# N819NY: 1986 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-08-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 3, 2005
- Exported to: Thailand
- 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: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 49479
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: August 12, 1986
- Certificate issued: April 4, 2005
- Last registry action: June 24, 2005
- Mode S code: AB2C0E
- Owner when cancelled: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC)
- Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston)
- Owner type: Corporation
- Owner's area on the map: 29.7568° N, 95.3657° W: Placed by OpenAirDocs at the center of ZIP code 77002, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N819NY
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=819NY
- Page: https://openairdocs.org/deregistered/N819NY-2005-08-03

From the FAA registry file of November 5, 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 (138, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA0400607](https://openairdocs.org/sdr/CALA0400607), Aug 20, 2004: SLAT TRACK. CRACKED. 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), Jun 5, 2004: BELTFRAME. CORRODED. 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), Jun 4, 2004: LONGERON. CORRODED. INSPECTION FOUND LONGERON 22L CORRODED AT STA 1287. REPAIRED IAW SRM 53-02, FIGURE 18.
- [SDR CALA0400515](https://openairdocs.org/sdr/CALA0400515), May 28, 2004: SKIN. CRACKED. 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 5
- [SDR CALA0400514](https://openairdocs.org/sdr/CALA0400514), May 28, 2004: ANGLE. CRACKED. 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), May 25, 2004: CUSP WEB. CRACKED. 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), May 25, 2004: FLOOR SUPPORT. CORRODED. 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-
- [SDR CALA0400504](https://openairdocs.org/sdr/CALA0400504), May 24, 2004: LONGERON. CRACKED. 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), May 24, 2004: FLOOR SUPPORT. CORRODED. 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 I
- [SDR CALA0400502](https://openairdocs.org/sdr/CALA0400502), May 23, 2004: CHANNEL. CORRODED. 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), Jan 25, 2004: CONNECTOR. SHORTED. 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 F
- [SDR CALA0400020](https://openairdocs.org/sdr/CALA0400020), Jan 12, 2004: WEB. CRACKED. 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), Jan 12, 2004: BEAM. DAMAGED. 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), Oct 31, 2002: FITTING. 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), Oct 31, 2002: SKIN. 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), Oct 29, 2002: ANGLE. 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), Jul 9, 2001: BATTERY. DISCHARGED. INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE FROM ROWS 1-7. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS WERE REMOVED AND REPLACED AND OPERATION CH
- [SDR CALA0001343](https://openairdocs.org/sdr/CALA0001343), Aug 31, 2000: SENSOR. INOPERATIVE. 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 R
- [SDR CALA0000992](https://openairdocs.org/sdr/CALA0000992), Jun 28, 2000: SEAT TRACK. CORRODED. 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 IA
- [SDR CALA0000990](https://openairdocs.org/sdr/CALA0000990), Jun 26, 2000: ATTACH ANGLE. CORRODED. 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
- [SDR CALA0000989](https://openairdocs.org/sdr/CALA0000989), Jun 26, 2000: SKIN. CANNING. 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.
- [SDR CALA0000988](https://openairdocs.org/sdr/CALA0000988), Jun 26, 2000: ANGLE. CRACKED. 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 A
- [SDR CALA0000987](https://openairdocs.org/sdr/CALA0000987), Jun 26, 2000: SKIN PANEL. CORRODED. 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 REM
- [SDR CALA0000986](https://openairdocs.org/sdr/CALA0000986), Jun 26, 2000: SEAT TRACK. CORRODED. 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
- [SDR CALA0000985](https://openairdocs.org/sdr/CALA0000985), Jun 26, 2000: TRIM TAB. DENTED. 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 PERFORME
- [SDR CALA0000965](https://openairdocs.org/sdr/CALA0000965), Jun 24, 2000: SKIN. DAMAGED. 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 WER
- [SDR CALA0000964](https://openairdocs.org/sdr/CALA0000964), Jun 24, 2000: SKIN. CORRODED. INSPECTION FOUND LT WING SKIN CORRODED AT XFS 164 - XFS 267. REPAIRED AREA IAW ECRA 5730-01700.
- [SDR CALA0000963](https://openairdocs.org/sdr/CALA0000963), Jun 24, 2000: SKIN. CORRODED. 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), Jun 24, 2000: BRACKET. CRACKED. 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, 
- [SDR CALA0000961](https://openairdocs.org/sdr/CALA0000961), Jun 24, 2000: SKIN. DENTED. 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
- [SDR CALA0000959](https://openairdocs.org/sdr/CALA0000959), Jun 24, 2000: SKIN. CRACKED. 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 I
- [SDR CALA0000958](https://openairdocs.org/sdr/CALA0000958), Jun 23, 2000: ATTACH ANGLE. CRACKED. 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
- [SDR CALA0000956](https://openairdocs.org/sdr/CALA0000956), Jun 21, 2000: SKIN. CORRODED. 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), Jun 20, 2000: SKIN. CORRODED. 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), Jun 20, 2000: CARGO TRACK. CORRODED. 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 
- [SDR CALA0000937](https://openairdocs.org/sdr/CALA0000937), Jun 20, 2000: FLOORBEAM. CORRODED. 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 
- [SDR CALA0000936](https://openairdocs.org/sdr/CALA0000936), Jun 20, 2000: FLOOR SUPPORT. CORRODED. 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 REM
- [SDR CALA0000935](https://openairdocs.org/sdr/CALA0000935), Jun 20, 2000: FLOOR SUPPORT. CORRODED. 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 REMOVE
- [SDR CALA0000934](https://openairdocs.org/sdr/CALA0000934), Jun 20, 2000: SKIN. DENTED. 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 M
- [SDR CALA0000933](https://openairdocs.org/sdr/CALA0000933), Jun 20, 2000: SKIN. CORRODED. 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 5730-016
- [SDR CALA0000932](https://openairdocs.org/sdr/CALA0000932), Jun 20, 2000: CARGO TRACK. CORRODED. 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 INS
- [SDR CALA0000931](https://openairdocs.org/sdr/CALA0000931), Jun 20, 2000: SEAT TRACK. CORRODED. 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-
- [SDR CALA0000930](https://openairdocs.org/sdr/CALA0000930), Jun 20, 2000: CARGO TRACK. CORRODED. 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 SP
- [SDR CALA0000923](https://openairdocs.org/sdr/CALA0000923), Jun 19, 2000: FITTING. CRACKED. 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 51-3
- [SDR CALA0000922](https://openairdocs.org/sdr/CALA0000922), Jun 19, 2000: ATTACH ANGLE. CORRODED. 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
- [SDR CALA0000921](https://openairdocs.org/sdr/CALA0000921), Jun 19, 2000: SEAT TRACK. CORRODED. 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), Jun 15, 2000: ANGLE. CORRODED. 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 
- [SDR CALA0000908](https://openairdocs.org/sdr/CALA0000908), Jun 15, 2000: SEAT TRACK. CORRODED. 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), Jun 13, 2000: DOOR FRAME. CRACKED. 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), Jun 13, 2000: CARGO TRACK. CORRODED. 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.

All 138: https://openairdocs.org/deregistered/N819NY-2005-08-03/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC91LA247](https://openairdocs.org/ntsb/NYC91LA247), Sep 28, 1991: Mcdonnell Douglas MD-82 (N819NY), East Boston, MA, minor damage. Probable cause: THE MALFUNCTION OF AN ELECTRICAL COMPONENT IN THE COCKPIT, WHICH RESULTED IN SMOKE AND THE SUBSEQUENT EMERGENCY EVACUATION OF THE PASSENGERS FROM THE AIRPLANE.

## FAA accident and incident reports (2)

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 19930511016219I](https://openairdocs.org/incident/19930511016219I), May 11, 1993: Doug DC982 (N819NY), San Francisco, CA. Right engine had three compressor stalls on climb. Returned to airport.
- [Accident 19910928043739A](https://openairdocs.org/incident/19910928043739A), Sep 28, 1991: Doug DC982 (N819NY), Boston, MA, Minor damage. Smoke in cockpit on taxi for departure. Stopped. Evacuated. Fuse holder for an instrument shorted.

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