# N35888: 1982 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2003-05-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 12, 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: 49117 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 3, 1982 - Certificate issued: March 18, 1999 - Last registry action: March 26, 2002 - Mode S code: A40616 - 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/N35888 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=35888 - Page: https://openairdocs.org/deregistered/N35888-2003-05-12 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 (119, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0001634](https://openairdocs.org/sdr/CALA0001634), Oct 23, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO LT TIE DOWN TRACK CORRODED UNDER CLIP NUTS AT FS 1230 - 1322. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51 - [SDR CALA0001633](https://openairdocs.org/sdr/CALA0001633), Oct 23, 2000: DOUBLER. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN DOUBLER AT RT WHEEL WELL FORWARD LOWER CORNER. REMOVED INTERCOSTAL AND DOUBLER AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-04 - [SDR CALA0001632](https://openairdocs.org/sdr/CALA0001632), Oct 23, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND FORWARD CARGO AFT RT TIE DOWN TRACK HAD CORRODED SCREW HOLES ON TOP AND BOTTOM. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51- - [SDR CALA0001631](https://openairdocs.org/sdr/CALA0001631), Oct 23, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO RT SIDE TIE DOWN TRACK CORRODED BETWEEN FS 1212 - 1322. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4 A - [SDR CALA0001619](https://openairdocs.org/sdr/CALA0001619), Oct 21, 2000: SKIN. GOUGED. INSPECTION FOUND RT AFT EMERGENCY EXIT DOOR CUTOUT SKIN GOUGED AT UPPER DOOR LATCH. THE RIVETS WERE REMOVED IAW SRM 51-30-2. THE SEAL DEPRESSOR WAS CUT IAW SRM - [SDR CALA0001618](https://openairdocs.org/sdr/CALA0001618), Oct 21, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND LT TIE DOWN TRACK IN AFT CARGO AREA CORRODED BETWEEN FS 1007 AND 1320. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4G. - [SDR CALA0001617](https://openairdocs.org/sdr/CALA0001617), Oct 21, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT RT END OF TRACK TO AFT BULKHEAD FRAME IN FWD CARGO PIT CORRODED AT STA 522. THE TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED - [SDR CALA0001600](https://openairdocs.org/sdr/CALA0001600), Oct 18, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED BETWEEN FS 160 AND 200, RBL 39. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10- - [SDR CALA0001599](https://openairdocs.org/sdr/CALA0001599), Oct 18, 2000: SUPPORT BRACKET. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN CENTER KEEL SUPPORT AT STA 948. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-01 AND 53-01. - [SDR CALA0001598](https://openairdocs.org/sdr/CALA0001598), Oct 18, 2000: ANGLE. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN ANGLE JUST FORWARD OF RUDDER TRIM ACTUATOR IN TAIL COMPARTMENT AREA AT STA 1485, RT SIDE. THE VENT BOX WAS REMOVED IAW SRM 51 - [SDR CALA0001595](https://openairdocs.org/sdr/CALA0001595), Oct 17, 2000: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL AND ATTACHING BRACKETS CORRODED IN AFT CARGO AREA BETWEEN FS 1148 - 1155, LONGERONS 29R AND 30. THE INTERCOSTAL AND BRACKETS WERE R - [SDR CALA0001594](https://openairdocs.org/sdr/CALA0001594), Oct 17, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 180, LBL 12 - 37. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30- - [SDR CALA0001593](https://openairdocs.org/sdr/CALA0001593), Oct 17, 2000: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT AFT END LOWER SIDE OF AFT ACCESSORY COMPARTMENT INTERCOSTAL BETWEEN FS 1497 AND 1510. THE INTERCOSTAL WAS REMOVED AND REPLACE - [SDR CALA0001592](https://openairdocs.org/sdr/CALA0001592), Oct 17, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FORWARD ENTRY FLOOR SUPPORT CORRODED BETWEEN FS 160 AND 190, LBL 40. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED - [SDR CALA0001589](https://openairdocs.org/sdr/CALA0001589), Oct 16, 2000: FLOORBEAM. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT FS 218, LBL 44. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW 53-05, FIGURE A AND 51-30-2. - [SDR CALA0001585](https://openairdocs.org/sdr/CALA0001585), Oct 15, 2000: PAN. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED BETWEEN FS 370 AND 427. THE DOOR PAN WAS REPLACED IAW SRM 51-30-2. THE OUTSIDE LOWER SCUFF PLATE WAS REPLA - [SDR CALA0001584](https://openairdocs.org/sdr/CALA0001584), Oct 15, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT CARGO TIEDOWN TRACK CORRODED IN AFT CARGO AREA AT FS 1007 - 1155. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-04, FIGURE - [SDR CALA0001583](https://openairdocs.org/sdr/CALA0001583), Oct 15, 2000: INTERCOSTAL. CORRODED. INSPECTION FOUND AFT CARGO CHANNEL INTERCOSTAL CORRODED ON DOOR JAMB. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2 AND 51-30- - [SDR CALA0001582](https://openairdocs.org/sdr/CALA0001582), Oct 15, 2000: SUPPORT BRACKET. CORRODED. INSPECTION FOUND LOWER BULKHEAD SUPPORT CORRODED IN AFT CARGO AREA AT FS 1322. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30 - [SDR CALA0001581](https://openairdocs.org/sdr/CALA0001581), Oct 15, 2000: INTERCOSTAL. GOUGED. INSPECTION FOUND A GOUGE IN RADIUS OF INTERCOSTAL AND CORROSION WAS NOTED BETWEEN FASTENERS ON LOWER ANGLE MATING SKIN AT FS 430 - 446, L28R. THE INTERCOSTAL WA - [SDR CALA0001577](https://openairdocs.org/sdr/CALA0001577), Oct 14, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT CARGO FLOOR SUPPORT CORRODED AT FS 1117 - 1155 BETWEEN L28L AND L28R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED I - [SDR CALA0001576](https://openairdocs.org/sdr/CALA0001576), Oct 14, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180, RBL 9 TO RBL 38. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-1 - [SDR CALA0001568](https://openairdocs.org/sdr/CALA0001568), Oct 13, 2000: FINGER DOUBLER. CORRODED. INSPECTION FOUND SKIN FINGER DOUBLER CORRODED AT FS 256, LONGERON 26L. THE FINGER DOUBLER WAS REMOVED AND A NEW FINGER DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND - [SDR CALA0001567](https://openairdocs.org/sdr/CALA0001567), Oct 13, 2000: ANGLE. CORRODED. INSPECTION FOUND MID CARGO RT TRACK FLOOR SUPPORT Z-ANGLE CORRODED AT FS 586 - 636. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-01, FIGURE 1. - [SDR CALA0001566](https://openairdocs.org/sdr/CALA0001566), Oct 13, 2000: PLATE. CORRODED. INSPECTION FOUND AFT CARGO CENTER THRESHOLD PLATE CORRODED AT STA 1231. THE THRESHOLD PLATE REMOVED AND REPLACED IAW SRM 51-10-3. - [SDR CALA0001565](https://openairdocs.org/sdr/CALA0001565), Oct 13, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND R-1 DOOR ENTRY FLOOR SUPPORT CORRODED AT FS 155 - 200. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1. - [SDR CALA0001564](https://openairdocs.org/sdr/CALA0001564), Oct 13, 2000: INTERCOSTAL. CRACKED. INSPECTION FOUND AN 8 INCH CRACK IN INTERCOSTAL AT SUB FLOOR INSIDE L-1 DOOR, FS 190, LBL 56. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30 - [SDR CALA0001563](https://openairdocs.org/sdr/CALA0001563), Oct 13, 2000: WEB. CRACKED. INSPECTION FOUND A 19 INCH CRACK IN CABIN RT CUSP WEB AT FS 218 - 237, RBL 44 - 54. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0001562](https://openairdocs.org/sdr/CALA0001562), Oct 13, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID PIT LT TIE DOWN TRACK CORRODED AT FASTENER HOLES FROM FS 541 - 790. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW 51-30- - [SDR CALA0001561](https://openairdocs.org/sdr/CALA0001561), Oct 13, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 200, RBL 4 TO LBL 4, LBL 8, AND RBL 10 TO 40. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALL - [SDR CALA0001560](https://openairdocs.org/sdr/CALA0001560), Oct 13, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT I/B CABIN SEAT TRACK CORRODED AT FS 200 - 265. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1. - [SDR CALA0001558](https://openairdocs.org/sdr/CALA0001558), Oct 12, 2000: SUPPORT FITTING. CORRODED. INSPECTION FOUND AFT CARGO BULKHEAD CENTER VERTICAL SUPPORT CORRODED AT FS 1322. THE VERTICAL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0001557](https://openairdocs.org/sdr/CALA0001557), Oct 12, 2000: HINGE. CORRODED. INSPECTION FOUND AFT LAV SERVICE PANEL ACCESS DOOR HINGE AND BRACKET CORRODED. THE DOOR HINGE AND BRACKET WERE REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-1, AN - [SDR CALA0001556](https://openairdocs.org/sdr/CALA0001556), Oct 12, 2000: FITTING. CORRODED. INSPECTION FOUND AFT CARGO SUPPORT FITTING CORRODED AT FS 1007, LONGERON 28R. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0001555](https://openairdocs.org/sdr/CALA0001555), Oct 12, 2000: FLOOR PANEL. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FIRST OFFICER''S SEAT LOWER FLOOR PANEL. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-4. - [SDR CALA0001554](https://openairdocs.org/sdr/CALA0001554), Oct 12, 2000: GALLEY TRACK. CORRODED. INSPECTION FOUND G-2 GALLEY SUPPORT CORRODED AT FS 218, RBL 11. THE GALLEY SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0001553](https://openairdocs.org/sdr/CALA0001553), Oct 12, 2000: RIB. CORRODED. INSPECTION FOUND FUSELAGE FAIRING MOUNTING RIB 5L CORRODED AT BOTTOM LOCATION FS 826, LONGERON 29L. DOUBLERS AND SHIM WERE INSTALLED IAW SRM 53-01, FIGURE 2. - [SDR CALA0001549](https://openairdocs.org/sdr/CALA0001549), Oct 12, 2000: SKIN. CRACKED. INSPECTION FOUND TWO CRACKS IN DOUBLER AROUND DOOR HANDLE OF FWD CARGO DOOR OUTER SKIN. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-3 - [SDR CALA0001548](https://openairdocs.org/sdr/CALA0001548), Oct 12, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN FS 1271 AND 1289 AT LONGERON 27L. THE DENT WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 5 - [SDR CALA0001537](https://openairdocs.org/sdr/CALA0001537), Oct 10, 2000: WEB. CORRODED. INSPECTION FOUND CORROSION UNDER AND ON FORWARD TORQUE BOX STRAP AND WEB AT FS 1155 - 1212. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51- - [SDR CALA0001536](https://openairdocs.org/sdr/CALA0001536), Oct 10, 2000: BEAM. CORRODED. INSPECTION FOUND LOWER HALF OF AFT CARGO DOOR JAMB BEAM CORRODED ON BOTH SIDES AT FS 1155 - 1212. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51 - [SDR CALA0001535](https://openairdocs.org/sdr/CALA0001535), Oct 10, 2000: WEB. CORRODED. INSPECTION FOUND WEB CORRODED AT FS 200, RBL 13, AFT OF FLOORBEAM. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED USING A SPLICE IAW SRM 51-10-2 AND 51-30-2. - [SDR CALA0001534](https://openairdocs.org/sdr/CALA0001534), Oct 10, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1030 - 1309. FLOOR PANELS WERE REMOVED TO GAIN ACCESS. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-0 - [SDR CALA0001533](https://openairdocs.org/sdr/CALA0001533), Oct 10, 2000: CHANNEL. CORRODED. INSPECTION FOUND ON O/B END OF INSIDE CHANNEL OF THE L-1 DOOR JAMB STRIP. THE CHANNEL WAS REPLACED IAW SRM 51-30-2 AND 51-10-3. - [SDR CALA0001532](https://openairdocs.org/sdr/CALA0001532), Oct 10, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 160, RBL 7 TO LBL 7. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53- - [SDR CALA0001531](https://openairdocs.org/sdr/CALA0001531), Oct 10, 2000: STRAP. CORRODED. INSPECTION FOUND STRAP CORRODED IN AFT PIT AT STA 1184 BETWEEN LONGERONS 29R AND 30. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 53-34-0, 51-10- - [SDR CALA0001528](https://openairdocs.org/sdr/CALA0001528), Oct 10, 2000: WEB. CORRODED. INSPECTION FOUND G-2 GALLEY SUPPORT CUSP WEB CORRODED AT FS 218, RBL 11. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001527](https://openairdocs.org/sdr/CALA0001527), Oct 10, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 200 - 237. THE SEAT TRACK WAS REMOVED AND REPLACED IAW 53-05, FIGURE 4A. - [SDR CALA0001520](https://openairdocs.org/sdr/CALA0001520), Oct 8, 2000: BRACKET. CORRODED. INSPECTION FOUND AFT CARGO TORQUE BOX CHANNEL BRACKET CORRODED IN DOOR JAMB AREA. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-10-4, AND 51-10-3. - [SDR CALA0001519](https://openairdocs.org/sdr/CALA0001519), Oct 8, 2000: INTERCOSTAL. CORRODED. INSPECTION FOUND AFT CARGO T-INTERCOSTAL CORRODED AROUND CLIPNUT HOLES IN DOOR JAMB AREA. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-10-4, AND All 119: https://openairdocs.org/deregistered/N35888-2003-05-12/reports.md ## Other aircraft with N35888 - [Cancelled 1945-10-12](https://openairdocs.org/deregistered/N35888-1945-10-12): Piper J4E, S/N 1421, built 1941. Owner: [Beard Robert D](https://openairdocs.org/faa-owner/BEARD%20ROBERT%20D), [Fort Wayne, IN](https://openairdocs.org/faa-place/IN/Fort%20Wayne) --- 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.