# N16887: 1982 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2003-05-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 22, 2003 - 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: 49116 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 21, 1982 - Certificate issued: March 18, 1999 - Last registry action: May 9, 2003 - Mode S code: A112F6 - 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/N16887 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16887 - Page: https://openairdocs.org/deregistered/N16887-2003-05-22 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 (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100538](https://openairdocs.org/sdr/CALA0100538), Jun 12, 2001: BATTERY. DISCHARGED. INSPECTION FOUND AFT CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA0001374](https://openairdocs.org/sdr/CALA0001374), Sep 3, 2000: BATTERY PACK. INOPERATIVE. INSPECTION FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00. - [SDR CALA0001293](https://openairdocs.org/sdr/CALA0001293), Aug 21, 2000: ANGLE. CORRODED. INSPECTION FOUND L-ANGLE CORRODED UNDER EXISTING DOUBLER AT CANTED BULKHEAD STA 1463, L16R. A NEW ANGLE SECTION WAS INSTALLED IAW SRM 53-03, FIGURE 27. - [SDR ALA0001292](https://openairdocs.org/sdr/ALA0001292), Aug 21, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT NUT PLATE MOUNT AREA, STA 1338 BELOW LT AFT LAV. A SPLICE SECTION WAS INSTALLED IAW SRM 51-30-0 AND 51-10-3. - [SDR CALA0001274](https://openairdocs.org/sdr/CALA0001274), Aug 18, 2000: ATTACH ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1486, L3R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IA - [SDR CALA0001271](https://openairdocs.org/sdr/CALA0001271), Aug 16, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 237 BETWEEN LONGERON 17L AND 18L. THE SKIN SECTION WAS REPLACED IAW ECRA 5330-02445. - [SDR CALA0001270](https://openairdocs.org/sdr/CALA0001270), Aug 16, 2000: WEB. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN WEB AT CANTED BULKHEAD STA 1463, LONGERON 17R. THE CRACKED SECTION OF WEB WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW - [SDR CALA0001269](https://openairdocs.org/sdr/CALA0001269), Aug 16, 2000: PAN. CHAFED. INSPECTION FOUND MAIN BAGGAGE BIN DOOR PAN CHAFED AT FORWARD EDGE OF NR 1 STOP PAD. REPAIRED IAW ECRA 5230-01540. - [SDR CALA0001268](https://openairdocs.org/sdr/CALA0001268), Aug 16, 2000: PAN. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN MAIN BAGGAGE BIN DOOR PAN UNDER NR 4 STOP PAD BRACKET AT AFT EDGE OF DOOR. REPAIRED IAW SRM 52-05, FIGURE 26A AND 50. - [SDR CALA0001267](https://openairdocs.org/sdr/CALA0001267), Aug 15, 2000: FLOORBEAM. WORN. INSPECTION FOUND CABIN FLOORBEAM WORN AT RT CENTER OF FORWARD CARGO BEAM, STA 389. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 86. - [SDR CALA0001265](https://openairdocs.org/sdr/CALA0001265), Aug 14, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AFT OF THE L-1 DOOR AND APPROXIMATELY 8 INCHES ABOVE FORWARD LAV SERVICE PANEL AT STA 226, LONGERON 17L-18L. INSPECTION FO - [SDR CALA0001264](https://openairdocs.org/sdr/CALA0001264), Aug 14, 2000: FITTING. CORRODED. INSPECTION FOUND LT SIDEWALL LOWER ATTACH FITTING CORRODED AT STA 200. A NEW FITTING WAS INSTALLED IAW SRM 51-30. - [SDR CALA0001245](https://openairdocs.org/sdr/CALA0001245), Aug 8, 2000: ANGLE. CORRODED. INSPECTION FOUND MAIN BAGGAGE BIN DOOR JAMB Z-ANGLE CORRODED AT I/B SIDE AROUND HI-SHEARS. THE CORROSION ON DOOR FRAME Z-ANGLE WAS REMOVED AND A REPAIR WAS INST - [SDR CALA0001244](https://openairdocs.org/sdr/CALA0001244), Aug 8, 2000: WEB. CORRODED. INSPECTION FOUND LT CUSP MEMBRANE CORRODED AT STA 200 JUST AFT OF MCD CUTOUT AT LOWER SIDE. THE CUSP MEMBRANE WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND ECRA - [SDR CALA0001232](https://openairdocs.org/sdr/CALA0001232), Aug 4, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 236. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F. - [SDR CALA9901511](https://openairdocs.org/sdr/CALA9901511), Nov 18, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS ABOVE BOTH LEFT AND RIGHT DOORS INOPERATIVE DURING EMERGENCY LIGHT TEST. THE POWER SUPPLY BATTERY PACK W - [SDR CALA9900214](https://openairdocs.org/sdr/CALA9900214), Mar 5, 1999: STRUT. REQD SERVICE. THE LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE NLG STRUT FLAT. A - [SDR CALA9801212](https://openairdocs.org/sdr/CALA9801212), Jul 6, 1998: PINS. WORN. THE FORCE REQUIRED TO RELEASE TAILCONE USING EXTERIOR HANDLE WAS BELOW LIMITS. WORN ALIGNMENT PINS AND RECEPTACLES WERE REPLACED AND LATCHES WERE ADJUSTED IAW M - [SDR CALA9801211](https://openairdocs.org/sdr/CALA9801211), Jul 2, 1998: WEB. CORRODED. INSPECTION FOUND WEB CORRODED AT STA 1212 AFT OF DOOR INBOARD OF LONGERON 27R. A REPAIR WAS INSTALLED IAW ECRA 5310-03742. - [SDR CALA9801186](https://openairdocs.org/sdr/CALA9801186), Jun 30, 1998: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN MAIN CABIN DOOR SKIN WITH DEEP WEAR MARKS ON HOLD OPEN HOOK PAN ON DOOR. A REPAIR DOUBLER WAS INSTALLED AND THE PAN WAS REP - [SDR CALA9801185](https://openairdocs.org/sdr/CALA9801185), Jun 29, 1998: SPACER. CORRODED. INSPECTION FOUND CORROSION ON AFT BAGGAGE BIN Z-ANGLE REPAIR SPACER AT STA 1155 TO 1212. THE REPAIR SPACER WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA9801184](https://openairdocs.org/sdr/CALA9801184), Jun 29, 1998: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT EXTERNAL HANDLE RECESS CUP OF MAIN CABIN DOOR INTERCOSTAL. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9801182](https://openairdocs.org/sdr/CALA9801182), Jun 26, 1998: BEAM. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF MAIN CABIN DOOR NR 1 HORIZONTAL BEAM FORWARD END. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31. - [SDR CALA9801176](https://openairdocs.org/sdr/CALA9801176), Jun 26, 1998: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF FORWARD GALLEY SERVICE DOOR NR 4 BEAM. THE NR 4 BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9601340](https://openairdocs.org/sdr/CALA9601340), Sep 29, 1996: FUEL CONTROL. LEAKING. A STRONG FUEL SMELL WAS NOTICED IN THE COCKPIT AND CABIN WHILE DESCENDING INTO CLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LEAKING FROM AP - [SDR CALA9601102](https://openairdocs.org/sdr/CALA9601102), Jul 25, 1996: CLIPS. OUT OF ADJUST. THE FORCE REQUIRED TO PULL INTERIOR AND EXTERIOR TAILCONE RELEASE HANDLES OUT OF CLIPS WAS EXCESSIVE. THE CLIPS WERE ADJUSTED IAW MM 53-53-00. - [SDR CALA9601094](https://openairdocs.org/sdr/CALA9601094), Jul 17, 1996: HAT SECTION. CORRODED. INSPECTION FOUND HAT SECTION CORRODED AROUND NUTPLATE HOLE BETWEEN PANEL J AND H AT FORWARD ENTRY. THE HAT SECTION WAS REMOVED AND A NEW HAT SECTION WAS INSTALL - [SDR CALA9601097](https://openairdocs.org/sdr/CALA9601097), Jul 12, 1996: SUB FLOOR. CORRODED. INSPECTION FOUND BOTTOM OF SUB-FLOOR CORRODED OUTBOARD OF LEFT OUTBOARD SEAT TRACK AT STA 1136-1274. THE SUB-FLOOR WAS REPLACED IAW SRM 51-30-02. - [SDR CALA9601099](https://openairdocs.org/sdr/CALA9601099), Jul 11, 1996: CHANNEL. CRACKED. INSPECTION FOUND Z-CHANNEL CRACKED AT STA 69. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, PAGE 9 AND SRM 51-30-5. - [SDR CALA9601095](https://openairdocs.org/sdr/CALA9601095), Jul 11, 1996: INTERCOSTAL. CRACKED. INSPECTION FOUND FIVE 1 INCH CRACKS IN INTERCOSTAL IN AFT BAGGAGE BIN AT STA 1309. THE CRACKS WERE STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGUR - [SDR CALA9601096](https://openairdocs.org/sdr/CALA9601096), Jul 10, 1996: INTERCOSTAL. CRACKED. INSPECTION FOUND A 10 INCH CRACK IN FORWARD BAGGAGE BIN INTERCOSTAL AT VHF ANTENNA MOUNT BETWEEN STA 465 AND STA 484. THE INTERCOSTAL WAS REMOVED AND A NEW ONE - [SDR CALA9601101](https://openairdocs.org/sdr/CALA9601101), Jul 9, 1996: LATCHES. OUT OF ADJUST. THE FORCE REQUIRED TO DROP TAILCONE USING THE INTERIOR RELEASE HANDLE AND AFT ENTRANCE DOOR RELEASE HANDLE WAS EXCESSIVE. THE TAILCONE LATCHES WERE ADJUSTED IAW - [SDR CALA9601100](https://openairdocs.org/sdr/CALA9601100), Jul 8, 1996: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED FORWARD OF PITOT TUBES. THE DENTED SECTION OF SKIN WAS REPLACED IAW SRM 51-30-2 AND SRM 51-30-5. - [SDR CALA9601098](https://openairdocs.org/sdr/CALA9601098), Jul 8, 1996: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN LONGERON 21R AND 22R AT STA 165. THE DENT WAS COLD-FORMED AND DYE CHECKED WITH NO CRACKS FOUND. AN INTERNAL DOUBLE - [SDR CALA9600770](https://openairdocs.org/sdr/CALA9600770), Jun 8, 1996: HYD LINE. LEAKING. THE RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO WHILE EN ROUTE. EMERGENCY GEAR EXTENSION WAS USED PRIOR TO LANDING. THE LT MLG DOOR WAS DAMAGED - [SDR CAL960542](https://openairdocs.org/sdr/CAL960542), Apr 27, 1996: OIL TANK VENT. CLOGGED. FLT NR 279 - EWR - PRIOR TO PUSH BACK CABIN BEGAN TO FILL WITH SMOKE. DURING T/S FOUND OIL LEAKED ON COALESCER BAGS DUE TO APU OIL TANK BEING OVERSERVICED. REMO ## Other aircraft with N16887 - [Cancelled 2008-06-03](https://openairdocs.org/deregistered/N16887-2008-06-03): Cessna 172S, S/N 172S10614, built 2007. Exported to Austria. Owner: [Atlantic Ferry Services Inc](https://openairdocs.org/faa-owner/ATLANTIC%20FERRY%20SERVICES%20INC), [Waterloo, IA](https://openairdocs.org/faa-place/IA/Waterloo) - [Cancelled 1979-05-09](https://openairdocs.org/deregistered/N16887-1979-05-09): Bell 206B, S/N 2332. Exported to Canada. Owner: [Bell Helicopter Textron](https://openairdocs.org/faa-owner/BELL%20HELICOPTER%20TEXTRON), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth) --- 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.