N576UP
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
MAIN DECK CRASH AXE FOUND DAMAGED/CORRODED REINSTALLED CRASH AXE INTO HOLDER ON MAIN CARGO DECK IAW AMM 25-60-00.
ENG 3 FIRE INDICATION FOR 20-30 SEC, WENT OUT. DIVERTED TO HKG, REPLACED NR 3 ENG LOWER AFT FIRE LOOP ASSY (TS682) IAW AMM 26-11-02/401 AND PERFORMED FIRE SYSTEM GROUND TEST IAW AMM 26-11-00/501 RESULT PASS.
FOUND THE UPPER DECK AISLE EMERGENCY LIGHT M4915 AND L5733 INOPERATIVE.
FOUND THE UPPER DECK AISLE EMERGENCY LIGHT M4915 AND L5733 INOP. I.A.W AMM 33-51-04-902-001-001 REV.114 REPLACED EMERGENCY LIGHT BATTERY (M5169) AT UPPER DECK SIDEWELL & PERFORMED EMERGENCY LIGHT (M4915 L5733) TEST, RESULT WAS SATISFACTORY.
DURING PERFORM EO-26856-JIC001 FOUND FASTENER HOLE CRACK AT STA 740 R/H SIDE. REPAIR DAMAGE AREA IAW UPS EO-94857-REQ1 REV.1 2.
DURING PERFORM EO-26856-JIC001 FOUND FASTENER HOLE CRACK AT STA 720 L/H SIDE. REPAIR DAMAGE AREA I.A.W. UPS EO-94856-REQ1 REV.1 2.
L1 DOOR EMERGENCY LIGHT L1854 INOP RELAMPED L1854 REFERENCE AMM 33-51-05-962-031. OPS CEHCK GOOD
LH INBOARD ELEVATOR DENTED ACCOMPLISHED PERMANENT REPAIR SEE TASK NUMBER FOR DETAILS T3F18E006RAL6. MAJOR REPAIR. COMPLETED PERMANENT REPAIR AND C/W STREPS 1-11 IAW EO-91370-REQ5. THIS CLEARS DEFERRAL.
DURING PS-1 FOUND SEVERAL EMERGENCY LIGHTS WITHOUT FUNCTION. PLEASE INVESTIGATE. FOUND LIGHTS L1853, L1854 AND L5735 WITHOUT FUNCTION. REPLACED AND TESTED EMERGENCY LIGHT BATTERY PACK M5170 IAW AMM 33-51-04-902-001-001 REV.110. FOUND SATIS.
FOUND L1 DOOR AFT SIDE NOT FLUSH WHEN CLOSED, DOOR JAMMED, EXCESSIVE FORCE TO OPEN, SUSPECT DOOR OUT OF RIG. PICTURES ATTACHED ADJUSTED LOWER L1 DOOR HINGE FITTING IAW 747AMM 52-11-01. OPS CHECK AND FIT OF DOOR OPERATION GOOD IAW 747 AMM 52-11-00.
FAULT- BEARING , NO.1 MAIN ENTRY FREIGHTER DOOR LATCH LH LOWER TORQUE TUBE , TOTAL:1EA.(REPLACE) OK TO WORK
*SUPPLEMENTAL SDR* FAULT - WORN - WEAR STRIP, NO.1 MAIN ENTRY DOOR LH CUTOUT MID HANDLE LATCH MECHANISM GUIDE (REPLACE). 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV 98 2. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV 98 AND BOEING DWG NO: 69B12975 SH 1 REV: B 3. JOB COMPLETED. REVIEWED
FAULT- BEARING , NO.1 MAIN ENTRY FREIGHTER DOOR LATCH LH LOWER TORQUE TUBE , TOTAL:1EA.(REPLACE) I.A.W AMM 52-11-01-735-080 REV 108 REPLACED L1 ENTRY DOOR LATCH ROLLER BEARING AND CONDITION CHECK NORMAL. C/W REVIEW
FAULT- WORN - BEARING , NO.1 MAIN ENTRY FREIGHTER DOOR LATCH RH UPPER TORQUE TUBE , TOTAL:1EA.(REPLACE) I.A.W AMM 52-11-01-735-080 REV 108 REPLACED L1 ENTRY DOOR LATCH ROLLER BEARING AND CONDITION CHECK NORMAL. C/W REVIEW
*** SDR FILED OPEN *** FAULT- WORN - BEARING , NO.1 MAIN ENTRY FREIGHTER DOOR LATCH RH UPPER TORQUE TUBE , TOTAL:1EA.(REPLACE) OK TO WORK
*** SDR FILED OPEN *** FAULT - WORN - WEAR STRIP, NO.1 MAIN ENTRY DOOR LH CUTOUT MID HANDLE LATCH MECHANISM GUIDE (REPLACE) OK TO WORK
EMERGENCY LIGHTS WILL NOT TURN OFF WHEN SWITCH IN OFF POSITION, ARM AND ON NORMAL. REPLACED S7 SWITCH ON ASSY 285U0230-13 X1081 FLIGHT ATTENDANT PANEL IAW CMM 31-17-90, WDM 33-51-71, SWPM 20-83-11. OPS CHECK GOOD IAW B747-400 AMM 33-51-00-735-014.
INSPECTION TYPE:NADOOR F\D OVHDFOUND LOCK HANDLE SLIGHTLY OUT OF POSITION, CYCLED HATCH OPEN / CLOSED SEVERAL TIMES, MSG SE;F ERASED. OK PER AMM 52-21-00
INSPECTION TYPE: 18FO FOUND U/D AISLE EMERGENCY LIGHT INOP. REPLACED THE U/D AISLE EMERGENCY LIGHT BATTERY ASSEMBLY M5168, AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST, RESULT WAS SATISFACTORY IAW AMM 33-51-04-902-001-001 REV 100.02.
INSPECTION TYPE: N/A ATB NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. IAS DISAGREE ALT DISAGREE AND STELL WARNING PLI SHOWED IN CAPTAINS FD STICK SHAKER WAS ON FOR ENTIRE FLIGHT IAS DISAGREE CHECKLIST WAS RAN. REMOVED AND REPLACED THE DAMAGED LEFT AOA VANE, IAW AMM 34-12-03-404-148. OPERATIONS CHECK GOOD. ESR: IPC 34-12-03-01-020J.
INSPECTION TYPE:N/AFLOOR PANEL PUNCTURED AT STA 1950LEFTREPAIRED DAMAGED PANEL PER SRM 53-00-50-2R-1
INSPECTION TYPE:C1CRACK WAS FOUND ON INNER SKIN OF FLAP PANEL(P/N:65B39205-72)OF #16 KRUGER FLAP T/E AREA,ILES 625.REPAIR I.A.W. 747-400F SRM 57-43-02 REPAIR 1 AND 51-70-08 REPAIR GENERAL REV. 86.02.
INSPECTION TYPE:NA**EMERGENCY DECLARED** ENCOUNTERED MODERATE INTERMITTENT SEVERE TURBULANCE FOR APPROX 60 SEC. FL 400 M. 83S A/C WT APPROX 497.0 LNAV DISENGAGED. AUTO PILOT REMAINED ENGAGED MOMENTARY STICK SHAKER 2-3 TIMES.C/W AIRPLANE COND INSP PER AMM 05-51-03-201 AFTER MOMENTARY STICK SHAKER AND CHK COND SATIS.
INSPECTION TYPE:N/A FACE SHEET MISSING 1"X.5" FROM FLOORBOARD STAT 1300 RBL 90. REPAIRED IAW SRM 53-00-50 2R-1. ALL WORK RECORDED ON NRC#167347. 5-11-19-1195530. ALL WORK COMPLETED ON NRC. THIS CLEARS D654156
DURING REPLACEMENT OF THE RT BODY GEAR ALT UPLOCK SENSOR. FOUND PRI SENSOR HEAD BROKEN. TROUBLESHOT IAW FIM 32-61 TASK 898 & 878. RIGHT BODY GEAR PRI SENSOR FAULT, SWAPPED RT BODY GEAR PRI UPLOCK SENSOR FROM RT BODY GEAR ALT UPLOCK SENSOR S1637, REPLACED THE RT BODY GEAR UPLOCK SENSOR & CMC PSEU TEST PASSED IAW AMM 32-61-11/201, AND AMM 32-09-03/501.
CRASH AXE DAMAGED. REMOVED AND REPLACED THE CRASH AXE AND SHEATH IAW AMM 25-60-00.
CARGO SMOKE CURTAIN TORN. REPAIRED THE SMOKE CURTAIN IAW AMM 25-59-00-308-036.
SMOKE CURTAIN AT BS 700 TORN AND MISSING FASTENERS. REPAIRED SMOKE CURTAIN IAW AMM 25-59-00-308-036.
AIR TURNBACK, LOSS OF HYDRAULIC SYSTEM NR 4. CHECKED THE NR 4 ENG CASE DRAIN DPI NOT POPPED, AND REPLACED EDP AND ADP CASE DRAIN FILTER, NO METAL CHIP IAW AMM 29-11-18, 29-11-00, REPLACED THE LT WING MLG DOWN LOCK ACTUATOR, SERVICED HYD SYS 1, 2, 3, 4 CONDITION NORMAL, CHECKED, NO LEAK FOUND, NO FAULT FOUND IAWAMM 32-32-15, AND AMM 12-12-01.
SUPERNUMERARY AREA EMERGENCY DECENT CONTAINER WILL NOT STAY CLOSED. REPLACED WORN HOOK AND LOOP IAW AMM 25-61-00.
NR 2 ENGINE FAN VIBRATION, AUTO DISPLAYED. OCCURRED AFTER TAKE OFF, STABLE CRUISE THRUST SETTING. TROUBLESHOT IAW FIM 71-00-00-101, FIG 118, NOTE 1, WITHIN LIMITS, OK FOR SERVICE
INSPECTION TYPE: 18FO, UPPER DECK EMERGENCY LIGHTS L1533, L5733 , L5767 AND M4915 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY (M5169) IAW AMM 33-51-04-902-001-001 REV.89.01, AND PERFORMED EMERGENCY LIGHT TEST, RESULT WAS SATISFACTORY.
EMERGENCY LIGHTS AT THE L1 DOOR ARE INOPERATIVE. REPLACED THE BULBS. OPS CHECKED GOOD IAW AMM 31-51-05-962-031.
PERFORMED THE FIRE, OVERHEAT TEST. THE TEST FAILED. ALL MN DECK DETECTORS FAILED. TROUBLESHOT AND FOUND ON FIRE TEST SWITCH ON THE OVERHEAD PANEL M7317 HAD ONE PIN NOT CONNECTED. R & R THE SWITCHING MODULE M7317 IAW AMM 26-10-02-4, REV 89.00. OPS CHECKED GOOD.
MCD NR 11 FWD THIRD ROW FROM THE LEFT FLOOR PANEL CRACKED AND DELAMINATED. FABRICATED NEW PANEL IAW EO B747-5320-42648-A.
LIFE RAFT UNPACKED. R & R LIFE RAFT IAW AMM 25-62-01.
INSPECTION TYPE:D1, DURING D1, PLUS C1 CHECK OF DATUM ACFT, BROKEN AND DENT WERE FOUND ON THE SKIN BS 2595, BETWEEN STRINGERS 38 - 42R. REPAIRED IAW SRID 4-3117883658, AND EO B-747-5330-59589-A.
DENT WAS FOUND ON THE INTERCOSTAL, AT BS 2108, LBL 7.625. REPAIR IAW SRID 4-3124562467, AND EO B747-5310-59635-A.
FOUR SUPERNUMERARY GOGGLES ELASTIC BANDS STRETCHED, UNUSEABLE. REPLACED THE SMOKE GOGGLES IAW MM 25-00-00 .
NR 1 EA, RT SUPERNUMERARY LIFE VEST STORAGE BAG TORN. REPLACED RT SUPERNUMERARY LIFE VEST AS NEEDED, REF MM 25-60-00, EFF SOURCE REF IPC 25-62-51-010.
HYD INDICATION .69 ON HYD SYS NR 4 AT THE DIRECTION OF THE COMPANY. R & R QTY TRANSMITTER IAW AMM 29-33-01-401. OPS TEST PASSED.
FWD BULB IN EMERGENCY EXIT LIGHT ON MAIN CARGO DECK CEILING INOPERATIVE, JUST INSIDE MAIN ENTRY DOOR, FWD OF CREW STAIRS. REPLACED THE BULB IAW AMM 33-51-02.
IN FLIGHT DECK, EMERGENCY DESCENT DEVICE COMPARTMENT IS MISSING SCREWS TO SECURE IT. INSTALLED REQUIRED FASTENERS. OK FOR SERVICE.
RT INBD AFT FLAP T/E WEDGE HAS A PUNCTURE IN INNER SKIN APPROX 10 FT FROM INBD EDGE. REPAIRED IAW EO B747-5750-53442-A.
LEFT INBD AFT FLAP HAS 2.5 INCH DENT IN LOWER SKIN 11 INCHES FROM OTBD EDGE. REPAIRED IAW EO B747-5750-53443-A.
MAIN DECK CTR FLOOR PANEL AT BS 1440, DAMAGED. REPAIRED IAW SRM 51-00-50-2R1.
HOLE IN FLOOR PANEL BS 1786. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-51433-A.
FLOOR PANEL, BS 1740-1840, LBL12-33 HAS TWO AREAS OF DAMAGE, FABRICATED NEW FLOOR PANEL IAW EO B747-5320-51434-A.
MCD FLOOR PANEL, BS 2064 DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-51435-A.
FLOOR PANEL, BS 2200, POS 18R PUNCTURED. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-51432-A.
AFT EMERGENCY LIGHT IN DOOR FRAME OF L1 DOOR INOPERATIVE. REMOVED & REPLACED BULB. OPS CHECKED OK IAW AMM 33-51-05.
MAIN CARGO DECK FLOORBOARD ON RT OTBD SIDE HAS SMALL HOLE, BS 1690. REPAIRED REF SRM 53-00-50-2R-1.
INSPECTION TYPE: C03, DURING C03 CHECK OF DATUM ACFT, TWO INCHES LONG CRACK DAMAGE WAS FOUND ON THE FRAME AT BS 2696.18, WL 292. REPAIR IAW EO B747-5310-49695-A AND SR:1-2407977602.
RT INBD T/E FLAP WEDGE HAS .5" HOLE. REPAIRED IAE EO B747-5750-48934-B.
FUSELAGE SKIN DAMAGED AT BS 2000 STR 42RT BELOW BULK PIT DOOR. REPAIRED IAW EO B747-5330-48290-D.
LT INBD FLAP T/E DAMAGED. REPAIRED IAW EO B747-5750-48492-A.
RT WING INBD AFT FLAP LOWER SKIN DENTED. REPAIRED IAW EO B747-5750-48266B.
BS 300 LT FLOOR PANEL DAMAGED, REF D486097, REPAIRED DAMAGED FLOOR PANEL IAW SRM 53-00-50-2R-1.
MAIN CARGO DECK FLOOR PANEL DAMAGED. LT BS 1740 AND 1790 (1 PANEL). FABRICATED NEW FLOOR PANEL IAW DWG 146U5817-15.
SKIN HAS A DENT AND GOUGE AT APROX 16.75" AFT OF LOWER FWD CARGO DOOR CUTOUT AND .75" BELOW SKIN LAP JOINT. FOUND CRACK AT DENT, CUT OUT DAMAGE AT BS 686 .5" BELOW SKIN LAP, STR 34R IAW SRM 53-00-01 REPAIR 11. CUTOUT IS 1.5"X 2.6", COMPLETED HFEC, VERIFIED DAMAGE REMOVAL, INSTALLED REPAIR IAW EO B747-5330-46431A.
ON TOUCHDOWN, RECEIVED A CREW REST SMOKE INDICATION. SMELLED SMOKE IN COCKPIT. COULD NOT DETERMINE SOURCE OF SMOKE. ENGINE AND WING ANTI-ICE WHERE BOTH OFF. INSTALLED NR 3 PACK WATER SEPARATOR COALESCER BAG IAW AMM 21-51-05-2 REV 72.
ON TOUCHDOWN GOT A CREW REST SMOKE INDICATION. SMELLED SMOKE IN COCKPIT. COULD NOT DETERMINE SOURCE OF SMOKE. ENG AND WING ANTIICE WERE BOTH OFF DEF 466023. DEICE FLUID (UREA) APPLIED TO RUNWAY. REPLACE NR1 AND NR2 PACK WATER SEPARATOR BAGS AND REMOVED NR3 AND MEL'D.
INSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E FAIRING FOUND DELAMINATION AT MOST OTBD SIDE. FIBREGLASS HOT BOND REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5 REV 59.
INSPECTION TYPE:C, LT WING INBD AFT FLAP LOWER SURFACE MID POSITION FOUND PUNCH HOLE. FIBERGLASS HOT BOND REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 59.
INSPECTION TYPE:C, RT WING OTBD FORE FLAP OTBD L/E FAIRING FOUND DELAMINATED. FIBREGLASS HOT BOND REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV.59.
INSPECTION TYPE:C, RT WING INBD MID FLAP T/E COVE PANEL LOWER SURFACE FOUND DELAMINATION. FIBREGLASS HOT BOND REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 59.
INSPECTION TYPE:C RHW O/B FORE FLAP I/B L/E AREA FOUND DELAMINATION. FIBREGLASS HOT BOND REPAIR PERFORMED IAW SRM 51-70-07 PAR 5A(1) FIG 5 REV 59.
PUNCTURE OF OUTER FACE SHEET OF FLOOR PANEL .60 X .30, STA 507, LBL 57. REPAIRED IAW SRM 53-00-50, PARA 4 C.
EMERGNCY EXIT LIGHT IN CEILING PANEL BY ENTRANCE DOOR IS INOP. RELAMPED EMERGENCY EXIT LIGHT IAW MM 33-51-07-2. OPS CKS NORMAL.
AIR TURN BACK DUE TO WHEEL WELL FIRE WARNING MESSAGE AT LEVEL OFF FL340, WHEEL WELL FIRE WARNING REPEATED ITSELF. PERFORMED VISUAL INSP AT BOTH WHEEL OVERHEAT DETECTOR, FOUND NO DEFECTS AND NO MESSAGE NOTED. PERFORMED POWER ENGINE RUN, AND CHECKED DUCT LEAK AT WHEEL WELL, OK REPLACED DUCT LEAK WHEEL WELL CONTROL CARD M826 PRECAUTIONARY.
MCD FLOOR PANEL HAS 3 PUNCTURES AT FWD EDGE AND 1 IN MIDDLE OF PANEL REPAIRED IAW 747-400F, SRM 53-00-50-2R, REPAIR NR1.
INSPECTION TYPE:1C LT WING INBD AFT FLAP T/E WEDGE LWR SKIN, COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A, FIG 5, REV 53.