# Service difficulty reports: N809NY, cancelled Nov 26, 2002

A list on [N809NY, cancelled Nov 26, 2002](https://openairdocs.org/deregistered/N809NY-2002-11-26.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 · 56 reports

- [SDR CALA0001979](https://openairdocs.org/sdr/CALA0001979.md): Cargo Track · gouged · Dec 21, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND GOUGES IN MID PIT RT AFT CARGO TRACK AT FS 693-788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1.
- [SDR CALA0001977](https://openairdocs.org/sdr/CALA0001977.md): Structure · cracked · Dec 21, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TORQUE BOX WEB CRACKED AT FS 200-208, LBL 54 (AFT OF L-1 DOOR). THE TORQUE BOX WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0001976](https://openairdocs.org/sdr/CALA0001976.md): Angle · corroded · Dec 21, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT Z-ANGLE THAT MOUNTS TO CARGO TRACK CORRODED AT FS 693-733. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4.
- [SDR CALA0001969](https://openairdocs.org/sdr/CALA0001969.md): Web · cracked · Dec 20, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK AT LIGHTENING HOLE OF AFT CARGO TORQUE BOX WEB, FS 1211, L27R. THE WEB, ATTACHING STRAPS, AND L-ANGLE SUPPORT WERE REMOVED AND A NEW WEB WAS INSTALLED USING ATTACHMENT PARTS IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0001964](https://openairdocs.org/sdr/CALA0001964.md): Support · cracked · Dec 20, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO FLOORBOARD SUPPORT IN CARGO DOOR AREA CRACKED AT FS 1136-1220. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR CALA0001956](https://openairdocs.org/sdr/CALA0001956.md): Angle · corroded · Dec 19, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-1 DOOR JAMB CUSP ANGLE CORRODED AT FS 200, LBL 54. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-5, ECRA 5310-04082, AND EA 9-5310-2-A809.
- [SDR CALA0001955](https://openairdocs.org/sdr/CALA0001955.md): Angle · cracked · Dec 18, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN L-1 DOOR FORWARD LOWER CORNER ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-8.
- [SDR CALA0001954](https://openairdocs.org/sdr/CALA0001954.md): Skin · dented · Dec 18, 2000 · N809NY · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND EXTERIOR SKIN OF MID CARGO DOOR DENTED IN TWO PLACES. THE DENTED AREAS WERE CUT OUT AND DOUBLER AND FILLER REPAIRS WERE INSTALLED IAW SRM 52-05, FIGURE 3, 51-10-3, AND ECRA 5230-01207.
- [SDR CALA0001953](https://openairdocs.org/sdr/CALA0001953.md): Cargo Track · corroded · Dec 18, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT FORWARD CARGO TIE DOWN TRACK CORRODED AT STA 218-370. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4.
- [SDR CALA0001952](https://openairdocs.org/sdr/CALA0001952.md): Floor Support · corroded · Dec 18, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT I/B OF DOOR SCUFF PLATE AT AFT SERVICE DOOR CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-14-3, FIGURE 12 AND 51-30-02.
- [SDR CALA0001951](https://openairdocs.org/sdr/CALA0001951.md): Rib · corroded · Dec 18, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FASTENER HOLES CORRODED IN MID PIT FORWARD BULKHEAD SUPPORT RIBS. THE SUPPORT RIBS(2) WERE REMOVED AND TWO NEW SUPPORT RIBS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0001950](https://openairdocs.org/sdr/CALA0001950.md): Stop · worn · Dec 18, 2000 · N809NY · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR STOP PADS NR 2, 5, & 6 CHAFED/WORN. THE WORN AREAS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-10-3 AND ECRA 5330-02819.
- [SDR CALA0001941](https://openairdocs.org/sdr/CALA0001941.md): Floor Support · corroded · Dec 18, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD ENTRY SUBFLOOR CORRODED AT FS 148, RBL 6 AND AT FS 160-170, RBL 9. A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-01, FIGURE 4 AND 51-10-3.
- [SDR CALA0001940](https://openairdocs.org/sdr/CALA0001940.md): Seat Track · corroded · Dec 18, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN LT I/B SEAT TRACK CORRODED AT FS 896. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-5.
- [SDR CALA0001939](https://openairdocs.org/sdr/CALA0001939.md): Intercostal · corroded · Dec 18, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1022-1041. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-10-5.
- [SDR CALA0001937](https://openairdocs.org/sdr/CALA0001937.md): Seat Track · corroded · Dec 17, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN RT SEAT TRACK CORRODED AT FS 265-790. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 53-04, FIGURE 4F, AND 53-05, FIGURE 4B.
- [SDR CALA0001936](https://openairdocs.org/sdr/CALA0001936.md): Web · cracked · Dec 17, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND 1 INCH CRACKS IN LT CUSP WEBS AT STA 1032, 1231, AND 1260. DOUBLERS WERE INSTALLED AT EACH CRACK LOCATION IAW SRM 53-01, FIGURE 2 AND 51-30-2.
- [SDR CALA0001935](https://openairdocs.org/sdr/CALA0001935.md): Cargo Track · corroded · Dec 17, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CARGO TRACK IN MID PIT CORRODED ON UPPER AND LOWER SURFACES BETWEEN STA 541 AND 788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-30-1.
- [SDR CALA0001934](https://openairdocs.org/sdr/CALA0001934.md): Floor Support · corroded · Dec 17, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD ENTRY SUBFLOOR AND FLOOR SUPPORT CORRODED AT FS 160-200, LBL 54. THE SUBFLOOR AND FLOOR SUPPORT WERE REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 53-14-1, FIGURE 11.
- [SDR CALA0001933](https://openairdocs.org/sdr/CALA0001933.md): Seat Track · corroded · Dec 17, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 256. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.
- [SDR CALA0001929](https://openairdocs.org/sdr/CALA0001929.md): Web · corroded · Dec 16, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CORRODED AT FS 200-237, LBL 56. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 53-14-1, FIGURE 11.
- [SDR CALA0001925](https://openairdocs.org/sdr/CALA0001925.md): Fitting · corroded · Dec 15, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND NR 1 GALLEY SUPPORT FITTINGS (TWO EACH) CORRODED IN FASTENER HOLES AT STA 160, RBL 44 AND RBL 50. THE FITTINGS WERE REMOVED AND NEW FITTINGS WERE INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0001924](https://openairdocs.org/sdr/CALA0001924.md): Door Frame · broken · Dec 15, 2000 · N809NY · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND A 2 INCH PIECE BROKEN OUT OF AFT CARGO DOOR FRAME CUTOUT AT AFT UPPER EDGE, BS 1211, LONGERON 21R. THE FRAME CUTOUT WAS REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA0001920](https://openairdocs.org/sdr/CALA0001920.md): Floor Support · corroded · Dec 15, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 140-150, RBL 54. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-30-2, AND 51-30-4.
- [SDR CALA0001919](https://openairdocs.org/sdr/CALA0001919.md): Doubler · chafed · Dec 15, 2000 · N809NY · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND DOUBLER AT FORWARD LOWER CORNER OF FORWARD CARGO DOOR CHAFED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-10-3.
- [SDR CALA0001915](https://openairdocs.org/sdr/CALA0001915.md): Web · corroded · Dec 14, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD ENTRY CUSP WEB CORRODED AT FS 200-205, RBL 49-54 ON AFT SIDE OF FLOORBEAM. THE CORRODED SECTION OF CUSP WEB WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-8.
- [SDR CALA0001914](https://openairdocs.org/sdr/CALA0001914.md): Seat Track · corroded · Dec 14, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT O/B SEAT TRACKS CORRODED AT FS 807-1136 AND AT STA 1136-1309. THE SEAT TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-1, 51-30-2, AND 51-10-2.
- [SDR CALA0001913](https://openairdocs.org/sdr/CALA0001913.md): Seat Track · corroded · Dec 14, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 1032-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED USING A SPLICE REPAIR IAW SRM 51-30-1, 51-10-4, 53-05, FIGURE 4, 51-30-5, AND 51-30-2.
- [SDR CALA0001912](https://openairdocs.org/sdr/CALA0001912.md): Cargo Track · corroded · Dec 14, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FORWARD CARGO LT TIE DOWN TRACK CORRODED BETWEEN FS 218 AND 522. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0001909](https://openairdocs.org/sdr/CALA0001909.md): Skin · dented · Dec 13, 2000 · N809NY · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND AFT FUSELAGE LT LOWER SKIN DENTED AT STA 1322, LONGERON 27L-28L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-10-3.
- [SDR CALA0001908](https://openairdocs.org/sdr/CALA0001908.md): Fitting · corroded · Dec 13, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND NR 1 GALLEY SUPPORT MOUNT FITTING CORRODED AT STA 160, RBL 12. THE GALLEY SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0001907](https://openairdocs.org/sdr/CALA0001907.md): Doubler · chafed · Dec 13, 2000 · N809NY · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD LOWER CORNER OF MID CARGO DOOR CHAFED. THE REPAIR DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.
- [SDR CALA0001901](https://openairdocs.org/sdr/CALA0001901.md): Floorbeam · corroded · Dec 12, 2000 · N809NY · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP OF FLOORBEAM CORRODED AROUND NUTPLATE HOLES IN R/H AFT LAV AT FS 1322, RBL 17 TO RBL 53. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 20A AND 51-30-05.
- [SDR CALA0001900](https://openairdocs.org/sdr/CALA0001900.md): Web · corroded · Dec 12, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT CUSP WEB CORRODED AT FS 1140 (L-2 DOOR). THE CUSP WEB WAS REMOVED AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-4, 53-14-3, AND 51-30-2.
- [SDR CALA0001893](https://openairdocs.org/sdr/CALA0001893.md): Seat Track · corroded · Dec 11, 2000 · N809NY · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT STA 225. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4F, AND 51-30-5.
- [SDR CALA0001892](https://openairdocs.org/sdr/CALA0001892.md): Skin · dented · Dec 11, 2000 · N809NY · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 294 BETWEEN LONGERON 24 AND 25L AND AT STA 225, L16L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-30-02.
- [SDR CALA0001881](https://openairdocs.org/sdr/CALA0001881.md): Floor Support · corroded · Dec 11, 2000 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD ENTRY SUB FLOOR AND ATTACHING STRUCTURE CORRODED AT FS 160-200, RBL 54. TORQUE BOX STRAP, SUB FLOOR ATTACH ANGLES, AND DOUBLER WERE REMOVED IAW SRM 51-30-5 AND 51-30-2. DOUBLERS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0001873](https://openairdocs.org/sdr/CALA0001873.md): Skin · dented · Dec 8, 2000 · N809NY · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 270, LONGERON 17L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 21 AND 51-30-0.
- [SDR CALA0001869](https://openairdocs.org/sdr/CALA0001869.md): Skin · dented · Dec 7, 2000 · N809NY · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 237-256. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38 AND 53-04.
- [SDR CALA9900215](https://openairdocs.org/sdr/CALA9900215.md): Sensor · inop · Mar 7, 1999 · N809NY · Doug DC982 · Landing Gear Position and Warning
  > THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR AT FAULT. THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR
- [SDR CALA9801968](https://openairdocs.org/sdr/CALA9801968.md): Cable · out of adj · Oct 19, 1998 · N809NY · Doug DC982 · Aerodynamic Fairings
  > THE AFT ENTRY DOOR TAILCONE RELEASE PULLED HIGH AT 25 POUNDS. THE CABLE AND CONDUIT WERE REPLACED AND AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 53-53-00.
- [SDR CALA9801967](https://openairdocs.org/sdr/CALA9801967.md): Longeron · corroded · Oct 19, 1998 · N809NY · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 24L CORRODED IN AFT CARGO COMPARTMENT AT STA 1231. REPAIRED IAW SRM 53-02, FIGURE 18.
- [SDR CALA9801966](https://openairdocs.org/sdr/CALA9801966.md): Beam · cracked · Oct 16, 1998 · N809NY · Doug DC982 · Service Doors
  > INSPECTION FOUND A CRACK IN FORWARD SERVICE DOOR LOWER BEAM. THE LOWER BEAM WAS REPLACED IAW SRM 51-30-2.
- [SDR CALA9801958](https://openairdocs.org/sdr/CALA9801958.md): Doubler · corroded · Oct 14, 1998 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION IN AFT BAG BIN AT STA 1309 JUST ABOVE LONGERON 23 LEFT SIDE. REMOVED AND REPLACED DOUBLER PER 51-30-02.
- [SDR CALA9801950](https://openairdocs.org/sdr/CALA9801950.md): Jamb · corroded · Oct 13, 1998 · N809NY · Doug DC982 · Fuselage Miscellaneous Structure
  > MBB DOOR JAMB BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM 51-30-02 AND 51-30-05.
- [SDR CALA9800686](https://openairdocs.org/sdr/CALA9800686.md): Strut · flat · Apr 21, 1998 · N809NY · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > THE NLG WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG STRUT FLAT. A NEW GLAND NUT WAS INSTALLED AND THE STRUT WAS REPACKED.
- [SDR CALA9800578](https://openairdocs.org/sdr/CALA9800578.md): Support · cracked · Mar 22, 1998 · N809NY · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND A.375 INCH CRACK AT LOWER RIVET HOLE IN FORWARD LEFT VERTICAL STABILIZER SPAR SUPPORT AT 37.3 INCHES AFT OF STA 1089.3 IN TAIL COMPARTMENT ABOVE CATWALK. THE AREA WAS REPAIRED IAW SRM 55-02, FIGURE 26.
- [SDR CALA9701236](https://openairdocs.org/sdr/CALA9701236.md): Oil Screen Cover · leaking · Aug 24, 1997 · N809NY · Doug DC982 · Turbine Engine Oil System
  > THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO FOLLOWED BY OIL PRESSURE DECREASING TO 10 PSI AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PLUG ON MAIN OIL SCREEN COVER LEAKING. A NEW OIL SCREEN COVER ASSE
- [SDR CALA9700663](https://openairdocs.org/sdr/CALA9700663.md): Fan · inoperative · May 6, 1997 · N809NY · Doug DC982 · Air Distribution Fan
  > LIGHT SMOKE WAS REPORTED IN CABIN WHILE EN ROUTE TO SEA. THE RECIRCULATION FAN CIRCUIT BREAKER WAS PULLED AND THE SMOKE CLEARED. THE AIRCRAFT LANDED AT SEA WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE AIR DISTRIBUTION FAN AT FAULT. THE FAN WAS REMOVED AN
- [SDR CALA9601473](https://openairdocs.org/sdr/CALA9601473.md): Support Leg · cracked · Oct 16, 1996 · N809NY · Doug DC982 · Spoilers
  > FOUND OUTBOARD SUPPORT BRACKET OF LEFT HAND GROUND SPOILER UPPER AFT LEG WITH ONE INCH CRACK IN SUPPORT LEG. REPLACED CROSS BRACE PER EC/RA 5710-01756.

Next page: https://openairdocs.org/deregistered/N809NY-2002-11-26/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 = 'N809NY' AND deregistration_id = 'N809NY-2002-11-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N809NY-2002-11-26/reports

---
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