# N119AA: 1972 Mcdonnell Douglas DC-10-10, registration cancelled 2002-06-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 12, 2002 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-10-10](https://openairdocs.org/model/mcdonnell-douglas-dc-10-10) (registry code 3022110) - Engine: [GE CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 46519 - Year built: 1972 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 10, 1972 - Certificate issued: October 4, 2000 - Last registry action: October 4, 2000 - Mode S code: A04DA3 - Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N119AA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=119AA - Page: https://openairdocs.org/deregistered/N119AA-2002-06-12 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-10-10: https://openairdocs.org/model/mcdonnell-douglas-dc-10-10.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HALA0000007](https://openairdocs.org/sdr/HALA0000007), Jan 3, 2000: WARNING LIGHT. ILLUMINATED. HNL - FLT 931 - SLAT DISAGREE LIGHT ILLUMINATED INTERMITTENTLY DURING CRUISE AT FL 350 MACH .82 MINUS 57 DEGREES CELSIUS. CONTINUITY CHECK SLATS SENSOR, NO DEFE - [SDR HALA9900235](https://openairdocs.org/sdr/HALA9900235), Nov 19, 1999: ENGINE. VIBRATION. NR 1 ENGINE IN CRUISE FL360, 1 HOUR OUT OF LAX HAD NOTICEABLE VIBRATION ABOVE 88.9 PCT, N2 94.0 PCT, NR 1 CSD TEMP 30 DEGREES CELSIUS RISE 60 DEGREES CELSIUS BE - [SDR HALA9900202](https://openairdocs.org/sdr/HALA9900202), Oct 19, 1999: COALESCER BAGS. DIRTY. FLT 2 - HNL - STRONG ODOR IN CABIN SERVICE AREA MOSTLY BURNING OIL SMELL, BUT ALSO LIGHT PLASTIC SMELL. REMOVED AND REPLACED ALL 3 WATER SEPARATOR SOCKS. PURGED - [SDR HALA9900108](https://openairdocs.org/sdr/HALA9900108), May 3, 1999: SPLICE. FAILED. IN FLIGHT, DOOR 1L, 2L, 3L, EMERGENCY LIGHTS DIMLY AND INTERMITTENTLY ILLUMINATED. OCCASSIONALLY BRIGHT. SEAT LIGHT ON LEFT AND RIGHT SIDE OF LEFT AISLE IN 'A' - [SDR HALA9800410](https://openairdocs.org/sdr/HALA9800410), Dec 16, 1998: ENGINE. FAILED. FLT 21 - SEA - NR 2 ENGINE FAILURE ON TAKEOFF ROLL. N1 STARTED DECREASING AND EGT STARTED INCREASING IMMEDIATELY AFTER POWER SET FOR TAKEOFF. EGT INCREASED TO 9 - [SDR HALA9800375](https://openairdocs.org/sdr/HALA9800375), Nov 3, 1998: LIGHT. INOPERATIVE. LAS - FLT 935 - NR 3 FUEL LEVER LIGHT WON'T TEST. NR 2 FUEL LEVER AND FIRE T-HANDLE LIGHT DON'T ILLUMINATE DURING FIRE WARNING TEST. REPLACED NR 3 ENGINE FUEL S - [SDR HALA9800099](https://openairdocs.org/sdr/HALA9800099), Apr 22, 1998: CONTROL VALVE. MALFUNCTIONED. LAS - FLT 03 - LOG PAGE 4091834 - WHILE TURNING ONTO RUNWAY FOR DEPARTURE, SELECTED FLAPS AT 10 DEGREES. SHORTLY AFTER FLAPS AND INDICATOR REACHED 10 DEGREES, T - [SDR HALA9800080](https://openairdocs.org/sdr/HALA9800080), Apr 1, 1998: CONTROL BOX. FAILED. HNL - FLT 10 - EMERGENCY LIGHT TEST INOP (GREEN LT) AND 2L AND 4L FAULT LIGHT CAME ON DURING TEST. REPLACED EMERGENCY LIGHT CONTROL BOX ON 2L AND 4L DOOR, OPS C - [SDR HALA9800018](https://openairdocs.org/sdr/HALA9800018), Jan 19, 1998: NPU. FAILED. FLT 26 - HNL - NAV UNREADABLE, BOTH HSI AND RMI HEADINGS WERE DIFFERENT IN NAV POSITION UP TO 50 DEGREES AT ONE POINT. HSI COURSE INDICATORS DID NOT AGREE WITH - [SDR HALA9800006](https://openairdocs.org/sdr/HALA9800006), Jan 8, 1998: FITTING. LOOSE. PDX - FLT 25 - ON TAKEOFF ROLL, CAPTAIN HAD NO AIRSPEED IND, F/O AIRSPEED READ 115 KTS, DID HIGH SPEED ABORT. LEAK TESTED CAPT PITOT/STATIC SYSTEM. FOUND LEAK A - [SDR HALA9700316](https://openairdocs.org/sdr/HALA9700316), Dec 19, 1997: RCCB. FAILED. HNL - FLT NR 4 - IN CRUISE FLIGHT, NR 1 GEN OFF LIGHT CAME ON. VOLT/FREQENCY ZERO. FOLLOWED ABNORMAL PROCEDURES AND RESET NR 1 GEN. VOLT/FREQS OK. 4 MINUTES LAT - [SDR HALA9700315](https://openairdocs.org/sdr/HALA9700315), Dec 19, 1997: CSD. FAILED. FLT 4 - HNL - ON CLIMB-OUT, AC BUS TIE NR 3 ISOL LIGHT CAME ON. CHECKED FREQ AT 392. NR 3 WOULD NOT PARALLEL. AIRCRAFT RETURNED TO HNL, WHERE A UNEVENTFUL LANDI - [SDR 98ZZZM145](https://openairdocs.org/sdr/98ZZZM145), Dec 19, 1997: ECU. FAILED. HNL - FLT NR 4 - IN CRUISE FLIGHT, NR 1 GEN OFF LIGHT CAME ON. VOLT/FREQENCY ZERO. FOLLOWED ABNORMAL PROCEDURES AND RESET NR 1 GEN. VOLT/FREQS OK. 4 MINUTES LAT - [SDR HALA9700231](https://openairdocs.org/sdr/HALA9700231), Nov 19, 1997: FITTING. CRACKED. DURING B-CHECK IN LAX, A CRACK WAS FOUND ON THE HORIZONTAL STAB UPPER RIGHT AFT FITTING, APPROX 2 INCHES INBOARD OF ATTACH BOLTS. HORIZONTAL STABILIZER UPPER LE - [SDR HALA96163](https://openairdocs.org/sdr/HALA96163), Nov 21, 1996: CADC. MALFUNCTIONED. SEA - FLT 2025 - OVERSPEED WARNING ON TAKEOFF AT 90 KNOTS. ABORTED TAKEOFF. NO STICK SHAKER. PERFORMED AURAL WARNING CHECKS PER TAFI 31-51-00 PAGE 105. PERFORME - [SDR HALA96129](https://openairdocs.org/sdr/HALA96129), Sep 3, 1996: CONTROL MODULE. MALFUNCTIONED. HNL - FLT 21 - FOUND EMERGENCY FLOOR LIGHTS, CABIN C, RIGHT SIDE CAME ON DURING FLIGHT. REPLACED THR NR 1 CONTROL MODULE AND THE OPERATIONAL CEHCK WAS OK. (M) - [SDR HAL9639](https://openairdocs.org/sdr/HAL9639), Apr 11, 1996: BATTERY PACK. DISCHARGED. HNL - FLT 10 - ON PRE-FLIGHT IN HNL, FOUND AFT POWER PACK OF EMERGENCY LIGHTING SYSTEM INOPERATIVE. REPLACED POWER PACK. OPS CHECK OK. (X) - [SDR HALA95161](https://openairdocs.org/sdr/HALA95161), Nov 23, 1995: CONNECTORS. DIRTY. HNL - FLT NR 25 - NR 1 FUEL LEVER, FIRE HANDLE AND A-LOOP LIGHT FLICKERED INTERMITTENTLY ON DESCENT WITH ENGINES AT IDLE. NO AURAL WARNING. MOVED NR 1 THROTTLE - [SDR HAL95092](https://openairdocs.org/sdr/HAL95092), Jul 6, 1995: FIRE LOOP. CHAFED. LAX - INFORMATION FROM LOG PAGE 142093. DURING ENGINE NR 1 LOOP , 'B' FLICKERED ON OVER A ONE MINUTE PERIOD. ACCOMPLISHED ABNORMAL PROCEDURE 1 IN FIRE PROTECTIO ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX73IL055](https://openairdocs.org/ntsb/LAX73IL055), May 9, 1973: Douglas DC-10 (N119AA), Tucson, AZ, incident, minor damage ## FAA accident and incident reports (2) 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 19890122007319I](https://openairdocs.org/incident/19890122007319I), Jan 22, 1989: Doug DC1010 (N119AA), Nashville, TN, Minor damage. Low oil pressure on NR3 engine. Shutdown engine. Diverted to Nashville. Shear at inlet to gear box caused failure. - [Incident 19881010062979I](https://openairdocs.org/incident/19881010062979I), Oct 10, 1988: Doug DC1010 (N119AA), New York, NY, Minor damage. Engine vibration and rising EGT on climbout. Dumped fuel and discharged fire bottles. Returned and landed safely. ## Other aircraft with N119AA - [Cancelled 2021-07-20](https://openairdocs.org/deregistered/N119AA-2021-07-20): Agusta A119, S/N 14505, built 2006. Owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) --- 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.