# N72825: 1986 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-07-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 14, 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: [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: 49485 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 5, 1986 - Certificate issued: April 4, 2005 - Last registry action: April 4, 2005 - Mode S code: A9C400 - 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/N72825 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=72825 - Page: https://openairdocs.org/deregistered/N72825-2005-07-14 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 (82, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0400482](https://openairdocs.org/sdr/CALA0400482), May 8, 2004: FITTING. CORRODED. INSPECTION FOUND FITTING AT AFT LOWER CORNER OF AFT BAGGAGE BIN DOOR CUTOUT CORRODED. A NEW FITTING WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0400165](https://openairdocs.org/sdr/CALA0400165), Feb 24, 2004: WIRE. SHORTED. MACH TRIM INOP LIGHT ILLUMINATED AND AIRCRAFT BEGAN TO DUTCH ROLL AT 31,000 FEET EN ROUTE. QRH PROCEDURE COMPLETED, BUT NO CHANGE RESULTED. THERE WAS MINIMUM CO - [SDR CALA0300021](https://openairdocs.org/sdr/CALA0300021), Jan 30, 2003: LONGERON. CRACKED. INSPECTION FOUND A 1/2" CRACK IN LONGERON 2R AT STA 1418. A SPLICE REPAIR WAS INSTALLED IAW ECRA 5311-01132. - [SDR CALA0200485](https://openairdocs.org/sdr/CALA0200485), Oct 3, 2002: FIRE DETECTOR. MALFUNCTIONED. THE MID CARGO DET "B" CARGO DETECTION AND SUPRESSION LIGHT ILLUMINATED WHILE AT CRUISE ENROUTE FROM IAH TO ORD. SHORTLY AFTERWARDS THE MASTER WARNING AND CARGO - [SDR CALA0200015](https://openairdocs.org/sdr/CALA0200015), Jan 11, 2002: BRACKET. CRACKED. INSPECTION FOUND A 1/2" CRACK IN VERTICAL STABILIZER R/H SIDE SUPPORT BRACKET FOR UPPER FAIRING ABOVE JACKSCREW. A DOUBLER WAS INSTALLED ON THE SUPPORT BRACKET - [SDR CALA0200007](https://openairdocs.org/sdr/CALA0200007), Jan 9, 2002: HINGE. CORRODED. INSPECTION FOUND LEFT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238. - [SDR CALA0200006](https://openairdocs.org/sdr/CALA0200006), Jan 9, 2002: HINGE. CORRODED. INSPECTION FOUND RIGHT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238. - [SDR CALA0100495](https://openairdocs.org/sdr/CALA0100495), May 23, 2001: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN RT VERTICAL STABILIZER LOWER ATTACH ANGLE, 6 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05. - [SDR CALA0100494](https://openairdocs.org/sdr/CALA0100494), May 23, 2001: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LT VERTICAL STABILIZER LOWER ATTACH ANGLE, 7 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05. - [SDR CALA0001243](https://openairdocs.org/sdr/CALA0001243), Aug 7, 2000: DOUBLER. CORRODED. INSPECTION FOUND AFT CARGO THRESHOLD EXTERNAL DOUBLER CORRODED AT FS 1160 - 1205, LONGERON 28R. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM - [SDR CALA0001242](https://openairdocs.org/sdr/CALA0001242), Aug 7, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND CARGO TIE DOWN TRACK CORRODED AT FS 1212 - 1220, LONGERON 28R. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-2, AN - [SDR CALA0001241](https://openairdocs.org/sdr/CALA0001241), Aug 7, 2000: STRAP. CORRODED. INSPECTION FOUND AFT LOWER CORNER STRAP OF AFT CARGO DOOR FRAME CORRODED AT STA 1212, L28R. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-2, - [SDR CALA0001240](https://openairdocs.org/sdr/CALA0001240), Aug 7, 2000: WEB. CORRODED. INSPECTION FOUND AFT PIT TORQUE BOX UPPER WEB CORRODED UNDER CARGO TIE DOWN TRACK AT FS 1212 - 1218 ABOVE LONGERON 28R. THE WEB WAS REMOVED AND A NEW SECTION WA - [SDR CALA0001239](https://openairdocs.org/sdr/CALA0001239), Aug 7, 2000: WEB. CRACKED. INSPECTION FOUND A .5 INCH CRACK ON AFT SIDE OF UPPER WEB IN AFT PIT AT STA 1212, RT SIDE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-24-0, FIGU - [SDR CALA0001238](https://openairdocs.org/sdr/CALA0001238), Aug 7, 2000: LONGERON. CORRODED. INSPECTION FOUND LONGERON 30 CORRODED AT STA 590 - 779. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-4, 51-30-2. THE EXISTING DOUBLER, WATER DRA - [SDR CALA0001237](https://openairdocs.org/sdr/CALA0001237), Aug 7, 2000: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT THREAD SUPPORT ANGLE AT FIFTH STEP FROM BOTTOM OF VENTRAL STAIRS. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 5 - [SDR CALA0001228](https://openairdocs.org/sdr/CALA0001228), Aug 6, 2000: WEB. CRACKED. INSPECTION FOUND LT CUSP WEB CRACKED O/B OF SEAT TRACK AT STA 1174 - 1304, LBL 54. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND - [SDR CALA0001227](https://openairdocs.org/sdr/CALA0001227), Aug 6, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1174 - 1309. THE SEAT TRACK AND FITTING WERE REMOVED AND A NEW TRACK AND FITTING WERE INSTALLED IAW SRM 51- - [SDR CALA0001226](https://openairdocs.org/sdr/CALA0001226), Aug 6, 2000: PAN. CORRODED. INSPECTION FOUND CORROSION AROUND FASTENERS OF FORWARD CARGO DOOR LOWER JAMB PAN. THE CORRODED AREA WAS CUT OUT AND A NEW PAN AND SPLICES WERE INSTALLED IAW SRM - [SDR CALA0001225](https://openairdocs.org/sdr/CALA0001225), Aug 6, 2000: PAN. CRACKED. INSPECTION FOUND THREE RIVET NUTS CRACKED AT FORWARD CARGO DOOR PAN FORWARD LOWER CORNER. THE CRACKS WERE 0.05 INCH LONG. THE CARGO DOOR PAN SECTION WAS REMOVED - [SDR CALA0001224](https://openairdocs.org/sdr/CALA0001224), Aug 6, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT CARGO TIE DOWN TRACK CORRODED AT STA 522 - 636, L28R. THE TIE DOWN TRACK WAS REMOVED AND A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 51-30-2, - [SDR CALA0001223](https://openairdocs.org/sdr/CALA0001223), Aug 6, 2000: ANGLE. CORRODED. INSPECTION FOUND RT FLOOR PANEL TRANSITION ANGLE CORRODED AT FS 598 - 636. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51- - [SDR CALA0001222](https://openairdocs.org/sdr/CALA0001222), Aug 6, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT CARGO TRACK CORRODED ON UPPER AND LOWER SURFACES IN FORWARD CARGO PIT AT FS 427 - 522. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2 AND 53-0 - [SDR CALA0001221](https://openairdocs.org/sdr/CALA0001221), Aug 6, 2000: SKIN. DENTED. INSPECTION FOUND FORWARD SKIN OF AFT CARGO DOOR DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 3. A DOUBLER, FILLER, AND SHIMS WERE INSTALLED IAW SRM - [SDR CALA0001220](https://openairdocs.org/sdr/CALA0001220), Aug 6, 2000: STOP. GOUGED. INSPECTION FOUND AFT CARGO DOOR STOPS GOUGED. REPAIRED IAW ECRA 5330-02819. - [SDR CALA0001219](https://openairdocs.org/sdr/CALA0001219), Aug 6, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND FORWARD CARGO PIT LT CARGO TRACK CORRODED ON UPPER AND LOWER SURFACES OF CLIP NUT FLANGES AT FS 370 - 522. THE CARGO TRACK WAS REMOVED AND A NE - [SDR CALA0001218](https://openairdocs.org/sdr/CALA0001218), Aug 6, 2000: FLOOR PANEL. CORRODED. INSPECTION FOUND AFT PIT FLOOR PANEL CORRODED AT FS 1212 - 1230. THE FLOOR PANEL WAS REMOVED AND A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-20, FIGURE 11, 51-10 - [SDR CALA0001217](https://openairdocs.org/sdr/CALA0001217), Aug 6, 2000: INTERCOSTAL. CORRODED. INSPECTION FOUND RT INTERCOSTAL CORRODED AT FS 1292 - 1309. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-50-2, 51-10-4, 51-30-2, A - [SDR CALA0001216](https://openairdocs.org/sdr/CALA0001216), Aug 6, 2000: FAIRING. CHAFED. INSPECTION FOUND UPPER RT HORIZONTAL STABILIZER FAIRING CRACKED AT FORWARD UPPER END AND CHAFING IN THREE AREAS AT FORWARD UPPER END AND DELAMINATION NEAR CENTE - [SDR CALA0001215](https://openairdocs.org/sdr/CALA0001215), Aug 6, 2000: WEB. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN TAIL COMPARTMENT FORWARD SIDE OF STA 1485 WEB LT SIDE SKIN. REMOVED WEB IAW SRM 51-30-2 AND STOP DRILLED CRACK IAW SRM 55-0 - [SDR CALA0001213](https://openairdocs.org/sdr/CALA0001213), Aug 6, 2000: SKIN. DENTED. INSPECTION FOUND LT AFT FUSELAGE SKIN DENTED AT FS 1497. A NEW SKIN PATCH WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-34, FIGURE 5, AND 51-60-0. - [SDR CALA0001212](https://openairdocs.org/sdr/CALA0001212), Aug 6, 2000: STRUCTURE. GOUGED. INSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD UPPER AND LOWER BARREL NUT HOLES GOUGED. REAMED BARREL NUT HOLES AND INSTALLED BUSHINGS IAW EA 9-5511-2-A0738 - [SDR CALA0001211](https://openairdocs.org/sdr/CALA0001211), Aug 6, 2000: DOOR FRAME. BENT. INSPECTION FOUND LOOSE AND PULLED RIVETS IN FUSELAGE SKIN AND AFT NLG DOOR JAMB WAS BENT AND GOUGED AT STA 110. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51- - [SDR CALA0001210](https://openairdocs.org/sdr/CALA0001210), Aug 6, 2000: FLANGE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT FUSELAGE AC SERVICING PANEL CUTOUT FLANGE. REMOVED AND REPLACED DOUBLER IAW SRM 53-34-0, FIGURE 4, SHEET 1. - [SDR CALA0001198](https://openairdocs.org/sdr/CALA0001198), Aug 2, 2000: WEB. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN WEB SKIN AT RT SIDE OF TAIL COMPARTMENT STA 1485, JUST FORWARD OF RUDDER TRIM. THE WEB AND ANGLE WERE REMOVED AND THE CRACK - [SDR CALA0001183](https://openairdocs.org/sdr/CALA0001183), Jul 28, 2000: PAN. CRACKED. INSPECTION FOUND AFT CARGO DOOR PAN CRACKED AT FORWARD UPPER CORNER AND AT APPROXIMATELY 12 INCHES FROM FORWARD UPPER CORNER. THE CRACKS WERE .25 INCH LONG. THE - [SDR CALA0001168](https://openairdocs.org/sdr/CALA0001168), Jul 26, 2000: STRAP. CORRODED. INSPECTION FOUND AFT PIT, AFT BULKHEAD, RIGHT SIDE RETAINER STRAP CORRODED AT FS 1338. A NEW RETAINER STRAP WAS INSTALLED IAW SRM 51-10-2, 53-24-0, FIGURE 11, A - [SDR CALA0001167](https://openairdocs.org/sdr/CALA0001167), Jul 26, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 807 - 1022, RBL 54. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F, 51-30-1, 51-30-5, AND 51-60-0. - [SDR CALA0001166](https://openairdocs.org/sdr/CALA0001166), Jul 26, 2000: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 1.6 INCH CRACK IN L-1 DOOR LOWER FORWARD CORNER SEAL ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND A NEW ATTACH ANGLE WAS INSTALLED IAW SRM - [SDR CALA0001165](https://openairdocs.org/sdr/CALA0001165), Jul 26, 2000: STRAP. CORRODED. INSPECTION FOUND AFT CARGO BAY FRAME STRAP CORRODED AT STA 1231, LONGERON 28R-30. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-4, 51-10-3, - [SDR CALA0001164](https://openairdocs.org/sdr/CALA0001164), Jul 26, 2000: DOUBLER. CHAFED. INSPECTION FOUND AFT CARGO DOOR OUTER LOWER AFT DOUBLER CHAFED. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0001162](https://openairdocs.org/sdr/CALA0001162), Jul 25, 2000: SKIN. GOUGED. INSPECTION FOUND THE AFT FUSELAGE SKIN DENTED AND GOUGED AT STA 1320 BELOW NR 2 ENGINE PYLON, LONGERON 19R. THE GOUGE WAS BLENDED IAW SRM 53-01, FIGURE 1, SHEET - [SDR CALA0001160](https://openairdocs.org/sdr/CALA0001160), Jul 25, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1212, LONGERON 28L-29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51 - [SDR CALA0001159](https://openairdocs.org/sdr/CALA0001159), Jul 25, 2000: CHANNEL. CORRODED. INSPECTION FOUND RIGHT O/B FLOOR PANEL HAT CHANNEL CORRODED AT STA 826 - 907, RBL 54. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-21-00. - [SDR CALA0001158](https://openairdocs.org/sdr/CALA0001158), Jul 25, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 796 - 946, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 53-05, FIGURE - [SDR CALA0001157](https://openairdocs.org/sdr/CALA0001157), Jul 25, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT SIDE CENTER SEAT TRACK CORRODED AT FS 1031 - 1241, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51 - [SDR CALA0001156](https://openairdocs.org/sdr/CALA0001156), Jul 25, 2000: PAN. CRACKED. INSPECTION FOUND A 1.2 INCH CRACK IN MID CARGO DOOR AFT PAN FLANGE ADJACENT TO TORQUE TUBE CAM. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 1. THE EXISTING - [SDR CALA0001155](https://openairdocs.org/sdr/CALA0001155), Jul 25, 2000: ANGLE. GOUGED. INSPECTION FOUND L-1 DOOR UPPER AFT LINER ATTACH ANGLE GOUGED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0001154](https://openairdocs.org/sdr/CALA0001154), Jul 25, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND LT CARGO TIE DOWN TRACK CORRODED AT STA 522 - 788, LONGERON 27L. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS AT STA 522 - 655 AND STA 684 - [SDR CALA0001151](https://openairdocs.org/sdr/CALA0001151), Jul 24, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155 - 1221, LONGERON 29R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. All 82: https://openairdocs.org/deregistered/N72825-2005-07-14/reports.md ## 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 19970614017779I](https://openairdocs.org/incident/19970614017779I), Jun 14, 1997: Doug DC982 (N72825), Kansas City, MO. Narrative: Continental airlines inc. flight COA142 departed cos enroute to ewr, June 14, 1997. After take-off, the cabin crew was unable to get water from… ## Other aircraft with N72825 - [Cancelled 2015-05-21](https://openairdocs.org/deregistered/N72825-2015-05-21): Destiny Powered Parachute DESTINY 2000, S/N 1B0117, built 2001. Sale reported, canceled. Owner: [Midland, TX](https://openairdocs.org/faa-place/TX/Midland) - [Cancelled 1955-10-12](https://openairdocs.org/deregistered/N72825-1955-10-12): Cessna 140, S/N 10011. Owner: [Howard Aviation Inc](https://openairdocs.org/faa-owner/HOWARD%20AVIATION%20INC) --- 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.