N155UP
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED PARCEL SERVICE CO. (IPXA) | Operator | 2013-08-14 – 2013-08-14 | Operator named in NTSB report |
| UNITED PARCEL SERVICE CO | Operator | 2013-08-14 – 2013-08-14 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
CAPTAIN`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.
INSPECTION 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.
INSPECTION 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.
FLOORBOARD DAMAGED. FABRICATED NEW FLOOR IAW A300-5320-16407.
INTERMITTENT 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 71-00-00-05.
INSPECTION 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 LANDING, MEDIUM AUTOBRAKES DID NOT WORK. USED MANUAL BRAKES. RR'D TRIPLE BRAKE PRESSURE INDICATOR. OPS CHECKS GOOD. REF AMM 32- 44-19-04; 32-43-00, PG 501; 32-45-00, PG 501.
INSPECTION 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 52-73-00 SCHEM 02 PG 106. FOUND WARNING LIGHT & BUZZER WARNING NORMAL, OK FOR SUBSEQUENT FLIGHT.
INSPECTION 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 LOCK MECH HANDLE.
INSPECTION TYPE:N/A DOOR SLIDE ARMING LEVER PIN RECEPTACLE IS OBSTRUCTED BY 1A PLUG. REMOVED PLASTIC PLUG IAW 52-50-00.
CREW ENTRY DOOR EMERGENCY EXIT LIGHT ASSY HAS TWO LAMPS INOP. RELAMPED, OPS CHECK OK.
ESPU BATT TIMEX. REMOVED AND REPLACED BATTERY IAW 33-51-14.
ON 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 APPROACH INTO EDFH AS WE RAN THE CHECKLISTS FOR NO FLAPS. EXTENDED CORRECTLY ON SCHEDULE. BITE ON SFCC C/O FOUND SATISFACTORY AND T/S C/O IAW AMM 27-54-00-04. AND OPS TEST C/O FOUND ALL SATISFACTORY. OK FOR FURTHER SERVICE.