N166AA

Cancelled 2002

Deregistered aircraft · 1973 Mcdonnell Douglas DC-10-10 · GE CF6-6 series

Cancelled
June 10, 2002
Status when cancelled
Valid registration
Serial number
46908
Year built
1973
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 19, 1973
Certificate issued
July 19, 1999
Last registry action
July 19, 1999
Mode S code
A107F9
Owner when cancelled
Federal Express Corp
Location
Memphis, TN
Owner type
Corporation

From the FAA registry file of October 28, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 3

FAA accident and incident reports matched to this aircraft by N166AA and the event date: up to this one’s cancellation.

Service difficulty reports · 15

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR AALA971396Hyd Fuse · crackedSFO - FLT 682 - AFTER TAKEOFF SFO DURING CLIMB-OUT WITH LANDING GEAR RETRACTED, LOST HYDRAULIC SYSTEM 3. ACCOMPLISHED ABNORMAL PROCEDURES, DUMPED FUEL, AND AIRCRAFT RETURNED TO SFO LANDING WITHOUT INCIDENT. REPLACED TRIM CYLINDER INTERLOCK FUSE. SERVICED HYAug 1, 1997 · N166AA · Doug DC1010 · Hydraulic System, MainSDR AALA970984Longeron · corrodedTUL - DEEP CORROSION ON LONGERON FROM SPLICE AT STATION 1109 TO STATION 1156. REMOVED AND INSTALLED NEW LONGERON 48L AS PER SRM 51-00-00 PAGE 5 SPLICED FRAME TO FACILITATE LONGERON INSTALLATION AS PER 53-30-00 PAGE 5. (M)May 26, 1997 · N166AA · Doug DC1010 · Fuselage Main, Longeron/StringerSDR AALA970983Angle · corrodedTULE - Z-ANGLE CORRODED STATION 1641-1661. SPLICED IN NEW SECTION OF 2 CHANNEL AND INSTALLED PER AARD 51-01-00 PAGE 05. (M)May 26, 1997 · N166AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970982Channel · corrodedTUL - 2-CHANNEL HAS CORROSION FROM STATION 1521-1701 LEFT. SPLICED IN NEW SECTION OF 2 CHANNEL AND INSTALLED PER AARD 51-01-00 PAGE 05. (M)May 26, 1997 · N166AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970987Casting · corrodedTUL - CORROSION IN TWO LOWER HOLES OF NR 2 LATCH BRACKET MOUNT CASTING FOR AFT CARGO DOOR. REMOVED CORROSION AND INSTALLED BUSINGS PER SRM 53-50-00 PAGE 81. (M)May 24, 1997 · N166AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970988Door Frame · corrodedTULE - DOOR FRAME CORRODED AT STATION 1705 LOWER FORWARD CORNER. INSTALLED REPAIR ANGLE PER ESO 7349 DATED 5-14-97. (M)May 23, 1997 · N166AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970962Floor Beam · damagedTUL - REPAIRS DUE TO CORROSION DAMAGE ON FLOOR BEAM, MORE CORROSION FOUND ON C-V. REMOVED AND REPLACED FLOOR BEAM IAW SRM 53-00-01. TST: 81,156 HOURS. CYCLES: 24,004. (X)May 21, 1997 · N166AA · Doug DC1010 · Fuselage Main, Floor BeamSDR AALA970999Angle · corrodedTUL - CORROSION WAS FOUND ON VERTICAL CAP ANGLE IN LT MLG WW. REMOVED ANGLE AEA0474-1. INSTALLED NEW ANGLE AEA0474-1 IAW SRM VOL 1 51-00-00 PAGE 2. (M)May 20, 1997 · N166AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970932Skin · dentedTUL - TWO DENTS BETWEEN STA 1721 AND STA 1701 OUT OF LIMITS REF: ADL 0032 AT 36 LT LONGERON FORWARD OF AFT CARGO DOOR. INSTALLED CLASS I PERMANENT REPAIR PER SRM 53-20-00 FIG 6. TST: 81,156.07 HOURS. CYCLES: 24,004. (X)May 19, 1997 · N166AA · Doug DC1010 · Fuselage Main, Plate/SkinSDR AALA970927Splice · corrodedTUL - LONGERON SPLICE PLATE CORRODED AT 48R STA 1718. REMOVED OLD PLATE, CLEANED AREA, TREATED, AND PRIMED. INSTALLED NEW SPLICE FITTING. TST: 81,156.07 HOURS. CYCLES: 24,004. (x)May 16, 1997 · N166AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970913Structure · corrodedTUL - STRUCTURE CORRODED IN AREA FWD OF BATTERY, LIGHT CORROSION ON SKIN. INSTALLED NEW LONGERONS 52, 51L, 51R. NEW SUPPORT FOR BATTERY BOX. SPLICED FRAME BETWEEN 48L AND 48R. REMOVED LIGHT CORROSION ON SKIN. TST: 81,156 HRS. CYCLES, 24,004. (X)May 16, 1997 · N166AA · Doug DC1010 · Fuselage Main, StructureSDR AALA970907Shear Tie · corrodedTUL - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE BETWEEN LONGERON 47R AND LONGERON 48R INSIDE AFT CARGO COMPARTMENT AT STA 1784. REMOVED AND REPLACED SHEAR TIE PER SRM 51-21-01, VOL II, AND SRM 51-31-01, VOL II. TST: 81,156.07 HRS. CYCLES, 24,004. (X)May 14, 1997 · N166AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA970906Angle · corrodedTUL - CORROSION FOUND ON Z-ANGLE FROM STA 1561 TO STA 1600. SPLICED IN NEW SECITON PER SRM 53-00-01. TST: 81,156 HRS, CYCLES, 24,004. (X)May 14, 1997 · N166AA · Doug DC1010 · Fuselage Miscellaneous StructureSDR AALA960908Bulkhead Tee · crackedTUL - DURING C-CHECK, FOUND CRACK IN FS 1156 BULKHEAD RIGHT TEE CAP INBOARD OF FIFTH FASTENER IN THE LOWER ROW OF FASTENERS FROM THE OUTBOARD END. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO 7349 DATE 5-14-97 AND SRM 51-35-01 VOL II, SRM 51-21-01, VOL IIJul 15, 1996 · N166AA · Doug DC1010 · Fuselage Main, BulkheadSDR AALA950415Eel Wire · brokenJFK - FLT 678 - DURING APPROACH, EMERGENCY FLOOR LIGHTS AT RT BETWEEN R1 AND R3 DOORS ILLUMINATED. ACFT LANDED JFK WITHOUT INCIDENT. REPAIRED BROKEN/SHORTED WIRING FROM AM1 TO 8. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)Mar 7, 1995 · N166AA · Doug DC1010 · Emergency Lighting

Other aircraft with N166AA · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N166AA is registered now to the first aircraft listed.