N362UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
NR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS. INSTALLED NR 1 ENGINE INLET COWL IAW AMM 71-11-01.
NR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS REMOVED #1 ENGINE INLET IAW AMM 71-11-01
EMERGENCY LIGHTS BATTERY DEPLETED. EMERGENCY LIGHTS BATTERY REPLACED BY SERVICEABLE. IAW AMM 33-51-07/401 REV 148. OPERATIONAL TEST C/O O.K.
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:657T1126-57 (REPAIR) THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04. REPAIR IAW B767-300BCF (REV. 49) SRM 53-00-50-2R-0.
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 814T3538-30 (REPAIR) ++ THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04. REPAIR IAW B767-300BCF (REV. 49) SRM 53-00-50-2R-0.
*** SUPPLEMENTAL SDR *** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMOPLISH SDR.
EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) OPEN
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 814T3538-27 (REPLACE) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.142 RESTORED MAIN DECK CARGO HANDLING JOB COMPLETED AND CONDITION CHECK NORMAL
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 814T3538-23 (REPLACE) I.A.W AMM 25-57-05-404-006, AMM 25-58-05-404-052 AND AMM 25-58-01-404-005 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL
FOUND MAIN DECK FLOOR DAMAGE, P/N: 814T3538-30 (REPLACE) THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04. REPAIR IAW B767-300BCF (REV. 49) SRM 53-00-50-2R-0.
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 657T1126-57 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 25-58-04-404-015, AMM 25-57-02-404-016 AND AMM 25-57-06-404-006 REV.142 RESTORED MAIN DECK CARGO HANDLING JOB COMPLETED AND CONDITION CHECK NORMAL
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:814T3538-25 (REPAIR) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL
GEAR DISAGREE - GEAR DOORS ON TAKEOFF - CHECKLIST HAD US BRING GEAR HANDLE UP UNTIL LANDING THEN LANDED NORMALLY. ALL LIGHTS EXTINGUISHED WHEN HANDLE WAS BROUGHT UP. CHECKED ADJUSTMENT OF LANDING GEAR CONTROL SYSTEM IAW. AMM 32-31-00-825-014, REV. 141. LIFTED THE AIRPLANE WITH JACKS IAW. AMM 07-11-01-582-015 REV. 141. PERFORMED EXTENSION AND RETRACTION OF THE LANDING GEAR IAW. AMM 32-32-00 PB 501 REV. 141. NO FAULTS FOUND AND NO ABNORMAL INDICATIONS DURING OPERATIONAL TEST. PRECAUTIONARY PERFORMED LUBRICATION OF MAIN LANDING GEARS AND DOORS IAW. AMM 12-21-14/301 AND AMM 12-21-15/301 REV. 141. LOWERED THE AIRPLANE IAW. AMM 07-11-01-582-017 REV. 141. SYSTEM OK TO CONTINUE. PROPER COMPANY QUALIFIED TO PERFORM THE ABOVE TASK C/O O.K I.A.W GMM REV 07A
GEAR DISAGREE - GEAR DOORS ON TAKEOFF - CHECKLIST HAD US BRING GEAR HANDLE UP UNTIL LANDING THEN LANDED NORMALLY. ALL LIGHTS EXTINGUISHED WHEN HANDLE WAS BROUGHT UP. ACCOMPLISHED PROXIMITY SWITCH ELECTRONICS UNIT TEST IAW AMM 32-09-04-704-013 REV141 UNTIL E STEP F. RESET NOT ACCOMPLISHED. TEST WITHOUT FAULTS.<BR>RAZLAF CRN97067976
**AIR TURNBACK**ON CLB OUT R ENG FUEL FILT EICAS MESSAGE. REPLACED R ENG FUEL FILTER IAW TASK 73-11-02-004-001-H00. FUEL FILTER PN: AC9227F1740 SN: LOT 45731740<BR>PACKING PN: M83248/1-243 SN: LOT 2213-243
INSPECTION TYPE:N/AFOUND EMERGENCY LIGHT AFT U/S.REPLACEMENT OF LAMP PERFORMED IAW AMM 33-51-03 PB201 REV 132.05.
INSPECTION TYPE:PDC UNARMED LIGHT DOESN'T TURN ON WHEN EMERGENCY LIGHT SWITCH IS IN OFF POSITION. CLEANED CONNCETOR D868 AND S1 SWITCH ON M43 EMERGENCY LTS CONTROL PANEL.
AFT CARGO WEB STIFFENER AT BS 1373, RBL 8, DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, RBL 3.5 WAS DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, LBL 33 WAS DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, LBL 8, WAS DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, RBL 38, DAMAGED. REPLACED THE STIFFENER.
ATF CARGO WEB STIFFENER AT BS 1373, RBL 20, WAS DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, RBL 12, WAS DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, LBL 44, DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, LBL 25 DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, LBL 17, DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1373, LBL 3.5 DAMAGED. REPLACED THE STIFFENER.
AFT CARGO WEB STIFFENER AT BS 1371, RBL 30, WAS DAMAGED. REPLACED THE STIFFENER.
THE LOWER, AFT CARGO FLOORBEAM ASSY WAS DAMAGE AT BS 1373. REPAIRED THE FLOORBEAM.
CREW ENTRY DOOR HANDLE EXTREMELY DIFFICULT TO OPERATE, CHECKED RIGGING. DOOR FOUND TO BE OUT OF RIG, 27LBS TO OPEN, 57LBS TO CLOSE. IAW MM 52-12-00-715-119.
FRAME TRANSITION RADIUS FOUND CRACKED FOUND APPROXIMATELY 5/16 INCH IN LENGTH, FOUND DURING HFEC INSPECTION AT BS 883.5, LBL 89, BELOW WL 200. THE FRAME WAS REPAIRED IAW EO B767-5310-69149, APPENDIX B.
A CRACK WAS FOUND APPROXIMATELY 3/8 INCH IN LENGTH IN THE FRAME TRANSITION RADIUS., FOUND DURING HFEC INSPECTION AT BS 903.5, RBL 89, BELOW WL 200. THE FRAME WAS REPAIRED IAW EO B767-5310-69148, APPENDIX B.