# Service difficulty reports: N8676A

A list on [N8676A](https://openairdocs.org/aircraft/N8676A.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 5 · 230 reports

- [SDR SWAA2026082401590](https://openairdocs.org/sdr/SWAA2026082401590.md): Wire · detached · Aug 19, 2026 · N8676A · Boeing 7378H4 · Light System Wiring
  > L1 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. FOUND WIRE W3142-0151-16 REMOVED FROM GROUND BLOCK GD3876. RE-PINNED WIRE TO GROUND BLOCK AND OPS CHECK OF EMERGENCY LIGHT L731 IS GOOD IAW WDM 33-51-12, SWPM 20-90-11, AND AMM 33-51-00-710-801.
- [SDR SWAA2026082475413](https://openairdocs.org/sdr/SWAA2026082475413.md): Handle · loose · Aug 12, 2026 · N8676A · Boeing 7378H4 · Service Doors
  > ASSIST HANDLE ON G1 GALLEY LOOSE. SECURED ASSIST HANDLE ON G1 GALLEY IAW AMM 25-31-11-400-801 SUBTASK 25-31-11-410-016.
- [SDR SWAA2026082411258](https://openairdocs.org/sdr/SWAA2026082411258.md): Lens · damaged · Aug 11, 2026 · N8676A · Boeing 7378H4 · Emergency Lighting
  > FORWARD L1 DOOR EXIT LENS REQUIRES REPLACEMENT. REMOVED AND REPLACED THE FWD L1 DOOR EXIT LIGHT LENS IAW AMM 33-51-01-960-801.
- [SDR SWAA2026082469658](https://openairdocs.org/sdr/SWAA2026082469658.md): Lamp · inoperative · Aug 11, 2026 · N8676A · Boeing 7378H4 · Emergency Lighting
  > L1 DOOR EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED L1 DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801. OPS CHECKED GOOD.
- [SDR SWAA2026082446338](https://openairdocs.org/sdr/SWAA2026082446338.md): Skin · delaminated · Aug 11, 2026 · N8676A · Boeing 7378H4 · Trailing Edge Flaps
  > FOUND LEFT OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22-401.
- [SDR SWAA2026082456139](https://openairdocs.org/sdr/SWAA2026082456139.md): Skin · delaminated · Aug 11, 2026 · N8676A · Boeing 7378H4 · Trailing Edge Flaps
  > FOUND RT OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT FLAP IAW AMM 27-51-22.
- [SDR SWAA2026082495892](https://openairdocs.org/sdr/SWAA2026082495892.md): Handle · unsecure · Aug 11, 2026 · N8676A · Boeing 7378H4 · Passenger/Crew Doors
  > L2 DOOR AIRFRAME SIDE ASSIST HANDLE NEEDS SECURED SECURED ASSIST HANDLE ON AIRFRAME SIDE AT L2 DOOR IAW AMM 25-21-25-420-801 SUBTASK 25-21-25-420-004 SECURED ASSIST HANDLE ON AIRFRAME SIDE AT L2 DOOR IAW AMM 25-21-25-420-801 SUBTASK 25-21-25-420-004.
- [SDR SWAA2026082475326](https://openairdocs.org/sdr/SWAA2026082475326.md): Handle · unsecure · Aug 11, 2026 · N8676A · Boeing 7378H4 · Service Doors
  > R2 DOOR AIRFRAME SIDE ASSIST HANDLE NEEDS SECURED. SECURED ASSIST HANDLE AT R2 DOOR AIRFRAME SIDE IAW AMM 25-21-25-420-801.
- [SDR SWAA2026082440515](https://openairdocs.org/sdr/SWAA2026082440515.md): Lamp · inoperative · Aug 11, 2026 · N8676A · Boeing 7378H4 · Emergency Lighting
  > L2 EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS, OP CHECKED L2 DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801. EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR SWAA2026082415394](https://openairdocs.org/sdr/SWAA2026082415394.md): Handle · unsecure · Aug 11, 2026 · N8676A · Boeing 7378H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED ASSIST HANDLE AT L1 DOOR IAW AMM 52-11-31-400-802 SUBTASK 52-11-31-020-011.
- [SDR SWAA2026010859154](https://openairdocs.org/sdr/SWAA2026010859154.md): Relay · failed · Jan 7, 2026 · N8676A · Boeing 7378H4 · Stabilizer Control System
  > ELECTRIC STAB TRIM FAIL DURING CLIMB OUT, AUTOPILOT WAS NOT ENGAGED. NEITHER CAP OR FO ELECTRIC STAB TRIM WAS OPERATIONAL. MANUAL TRIM OPERATED NORMALLY. R & R R64 STAB TRIM CONTROL RELAY IAW WDM 27-41-12. NO DEFECTS NOTED.
- [SDR SWAA2025122254054](https://openairdocs.org/sdr/SWAA2025122254054.md): Cover · loose · Dec 19, 2025 · N8676A · Boeing 7378H4 · Emergency Lighting
  > FWD SERVICE DOOR EXIT COVER (LOWER) CAME OFF. SECURED FWD SERVICE DOOR EXIT COVER IAW MM 33-51-01
- [SDR SWAA2025121552653](https://openairdocs.org/sdr/SWAA2025121552653.md): Trim Motor · inoperative · Dec 13, 2025 · N8676A · Boeing 7378H4 · Stabilizer Control System
  > CREW REPORTS STAB TRIM INOPERATIVE, WORKS WITH AUTOPILOT. R & R STABILIZER TRIM MOTOR IAW AMM 27-41-71. TESTED GOOD IAW AMM 27-41-71-700-801.
- [SDR SWAA2025103030124](https://openairdocs.org/sdr/SWAA2025103030124.md): Bulb · inoperative · Oct 30, 2025 · N8676A · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT, AFT OF L2 DOOR NO ILLUMINATION DURING EMERGENCY LIGHT OPS CHK. PLACED THE BULB IAW MM 33-51-00.
- [SDR SWAA2025091614417](https://openairdocs.org/sdr/SWAA2025091614417.md): Battery · inoperative · Sep 14, 2025 · N8676A · Boeing 7378H4 · Emergency Lighting
  > LH EMERGENCY. EXIT LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY AT LT 12CBA POSITION.
- [SDR SWAA2025062384569](https://openairdocs.org/sdr/SWAA2025062384569.md): Sensor · faulty · Jun 23, 2025 · N8676A · Boeing 7378H4 · Leading Edge Slat Control System
  > LE FLAP TRANSIT LIGHT CAME ON WHEN FLAPS 15 SELECTED AND STAYED ON <[01]. R&R #4 LEADING EDGE FLAP PROXIMITY SENSOR REF AMM 27-88-11. OPS CHECK GOOD.
- [SDR SWAA2024122379900](https://openairdocs.org/sdr/SWAA2024122379900.md): Light · inoperative · Dec 20, 2024 · N8676A · Boeing 7378H4 · Emergency Lighting
  > FORWARD ENTRY DOOR SLIDE EMERGENCY LIGHT INOP<[01] RE LAMPED FORWARD ENTRY DOOR SLIDE EMERGENCY LIGHT;OPS CHECKS GOOD PER MM 33-51-04;[02] RE LAMPED FORWARD ENTRY DOOR SLIDE EMERGENCY LIGHT;OPS CHECKS GOOD PER MM 33-51-04. ADDED SELECT REFERENCE.;[03] VERIFIED
- [SDR SWAA2024122379541](https://openairdocs.org/sdr/SWAA2024122379541.md): Megaphone · broken · Dec 19, 2024 · N8676A · Boeing 7378H4 · Emergency Equipment
  > FORWARD CABIN MEGAPHONE HANDLE IS BROKEN AWAY FROM HORN.<[01] REPLACED FWD CABIN MEGAPHONE IN REFERENCE TO AMM 25-64-00.;[02] ROBERT WALESA (TECHNICIAN); 19-DEC-2024 18:57 UTC<BR>REPLACED FWD CABIN MEGAPHONE IN REFERENCE TO AMM 25-64-00.
- [SDR SWAA2024122378971](https://openairdocs.org/sdr/SWAA2024122378971.md): Battery Pack · inoperative · Dec 18, 2024 · N8676A · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVER WING EXIT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED RIGHT OVER WING EMERGENCY LIGHT BATTERY PACK;ROW 13R PER MM 33-51-06. OPS CHECKS GOOD PER MM 33-51-00;[02] INSPECTED WORK PERFORMED
- [SDR SWAA2024122375283](https://openairdocs.org/sdr/SWAA2024122375283.md): Channel · cracked · Dec 9, 2024 · N8676A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOORBOARD SUPPORT CHANNEL CRACKED AT I/B ATTACH POINT AT APPROXIMATELY STA. 540 BETWEEN FLOOR BEAM AT LBL 0.07 TO SEAT TRACK FLOOR BEAM AT RBL 24.82.<[01] REMOVED DAMAGE FLOOR BOARD SUPPORT (BREAK ASSY-PNL) AT ST. 540 BETWEEN FLOOR BEAM AT LBL 0.07 TO SEAT TR
- [SDR SWAA2024122375284](https://openairdocs.org/sdr/SWAA2024122375284.md): Channel · cracked · Dec 9, 2024 · N8676A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOORBOARD SUPPORT CHANNEL CRACKED AT I/B ATTACH POINT AT APPROXIMATELY STA. 540 BETWEEN FLOOR BEAM AT LBL 0.07 TO SEAT TRACK FLOOR BEAM AT LBL 24.82.<[01] REMOVED DAMAGE FLOOR BOARD SUPPORT (BREAK ASSY-PNL) AT ST. 540 BETWEEN FLOOR BEAM AT LBL 0.07 TO SEAT TR
- [SDR SWAA2024122374443](https://openairdocs.org/sdr/SWAA2024122374443.md): Mount Bracket · cracked · Dec 5, 2024 · N8676A · Boeing 7378H4 · Wing Miscellaneous Structure
  > PANEL 551FB HAS A CRACKED MOUNTING ANGLE. REMOVED AND REPLACED MOUNTING BRACKET PER SRM 51-40-02. INSPECTED WORK PERFORMED. REMOVED AND REPLACED MOUNTING BRACKET PER SRM 51-40-02.
- [SDR SWAA2024122374124](https://openairdocs.org/sdr/SWAA2024122374124.md): Bracket · cracked · Dec 5, 2024 · N8676A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 414 FAN COWL ASSY. #1 ENGINE INBOARD: OIL DOOR WIND DEFLECTOR BRACKET IS CRACKED. MARKED. PANEL 414 FAN COWL ASSY. #1 ENGINE INBOARD: OIL DOOR WIND DEFLECTOR BRACKET IS CRACKED. MARKED.<[01] #1 ENGINE I/B (R/H) FAN COWL WAS REPLACED ON TASK CARD TTG8Q00S
- [SDR SWAA2024122374442](https://openairdocs.org/sdr/SWAA2024122374442.md): Attach Bracket · cracked · Dec 5, 2024 · N8676A · Boeing 7378H4 · Wing, Attach Fittings
  > DEFLECTION RIB ATTACH BRACKET IS CRACKED<[01] REMOVED DAMAGED BRACKET PER SRM 51-40-02.;[02] REMOVED AND REPLACED DEFLECTION RIB ATTACH CLIP PER SRM 51-40-02.;[03] 2. THOMAS BAUER (TECHNICIAN); 07-DEC-2024 21:25 UTC<BR>REMOVED AND REPLACED DEFLECTION RIB ATTAC
- [SDR SWAA2024122073800](https://openairdocs.org/sdr/SWAA2024122073800.md): Floor Panel · delaminated · Dec 3, 2024 · N8676A · Boeing 7378H4 · Fuselage Floor Panel
  > CENTER CABIN FLOOR PANEL 241 GF DELAMINATED<[01] REMOVED AND REPLACED WITH NEW SERVICEABLE FLOOR PANEL IAW AMM 53-21-00.;[02] C/W INSPECTION
- [SDR SWAA2024122073801](https://openairdocs.org/sdr/SWAA2024122073801.md): Floor Panel · delaminated · Dec 3, 2024 · N8676A · Boeing 7378H4 · Fuselage Floor Panel
  > CENTER CABIN FLOOR PANEL 241 KF DELAMINATED<[01] REMOVED AND REPLACED WITH NEW SERVICEABLE FLOOR PANEL 241KF PER AMM 53-21-00.;[02] COMPLIED WITH CORRECTIVE ACTION #1.
- [SDR SWAA2024122073802](https://openairdocs.org/sdr/SWAA2024122073802.md): Floor Panel · delaminated · Dec 3, 2024 · N8676A · Boeing 7378H4 · Fuselage Floor Panel
  > CENTER CABIN FLOOR PANEL 241 RF DELAMINATED<[01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00-400-801.;[02] COMPLIED WITH CORRECTIVE ACTION#1.
- [SDR SWAA2024122373310](https://openairdocs.org/sdr/SWAA2024122373310.md): Attach Angle · cracked · Dec 2, 2024 · N8676A · Boeing 7378H4 · Wing, Attach Fittings
  > RW TE COVE; FIRST RIB INBOARD OF THE DEFLECTION CONTROL RIB (ORSS 275); UPPER INBOARD SIDE OF THE RIB ATTACH ANGLE IS CRACKED RW TE COVE FIRST RIB INBOARD OF THE DEFLECTION CONTROL RIB (ORSS 275) UPPER INBOARD SIDE OF THE RIB ATTACH ANGLE IS CRACKED<[01] REMOV
- [SDR SWAA2024122373311](https://openairdocs.org/sdr/SWAA2024122373311.md): Attach Angle · cracked · Dec 2, 2024 · N8676A · Boeing 7378H4 · Wing, Attach Fittings
  > RW DEFLECTION CONTROL RIB; INBOARD AFT ATTACH ANGLE CRACKED RW DEFLECTION CONTROL RIB INBOARD AFT ATTACH ANGLE CRACKED<[01] REMOVED AND REPLACED INBOARD AFT ATTACH ANGLE PER SRM 51-40-02.;[02] VERIFIED REPLACEMENT OF THE INBOARD AFT ATTACH ANGLE BRACKET PER SR
- [SDR SWAA2024122373308](https://openairdocs.org/sdr/SWAA2024122373308.md): Angle · cracked · Dec 2, 2024 · N8676A · Boeing 7378H4 · Wing Miscellaneous Structure
  > L/H WING DEFLECTION RIB; UPPER PANEL; CENTER COVE RIB ANGLE CRACKED(BACKSIDE).<[01] REMOVED CRACKED ANGLE PER SRM 51-40-02.;[02] REMOVED AND REPLACED INBD.DEFLECTION RIB CENTER COVE ATTACH ANGLE PER SRM 51-40-02.;[03] THOMAS BAUER (TECHNICIAN); 08-DEC-2024 01:
- [SDR SWAA2024122372990](https://openairdocs.org/sdr/SWAA2024122372990.md): Floor Panel · cracked · Nov 30, 2024 · N8676A · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 661BB HAS SEVERAL FASTENER HOLES DAMAGED; PULLED SURFACE & CRACKING.<[01] FILLED DAMAGED HOLES; APPLIED PRE-PREG REPAIR PLIES AND COOKED REPAIR PER SRM 51-70-05-2R-9.;[02] ENTERED IN ERROR;[03] REPAIRED DAMAGED FASTENER HOLES PER SRM 51-70-05-2R-9.;[04]
- [SDR SWAA2024122372730](https://openairdocs.org/sdr/SWAA2024122372730.md): Attach Angle · cracked · Nov 30, 2024 · N8676A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > L/H A/C BAY AFT WALL STA 663 AND APPROX. LBL 8 VAPOR BARRIER ATTACH ANGLE IS CRACKED AT RIVET HOLE IN VERTICAL FLANGE.<[01] CUT AND REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5;[02] COMPLIED WITH SURFACE INSPECTION OF CUTOUT AND HOLE PROBE INS
- [SDR SWAA2024122372727](https://openairdocs.org/sdr/SWAA2024122372727.md): Attach Angle · cracked · Nov 30, 2024 · N8676A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > R/H A/C BAY AFT WALL STA 663 AND APPROX. RBL 8 VAPOR BARRIER ATTACH ANGLE IS CRACKED AT RIVET HOLE IN VERTICAL FLANGE.<[01] CUT AND REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5;[02] COMPLIED WITH SURFACE INSPECTION OF CUTOUT AND HOLE PROBE INS
- [SDR SWAA2024021551810](https://openairdocs.org/sdr/SWAA2024021551810.md): Battery Pack · inoperative · Feb 13, 2024 · N8676A · Boeing 7378H4 · Emergency Lighting
  > CEILING EMRGCY LTS INOP @ ROW 18;21 DEF<[01] R/R EMRGCY LT BATT PACK @ ROW 20 DEF PER AMM 33-51-06. LIGHT OPS - OK.
- [SDR SWAA2023122732899](https://openairdocs.org/sdr/SWAA2023122732899.md): Battery Pack · inoperative · Dec 17, 2023 · N8676A · Boeing 7378H4 · Emergency Lighting
  > AFT GALLEY R/H EMERGENCY LIGHT BATTERY PACK INOP<[01] REMOVED AND REPLACED EMAERGENCY LIGHT BATTERY PACK AT STA 952R PER MM 33-51-06;[02] AFT GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[03] INSPECTED AS REQUIRED
- [SDR SWAA2023122732985](https://openairdocs.org/sdr/SWAA2023122732985.md): Battery Pack · inoperative · Dec 17, 2023 · N8676A · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHTS BATTERY PACK AT STA 565L IS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 565L PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] INSPECTED AS REQUIRED
- [SDR SWAA2023122732986](https://openairdocs.org/sdr/SWAA2023122732986.md): Battery Pack · inoperative · Dec 17, 2023 · N8676A · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 565R IS INOP<[01] REMOVED AND REPLACE EMERGENCY LIGHT BATTERY PACK AT STA 565R PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] INSPECTED AS REQUIRED
- [SDR SWAA2023122831574](https://openairdocs.org/sdr/SWAA2023122831574.md): Track · cracked · Dec 14, 2023 · N8676A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORIZONTAL STAB UPPER AFT BLADE SEAL FWD TRACK IS CRACKED.<[01] INSTALLED R/H HORIZONTAL STAB UPPER AFT BLADE SEAL FWD TRACK PER SRM 51-40-02;[02] VERIFIED INSTALLATION OF NEW R/H HORIZONTAL STAB UPPER AFT BLADE SEAL FWD TRACK PER SRM 51-40-02
- [SDR SWAA2023122833189](https://openairdocs.org/sdr/SWAA2023122833189.md): Stringer · incorrect · Dec 7, 2023 · N8676A · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > BS 727 INNER CHORD AT STRINGER 18A LEFT SIDE GAP IS 0.018'<[01] REPAIRED PER EO-5311-E-14577-NG.;[02] REPAIRED PER EO-5311-E-14577-NG ON FAULT #TTG8Q00Q4Y4H.;[03] INSPECTED AS REQUIRED
- [SDR SWAA2023122833290](https://openairdocs.org/sdr/SWAA2023122833290.md): Stringer · incorrect · Dec 7, 2023 · N8676A · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > BS 727 INNER CHORD AT STRINGER 18A RIGHT SIDE GAP IS 0.045' AT THE UPPER AND 0.040' AT THE BOTTOM<[01] REPAIRED PER EO-5311-E-14625-NG ON FAULT #TTG8Q00Q4Z2Z.;[02] VERIFIED ALL WORK STEPS COMPLETED ON EO-5311-E-14625-NG
- [SDR SWAA2023122828959](https://openairdocs.org/sdr/SWAA2023122828959.md): Angle · corroded · Dec 7, 2023 · N8676A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO RH TRANSITION ANGLE HAS CORROSION FROM STA. 500E TO 500F.<[01] BLENDED AREAS; REMOVED.010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED DAMAGE FROM STA. 500D+10 TO 500F+10 PER SRM 53-00-53-2R-5. FABRICATED REPAIR PARTS PER
- [SDR SWAA2023122828480](https://openairdocs.org/sdr/SWAA2023122828480.md): Nut · inoperative · Dec 6, 2023 · N8676A · Boeing 7378H4 · Escape Slide
  > FORWARD ENTRY DOOR ESCAPE SLIDE FORWARD MOUNT BARREL NUT BAD.<[01] REPLACED BARREL NUT PER SOPM 20-50-01.;[02] C/W INSPECTION.
- [SDR SWAA2023122828481](https://openairdocs.org/sdr/SWAA2023122828481.md): Fastener · loose · Dec 6, 2023 · N8676A · Boeing 7378H4 · Emergency Equipment
  > FORWARD ENTRY DOOR ESCAPE SLIDE RIGHT HAND GIRT BAR BRACKET LOOSE.<[01] R/R FASTENER IAW SRM 51-40-02.;[02] C/W INSPECTION.
- [SDR SWAA2023122728495](https://openairdocs.org/sdr/SWAA2023122728495.md): Plate · loose · Dec 6, 2023 · N8676A · Boeing 7378H4 · Galley Doors
  > AFT SERVICE DOOR INTERNAL HANDLE CAMPLATE LOOSE.<[01] SECURED CAMPLATE PER M/M REF 52-41-11;[02] C/W INSPECTION.
- [SDR SWAA2023122827970](https://openairdocs.org/sdr/SWAA2023122827970.md): Floor Panel · delaminated · Dec 5, 2023 · N8676A · Boeing 7378H4 · Fuselage Floor Panel
  > FOLLOWING FWD WET AREA FLOOR BOARDS HAVE DENTS/DELAMINATION; 231CF; 231BF; 231AF; 222DF; 222CF; 221GF; 221FF; 221EF; 221CF; AND 221DF.<[01] REPLACED FLOOR PANEL 231AF ON TTG8Q00P6GLG.<BR>REPLACED FLOOR PANEL 231BF ON TTG8Q00P6GLE.<BR>REPLACED FLOOR PANEL 231CF
- [SDR SWAA2023122827972](https://openairdocs.org/sdr/SWAA2023122827972.md): Floor Panel · delaminated · Dec 5, 2023 · N8676A · Boeing 7378H4 · Fuselage Floor Panel
  > 221BF AND 221AF FWD WET AREA FLOOR BOARDS HAVE DENTS/DELAMINATION.<[01] NEW FLOOR PANEL 221BF INSTALLED ON TTG8Q00P6GMR<BR>NEW FLOOR PANEL 221AF INSTALLED ON TTG8Q00P6GM4;[02] NEW FLOOR PANEL 221BF INSTALLED ON TTG8Q00P6GM2<BR>NEW FLOOR PANEL 221AF INSTALLED O
- [SDR SWAA2023122827679](https://openairdocs.org/sdr/SWAA2023122827679.md): Liner · torn · Dec 5, 2023 · N8676A · Boeing 7378H4 · Service Doors
  > FWD SERVICE DOOR (R-1) LINER TEDLAR COVERING TORN IN 2 AREAS. (SLIDE MOUNT FASTENER AND HANDLE AREAS MARKED)<[01] REMOVED AND REPLACED LINER PER M/M REF 52-41-31;[02] NEW DOOR LINER TO BE INSTALLED ON FAULT TTG8R007M6VR.
- [SDR SWAA2024010227240](https://openairdocs.org/sdr/SWAA2024010227240.md): Angle · corroded · Dec 4, 2023 · N8676A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA 727G+6 LBL 21 WL 156. MRKD<[01] REPAIR ACCOMPLISHED ON CARD TTG8Q00Q22QW.
- [SDR SWAA2024010227232](https://openairdocs.org/sdr/SWAA2024010227232.md): Angle · corroded · Dec 4, 2023 · N8676A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA 727G+9 LBL 21 WL 156. MRKD<[01] REPAIR ACCOMPLISHED ON CARD TTG8Q00Q22QW.
- [SDR SWAA2024010227233](https://openairdocs.org/sdr/SWAA2024010227233.md): Angle · corroded · Dec 4, 2023 · N8676A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA 727G+13 LBL 21 WL 156. MRKD<[01] REPAIR ACCOMPLISHED ON CARD TTG8Q00Q22QW.

Next page: https://openairdocs.org/aircraft/N8676A/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 = 'N8676A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8676A/reports

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