# Service difficulty reports: N8687A

A list on [N8687A](https://openairdocs.org/aircraft/N8687A.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 2 · 88 reports

- [SDR SWAA2026081014795](https://openairdocs.org/sdr/SWAA2026081014795.md): Battery Pack · inoperative · Aug 3, 2026 · N8687A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1695 ARE INOPERATIVE. REPLACED THE BATTERY PACK M1695 AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.
- [SDR SWAA2026080716825](https://openairdocs.org/sdr/SWAA2026080716825.md): Nut · broken · Aug 1, 2026 · N8687A · Boeing 7378H4 · Passenger/Crew Doors
  > UPON INSTALLATION OF G1, ASSIST HANDLE RETAINING NUT FOUND BROKEN UPON INSTALLATION OF G1 ASSIST HANDLE RETAINING NUT FOUND BROKEN. REPLACED BROKEN NUT ON G1 ASSIST HANDLE IAW CMM 25-31-67 PG. 7001 ASSEMBLY STEP 3. A. AND FIG 1.
- [SDR SWAA2026020266359](https://openairdocs.org/sdr/SWAA2026020266359.md): Lens · detached · Jan 30, 2026 · N8687A · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD CIELING EXIT LIGHT LENS FELL OFF. R & R LIGHT ASSY REF AMM 33-51-01
- [SDR SWAA2026010557567](https://openairdocs.org/sdr/SWAA2026010557567.md): Lens · missing · Jan 1, 2026 · N8687A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN MID CABIN NOT IN PLACE, NEEDS TO BE INSTALLED. INSTALLED MID CABIN EXIT SIGN LENS PER AMM 33-51-02
- [SDR SWAA2025120140999](https://openairdocs.org/sdr/SWAA2025120140999.md): Light · broken · Nov 29, 2025 · N8687A · Boeing 7378H4 · Emergency Lighting
  > CENTER AISLE EXIT LIGHT BROKEN. REINSTALLED MID CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01. ACFT OK FOR SERVICE.
- [SDR SWAA2025120140801](https://openairdocs.org/sdr/SWAA2025120140801.md): Acm · seized · Nov 29, 2025 · N8687A · Boeing 7378H4 · Cabin Cooling System
  > LEFT ACM LIGHT ILLUMANTED FOLLOWED BY AN ODOR IN THE FLIGHT DECK. OK TO CONTINUE IAW MEL 21-1-01, SP1, AUTH 295231, FOUND LT ACM DAMAGED & SEIZED. R & R LT ACM IAW AMM 21-51-04. OPS CHECKED GOOD.
- [SDR SWAA2025102125446](https://openairdocs.org/sdr/SWAA2025102125446.md): Lens · detached · Oct 18, 2025 · N8687A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN FROM THE CENTER CABIN CEILING FELL OFF. RESURCURED CENTER CABIN EMERGENCY EXIT SIGN COVER REF. SIP.
- [SDR SWAA2025102025244](https://openairdocs.org/sdr/SWAA2025102025244.md): Battery · inoperative · Oct 17, 2025 · N8687A · Boeing 7378H4 · Emergency Equipment
  > AFT LH OB EMERGENCY FLASHLIGHT INOP. R & R THE EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00.
- [SDR SWAA2025092316604](https://openairdocs.org/sdr/SWAA2025092316604.md): Girt Bar · out of adjust · Sep 20, 2025 · N8687A · Boeing 7378H4 · Emergency Equipment
  > FORWARD SERVICE DOOR GIRT BAR EXTENDED MORE THAN NORMAL. ADJUSTED FWD SERVICE DOOR GIRT BAR PER AMM 25-66-01.
- [SDR SWAA2025082708038](https://openairdocs.org/sdr/SWAA2025082708038.md): Sign · detached · Aug 25, 2025 · N8687A · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD EXIT SIGN BETWEEN ROWS 15 AND 16 FELL FROM CEILING. REINSTALL OVERHEAD EXIT SIGN AS PER AMM 33-51-00. REINSTALLED OVERHEAD EXIT SIGN IAW AMM 33-51-01.
- [SDR SWAA2025052771563](https://openairdocs.org/sdr/SWAA2025052771563.md): Battery Pack · inoperative · May 16, 2025 · N8687A · Boeing 7378H4 · Emergency Lighting
  > LEFT OVER WING HATCH EMERGENCY LIGHTS INOP. R&R EMERGENCY LIGHT BATTERY PACK AT M1694 IAW AMM 33-51-06.
- [SDR SWAA2025052770777](https://openairdocs.org/sdr/SWAA2025052770777.md): Lens · missing · May 13, 2025 · N8687A · Boeing 7378H4 · Emergency Lighting
  > FWD LAVATORY EMERGENCY FLOOR PROXIMITY EXIT INDICATOR LIGHT LENS COVER LOCKING TAB ON THE BASE MISSING. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY; OPS CHECK GOOD IAW AMM 33-51-01.
- [SDR SWAA2025052867661](https://openairdocs.org/sdr/SWAA2025052867661.md): Fairing · debonded · May 6, 2025 · N8687A · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING #3 TRAILING EDGE FLAP AFT SUPPORT FAIRING TAILCONE HAS ELONGATED FASTENERS HOLES.<[01] REMOVED AND INSTALLED SERVICEABLE LEFT WING #3 TRAILING EDGE FLAP AFT SUPPORT FAIRING TAILCONE IAW AMM 27-51-18.;[02] COMPLIED WITH STEP#2 AND CORRECTIVE ACTION#1.
- [SDR SWAA2025052864520](https://openairdocs.org/sdr/SWAA2025052864520.md): Cowl Door · cracked · Apr 26, 2025 · N8687A · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > #1 ENGINE INBOARD FAN COWL; PANEL 414; WEB AFT OF OIL SERVICE DOOR CRACKED. REMOVED AND REPLACE #1 ENG I/B FAN COWL IAW AMM 71-11-02.
- [SDR SWAA2025052864522](https://openairdocs.org/sdr/SWAA2025052864522.md): Cowl Door · cracked · Apr 26, 2025 · N8687A · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > #2 ENGINE OUTBOARD FAN COWL; PANEL 424; WEB AFT OF THE OIL SERVICE DOOR CRACKED.<[01] REMOVED AND REPLACED #2 ENGINE OUTBOARD FAN COWL PER AMM 71-11-02 AND MT# 7111-E-17063-NG. REFERENCE TTG8Q00S5H19 FOR WORK ACCOMPLISHED AND PARTS INFORMATION.;[02] INSPECTED
- [SDR SWAA2025052764525](https://openairdocs.org/sdr/SWAA2025052764525.md): Seal · cracked · Apr 26, 2025 · N8687A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > TAIL PANEL 333AT BLADE SEAL CRACKED. REMOVED AND INSTALLED NEW SEAL PER. SRM 51-40-02.
- [SDR SWAA2025052764523](https://openairdocs.org/sdr/SWAA2025052764523.md): Seal · cracked · Apr 26, 2025 · N8687A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > PANEL 343AT METAL BLADE SEAL CRACKED. REMOVED AND INSTALLED NEW SEAL PER. SRM 51-40-02.
- [SDR SWAA2025052764531](https://openairdocs.org/sdr/SWAA2025052764531.md): Seal · cracked · Apr 26, 2025 · N8687A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > TAIL PANEL 323BL SLIDER SEAL CRACKED. REMOVED AND REPLACED SLIDER SEAL I.A.W SRM 51-40-02. REMOVED AND REPLACED SLIDER SEAL I.A.W SRM 51-40-02.
- [SDR SWAA2025052864261](https://openairdocs.org/sdr/SWAA2025052864261.md): Skin · delaminated · Apr 25, 2025 · N8687A · Boeing 7378H4 · Trailing Edge Flaps
  > R/H O/B AFT FLAP LOWER INBD CORNER HAS PREVIOUS REPAIR THAT HAS DELAMED. REMOVED PREVIOUS REPAIR;,NO ADDITIONAL DAMAGE NOTED PER SRM 57-53-01-2R-14, ACCOMPLISHED TAP TEST PER NDT MANUAL PART 1 51-05-01. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER & BONDE
- [SDR SWAA2025052764264](https://openairdocs.org/sdr/SWAA2025052764264.md): Bracket · cracked · Apr 25, 2025 · N8687A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON; LOWER AFT FAIRING CRACKED AT THE AFT 'V' SHAPE FITTING BRACKET THAT THE HYDRAULIC LINES PASS THROUGH. REMOVED DAMAGED #2 PYLON AFT FITTING BRACKET PER SRM 51-40-02. LOCATED, DRILLED, & INSTALLED #2 ENGINE AFT PYLON FAIRING AFT WEDGE BRACKE
- [SDR SWAA2025052153379](https://openairdocs.org/sdr/SWAA2025052153379.md): Panel · damaged · Apr 25, 2025 · N8687A · Boeing 7378H4 · Wing Main, Frame Structure
  > PANEL 561BB HAS ONE FASTENER HOLE THAT IS ELONGATED AND ALSO HAS COUNTER SINK DAMAGE.<[01] REPAIRED DAMAGED AREA PER SRM 51-70-08-0G-0.;[02] C/W INSPECTION
- [SDR SWAA2025052753370](https://openairdocs.org/sdr/SWAA2025052753370.md): Angle · cracked · Apr 24, 2025 · N8687A · Boeing 7378H4 · Fuselage Main, Bulkhead
  > CRACK FOUND ON VAPOR BARRIER ATTACH ANGLE RBL 34; STA 663<[01] REMOVED FASTENERS AND MATCH-DRILLED REPLACEMENT ANGLE PER SRM 51-40-02;[15] REMOVED AND REPLACED R/H VAPOR BARRIER ATTACH ANGLE @ STA 663 IAW SRM 51-40-02; BOEING DRAWING NUMBER 111A1000; AND EA M-
- [SDR SWAA2025052753374](https://openairdocs.org/sdr/SWAA2025052753374.md): Skin · delaminated · Apr 24, 2025 · N8687A · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT OUTBOARD AFT FLAP HAS A HUGE DELAMINATION ON THE UPPER INBOARD SURFACE. (MARKED)<[01] OK TO INSTALL AFT FLAP;[02] REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP PER. AMM 27-51-22PERFORMED LEFT WING OUTBOARD AFT FLAP ADJUSTMENT IAW AMM 27-51-22-400-801.;[03]
- [SDR SWAA2025052853315](https://openairdocs.org/sdr/SWAA2025052853315.md): Handle · loose · Apr 22, 2025 · N8687A · Boeing 7378H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR INNER HANDLE IS LOOSE. REMOVED AND REPLACED INTERIOR HANDLE BOLTS (2) EA IAW AMM 52-11-31. REMOVED AND REPLACED INTERIOR HANDLE BOLTS (2) EA IAW AMM 52-11-31 C/W INSPECTION
- [SDR SWAA2025052853356](https://openairdocs.org/sdr/SWAA2025052853356.md): Handle · out of adjust · Apr 22, 2025 · N8687A · Boeing 7378H4 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR EXTERIOR HANDLE WILL NOT RETRACT WHEN DOOR IS CLOSED. ADJUSTED DOOR IAW AMM 52-11-00. INSPECTED WORK PERFORMED
- [SDR SWAA2025040921923](https://openairdocs.org/sdr/SWAA2025040921923.md): Flashlight · failed · Apr 6, 2025 · N8687A · Boeing 7378H4 · Emergency Equipment
  > RIGHT HAND AFT INBOARD EMERGENCY FLASHLIGHT NOT TESTING. OK TO CONTINUE PER MEL 25-12-01; SP1B; AUTHORIZATION #245910 RIGHT HAND AFT INBOARD EMERGENCY FLASHLIGHT NOT TESTING. OK TO CONTINUE PER MEL 25-12-01 SP1B AUTHORIZATION # <[01]. REPLACED RH AFT INBOARD
- [SDR SWAA2025040822082](https://openairdocs.org/sdr/SWAA2025040822082.md): Flashlight · no test · Apr 5, 2025 · N8687A · Boeing 7378H4 · Emergency Equipment
  > CREW REPORTS RH AFT IB EMERGENCY FLASHLIGHT NOT TESTING<[01] REMOVED AND REPLACED RH AFT IB EMERGENCY FLASHLIGHT PER AMM 35-55-00
- [SDR SWAA2024102150426](https://openairdocs.org/sdr/SWAA2024102150426.md): Fuel Filter · contaminated · Oct 17, 2024 · N8687A · Boeing 7378H4 · Fuel Controlling System
  > AT APPROX 500 AGL # 2 FILTER BYPASS LIGHT ILLUMINATED<[01] PERFORMED FIM 73-05 TASK 801 THRU STEP 2.D.1.B. FOUND METAL CONTAMINATION IN FUEL FILTER. FILTER SENT TO PHX FOR ANALYSIS. REINSTALLED NEW FUEL FILTER AND PERFORMED IDLE LEAK CHECK WITH NO FUEL FILTER
- [SDR SWAA2024091135091](https://openairdocs.org/sdr/SWAA2024091135091.md): Panel · cracked · Sep 7, 2024 · N8687A · Boeing 7378H4 · Aerodynamic Fairings
  > CRACK ON PANEL 194 FL; EDGE OF APU DRAIN MAST HOLE. CRACK ON PANEL 194 FL EDGE OF APU DRAIN MAST HOLE.<[01] ACCOMPLISHED PERMANENT REPAIR PER.SRM.53-60-70-2R-1 REPAIR1; AND SRM.51-70-05-2R-1 REPAIR 1.;[02] C/W
- [SDR SWAA2024091135180](https://openairdocs.org/sdr/SWAA2024091135180.md): Panel · delaminated · Sep 7, 2024 · N8687A · Boeing 7378H4 · Aerodynamic Fairings
  > PANEL 194GL HAS DELAM 10IN. L X 1.25W EXTENDING 4IN.12IN. AFT OF PANEL L/E AND 13IN. UP FROM PANEL LOWER EDGE. PANEL 194GL HAS DELAM 10IN. L X 1.25W EXTENDING 4IN.12IN. AFT OF PANEL L/E AND 13IN. UP FROM PANEL LOWER EDGE.<[01] REPAIRED PANEL PER SRM 53-60-70-2
- [SDR SWAA2024082628698](https://openairdocs.org/sdr/SWAA2024082628698.md): Panel · cracked · Aug 21, 2024 · N8687A · Boeing 7378H4 · Fuselage Main, Structure
  > A CRACK ON THE EDGE OF THE HOLE WHERE THE APU DRAIN MAST LINE GO THROUGH ON PANEL 194FL.<[01] ACCOMPLISHED EA 24-153-02300
- [SDR SWAA2024082328697](https://openairdocs.org/sdr/SWAA2024082328697.md): Drain Mast · missing · Aug 21, 2024 · N8687A · Boeing 7378H4 · Aircraft Fuel Distribution System
  > APU FUEL DRAIN MAST MISSING<[01] ADDED PART INFORMATION;[02] INSTALLED APU DRAIN MAST PER AMM 28-25-07
- [SDR SWAA2024052988739](https://openairdocs.org/sdr/SWAA2024052988739.md): Skin · cracked · May 22, 2024 · N8687A · Boeing 7378H4 · Fuselage Main, Structure
  > FOUND POWER RECEPTACLE LOWER SKIN EDGE CRACKED<[01] ACCOMPLISHED REPAIR PER SRM 51-40-02-0G-0 SRM 53-10-15-2R-4 REPAIR 4 IPC 52-48-51-02B DWG 141A3722;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024052987971](https://openairdocs.org/sdr/SWAA2024052987971.md): Battery Pack · inoperative · May 20, 2024 · N8687A · Boeing 7378H4 · Emergency Lighting
  > SEVERAL PAX CABIM EMERGENCY LIGHTS INOP<[01] PERFORMED T/S OF EMERGENCY LIGHTS FOUND M1676; M1670; M1671; AND M1673 DEFECTS; REF. TO B 737 FIM TASK 33-50-TASK 801.<BR>REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACKS AT POSITIONS M1676; M1670; M1671 & M1673
- [SDR SWAA2024052986487](https://openairdocs.org/sdr/SWAA2024052986487.md): Floor Panel · installed · May 16, 2024 · N8687A · Boeing 7378H4 · Fuselage Floor Panel
  > INSPECTION REJECTION: FAILURE TO BE ACCOMPLISHED (NDT) HFEC PROCEDURE OF THE TRIMMED EDGE FOR FREE CRACK CONDITION INDICATED PER EA M-21-153-00734 REF: TTG8Q00T3V7U.<[01] ACCOMPLISHED FLIGHT DECK FLOOR REPAIR PER EA M-21-153-00734 SRM 51-40-02-0G-0 DRW 141A063
- [SDR SWAA2024052983358](https://openairdocs.org/sdr/SWAA2024052983358.md): Scuff Plate · cracked · May 7, 2024 · N8687A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FOUND AFT CARGO AFT SCUFF PLATE AFT CORNER HAS A CRACK. REPAIRED AFT CARCO AFT SCUFF PLATE.
- [SDR SWAA2024052882230](https://openairdocs.org/sdr/SWAA2024052882230.md): Floor Panel · delaminated · May 4, 2024 · N8687A · Boeing 7378H4 · Fuselage Floor Panel
  > FWD WET AREA FLOOR PANEL DELAMINATED PART # 141A5810-464<[01] LATE ENTRY: RECEIVED NEW FLOOR PANEL PN# 141A5810-464 INSTALLATION WAS ACCOMPLISHED 5/16/2024 ON #TTG8Q00S01F9.;[02] FINAL INSPECTION; VERIFIED STEP #1.;[03] AUDIT C/W REF. MPM 52.02.02.
- [SDR SWAA2024052981709](https://openairdocs.org/sdr/SWAA2024052981709.md): Floor Support · cracked · May 2, 2024 · N8687A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACKED AT FASTENER HOLES BL 0 BETWEEN BS 380 & 400. REMOVED AND INSTALLED NEW ANGLE SUPPORT UPPER CAP AT FWD CABIN FLOOR SUPPORT INTERCOSTAL UPPER CAP IAW SRM 51-40-02-0G-0.
- [SDR SWAA2024052981701](https://openairdocs.org/sdr/SWAA2024052981701.md): Floor Support · cracked · May 2, 2024 · N8687A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACK AT LBL 13 BETWEEN STA 380 AND STA 400. REMOVED AND INSTALLED NEW FLOOR SUPPORT INTERCOSTAL UPPER CAP AT FWD CABIN WET AREA LBL 13 BETWEEN BS 380 & 400 IAW SRM-51-40-02-0G-0 AND DWG 143A5400.
- [SDR SWAA2024052981710](https://openairdocs.org/sdr/SWAA2024052981710.md): Floor Panel · delaminated · May 2, 2024 · N8687A · Boeing 7378H4 · Fuselage Floor Panel
  > FWD CABIN WET AREA FLOOR PANEL 221GF TOP LAYER DELAMITED AND FWD O/B CORNER BROKEN. FAULT WAS RESOLVED ON ANOTHER FAULT; REF TO TTG8Q00T3U69. FOR INSTALLATION REF TO TTG8Q00S01RX.
- [SDR SWAA2024052981935](https://openairdocs.org/sdr/SWAA2024052981935.md): Floor Support · cracked · May 2, 2024 · N8687A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL 1. REMOVED AND INTALLED NEW SUPPORT BREAK AT MAIN CABIN CENTER SECTION FLOOR PER SRM 51-40-02-0G-0.
- [SDR SWAA2024052981940](https://openairdocs.org/sdr/SWAA2024052981940.md): Floor Support · cracked · May 2, 2024 · N8687A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL 1. REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK AT STA 540 RBL 1 REF. SRM 51-40-02-0G-0.
- [SDR SWAA2024052981700](https://openairdocs.org/sdr/SWAA2024052981700.md): Floorbeam · corroded · May 2, 2024 · N8687A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION SPOT FOUND AT FWD CABIN WET AREA FLOOR SUPPORT BEAM TOP SURFACE<BR>STA 294.5 RBL 13 MKD DOT<[01] STEP 14 FABRICATED ANGLES NOT HEAT TREATED;[02] CORRECTION: REJECT: STEP 14 FABRICATED ANGLES NOT HEAT TREATED;[03] REJECTION COMPLETED.;[04] ACCOMPLISHE
- [SDR SWAA2024052981943](https://openairdocs.org/sdr/SWAA2024052981943.md): Floorbeam · corroded · May 2, 2024 · N8687A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR BEAM SUPPORT STA 947.5;RBL50 AFT OUTBOARD FITTING SUPPORT GALLEY;AT INBOARD POSITION HAS CORROSION.<[01] ACCOMPLISHED REPAIR AT AFT WET AREA FLOOR BEAM SUPPORT STA 947.5 RBL50 AS PER SRM-53-70-51-2R-5 AND SRM-51-40-02-0G-0.<BR>SEALANT MIXED
- [SDR SWAA2024052981951](https://openairdocs.org/sdr/SWAA2024052981951.md): Retainer · cracked · May 2, 2024 · N8687A · Boeing 7378H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STAB UPPER PANEL 333AT BLADE SEAL RETAINER CRACK.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STAB UPPER PANEL 333AT BLADE SEAL RETAINER AS PER SRM 51-40-02-0G-0;[02] VERIFIED LEFT HORIZONTAL STAB UPPER PANEL 333AT BLADE SEAL RETAINER REPLACEMENT
- [SDR SWAA2024052981952](https://openairdocs.org/sdr/SWAA2024052981952.md): Retainer · cracked · May 2, 2024 · N8687A · Boeing 7378H4 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STAB PANEL 343AT BLADE SEAL RETAINER CRACK.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB PANEL 343AT BLADE SEAL RETAINER REF. SRM 51-40-02-0G-0;[02] VERIFIED RIGHT HORIZONTAL STAB PANEL 343AT BLADE SEAL RETAINER REPLACEMENT.;[03] AUDIT
- [SDR SWAA2024052981706](https://openairdocs.org/sdr/SWAA2024052981706.md): Web · cracked · May 2, 2024 · N8687A · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING DEFLECTOR RIB CONTROL FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER WEB CRACKED @ O/B END. REMOVED AND INSTALLED NEW WEB RETAINER AT LEFT WING DEFLECTOR RIB CONTROL FIXED PANEL LOWER HORIZONTAL AS PER SRM-51-40-02-0G-0. VERIFIED STEP 1 FINAL AUD
- [SDR SWAA2024052981435](https://openairdocs.org/sdr/SWAA2024052981435.md): Plate · corroded · May 1, 2024 · N8687A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AT AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB PLATE. COMPLETED INSTALLATION OF NEW LOWER SILL WEB AT AFT CARGO COMPARTMENT DOOR CUTOUT PER SRM 51-40-02-0G-0 AND DWG#146A8340;[02] VERIFIED INSTALLATION OF NEW LOWER SILL WEB AT AFT CARGO COMPA
- [SDR SWAA2024052981437](https://openairdocs.org/sdr/SWAA2024052981437.md): Channel · corroded · May 1, 2024 · N8687A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT L/H SIDE FLOOR SUPPORT Z CHANNEL CORRODED S-26L FROM STA 727E STA 807. REMOVED; RECEIVED AND INSTALLED NEW SUPPORT Z CHANNEL AT AFT CARGO L/H BTW STA 727E TO 807 AS PER B737-700 SRM 51-40-02-0G-0 AND DWG#146A7500.;[02] FINAL INSPECTION;
- [SDR SWAA2024052981440](https://openairdocs.org/sdr/SWAA2024052981440.md): Strap · corroded · May 1, 2024 · N8687A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR SUPPORT STRAP FASTENER HOLE AT S26R BS 887. REMOVED CORROSION AT AFT CARGO BAY FLOOR SUPPORT STRAP FASTENER HOLE AT S26R BS 887 IAW SRM 51-10-02-0G-0 & SRM 53-00-53-1A-2. REVEALED CRACK ON THE FLOOR SUPPORT STRAP FASTENER HOLE & FOUND TO

Next page: https://openairdocs.org/aircraft/N8687A/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 = 'N8687A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8687A/reports

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