# Service difficulty reports: N819NY, cancelled Aug 3, 2005

A list on [N819NY, cancelled Aug 3, 2005](https://openairdocs.org/deregistered/N819NY-2005-08-03.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 3 · 138 reports

- [SDR CALA0400607](https://openairdocs.org/sdr/CALA0400607.md): Slat Track · cracked · Aug 20, 2004 · N819NY · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND A 1.5 INCH CRACK IN NR 10 AUX TRACK SLAT CAN XOS 380.229. THE NR 10 AUX TRACK SLAT, CAN WAS REMOVED AND REPLACED IAW SRM 51-30-0 AND 51-20-0.
- [SDR CALA0400524](https://openairdocs.org/sdr/CALA0400524.md): Beltframe · corroded · Jun 5, 2004 · N819NY · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CORRODED AT STA 1287, LONGERON 23L. A NEW SECTION OF FRAME WAS SPLICED IN IAW SRM 53-03, FIGURE 2A.
- [SDR CALA0400522](https://openairdocs.org/sdr/CALA0400522.md): Longeron · corroded · Jun 4, 2004 · N819NY · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 22L CORRODED AT STA 1287. REPAIRED IAW SRM 53-02, FIGURE 18.
- [SDR CALA0400515](https://openairdocs.org/sdr/CALA0400515.md): Skin · cracked · May 28, 2004 · N819NY · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 6 INCH CRACK IN FORWARD BAGGAGE BIN DOOR INNER SKIN AT BOTTOM AFT SIDE. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 52-05, FIGURE 26A.
- [SDR CALA0400514](https://openairdocs.org/sdr/CALA0400514.md): Angle · cracked · May 28, 2004 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN RIGHT WHEEL WELL FORWARD END ANGLE AT KEEL BEAM, STA 984. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA0400507](https://openairdocs.org/sdr/CALA0400507.md): Cusp Web · cracked · May 25, 2004 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN LT CUSP MEMBRANE AT STA 1271. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 96.
- [SDR CALA0400505](https://openairdocs.org/sdr/CALA0400505.md): Floor Support · corroded · May 25, 2004 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 168.7 AND 200, 14 INCHES INSIDE FORWARD SERVICE DOOR. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA0400504](https://openairdocs.org/sdr/CALA0400504.md): Longeron · cracked · May 24, 2004 · N819NY · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.25 INCH CRACK IN LONGERON 4L AT STA 160. A LONGERON SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18.
- [SDR CALA0400503](https://openairdocs.org/sdr/CALA0400503.md): Floor Support · corroded · May 24, 2004 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 200 FROM SIX INCHES I/B OF LEFT I/B SEAT TRACK TO CENTER SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA0400502](https://openairdocs.org/sdr/CALA0400502.md): Channel · corroded · May 23, 2004 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RIGHT HAT SECTION CORRODED AT STA 148-200, RBL 12. A NEW HAT SECTION WAS INSTALLED IAW SRM 53-14-01, 51-10-04, AND 51-30-01.
- [SDR CALA0400058](https://openairdocs.org/sdr/CALA0400058.md): Connector · shorted · Jan 25, 2004 · N819NY · Doug DC982 · Wash Water System
  > THE FORWARD LAV WATER HEATER CIRCUIT BREAKER POPPED WHILE ON DESCENT INTO EWR. THE LAV SMOKE DETECTOR ACTIVATED AND THE FLIGHT ATTENDANTS NOTICED SMOKE IN THE FORWARD LAV SHORTLY AFTER THE C/B POPPED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT EWR W
- [SDR CALA0400020](https://openairdocs.org/sdr/CALA0400020.md): Web · cracked · Jan 12, 2004 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN WEB CUTOUT AT STA 1155, LONGERON 27R IN AFT BAGGAGE BIN. THE WEB CUTOUT WAS REPAIRED IAW ECRA 5310-04393.
- [SDR CALA0400019](https://openairdocs.org/sdr/CALA0400019.md): Beam · damaged · Jan 12, 2004 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FASTENER HOLE ELONGATED IN MID CARGO DOOR THRESHOLD ZEE BEAM. THE FASTENER HOLE WAS REPAIRED IAW ECRA 5311-01182.
- [SDR CALA0200519](https://openairdocs.org/sdr/CALA0200519.md): Fitting · Oct 31, 2002 · N819NY · Doug DC982 · Doors
  > AFT SERVICE DOOR HOLD OPEN HOOK PAN ON DOOR CRACKED. REMOVED AND REPLACED HOOK PAN IAW SRM 51-40-02.
- [SDR CALA0200518](https://openairdocs.org/sdr/CALA0200518.md): Skin · Oct 31, 2002 · N819NY · Doug DC982 · Service Doors
  > AFT SERVICE DOOR OUTER SKIN CRACKED IN TWO PLACES AFT END OF HOLD OPEN HOOK WELL. REPAIRED DOOR SKIN PER ECRA 5205-01008 AND SRM 52-05, FIG 20A.
- [SDR CALA0200511](https://openairdocs.org/sdr/CALA0200511.md): Angle · Oct 29, 2002 · N819NY · Doug DC982 · Fuselage Structure (General)
  > LT ATTACH ANGLE FOR VERTICLE TO FUSELAGE IS CRACKED AT STA 1474. INSTALLED REPAIR ON ATTACH ANGLE PER SRM 53-05 FIG 23 AND SRM 53-05 FIG 23A.
- [SDR CALA0100642](https://openairdocs.org/sdr/CALA0100642.md): Battery · discharged · Jul 9, 2001 · N819NY · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE FROM ROWS 1-7. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA0001343](https://openairdocs.org/sdr/CALA0001343.md): Sensor · inoperative · Aug 31, 2000 · N819NY · Doug DC982 · Landing Gear Position and Warning
  > THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF FROM IAH. CHECKLIST PROCEDURES WERE FOLLOWED AND THE GEAR WAS LOWERED AND RAISED. THE NOSE GEAR PIN ON PEDESTAL INDICATED NOSE GEAR WAS FULL DOWN. THE AIRCRAFT WAS RETURNED
- [SDR CALA0000992](https://openairdocs.org/sdr/CALA0000992.md): Seat Track · corroded · Jun 28, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED ON FLOOR PANEL FLANGES AT STA 1145-1175, LBL 44. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, 51-10-4, AND 51-10-3.
- [SDR CALA0000990](https://openairdocs.org/sdr/CALA0000990.md): Attach Angle · corroded · Jun 26, 2000 · N819NY · Doug DC982 · Service Doors
  > INSPECTION FOUND L-1 DOOR LOWER AFT GIRT BAR ATTACH ANGLE CORRODED AT FS 200, LBL 54. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0000989](https://openairdocs.org/sdr/CALA0000989.md): Skin · canning · Jun 26, 2000 · N819NY · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR EXTERIOR SKIN OIL CANNING AND DENTED BELOW AFT HINGE. THE AFT DOOR ARM WAS REMOVED IAW MM 52-31-01. REMOVED WEB IAW SRM 51-10-4. THE DAMAGED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 3. A DOUBLER WAS INSTALLED IAW SRM 52-05, FI
- [SDR CALA0000988](https://openairdocs.org/sdr/CALA0000988.md): Angle · cracked · Jun 26, 2000 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR FORWARD UPLOCK ANGLE AT FS 1720, LBL 40. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.
- [SDR CALA0000987](https://openairdocs.org/sdr/CALA0000987.md): Skin Panel · corroded · Jun 26, 2000 · N819NY · Doug DC982 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND THAT THE LT AND RT HORIZONTAL STABILIZERS HAD BARREL NUT HOLES CORRODED WITH MISSING SEALANT. THE CORRODED BARREL NUTS AND PLI WASHERS WERE REMOVED AND REPLACED IAW MM 20-10-14. THE CORROSION WAS REMOVED AND BUSHINGS WERE INSTALLED IAW ECRA
- [SDR CALA0000986](https://openairdocs.org/sdr/CALA0000986.md): Seat Track · corroded · Jun 26, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1145 - 1175, LBL 44. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, 51-10-4, AND 51-10-3.
- [SDR CALA0000985](https://openairdocs.org/sdr/CALA0000985.md): Trim Tab · dented · Jun 26, 2000 · N819NY · Doug DC982 · Rudder, Tab Structure
  > INSPECTION FOUND RT SIDE OF RUDDER TRIM TAB DENTED. THE TRIM TAB WAS REMOVED AND REPLACED IAW MM 27-20-02, PARAGRAPH 3A, B, C. A WEIGHT AND BALANCE WAS PERFORMED ON THE TAB IAW SRM 55-40-1 AND THE CHECK WAS WITHIN LIMITS.
- [SDR CALA0000965](https://openairdocs.org/sdr/CALA0000965.md): Skin · damaged · Jun 24, 2000 · N819NY · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RADOME TO FUSELAGE SKIN DAMAGED AT FS 37, BL 0. THE RADOME WAS REMOVED IAW MM 53-51-00 AND THE DAMAGED AREA WAS CUT OUT. FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5330-02968 AND EA 9-5331-2-A0718. THE RADOME WAS REINSTALLED IAW MM 53-51-00
- [SDR CALA0000964](https://openairdocs.org/sdr/CALA0000964.md): Skin · corroded · Jun 24, 2000 · N819NY · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING SKIN CORRODED AT XFS 164 - XFS 267. REPAIRED AREA IAW ECRA 5730-01700.
- [SDR CALA0000963](https://openairdocs.org/sdr/CALA0000963.md): Skin · corroded · Jun 24, 2000 · N819NY · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING LOWER SKIN CORRODED AT MID BUTT, XFS 170 - XFS 290. THE AREA WAS REPAIRED IAW EA 9-5731-2-A0711 AND ECRA 5730-01700.
- [SDR CALA0000962](https://openairdocs.org/sdr/CALA0000962.md): Bracket · cracked · Jun 24, 2000 · N819NY · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING NR 1 SLAT TRACK LOWER FAIRING I/B BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-01, 51-10-04, 51-10-3.
- [SDR CALA0000961](https://openairdocs.org/sdr/CALA0000961.md): Skin · dented · Jun 24, 2000 · N819NY · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR OUTER SKIN AFT MID EDGE DENTED AND TORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, EA 9-5231-2-A0724, AND ECRA 5230-01559.
- [SDR CALA0000959](https://openairdocs.org/sdr/CALA0000959.md): Skin · cracked · Jun 24, 2000 · N819NY · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR JAMB SKIN AT APPROXIMATELY 20 FROM FORWARD LOWER CORNER, FS 389, LONGERON 27R. A FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-05, FIGURE 82, 51-30-2, AND 51-30-5.
- [SDR CALA0000958](https://openairdocs.org/sdr/CALA0000958.md): Attach Angle · cracked · Jun 23, 2000 · N819NY · Doug DC982 · Vertical Stabilizer, Attach Fittings
  > INSPECTION FOUND A 2 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT RT AFT END, STA 1275. FASTENERS WERE REMOVED AND THE CRACKED AREA WAS CUT OUT IAW SRM 51-30-5 AND 53-05, FIGURE 23. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 23, 51-
- [SDR CALA0000956](https://openairdocs.org/sdr/CALA0000956.md): Skin · corroded · Jun 21, 2000 · N819NY · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LOWER SKIN SURFACE CORRODED JUST O/B OF VORTILON AT XCW62-XRS 335. THE SKIN WAS REPAIRED IAW ECRA 5730-01700.
- [SDR CALA0000939](https://openairdocs.org/sdr/CALA0000939.md): Skin · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND LT WING LOWER SKIN CORRODED AT NR 1 FLAP HINGE, XRS 111.5. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW EA 9-5731-2-A0700 AND ECRA 5730-01695.
- [SDR CALA0000938](https://openairdocs.org/sdr/CALA0000938.md): Cargo Track · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT TIE DOWN TRACK CORRODED IN MID CARGO AREA AT STA 522 - 786.5, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0000937](https://openairdocs.org/sdr/CALA0000937.md): Floorbeam · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MID CARGO DOOR CUTOUT FLOORBEAM CORRODED AT FS 636 - 712, LONGERON 27R. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05. FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-02.
- [SDR CALA0000936](https://openairdocs.org/sdr/CALA0000936.md): Floor Support · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED IN MID CARGO AREA AT FS 693 - 731, LONGERON 27R AND AT FS 786 BETWEEN LONGERON 28L AND 28R. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-1.
- [SDR CALA0000935](https://openairdocs.org/sdr/CALA0000935.md): Floor Support · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED IN MID CARGO AREA AT STA 522 BETWEEN LONGEROSN 28L & 28R AND BETWEEN LONGERON 24L & 24R. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000934](https://openairdocs.org/sdr/CALA0000934.md): Skin · dented · Jun 20, 2000 · N819NY · Doug DC982 · Ailerons
  > INSPECTION FOUND LT AILERON UPPER SURFACE DENTED. A DOUBLER WAS INSTALLED IAW SRM 57-01. AN ADJUSTMENT TEST OF AILERON TRIM AND CONTROL TABS WAS PERFORMED IAW MM 27-10-05.
- [SDR CALA0000933](https://openairdocs.org/sdr/CALA0000933.md): Skin · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LOWER SKIN SURFACE CORRODED JUST FORWARD OF NR 2 FLAP HINGE AT XRS 111.5. REPAIRED IAW SRM 57-03, FIGURE 24A, SHEET 4 AND ECRA 5730-01694.
- [SDR CALA0000932](https://openairdocs.org/sdr/CALA0000932.md): Cargo Track · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT TIE DOWN TRACK CORRODED UNDER NUT CLIPS IN FORWARD PIT AT FS 218 - 538, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR CALA0000931](https://openairdocs.org/sdr/CALA0000931.md): Seat Track · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 720 - 795, RBL 54.5. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 53-05, FIGURE 4F, 51-30-1, AND 51-30-5.
- [SDR CALA0000930](https://openairdocs.org/sdr/CALA0000930.md): Cargo Track · corroded · Jun 20, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT TIE DOWN TRACK CORRODED IN AFT CARGO AREA AT FS 1007 - 1320, LONGERON 27L. THE TIE DOWN TRACK AND SPLICE WERE REMOVED AND A NEW TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 53-05, FIGURE 4B.
- [SDR CALA0000923](https://openairdocs.org/sdr/CALA0000923.md): Fitting · cracked · Jun 19, 2000 · N819NY · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2 INCH CRACK IN MID CARGO DOOR LOWER FORWARD STOP INNER SUPPORT FITTING. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-1.
- [SDR CALA0000922](https://openairdocs.org/sdr/CALA0000922.md): Attach Angle · corroded · Jun 19, 2000 · N819NY · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND L-1 DOOR LOWER AFT GIRT BAR ATTACH ANGLE CORRODED, BS 200, LBL 54. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0000921](https://openairdocs.org/sdr/CALA0000921.md): Seat Track · corroded · Jun 19, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 1207, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-5, AND 53-05, FIGURE 4F.
- [SDR CALA0000909](https://openairdocs.org/sdr/CALA0000909.md): Angle · corroded · Jun 15, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT CARGO TRACK Z-ANGLE CORRODED IN FORWARD PIT JUST AFT OF DOOR, FS 427, LONGERON 27R. THE Z-ANGLE AND A SUPPORT ANGLE WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-30-1.
- [SDR CALA0000908](https://openairdocs.org/sdr/CALA0000908.md): Seat Track · corroded · Jun 15, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1174, LBL 52.5. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000898](https://openairdocs.org/sdr/CALA0000898.md): Door Frame · cracked · Jun 13, 2000 · N819NY · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND A 1 INCH CRACK IN RT WHEEL WELL FORWARD I/B CORNER OF DOOR JAMB FRAME. THE DOOR JAMB FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-02.
- [SDR CALA0000894](https://openairdocs.org/sdr/CALA0000894.md): Cargo Track · corroded · Jun 13, 2000 · N819NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CARGO TRACK IN FORWARD PIT CORRODED AT FS 351, LONGERON 27R. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.

Next page: https://openairdocs.org/deregistered/N819NY-2005-08-03/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 = 'N819NY' AND deregistration_id = 'N819NY-2005-08-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N819NY-2005-08-03/reports

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