# Service difficulty reports: N376US, cancelled Jan 18, 2006

A list on [N376US, cancelled Jan 18, 2006](https://openairdocs.org/deregistered/N376US-2006-01-18.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 · 71 reports

- [SDR USAA050003](https://openairdocs.org/sdr/USAA050003.md): Skin · cracked · Jan 7, 2005 · N376US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.750 INCH, STATION 74-2 AT STRINGER 19R. INSTALLED DOUBLER IAW 53-00-01. (M)
- [SDR SB04162](https://openairdocs.org/sdr/SB04162.md): Battery Pack · discharged · Dec 5, 2004 · N376US · Boeing 7373B7 · Emergency Lighting
  > ORD - MAINTENANCE REPORTED A FEW OF THE AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR USAASB04117](https://openairdocs.org/sdr/USAASB04117.md): Indicator · malfunctioned · Sep 2, 2004 · N376US · Boeing 7373B7 · Trailing Flap Position Indicating System
  > BOS - FLT 2022 - ON APPROACH TO BOS, FROM DCA, THE RIGHT FLAP LAGGED BEHIND THE LEFT FLAP TO THE POINT WHERE SELECTING FLAPS TO 25 UNITS, FLAPS ASSYMETRY PROTECTION TOOK PLACE. CREW ACCOMPLISHED A GO AROUND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RE
- [SDR USAASB04111](https://openairdocs.org/sdr/USAASB04111.md): Fuse · blown · Aug 16, 2004 · N376US · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE EMERGENCY LIGHT ABOVE THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED THE FUSES AT THE M1132 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA040424](https://openairdocs.org/sdr/USAA040424.md): Flange · cracked · Aug 11, 2004 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND ATTACH FLANGE CRACKED, 4 INCHES, LEFT RAM AIR INLET DUCT HANGAR ATTACHED TO LOWER SURFACE CETNER TANK. DURING REPLACEMENT, HOLE FOUND DAMAGED, OVERSIZED, FREEZE PLUG INSTALLED PER EA 78847. (M)
- [SDR USAA040425](https://openairdocs.org/sdr/USAA040425.md): Mount · damaged · Aug 11, 2004 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND MOUNT HOLE BORE, DAMAGE TO BORE OF MOUNT HOLE, AFT OUTBOARD MOUNT HOLE FOR RAM AIR DUCT LEFT SIDE. OVERSIZED HOLE, INSTALLED FREEZE PLUG PER EA 78847. (M)
- [SDR USAA040416](https://openairdocs.org/sdr/USAA040416.md): Spar · cracked · Aug 11, 2004 · N376US · Boeing 7373B7 · Wing Spar
  > PIT - FOUND REAR SPAR UPPER CHORD CRACKED.1888 INCH, RIGHT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED DOUBLER PER EA 78782. (M)
- [SDR USAA040415](https://openairdocs.org/sdr/USAA040415.md): Spar · cracked · Aug 11, 2004 · N376US · Boeing 7373B7 · Wing Spar
  > PIT - FOUND REAR SPAR UPPER CHORD CRACKED.1888 INCH, AFT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED FREEZE PLUG PER EA 78781. (M)
- [SDR USAA040421](https://openairdocs.org/sdr/USAA040421.md): Bulkhead · cracked · Aug 9, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND BULKHEAD SKIN CRACKED.5 INCH, BL 0, WL 186, STATION 178 BULKHEAD. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-10-08, FIG 203. (M)
- [SDR USAA040419](https://openairdocs.org/sdr/USAA040419.md): Fitting · corroded · Aug 9, 2004 · N376US · Boeing 7373B7 · Fuselage, Landing Gear Attach Fittings
  > PIT - FOUND BEAM FITTING PITTED AND ELONGED, LEFT L/G SUPPORT BEAM STABILIZER BEAM LUG FITTING, ATTACH BOLT HOLES. REAMED HOLES AND INSTALLED FREEZE PLUGS AND REDRILLED HOLES TO ORIGINAL SIZE PER SRM 51-20-10 AND EA 78853. (M)
- [SDR USAA040420](https://openairdocs.org/sdr/USAA040420.md): Bulkhead · cracked · Aug 9, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND BULKHEAD SKIN CRACKED.75 INCH, STATION 178 BULKHEAD LBL 5.7 ABOVE WL 184, INBOARD SIDE. REMOVED CRACK AND INSTALLED DOUBLER PER EO 5300V155. (M)
- [SDR USAA040423](https://openairdocs.org/sdr/USAA040423.md): Support Angle · cracked · Aug 4, 2004 · N376US · Boeing 7373B7 · Wing Miscellaneous Structure
  > PIT - FOUND SUPPORT ANGLE CRACKED 1.125 INCH LONG, LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE AT REAR SPAR STAITON 243. REPLACED SUPPORT ANGLE PER BOEING DWG 69-39228, SRM 51-10-00. (M)
- [SDR USAA040370](https://openairdocs.org/sdr/USAA040370.md): Skin · cracked · Aug 3, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED.75 INCH, UNDER DOUBLER PLATE, FS 328 ABOVE STRINGER 17R AT SILL PLATE FASTENERS. REPAIRED PLATES AND FILLERS INSTALLED PER SRM 53-10-01 FIG 202. (M)
- [SDR USAA040381](https://openairdocs.org/sdr/USAA040381.md): Fitting · corroded · Jul 29, 2004 · N376US · Boeing 7373B7 · Wing, Attach Fittings
  > PIT - FOUND FITTING CORRODED.25 INCH AREA, RIGHT WING AFT SPAR AND LG BEAM GEAR DOOR HINGE POINT OUTBOARD. REAMED AND COUTNERSINK NEW FITTING PER MM 20-50-11-2-912-002 FIG 202. (M)
- [SDR USAA040374](https://openairdocs.org/sdr/USAA040374.md): Fitting · cracked · Jul 29, 2004 · N376US · Boeing 7373B7 · Wing, Attach Fittings
  > FOUND AFT SPAR ATTACH FITTING CRACKED.25 INCH, LANDING GEAR BEAM AFT SPAR ATTACH FITTING, RIGHT WING AFT SPAR. MODIFIED PART INSTALLED PER EO 5702V054. (M)
- [SDR USAA040378](https://openairdocs.org/sdr/USAA040378.md): Fitting · galled · Jul 28, 2004 · N376US · Boeing 7373B7 · Wing, Attach Fittings
  > PIT - FOUND GALLED FITTING, MLG WALKING BEAM, RIGHT WING REAR SPAR, STATION 200. DEFECTIVE PART REPLACED WITH IDENT PART NR PER BMM 20-50-11-2-912-002 FIG 202. (M)
- [SDR USAA040371](https://openairdocs.org/sdr/USAA040371.md): Panel · cracked · Jul 28, 2004 · N376US · Boeing 7373B7 · Nacelle/Pylon, Plate/Skin
  > PIT - FOUND PYLON CRACKED.5 INCH, UPPER PYLON SKIN AT ACCESS PANEL OPENING FOR PANEL 5827R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M)
- [SDR USAA040372](https://openairdocs.org/sdr/USAA040372.md): Fitting · cracked · Jul 27, 2004 · N376US · Boeing 7373B7 · Wing, Attach Fittings
  > PIT - FOUND FITTING CRACKED.75 INCH, RIGHT WING REAR SPAR STATION 224. INSTALLED NEW SUPPORT FITTING PER EA 78781. (M)
- [SDR USAA040382](https://openairdocs.org/sdr/USAA040382.md): Attach Fitting · corroded · Jul 25, 2004 · N376US · Boeing 7373B7 · Wing, Landing Gear Attach Fittings
  > PIT - FOUND ACTUATOR ATTACH FITTING.25 INCH AREA, RIGHT MLG BEAM NR 6 SPOILER ACTUATOR ATTACH FITTING. INSTALLED NEW FITTING PER BMM 20-50-11-2-912-002 FIG 202. (M)
- [SDR USAA040422](https://openairdocs.org/sdr/USAA040422.md): Support Beam · corroded · Jul 23, 2004 · N376US · Boeing 7373B7 · Fuselage, Landing Gear Attach Fittings
  > PIT - FOUND SUPPORT BEAM CORRODED.5 INCH BY.25 INCH, AND.375 INCH BY.25 INCH BY.25 INCH, CORROSION PITTING WITH WEAR, LEFT MLG SUPPORT BEAM, STAB BEAM LUG FITTING HOLES (3).
- [SDR USAA040373](https://openairdocs.org/sdr/USAA040373.md): Bulkhead · cracked · Jul 23, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND BULKHEAD WEB CRACKED.5 INCH, FS 178 BULKHEAD WEB, B/L0, WL/L 186. INSTALLED DOUBLER, FILLER PER SRM 53-10-08 FIG 203. (M)
- [SDR USAA040383](https://openairdocs.org/sdr/USAA040383.md): Stiffener · gouged · Jul 22, 2004 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND VERTICAL STIFFENER GOUGED.020 INCH, LT SIDE OF KEELBEAM AT STATION 634, INBOARD. FABRICATED AND REPLACED STIFFENER PER SRM 53-60-12 FIG 1. (M)
- [SDR USAA040376](https://openairdocs.org/sdr/USAA040376.md): Stringer · cracked · Jul 21, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND STRINGER CRACKED.5 INCH, FS 1120, STRINGER 5A, LEFT SIDE. INSTALLED REPAIR ANGLE PE TYPICAL REPAIR 53-80-04. (M)
- [SDR USAA040377](https://openairdocs.org/sdr/USAA040377.md): Frame · cracked · Jul 21, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND FRAME CRACKED.5 INCH, BELTFRAME STATION 767 AT STRINGER S14L. INSTALLED DOUBLER AND FILLERS PER SRM 53-00-07 PAGES 202-203. (M)
- [SDR USAA040375](https://openairdocs.org/sdr/USAA040375.md): Bulkhead · cracked · Jul 21, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND SKIN CRACKED 1.25 INCH, THROUGH FASTENER STATION 1040 BL-0 AFT PRESSURE BULKHEAD, 9 FASTENERS ABOVE CENTER OF BULKHEAD. MANUFACTURED FILLER AND DOUBLER PER 53-80-08 FIG 201. (M)
- [SDR USAA040379](https://openairdocs.org/sdr/USAA040379.md): Intercostal · corroded · Jul 21, 2004 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH AREA, FS 990, STATION 21, LEFT. FABRICATED NEW INTERCOSTAL PER 51-40-02. CORROSION LEVEL 1, TASK NR C53-202-01. (M)
- [SDR USAA040380](https://openairdocs.org/sdr/USAA040380.md): Floorbeam · corroded · Jul 21, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > PIT - FOUND BEAM CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BEAM, FS 993, RBL 14-44. MANUFACTURED NEW SUPPORT ANGLE PER BOEING DWG 65C19883. CORROSION LEVEL 1, TASK NR C53-107-02. (M)
- [SDR USAA040369](https://openairdocs.org/sdr/USAA040369.md): Bulkhead · cracked · Jul 19, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND BULKHEAD SKIN CRACKED.25 INCH, AT RIVET OUTBOARD OF RBL 57 AT WL 234 STATION 178 BULKHEAD. INSTALLED DOUBLER PER EO 5300V153. (M)
- [SDR USAA040368](https://openairdocs.org/sdr/USAA040368.md): Skin · delaminated · Jul 13, 2004 · N376US · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND TOP SKIN AND CORE MATERIAL DELAMINATED 3 INCH BY 4 INCH AREA, NR 3 SLAT INBOARD T/E CORNER. INSTALLED NEW CORE, INSTALLED FILLER AND UPPER DOUBLER PER BOEING SRM 51-70-10. (M)
- [SDR USAA040367](https://openairdocs.org/sdr/USAA040367.md): Skin · chafed · Jul 13, 2004 · N376US · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND LOWER SKIN SURFACE CHAFED 2 INCH BY 1 INCH, NR 4 SLAT INBOARD TRAILING EDGE. REMOVED CHAFED AREA, BONDED, SEALED EDGE AND REFINISHED PER BOEING SRM 51-70-10. (M)
- [SDR USAA040437](https://openairdocs.org/sdr/USAA040437.md): Skin · corroded · Jul 8, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CORRODED.25 INCH BY.5 INCH SPOT, AFT PRESS BULKHEAD, AFT SIDE, STATION 1016 BL 0. CLEANED LIGHT CORROSION PER SRM 51-21-31. (M)
- [SDR USAA040341](https://openairdocs.org/sdr/USAA040341.md): Web · cracked · Jul 7, 2004 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT FOUND WEB CRACKED 2 INCHES, STATION 1040, BL 0, 9 RIVETS UP FROM CENTER OF AFT PRESSURE DOME. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-80-08. (M)
- [SDR USA2004F00052](https://openairdocs.org/sdr/USA2004F00052.md): Shutoff Valve · failed · May 8, 2004 · N376US · Boeing 7373B7 · Cabin Cooling System
  > RT PACK TRIP OFF LIGHT ILLUMINATED, WOULD NOT RESET. LT PACK TRIP OFF LIGHT ILLUMINATED DURING TEMP ADJMT. IMMEDIATE DESCENT WAS INITIATED TO 10,000 FT BUT CABIN ALTITUDE CLIMBED ABOVE 14,000 FT DEPLOYING OXYGEN MASKS. LT PACK RESET, PRESS WAS REGAINED. F
- [SDR USAASB04049](https://openairdocs.org/sdr/USAASB04049.md): Wire Harness · faulty · May 3, 2004 · N376US · Boeing 7373B7 · Engine Indicating System Wiring
  > PIT - FLT 991 - EN ROUTE FROM PHL TO DFW, SOUTH OF PIT, CREW REPORTED THE NR 2 ENGINE EGT SPIKED TO 1,000 DEGREES WITH THE RED OVERHEAT LIGHT ILLUMINATING. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW REDUCED POWER ON THE NR 2 ENGINE AND THE LIGHT EXTINGUI
- [SDR USAA040187](https://openairdocs.org/sdr/USAA040187.md): Skin · cracked · Apr 29, 2004 · N376US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.35 INCHES, STATION 760 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)
- [SDR USAA030192](https://openairdocs.org/sdr/USAA030192.md): Skin · cracked · Sep 13, 2003 · N376US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED.5 INCH, AFT ENTRY DOOR LOWER HINGE CUTOUT AT STATION 947.5, S-14L. DOUBLERS INSTALLED PER EA 76982 AND SRM 53-60-01, FIG 1, FIG 207. (M)
- [SDR USAASB02093](https://openairdocs.org/sdr/USAASB02093.md): Battery Pack · discharged · May 13, 2002 · N376US · Boeing 7373B7 · Emergency Lighting
  > EWR - MAINTENANCE FOUND THE FORWARD TO MID CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB02056](https://openairdocs.org/sdr/USAASB02056.md): Battery Pack · cracked · Mar 18, 2002 · N376US · Boeing 7373B7 · Emergency Lighting
  > PHL - MAINTENANCE REPORTED AN OVERHEAD EMERGENCY LIGHT BATTERY PACK, FOR LOW LEVEL LIGHTING, WAS LEAKING FROM CEILING INTO OVERHEAD COMPARTMENT ABOVE SEAT ROW 1C. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB02055](https://openairdocs.org/sdr/USAASB02055.md): Light · failed · Mar 18, 2002 · N376US · Boeing 7373B7 · Emergency Lighting
  > IND - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 6ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET ASSEMBLY AT SEAT ROW 6 ABC. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB01251](https://openairdocs.org/sdr/USAASB01251.md): Battery Pack · discharged · Sep 11, 2001 · N376US · Boeing 7373B7 · Emergency Lighting
  > ORD - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MID LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB00325](https://openairdocs.org/sdr/USAASB00325.md): Acm · overserviced · Nov 22, 2000 · N376US · Boeing 7373B7 · Cabin Cooling System
  > PIT - FLT 9550 - AIRCRAFT WAS ON A TEST HOP AFTER A MAINTENANCE CHECK, WHEN JUST AFTER TAKEOFF, A SMALL AMOUNT OF SMOKE WAS NOTED IN THE COCKPIT. FLIGHT RETURNED TO FIELD AT PIT WITHIN MINUTES OF TAKEOFF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY
- [SDR USAA001979](https://openairdocs.org/sdr/USAA001979.md): Frame · cracked · Nov 22, 2000 · N376US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.25 INCH, FS 663.75 AT CUTOUT FOR NR 1 STRINGER. INSTALLED REPAIR PER SRM 53-00-07 FIG 207 SHT 6. (M)
- [SDR USAA001947](https://openairdocs.org/sdr/USAA001947.md): Skin · delaminated · Nov 18, 2000 · N376US · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER DELAMINATED IN 7 AREAS, LEFT AND RIGHT RUDDER SKIN DELAMINATE 1ST LAYER. 200-230 DEGREE CURE. WET LAY UP REPAIR USING 51-70-17 THEN BALANCED PER 51-60-00 AND EA 56867. (M)
- [SDR USAA002107](https://openairdocs.org/sdr/USAA002107.md): Bracket · cracked · Nov 3, 2000 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND ANGLE BRACKET CRACKED.25 INCH, STATION 440 BETWEEN STRINGER 8 AND 9 RT OVERHEAD PIN ATT PT. INSTALLED.045 INCH ANGLE COUPLER PER US AIRWAYS TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA002108](https://openairdocs.org/sdr/USAA002108.md): Fitting · corroded · Oct 25, 2000 · N376US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND FITTINGS CORRODED.75 INCH BY 1 INCH, STRINGER FITTINGS STATION 1016 STRINGER 23L, 24L, 25L. CORROSION LEVEL 1 TASK NR C53-701-01. CLEANED CORROSION, TREATED AND PRIMED. (M)
- [SDR USAA002110](https://openairdocs.org/sdr/USAA002110.md): Ring · corroded · Oct 25, 2000 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND DOME SUPPORT RING CORRODED.5 INCH BY 1.5 INCH, STATION 1016 DOME SUPPORT RING 23R-21R AND 18R-8R. CLEANED CORROSION, TREATED AND PRIMED PER 51-20-02. (M)
- [SDR USAA002109](https://openairdocs.org/sdr/USAA002109.md): Bracket · cracked · Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND ANGLE BRACKET CRACKED.25 INCH, STATION 380 BETWEEN STRINGER 8 AND 9 RT OVERHEAD BIN ATTACH PT. INSTALLED.045 INCH ANGLE DOUBLER PER US AIRWAYS TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA002111](https://openairdocs.org/sdr/USAA002111.md): Web · cracked · Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND WEB CRACKED 1.5 INCH, WL 207, RBL 28 AFT STATION 178 LIGHTENING HOLE. REMOVED, FABRICATED NEW WEB FROM.071 2024-T3 AND INSTALLED. (M)
- [SDR USAA001726](https://openairdocs.org/sdr/USAA001726.md): Skin · cracked · Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - SKIN CRACKED.25 INCH, STA 440 STR 8 AND STR 9 RT OVERHEAD ATTACH POINT. INSTALLED.045 INCH ANGLE DOUBLER PER TYPICAL REPAIR 53-10-14. (X)
- [SDR USAA001725](https://openairdocs.org/sdr/USAA001725.md): Skin · cracked · Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - SKIN CRACKED.25 INCH, STA 380 STR 8 AND STR 9 RT OVERHEAD ATTACH POINT. INSTALLED.045 INCH ANGLE DOUBLER PER TYPICAL REPAIR 53-10-14. (X)

Next page: https://openairdocs.org/deregistered/N376US-2006-01-18/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 = 'N376US' AND deregistration_id = 'N376US-2006-01-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N376US-2006-01-18/reports

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