# N125AA: 1972 Mcdonnell Douglas DC-10-10, registration cancelled 2010-04-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 8, 2010 - Status when cancelled: Triennial form not returned - 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: 46525 - Year built: 1972 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 12, 1999 - Certificate issued: June 10, 2003 - Last registry action: June 16, 2009 - Mode S code: A06646 - 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/N125AA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=125AA - Page: https://openairdocs.org/deregistered/N125AA-2010-04-08 From the FAA registry file of October 31, 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HALA0000341](https://openairdocs.org/sdr/HALA0000341), Oct 11, 2000: CONTROLLER. FAILED. PDX - FLT 25 - NR 3 MANIFOLD FAIL LIGHT CAME ON DURING FLIGHT. FOLLOWED CHECKLIST AND TURNED OFF NR 3 PNEU AND NR 3 PACK. PRESSURIZED PNEU SYSTEM 3. INSPECTED A - [SDR HALA0000269](https://openairdocs.org/sdr/HALA0000269), Aug 23, 2000: FIRE LOOP. FAILED. HNL - FLT 931 - NR 1 ENGINE B LOOP WILL NOT TEST. CHECKED SERIES RESISTANCE B LOOP AT 7 OHMS. REPLACED TEST RELAY K2-154 PRECAUTIONARY CHANGE, OPS AND FIRE TEST - [SDR HALA0000235](https://openairdocs.org/sdr/HALA0000235), Jul 22, 2000: ENGINE. FAILED. FLT 3 - LAX - SLIGHT SMELL STARTED, 1 MINUTE LATER AIRCRAFT SHUDDERED. NR 1 EGT WENT OVER 900 DEG N2 DECAYED SHUT NR 1 ENGINE DOWN. ALTITUDE 12,000 FEET. REMOVE - [SDR HALA9900233](https://openairdocs.org/sdr/HALA9900233), Nov 19, 1999: HOUSING. CRACKED. HNL - FLT 939 - HYDRAULIC SYSTEM 3 LEVEL OFF LIGHT ON. SYSTEM 3 HYDRAULIC QUANTITY ZERO, IT HAPPENED ON FINAL APPROACH AFTER ALL FLAPS OUT. PUMPS WERE TURNED OF - [SDR HALA9900196](https://openairdocs.org/sdr/HALA9900196), Sep 27, 1999: BUS CONTROL. FAILED. SEA - FLT 21 - NR 2 GEN OFF LIGHT ON. ISSUED MEL 24-01 AUTH NR 9-194C-B. DURING OVERNIGHT MAINTENANCE RREMOVED AND REPLACED BUS CONTROL UNIT CHECKS OK. REMOVED - [SDR HALA9900060](https://openairdocs.org/sdr/HALA9900060), Feb 23, 1999: WARNING LIGHT. ILLUMINATED. HNL - FLT 466 - AFTER LANDING SLAT YELLOW DISAGREE LIGHT REMAINED ON AFTER RETRACTING FLAPS. RECYCLED FLAPS TO 50 DEGREES AND BACK AND LIGHT REMAINED ON. SECURI - [SDR HALA9900057](https://openairdocs.org/sdr/HALA9900057), Feb 20, 1999: SENSOR. FAILED. FLT 939 - LAX - SLAT DISAGREE LIGHT ILLUMINATED WHEN FLAPS ARE SET FOR 2 DEGREE, TAKEOFF DISAGREE LIGHT DOES NOT GO OUT UNTIL FLAP SLAT RETRACTED. REPLACED RIGH - [SDR HALA9900019](https://openairdocs.org/sdr/HALA9900019), Jan 17, 1999: SENSOR. MALFUNCTIONED. HNL - FLT 482 - NR 3 ENGINE 'A' LOOP WILL NOT TEST, 'B' TEST OK. REMOVED AND REPLACED CONNECTOR PYLON LOOP 'A' NR 3 ENGINE. 'A' LOOP TEST OP CHECKED GOOD. (M) - [SDR HALA9900005](https://openairdocs.org/sdr/HALA9900005), Jan 8, 1999: RELAY. MALFUNCTIONED. HNL - FLT 25 - NR 3 ENGINE 'A' LOOP WILL NOT TEST. LOOP 'B' TEST OK. REMOVED AND REPLACED R2-153 RELAY GRN TEST GOOD. (M) - [SDR HALA9800418](https://openairdocs.org/sdr/HALA9800418), Dec 17, 1998: OVEN. FAILED. FLT 21 - HNL - OVEN NR 3 STARTED TO SMOKE IN FLIGHT. INSPECTION SHOWED THIS WAS NOT DUE TO MEAL BURNING. SMOKE CAME OUT THROUGH BOTTOM OF OVEN ONLY. OPS CHECK, - [SDR HALA9800408](https://openairdocs.org/sdr/HALA9800408), Dec 10, 1998: VALVE. FAILED. FLT NR 1 - LAX - RIGHT DUMP VALVE DID NOT OPEN DURING DUMP OPERATION. COMPLIED WITH AFM AND VALVE DID NOT OPEN. AIRCRAFT HAD ABORTED FLIGHT WITH STRONG ODOR IN - [SDR HALA9800404](https://openairdocs.org/sdr/HALA9800404), Dec 10, 1998: AIR DIST. ODOR. LAX - FLT 1 - STRONG ODOR IN CABIN AND COCKPIT, ABORTED FLIGHT. AIRCRAFT RETURNING TO LAX. ACCOMP CLEANING OF HEAT EXCHANGERS PER MM 21-53-01. CLEANED APU INLET - [SDR HALA9800136](https://openairdocs.org/sdr/HALA9800136), May 27, 1998: WIRE. BROKEN. HNL - FLT 482 - ENGINE NR 1 ANTI-ICE DISAGREE LIGHT ILLUMINATED WITH NR 1 ENGINE ANTI-ICE SWITCH OFF. ACCOMPLISHED ABNORMAL PROCEDURES SECTION 6-6. REPAIRED BRO - [SDR HALA9700299](https://openairdocs.org/sdr/HALA9700299), Dec 4, 1997: PROX BOX. FAILED. HNL - FLT 10 - SLAT DISAGREE LIGHT CAME ON WITH SLAT IN TAKEOFF POSITION ON APPROACH, THEN WENT BACK TO TAKEOFF. REMOVED AND REPLACED PROX BOX. (M) - [SDR HALA9700294](https://openairdocs.org/sdr/HALA9700294), Dec 1, 1997: BATTERY. DISCHARGED. HNL - FLT 3 - FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPS CHECK GOOD. (M) - [SDR HALA9700291](https://openairdocs.org/sdr/HALA9700291), Nov 30, 1997: PUMP. FAILED. HNL - FLT 1215 - LOST HYDRAULIC QTY ON NR 3 SYSTEM, DURING FLIGHT. ALTERNATE GEAR EXTENTION PERFORMED. FOUND 2/3 REVERSIBLE PUMP BYPASSING TO OVERFLOW. REPLACED - [SDR AALA971079](https://openairdocs.org/sdr/AALA971079), Jun 16, 1997: LONGERON. CORRODED. TUL - LONGERON NR 48R OUTBOARD ATTACHMENT FLANGE CORRODED IN SEVERAL LOCATIONS. REPAIRED LONGERON BY INSTALLING 7075-T6 .063 INCH DOUBLER REF DC-10 SRM 53-00-01 - [SDR AALA971076](https://openairdocs.org/sdr/AALA971076), Jun 15, 1997: SUPPORT. CRACKED. TUL - FLOOR SUPPORT CRACKED AT STATION 755 UPPER ATTACH FLANGE. REMOVED DAMAGED SECTION OF FLOOR SUPPORT. INSTALLED NEW SUPPORT SECTION AND DOUBLER PER SRM VOL - [SDR AALA971084](https://openairdocs.org/sdr/AALA971084), Jun 13, 1997: SHEAR TIE. CORRODED. TUL - SHEAR TIES CORRODED BETWEEN LONGERON 51 RT AND 51 LT STATION 1139. REMOVED AND REPLACED SHEAR TIES PER AARD 51-21-00. (M) - [SDR AALA971074](https://openairdocs.org/sdr/AALA971074), Jun 12, 1997: FITTING. CORRODED. TUL - AFT END OF LONGERON 52 CORRODED AT 'T' FITTING FOR PRESS DOM. REMOVED LONGERON 52 DUE TO EXCESS CORROSION REF DC10 AARD 51-01-00-03. INSTALLED NEW FABRICA - [SDR AALA971077](https://openairdocs.org/sdr/AALA971077), Jun 11, 1997: SKIN. CORRODED. TUL - BULGE IN BEAUTY STRIP SKIN AT STATION 1156 LONGERON 48 RIGHT. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM VOL 1 53-20-00. (M) - [SDR AALA971090](https://openairdocs.org/sdr/AALA971090), Jun 3, 1997: SUPPORT. CORRODED. TUL - FOUND CORROSION ON SUPPORT STRUCTURE FOR ROLLER TRAY 2ND FROM RT OUTBOARD. INSTALLED NEW ROLLER SUPPORT PER AARMD 51-10-00-21 REPAIR 1. (M) - [SDR AALA971089](https://openairdocs.org/sdr/AALA971089), Jun 3, 1997: FLOORBOARD. CORRODED. TUL - FOUND FLOORBOARD LANDING CORRODED LOCATED BETWEEN LEFT Z-ANGLE AND 2ND TRACK INBOARD FROM Z-ANGLE. INSTALLED NEW LANDING PER AARD 51-01-00-5 ITEMS AARD 51 - [SDR AALA971088](https://openairdocs.org/sdr/AALA971088), Jun 3, 1997: ANGLE. CORRODED. TUL - FLOORBOARD NUT PLATE ANGLE HAS CORROSION INBOARD OF Z-ANGLE. INSTALLED NEW ANGLE PER AARD 51-01-00-05 ITEM 5, AARD 51-10-00-21 REPAIR 1. (M) - [SDR AALA971087](https://openairdocs.org/sdr/AALA971087), Jun 3, 1997: SILL. CORRODED. TUL - STATION 1099 AFT SILL BELOW AND AFT OF RT UNLOAD BAR PULLEY CONFIG, SILL HAS HEAVY CORROSION AROUND NUTPLATE. INSTALL NEW SILL PER AARD 51-01-00-05 ITEM 5 - [SDR AALA971085](https://openairdocs.org/sdr/AALA971085), Jun 3, 1997: ROLLER TRAY. CORRODED. TUL - CENTER ROLLER TRAY AT STATION 999 HAS SURFACE CORROSION ON RIGHT FLANGE DOUBLER. INSTALLED NEW ANGLES PER AARD 51-01-00-05 ITEMS 5, AARD 51-10-00-21 REPAI - [SDR AALA970998](https://openairdocs.org/sdr/AALA970998), May 31, 1997: SEAT TRACK. CORRODED. TUL - NR 1 SEAT TRACK CORRODED FROM RIGHT SIDE JUST AFT OF RIGHT DOOR IN SEVERAL PLACES. INSTALL REPAIR PER SRM 53-70-00 P 66 AND ALODINE, PRIME. (M) - [SDR AALA971036](https://openairdocs.org/sdr/AALA971036), May 30, 1997: SPLICE. CORRODED. TUL - FOUD STRINGER SPLICE FROM STATION 979 TO 999 HAS SURFACE CORROSION AT STRINGER 52. INSTALLED NEW STRINGER SPLICE AS PER SRM 53-10-00. (M) - [SDR AALA970997](https://openairdocs.org/sdr/AALA970997), May 29, 1997: SUPPORT. CORRODED. TUL - FOUND CORROSION ON THE RIGHT SIDE OF G1A GALLEY (FWD EDGE). ACCOMPLISHED REPAIR OF FORWARD BEAM RIGHT SIDE OF P-LIFT IAW ESO DATED 5-29-97 ADN 7349. (M) - [SDR AALA970986](https://openairdocs.org/sdr/AALA970986), May 23, 1997: SUPPORT. CORRODED. TUL - FIRST SUPPORT RIGHT OF CENTER SEAT TRACK UNDER GALLEY 1, HAS CORROSION AROUND MOUNT HOLES. INSTALLED F/B SUPPORT RT OF CENTER SEAT TRACK UNDER GALLER 1 PE - [SDR AALA970985](https://openairdocs.org/sdr/AALA970985), May 23, 1997: SUPPORT. CORRODED. TUL - FOUND CORROSION ON FLOOR SUPPORT, FIRST SUPPORT LEFT OF CENTER SEAT TRACK UNDER GALLEY 1. INSTALLED FLOORBOARD SUPPORT LEFT OF CENTE RSEAT TRACK UNDER GAL - [SDR AALA970963](https://openairdocs.org/sdr/AALA970963), May 21, 1997: DOOR TRACK. CORRODED. TUL - LEFT FIRE BLOCK DOOR TRACK STA 879 INBOARD OF LOWER LOBE GALLEY. TRACK NR 2 HEAVY CORROSION. REPLACED CORRODED PORTION OF FIRE BLOCK DOOR TRACK PER DC 10- ## FAA accident and incident reports (5) 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 19971130041049I](https://openairdocs.org/incident/19971130041049I), Nov 30, 1997: Doug DC1010 (N125AA), Honolulu, HI. Lost NR1 hydro system. Manual gear extend. NR3 reversible pump failed. Pumped fluid out. Replaced NR3 hydro system. - [Incident 19810618041719I](https://openairdocs.org/incident/19810618041719I), Jun 18, 1981: Doug DC1010 (N125AA), Chicago, IL. Compressor stall on number 3 engine as power levers were retaraded. Engine shut down as precautionary. No defect. - [Incident 19800909081809I](https://openairdocs.org/incident/19800909081809I), Sep 9, 1980: Doug DC1010 (N125AA), Chicago, IL. Aborted takeoff due to compressor stalls, flames from tail pipe. Adjusted variable stator vanes,engine checked ok - [Incident 19790105000499I](https://openairdocs.org/incident/19790105000499I), Jan 5, 1979: Doug DC1010 (N125AA), Boston, MA. Aircraft returned to Boston due to inflight engine failure due to pn 3276 - [Incident 19780330011999I](https://openairdocs.org/incident/19780330011999I), Mar 30, 1978: Doug DC10/ (N125AA), Los Angeles, CA. TRACON issued altitude warning to the pilot on approach. He was 7 miles out at 1000 feet. ## Other aircraft with N125AA - [Registered now](https://openairdocs.org/aircraft/N125AA): Airbus A321-231, S/N 6272, built 2014 --- 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.