N364UP
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
23 reports on file, 2018-06-11 – 2024-09-06.
Part: SEAL DEPRESSOR — DEFORMED (ZONE 200) · airframe 51,140 hrs · 18,057 cycles
DEFORMED DEPRESSOR SEAL, MAIN DECK CGO DOOR AFT CUTOUT AREA. (REPLACE). INSTALLED DEPRESSOR SEAL, I.A.W AMM 20-11-00-910-802 REV.142.
Part: ANGLE — CRACKED (ZONE 100) · airframe 51,140 hrs · 18,057 cycles
FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 RBL 80 INBOARD (REPLACE). FABRICATE P/N: 657T1338-6 PER BOEING DWG NO: 657T1338 SH. 3 REV."-"; PL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV. 7C REQUIREMENT AND EGAT WORK SHEET NO. 40819. INSTALL FABRICATED PART I.A.W SRM 51-40-02-0G REV. 50 AND BOEING DWG NO: 657T1332 SH. 5 REV. A. JOB COMPLETED.
Part: ANGLE — CRACKED (ZONE 100) · airframe 51,140 hrs · 18,057 cycles
FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD. (REPLACE). I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
Part: ANGLE — CRACKED (ZONE 100) · airframe 51,140 hrs · 18,057 cycles
FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD. (REPLACE). I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
Part: DRAIN — NO DISCREPANCY (ZONE 100) · airframe 51,140 hrs · 18,057 cycles
*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) C/W EO 8217. COMPLETED SDR.
Part: DRAIN — NO DISCREPANCY · airframe 51,140 hrs · 18,057 cycles
*SDR FILED OPEN* FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.
Part: ANGLE — CRACKED (ZONE 100) · airframe 51,140 hrs · 18,057 cycles
FOUND BULK CARGO COMPARTMENT LEFT AREA ANGEL CRACK AT STA 1578 LBL 80 INBOARD (REPLACE). FABRICATE P/N: 657T1338-5 PER BOEING DWG NO: 657T1338 SH.3 REV."-"; PL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV. 7C REQUIREMENT. INSTALL FABRICATED PART I.A.W SRM 51-40-02-0G REV. 50 AND BOEING DWG NO: 657T1332 SH. 5 REV. A.
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 51,140 hrs · 18,057 cycles
FOUND MAIN DECK FLOOR PANEL DENT, P/N: 814T3538-65. (REPAIR). I.A.W AMM 53-01-06-400-801 REV 142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 51,140 hrs · 18,057 cycles
FOUND MAIN DECK FLOOR PANEL DENT, P/N: 814T3538-23. (REPAIR). I.A.W AMM 53-01-06-400-801 REV 142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 51,140 hrs · 18,057 cycles
FOUND MAIN DECK FLOOR PANEL DENT, P/N: 814T3538-16. (REPAIR). I.A.W AMM 53-01-06-400-801 REV 142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 51,140 hrs · 18,057 cycles
FOUND MAIN DECK FLOOR PANEL DENT, P/N: 814T3538-28. (REPAIR). I.A.W AMM 53-01-06-400-801 REV 142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
Part: WARNING MESSAGE — FALSE INDICATION (LE FLAP SYS) · airframe 50,934 hrs · 17,914 cycles
AIR TURN BACK* LE SLA ASYMMETRY AFTER TAKEOFF: AIR TURN BACK TO VIENNA CARRIED OUT SLAT #8 WEAR LIMIT CHECK PER AMM TASK 27-81-02-226-001 AND WEAR LIMIT CHECK FOR #8 SLAT TRACK PER AMM TASK 27-81-34-226-002. NO FINDINGS. FURTHER PERFOMRED INDUCTANCE / RESISTANCE CHECK OF ALL SLAT SENSORS. MEASURMENTS WITH BREAKOUT BOX IAW AMM 32-09-13/501. ALL RESULTS WITHIN LIMITS. SEE ATTACHAMENT FOR VALUES. PER TECHSUPPORT REQUEST CHECKED ACP MIC SWITCH LIGHTS FOR FLICKERING DURING RUDDER TRIM OPERATION. NO FINDINGS. OPERATED FLAPS / SLATS SEVERAL TIMES WITH ADP AND WITHOUT ADP IAW AMM 27.81-00 UNABLE TO REPRODUCE LE SLAT MESSAGE ON GROUND. AIRCRAFT OK TO CONTINUE.
Part: DRIVE ASSY — LACK OF LUBE (SLAT SYSTEM) · airframe 50,925 hrs · 17,907 cycles
EMERGENCY DECLARED, ON CLIMBOUT, RETRACTING FLAPS, THE 'LE SLAT ASSYMMETRY' EICAS MSG ILLUMINATED AND FLAP IND WAS BETWEEN UP & 1. IT MOMENTARILY CLEARED AD FLAP NEEDLE WENT TO 'UP'. THE EICAS MSG RETURNED AND NEEDLE... OPENED ACCESS PANELS, CLEANED SLAT DRIVE MECHANISM AND LUBRICATED SLAT #8 AND #9 . CLOSED PANELS. DURING CLOSING REPLACED SEVERAL SCREWS IAW AMM 12-21-080-600-803 REV 142.
Part: PROXIMITY SENSOR — INOPERATIVE (TE FLAPS) · airframe 50,927 hrs · 17,908 cycles
ON CLIMBOUT, RETRACTING FLAPS, THE 'LE SLAT ASSYMMETRY' EICAS MSG ILLUMINATED AND FLAP IND WAS BETWEEN UP & 1. IT MOMENTARILY CLEARED AD FLAP NEEDLE WENT TO 'UP'. THE EICAS MSG RETURNED AND NEEDLE... LEADING EDGE SLAT SENSOR SWITCH OPERATIONAL TEST C/O SEVERAL TIMES IAW AMM 27-88-00-715-098 REV. 142. NO FAULTS ON PSEU, NO EICAS MSG. TEST SATIS.
Part: WARNING MESSAGE — ILLUMINATED (SLAT ASYM) · airframe 50,762 hrs · 17,789 cycles
*EMERGENCY DECLARED* LE SLAT ASYM ON DEPARTURE FROM VCE FIM 27-51 FAULT TREE 809 C/OUT EXISTING FAULT PRESENT NO FAULT HISTORY FAULT ON FLIGHT "0" AND "-8" "TE FLAP" SEE FIM "27-51104" IAW TABLE A "FLAP DISAGREE IND. BUT BITE CANNOT IDENTIFY THE SPECIFIC FAULT. FLAP/SLAT EXTENCION RETRACTION PERFORMED SEVERAL TIME AS NO FAULT IN NORMAL "HYD" AND ALTERNATE "ELECTRIC"MODE. AMM 27-81-00/201
Part: WINDOW — ARCED (L1) · airframe 50,490 hrs · 17,564 cycles
CAPT WINDOW SHATTERED DUE TO ARCING. REMOVED AND REPLACED L1 WINDOW IAW AMM 56-11-01/401. REMOVED AND REPLACED WHCU M191 IAW AMM 30-41-01/401, NO FAULTS NOTED.
Earlier reports · 2018–2023 · 7 reports
2023
Part: SLAT SYSTEM — INOPERATIVE (UNKNOWN) · airframe 50,345 hrs · 17,457 cycles
**EMERGENCY DECLARED**LE SLAT ASYMMETRY AT FL150. SPEED BRAKES EXTENDED. RAN CHECK LIST LANDED NOT SLATS/FLAPS 30 DEGREES. FIM 32-09 FAULT TREE 803 BLOCKS1, 2,3,4,14A,37,7,8. SENSOR S298 FAULT SHOWN INTIALLY. UPON INSPECTION FOUND SENSOR TO BE DIRTY AND OBSCURED. SENSOR S298 CLEANED AND PSEU ON GROUND SYSTEM TEST PERFORMED WITH NO FAULTS. FLAPS/SLATS CYCLED VARIOUS TIMES WITH NO FAULT. LE SLAT ASSYMETRY B LEVEL MESSAGE NO LONGER SHOWN. OK FOR SVC.
2022
Part: SKIN — CRACKED (FUSELAGE SKIN) · airframe 49,052 hrs · 16,446 cycles
INSPECTION TYPE:C9CRACK ON RH FUSELAGE SKIN AFT OF STA 1725.5 BUTT SPLICE AT S-7R.REPAIR I.A.W BOEING SR:3-5432213643, 767-300BCF SRM 53-80-01 REPAIR 5, DETAIL III, REV 44.00 AND UPS EO B767-5330-24301-L APPC C.
2020
Part: SKIN — CRACKED (BS 1654) · airframe 46,932 hrs · 14,687 cycles
INSPECTION TYPE: C8 CRACK FOUND ON FUSELAGE SKIN AT STA 1654.5 S-13 AR. REPAIR, IAW BOEING SR 4-4884706014, 767-300BCF SRM 53-80-01 REPAIR 7, REV 38 AND UPS EO B767-5330-78006-A.
2019
Part: THRUST REVERSER — INOPERATIVE (RT ENGINE) · airframe 46,102 hrs · 13,928 cycles
INSPECTION TYPE:ETOPUPON LANDING RIGHT THRUST REVERSER FAILED TO DEPLOY. AMBER REV ILLUMINATED.ACCOMPLISHED OPS TEST OF RH THRUST REVERSER IAW AMM 78-31-00 PB 201 REV 128.06. FOUND SATIS WITHOUT FAULTS. SYSTEM OK TO CONTINUE. ROTHE CGN3738.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,874 hrs · 13,712 cycles
INSPECTION TYPE:N/A FOUND SEVERAL EMERGENCY LIGHTS INOP. NEW LAMPS INSTALLED. TEST SATIS IAW AMM 33-51-00 REV 127.04.
2018
Part: STRINGER — CRACKED (RT WING) · airframe 45,217 hrs · 13,121 cycles
INSPECTION TYPE:SV, ONE CRACK WAS FOUND ON THE RT WING UPPER STRINGER U-19 (PN 112T3319-4) AT WS 616.2. REPAIR IAW SRM 57-00-03 REPAIR 1, REV 32.00 2.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 45,217 hrs · 13,121 cycles
INSPECTION TYPE:SV, ONE CRACK WAS FOUND IN THE FUSELAGE STRINGER (PN 143T3001-433) AT STA 478, S-32LREPAIR IAW SRM 53-00-03 REPAIR 2, REV 31.00.