# Service difficulty reports: N371US, cancelled Mar 28, 2006

A list on [N371US, cancelled Mar 28, 2006](https://openairdocs.org/deregistered/N371US-2006-03-28.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 · 86 reports

- [SDR SB05065](https://openairdocs.org/sdr/SB05065.md): Power Supply · inoperative · May 28, 2005 · N371US · Boeing 7373B7 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION M1135 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD.
- [SDR USAASB04040](https://openairdocs.org/sdr/USAASB04040.md): Battery Pack · inoperative · Mar 30, 2004 · N371US · Boeing 7373B7 · Emergency Lighting
  > PIT - MAINTENANCE REPORTED THE MID CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLCED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB03214](https://openairdocs.org/sdr/USAASB03214.md): Power Supply · inoperative · Dec 13, 2003 · N371US · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE LT OVERWING HATCH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M)
- [SDR USAASB03207](https://openairdocs.org/sdr/USAASB03207.md): Charger · inoperative · Nov 24, 2003 · N371US · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE LT OVERWING EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M)
- [SDR USAA030026](https://openairdocs.org/sdr/USAA030026.md): Skin · cracked · Mar 9, 2003 · N371US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 2 INCH, BS 727E AND S24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USA2002F00072](https://openairdocs.org/sdr/USA2002F00072.md): Module · faulty · Jul 30, 2002 · N371US · Boeing 7373B7 · Fire Detection
  > ON DESCENT, THE FIRE WARNING ANNUNCIATOR ON THE GLARESHIELD ILLUMINATED. CREW COULD NOT CANCEL THE LIGHT. NO OTHER INDICATIONS OF FIRE WAS NOTED. FIRE DETECTION TESTS NORMAL OTHERWISE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLAC
- [SDR USAA020211](https://openairdocs.org/sdr/USAA020211.md): Frame · corroded · Jun 1, 2002 · N371US · Boeing 7373B7 · Fuselage Main, Frame
  > TPA - FOUND FRAME CORRODED 3 INCH BY 1.5 INCH AREA, STATION 251.6 RIGHT SIDE NOSE W/W AREA. CORROSION LEVEL 2, TASK NR C53-100-01. FABRICATED NEW PARTS PER SRM, REPLACED OLD CHORD ANGLE PER SRM 53-00-7 FIG 204. (M)
- [SDR USAASB02044](https://openairdocs.org/sdr/USAASB02044.md): Light · inoperative · Mar 7, 2002 · N371US · Boeing 7373B7 · Emergency Lighting
  > PHL - MAINTENANCE REPORTED THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT ROW 5 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 5 ABC. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB01333](https://openairdocs.org/sdr/USAASB01333.md): Battery Pack · discharged · Dec 2, 2001 · N371US · Boeing 7373B7 · Emergency Lighting
  > PIT - MAINTENANCE FOUND THE MID CABIN, CENTER OVERHEAD EMERGENCY EXIT LIGHT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAA010894](https://openairdocs.org/sdr/USAA010894.md): Skin Panel · buckled · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND SKIN PANEL BUCKLED APPROXIMATELY 3 SQUARE INCHES, KEEL BEAM STATION 663 TO 685. REMOVED AND REPLACED KEEL BEAM LOWER PANEL PER SRM 51-10-02. (M)
- [SDR USAA010895](https://openairdocs.org/sdr/USAA010895.md): Fitting · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FITTING CORRODED 3 INCHES BY 2 INCH AREA, BS 727, STRINGER 27R, AFT CARGO COMPARTMENT. CORROSION LEVEL 2 TASK NR C53-202-01. FABRICATED AND INSTALLED FITTING PER BAC DRAWING NR 65-73746 AND SRM 51-10-02. (M)
- [SDR USAA010905](https://openairdocs.org/sdr/USAA010905.md): Attach Fitting · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Horizontal Stabilizer, Attach Fittings
  > CLT - FOUND UPPER ATTACH LUGS APPROX.5 INCH TOTAL AREA, CORRODED, LEFT HORIZONTAL STABILIZER CENTER SECTION, FRONT SPAR. REAMED CLEVIS TO REMOVE CORROSION, MACHINED AND INSTALLED NEW BUSHING PER SRM 55-10-10. (M)
- [SDR USAA010904](https://openairdocs.org/sdr/USAA010904.md): Attach Fitting · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Horizontal Stabilizer, Attach Fittings
  > CLT - FOUND LUG ATTACH FITTING CORRODED APPROX 5 INCH AREA, LEFT HORIZONTAL STABILIZER CENTER SECTION, REAR SPAR FORWARD LUG, FORWARD FACE. LUG SPOT FACED TO DEPTH OF.070 INCH PER SRM 55-10-10 GRAPH II. (M)
- [SDR USAA010903](https://openairdocs.org/sdr/USAA010903.md): Attach Fitting · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Horizontal Stabilizer, Attach Fittings
  > CLT - FOUND ATTACH LUG FITTING CORRODED.75 INCH TOTAL SURFACE AREA, LEFT HORIZONTAL STABILIZER CENTER SECTION, FRONT LOWER FORWARD LUG. CORROSION REMOVED, FABRICATED AND INSTALLED NEW BUSHING PER SRM 55-10-10. (M)
- [SDR USAA010902](https://openairdocs.org/sdr/USAA010902.md): Shear Tie · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - FOUND FRAME SHEAR TIE CORRODED.5 INCH BY.5 INCH, BS 947.5, BETWEEN S27L AND S26L. CORROSION LEVEL 1, TASK NR C53-208-01. REMOVED AND REPLACED SHEAR TIE PER SRM 51-01-2. (M)
- [SDR USAA010901](https://openairdocs.org/sdr/USAA010901.md): Shear Tie · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - FOUND FRAME SHEAR TIE CORRODED 14 INCH AREA, BS 727A, LBL 7 AND RBL 7. CORROSION LEVEL 1 TASK NR C53-202-01. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-2. (M)
- [SDR USAA010900](https://openairdocs.org/sdr/USAA010900.md): Keelbeam · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Keel
  > CLT - FOUND KEEL BEAM CHORD CORRODED 6 INCHES BY 2 INCHES, BS 500C PLUS 9 TO 500D, RBL 7. DAMAGE REMOVED, INSTALLED REPAIR ANGLES PER SRM 53-30-12 FIG 202, EA 69842. (M)
- [SDR USAA010899](https://openairdocs.org/sdr/USAA010899.md): Keelbeam · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Keel
  > CLT - FOUND KEEL BEAM STRINGER CORRODED 3 INCHES BY 4 INCH AREA, BS 727D TO E, LEFT KEEL BEAM. CORROSION LEVEL 2, TASK NR C53-202-01. REMOVED KEEL BEAM, REMOVED CORROSION, REINSTALLED KEEL BEAM AND REPAIR DOUBLER/TRIPLER PER EA 69835. (M)
- [SDR USAA010898](https://openairdocs.org/sdr/USAA010898.md): Frame · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FRAME CORRODED 14 INCH AREA, BS 727B, LEFT AND RIGHT KEEL BEAMS, LOWER FLANGE. REMOVED DAMAGE, INSTALLED NEW FRAME SECTION PER SRM 51-40-02 AND 51-40-05. (M)
- [SDR USAA010987](https://openairdocs.org/sdr/USAA010987.md): Keelbeam · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Keel
  > CLT - FOUND LOWER CHORD OUTBOARD FLANGE CORRODED 1 INCHES BY 22 INCH, BS 673-695 RIGHT, BS 693-727 KEEL BEAMS. CORROSION LEVEL 2 TASK C53-100-01. REMOVED DAMAGE, INSTALLED REPAIR STRAPS LEFT AND RIGHT SIDE PER EA 69794. (M)
- [SDR USAA010896](https://openairdocs.org/sdr/USAA010896.md): Keelbeam · corroded · Jul 20, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Keel
  > CLT - FOUND KEEL BEAM CORRODED 5 SQUARE INCHES, BS 767, RIGHT KEEL BEAM SPLICE. CORROSION LEVEL 2 TASK NR C53-202-01. REMOVED KEEL BEAM, REMOVED CORROSION, REINSTALLED KEEL BEAM AND REPAIR DOUBLER/TRIPLER PER EA 69835. (M)
- [SDR USAA010893](https://openairdocs.org/sdr/USAA010893.md): Frame · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - FOUND Z-CHORD CORRODED 4 INCHES BY 1 INCH AREA, BS 270, RBL 6. DAMAGED REMOVED, INSTALLED Z-CHORD REPAIR KIT PER TR 53-20-08. (M)
- [SDR USAA010892](https://openairdocs.org/sdr/USAA010892.md): Frame · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - FOUND FRAME CHORD CORRODED 1 INCHES BY 3 INCHES, BS 500D, RBL 7, FORWARD CARGO FLOOR. CORRODED LEVEL 1 TASK NR C53-208-01. DAMAGE REMOVED, INSTALLED REPAIR ANGLES EPR EA 69842. (M)
- [SDR USAA010891](https://openairdocs.org/sdr/USAA010891.md): Channel · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Cargo/Baggage Doors
  > CLT - FOUND CHANNEL CORRODED 5 SQUARE INCH AREA CORRODED, AFT CARGO DOOR, LOWER WILL STRUCTURE. REMOVED AND REPLACED CHANNEL PER SRM 51-10-01 AND 51-10-02. (M)
- [SDR USAA010890](https://openairdocs.org/sdr/USAA010890.md): Angle · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND Z-ANGLE CORRODED 4 INCHES BY 40 INCHES AFT ENTRY DOOR SILL. CORROSION LEVEL 1, TASK C53-202-01. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. (M)
- [SDR USAA010889](https://openairdocs.org/sdr/USAA010889.md): Frame · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - FOUND FRAME CORRODED 10 INCHES BY 1 INCH AREA, BS 807 LBL 5 TO RBL 5, AFT CARGO. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 53-00-07 AND 51-40-02. (M)
- [SDR USAA010888](https://openairdocs.org/sdr/USAA010888.md): Shear Tie · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - FOUND SHEAR TIE CORRODED 1 INCH BY 5 INCH AREA, BS 807, BETWEEN RBL 15 TO 20, AT BELLY SKIN LEVEL. FABRICATED AND REPLACED SHEAR TIE PER SRM 51-10-01 AND BAC DRAWING NR 69-43277. (M)
- [SDR USAA010887](https://openairdocs.org/sdr/USAA010887.md): Stringer · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND STRINGER CORRODED 14 INCHES BY 2.5 INCHES, BS 907 TO 927, S25L, BELOW AFT CARGO FLOOR. REMOVED AND REPLACED STRINGER PER SRM 51-40-02. (M)
- [SDR USAA010886](https://openairdocs.org/sdr/USAA010886.md): Stringer · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - FOUND STRINGER CORRODED 6 INCHES BY 1 INCH AREA, BS 1006 TO 1016, STRINGER 26R. REMOVED DAMAGE, SPLICED IN NEW STRINGER SECTION PER SRM 51-40-04 AND BAC DRAWING NR 65-45776. (M)
- [SDR USAA010885](https://openairdocs.org/sdr/USAA010885.md): Floorbeam · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 4 INCHES BY 2 INCH AREA, BS 1006, LBL 8 TO LBL 12. REPLACED UPPER T-CAP PER EA 69770 AND TR 53-10-05A. (M)
- [SDR USAA010883](https://openairdocs.org/sdr/USAA010883.md): Frame · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - FOUND FRAME CORRODED 6 SQUARE INCH AREA, BS 1006, STRINGER 23R TO FLOOR LEVEL. CORROSION LEVEL 1 TASK NR C53-107-02. REMOVED DAMAGE, INSTALLED REPLACEMENT FRAME SECTION PER SRM 51-10-02, 51-40-02, 51-40-03. (M)
- [SDR USAA010881](https://openairdocs.org/sdr/USAA010881.md): Floorbeam · corroded · Jul 19, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH AREA, BS 1016 LBL 6 TO LBL 34. CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR 53-10-05A. (M)
- [SDR USAA010874](https://openairdocs.org/sdr/USAA010874.md): Frame · dented · Jul 18, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - FOUND FRAME UPPER FLANGE DENTED, 1 INCH LONG, BS 747 RBL 24 AFT CARGO FLOOR. DAMAGE REMOVED, INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-07. (M)
- [SDR USAA010875](https://openairdocs.org/sdr/USAA010875.md): Bulkhead · gouged · Jul 18, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD WEB GOUGED.016 INCH DEEP BY.150 INCH LONG, BS 178 WL 176 LBL 5.5. TRIMMED OUT DAMAGE, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND EA 69798. (M)
- [SDR USAA010878](https://openairdocs.org/sdr/USAA010878.md): Floorbeam · corroded · Jul 18, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 18 INCH AREA, BS 986.5, BL 0 TO RBL 18. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR 53-10-05A. (M)
- [SDR USAA010877](https://openairdocs.org/sdr/USAA010877.md): Floorbeam · corroded · Jul 18, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED, ENTIRE LENGTH OF FLOORBEAM, BS 294.5 STRINGER 17L TO 17R. CORROSION LEVEL 1, TASK NR C53-107-02. DAMAGE REMOVED, INSTALLED DOUBLER PER SRM 53-10-51. (M)
- [SDR USAA010876](https://openairdocs.org/sdr/USAA010876.md): Angle · corroded · Jul 18, 2001 · N371US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND CREASEBEAM ANGLE CORRODED 40 INCHES, BS 947.5 AFT SERVICE DOOR FRAME. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED Z-ANGLE AND WEB PER SRM 51-10-2, 51-40-2, AND 53-60-15. (M)
- [SDR USAA010809](https://openairdocs.org/sdr/USAA010809.md): Frame · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORD CRACKED TWO PLACES, 1.75 INCHES ON LEFT SIDE, 1 INCH ON RIGHT SIDE, BS 178, WL 207, LEFT AND RIGHT SIDE. DAMAGE REMOVED, SPLICED IN NEW REPAIR SECTION PER EO 5300V157. (M)
- [SDR USAA010812](https://openairdocs.org/sdr/USAA010812.md): Pressure Panel · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > CLT - FOUND FLOORWEB CRACKED TWO PLACES.5 INCH, BS 178 WL 207, LEFT AND RIGHT SIDE. REMOVED AND REPLACED FLOORWEB PER EO 5300V157 AND SRM 51-10-2. (M)
- [SDR USAA010814](https://openairdocs.org/sdr/USAA010814.md): Frame · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FRAME CRACKED.25 INCH, BS 807, BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA010824](https://openairdocs.org/sdr/USAA010824.md): Tie Clip · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND TIE CLIP CRACKED TWO PLACES.25 INCH, BS 663, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA010826](https://openairdocs.org/sdr/USAA010826.md): Frame · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FRAME CRACKED.25 INCH, BS 887 BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA010828](https://openairdocs.org/sdr/USAA010828.md): Frame · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FRAME CRACKED APPROXIMATELY.25 INCH, BS 847, BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA010829](https://openairdocs.org/sdr/USAA010829.md): Frame · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FRAME CRACKED APPROX.25 INCH, BS 847, BETWEEN STRINGER 8 AND 9R. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)
- [SDR USAA010830](https://openairdocs.org/sdr/USAA010830.md): Skin · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FUSELAGE SKIN CRACKED.25 INCH, BS 727C, STRINER 24L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 225. (M)
- [SDR USAA010831](https://openairdocs.org/sdr/USAA010831.md): Frame · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FRAME CRACKED 1 INCH, BS 616, RIGHT CREASE BEAM, INNER CHORD ANGLE. DAMAGE REMOVED, INSTALLED REPAIR ANGLE AND FILLER PER TYPICAL REPAIR 53-62-01. (M)
- [SDR USAA010832](https://openairdocs.org/sdr/USAA010832.md): Door Frame · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND DOOR FRAME CRACKED TWO PLACES 1 INCH EACH, BS 294.5, RBL 55, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA010833](https://openairdocs.org/sdr/USAA010833.md): Angle · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND SUPPORT ANGLE CRACKED 5 INCHES, BS 290 TO 294.5, RBL 55, INBOARD CREASE BEAM ANGLE. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-01-02. (M)
- [SDR USAA010834](https://openairdocs.org/sdr/USAA010834.md): Frame · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Structure (General)
  > CLT - FOUND FRAME CRACKED 3 INCHES, BS 954, BETWEEN STRINGER 9 AND 10R, INNER RADIUS. DAMAGE REMOVED, INSTALLED NEW PARTS PER SRM 51-40-03, 51-40-02 AND BAC DRAWING NR J65-46561. (M)
- [SDR USAA010835](https://openairdocs.org/sdr/USAA010835.md): Skin · cracked · Jul 16, 2001 · N371US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND FUSELAGE SKIN CRACKED.8 INCH, BETWEEN BS 727D AND E, BL 0. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 51-20-01, 51-40-00 AND 53-00-01 FIG 202. (M)

Next page: https://openairdocs.org/deregistered/N371US-2006-03-28/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 = 'N371US' AND deregistration_id = 'N371US-2006-03-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N371US-2006-03-28/reports

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