# N825US: 1984 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2003-10-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 31, 2003 - Exported to: Colombia - 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) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49237 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: June 22, 1984 - Certificate issued: December 26, 2002 - Last registry action: December 26, 2002 - Mode S code: AB4541 - Owner when cancelled: [Finova Capital Corp](https://openairdocs.org/faa-owner/FINOVA%20CAPITAL%20CORP) - Location: [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale) - Owner type: Corporation - Owner's area on the map: 33.4945° N, 111.9207° W: Placed by OpenAirDocs at the center of ZIP code 85251, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N825US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=825US - Page: https://openairdocs.org/deregistered/N825US-2003-10-31 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAD01138](https://openairdocs.org/sdr/USAAD01138), Jul 28, 2001: POWER SUPPLY. DEFECTIVE. EWR - THE CEILING MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 12-15 WOULD NOT EXTINGUISH WITH THE SHIPS POWER OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPP - [SDR USAAD01124](https://openairdocs.org/sdr/USAAD01124), Jun 12, 2001: SLIDE. PHL - THE FORWARD ENTRY DOOR EVACUATION SLIDE GIRT BAR WAS HARD TO ENGAGE AND DISENGAGE. MAINTENANCE REPLACED THE EVACUATION SLIDE AND GIRT BAR. (M) - [SDR USAAD01123](https://openairdocs.org/sdr/USAAD01123), Jun 8, 2001: LIGHT. INOPERATIVE. PIT - THE EMERGENCY LIGHT ASSEMBLY AT SEAT 20 LEFT SIDE DOES NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AT ROW 20 LEFT SIDE. (M) - [SDR USAAD01119](https://openairdocs.org/sdr/USAAD01119), Jun 1, 2001: BATTERY PACK. DISCHARGED. PIT - THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAD01109](https://openairdocs.org/sdr/USAAD01109), May 16, 2001: LANYARD. DETERIORATED. PHL - THE FORWARD SERVICE DOOR EVACUATION SLIDE LANYARD WAS DETERIORATED. MAINTENANCE REPLACED THE LANYARD ASSEMBLY. (M) - [SDR USAAD01063](https://openairdocs.org/sdr/USAAD01063), Mar 23, 2001: STRUT. DISCHARGED. PIT-ABE - FLT 1422 - THE NOSE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE GEAR AND PER - [SDR USAA002193](https://openairdocs.org/sdr/USAA002193), Dec 15, 2000: LONGERON. CORRODED. LONGERON 29 RIGHT, AT STATION 1309-1338, CORROSION.SPLICED IN NEW SECTION OF LONGERON. - [SDR USAADD00148](https://openairdocs.org/sdr/USAADD00148), Sep 21, 2000: STRUT. DISCHARGED. TPA-PIT - FLT 1264 - AFTER TAKEOFF, THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE - [SDR USAAD00128](https://openairdocs.org/sdr/USAAD00128), Aug 9, 2000: ENGINE. FAILED. CLT-MCI - FLT 935 - AT APPROXIMATELY 23,000 FT, THE FLIGHT ATTENDANT REPORTED THE RIGHT ENGINE MADE AN ODD SOUND. ALL ENGINE INDICATIONS WERE NORMAL. AT ABOUT 3 - [SDR USAAD00082](https://openairdocs.org/sdr/USAAD00082), May 23, 2000: VALVE. LEAKING. MSY/CLT - FLT 796 - ON CLIMB-OUT, THE CABIN FILLED WITH SMOKE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A LEAKING LE - [SDR USAAD00013](https://openairdocs.org/sdr/USAAD00013), Jan 18, 2000: WARNING SYSTEM. ACTIVATED. PHL-ROC - FLT 2208 - AFTER THE LANDING GEAR EXTENSION DURING APPROACH THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. THE APPROACH WAS ABORTED AND THE LANDING GEA - [SDR USAAD99116](https://openairdocs.org/sdr/USAAD99116), Aug 18, 1999: VALVE. FAILED. CLT-CMH - FLT 8003, THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF AND THE FLOW LIGHT WAS ON CONTINUOUSLY. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOU - [SDR USAAD99059](https://openairdocs.org/sdr/USAAD99059), Apr 27, 1999: WATER SEPARATOR. BLOWN. CLT - FL 1646 - AFTER TAKEOFF, CREW REPORTED THAT THERE WAS SMOKE IN THE CABIN. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NO - [SDR USAAD99052](https://openairdocs.org/sdr/USAAD99052), Mar 19, 1999: FUSE. FRACTURED. LGA-TPA - FLT 2186 - DURING CRUISE, THE RIGHT HYDRAULIC PRESSURE DROPPED TO JUST ABOVE ZERO AND THE RIGHT HYDRAULIC QTY WAS DROPPING. THE A/C DIVERTED TO BWI AN - [SDR USAAD99043](https://openairdocs.org/sdr/USAAD99043), Mar 10, 1999: MECHANISM. NOT LATCHED. FLL-PHL FLT 1430 - AFTER TAKEOFF THE CABIN PRESSURE FLOW LIGHT ILLUMINATED AND TEH CABIN WOULD NOT PRESSURIZE IN AUTO OR MANUAL. THE AIRCRAFT DIVERTED TO MCO AN - [SDR USAAD99018](https://openairdocs.org/sdr/USAAD99018), Jan 23, 1999: SEAL. MALFUNCTIONED. CLT-BUF - FLT 1223 - AFTER TAKEOFF, THE CABIN WOULD ONLY PRESSURIZE TO 1 PSI WITH THE OUTFLOW VALVE FULLY CLOSED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED - [SDR USAAD99010](https://openairdocs.org/sdr/USAAD99010), Jan 16, 1999: MECHANISM. OUT OF SEQUENCE. CLT/ORD - FLT 1527 - AFTER TAKEOFF, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT IN EITHER THE AUTO OR MANUAL MODE. THE AIRCRAFT RETURNED TO THE FIELD AND LAN - [SDR USAAD98167](https://openairdocs.org/sdr/USAAD98167), Sep 27, 1998: SEAL. LEAKING. PIT-LGA FLT 1498 - DURING CLIMB-OUT, THE AIRCRAFT WOULD NOT PRESSURIZE. THE FLIGHT ATTENDANT REPORTED A LOUD NOISE AROUND THE L2 DOOR. THE AIRCRAFT RETURNED TO - [SDR USAAD98165](https://openairdocs.org/sdr/USAAD98165), Sep 26, 1998: SEAL. MALFUNCTIONED. CLT-BDL - FLT 995 - AFTER TAKEOFF, THE AFT LEFT SERVICE DOOR DID NOT SEAL WELL. THE CAPTAIN RECEIVED A FLOW LIGHT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED - [SDR USAAD98154](https://openairdocs.org/sdr/USAAD98154), Aug 31, 1998: CSD. FAILED. PHL-TPA - FLT 433 - EN ROUTE THE RIGHT ENGINE DRIVEN GENERATOR BECAME INOPERATIVE. THE FLIGHT CREW STARTED THE APU TO USE THE APU GENERATOR. ABOUT 20 MINUTES LA - [SDR 98ZZZM771](https://openairdocs.org/sdr/98ZZZM771), Aug 31, 1998: GENERATOR. FAILED. PHL-TPA - FLT 433 - EN ROUTE THE RIGHT ENGINE DRIVEN GENERATOR BECAME INOPERATIVE. THE FLIGHT CREW STARTED THE APU TO USE THE APU GENERATOR. ABOUT 20 MINUTES LA - [SDR USAAD98144](https://openairdocs.org/sdr/USAAD98144), Aug 15, 1998: SEAL. LOOSE. PHL - FLT 200 - AFTER TAKEOFF, THE CREW HEARD A LOUD BANGING SOUND AND THE FORWARD SERVICE DOOR FAILED TO SEAL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WI - [SDR USAAD98117](https://openairdocs.org/sdr/USAAD98117), Jun 30, 1998: DOOR. NOT CLOSED. CLT - FLT 237 - AFTER TAKEOFF, CREW REPORTED THEY COULD NOT PRESSURIZE THE AIRCRAFT. FLIGHT ATTENDANTS REPORTED THAT THE L2 DOOR WAS NOT CLOSED PROPERLY AND WAS - [SDR USAA980175](https://openairdocs.org/sdr/USAA980175), Apr 26, 1998: SKIN. CRACKED. PIT - DURING Q-3 CHECK, FOUND .50 INCH LONG CRACK IN SKIN AT STA 1380 ABOVE LONGERON 14R. INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 38 SHEET 21. (X) - [SDR USAAD98006](https://openairdocs.org/sdr/USAAD98006), Jan 11, 1998: BATTERY. DISCHARGED. CLT - EMERGENCY LIGHTS IN TAIL COMPARTMENT CEILING INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD97193](https://openairdocs.org/sdr/USAAD97193), Nov 2, 1997: SLIDE. FAILED. PIT - THE TAILCONE INADVERTENTLY DEPLOYED BUT THE EMERGENCY EVACUATION SLIDE DID NOT. MAINTENANCE REPLACED THE TAILCONE ASSEMBLE DUE TO DAMAGE AND THE EMERGENCY - [SDR USAAD97182](https://openairdocs.org/sdr/USAAD97182), Oct 18, 1997: GEN CONTL UNIT. INOPERATIVE. CLT - FL 1005 - EN ROUTE CLT-SRQ, THE LEFT GENERATOR TRIPPED THE LEFT AC BUS AND LEFT GENERATOR OFF. THE LEFT GENERATOR OFF LIGHT ILLUMINATED. AFTER STARTING TH - [SDR USAAD97159](https://openairdocs.org/sdr/USAAD97159), Sep 18, 1997: ANTI-ICE DUCT. FAILED. PBI - FL 1681 - AFTER TAKEOFF, CREW RECEIVED THE LEFT ENGINE FIRE WARNING INDICATION. CREW WENT THROUGH EMERGENCY PROCEDURES AND WARNING EXTINGUISHED (ENGINE WA - [SDR USAAD97127](https://openairdocs.org/sdr/USAAD97127), Jul 25, 1997: CONTROLLER. FAULTY. CLT - FL 1090 - CAPTAIN REPORTED THAT HE HAD PRESSURIZATION CONTROL PROBLEMS. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. THE AFT PRESSURIZATION - [SDR USAAD97125](https://openairdocs.org/sdr/USAAD97125), Jul 23, 1997: SWITCH. FAILED. PIT - FLT 1233 - APPROXIMATELY 80 MILES OUT OF PIT, CREW RECEIVED THE RIGHT ENGINE OIL CLOG LIGHT. CREW SHUT DOWN THE RIGHT ENGINE. FLIGHT RETURNED TO PIT AND L - [SDR USAAD97081](https://openairdocs.org/sdr/USAAD97081), May 10, 1997: DOOR. NOT CLOSED. FLT 222 - PIT-BDL - DURING CLIMB-OUT FROM PIT, THE AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL MODE. FLIGHT LEVELLED OFF AT 8000 FEET AND THEN RETURNED TO P - [SDR USAA950467](https://openairdocs.org/sdr/USAA950467), Apr 17, 1995: SKIN. CRACKED. PIT - DURING Q-6 CHECK INSPECTION, FOUND CRACK 1.25 INCHES LEFT UPPER FORWARD CORNER OF MAIN ENTRANCE DOOR FUSELAGE SKIN (X-RAY INSPECTION). CUT OUT DAMAGED ARE ## Other aircraft with N825US - [Registered now](https://openairdocs.org/aircraft/N825US): Diamond Aircraft Ind DA 40, S/N 40.825, built 2007 --- 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.