# N8688J: 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: 36939
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 17, 2016
- Certificate issued: July 12, 2016
- Expires: July 31, 2029
- Mode S code: ABF008
- 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=8688J
- Page: https://openairdocs.org/aircraft/N8688J

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 N8688J.

## FAA accident and incident reports

None matched to N8688J.

## 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 SWAA2026101465049](https://openairdocs.org/sdr/SWAA2026101465049), Oct 10, 2026: FLASHLIGHT. OUT OF POSITION. CABIN EMERGENCY FLASHLIGHT WILL NOT TEST. REPOSITIONED AFT FO SIDE OTBD FLASHLIGHT TO CORRECT POSITION AND TESTED GOOD IAW AMM 25-64-00.
- [SDR SWAA2026040786379](https://openairdocs.org/sdr/SWAA2026040786379), Apr 4, 2026: LENS. BROKEN. CREW REPORTED FLOOR EXIT SIGN LENS BROKEN AT 14A. REPLACED THE LENS IAW AMM 33-51-01
- [SDR SWAA2025052172546](https://openairdocs.org/sdr/SWAA2025052172546), May 19, 2025: BATTERY. INOPERATIVE. CREW REPORTS AFTER FA FLASHLIGHT INOP <[01]. REPLACED BATTERY PER AMM 25-64-00.
- [SDR SWAA2025042424652](https://openairdocs.org/sdr/SWAA2025042424652), Apr 15, 2025: BATTERY PACK. INOPERATIVE. FWD GALLEY EMERGENCY LIGHTS INOP. <[01] R&R EMERGENCY LIGHTS BATTERY PACKS. OPS CHECK GOOD IAW AMM 33-51-06.; [02] VERIFIED.
- [SDR SWAA2025042423230](https://openairdocs.org/sdr/SWAA2025042423230), Apr 9, 2025: BATTERY PACK. INOPERATIVE. LEFT CABIN BULLNOSE EMERGENCY LIGHTS INOP <[01]. R&R EMERGENCY LIGHTS BATTERY PACKS. OPS CHECK GOOD IAW AMM 33-51-06.; [02] C/W INSPECTION OF C/A #1.
- [SDR SWAA2025042421939](https://openairdocs.org/sdr/SWAA2025042421939), Apr 5, 2025: STRIP. ELONGATED. AFT CARGO L/H AND R/H CAP STRIPS AND SPLICE PLATES; SEVERAL HAVE SEVERAL ELONGATED HOLES IN VARIOUS LOCATIONS. <[01] REPLACE AFT CARGO L/H AND R/H CAP STRIPS AN
- [SDR SWAA2025042427986](https://openairdocs.org/sdr/SWAA2025042427986), Apr 5, 2025: SPLICE PLATE. ELONGATED. AFT CARGO L/H AND R/H CAP STRIPS AND SPLICE PLATES; SEVERAL HAVE SEVERAL ELONGATED HOLES IN VARIOUS LOCATIONS. <[01] REPLACE AFT CARGO L/H AND R/H CAP STRIPS AN
- [SDR SWAA2025042421441](https://openairdocs.org/sdr/SWAA2025042421441), Apr 3, 2025: ANGLE. CRACKED. RAISED FAULT TO DOCUMENT INSPECTION BUYOFF OF REPAIR AT RH A/C BAY STA 663 RBL 9' VAPOR BARRIER CLOSE OUT ANGLE CRACKED REF FAULT BARCODE# TTG8Q00ZD6K0 <[01] RE
- [SDR SWAA2025042320443](https://openairdocs.org/sdr/SWAA2025042320443), Apr 1, 2025: ATTACH ANGLE. CRACKED. LT WING TRAILING EDGE DEFLECTION CONTROL RIB ATTACH ANGLE TO INBD WEB IS CRACKED. <[01] REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-40-02.; [02] VERIFIED REMOV
- [SDR SWAA2025042419377](https://openairdocs.org/sdr/SWAA2025042419377), Mar 28, 2025: TAIL CONE. ELONGATED. #6 FLAP TRACK FAIRING TAIL CONE UPPER CENTER MOUNT HOLE ELONGATED. <[01] REPAIRED UP TO PARAGRAPH 4 K PER SRM 51-70-04-2R-9; [02] VERIFIED REPAIRED UP TO PARAGR
- [SDR SWAA2025042509847](https://openairdocs.org/sdr/SWAA2025042509847), Mar 26, 2025: WEB. ELONGATED. LT VERTICAL WEB AT STA 663 FROM LBL 5 TO LBL 35 HAS 7 EA FASTENER HOLES ELONGATED <[01]. REMOVED FASTENERS COMMON TO 663 VERTICAL WEB FROM LBL 5 TO LBL 35 PER S
- [SDR SWAA2025042408271](https://openairdocs.org/sdr/SWAA2025042408271), Mar 21, 2025: DOOR. CRACKED. #1 ENGINE INBOARD FAN COWL WEB AFT OF OIL SERVICE DOOR IS CRACKED. (MARKED) <[01] #1 ENGINE INBOARD FAN COWL REPLACED ON TTG8Q00S5GXN.; [02] INSPECTED WORK PERF
- [SDR SWAA2025042408272](https://openairdocs.org/sdr/SWAA2025042408272), Mar 21, 2025: DOOR. CRACKED. #2 ENGINE OUTBOARD FAN COWL; WEB AFT OF OIL SERVICE DOOR IS CRACKED. (MARKED) <[01] REMOVED AND REPLACED #2 ENGINE OUTBOARD FAN COWL ON TTG8Q00S5GXN.
- [SDR SWAA2025042407806](https://openairdocs.org/sdr/SWAA2025042407806), Mar 20, 2025: ANGLE. CRACKED. RH A/C BAY STA 663 RBL 9' VAPOR BARRIER CLOSE OUT ANGLE CRACKED <[01] RH A/C BAY STA 663 VAPOR BARRIER CLOSE OUT ANGLE HAS ADDITIONAL CRACK DAMAGE AT RBL31. ANG
- [SDR SWAA2025042407792](https://openairdocs.org/sdr/SWAA2025042407792), Mar 20, 2025: ANGLE. CRACKED. LH A/C BAY STA 663 LBL 9' VAPOR BARRIER CLOSE OUT ANGLE CRACKED <[01]. LH A/C BAY STA 663 VAPOR BARRIER CLOSE OUT ANGLE HAS ADDITIONAL CRACK DAMAGE AT LBL42. AN
- [SDR SWAA2025042407811](https://openairdocs.org/sdr/SWAA2025042407811), Mar 20, 2025: PANEL. DELAMINATED. #1 ENGINE PANEL 434BL UPPER AFT CORNER HAS EDGE DAMAGE AND IS DELAMINATED (MARKED) <[01]. REPAIRED DAMAGED AREA PER SRM 51-70-04-2R-13; [02] C/W INSPECTION OF C
- [SDR SWAA2025042407808](https://openairdocs.org/sdr/SWAA2025042407808), Mar 20, 2025: WEB. CRACKED. R/H UPPER FIXED TRAILING EDGE PANEL ATTACH WEB INBOARD OF DEFLECTION RIB IS CRACKED. <[01] REMOVED DAMAGED WEB PER SRM 51-40-02.; [02] REMOVED AND REPLACED RT W
- [SDR SWAA2025042423564](https://openairdocs.org/sdr/SWAA2025042423564), Mar 19, 2025: DOUBLER. LOOSE. RT WING UPPER T/E PANEL LOOSE AT DEFLECTION ARM ATTACH POINT. <[01] REMOVED DAMAGE ON DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-4 AND REMOVED DAMAGE 
- [SDR SWAA2025042407617](https://openairdocs.org/sdr/SWAA2025042407617), Mar 19, 2025: PLATE. CRACKED. RT WING WIGGLE PLATE CRACKED AT PANEL 651EB FWD ATTACH POINT. <[01] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.; [02] REMOVED AND REPLACED WIGGLE PLATE 
- [SDR SWAA2025042307619](https://openairdocs.org/sdr/SWAA2025042307619), Mar 19, 2025: FLOORBOARD. DELAMINATED. CABIN FLOORBOARD 231NF HAS DELAMINATION. <[01] REMOVED CABIN FLOORBOARD 231NF IAW AMM 53-21-00. APPLIED CIC TO THE FLOOR STRUCTURE UNDER THIS FLOORBOARD IAW AMM
- [SDR SWAA2025042307626](https://openairdocs.org/sdr/SWAA2025042307626), Mar 19, 2025: FLOORBOARD. DELAMINATED. CABIN FLOORBOARD 242KF HAS DELAMINATION. <[01] OK TO INSTALL; [02] R & R CABIN FLOORBOARD 242KF IN REFERENCE TO AMM 53-21-00.; [03] INSPECTION C/W; R & R CABIN 
- [SDR SWAA2025042307620](https://openairdocs.org/sdr/SWAA2025042307620), Mar 19, 2025: FLOORBOARD. DELAMINATED. CABIN FLOORBOARD 241SF HAS DELAMINATION. <[01] REMOVED CABIN FLOORBOARD 241SF IAW AMM 53-21-00. APPLIED CIC TO THE FLOOR STRUCTURE UNDER THIS FLOORBOARD IAW AMM
- [SDR SWAA2025042307621](https://openairdocs.org/sdr/SWAA2025042307621), Mar 19, 2025: FLOORBOARD. DELAMINATED. CABIN FLOORBOARD 241RF HAS DELAMINATION. <[01] REMOVED CABIN FLOORBOARD 241RF IAW AMM 53-21-00. APPLIED CIC TO THE FLOOR STRUCTURE UNDER THIS FLOORBOARD IAW AMM
- [SDR SWAA2025042307622](https://openairdocs.org/sdr/SWAA2025042307622), Mar 19, 2025: FLOORBOARD. DELAMINATED. CABIN FLOORBOARD 242MF HAS DELAMINATION. <[01] OK TO INSTALL; [02] R & R CABIN FLOORBOARD 242MF IN REFERENCE TO AMM 53-21-00.; [03] INSP C/W; R & R CABIN FLOORB
- [SDR SWAA2025042307623](https://openairdocs.org/sdr/SWAA2025042307623), Mar 19, 2025: FLOORBOARD. DELAMINATED. CABIN FLOORBOARD 242NF HAS DELAMINATION. <[01] OK TO INSTALL; [02] R & R CABIN FLOORBOARD 242NF IN REFERENCE TO AMM 53-21-00.; [03] INSP C/W; R & R CABIN FLOORB
- [SDR SWAA2025042307786](https://openairdocs.org/sdr/SWAA2025042307786), Mar 18, 2025: PLATE. WORN. LEFT WING - DEFLECTION CONTROL RIB; SERRATED PLATE WORN AT ATTACH POINT. <[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .070?. DAMAGE FOUN
- [SDR SWAA2025042406237](https://openairdocs.org/sdr/SWAA2025042406237), Mar 17, 2025: FLAP. DELAMINATED. L/H WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATION ON UPPER SURFACE ON I/B CORNER <[01]. RII: OK TO INSTALL L/H WING OUTBOARD AFT FLAP ASSEMBLY.; [02] INSPECT
- [SDR SWAA2025042406238](https://openairdocs.org/sdr/SWAA2025042406238), Mar 17, 2025: FLAP. DELAMINATED. R/H WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATION ON LOWER SURFACE ON I/B CORNER <[01]. REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP PER. AMM. 27-51-22.
- [SDR SWAA2025012789812](https://openairdocs.org/sdr/SWAA2025012789812), Jan 26, 2025: FLASHLIGHT. INOPERATIVE. AFT LEFT FLASHLIGHT INOP. BLINKED RED ONCE THEN BLANK.<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024111858966](https://openairdocs.org/sdr/SWAA2024111858966), Nov 12, 2024: SLIDE. OUT OF ADJUST. L1 DOOR SLIDE FELL OUT OF STOWAGE BOX NEED LOGPAGE<[01] REF AMM 25-66-01 RE INSTALLED FWD ENTRY DOOR SLIDE AS REQUIRED. OK FOR SERVICE
- [SDR SWAA2024091637431](https://openairdocs.org/sdr/SWAA2024091637431), Sep 13, 2024: POWER SUPPLY. INOPERATIVE. RH OVERWING EXIT AND RH WING TO BODY EMERGENCY LIGHTS OUT.<[01] REMOVED AND REPLACED BOTH POWER SUPPLIES ON RH OVERWING EXIT AND RH WING TO BODY EMERGENCY LIGHT
- [SDR SWAA2024072917646](https://openairdocs.org/sdr/SWAA2024072917646), Jul 26, 2024: FUEL FILTER. INOPERATIVE. #1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED<[01] REMOVED AND REPLACED #1 ENG FUEL FILTER IRW AMM 73-11-02. OPS AND LEAK CHECK GOOD AT THIS TIME.
- [SDR SWAA2024050983648](https://openairdocs.org/sdr/SWAA2024050983648), May 7, 2024: BATTERY. NO TEST. BOTH FWD GALLEY FLASHLIGHTS DO NOT TEST<[01] REMOVED AND REPLACED BOTH FWD FLASHLIGHT BATTERIES IAW AMM 25-64-00
- [SDR SWAA2024050882799](https://openairdocs.org/sdr/SWAA2024050882799), May 5, 2024: BATTERY PACK. INOPERATIVE. R/H AFT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED R/H BATTERY PACK AT SEAT 20DEF AND PERFORMED A GOOD OPERATIONAL CHECK OF THE AFT EMERGENCY LIGHTS IAW SW
- [SDR SWAA2024050882733](https://openairdocs.org/sdr/SWAA2024050882733), May 5, 2024: BATTERY PACK. INOPERATIVE. R/H OVER WING EMERGENCY EXIT DOOR LIGHTS INOP<[01] REMOVED AND REPLACED R/H OVERWING EMERGENCY BATTERY PACK IAW AMM 33-51-06-960-805. TROUBLESHOT AND FOUND R/H 
- [SDR SWAA2024050882734](https://openairdocs.org/sdr/SWAA2024050882734), May 5, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOP AT R1 DOOR<[01] REMOVED AND REPLACED R1 BATTERY PACK M2816 IAW B737 AMM 33-51-06-960-805. EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51-00
- [SDR SWAA2024050883418](https://openairdocs.org/sdr/SWAA2024050883418), May 5, 2024: CHARGER. INOPERATIVE. L/H AFT CABIN EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED LEFT HAND SEAT 20 ABC EMERGENCY BATTERY CHARGER AND BATTERY PACK AND PERFORMED A GOOD OPERATIONAL 
- [SDR SWAA2024050882800](https://openairdocs.org/sdr/SWAA2024050882800), May 5, 2024: BATTERY PACK. INOPERATIVE. L/H AFT CABIN EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED LEFT HAND SEAT 20 ABC EMERGENCY BATTERY CHARGER AND BATTERY PACK AND PERFORMED A GOOD OPERATIONAL 
- [SDR SWAA2024050980920](https://openairdocs.org/sdr/SWAA2024050980920), Apr 30, 2024: PANEL. CRACKED. AFT CARGO PANEL 142NW HAS CRACKS.<[01] RECEIVED NEW PANEL 142NW P/N 453A2510-1 ITEM NUMBER SS5277000040 REF BAC DWG 453A2510 REV C AND B737-NG AIPC 25-52-19-01B
- [SDR SWAA2024050978800](https://openairdocs.org/sdr/SWAA2024050978800), Apr 24, 2024: FLOOR PANEL. DAMAGED. COSTUMER REQUEST EVALUATE AND REPAIR POPPING SOUND ON FLOOR PANEL 231DF<[01] REMOVED AND REPLACED PANEL 231DF PER REFERENCE 737NG AMM 53-21-00-400-801-NG;[02] R
- [SDR SWAA2024050978358](https://openairdocs.org/sdr/SWAA2024050978358), Apr 23, 2024: FLOORBOARD. CRACKED. MAIN CABIN FLOORBOARD PANEL BREAK CRACKED AT BL 0 STATION 540 (LEFT PANEL BREAK PIECE)<[01] REMOVED AND REINSTALLED CABIN FLOOR PANEL 231UF REF B737-NG AMM 53-2
- [SDR SWAA2024050978359](https://openairdocs.org/sdr/SWAA2024050978359), Apr 23, 2024: FLOORBOARD. CRACKED. MAIN CABIN FLOORBOARD PANEL BREAK AT STATION 540 BL 0 CRACKED (RIGHT SIDE PIECE)<[01] REMOVED AND REPLACED PANEL BREAK REF BAC DWG 143A0060 REV A AND B737-800 S
- [SDR SWAA2024050977211](https://openairdocs.org/sdr/SWAA2024050977211), Apr 20, 2024: ATTACH ANGLE. CRACKED. FWD CARGO @ STA 500G @ STR-26R LOCATED UNDER RIGHT TRANSITION PANEL FRAME ATTACH AFT CLIP CRACKED<[01] REMOVED AND REPLACED IAW BOEING 737 DRW 143A7505 REV- AND
- [SDR SWAA2024050876400](https://openairdocs.org/sdr/SWAA2024050876400), Apr 18, 2024: ATTACH ANGLE. CRACKED. [DOT W490] FWD CARGO AT STA.500H AT S-26L; LOCATED UNDER LEFT TRANSITION PANEL FRAME ATTACH FWD CLIP CRACKED.<[01] INSTALLED CLIP IAW B737-800 SRM 51-740-02;[02
- [SDR SWAA2024050876398](https://openairdocs.org/sdr/SWAA2024050876398), Apr 18, 2024: STRINGER CLIP. CRACKED. [DOT W489] FWD CARGO AT STA.500 I AT S-26L; LOCATED UNDER LEFT TRANSITION PANEL STRINGER CLIP CRACKED.<[01] INSTALLED INTERCOSTAL IAW B737-800 SRM 51-40-02;[02]
- [SDR SWAA2024050876399](https://openairdocs.org/sdr/SWAA2024050876399), Apr 18, 2024: STRINGER CLIP. CRACKED. [DOT W491] FWD CARGO AT STA.500 I AT S-26R; LOCATED UNDER RIGHT TRANSITION PANEL STRINGER CLIP CRACKED.<[01] REMOVED AND REPLACED IAW BOEING DRW143A1233 REV:A A
- [SDR SWAA2024050876396](https://openairdocs.org/sdr/SWAA2024050876396), Apr 18, 2024: ATTACH ANGLE. CRACKED. [DOT W492] FWD CARGO AT STA.500H AT S-26R; LOCATED UNDER RIGHT TRANSITION PANEL FRAME ATTACH AFT CLIP CRACKED.<[01] REMOVED AND REPLACED PER [B737-800 SRM 51-40
- [SDR SWAA2024050876402](https://openairdocs.org/sdr/SWAA2024050876402), Apr 18, 2024: ATTACH ANGLE. CRACKED. [DOT W100] FWD CARGO AT STA.500H AT S-26R; LOCATED UNDER RIGHT TRANSITION PANEL FRAME ATTACH FWD CLIP CRACKED.<[01] REMOVED AND REPLACED IAW BOEING DRW 143A7505
- [SDR SWAA2024050876401](https://openairdocs.org/sdr/SWAA2024050876401), Apr 18, 2024: ATTACH ANGLE. CRACKED. [DOT W101] FWD CARGO AT STA.500G AT S-26R; LOCATED UNDER RIGHT TRANSITION PANEL FRAME ATTACH FWD CLIP CRACKED.<[01] REMOVED & INSTALLED IAW BAC DWG 143A7505-128
- [SDR SWAA2024050876393](https://openairdocs.org/sdr/SWAA2024050876393), Apr 18, 2024: FLOOR SUPPORT. CRACKED. [DOT B765] FWD CARGO UNDER FLOOR AT STA 400; LEFT TRANSITION PANEL ATTACH INTERCOSTAL CRACKED AS MARKED.<[01] REMOVED; FABRICATED; LOCATED; DRILLED; AND INSTALL

All 101: https://openairdocs.org/aircraft/N8688J/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 N8688J

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8688J before.

- [Cancelled 2007-11-21](https://openairdocs.org/deregistered/N8688J-2007-11-21): Cessna 150G, S/N 15066588, built 1967. Triennial form not returned. Owner: [Lamb Steven J](https://openairdocs.org/faa-owner/LAMB%20STEVEN%20J), [Pleasanton, CA](https://openairdocs.org/faa-place/CA/Pleasanton)

## 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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