# N14889: 1982 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2003-07-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 23, 2003 - Exported to: Indonesia - Status when cancelled: Second triennial mailing, no response - 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: 49118 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 11, 1982 - Certificate issued: March 18, 1999 - Last registry action: March 26, 2002 - Mode S code: A0C3FA - Owner when cancelled: [Castle Harbour-I LLC](https://openairdocs.org/faa-owner/CASTLE%20HARBOUR-I%20LLC) - Location: Hamilton, Bermuda - Physical address: Hamilton, Bangladesh - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N14889 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14889 - Page: https://openairdocs.org/deregistered/N14889-2003-07-23 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 (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100828](https://openairdocs.org/sdr/CALA0100828), Aug 31, 2001: DUCT. BLOWN. THE CREW RECEIVED A FIRE WARNING INDICATION FROM THE RT ENGINE DURING CLIMBOUT OF IAH. THE THROTTLE WAS RETARDED AND THE FIRE WARNING INDICATION WENT OUT. THE A - [SDR CALA0100580](https://openairdocs.org/sdr/CALA0100580), Jun 22, 2001: FUSE. BLOWN. INSPECTION FOUND L-2 DOOR AND AFT STAIRWAY DOOR EXIT IDENTIFIER LIGHTS INOPERATIVE. THE FUSE FOR BATTERY PACK IN AFT CABIN DROP CEILING WAS REPLACED AND OPERATI - [SDR CALA0100225](https://openairdocs.org/sdr/CALA0100225), Mar 13, 2001: BEAM. CORRODED. INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED. A DOUBLER, SPACER, AND FASTENERS WERE INSTALLED. - [SDR CALA0100213](https://openairdocs.org/sdr/CALA0100213), Mar 8, 2001: WEB. CORRODED. INSPECTION FOUND FORWARD SIDE OF AFT CARGO TORQUE BOX WEB CORRODED. THE TORQUE BOX WEB AND ATTACHMENTS WERE REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-5, - [SDR CALA0100198](https://openairdocs.org/sdr/CALA0100198), Mar 3, 2001: DOOR FRAME. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED AROUND RIVNUTS. THE CORRODED AREA OF DOOR PAN WAS CUT OUT AND A REPAIR ANGLE AND SPLICE ANGLES WERE INSTAL - [SDR CALA0001837](https://openairdocs.org/sdr/CALA0001837), Nov 25, 2000: CABLE. OUT OF RIG. THE TAILCONE PULL FROM THE INTERIOR AND AFT DOOR HANDLES EXCEEDED LIMITS TO DROP TAIL CONE. THE TAILCONE CABLES WERE RIGGED IAW MM 53-53-00 AND OPERATION CHECKE - [SDR CALA0000940](https://openairdocs.org/sdr/CALA0000940), Jun 20, 2000: PROXIMITY SWITCH. OUT OF ADJ. THE RED NOSE GEAR WARNING LIGHT REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF FROM BWI. WHEN THE GEAR WAS EXTENDED FOR RETURN TO BWI THREE GREEN DO - [SDR CALA9802044](https://openairdocs.org/sdr/CALA9802044), Nov 5, 1998: HANDLE. OUT OF ADJUST. THE FORCE REQUIRED TO RELEASE TAIL CONE USING THE EXTERIOR, INTERIOR, AND AFT ENTRY DOOR HANDLES WAS OUT OF LIMITS. THE HANDLES WERE ADJUSTED AND TESTED IAW MM - [SDR CALA9802035](https://openairdocs.org/sdr/CALA9802035), Nov 4, 1998: FRAME. CORRODED. INSPECTION FOUND CORROSION ON CUSP MEMBRANE AND AFT SIDE OF FRAME AT STA 200 TO 204 JUST AFT OF MAIN CABIN DOOR AFT LOWER CORNER INSIDE LIGHTENING HOLE. A REPAI - [SDR CALA9802006](https://openairdocs.org/sdr/CALA9802006), Nov 1, 1998: FITTING. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN LT WHEEL WELL FITTING AT FLAP ACTUATOR MOUNTS STA 980. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA9801995](https://openairdocs.org/sdr/CALA9801995), Oct 27, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND L/H INBOARD SEAT TRACK CORRODED AT STA 1212-1309. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-1. - [SDR CALA9802003](https://openairdocs.org/sdr/CALA9802003), Oct 23, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND L/H INBOARD SEAT TRACK CORRODED AT STA 221. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGUR - [SDR CALA9802002](https://openairdocs.org/sdr/CALA9802002), Oct 23, 1998: INTERCOSTAL. CRACKED. INSPECTION FOUND A 2.5 CRACK IN INTERCOSTAL AT #1 VHF ANTENNA, STA 474. A NEW INTERCOSTAL WAS INSTALLED IAW EA 5330-01823. - [SDR CALA9801980](https://openairdocs.org/sdr/CALA9801980), Oct 20, 1998: SKIN. SCRATCHED. INSPECTION FOUND LT FUSELAGE SKIN SCRATCHED AT STA 237, LONGERON 17L. THE EXISTING DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5 AND ECRA 5330-02445 - [SDR CALA9800019](https://openairdocs.org/sdr/CALA9800019), Jan 13, 1998: BATTERIES. DISCHARGED. INSPECTION FOUND EMERGENCY LIGHTS ON CEILING ABOVE ROW 1 TO 4 AND ROW 22 TO 30 INOPERATIVE. THE BATTERIES IN FORWARD CABIN CEILING AND ABOVE ROW 24 WERE REMOVED - [SDR CALA9701159](https://openairdocs.org/sdr/CALA9701159), Aug 2, 1997: UPLOCK SENSOR. OUT OF ADJUST. THE NOSE GEAR UNSAFE LIGHT ILLUMINATED DURING CLIMBOUT. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE NOSE GEAR UNSAFE LIGHT EXTINGUISHED. THE FLIGHT WAS COMPL - [SDR CALA9700313](https://openairdocs.org/sdr/CALA9700313), Mar 6, 1997: ACTUATOR. LEAKING. THE HYDRAULIC QUANTITY DROPPED TO TWO QUARTS ON FINAL APPROACH, WHEN THE LANDING GEAR WAS LOWERED. THE NOSE GEAR CAME DOWN AND LOCKED ABOUT 30 SECONDS AFTER GEA - [SDR CALA9601605](https://openairdocs.org/sdr/CALA9601605), Oct 29, 1996: FRAME. CRACKED. INSPECTION FOUND .50 INCH CRACKS IN CANTED BELTFRAME AT STA 1446, LONGERONS 3, 4, AND 5R. THE FRAME WAS REPAIRED IAW SRM 53-03. - [SDR CALA9601297](https://openairdocs.org/sdr/CALA9601297), Sep 5, 1996: ENGINE. FAILED. THE TOWER REPORTED FIRE FROM THE NR 2 ENGINE TAILCONE AREA DURING TAXI OUT. THE CAPTAIN DISCHARGED BOTH ENGINE FIRE BOTTLES AND THE FIRE DEPARTMENT WAS SUMMONED - [SDR CALA9601206](https://openairdocs.org/sdr/CALA9601206), Aug 21, 1996: BEARING. FAILED. THE WHEEL NOT TURNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT LOW SPEED AND THE AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE FOUND THE N - [SDR CAL950487](https://openairdocs.org/sdr/CAL950487), Jun 14, 1995: EEL WIRING. BROKEN. EWR - FLT 0346 - INSPECTION FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 19-31 INOPERATIVE. MAINTENANCE FOUND WIRING TO LIGHTS BROKEN. THE WIRES WERE SPLICED AN - [SDR CAL950430](https://openairdocs.org/sdr/CAL950430), May 30, 1995: EEL BATT CHARGER. INOPERATIVE. FLT NR 1421 - EWR - WHEN EXTERNAL POWER WAS DISCONNECTED AT THE GATE, NONE OF THE OVERHEAD EMERGENCY LIGHTS BEHIND ROW 28 CAME ON. SOME BURNT OUT BULBS HAD TO B - [SDR CAL950416](https://openairdocs.org/sdr/CAL950416), May 24, 1995: SEPARATOR. FROZEN SHUT. IAH - FLT 0108 - THE AIRCRAFT STARTED LOSING PRESSURE AT 37,000 FEET WITH DE-ICING ON, AND OXYGEN MASKS WERE DROPPED MANUALLY. CREW ATTEMPTED SECONDARY WHICH IN ## 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 19960906037179I](https://openairdocs.org/incident/19960906037179I), Sep 6, 1996: Doug DC982 (N14889), New York, NY, Damage unknown. Narrative: aircraft N14889 was being pushed back from the gate onto taxi-way "a" at laguardia airport. During push #1 engine was successfully started. During… ## Other aircraft with N14889 - [Cancelled 1956-02-17](https://openairdocs.org/deregistered/N14889-1956-02-17): Howard DGA-11, S/N 201, built 1937. Owner: [Foster Ray M DBA](https://openairdocs.org/faa-owner/FOSTER%20RAY%20M%20DBA), [Hayward, CA](https://openairdocs.org/faa-place/CA/Hayward) --- 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.