# N14890: 1982 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2003-07-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 14, 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: 49114
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 2, 1982
- Certificate issued: March 18, 1999
- Last registry action: March 26, 2002
- Mode S code: A0C414
- Owner when cancelled: [Castle Harbour-I LLC](https://openairdocs.org/faa-owner/CASTLE%20HARBOUR-I%20LLC)
- Location: Hamilton, Bermuda
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N14890
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14890
- Page: https://openairdocs.org/deregistered/N14890-2003-07-14

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 (45)

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

- [SDR CALA0100468](https://openairdocs.org/sdr/CALA0100468), May 17, 2001: MEGAPHONE. INOPERATIVE. THE AFT CABIN MEGAPHONE WAS FOUND INOPERATIVE DURING TEST. THE AFT CABIN MEGAPHONE WAS REMOVED AND REPLACED IAW MM 25-60-00.
- [SDR CALA0000181](https://openairdocs.org/sdr/CALA0000181), Feb 22, 2000: CABLE. OUT OF RIG. THE FORCE REQUIRED TO DROP TAILCONE USING EXTERIOR AND INTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE RIGGED AND DROP CHECK WAS GOOD IAW 
- [SDR CALA0000177](https://openairdocs.org/sdr/CALA0000177), Feb 17, 2000: BELTFRAME. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME AT STA 1380 BETWEEN LONGERONS 4L AND 5L. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.
- [SDR CALA0000176](https://openairdocs.org/sdr/CALA0000176), Feb 17, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 216 BETWEEN LONGERON 14R AND 15R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0000175](https://openairdocs.org/sdr/CALA0000175), Feb 17, 2000: FITTING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN DOOR LOWER AFT STOP AREA INTERNAL FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA0000173](https://openairdocs.org/sdr/CALA0000173), Feb 17, 2000: DOOR JAMB. CRACKED. INSPECTION FOUND TWO 1.5 INCH CRACKS IN MAIN CABIN DOOR JAMB BOX GUSSET AT STA 207, LONGERONS 11L AND 15L. REPAIRS WERE INSTALLED AT EACH LOCATION IAW ECRA 5310
- [SDR CALA0000161](https://openairdocs.org/sdr/CALA0000161), Feb 17, 2000: BELTFRAME. CORRODED. INSPECTION FOUND FORWARD FACE OF BELTFRAME IN AFT BAG BIN CORRODED AT STA 1322, LONGERON 23L TO 29R. THE BELTFRAME WAS REPLACED AND A SPLICE REPAIR WAS INSTALLE
- [SDR CALA0000159](https://openairdocs.org/sdr/CALA0000159), Feb 16, 2000: FLOORBEAM. WORN. INSPECTION FOUND CABIN FLOORBEAM LOWER FLANGE WORN AT STA 1193 IN AFT CARGO COMPARTMENT. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 86.
- [SDR CALA0000157](https://openairdocs.org/sdr/CALA0000157), Feb 14, 2000: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT STAIR DOOR ANGLE AT UPPER HINGE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000156](https://openairdocs.org/sdr/CALA0000156), Feb 14, 2000: CARGO TRACK. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN TIE DOWN RAIL IN AFT BAG BIN AT STA 1271, LT SIDE. THE TIE DOWN RAIL WAS REMOVED AND A NEW TIE DOWN RAIL WAS INSTALLED IAW SR
- [SDR CALA0000155](https://openairdocs.org/sdr/CALA0000155), Feb 14, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RIGHT TIE DOWN RAIL TRACK CORRODED IN MID CARGO COMPARTMENT AT STA 693 TO AFT BULKHEAD. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-3
- [SDR CALA0000154](https://openairdocs.org/sdr/CALA0000154), Feb 14, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND LT TIE DOWN RAIL IN AFT CARGO COMPARTMENT CORRODED. THE TIE DOWN RAIL WAS REPLACED IAW SRM 51-10-3 AND 51-30-0.
- [SDR CALA0000150](https://openairdocs.org/sdr/CALA0000150), Feb 12, 2000: INTERCOSTAL. CORRODED. INSPECTION FOUND UPPER LEFT OF INTERCOSTAL CORRODED UNDER LEFT TIE DOWN RAIL AT STA 1309-1322, L28L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-20-02.
- [SDR CALA0000149](https://openairdocs.org/sdr/CALA0000149), Feb 11, 2000: INTERCOSTAL. CRACKED. INSPECTION FOUND MAIN CABIN DOOR INTERCOSTAL CRACKED BETWEEN NR 4 AND NR 5 BEAMS AFT OF INSIDE DOOR HANDLE. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-
- [SDR CALA0000144](https://openairdocs.org/sdr/CALA0000144), Feb 10, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RT I/B SEAT TRACK CORRODED AT STA 200-280. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-3.
- [SDR CALA9900109](https://openairdocs.org/sdr/CALA9900109), Feb 5, 1999: SUPPORT. BROKEN. THE LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION BOUND FOR EWR. THE GEAR WAS CYCLED TWICE, BUT THE LIGHT WOULD NOT EXTINGUISH. THE FLIGHT 
- [SDR CALA9800445](https://openairdocs.org/sdr/CALA9800445), Mar 14, 1998: ANGLE. CRACKED. INSPECTION FOUND A .375 INCH CRACK IN VERTICAL STABILIZER FORWARD RIGHT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT AB
- [SDR CALA9800224](https://openairdocs.org/sdr/CALA9800224), Feb 12, 1998: BELTFRAME. CRACKED. INSPECTION FOUND A 2 CRACK IN BELTFRAME AT LONGERON 2R AND A 2 CRACK IN BELTFRAME AT LONGERON 2L, STA 1418. A DOUBLER WAS INSTALLED TO ENCOMPASS BOTH CRACKS IAW
- [SDR CALA9800215](https://openairdocs.org/sdr/CALA9800215), Feb 11, 1998: CABLES. OUT OF ADJUST. THE TAILCONE EXTERIOR RELEASE HANDLE PULLED AT 15 POUNDS. THE TAILCONE WAS RIGGED IAW WORK CARD 08-5350-1-0008.
- [SDR CALA9800213](https://openairdocs.org/sdr/CALA9800213), Feb 10, 1998: ANGLE. CRACKED. INSPECTION FOUND VERTICAL FIN INNER ATTACH ANGLE ON RT AND LT SIDES CRACKED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA9800212](https://openairdocs.org/sdr/CALA9800212), Feb 10, 1998: LONGERON. CRACKED. INSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 18.
- [SDR CALA9800205](https://openairdocs.org/sdr/CALA9800205), Feb 10, 1998: SPLICE. CORRODED. INSPECTION FOUND CORROSION ON TIEDOWN RAIL SPLICE AT STA 1220, LONGERON 28L, IN AFT CARGO COMPARTMENT. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AN
- [SDR CALA9800204](https://openairdocs.org/sdr/CALA9800204), Feb 10, 1998: ANGLE. CORRODED. INSPECTION FOUND CORROSION IN LOWER FORWARD CORNER OF AFT CARGO DOOR CUTOUT AT STA 1155. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CALA9800203](https://openairdocs.org/sdr/CALA9800203), Feb 10, 1998: FITTING. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN AFT CABIN DOOR BEAM END FITTING AT LEFT CENTER STOP. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CALA9800188](https://openairdocs.org/sdr/CALA9800188), Feb 5, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1155, LONGERON 30 IN AFT CARGO COMPARTMENT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9800187](https://openairdocs.org/sdr/CALA9800187), Feb 5, 1998: SUPPORT. CORRODED. INSPECTION FOUND CORROSION ON THRESHOLD SUPPORT TEE BETWEEN STA 1155 AND 1174 AT AFT CARGO DOOR CUTOUT. THE THRESHOLD SUPPORT WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9800186](https://openairdocs.org/sdr/CALA9800186), Feb 5, 1998: CLIPS. BROKEN. INSPECTION FOUND AFT FUSELAGE TAIL CONE EXTERIOR RELEASE HANDLE CLIPS BENT AND BROKEN. NEW CLIPS WERE INSTALLED AND TESTED IAW MM 53-53-00.
- [SDR CALA9800185](https://openairdocs.org/sdr/CALA9800185), Feb 4, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1.4 INCH CRACK IN AFT CABIN DOOR ANGLE INSIDE DOOR AT CENTER RIGHT DOOR STOP. THE ANGLE WAS REPLACED IAW SRM 51-30-2.
- [SDR CALA9800003](https://openairdocs.org/sdr/CALA9800003), Jan 6, 1998: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK ABOVE BUMPER PAD IN LT MLG DOOR. THE CRACKED SKIN WAS REMOVED AND REPLACED IAW SRM 52-05.
- [SDR CALA9601171](https://openairdocs.org/sdr/CALA9601171), Aug 15, 1996: APU COMPRESSOR. DAMAGED. THERE WAS A STRONG PUNGENT ODOR IN THE AIRCRAFT CABIN SHORTLY AFTER TAKEOFF. NO ODOR WAS NOTICED DURING CRUISE PORTION OF FLIGHT WITH BOTH PACKS OPERATING. MAIN
- [SDR CAL960620](https://openairdocs.org/sdr/CAL960620), May 17, 1996: DOWNLOCK SENSOR. INOPERATIVE. FLT 1105 - CLE - THE LEFT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION ON APPROACH TO CLE. CYCLING THE GEAR DID NOT HELP. THE GEAR WAS MANUALLY EX
- [SDR CAL960377](https://openairdocs.org/sdr/CAL960377), Feb 14, 1996: BRACKET. CORRODED. MIA - INSPECTION FOUND BRACKET PLATE CORRODED AT INTERSECTION OF FUSELAGE RIGHT CUSP FITTING AND FLOORBEAM, STATION 1338. THE CORRODED PLATE WAS REMOVED AND A N
- [SDR CAL960376](https://openairdocs.org/sdr/CAL960376), Feb 13, 1996: SUPPORT BRACKETS. CRACKED. MIA - INSPECTION FOUND 3 SUPPORT BRACKETS CRACKED AT RT WING FIXED LEADING EDGE INNER RIB. TWENTY INCHES OUTBOARD OF SLAT TRACK NR 2. THE CRACKS WERE 2 INCHES, 
- [SDR CAL960378](https://openairdocs.org/sdr/CAL960378), Feb 12, 1996: FASTENERS. BROKEN. MIA - INSPECTION FOUND TWO FASTENER HEADS POPPED ON RIGHT SIDE OF FUSELAGE AT FS 1000 AND 1005 BETWEEN L18R AND L19R, BELOW CUSP LINE. THE FASTENERS WERE REMOVE
- [SDR CAL960390](https://openairdocs.org/sdr/CAL960390), Feb 11, 1996: SUPPORT. CRACKED. MIA - INSPECTION FOUND A .75 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT, JUST INBOARD OF NR 1 SPOILER ACTUATO
- [SDR CAL960389](https://openairdocs.org/sdr/CAL960389), Feb 11, 1996: SUPPORT. CRACKED. MIA - INSPECTION FOUND A 1 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT, JUST OUTBOARD OF NR 1 SPOILER ACTUATOR
- [SDR CAL960380](https://openairdocs.org/sdr/CAL960380), Feb 11, 1996: ANGLE. CORRODED. MIA - INSPECTION FOUND THREE FLOOR SUPPORT 'Z' ANGLES CORRODED UNDER FLOORBOARD AT FORWARD ENTRY DOOR SILL AREA. THE FLOOR SUPPORT ANGLES WERE REMOVED AND REPLA
- [SDR CAL960379](https://openairdocs.org/sdr/CAL960379), Feb 11, 1996: WEB. CORRODED. MIA - INSPECTION FOUND HORIZONTAL WEB CORRODED AT THRESHOLD OF FORWARD ENTRY DOOR, 4 INCHES INBOARD OF AFT CORNER OF CUTOUT. THE CORROSION WAS REMOVED IAW SRM 5
- [SDR CAL960388](https://openairdocs.org/sdr/CAL960388), Feb 9, 1996: SUPPORT. CRACKED. MIA - INSPECTION FOUND A .6250 INCH CRACK IN FUSELAGE FAIRING SUPPORT ANGLE AT FS 807 BETWEEN LONGERON 25L AND LONGERON 26L. (X)
- [SDR CAL960381](https://openairdocs.org/sdr/CAL960381), Feb 9, 1996: ANGLE. CRACKED. MIA - INSPECTION FOUND A .5625 INCH CRACK IN FUSELAGE FAIRING SUPPORT ANGLE AT FS 807, BETWEEN L26R AND L27R. THE CRACK WAS STOP DRILLED. REPAIR ANGLES WERE FAB
- [SDR CAL951033](https://openairdocs.org/sdr/CAL951033), Nov 12, 1995: GEAR HANDLE. BINDING. EWR - FLT 0609 - ALL THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHTS EXTINGUISHED. MAINTENANCE CLEANED A
- [SDR CAL950723](https://openairdocs.org/sdr/CAL950723), Aug 17, 1995: FIRE LOOP. INOPERATIVE. FLT NR 0114 - IAH - THE NR 1 ENGINE LOOP 'A' AND FIRE DETECT LOOP LIGHT ILLUMINATED WHILE ON DESCENT INTO IAH AT 15,000 FEET. 'ABNORMAL' PROCEDURES WERE COMPLIE
- [SDR CAL950151](https://openairdocs.org/sdr/CAL950151), Feb 24, 1995: SWITCH. FAILED. FLT NR 0132 - EWR - ALL THREE GEAR INDICATORS REMAINED RED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND ONLY THE NOSE GEAR LIGHT AND DOOR LIGHT REMAINED ON. T
- [SDR CAL950015](https://openairdocs.org/sdr/CAL950015), Jan 7, 1995: GRD SHIFT MECH. FROZEN. FLT NR 0262 - CLE - THE THREE GEAR RED UNSAFE LIGHTS AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED LEAVING CLE. THE GEAR WAS EXTENDED A
- [SDR CAL950003](https://openairdocs.org/sdr/CAL950003), Jan 3, 1995: DUCT. BLOWN. SAT - FLT 0437 - A STRONG BURNING ODOR WAS OBSERVED IN THE COCKPIT AND CABIN ON FINAL APPROACH TO SAT WITH THE ICE PROTECTION ON. THE AIRCRAFT LANDED WITHOUT 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 20001224023969I](https://openairdocs.org/incident/20001224023969I), Dec 24, 2000: Doug DC982 (N14890), Tampa, FL, Minor damage. (-23) On December 24, 2000 at 2225 EST, a mc donnell Douglas DC-9-82 a/c, N14890, operated by Continental airlines, flight 1663, from Tampa International…

## Other aircraft with N14890

- [Cancelled 2014-02-19](https://openairdocs.org/deregistered/N14890-2014-02-19): Cessna 182T, S/N 18281902. Exported to Australia. Owner: [Joffrion Patrick H](https://openairdocs.org/faa-owner/JOFFRION%20PATRICK%20H), [Orange Beach, AL](https://openairdocs.org/faa-place/AL/Orange%20Beach)

---
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.