N155UP

Cancelled 2014

Deregistered aircraft · 2004 Airbus A300 F4-622R · Pratt & Whitney PW4158

Cancelled
February 21, 2014
Status when cancelled
Third renewal notice
Serial number
0841
Year built
2004
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
March 24, 2004
Certificate issued
February 13, 2004
Last registry action
March 16, 2010
Mode S code
A0DE92
Owner when cancelled
United Parcel Service Co
Owner type
Corporation

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.

NTSB investigations · 1

Matched to this aircraft by N155UP and the event date: up to this one’s cancellation.

Service difficulty reports · 12

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

SDR IPXA12173590Adc · inoperativeCAPTAIN`S AIRSPEED WENT TO 80 KNOTS, F/O WENT TO ZIPPER CAPTAIN`S ALT REMAINED CORRECT F/O ALT WENT 300' HIGH YAW DAMPER CLICKED OFF. NO FLAGS OR ECAM WARNINGS. EMERGENCY DECLARED. REPLACED NR 1 ADC IAW MM 34-11-34-04.May 15, 2012 · N155UP · Airbus A300F4622R · Air Data ComputerSDR IPXA11167505Skin · damagedINSPECTION TYPE:3C, FUSELAGE SKIN DAMAGE AT FR 84 TO FR 86 AT STR 44L TO STR 45L TAPE APPLIED. ACCOMPLISHED REPAIR ON FUSELAGE SKIN AT FR84 TO FR 86 STR 44L TO STR 45L IAW SRM 53-10-12, FIG 210.Jun 11, 2011 · N155UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA11167450Floorboard · puncturedINSPECTION TYPE:3C, DEFERRAL ITEM D-452781 TEMP REPAIR TO HOLE IN BULK PIT FLOOR AT FR 66 TO FR 67 28 IN LT OF CENTERLINE. FABRICATED BULK CARGO FLOORBOARD NR161GF IAW EO A300-5320-16407-E, APPENDIX D.Jun 11, 2011 · N155UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA09158033Floor Panel · damagedFLOORBOARD DAMAGED. FABRICATED NEW FLOOR IAW A300-5320-16407.Dec 27, 2009 · N155UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA09157344Pressure Switch · smokeINTERMITTENT ENGINE OIL LOW PRESSURE LIGHT. CREW HEARD LOUD POP OVER COCKPIT SPEAKER FOLLOWED BY AND AFT BULK CARGO SMOKE INDICATION. EMERGENCY DECLARED. REPLACED NR 1 ENGINE LOW OIL PRESS SWITCH PER MM 79-34-11-04. RAN ENG LEAK AND OPS CKD OK PER MM 71-00-00-Sep 11, 2009 · N155UP · Airbus A300F4622R · Engine Oil Indicating SystemSDR IPXA09157281Indicator · faultyINSPECTION TYPE:N/A AFTER LANDING GEAR EXTENSION, THE RESIDUAL BRAKE PRESSURE ON THE LEFT GAUGE INDICATED ABOUT 2500-3000 PSI. CYCLED THE LANDING GEAR - DUAL PR PRESSURE SHOWED ABOUT 200-250 PSI. PUMPED THE BRAKE PEDALS AND SELECTED MEDIUM AUTOBRAKES. UPON Sep 4, 2009 · N155UP · Airbus A300F4622R · Landing Gear Brake SystemSDR IPXA09156927Warning System · false activationINSPECTION TYPE:N/A CABIN OVER PRESSURE HORN LOCATED ON MAIN ENTRY DOOR SOUNDS CONTINUOUSLY. ALL DOOR PRESSURIZATION READINGS NORMAL. PERFORMED EMERGENCY ESCAPE SLIDE RELEASE AND RESIDUAL PRESSURE WARNING ADJ/TEST PROCEDURE IAW AMM 52-73-00-05 AND ASM 52-73-Aug 3, 2009 · N155UP · Airbus A300F4622R · Cabin Pressure Control SystemSDR UPS09154529Arm · unknownINSPECTION TYPE:N/A MAIN CREW ENTRY DOOR WILL NOT SHUT OR LOCK. INSTALLED 2 CONNECTING ARMS AND 2 PINS. CYCLED DOOR LOCK MECHANISM, OPS NORMAL. PERFORMED INSPECTION PER 52-10-20-06 AND OPS CHECK PER 52- 10-20-05. INSPECTED AND OPS CHECK NORMAL OF OUTSIDE LFeb 3, 2009 · N155UP · Airbus A300F4622R · Passenger/Crew DoorsSDR UPS09154429Arming Lever · obstructedINSPECTION TYPE:N/A DOOR SLIDE ARMING LEVER PIN RECEPTACLE IS OBSTRUCTED BY 1A PLUG. REMOVED PLASTIC PLUG IAW 52-50-00.Jan 24, 2009 · N155UP · Airbus A300F4622R · Emergency ExitsSDR UPS06148342Light · inoperativeCREW ENTRY DOOR EMERGENCY EXIT LIGHT ASSY HAS TWO LAMPS INOP. RELAMPED, OPS CHECK OK.Oct 22, 2006 · N155UP · Airbus A300F4622R · Emergency LightingSDR UPS06146143Battery · inoperativeESPU BATT TIMEX. REMOVED AND REPLACED BATTERY IAW 33-51-14.Feb 11, 2006 · N155UP · Airbus A300F4622R · Emergency LightingSDR UPS06146089Flap System · failedON APPROACH TO CGN, FLAPS W/N EXTEND PAST 15. A/C DIVERTED. EMERGENCY DECLARED. UPON APPRIVAL AT EDDK THE SLATS EXTENDED FULLY AND THE FLAP GAUGE INDICATED LESS THAN 15 FLAPS. WE SEQUENCED THE FLAP HANDLE THROUGH AGAIN GETTING THE SAME INDICATIONS. ON APPROACHFeb 1, 2006 · N155UP · Airbus A300F4622R · Trailing Edge Flap Control System