# N8684F: 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: 36653
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 24, 2016
- Certificate issued: June 16, 2016
- Expires: June 30, 2029
- Mode S code: ABEF79
- 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=8684F
- Page: https://openairdocs.org/aircraft/N8684F

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 N8684F.

## FAA accident and incident reports

None matched to N8684F.

## Service difficulty reports (101, 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 SWAA2026032683505](https://openairdocs.org/sdr/SWAA2026032683505), Mar 26, 2026: UNKNOWN. ODOR. FLIGHT ATTENDANTS REPORTED BURNING WIRE SMELL IN AFT GALLEY NO VISIBLE SMOKE; SMELL PERSISTED THROUGHOUT FLIGHT<[01] PERFORMED CONDITIONAL INSPECTION PER AMM 05
- [SDR SWAA2026010557659](https://openairdocs.org/sdr/SWAA2026010557659), Jan 2, 2026: TRAY. BROKEN. TRAY TABLE BROKEN ROW 14A. RE-INSTALLED TRAY TABLE 14A OTBD ARM TO TABLE PER CMM 25-22-46.
- [SDR SWAA2025121652125](https://openairdocs.org/sdr/SWAA2025121652125), Dec 12, 2025: LENS. DETACHED. OVERWING EXIT LIGHT LENS FELL OFF. INSTALLED THE LENS IAW 33-51-01.
- [SDR SWAA2025082708003](https://openairdocs.org/sdr/SWAA2025082708003), Aug 25, 2025: LAMP. INOPERATIVE. RIGHT AFT OVERWING EMERGENCY EXIT LIGHT LAMP OUT. RELAMPED RT AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04.
- [SDR SWAA2025062484547](https://openairdocs.org/sdr/SWAA2025062484547), Jun 22, 2025: TRANSMITTER. INOPERATIVE. TRAILING EDGE FLAP /DISAGREE /ASYMMETRY TRAILING EDGE FLAP DISAGREE / ASYMMETRY <1<[01] ALT FLAP SWITCH USED SWITCH TO DRIVE FLAPS DOWN ;SWITCH IN COCKPIT NOT S
- [SDR SWAA2025061079867](https://openairdocs.org/sdr/SWAA2025061079867), Jun 9, 2025: TRANSMITTER. MALFUNCTIONED. DURING APP AT MDW WHEN SELECTING FLAPS 5; WE GOT A SPLIT FLAP; RAN QRH PER OPPS T427 IS LAGGING ON AHM FSEU BITE FC 27-53279 CONFIRMED NO CB TRIPPED<[01] REMOVE
- [SDR SWAA2025051265576](https://openairdocs.org/sdr/SWAA2025051265576), Apr 29, 2025: FAIRING. DAMAGED. #6 CANOE FAIRING HAS ELONGATED SEAL FASTENER HOLES.<[01] A NEW #6 CANOE FAIRING WAS ORDERED FOR A/C. NEW CANOE FAIRING WILL BE INSTALLED ON FAULT # TTG8Q00ZVLVW
- [SDR SWAA2025051265004](https://openairdocs.org/sdr/SWAA2025051265004), Apr 28, 2025: SEAL. CRACKED. RT STAB UPPER FWD SLIDING SEAL ON FUSELAGE CRACKED.<[01] REMOVED RH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31.;[02] REPLACED RH HORIZONTAL UPPER FWD SL
- [SDR SWAA2025051264513](https://openairdocs.org/sdr/SWAA2025051264513), Apr 27, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHT EXTERNAL OF AFT R/H OVERWING EXIT WILL NOT ILLUMINATE.<[01] REMOVED AND REPLACED BATTERY PACK M1671 PER AMM 33-51-06. NO FAULTS NOTED.;[02]
- [SDR SWAA2025051264670](https://openairdocs.org/sdr/SWAA2025051264670), Apr 27, 2025: BATTERY PACK. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHTS BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 AT STA 565L PER MM 33-51-06;[02] LEFT OVERWING EME
- [SDR SWAA2025051264671](https://openairdocs.org/sdr/SWAA2025051264671), Apr 27, 2025: BATTERY PACK. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK M1695 AT STA 565R IS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1695 AT STA 565R PER MM33-51-06;[0
- [SDR SWAA2025051251405](https://openairdocs.org/sdr/SWAA2025051251405), Apr 22, 2025: SUPPORT ANGLE. CRACKED. R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE P
- [SDR SWAA2025050526851](https://openairdocs.org/sdr/SWAA2025050526851), Apr 22, 2025: ANGLE. CRACKED. R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE P
- [SDR SWAA2025050535622](https://openairdocs.org/sdr/SWAA2025050535622), Apr 22, 2025: SUPPORT ANGLE. CRACKED. R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE P
- [SDR SWAA2025050751397](https://openairdocs.org/sdr/SWAA2025050751397), Apr 19, 2025: ATTACH BRACKET. CRACKED. RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS
- [SDR SWAA2025050526424](https://openairdocs.org/sdr/SWAA2025050526424), Apr 19, 2025: BRACKET. CRACKED. RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS
- [SDR SWAA2025050535614](https://openairdocs.org/sdr/SWAA2025050535614), Apr 19, 2025: BRACKET. CRACKED. RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS
- [SDR SWAA2025051251345](https://openairdocs.org/sdr/SWAA2025051251345), Apr 14, 2025: BRACKET. CRACKED. LT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR CRACKED. SEE ATTACHED PICS.<[01] REMOVED AND REPLACED CONDUIT BRACKET. IAW SRM 51-40-02;[02] 
- [SDR SWAA2025051251332](https://openairdocs.org/sdr/SWAA2025051251332), Apr 12, 2025: SUPPORT BRACKET. CORRODED. R/H WING L/E FUELING GAUGES SUPPORT BRACKET HAS SEVERAL AREAS OF SURFACE CORROSION. MRKD<[01] REMOVED AND REPLACED R/H WING L/E REFUELING GAUGES SUPPORT BRACKET
- [SDR SWAA2025050523404](https://openairdocs.org/sdr/SWAA2025050523404), Apr 10, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 34<[01] REMOVED BS 63 R/H VAPOR BARRIER ANGLE PER SRM 51-40-02.;[02] MATCH DRILLED NEW ANGLE PER SRM 51-40-02. 
- [SDR SWAA2025050535537](https://openairdocs.org/sdr/SWAA2025050535537), Apr 10, 2025: ATTACH ANGLE. CRACKED. BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 34. REMOVED BS 63 R/H VAPOR BARRIER ANGLE PER SRM 51-40-02. MATCH DRILLED NEW ANGLE PER SRM 51-40-02. INSTALLED
- [SDR SWAA2024121777031](https://openairdocs.org/sdr/SWAA2024121777031), Dec 13, 2024: SIGN. BROKEN. OVERHEAD EMERGENCY EXIT SIGN AT OVERNIGHT EXITS BROKEN.<[01] REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT SIGN ASSY AT OVERWING EXITS IAW AMM 33-51-01. OP CHECK
- [SDR SWAA2024101748765](https://openairdocs.org/sdr/SWAA2024101748765), Oct 14, 2024: COVER. MISSING. CENTER AISLE FORWARD EXIT LOCATOR SIGN MISSING<[01] INSTALLED MISSING LENSE COVER PER SIP
- [SDR SWAA2024100744089](https://openairdocs.org/sdr/SWAA2024100744089), Oct 1, 2024: SIGN. BROKEN. CENTER EMERGENCY EXIT SIGN BROKEN<[01] REPLACED CENTER EMER EXIT SIGN LENS PER M/M 33-51-01.
- [SDR SWAA2024081325122](https://openairdocs.org/sdr/SWAA2024081325122), Aug 10, 2024: COVER. DETACHED. EMERGENCY EXIT LIGHT CEILING MOUNTED COVER FELL OFF<[01] REINSTALLED COVER PER SIP
- [SDR SWAA2024071814095](https://openairdocs.org/sdr/SWAA2024071814095), Jul 18, 2024: LENS. LOOSE. EMERGENCY EXIT ROW SIGN ON OVHD LENS FELL OFF<[01] REINSTALLED OVERWING EXIT SIGN LENS IAW AMM 33-51-01. A/C OK FOR SERVICE
- [SDR SWAA2024070106909](https://openairdocs.org/sdr/SWAA2024070106909), Jun 28, 2024: BRACKET. BROKEN. MID CABIN EXIT SIGN BRACKET BROKEN<[01] RESECURED MID CABIN EXIT SIGN LENS PER MM 33-51-03; OPS CK GOOD
- [SDR SWAA2024050279621](https://openairdocs.org/sdr/SWAA2024050279621), Apr 27, 2024: LIGHT. BROKEN. FWD LAV A EXIT LIGHT IS BROKEN.<[01] REMOVED AND REPLACED FWD LAV A EXIT LIGHT PER SOPM 20-50-01.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024050276757](https://openairdocs.org/sdr/SWAA2024050276757), Apr 18, 2024: FLOORBEAM. CORRODED. CORROSION ON AFT WET AREA FLOOR BEAM AT BS 947; RBL 23; WL 208.<[01] REMOVED DAMAGED SECTION AND ACCOMPLISHED REPAIR OF FLOOR BEAM AT BS 947 RBL 8.5' TO RBL 41.
- [SDR SWAA2024050776755](https://openairdocs.org/sdr/SWAA2024050776755), Apr 17, 2024: NONE. NONE. REMOVE AND REINSTALL RIGHT ELEVATOR FOR PAINT<[01] REMOVED AND REINSTALLED RH ELEVATOR IAW AMM 27-31-11-400-801. SEE PREVIOUS STEPS TO VERIFY.
- [SDR SWAA2024050776754](https://openairdocs.org/sdr/SWAA2024050776754), Apr 17, 2024: NONE. NONE. REMOVE AND REINSTALL LEFT ELEVATOR FOR PAINT<[01] REMOVED AND REINSTALLED LH ELEVATOR IAW AMM 27-31-11-400-801. SEE PREVIOUS STEPS TO VERIFY.
- [SDR SWAA2024050676437](https://openairdocs.org/sdr/SWAA2024050676437), Apr 17, 2024: BRACKET. CRACKED. BOTH BRACKETS CRACKED ON ASD PANEL 844DZ<[01] REPLACED BOTH FWD AND AFT BRACKETS ON ASD PANEL 844DZ PER SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<B
- [SDR SWAA2024050276423](https://openairdocs.org/sdr/SWAA2024050276423), Apr 17, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241GF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED FLOOR PANEL 241GF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] INSTALLED
- [SDR SWAA2024050276424](https://openairdocs.org/sdr/SWAA2024050276424), Apr 17, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242HF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242HF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] OK TO CLOSE GRA
- [SDR SWAA2024050276426](https://openairdocs.org/sdr/SWAA2024050276426), Apr 17, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242GF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242GF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242
- [SDR SWAA2024050276427](https://openairdocs.org/sdr/SWAA2024050276427), Apr 17, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242MF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242MF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242
- [SDR SWAA2024050276425](https://openairdocs.org/sdr/SWAA2024050276425), Apr 17, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242NF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242NF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242
- [SDR SWAA2024050276428](https://openairdocs.org/sdr/SWAA2024050276428), Apr 17, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241MF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 241MF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] INSTALLED PANEL
- [SDR SWAA2024050276422](https://openairdocs.org/sdr/SWAA2024050276422), Apr 17, 2024: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 231KF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 231KF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 231
- [SDR SWAA2024050276080](https://openairdocs.org/sdr/SWAA2024050276080), Apr 17, 2024: FLOOR SUPPORT. CRACKED. PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 52; WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT TOP ANGLE AT STA 380-400; LBL 52; WL 208 PER
- [SDR SWAA2024050276436](https://openairdocs.org/sdr/SWAA2024050276436), Apr 17, 2024: FLOOR SUPPORT. CRACKED. PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 1; WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT TOP ANGLE AT STA 380-400; LBL 1; WL 208 PER S
- [SDR SWAA2024050276431](https://openairdocs.org/sdr/SWAA2024050276431), Apr 17, 2024: FLOOR SUPPORT. CRACKED. PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 13; WL 208.<[01] REMOVED AND REPLACE PASSENGER CABIN FWD FLOOR SUPPORT AT BS 380-400; LBL 13; WL
- [SDR SWAA2024050276064](https://openairdocs.org/sdr/SWAA2024050276064), Apr 17, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] REMOVED FWD CARGO BAY R/H FL
- [SDR SWAA2024050276065](https://openairdocs.org/sdr/SWAA2024050276065), Apr 17, 2024: SHIELD. CORRODED. CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED FWD CARGO BAY AFT SHIELD; LOCATED; DRI
- [SDR SWAA2024050276066](https://openairdocs.org/sdr/SWAA2024050276066), Apr 17, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500D+6' TO BS500I LBL22 WL156<[01] ' THE DAMAGE WAS REPAIRED
- [SDR SWAA2024050276434](https://openairdocs.org/sdr/SWAA2024050276434), Apr 17, 2024: WEB. CORRODED. CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01] REMOVED AFT CARGO BAY SUB THRESHOLD WEB; LOCATE
- [SDR SWAA2024050276429](https://openairdocs.org/sdr/SWAA2024050276429), Apr 17, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727H+21' TO BS807+3' LBL22 WL156<[01] REMOVED DAMAGED SECTIO
- [SDR SWAA2024050276435](https://openairdocs.org/sdr/SWAA2024050276435), Apr 17, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] REMOVED AFT CARGO BAY R/H
- [SDR SWAA2024050276430](https://openairdocs.org/sdr/SWAA2024050276430), Apr 17, 2024: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AFT CARGO BAY SHIELD FWD OF CARGO DOO
- [SDR SWAA2024050276441](https://openairdocs.org/sdr/SWAA2024050276441), Apr 17, 2024: STRAP. CORRODED. CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 727I+5 RBL 16 TO LBL 16 WL 156<[01] RECEIVED NEW AFT CARGO BAY FLOOR T STRAP BS 727I+5 RBL 16 TO LBL 16 WL 156 ON PO

All 101: https://openairdocs.org/aircraft/N8684F/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 N8684F

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8684F before.

- [Cancelled 1996-12-11](https://openairdocs.org/deregistered/N8684F-1996-12-11): Hughes Helicopters HUGHES 369D, S/N 1170228D. Triennial form not returned. Owner: [Gatx Capital Corp](https://openairdocs.org/faa-owner/GATX%20CAPITAL%20CORP), [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco)

## 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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