# Service difficulty reports: N14871, cancelled Dec 7, 2004

A list on [N14871, cancelled Dec 7, 2004](https://openairdocs.org/deregistered/N14871-2004-12-07.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 · 100 reports

- [SDR CALA0400561](https://openairdocs.org/sdr/CALA0400561.md): Panel · cracked · Jul 2, 2004 · N14871 · Doug DC981 · Wing, Plate/Skin
  > INSPECTION FOUND A 6 INCH CRACK IN RIGHT WING PANEL AT WING STA XFS 70-196. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0400572](https://openairdocs.org/sdr/CALA0400572.md): Longeron · cracked · Jun 24, 2004 · N14871 · Doug DC981 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A SMALL CRACK IN LOWER EDGE OF THE VERTICAL LEG OF LONGERON 20L AT APPROXIMATELY STA 995. THE CRACK RAN FROM THE BOTTOM EDGE OF THE VERTICAL FLANGE TO THE FIRST FASTENER HOLE LOCATION WHERE IT TERMINATED. THE LONGERON WAS REPAIRED IAW ECRA 5
- [SDR CALA0400542](https://openairdocs.org/sdr/CALA0400542.md): Angle · corroded · Jun 22, 2004 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO DOOR FORWARD DOOR JAMB ANGLE CORRODED AT STA 1155, LONGERON 27R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0400540](https://openairdocs.org/sdr/CALA0400540.md): Stand Off · corroded · Jun 18, 2004 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR STANDOFF CORRODED AT STA 200 CENTER OF FLOOR. THE FLOOR STANDOFF WAS REMOVED AND REPLACED IAW SRM 51-30-5-001.
- [SDR CALA0400539](https://openairdocs.org/sdr/CALA0400539.md): Floor Support · corroded · Jun 18, 2004 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 200-230, LBL 15. THE FLOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-3.
- [SDR CALA0400538](https://openairdocs.org/sdr/CALA0400538.md): Floor Support · corroded · Jun 18, 2004 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT TRACK CORRODED AT STA 160-200, RBL 7. THE FLOOR SUPPORT TRACK WAS REPLACED IAW SRM 51-30-3.
- [SDR CALA0300111](https://openairdocs.org/sdr/CALA0300111.md): Angle · corroded · Mar 10, 2003 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PRESSURE BULKHEAD ANGLE CORRODED AT STA 1338, LONGERON 28R TO 30. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30.
- [SDR CALA0300109](https://openairdocs.org/sdr/CALA0300109.md): Skin · gouged · Mar 9, 2003 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT JACK POINT, STA 1338. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 9.
- [SDR CALA0300114](https://openairdocs.org/sdr/CALA0300114.md): Skin · delaminated · Mar 7, 2003 · N14871 · Doug DC981 · Leading Edge Devices
  > MAINTENANCE FOUND THE L/H INBOARD FLAP OUTBOARD VANE UPPER SKIN DELAMINATED. THE FINAL TRIM OUT AREA MEASURED 4.7" X 5.6". THE SKIN WAS REPAIRED IAW ECRA 5750-03755.
- [SDR CALA0300113](https://openairdocs.org/sdr/CALA0300113.md): Skin · delaminated · Mar 7, 2003 · N14871 · Doug DC981 · Leading Edge Devices
  > MAINTENANCE FOUND THE R/H INBOARD FLAP OUTBOARD VANE UPPER SKIN DELAMINATED. THE FINAL TRIM OUT AREA MEASURED 4.3" X 6.4". THE SKIN WAS REPAIRED IAW ECRA 5750-03756.
- [SDR CALA0300104](https://openairdocs.org/sdr/CALA0300104.md): Skin · cracked · Mar 7, 2003 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.01" CRACK IN FUSELAGE SKIN AT STA 1338, LONGERON 10R. REPAIRED IAW ECRA 5330-03221 AND ECRA 5330-03220.
- [SDR CALA0300103](https://openairdocs.org/sdr/CALA0300103.md): Skin · cracked · Mar 7, 2003 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND 0.01" CRACK IN FUSELAGE SKIN AT STA 1338 BELOW LONGERON 4R. REPAIRED IAW ECRA 5330-03221 AND ECRA 5330-03220.
- [SDR CALA0300096](https://openairdocs.org/sdr/CALA0300096.md): Skin · cracked · Mar 6, 2003 · N14871 · Doug DC981 · Passenger/Crew Doors
  > INSPECTION FOUND A 1/4" CRACK IN MAIN CABIN DOOR EXTERIOR SKIN AT LOWER FORWARD CORNER. A REPAIR WAS INSTALLED IAW SRM 52-05.
- [SDR CALA0300092](https://openairdocs.org/sdr/CALA0300092.md): Beltframe · cracked · Mar 3, 2003 · N14871 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND A 1/2" CRACK IN CANTED BELTFRAME AT STA 1416, LONGERON 4L TO 4R. INSTALLED NEW FRAME IAW SRM 51-00.
- [SDR CALA0300091](https://openairdocs.org/sdr/CALA0300091.md): Cargo Track · corroded · Mar 3, 2003 · N14871 · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT BAGGAGE BIN RT TIE DOWN TRACK HOLES CORRODED AT STA 1136 - 1155. A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 53-23-00.
- [SDR CALA0300090](https://openairdocs.org/sdr/CALA0300090.md): Beltframe · cracked · Mar 3, 2003 · N14871 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND A 1/2" CRACK IN CANTED BELTFRAME AT STA 1446, LONGERON 6R TO 5L. THE BELTFRAME WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300076](https://openairdocs.org/sdr/CALA0300076.md): Cargo Track · corroded · Feb 28, 2003 · N14871 · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT BAGGAGE BIN LT TIE DOWN TRACK HOLES CORRODED BETWEEN STA 1231-1271. THE TIE DOWN TRACK WAS REPLACED IAW SRM 53-23-0.
- [SDR CALA0200023](https://openairdocs.org/sdr/CALA0200023.md): Link · failed · Jan 15, 2002 · N14871 · Doug DC981 · Landing Gear Door Retract Section
  > WHEN THE GEAR WAS RAISED AFTER TAKEOFF, THE GEAR RETRACTED WITH ALL INDICATIONS NORMAL. THERE WAS A LOUD NOISE INDICATIVE OF THE NOSE GEAR DOOR HANGING DOWN AND WHICH WAS ACCOMPANIED BY STRONG VIBRATION IN THE NOSE GEAR AREA. THE GEAR WAS CYCLED WITH NO CHANGE
- [SDR CALA0101043](https://openairdocs.org/sdr/CALA0101043.md): Slide · failed · Dec 29, 2001 · N14871 · Doug DC981 · Escape Slide
  > THE L-1 DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT TEST. THE SLIDE WAS REMOVED AND REPLACED IAW WORK CARD 08-2560-1-4300.
- [SDR CALA0101042](https://openairdocs.org/sdr/CALA0101042.md): Slide · failed · Dec 29, 2001 · N14871 · Doug DC981 · Escape Slide
  > THE R-1 DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT TEST. THE SLIDE WAS REMOVED AND REPLACED IAW WORK CARD 08-2560-1-4300.
- [SDR CALA0100591](https://openairdocs.org/sdr/CALA0100591.md): Battery Pack · discharged · Jun 24, 2001 · N14871 · Doug DC981 · Emergency Lighting
  > THE LT AND RT FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE DURING TEST. THE B5-103 BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0100039](https://openairdocs.org/sdr/CALA0100039.md): Light · inoperative · Jan 17, 2001 · N14871 · Doug DC981 · Emergency Lighting
  > INSPECTION FOUND FORWARD ENTRY PORTABLE EMERGENCY LIGHT INOPERATIVE. THE FORWARD ENTRY EMERGENCY LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0001680](https://openairdocs.org/sdr/CALA0001680.md): Floor Support · corroded · Oct 30, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200, RBL 41 - 55. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0001678](https://openairdocs.org/sdr/CALA0001678.md): Cargo Track · corroded · Oct 28, 2000 · N14871 · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FORWARD RT SIDE CARGO TRACK IN MID PIT CORRODED AT STA 541 - 636. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2.
- [SDR CALA0001677](https://openairdocs.org/sdr/CALA0001677.md): Strap · corroded · Oct 28, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID CARGO LOWER DOOR JAMB CORRODED AT FS 640 - 690. THE CORRODED STRAP WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-7, AND 51-10-4.
- [SDR CALA0001676](https://openairdocs.org/sdr/CALA0001676.md): Web · corroded · Oct 28, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT CUSP WEB CORRODED UNDER FLOOR SUPPORT AT FS 1136 - 1155. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.
- [SDR CALA0001675](https://openairdocs.org/sdr/CALA0001675.md): Floor Support · corroded · Oct 28, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 140 - 200, RBL 7. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-30-2.
- [SDR CALA0001674](https://openairdocs.org/sdr/CALA0001674.md): Floor Support · corroded · Oct 28, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 200, LBL 11 AND LBL 3 - RBL 3. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0001673](https://openairdocs.org/sdr/CALA0001673.md): Floor Support · corroded · Oct 28, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 200, LBL 43. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.
- [SDR CALA0001672](https://openairdocs.org/sdr/CALA0001672.md): Floor Support · corroded · Oct 28, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 150 - 200, LBL 7 AND RBL 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-2, 51-30-5, AND 51-30-1.
- [SDR CALA0001671](https://openairdocs.org/sdr/CALA0001671.md): Strap · corroded · Oct 28, 2000 · N14871 · Doug DC981 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO LOWER DOOR JAMB CORRODED AT FS 1155 - 1211. THE CORRODED STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND ECRA 5310-03027.
- [SDR CALA0001670](https://openairdocs.org/sdr/CALA0001670.md): Skin · dented · Oct 27, 2000 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1251 - 1271 BETWEEN LONGERON 22R AND 23R. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 20, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0001668](https://openairdocs.org/sdr/CALA0001668.md): Floor Support · corroded · Oct 27, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3.
- [SDR CALA0001667](https://openairdocs.org/sdr/CALA0001667.md): Skin · cracked · Oct 27, 2000 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND L-1 DOOR JAMB TORQUE BOX SKIN AFT LEG CRACKED AT FS 200. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW EA 9-5314-2-A0781, SRM 51-10-3, 51-30-3, 51-30-2, AND ECRA 5310-04051.
- [SDR CALA0001666](https://openairdocs.org/sdr/CALA0001666.md): Skin · dented · Oct 27, 2000 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT EXTERNAL FUSELAGE SKIN DENTED AT FS 37 BETWEEN LONGERON 6R AND 18R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-60, 53-01, FIGURE 7, 51-10-3, AND 51-30-2.
- [SDR CALA0001665](https://openairdocs.org/sdr/CALA0001665.md): Fitting · cracked · Oct 27, 2000 · N14871 · Doug DC981 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND EXTERNAL FUSELAGE LOWER T-FITTING CRACKED AT FS 864, LONGERON 30. THE T-FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4.
- [SDR CALA0001664](https://openairdocs.org/sdr/CALA0001664.md): Floor Support · punctured · Oct 27, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT ANGLE PUNCTURED AT STA 541, L28R TO 28L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, FIGURE 7A, AND 51-10-4.
- [SDR CALA0001663](https://openairdocs.org/sdr/CALA0001663.md): Skin · dented · Oct 27, 2000 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AND GOUGED AT FS 290 BETWEEN LONGERON 23L AND 24L. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, VIEW 1.
- [SDR CALA0001662](https://openairdocs.org/sdr/CALA0001662.md): Web · cracked · Oct 27, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THREE 2 INCH CRACKS IN LT SIDE VENT BOX AREA UPPER AFT CORNER WEB AT FORWARD SIDE OF FRAME STA 1485. THE CRACKS WERE STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2.
- [SDR CALA0001661](https://openairdocs.org/sdr/CALA0001661.md): Pan · cracked · Oct 26, 2000 · N14871 · Doug DC981 · Landing Gear Doors
  > INSPECTION FOUND A 1 INCH CRACK IN RT MLG I/B DOOR FORWARD SIDE TOP CORNER. THE DOOR PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-2, 51-10-4, 51-30-2, AND 51-30-5.
- [SDR CALA0001660](https://openairdocs.org/sdr/CALA0001660.md): Frame · cracked · Oct 26, 2000 · N14871 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD FRAME SUPPORT ANGLE AT FS 229 - 256, LONGERON 1L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2.
- [SDR CALA0001659](https://openairdocs.org/sdr/CALA0001659.md): Web · corroded · Oct 26, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON SUB FLOOR AND UNDER CUSP WEB AT FS 175, LBL 54. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WAS INSTALLED IAW SRM 51-10-4, 53-14-1, 51-10-3, 51-30-2, AND 51-30-5.
- [SDR CALA0001648](https://openairdocs.org/sdr/CALA0001648.md): Frame · corroded · Oct 25, 2000 · N14871 · Doug DC981 · Fuselage Main, Structure
  > INSPECTION FOUND CABIN WINDOW FRAME 41L CORRODED ON FORWARD AND AFT FLANGES AT STA 984 AND 1003. A REPAIR AND WINDOW DOUBLER WAS INSTALLED IAW EA 9-5330-2-A0794, ECRA 5330-02998, AND DOUGLAS DRAWING SRO9530053.
- [SDR CALA0001647](https://openairdocs.org/sdr/CALA0001647.md): Cargo Track · corroded · Oct 25, 2000 · N14871 · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT FS 522 - 798. THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE TRACK WAS TREATED AND PRIMED FROM FS 522 - 617 AND FROM 700 - 798. FS 617 - 700 WAS FOUND OUT OF LIMITS. A REPAIR TRACK WAS INSTALLED FROM
- [SDR CALA0001646](https://openairdocs.org/sdr/CALA0001646.md): Floor Panel · cracked · Oct 25, 2000 · N14871 · Doug DC981 · Fuselage Floor Panel
  > INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B FLOOR PANEL EDGE AT FS 927 - 1003. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-01.
- [SDR CALA0001645](https://openairdocs.org/sdr/CALA0001645.md): Web · corroded · Oct 24, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUBFLOOR WEB CORRODED AT FS 218, RBL 11 UPON REMOVAL OF GALLEY SUPPORT AND FITTING. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-30-2, AND 51-30-8.
- [SDR CALA0001644](https://openairdocs.org/sdr/CALA0001644.md): Door Frame · dented · Oct 24, 2000 · N14871 · Doug DC981 · Fuselage Main, Structure
  > INSPECTION FOUND R-1 DOOR JAMB AT AFT CENTER AREA MAIN FRAME BEHIND ROLLER ASSEMBLY DENTED IN RADIUS. THE DOOR STOP WAS REMOVED IAW SRM 51-30-1. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 42, 51-30-1, AND 51-30-2. A NEW DOOR STOP WAS INSTALLED IAW SRM 51-
- [SDR CALA0001638](https://openairdocs.org/sdr/CALA0001638.md): Skin · corroded · Oct 23, 2000 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN UNDER FWD WING TO BODY FAIRING CORRODED AT STA 769 BETWEEN STRINGERS 28R AND 27R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 53 AND FILLET ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0001637](https://openairdocs.org/sdr/CALA0001637.md): Skin · dented · Oct 23, 2000 · N14871 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 170 BETWEEN LONGERONS 20R - 21R. THE DENTED AREA WAS REPAIRED WITH A DOUBLER IAW SRM 53-04, FIGURE 38G.
- [SDR CALA0001636](https://openairdocs.org/sdr/CALA0001636.md): Floor Support · corroded · Oct 23, 2000 · N14871 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 168, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-30-5, AND 51-10-3.

Next page: https://openairdocs.org/deregistered/N14871-2004-12-07/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 = 'N14871' AND deregistration_id = 'N14871-2004-12-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14871-2004-12-07/reports

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