# N809NY: 1984 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2002-11-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 26, 2002 - Exported to: Indonesia - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49263 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 17, 1984 - Certificate issued: February 7, 2001 - Last registry action: November 20, 2002 - Mode S code: AB048F - Owner when cancelled: [East Trust Sub 12](https://openairdocs.org/faa-owner/EAST%20TRUST%20SUB%2012) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N809NY - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=809NY - Page: https://openairdocs.org/deregistered/N809NY-2002-11-26 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (56, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0001979](https://openairdocs.org/sdr/CALA0001979), Dec 21, 2000: CARGO TRACK. GOUGED. 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), Dec 21, 2000: STRUCTURE. CRACKED. 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), Dec 21, 2000: ANGLE. CORRODED. 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), Dec 20, 2000: WEB. CRACKED. 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 - [SDR CALA0001964](https://openairdocs.org/sdr/CALA0001964), Dec 20, 2000: SUPPORT. CRACKED. 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- - [SDR CALA0001956](https://openairdocs.org/sdr/CALA0001956), Dec 19, 2000: ANGLE. CORRODED. 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 5310-04 - [SDR CALA0001955](https://openairdocs.org/sdr/CALA0001955), Dec 18, 2000: ANGLE. CRACKED. 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- - [SDR CALA0001954](https://openairdocs.org/sdr/CALA0001954), Dec 18, 2000: SKIN. DENTED. 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 - [SDR CALA0001953](https://openairdocs.org/sdr/CALA0001953), Dec 18, 2000: CARGO TRACK. CORRODED. 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 - [SDR CALA0001952](https://openairdocs.org/sdr/CALA0001952), Dec 18, 2000: FLOOR SUPPORT. CORRODED. 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 5 - [SDR CALA0001951](https://openairdocs.org/sdr/CALA0001951), Dec 18, 2000: RIB. CORRODED. 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 - [SDR CALA0001950](https://openairdocs.org/sdr/CALA0001950), Dec 18, 2000: STOP. WORN. 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 51-1 - [SDR CALA0001941](https://openairdocs.org/sdr/CALA0001941), Dec 18, 2000: FLOOR SUPPORT. CORRODED. 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, FIGUR - [SDR CALA0001940](https://openairdocs.org/sdr/CALA0001940), Dec 18, 2000: SEAT TRACK. CORRODED. 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), Dec 18, 2000: INTERCOSTAL. CORRODED. 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), Dec 17, 2000: SEAT TRACK. CORRODED. 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- - [SDR CALA0001936](https://openairdocs.org/sdr/CALA0001936), Dec 17, 2000: WEB. CRACKED. 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), Dec 17, 2000: CARGO TRACK. CORRODED. 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 - [SDR CALA0001934](https://openairdocs.org/sdr/CALA0001934), Dec 17, 2000: FLOOR SUPPORT. CORRODED. 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 - [SDR CALA0001933](https://openairdocs.org/sdr/CALA0001933), Dec 17, 2000: SEAT TRACK. CORRODED. 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), Dec 16, 2000: WEB. CORRODED. 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, FIGUR - [SDR CALA0001925](https://openairdocs.org/sdr/CALA0001925), Dec 15, 2000: FITTING. CORRODED. 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 WE - [SDR CALA0001924](https://openairdocs.org/sdr/CALA0001924), Dec 15, 2000: DOOR FRAME. BROKEN. 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 IA - [SDR CALA0001920](https://openairdocs.org/sdr/CALA0001920), Dec 15, 2000: FLOOR SUPPORT. CORRODED. 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, 51-3 - [SDR CALA0001919](https://openairdocs.org/sdr/CALA0001919), Dec 15, 2000: DOUBLER. CHAFED. 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, - [SDR CALA0001915](https://openairdocs.org/sdr/CALA0001915), Dec 14, 2000: WEB. CORRODED. 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 DO - [SDR CALA0001914](https://openairdocs.org/sdr/CALA0001914), Dec 14, 2000: SEAT TRACK. CORRODED. 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 - [SDR CALA0001913](https://openairdocs.org/sdr/CALA0001913), Dec 14, 2000: SEAT TRACK. CORRODED. 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 51-3 - [SDR CALA0001912](https://openairdocs.org/sdr/CALA0001912), Dec 14, 2000: CARGO TRACK. CORRODED. 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 A - [SDR CALA0001909](https://openairdocs.org/sdr/CALA0001909), Dec 13, 2000: SKIN. DENTED. 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), Dec 13, 2000: FITTING. CORRODED. 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), Dec 13, 2000: DOUBLER. CHAFED. 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), Dec 12, 2000: FLOORBEAM. CORRODED. 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 - [SDR CALA0001900](https://openairdocs.org/sdr/CALA0001900), Dec 12, 2000: WEB. CORRODED. 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 51-3 - [SDR CALA0001893](https://openairdocs.org/sdr/CALA0001893), Dec 11, 2000: SEAT TRACK. CORRODED. 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 - [SDR CALA0001892](https://openairdocs.org/sdr/CALA0001892), Dec 11, 2000: SKIN. DENTED. 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, FIGUR - [SDR CALA0001881](https://openairdocs.org/sdr/CALA0001881), Dec 11, 2000: FLOOR SUPPORT. CORRODED. 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 REM - [SDR CALA0001873](https://openairdocs.org/sdr/CALA0001873), Dec 8, 2000: SKIN. DENTED. 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), Dec 7, 2000: SKIN. DENTED. 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), Mar 7, 1999: SENSOR. INOP. THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC - [SDR CALA9801968](https://openairdocs.org/sdr/CALA9801968), Oct 19, 1998: CABLE. OUT OF ADJ. 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), Oct 19, 1998: LONGERON. CORRODED. 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), Oct 16, 1998: BEAM. CRACKED. 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), Oct 14, 1998: DOUBLER. CORRODED. 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), Oct 13, 1998: JAMB. CORRODED. 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), Apr 21, 1998: STRUT. FLAT. 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 NU - [SDR CALA9800578](https://openairdocs.org/sdr/CALA9800578), Mar 22, 1998: SUPPORT. CRACKED. 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 ABO - [SDR CALA9701236](https://openairdocs.org/sdr/CALA9701236), Aug 24, 1997: OIL SCREEN COVER. LEAKING. 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 WITHO - [SDR CALA9700663](https://openairdocs.org/sdr/CALA9700663), May 6, 1997: FAN. INOPERATIVE. 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 WITH - [SDR CALA9601473](https://openairdocs.org/sdr/CALA9601473), Oct 16, 1996: SUPPORT LEG. CRACKED. 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. All 56: https://openairdocs.org/deregistered/N809NY-2002-11-26/reports.md ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19900214009669I](https://openairdocs.org/incident/19900214009669I), Feb 14, 1990: Doug DC982 (N809NY), Denver, CO, Minor damage. Tail cone came off and escape slide deployed on rollout. Found emergency slide handle not in its detent. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.