# Service difficulty reports: N8671D

A list on [N8671D](https://openairdocs.org/aircraft/N8671D.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 · 98 reports

- [SDR SWAA2026082689480](https://openairdocs.org/sdr/SWAA2026082689480.md): Light · intermittent · Aug 22, 2026 · N8671D · Boeing 7378H4 · Emergency Lighting
  > AFT EMERGENCY EXIT FLUORESCENT LIGHT ON F/O SIDE FLICKERS. PERFORMED OPS CHECK OF AFT RIGHT OVERWING EMERGENCY EXIT SIDE WALL LIGHT REF AMM 33-21-00. OPS CHECK GOOD. OPS CHECK OF EMERGENCY LIGHT GOOD REF AMM 33-51-00.
- [SDR SWAA2026081296229](https://openairdocs.org/sdr/SWAA2026081296229.md): Lens · detached · Aug 8, 2026 · N8671D · Boeing 7378H4 · Emergency Lighting
  > CENTER EMERGENCY EXIT LIGHT FELL OFF, SECURED EMERGENCY LIGHT LENS ON IAW AMM 33-51-01.
- [SDR SWAA2026010959153](https://openairdocs.org/sdr/SWAA2026010959153.md): Light · detached · Jan 7, 2026 · N8671D · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT AT ROW 23 SEAT C, FELL OUT OF CEILING. REINSTALLED LIGHT ASSEMBLY AT ROW 23 SEAT C IAW AMM 33-51-03
- [SDR SWAA2025121043206](https://openairdocs.org/sdr/SWAA2025121043206.md): Battery Pack · inoperative · Dec 5, 2025 · N8671D · Boeing 7378H4 · Emergency Lighting
  > R1 DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND INSTALLED EMERGENCY BATTERY PACK FOR R1 DOOR AMM 33-51-06-960-805 AND OPS CHECK GOOD. REMOVED AND INSTALLED EMERGENCY BATTERY PACK FOR R1 DOOR IAW AMM 33-51-06-960-805 AND OPS CHECK GOOD.
- [SDR SWAA2025110631204](https://openairdocs.org/sdr/SWAA2025110631204.md): Girt Bar · loose · Nov 3, 2025 · N8671D · Boeing 7378H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR BRACKET RIVETS LOOSE. OK TO CONTINUE PER TLD EA M-23-125-01839.
- [SDR SWAA2025071491117](https://openairdocs.org/sdr/SWAA2025071491117.md): Engine · failed · Jul 13, 2025 · N8671D · Boeing 7378H4 · Engine (Turbine/Turboprop)
  > ENGINE FAILURE AFTER DEPARTURE AT 3000. R&R #1ENGINE IN REF MT 771-00-01. OPS & LEAK CHECK GOOD. AIRCRAFT OK TO CONTINUE IN SERVICE.
- [SDR SWAA2025071590378](https://openairdocs.org/sdr/SWAA2025071590378.md): Engine · failed · Jul 11, 2025 · N8671D · Boeing 7378H4 · Engine (Turbine/Turboprop)
  > ENGINE FAILURE AFTER DEPARTURE @ 3000'
- [SDR SWAA2025071089127](https://openairdocs.org/sdr/SWAA2025071089127.md): Flashlight · inoperative · Jul 8, 2025 · N8671D · Boeing 7378H4 · Emergency Equipment
  > AFT LEFT OUTBOARD FLASH LIGHT INOPERATIVE. R&R FLASHLIGHT & BATTERY PER AMM 25-64-00.
- [SDR SWAA2025071090042](https://openairdocs.org/sdr/SWAA2025071090042.md): Battery · inoperative · Jul 8, 2025 · N8671D · Boeing 7378H4 · Emergency Equipment
  > AFT LEFT OUTBOARD FLASH LIGHT INOPERATIVE. R & R FLASHLIGHT & BATTERY IAW AMM 25-64-00.
- [SDR SWAA2024122680637](https://openairdocs.org/sdr/SWAA2024122680637.md): Seat Track · loose · Dec 24, 2024 · N8671D · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER SEAT ROWS LOOSE IN TRACK AT 15ABC; 16DEF; 22DEF AND 23 ABC.<[01] SECURED LOOSE SEAT TRACKS AT SEAT ROWS 15ABC;16DEF;22DEF AND 23ABC PER AMM 25-22-00
- [SDR SWAA2024121777693](https://openairdocs.org/sdr/SWAA2024121777693.md): Door · out of adjust · Dec 15, 2024 · N8671D · Boeing 7378H4 · Galley Doors
  > FWD SERVICE DOOR DIFFICULT TO CLOSE<[01] ADJUSTED FORWARD SERVICE DOOR. REFERENCE M/M 52-41-21. OPS CHECKS OK
- [SDR SWAA2024110649672](https://openairdocs.org/sdr/SWAA2024110649672.md): Wedge · delaminated · Oct 17, 2024 · N8671D · Boeing 7378H4 · Leading Edge Devices
  > LEFT WING #1 SLAT TRAILING EDGE WEDGE LOWER SURFACE IS DELAMINATED ON OUTBOARD END.<[01] REMOVED #1 SLAT IN REF TO AMM 27-81-21;[02] REMOVED #1 SLAT BOTH MAIN TRACKS IN REF 27-81-21;[03] INSTALLED #1 SLAT AND INBD AND OUTBD MAIN TRACKS PER AMM 27-81-21;[04] VE
- [SDR SWAA2024110649673](https://openairdocs.org/sdr/SWAA2024110649673.md): Wedge · delaminated · Oct 17, 2024 · N8671D · Boeing 7378H4 · Leading Edge Devices
  > RIGHT WING #8 SLAT TRAILING EDGE WEDGE LOWER SURFACE IS DELAMINATED ON OUTBOARD END.<[01] REMOVED #8 SLAT WITH THE TRACK PER AMM 27-81-21;[02] OK TO INSTALL THE #8 SLAT;[03] INSTALLED SERVICEABLE #8 SLAT REF AMM 27-81-21;[04] VERIFIED CORRECTIVE ACTION #3; AND
- [SDR SWAA2024110649940](https://openairdocs.org/sdr/SWAA2024110649940.md): Floor Support · cracked · Oct 17, 2024 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CABIN FLOOR INTERCOSTAL CRACKED AT STA 540 LBL 1.<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02;[02] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02;[03] JAMES LYNCH (TECHNICIAN); 17-OCT-2024 22:33 UTC<BR>REMOVED AND REPLACED INTERCOSTAL PER SRM 51-
- [SDR SWAA2024110649941](https://openairdocs.org/sdr/SWAA2024110649941.md): Floor Support · cracked · Oct 17, 2024 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CABIN FLOOR INTERCOSTAL CRACKED AT STA 540 RBL 1. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02
- [SDR SWAA2024110648128](https://openairdocs.org/sdr/SWAA2024110648128.md): Skin · delaminated · Oct 13, 2024 · N8671D · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING OUTBOARD AFT FLAP; THE INBOARD UPPER SURFACE HAS AN AREA OF DELAMINATION. (MARKED)<[01] REMOVED L/H OUTBD AFT FLAP PER AMM 27-51-22;[02] INSTALLED SERVICEABLE REPLACEMENT L/H OUTBD AFT FLAP IAW AMM 27-51-22-400-801.;[03] INSPECTED WORK PERFORMED ON C
- [SDR SWAA2024110747347](https://openairdocs.org/sdr/SWAA2024110747347.md): Skin · delaminated · Oct 10, 2024 · N8671D · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE IS DELAMINATED ON TRAILING EDGE.<[01] REMOVED LEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE PER SRM 51-40-02.;[02] PART REMOVAL ONLY;[03] DRILL NEW LEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE (TOP SIDE ONLY
- [SDR SWAA2024110746936](https://openairdocs.org/sdr/SWAA2024110746936.md): Angle · cracked · Oct 9, 2024 · N8671D · Boeing 7378H4 · Trailing Edge Flaps
  > LT WING L-ANGLE CRACKED AT DEFLECTION RIB O/B #3 FLAP TRACK AT FWD WEB SUPPORT<[01] REMOVED ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02.;[02] REMOVED AND REPLACED DEFLECTION RIB CLIP I.A.W SRM 51-40-02.;[03] DUSTIN WYATT (TECHNICIAN); 17-OCT-2024 20:21 UTC<BR>REMOV
- [SDR SWAA2024110646344](https://openairdocs.org/sdr/SWAA2024110646344.md): Vapor Barrier · cracked · Oct 8, 2024 · N8671D · Boeing 7378H4 · Fuselage Main, Bulkhead
  > L/H A/C BAY AFT WALL UPPER ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE AT APPROX. STA.663; LBL-9'.<[01] REMOVED FASTENERS FOR VAPOR BARRIER ANGLE REPAIR IAW SRM 57-10-10-2R-5.;[02] CUT OUT VAPOR BARRIER ANGLE FOR REPAIR;[03] ACCOMPLISHED HFEC HOLE PROBE AN
- [SDR SWAA2024110646343](https://openairdocs.org/sdr/SWAA2024110646343.md): Vapor Barrier · cracked · Oct 8, 2024 · N8671D · Boeing 7378H4 · Fuselage Main, Bulkhead
  > R/H A/C BAY AFT WALL UPPER ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE AT APPROX. STA.663; RBL-9'.<[01] SIGNED STEPS 1;2;3 AND 5;[02] INSPECTED WORK ACCOMPLISHED IN C/A #1. TRANSFERED STEPS 1; 2; 3 AND 5 TO SEPERATE FAULTS AS REQURIED PER MPM 52.02.01.;[03
- [SDR SWAA2024100343541](https://openairdocs.org/sdr/SWAA2024100343541.md): Light · inoperative · Sep 30, 2024 · N8671D · Boeing 7378H4 · Emergency Lighting
  > FWD R/H EMERGENCY LIGHT INOP AND AFT R/H SIDE EMERGENCY LIGHT INOP<[01] RELAMPED RH FWD & AFT RH EMERGENCY LIGHTS IAW AMM 33-51-04 OP CHECK GOOD.
- [SDR SWAA2024091034840](https://openairdocs.org/sdr/SWAA2024091034840.md): Battery Pack · inoperative · Sep 6, 2024 · N8671D · Boeing 7378H4 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INOP (LH 4;5;6 AREA LIGHT; LH WING TO BODY)<[01] R&R EMERGENCY LIGHT CHARGER AND BATTERY PACK AT M1670 OPS OK IAW AMM 33-51-06.
- [SDR SWAA2024050983962](https://openairdocs.org/sdr/SWAA2024050983962.md): Fairing · cracked · May 9, 2024 · N8671D · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > #2 ENGINE STRUT AFT FAIRING STRUCTURE CRACK. STARTED REMOVAL OF #2 ENGINE AFT FAIRING WEDGE PER SRM 51-40-02. R & R RT STRUT AFT FAIRING IB PANEL IAW SRM 51-40-02.
- [SDR SWAA2024050983474](https://openairdocs.org/sdr/SWAA2024050983474.md): Web · cracked · May 8, 2024 · N8671D · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > #2 ENGINE AFT PYLON TE WEDGE FWD WEB CRACKED. CRACK TERMINATES AT EDGE OF MATERIAL AND UNDER OVERLAP; APPR 2.5 IN LENGTH<[01] 04 - REPAIRED PER EA-GENERAL 24-154-01241 (EA ATTACHED TO AN AIRCRAFT FAULT)]
- [SDR SWAA2024050983479](https://openairdocs.org/sdr/SWAA2024050983479.md): Seal · cracked · May 8, 2024 · N8671D · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED.<[01] R/R LEFT HORIZ STAB FORWARD UPPER SPAR SLIDING SEAL REF AMM 53-31-31.
- [SDR SWAA2024050380836](https://openairdocs.org/sdr/SWAA2024050380836.md): Sensing Element · shorted · Apr 29, 2024 · N8671D · Boeing 7378H4 · Fire Detection
  > WHEEL WELL FIRE LIGHT ON DECENT. INDICATION EXTINGUISHED ON GEAR EXTENTION. NO ABNORMAL SMELLS NOTED.<[01] OK TO CONTINUE PER MEL 26-4-01 SP#1 & SP#3;[02] PERFORMED BITE CHECK AND FOUND FAULT CODE 84 ?WHEEL WELL FIRE ALARM? FLAGGED. PERFORMED RESISTANCE CHECK
- [SDR SWAA2024041774682](https://openairdocs.org/sdr/SWAA2024041774682.md): Battery · inoperative · Apr 14, 2024 · N8671D · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY FLASHLIGHT WILL NOT TURN OFF<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]<BR>RR?D AFT GALLEY FLASHLIGHT BATTERY IAW AMM 25-64-00
- [SDR SWAA2024010336791](https://openairdocs.org/sdr/SWAA2024010336791.md): Battery Pack · inoperative · Jan 1, 2024 · N8671D · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS MID CABIN LEFT SIDE INOP<[01] REMOVED AND REPLACED M1670 EMERGENCY LIGHT POWER SUPPLY BATTERY PACK PER AMM 33-51-06; SYSTEM OPT CHECKS GOOD
- [SDR SWAA2023091499623](https://openairdocs.org/sdr/SWAA2023091499623.md): Gauge · out of position · Sep 13, 2023 · N8671D · Boeing 7378H4 · Escape Slide
  > PLASTIC COVER OVER AFT SLIDE PRESSURE GAGE OUT OF POSITION. INSTALLED NEW R2 SLIDE GAUGE WINDOW IAW SIP. NO DEFECTS NOTED. PLACARDS REMOVED AND MX PROCEDURES C/W.
- [SDR SWAA2023082390447](https://openairdocs.org/sdr/SWAA2023082390447.md): Battery Pack · damaged · Aug 18, 2023 · N8671D · Boeing 7378H4 · Emergency Lighting
  > AFT GALLEY R/H EMERGENCY BATTERY PACK CHARGER PUSH TO TEST BUTTON IS DAMAGED<[01] REMOVED AND REPLACED AFT GALLEY EMERGENCY LIGHT BATTERY CHARGER AND PERFORMED INSTALLATION TEST PER AMM 33-51-06;[02] VERIFIED
- [SDR SWAA2023082288726](https://openairdocs.org/sdr/SWAA2023082288726.md): Light · broken · Aug 12, 2023 · N8671D · Boeing 7378H4 · Emergency Lighting
  > AFT CEILING EXIT LIGHT IS BROKEN.<[01] R&R AFT CEILING EXIT LIGHT BALLAST PER AMM 33-51-01.;[02] AFT CEILING EXIT LIGHT NEEDS OPS CHECK.;[03] INSPECTION C/W C/A#1 ABOVE. R&R AFT CEILING EXIT LIGHT BALLAST PER AMM 33-51-01.;[04] R&R AFT CEILING EXIT LIGHT BALLA
- [SDR SWAA2023082288843](https://openairdocs.org/sdr/SWAA2023082288843.md): Sign · broken · Aug 12, 2023 · N8671D · Boeing 7378H4 · Emergency Lighting
  > AFT ENTRY DOOR EXIT SIGN BALLAST IS BROKEN.<[01] R&R AFT ENTRY DOOR EXIT SIGN BALLAST.;[02] AFT ENTRY DOOR EXIT SIGN NEEDS OPS CHECK.;[03] INSPECTION C/W C/A#1 ABOVE.;[04] R&R AFT ENTRY DOOR EXIT SIGN BALLAST; OP CK GOOD PER AMM 33-51-00.;[05] INSPECTED WORK P
- [SDR SWAA2023082387651](https://openairdocs.org/sdr/SWAA2023082387651.md): Strap · corroded · Aug 10, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR BOARD STRAP DAMAGED AT 727-I<[01] REMOVED STRAP AND REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.052'). STRAP IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AND REPLACED FLOORBOARD STRAP PER SRM 51-40-02;[03] R
- [SDR SWAA2023083095000](https://openairdocs.org/sdr/SWAA2023083095000.md): Floor Panel · corroded · Aug 5, 2023 · N8671D · Boeing 7378H4 · Cargo Compartments
  > PNL 120CF HAS CORROSION ALONG THE SIDES.<[01] REMOVED AND REPLACED WITH NEW PANEL PER AMM 25-52-10;[02] C/W INSPECTION
- [SDR SWAA2023082286270](https://openairdocs.org/sdr/SWAA2023082286270.md): Floor Panel · corroded · Aug 5, 2023 · N8671D · Boeing 7378H4 · Fuselage Floor Panel
  > PNL 120DF HAS CORROSION ALONG THE SIDES.<[01] REPLACED AND INSTALLED NEW FLOOR PANEL PER AMM 25-52-10 SEE TASK TTG8Q00MN032 FOR FLOOR PANEL SEALANT;[02] VERIFIED C/A #1.
- [SDR SWAA2023082487016](https://openairdocs.org/sdr/SWAA2023082487016.md): Web · cracked · Aug 3, 2023 · N8671D · Boeing 7378H4 · Engine (Turbine/Turboprop)
  > #1 ENGINE; I/B FAN COWL; WEB CRACKED BELOW OIL SERVICE DOOR<[01] REMOVED AND REPLACED WEB IAW SRM 51-40-02
- [SDR SWAA2023082383853](https://openairdocs.org/sdr/SWAA2023082383853.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727D-727E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE.002 INCHES IN DEPTH. DAMAGE FOUND TO BE OUT OF LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT # TTG8Q00
- [SDR SWAA2023082383850](https://openairdocs.org/sdr/SWAA2023082383850.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727J-747<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE.022 INCHES IN DEPTH. DAMAGE FOUND TO BE OUT OF LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE FROM STA 727 TO S
- [SDR SWAA2023082383872](https://openairdocs.org/sdr/SWAA2023082383872.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727I-727J<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE.008 INCHES IN DEPTH. DAMAGE FOUND TO BE OUT OF LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT # TTG8Q00
- [SDR SWAA2023082383851](https://openairdocs.org/sdr/SWAA2023082383851.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727G-727H<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE.002 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT
- [SDR SWAA2023082383873](https://openairdocs.org/sdr/SWAA2023082383873.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727F-727G<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE.003 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT
- [SDR SWAA2023082383852](https://openairdocs.org/sdr/SWAA2023082383852.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727E-727F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE.001 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT
- [SDR SWAA2023082383854](https://openairdocs.org/sdr/SWAA2023082383854.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE CORROSION STA 787-807<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE.003 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON TTG8Q00
- [SDR SWAA2023082383875](https://openairdocs.org/sdr/SWAA2023082383875.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE CORROSION STA 747-767<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE.006 INCHES IN DEPTH. DAMAGE FOUND TO BE OUT OF LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] REMOVED LH TRANSITION ANGLE FROM STA 847 TO ST
- [SDR SWAA2023082383855](https://openairdocs.org/sdr/SWAA2023082383855.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE CORROSION STA 767-787<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE.001 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON TTG8Q00
- [SDR SWAA2023082383856](https://openairdocs.org/sdr/SWAA2023082383856.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727I-727J<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE.008 INCHES IN DEPTH. DAMAGE FOUND TO BE OUT OF LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] REMOVED LH TRANSITION ANGLE FROM STA 847 TO
- [SDR SWAA2023082383876](https://openairdocs.org/sdr/SWAA2023082383876.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727H-727I<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE.002 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT
- [SDR SWAA2023082383877](https://openairdocs.org/sdr/SWAA2023082383877.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727G-727H<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE.003 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT
- [SDR SWAA2023082383878](https://openairdocs.org/sdr/SWAA2023082383878.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727F-727G<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE.003 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT
- [SDR SWAA2023082383879](https://openairdocs.org/sdr/SWAA2023082383879.md): Angle · corroded · Jul 30, 2023 · N8671D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727E-727F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE.001 INCHES IN DEPTH. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2. DAMAGED SECTION TO BE REPLACED ON FAULT

Next page: https://openairdocs.org/aircraft/N8671D/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 = 'N8671D' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8671D/reports

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