# Service difficulty reports: N8688J

A list on [N8688J](https://openairdocs.org/aircraft/N8688J.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 101 reports

- [SDR SWAA2026101465049](https://openairdocs.org/sdr/SWAA2026101465049.md): Flashlight · out of position · Oct 10, 2026 · N8688J · Boeing 7378H4 · Emergency Equipment
  > 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.md): Lens · broken · Apr 4, 2026 · N8688J · Boeing 7378H4 · Emergency Lighting
  > CREW REPORTED FLOOR EXIT SIGN LENS BROKEN AT 14A. REPLACED THE LENS IAW AMM 33-51-01
- [SDR SWAA2025052172546](https://openairdocs.org/sdr/SWAA2025052172546.md): Battery · inoperative · May 19, 2025 · N8688J · Boeing 7378H4 · Emergency Equipment
  > CREW REPORTS AFTER FA FLASHLIGHT INOP <[01]. REPLACED BATTERY PER AMM 25-64-00.
- [SDR SWAA2025042424652](https://openairdocs.org/sdr/SWAA2025042424652.md): Battery Pack · inoperative · Apr 15, 2025 · N8688J · Boeing 7378H4 · Emergency Lighting
  > 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.md): Battery Pack · inoperative · Apr 9, 2025 · N8688J · Boeing 7378H4 · Emergency Lighting
  > 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.md): Strip · elongated · Apr 5, 2025 · N8688J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > 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 AND SPLICE PLATES; PER AMM 25-52-10 REF- [TTG8Q00ZHKG1] DUPLICATE WORK PERFORMED.; [02] C/W INSPECTIO
- [SDR SWAA2025042427986](https://openairdocs.org/sdr/SWAA2025042427986.md): Splice Plate · elongated · Apr 5, 2025 · N8688J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > 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 AND SPLICE PLATES; PER AMM 25-52-10 REF- [TTG8Q00ZHKG1] DUPLICATE WORK PERFORMED.; [02] C/W INSPECTION
- [SDR SWAA2025042421441](https://openairdocs.org/sdr/SWAA2025042421441.md): Angle · cracked · Apr 3, 2025 · N8688J · Boeing 7378H4 · Wing Main, Frame Structure
  > 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] REMOVED AND REPLACED RH A/C BAY STA 663 RBL 9' VAPOR BARRIER CLOSE OUT ANGLE PER SRM 51-40-02 AND 57-1
- [SDR SWAA2025042320443](https://openairdocs.org/sdr/SWAA2025042320443.md): Attach Angle · cracked · Apr 1, 2025 · N8688J · Boeing 7378H4 · Trailing Edge Flap Control System
  > 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 REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-40-02.
- [SDR SWAA2025042419377](https://openairdocs.org/sdr/SWAA2025042419377.md): Tail Cone · elongated · Mar 28, 2025 · N8688J · Boeing 7378H4 · Trailing Edge Flaps
  > #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 PARAGRAPH 4 K PER SRM 51-70-04-2R-9. PART REQUIREMENTS.; [03] FINISHED REPAIR PER SRM 51-70-04-2R-9; [04]
- [SDR SWAA2025042509847](https://openairdocs.org/sdr/SWAA2025042509847.md): Web · elongated · Mar 26, 2025 · N8688J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > 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 SRM 51-40-02.; [02] FABRICATED REPLACEMENT WEB PER BOEING SMAL (CONTROL #0271100384) BOEING DRAWING
- [SDR SWAA2025042408271](https://openairdocs.org/sdr/SWAA2025042408271.md): Door · cracked · Mar 21, 2025 · N8688J · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > #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 PERFORMED.
- [SDR SWAA2025042408272](https://openairdocs.org/sdr/SWAA2025042408272.md): Door · cracked · Mar 21, 2025 · N8688J · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > #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.md): Angle · cracked · Mar 20, 2025 · N8688J · Boeing 7378H4 · Wing Main, Frame Structure
  > 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. ANGLE REQUIRES REPLACEMENT REFERENCE SRM 57-10-10-2R-5.;[02] BEGAN REMOVING FASTENERS PER SRM 51-40-02.
- [SDR SWAA2025042407792](https://openairdocs.org/sdr/SWAA2025042407792.md): Angle · cracked · Mar 20, 2025 · N8688J · Boeing 7378H4 · Wing Main, Frame Structure
  > 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. ANGLE REQUIRES REPLACEMENT REFERENCE SRM 57-10-10-2R-5.; [02] BEGAN REMOVAL OF FASTENERS PER SRM 51-4
- [SDR SWAA2025042407811](https://openairdocs.org/sdr/SWAA2025042407811.md): Panel · delaminated · Mar 20, 2025 · N8688J · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > #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/A #1; [03] CORRECTED FAILURE TYPE LINE FROM NO TO YES ON BEHALF OF THE AMT.; [04] CERTIFIED.
- [SDR SWAA2025042407808](https://openairdocs.org/sdr/SWAA2025042407808.md): Web · cracked · Mar 20, 2025 · N8688J · Boeing 7378H4 · Trailing Edge Flaps
  > 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 WING UPPER FIXED TRAILING EDGE ATTACH WEB PER SRM 51-40-02.; [03] REMOVED AND REPLACED RT WING UPPER
- [SDR SWAA2025042423564](https://openairdocs.org/sdr/SWAA2025042423564.md): Doubler · loose · Mar 19, 2025 · N8688J · Boeing 7378H4 · Trailing Edge Flaps
  > 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 ON SUPPORT BEAM PER SRM 57-51-02-2R-1.; [02] C/W INSPECTION OF REPAIR AREA. ACCOMPLISHED HFEC HOLE P
- [SDR SWAA2025042407617](https://openairdocs.org/sdr/SWAA2025042407617.md): Plate · cracked · Mar 19, 2025 · N8688J · Boeing 7378H4 · Wing, Control Surfaces
  > 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 PER SRM 51-40-02. C/W INSPECTION.
- [SDR SWAA2025042307619](https://openairdocs.org/sdr/SWAA2025042307619.md): Floorboard · delaminated · Mar 19, 2025 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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 51-21-91.; [02] CIC WAS APPLIED AT 4:30 AM; 4-2-2025.; [03] R & R CABIN FLOORBOARD 231NF IN REFEREN
- [SDR SWAA2025042307626](https://openairdocs.org/sdr/SWAA2025042307626.md): Floorboard · delaminated · Mar 19, 2025 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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 FLOORBOARD 242KF IN REFERENCE TO AMM 53-21-00.
- [SDR SWAA2025042307620](https://openairdocs.org/sdr/SWAA2025042307620.md): Floorboard · delaminated · Mar 19, 2025 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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 51-21-91.; [02] CIC WAS APPLIED AT 4:30 AM; 4-2-2025.; [03] R & R CABIN FLOORBOARD 241SF IN REFEREN
- [SDR SWAA2025042307621](https://openairdocs.org/sdr/SWAA2025042307621.md): Floorboard · delaminated · Mar 19, 2025 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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 51-21-91.; [02] CIC WAS APPLIED AT 4:30 AM; 4-2-2025.; [03] R & R CABIN FLOORBOARD 241RF IN REFERE
- [SDR SWAA2025042307622](https://openairdocs.org/sdr/SWAA2025042307622.md): Floorboard · delaminated · Mar 19, 2025 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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 FLOORBOARD 242MF IN REFERENCE TO AMM 53-21-00.
- [SDR SWAA2025042307623](https://openairdocs.org/sdr/SWAA2025042307623.md): Floorboard · delaminated · Mar 19, 2025 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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 FLOORBOARD 242NF IN REFERENCE TO AMM 53-21-00.
- [SDR SWAA2025042307786](https://openairdocs.org/sdr/SWAA2025042307786.md): Plate · worn · Mar 18, 2025 · N8688J · Boeing 7378H4 · Wing, Control Surfaces
  > 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 FOUND TO BE BEYOND ALLOWABLE LIMITS AS GIVEN IN SRM 57-51-02-1A-1.; [02] CUT OUT AFFECTED DAMAGE AREA I.
- [SDR SWAA2025042406237](https://openairdocs.org/sdr/SWAA2025042406237.md): Flap · delaminated · Mar 17, 2025 · N8688J · Boeing 7378H4 · Trailing Edge Flaps
  > 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] INSPECTED THE WORK PERFORMED ON STEP #1; NO DEFECTS NOTED.; [03] REMOVED AND REPLACED LEFT WING OUTBOARD A
- [SDR SWAA2025042406238](https://openairdocs.org/sdr/SWAA2025042406238.md): Flap · delaminated · Mar 17, 2025 · N8688J · Boeing 7378H4 · Trailing Edge Flaps
  > 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. OUTBOARD AFT FLAP ADJUSTMENT GOOD IAW AMM 27-51-22; [02] INSPECTED WORK PERFORMED.
- [SDR SWAA2025012789812](https://openairdocs.org/sdr/SWAA2025012789812.md): Flashlight · inoperative · Jan 26, 2025 · N8688J · Boeing 7378H4 · Emergency Equipment
  > 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.md): Slide · out of adjust · Nov 12, 2024 · N8688J · Boeing 7378H4 · Escape Slide
  > 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.md): Power Supply · inoperative · Sep 13, 2024 · N8688J · Boeing 7378H4 · Emergency Lighting
  > 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 LIGHTS PER AMM 33-51-06. OP CHECK GOOD.
- [SDR SWAA2024072917646](https://openairdocs.org/sdr/SWAA2024072917646.md): Fuel Filter · inoperative · Jul 26, 2024 · N8688J · Boeing 7378H4 · Engine Fuel Distribution
  > #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.md): Battery · no test · May 7, 2024 · N8688J · Boeing 7378H4 · Emergency Equipment
  > 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.md): Battery Pack · inoperative · May 5, 2024 · N8688J · Boeing 7378H4 · Emergency Lighting
  > 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 SWA AMM 33-51-06.;[02] PARTS TRANSACTION DONE VIA TELECOM;[03] REMOVED AND REPLACED R/H BATTERY PACK A
- [SDR SWAA2024050882733](https://openairdocs.org/sdr/SWAA2024050882733.md): Battery Pack · inoperative · May 5, 2024 · N8688J · Boeing 7378H4 · Emergency Lighting
  > 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 AFT EMERGENCY OVERWING EXIT SIGN DISCONNECTED. RECONNECTED EXIT SIGN IAW WDM WDM 33-51-13. R/H OVERW
- [SDR SWAA2024050882734](https://openairdocs.org/sdr/SWAA2024050882734.md): Battery Pack · inoperative · May 5, 2024 · N8688J · Boeing 7378H4 · Emergency Lighting
  > 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 33-51-00-710-801;[02] EMERGENCY LIGHTS INOP AT R1 DOOR
- [SDR SWAA2024050883418](https://openairdocs.org/sdr/SWAA2024050883418.md): Charger · inoperative · May 5, 2024 · N8688J · Boeing 7378H4 · Emergency Lighting
  > 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 CHECK OF THE AFT LEFT HAND EMERGENCY LIGHTS IAW SWA AMM 33-51-06.;[02] REMOVED AND REPLACED LEFT HAN
- [SDR SWAA2024050882800](https://openairdocs.org/sdr/SWAA2024050882800.md): Battery Pack · inoperative · May 5, 2024 · N8688J · Boeing 7378H4 · Emergency Lighting
  > 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 CHECK OF THE AFT LEFT HAND EMERGENCY LIGHTS IAW SWA AMM 33-51-06.;[02] REMOVED AND REPLACED LEFT HAN
- [SDR SWAA2024050980920](https://openairdocs.org/sdr/SWAA2024050980920.md): Panel · cracked · Apr 30, 2024 · N8688J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > 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 PANEL INSTALLED ON CUSTOMER CARD TTG8Q00T278P AND HAECO CARD 20156.;[02] VERIFIED RECEIVED NEW PANE
- [SDR SWAA2024050978800](https://openairdocs.org/sdr/SWAA2024050978800.md): Floor Panel · damaged · Apr 24, 2024 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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] REMOVED AND REPLACED PANEL 231DF PER REFERENCE 737NG AMM 53-21-00-400-801-NG. VERIFIED.
- [SDR SWAA2024050978358](https://openairdocs.org/sdr/SWAA2024050978358.md): Floorboard · cracked · Apr 23, 2024 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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 53-21-00-400-801 - REMOVED AND REPLACED PANEL BREAK REF BAC DWG 143A0060 REV A AND B737-800 SRM 51-40-02
- [SDR SWAA2024050978359](https://openairdocs.org/sdr/SWAA2024050978359.md): Floorboard · cracked · Apr 23, 2024 · N8688J · Boeing 7378H4 · Fuselage Floor Panel
  > 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 SRM 51-40-02;[02] VERIFIED REMOVED AND REPLACED PANEL BREAK REF BAC DWG 143A0060 REV A AND B737-800 S
- [SDR SWAA2024050977211](https://openairdocs.org/sdr/SWAA2024050977211.md): Attach Angle · cracked · Apr 20, 2024 · N8688J · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > 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 B737-800 SRM 51-40-02;[02] VERIFIED REMOVED AND REPLACED IAW BOEING 737 DRW 143A7505 REV- AND B737-
- [SDR SWAA2024050876400](https://openairdocs.org/sdr/SWAA2024050876400.md): Attach Angle · cracked · Apr 18, 2024 · N8688J · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > [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] VERIFIED REMOVAL AND INSTALLATION OF CLIP AT STA. 55H STR. 26L IAW B737-800 SRM 51-740-02;[03] VER
- [SDR SWAA2024050876398](https://openairdocs.org/sdr/SWAA2024050876398.md): Stringer Clip · cracked · Apr 18, 2024 · N8688J · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > [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] CORRECTION TO CORRECTIVE ACTION: INSTALLED NEW CLIP AND REINSTALLED INTERCOSTAL AT LT.HD. STA. 500
- [SDR SWAA2024050876399](https://openairdocs.org/sdr/SWAA2024050876399.md): Stringer Clip · cracked · Apr 18, 2024 · N8688J · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > [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 AND B737-800 SRM 51-40-02;[02] VERIFIED REMOVED AND REPLACED IAW BOEING DRW143A1233 REV:A AND B737-80
- [SDR SWAA2024050876396](https://openairdocs.org/sdr/SWAA2024050876396.md): Attach Angle · cracked · Apr 18, 2024 · N8688J · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > [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 51-40-02] & BAC DWG 143A7502-154 REV -;[02] VERIFIED REMOVED AND REPLACED PER [B737-800 SRM 51-40-02] & B
- [SDR SWAA2024050876402](https://openairdocs.org/sdr/SWAA2024050876402.md): Attach Angle · cracked · Apr 18, 2024 · N8688J · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > [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 REV- AND B737-800 SRM 51-40-02;[02] VERIFIED REMOVED AND REPLACED IAW BOEING DRW 143A7505 REV- AND
- [SDR SWAA2024050876401](https://openairdocs.org/sdr/SWAA2024050876401.md): Attach Angle · cracked · Apr 18, 2024 · N8688J · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > [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 REV - AND B737 SRM 51-40-02;[02] VERIFIED REMOVED & INSTALLED IAW BAC DWG 143A7505-128 REV - AND B7
- [SDR SWAA2024050876393](https://openairdocs.org/sdr/SWAA2024050876393.md): Floor Support · cracked · Apr 18, 2024 · N8688J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > [DOT B765] FWD CARGO UNDER FLOOR AT STA 400; LEFT TRANSITION PANEL ATTACH INTERCOSTAL CRACKED AS MARKED.<[01] REMOVED; FABRICATED; LOCATED; DRILLED; AND INSTALLED NEW BAFFLE (INTERCOSATAL) REF BAC DWG 143A7505 REV:-; B737-NG SRM 51-40-02;[02] REMOVED; FABRICAT

Next page: https://openairdocs.org/aircraft/N8688J/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N8688J' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8688J/reports

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