# N807US: 1981 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2004-06-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 18, 2004 - Exported to: Swaziland - 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-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 48039 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 9, 1981 - Certificate issued: June 8, 2004 - Last registry action: June 8, 2004 - Mode S code: AAFDB1 - Owner when cancelled: [Alameda Corp Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORP%20TRUSTEE) - Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio) - Owner type: Corporation - Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N807US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807US - Page: https://openairdocs.org/deregistered/N807US-2004-06-18 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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR LCQ](https://openairdocs.org/sdr/LCQ), Oct 30, 2001: PAD. CRACKED. CRACK INDICATIONS AROUND JACK PAD ON BOTTOM OF LOWER SEGMENT OF RT MAIN LANDING GEAR. - [SDR USAAD01148](https://openairdocs.org/sdr/USAAD01148), Aug 10, 2001: CONTROL VALVE. OUT OF RIG. PIT-BOS - FLT 564 - DURING APPROACH, RECEIVED LANDING GEAR UNSAFE INDICATIONS WHEN THE LANDING GEAR WAS SELECTED DOWN. RECYCLED THE LANDING GEAR AND RECEIVED NO - [SDR USAAD01147](https://openairdocs.org/sdr/USAAD01147), Aug 7, 2001: BATTERY. INOPERATIVE. IND - THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 30 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT ROW 30. OPS CHECKED OK. (M) - [SDR USAAD01144](https://openairdocs.org/sdr/USAAD01144), Aug 2, 2001: BATTERY. INOPERATIVE. TPA - THE EMERGENCY PACK WILL NOT TEST ROW 11. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USAAD01125](https://openairdocs.org/sdr/USAAD01125), Jun 13, 2001: BATTERY. DISCHARGED. IND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD01112](https://openairdocs.org/sdr/USAAD01112), May 21, 2001: BATTERY. DISCHARGED. BOS - THE LOW LEVEL LIGHTS FAILED TO TEST AT SEAT ROWS 1, 11, 25 AND 30. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD01049](https://openairdocs.org/sdr/USAAD01049), Mar 13, 2001: COALESCER BAG. CONTAMINATED. CLT-EWR - FLT 554 - AFTER TAKEOFF, SMOKE APPEARED IN THE REAR CABIN. THE LEFT AIR CONDITIONING PACK WAS TURNED OFF AND THE SMOKE DISSIPATED. THE AIRCRAFT CONTIN - [SDR USAAD01032](https://openairdocs.org/sdr/USAAD01032), Feb 17, 2001: LIGHT. OUT OF POSITION. MCO - THE EMERGENCY LIGHTS AT ROWS 30, 25, AND 20 WERE FOUND TO BE OUT OF POSITION. THE LIGHTS WERE PLACED INTO THEIR CORRECT POSITIONS. (M) - [SDR USAAD01021](https://openairdocs.org/sdr/USAAD01021), Feb 5, 2001: LIGHT. SHORTED. MHT-PIT - FLT 395 - DURING CRUISE, THE EMERGENCY LIGHTS ILLUMINATED WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION. WITH THE EMERGENCY LIGHT SWITCH IN THE - [SDR USAA010163](https://openairdocs.org/sdr/USAA010163), Jan 17, 2001: FITTING. CRACKED. PIT - FOUND FITTING CRACKED .75 INCH, LEFT SPOILER ACTUATOR FITTING AT BOLT BOSS. REPLACED PART PER EO 5788M381. (M) - [SDR USAAD00171](https://openairdocs.org/sdr/USAAD00171), Nov 2, 2000: BATTERY. DISCHARGED. MCO - THE OVERHEAD EMERGENCY LIGHTS FOR ROWS 17-24 WERE FOUND TO BE INOPERTIVE. MAINTENANCE REPLACED THE BATTERIES IN TWO BATTERY PACKS. OPS CHECKED OK. (M) - [SDR USAAD00045](https://openairdocs.org/sdr/USAAD00045), Mar 31, 2000: BATTERY. DISCHARGED. TPA - THE FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 9 AND 11, AND THE REMAINING LIGHTS WERE DIM. MAINTENANCE REPLACED THE FLOOR LEVEL EMERGENCY LIGH - [SDR USAAD00044](https://openairdocs.org/sdr/USAAD00044), Mar 30, 2000: HYDRAULIC SYSTEM. OVERSERVICED. BTV-PIT - FLT 1221 - NOTICED BURNING RUBBER SMELL IN COCKPIT AND CABIN BETWEEN 800 AND 3000 FEET DURING TAKEOFF. USED FULL POWER AND BOTH PACKS ON, SMELL WAS NO - [SDR USAAD99149](https://openairdocs.org/sdr/USAAD99149), Oct 19, 1999: BATTERY. DISCHARGED. CLT - THE EMERGENCY LIGHTS IN THE FIRST CLASS SECTION OF THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE EMERGENCY LIGHTS. (M) - [SDR USAA991069](https://openairdocs.org/sdr/USAA991069), Sep 26, 1999: SKIN. CRACKED. PIT - DURING RON VISIT, FOUND 1 INCH CRACK IN SKIN AT RIGHT STATION 69.5 LONGERON 20 RT. INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) - [SDR USAAD98209](https://openairdocs.org/sdr/USAAD98209), Nov 22, 1998: DRAG LINK. OUT OF ADJUST. PIT-EWR - FLT 1642 - ON TAKEOFF, THERE WAS SEVERE NOSE WHEEL VIBRATION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SHIMMED THE - [SDR USAAD98164](https://openairdocs.org/sdr/USAAD98164), Sep 23, 1998: PUMP. FAILED. PIT-MDT - FLT 710 - AFTER TAKEOFF THE PRESSURE WENT TO ZERO FOR THE LEFT ENGINE HYDRAULIC PUMP. FOR MAINTENANCE CONVENIENCE THE AIRCRAFT RETURNED TO THE FIELD A - [SDR USAAD98133](https://openairdocs.org/sdr/USAAD98133), Aug 5, 1998: DOOR. OPEN. BOS - FLT 1924 - AIRCRAFT EXPERIENCED HEAVY VIBRATION FROM NOSE WHEEL AREA AFTER GEAR RETRACTION. MAINTENANCE FOUND THE RIGHT NOSE GEAR DOOR OPEN. THE DOOR WAS - [SDR USAA980157](https://openairdocs.org/sdr/USAA980157), Apr 5, 1998: SKIN. CRACKED. PIT - DURNIG C-2 CHECK, FOUND .5 INCH CRACK AT STATION 984 LONGERON 20 LEFT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-28. (M) - [SDR USAA980156](https://openairdocs.org/sdr/USAA980156), Apr 5, 1998: SKIN. CRACKED. PIT - DURING C-2 CHECK, FOUND .5 INCH CRACK IN SKIN AT STATION 984 LONGERON 20 RIGHT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-28. (M) - [SDR USAAD97205](https://openairdocs.org/sdr/USAAD97205), Nov 8, 1997: TEMP BULB. FAILED. PIT - FLT 1108 - AIRCRAFT DIVERTED FROM BDL DUE TO ICING CONDITIONS. CREW EXPERIENCED RIGHT ICE PROTECTION TEMP HIGH LIGHT ON AND OFF AT CRUISE ALTITUDE WITH TH - [SDR USAAD97191](https://openairdocs.org/sdr/USAAD97191), Oct 30, 1997: LINE. FAILED. PIT - FL 8001 - CREW REPORTED LOSS OF LEFT HYDRAULIC QUANTITY AND PRESSURE EN ROUTE. MAINTENANCE REPLACED A BROKEN HYDRAULIC LINE AT THE PRESSURE FILTER IN THE - [SDR USAAD97119](https://openairdocs.org/sdr/USAAD97119), Jul 11, 1997: DUCTS. LOOSE. DFW/PIT - FLT 335 - 0N CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO FIELD. FOUND RT AND LT ACM EXHAUST DUCTS OFF. RECONNECTED, CHECKED GOOD. (X) - [SDR USAAD97035](https://openairdocs.org/sdr/USAAD97035), Feb 6, 1997: SWITCH. FAILED. BOS/CLT - FLT 1071 - AT FL 350, RIGHT PACK TRIPPED OFF, DESCENDED TO FL 250. THE LEFT PACK THEN TRIPPED OFF. BEGAN EMERGENCY DESCENT. AT FL 180, THE CABIN ALTIT - [SDR USAAD96012A](https://openairdocs.org/sdr/USAAD96012A), Jan 25, 1996: GENERATOR. FAILED. CLT - CREW RECEIVED FAULT LIGHT ON LEFT ELECTRIC BUS. RESET WOULD NOT CURE PROBLEM. APU STARTED, BUT IT WOULD NOT POWER THE BUS. FLIGHT DIVERTED TO CLT AND LAND - [SDR USAAD96011A](https://openairdocs.org/sdr/USAAD96011A), Jan 25, 1996: FIRE LOOPS. MALFUNCTIONED. TYS - FL 285 - EN ROUTE BNA-BWI, CREW RECEIVED RIGHT ENGINE 'B' LOOP FIRE WARNING. CREW FOLLOWED PILOT HANDBOOK PROCEDURES. SHORTLY THEREAFTER, THE CREW RECEIVE - [SDR USAA950071](https://openairdocs.org/sdr/USAA950071), Jan 10, 1995: CLIPS. CORRODED. PIT - DURING Q-3 CHECK INSPECTION ACCOMPLISHED CORROSION CONTROL TASK ITEM NR C51-53300 AND FOUND LEVEL II CORROSION AT THE FORWARD CARGO DOOR HINGE ATTACH FLAN - [SDR USAA950070](https://openairdocs.org/sdr/USAA950070), Jan 9, 1995: CUSP MEMBRANE. CRACKED. PIT - DURING Q-3 CHECK INSPECTION, FOUND 1.25 INCH CRACK AT STATION 906 RT CUSP MEMBRANE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2. ( - [SDR USAA950069](https://openairdocs.org/sdr/USAA950069), Jan 9, 1995: CUSP MEMBRANE. CRACKED. PIT - DURING Q-3 CHECK INSPECTION, FOUND A 3 INCH CRACK AT STATION 885 RT CUSP MEMBRANE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 1 AND - [SDR USAA950067](https://openairdocs.org/sdr/USAA950067), Jan 5, 1995: ANGLE. CRACKED. PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK AT STRINGER 1388 AFT SIDE OF CANTED BELT FRAME RT SIDE ATTACH ANGLE. INSTALLED ATTACH ANGLE STRAP REPAIR - [SDR USAA950066](https://openairdocs.org/sdr/USAA950066), Jan 5, 1995: LONGERONS. CRACKED. PIT - DURING Q-3 CHECK INSPECTION, FOUND .5 INCH AND .75 INCH CRACK IN STATION 1452 LONGERONS 3R AND 3L. MANUAL NEW CLIP AND REPAIRED PER SRM 53-03. (Z) - [SDR USAA950065](https://openairdocs.org/sdr/USAA950065), Jan 5, 1995: LONGERON. CRACKED. PIT - DURING Q-3 CHECK INSPECTION, FOUND SEVERAL CRACKS IN LONGERON 17L AT STATION 280. REPLACED LONGERON AND SPLICED PER SRM 53-02 FIG 2 AND USAIR EA NR 2893. - [SDR USAA950064](https://openairdocs.org/sdr/USAA950064), Jan 5, 1995: ANGLE. CRACKED. PIT - DURING Q-3 CHECK INSPECTION, FOUND .75 INCH CRACK AT STATION 1388 RT SIDE OF VERTICAL STAB ATTACH ANGLE. STOP DRILLED AND INSTALLED REPAIR ANGLES PER SRM ## Other aircraft with N807US - [Registered now](https://openairdocs.org/aircraft/N807US): Dehavilland DHC-6-300, S/N 807 --- 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.