N1834U

Cancelled 2002

Deregistered aircraft · 1972 Mcdonnell Douglas DC-10-10 · GE CF6-6 series

Cancelled
June 10, 2002
Status when cancelled
Valid registration
Serial number
47966
Year built
1972
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
November 8, 1972
Certificate issued
May 22, 2000
Last registry action
May 22, 2000
Mode S code
A14EC8
Owner when cancelled
Federal Express Corporation
Location
Memphis, TN
Owner type
Corporation

From the FAA registry file of October 27, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 4

FAA accident and incident reports matched to this aircraft by N1834U and the event date: up to this one’s cancellation.

Service difficulty reports · 10

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

SDR 99UAL900090Tube · leakingSLIDE/RAFT FAILED AIR RETENTION TEST DUE TO SEAM SEPARATION IN TUBE ASSEMBLY. *S/D* SEAM SEPARATION IN INFLATABLE TUBE ASSEMBLY. UNIT IS BEYOND ECONOMICAL REPAIR AND WAS SCRAPPED.Feb 1, 1999 · N1834U · Doug DC1010 · Life RaftSDR 98UAL900573Line · leakingODOR IN CABIN AROUND DOOR 3 AREA ON TAKEOFF, CLIMB AND INTERMITTENTLY IN CRUISE. SMELLS LIKE HOT OIL. REPAIRED HYDRAULIC LEAK NEAR APU INLET, BURNED OUT ALL 3 PACKS. REPLACED ALL 3 COALESCER BAGS. THERE HAVE BEEN NO REOCCURANCES.Nov 25, 1998 · N1834U · Doug DC1010 · Hydraulic System, MainSDR 98UAL900006Structure · damagedFUSELAGE SKIN AND UNDERLYING CIRCUMFERENTIAL FRAMES DAMAGED DURING PUSHBACK. DAMAGE OCCURRED ALONG A HORIZONTAL REFERENCE LINE APPROX 6 INCHES BELOW AND PARALLEL TO THE LOWER EDGE OF THE L1 DOOR CUTOUT. SKIN PANEL BETWEEN STA 304 AND STA 401 BUTT JOINTS AND Dec 17, 1997 · N1834U · Doug DC1010 · Fuselage Main, StructureSDR 97UAL900573Fire Wire · chafedNR 2 FIRE DETECTION LOOP-B LIGHT ON INTERMITTANTLY. *S/D* FOUND CHAFED WIRES ON LOOP-B WIRE HARNESS IN AFT FIREWALL J BOX. REPLACED WIRING AS REQUIRED.Jul 26, 1997 · N1834U · Doug DC1010 · Fire DetectionSDR 97UAL900564Wire · damagedNR 2 N1 WAS 10 PERCENT BELOW NR 1 N1 AND NR 3 N1 WITH THE THROTTLE AHEAD OF NR 1 AND NR 3. NR 2 N2 WAS SAME AS NR 1 N2 AND NR 3 N2. FUEL PRESSURE FOR NR 2 WAS FLUCTUATING BETWEEN 100 TO 120 PSI. RETURN TO SFO. *S/D* FOUND DAMAGED WIRES AND CORRODED CONTACJul 19, 1997 · N1834U · Doug DC1010 · Engine Indicating System WiringSDR 96UAL900651Floorbeam · crackedCRACK IN FLOORBEAM FORWARD CARGO PIT AT STATION 899 APPROXIMATELY 2 FEET FROM LEFT WALL. *S/D* A REPAIR OF STATION 899 FLOORBEAM WAS ACCOMPLISHED.Aug 22, 1996 · N1834U · Doug DC1010 · Fuselage Main, Floor BeamSDR 96UAL900458Skin · corrodedON WALK-AROUND, FOUND FUSELAGE SKIN AT BODY STATION 979 HAD EXTENSIVE CORROSION BETWEEN LONGERONS 44L AND 47L. DAMAGE EXCEEDED SRM ALLOWABLES FOR MATERIAL LOSS. CLEANUP OF CORROSION RESULTED IN A 32.0 INCH BY 8.0 INCH SECTION OF SKIN BEING REMOVED. THE CORRJun 17, 1996 · N1834U · Doug DC1010 · Fuselage Main, Plate/SkinSDR 96UAL900171Slide/Raft · failed testNR 3 RT SLIDE/RAFT REMOVED FOR TIME EXPIRATION. UNIT FAILED THE AIR RETENTION TEST DUE TO LEAKING AROUND THE COMMUNICATOR TUBE. RETURNED UNIT TO MANUFACTURER FOR REPAIR.Mar 6, 1996 · N1834U · Doug DC1010 · Escape SlideSDR 96UAL900044Tee Assy · rupturedUNWANTED FUEL TRANSFER INTO NR 2 MAIN TANK WITH FILL VALVE SWITCH IN CLOSED POSITION AND NR 2 MAIN FILL VALVE LIGHT INDICATING FILL VALVE IS IN CLOSED POSITTION. A WELD FAILED ALLOWING A PRESSURE RELIEF VALVE TO COME OFF THE FUEL MANIFOLD. REPLACED RUPTURED Jan 18, 1996 · N1834U · Doug DC1010 · Aircraft Fuel Distribution SystemSDR 95UAL900133Cooling Assy · packing wornSTRONG OIL SMELL IN AIRCRAFT, BELIEVE COMING FROM APU. REPLACED C-1, STATOR, RING AND COOLING FAN ASSEMBLY.Sep 14, 1995 · N1834U · Doug DC1010 · Airborne Auxiliary Power Unit (APU) System

Other aircraft with N1834U · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N1834U is registered now to the first aircraft listed.