun 10, 2025: LIGHT. CRACKED. FWD LAV A EXIT LIGHT BASE CRACKED. REMOVED AND REPLACED PER AMM 33-51-01-960-802-NG.
- [SDR SWAA2025062576835](https://openairdocs.org/sdr/SWAA2025062576835), Jun 1, 2025: COWL DOOR. CRACKED. #1 ENGINE INBOARD FAN COWL; 414; STIFFENER AFT OF THE OIL SERVICE DOOR IS CRACKED.<[01] #1 ENG. I/B FAN COWL WILL REPLACED ON MT 7111-E-17063-NG (REP - RIGHT-HA
- [SDR SWAA2025062575975](https://openairdocs.org/sdr/SWAA2025062575975), May 29, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE HAS A CRACK AT APPROXIMATELY RBL 9<[01] REMOVED FASTENERS FROM BS 663 VAPOR BARRIER ATTACH ANGLE LOWER LEG PER SRM 57-10-10-2R
- [SDR SWAA2025062475974](https://openairdocs.org/sdr/SWAA2025062475974), May 29, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE HAS A CRACK AT APPROXIMATELY LBL 9. REMOVED FASTENERS FROM BS 663 VAPOR BARRIER ATTACH ANGLE LOWER LEG PER SRM 57-10-10-2R-5. 
- [SDR SWAA2025062578653](https://openairdocs.org/sdr/SWAA2025062578653), May 28, 2025: FITTING. LOOSE. LEFT WING TRAILING EDGE - DEFLECTION CONTROL RIB SUPPORT BEAM ATTACHMENT FASTENERS ARE LOOSE AT SERRATED PLATE.<[01] REMOVED INBD AND OUTBD SERRATED PLATES FOR 
- [SDR SWAA2025031103563](https://openairdocs.org/sdr/SWAA2025031103563), Mar 9, 2025: FLASHLIGHT. NO TEST. AFT GALLEY FLASH LIGHT WONT TEST AND SEAL BROKEN<[01] REPLACED AFT GALLEY FLASHLIGHT BATTERY REF AMM 25-64-00.
- [SDR SWAA2024121675810](https://openairdocs.org/sdr/SWAA2024121675810), Dec 11, 2024: BATTERY PACK. FAILED. EMERGENCY LIGHTING BATTERY PACK FWD OF R/H OVER WING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024120273208](https://openairdocs.org/sdr/SWAA2024120273208), Dec 2, 2024: LIGHT. INOPERATIVE. AFT ENTRY EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED LIGHT PER AMM 33-51-04. OP CHECK GOOD.
- [SDR SWAA2024112060977](https://openairdocs.org/sdr/SWAA2024112060977), Nov 17, 2024: FLASHLIGHT. DAMAGED. FWD OTBD FLASHLIGHT UNDER FLIGHT JUMP SEAT UNUSABLE FWD OTBD FLASHLIGHT UNUSABLE<[01] R&R FLASHLIGHT REF MM 25-64-00. THIS CLEARS MEL 25-12-01 #223812
- [SDR SWAA2024092540454](https://openairdocs.org/sdr/SWAA2024092540454), Sep 23, 2024: BULB. INOPERATIVE. R2 SERVICE DOOR SLIDE LIGHT INOP. REMOVED AND REPLACED BULB FOR R2 EMERGENCY SLIDE-EXTERIOR. REPLACED IAW AMM 33-51-01.
- [SDR SWAA2024081225069](https://openairdocs.org/sdr/SWAA2024081225069), Aug 9, 2024: SIGN. CRACKED. OVERWING CIELING EXIT SIGN COVER CRACKED<[01] R&R OVERWING CIELING EXIT SIGN COVER PER AMM 33-51-01
- [SDR SWAA2024061802689](https://openairdocs.org/sdr/SWAA2024061802689), Jun 17, 2024: CONNECTOR. DISCONNECTED. EMERGENCY LIGHT ON BACK OF FWD LAV INOP<[01] FOUND EMERGENCY LIGHT ON BACK OF FWD LAV UNPLUGGED; PLUGGED BACK IN AS PER AMM 33-51-01-960-801;[02] VERIFIED STEP 
- [SDR SWAA2024061802021](https://openairdocs.org/sdr/SWAA2024061802021), Jun 15, 2024: BATTERY PACK. INOPERATIVE. SEVERAL PAX CABIN EMERGENCY LIGHTS INOPERATIVE<[01] OPENED ACCESS PANEL TO PERFORM CABIN EMERGENCY LIGHTS; PERFORMED T/S AND FOUND M1676(R); M2335(L); M1694(L);
- [SDR SWAA2024061801294](https://openairdocs.org/sdr/SWAA2024061801294), Jun 13, 2024: FLOOR PANEL. DAMAGED. FABRICATION OF FLOOR PANEL #120CF AT FWD CARGO COMPARTMENT<[01] FABRICATED FWD CARGO FLOOR PANEL 120CF PER AMM 25-52-01-201-801 AND DWG # 453A1610 INSTALLATION 
- [SDR SWAA2024062102105](https://openairdocs.org/sdr/SWAA2024062102105), Jun 12, 2024: PANEL. DAMAGED. LEFT WING DEFLECTOR CONTROL RIB UPPER COMPOSITE PANEL HAS 4 EACH ELONGATED HOLES AS MARKED<[01] ACCOMPLISHED REPAIR AT LEFT WING DEFLECTOR CONTROL RIB UPPER COM
- [SDR SWAA2024061897820](https://openairdocs.org/sdr/SWAA2024061897820), Jun 3, 2024: FLOOR PANEL. DELAMINATED. LEFT PASSENGER CABIN FLOOR PANEL 221AF; SURFACE DELAMINATED.<[01] RECEIVED PANEL 221AF; PART #: 141A5810-728; PANEL WILL BE CLOSED ON TASK [TTG8Q00T3487];[02] V
- [SDR SWAA2024062097326](https://openairdocs.org/sdr/SWAA2024062097326), Jun 2, 2024: FLOOR PANEL. CRACKED. FLOOR PANEL 221BF CRACKED AT CORNER ON BOTTOM LEFT SIDE<[01] THIS FAULT WIIL BE RESOLVED IN ANOTHER FAUL (TTG8Q00TPJPY).;[02] FINAL INSPECTION; VERIFIED STEP #1
- [SDR SWAA2024061897613](https://openairdocs.org/sdr/SWAA2024061897613), Jun 2, 2024: FLOOR PANEL. CORRODED. FWD CARGO COMPARTMENT FLOOR PANEL#120CF HAS CORROSSION AROUND THE EDGES.<[01] RECIEVED MATERIAL 2024 T3 CLAD .071' P/O # 1749056 ; FABRICATION WILL BE ACCOMPLIS
- [SDR SWAA2024061897614](https://openairdocs.org/sdr/SWAA2024061897614), Jun 2, 2024: FLOOR PANEL. CORRODED. AFT CARGO COMPARTMENT FLOOR PANEL#140DF AFT OF STA. 890 UPPER SURFACE EDGE HAS CORROSION.<[01] NEW PART (AFT CARGO FLOOR PANEL 140 DF) RECEIVED; FOR INSTALLATIO
- [SDR SWAA2024061897612](https://openairdocs.org/sdr/SWAA2024061897612), Jun 2, 2024: FLOOR PANEL. CORRODED. FWD CARGO COMPARTMENT FLOOR PANEL#120BF HAS CORROSSION AROUND THE EDGES.<[01] AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024061897615](https://openairdocs.org/sdr/SWAA2024061897615), Jun 2, 2024: FLOOR PANEL. CORRODED. FWD CARGO COMPARTMENT FLOOR PANEL#120DF HAS CORROSSION AROUND THE EDGES.<[01] RECEIVED NEW FWD CARGO COMPARTMENT FLOOR PANEL#120DF; INSTALLATION WILL BE ACCOMPL
- [SDR SWAA2024061897316](https://openairdocs.org/sdr/SWAA2024061897316), Jun 1, 2024: FLOOR PANEL. CRACKED. FWD WET AREA PANEL CRACK # 141A5810-729<[01] REVEIVED NEW PANEL 221BF; PART #: 141A5810-729; PANEL WILL BE CLOSED ON TASK [TTG8Q00TPJPY].;[02] REVEIVED NEW PANE
- [SDR SWAA2024061897315](https://openairdocs.org/sdr/SWAA2024061897315), Jun 1, 2024: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL#241#AF DELAMINATED<[01] RECEIVED NEW FLOORPANEL PN. 144A5810-127; PANEL WILL BE CLOSED ON TTG8Q00T33ZX .;[02] FINAL INSPECTION; VERIFIED 
- [SDR SWAA2024061897320](https://openairdocs.org/sdr/SWAA2024061897320), Jun 1, 2024: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL#231XF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL P.N# 144A5810-126; PANEL WILL BE CLOSED ON TTG8QOOT343M.;[02] VERIFIED STEP:1<BR>AUDIT C/
- [SDR SWAA2024061897321](https://openairdocs.org/sdr/SWAA2024061897321), Jun 1, 2024: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL#241DF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL #144A5810-128; PANEL WILL BE CLOSED ON TTG8T33ZT.;[02] CORRECTING STE 1:RECEIVED NEW FLOO
- [SDR SWAA2024061897319](https://openairdocs.org/sdr/SWAA2024061897319), Jun 1, 2024: CHANNEL. CORRODED. FORWARD CARGO COMPARTMENT Z CHANNEL L/H HAS CORROSION FROM STA 500 TO STA 500E<[01] REMOVED AND REPLACED L/H Z CHANNEL FORWARD CARGO COMPARTMENT FROM STA 480+8 
- [SDR SWAA2024061897322](https://openairdocs.org/sdr/SWAA2024061897322), Jun 1, 2024: CHANNEL. CORRODED. FORWARD CARGO COMPARTMENT Z CHANNEL L/H HAS CORROSION FROM STA 500E TO STA 500I<[01] THIS N/R WILL BE CLOSED ON TTG8Q00TPJQH;[02] (RII) FINAL INSPECTION; VERIFI
- [SDR SWAA2024061894392](https://openairdocs.org/sdr/SWAA2024061894392), May 31, 2024: NOT REPORTED. CORRODED. CORROSION AT MAIN CABIN AFT WET AREA STA 947 RBL 50 UNDER HARD POINT<[01] ACCOMPLISHED REPAIR AT MAIN CABIN AFT WET AREA STA 947 RBL 50 UNDER HARD POINT SRM 51-
- [SDR SWAA2024061896979](https://openairdocs.org/sdr/SWAA2024061896979), May 31, 2024: WEB. CORRODED. CORROSION FOUND AFT CARGO DOOR CUTOUT LOWER WEB FROM STA 787 + 16 TO STA 847 RBL 27 WL 155.5 HAS SPOTS OF CORROSION.<[01] EVALUATED DAMAGE AT AFT CARGO DOOR CUT
- [SDR SWAA2024061891704](https://openairdocs.org/sdr/SWAA2024061891704), May 30, 2024: DOUBLER. DETERIORATED. EXTERNAL POWER RECEPTACLE CUT-OUT; AT LOWER EDGE DOBLER SKIN MISSING. FABRICATED AND INSTALLED NEW REPAIR PARTS AND RUBBING BLOCK AT EXTERNAL POWER RECEPTACLE C
- [SDR SWAA2024061891700](https://openairdocs.org/sdr/SWAA2024061891700), May 30, 2024: SKIN. DELAMINATED. LEFT WING O/B MAIN FLAP AFT FLAP; I/B LOWER SKIN SECTION DELAMINATED DOT 223-LWAF11.<[01] REMOVED AND INSTALLED NEW LEFT WING O/B AFT FLAP. AS PER AMM 27-51-22-
- [SDR SWAA2024061891706](https://openairdocs.org/sdr/SWAA2024061891706), May 30, 2024: SKIN. DELAMINATED. RIGHT WING O/B MAIN FLAP AFT FLAP; I/B LOWER SKIN SECTION DELAMINATED DOT 223-LWAF18.<[01] REMOVED AND INSTALLED NEW RIGHT WING O/B AFT FLAP. AS PER AMM AMM 27-
- [SDR SWAA2024061891701](https://openairdocs.org/sdr/SWAA2024061891701), May 30, 2024: POST. CORRODED. MAIN CABIN LAVATORY D FWD WALL PANEL DOOR POST CORRORED.<[01] REMOVED AND REINSTALLED MAIN CABIN LAVATORY D FWD WALL PANEL DOOR IN REF B737 CMM 25-40-42.;[02] V
- [SDR SWAA2024061891702](https://openairdocs.org/sdr/SWAA2024061891702), May 30, 2024: POST. CORRODED. MAIN CABIN LAVATORY E FWD WALL PANEL DOOR POST CORRORED.<[01] REMOVED LAVATORY E FWD WALL PANEL AS PER REF CMM 25-40-44;[02] REMOVED AND REINSTALLED MAIN CABIN 
- [SDR SWAA2024061901021](https://openairdocs.org/sdr/SWAA2024061901021), May 29, 2024: ANGLE. CRACKED. RIGHT WING O/B DEFLECTION CONTROL RIB PANEL; LOWER HORIZONTAL SEAL RETAINER ANGLE CRACK.<[01] REMOVED AND REPLACED RIGHT WING O/B DEFLECTION CONTROL RIB PANEL; 
- [SDR SWAA2024061902102](https://openairdocs.org/sdr/SWAA2024061902102), May 29, 2024: RETAINER. CRACKED. LEFT WING O/B DEFLECTION CONTROL RIB PANEL; LOWER HORIZONTAL SEAL RETAINER ANGLE CRACK.<[01] INSTALLED L LOWER HORIZONTAL SEAL RETAINER ANGLE AT LEFT WING O/B D
- [SDR SWAA2024061891307](https://openairdocs.org/sdr/SWAA2024061891307), May 29, 2024: POST. CORRODED. MAIN CABIN LAV A DOOR POST CORRORED AT THE BOTTOM.<[01] REMOVED AND REPLACED DOOR POST AT MAIN CABIN AFT LAV A IN REF B737 CMM 25-40-40;[02] FINAL INSPECTION; V
- [SDR SWAA2024061891308](https://openairdocs.org/sdr/SWAA2024061891308), May 29, 2024: POST. CORRODED. MAIN CABIN AFT LAV D DOOR POST CORRORED AT THE BOTTOM.<[01] REMOVED AND REPLACED DOOR POST AT MAIN CABIN AFT LAV D IN REF B737 CMM 25-4042;[02] CORRECT STEP 2:R
- [SDR SWAA2024061891309](https://openairdocs.org/sdr/SWAA2024061891309), May 29, 2024: POST. CORRODED. MAIN CABIN AFT LAV E DOOR POST CORRORED AT THE BOTTOM.<[01] REMOVED AND REPLACED LAV E DOOR POST AT MAIN CABIN AFT E IN REF B737 CMM 25-40-44;[02] FINAL INSPECT
- [SDR SWAA2024052288708](https://openairdocs.org/sdr/SWAA2024052288708), May 22, 2024: CONTROLLER. FAILED. CABIN CLIMB/ PRESSURIZATION FAIL<[01] FOUND #2 CPC FAULTING CABIN PRESS CONTROL MODULE. R&R'D OVERHEAD CABIN PRESS CONTROL MODULE . SWEEP TEST PASS . NO FAULTS 
- [SDR SWAA2024032768165](https://openairdocs.org/sdr/SWAA2024032768165), Mar 27, 2024: MEGAPHONE. DAMAGED. AFT MEGAPHONE DAMAGED<[01] REMOVED AND REPLACED AFT MEGAPHONE AND CKS OK. REF AMM 25-64-00
- [SDR SWAA2024032166273](https://openairdocs.org/sdr/SWAA2024032166273), Mar 21, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT SIGN ABOVE L2 DOOR IS INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK FOR THE EMERGENCY EXIT SIGN ABOVE L2 DOOR; PER [AMM 33-51-06-960-805-NG (
- [SDR SWAA2024011240321](https://openairdocs.org/sdr/SWAA2024011240321), Jan 12, 2024: LIGHT. INOPERATIVE. LH AFT EXIT DOOR EMERGENCY LIGHT IS INOP.<[01] REPLACED TERMINAL FOR LEFT AFT DOOR EMERGENCY LIGHT IAW SWPM 20-30-11
- [SDR SWAA2023120126582](https://openairdocs.org/sdr/SWAA2023120126582), Nov 30, 2023: FLASHLIGHT. INOPERATIVE. FWD FA JUMP SEAT FLASHLIGHT INOP<[01] RESECURED LIGHT. OPS CH GOOD PER AMM 33-55-00
- [SDR SWAA2023101710542](https://openairdocs.org/sdr/SWAA2023101710542), Oct 14, 2023: FAIRING. CRACKED. #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY CRACK - PERMANENT REPAIR<[01] R&R AFT PYLON STRUT FAIRING ASSY PER SRM 51-40-02 AND 51-10-02

All 81: https://openairdocs.org/aircraft/N8692F/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

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