N572UP
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
FOUND NO.1 ENTRY DOOR LOWER SEAL DAMAGED
AFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT ENG 3 PUMPS ARE STRONGER THAN ENG 2 PUMPS DEFERRED IAW EO-97441.
AFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT ENG 3 PUMPS ARE STRONGER THAN ENG2 PUMPS. REMOVED AND REPLACED MAIN 2 AFT BOOST PUMP REF AMM 28-22-03. OPS CHECKED GOOD AT THIS TIME REF AMM 28-22-03. THIS CLEAR DEFERRAL.
AT FL 370 FWD WINDOW LEFT CRACKED. R & R L1 WINDOW IAW AMM 56-11-01/401. REPLACED WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01/401. OPS CHKD WINDSHIED HEATER SYS AND WIPER IAW AMM 30-41-00/501 & 30-42-00/501, CHKD NORMAL, AIRCRAFT OK FOR SERVICE.
AT FL 370, FWD WINDOW LEFT CRACKED
AIR TURN BACK, NR 3 STARTER CUTOUT EICAS MESSAGE IN CLIMB, CONTINUED THROUGH FLIGHT. QRH PROCEDURE FOLLOWED. R & R NR 3 ENG START VALVE IAW AMM 80-11-02/401 & OPS CHECKED NORMAL.
DAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND DIRECT AFTER LANDING WE FOUND DAMAGE TO THE TAIL AREA OF THE AIRPLANE. BEFORE GROUND HANDLING TOUCHED THE AIRPLANE AT CGN. WE FOUND FOLLOWING DAMAGES BELOW THE TAIL STAND MOUNT:ONE TIME WE HAD A DENT AND SCRATCH DIRECTLY ON TOP OF A RIVET. (DAMAGE STARTS APPROX. 3.INCH BELOW TAIL JACK MOUNT)DEPTH: 0.1335 INCHLENGTH: 2.25 INCH WIDTH: 0.5 INCH. THERE IS ALSO A CRACK DIRECTLY NEXT TO THIS DAMAGE. <BR>LENGTH: 4 INCHES THE SECOND DAMAGE IS A SCRATCH DIRECTLY BELOW THE PREVIOUS DAMAGE. (DAMAGE STARTS APPROX. 5.INCH BELOW TAIL JACK MOUNT) LENGTH: 2.5 INCH WIDTH: 0.25 INCH.
DAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND FOR CORRECTIVE ACTION PLEASE SEE REF: EO-92470-REQ1 (SECTION 48 FUSELAGE SKIN PANEL DENT, GOUGE, AND CRACK DAMAGE FORWARD OF STA 2598; BETWEEN STR 38R AND 46R - CATEGORY B REPAIR) COMPLIED WITH EO-92470
EMERGENCY LIGHT IN CEILING PANEL ABOVE L-1 DOOR FWD BULB INOP. RE-LAMPED FWD BULB IN EMERGENCY CEILING LIGHT ABOVE L1 DOOR PER AMM 33-51-07. OPS CHECK GOOD PER AMM 33-51-00.
MAIN CARGO DECK FLOOR PANEL APPROX. STA 1140 L TO APPROX STA 1220L CRACKED ALONG ENTIRE OUTBID LENGTH MARKED WITH TAPE. INSTALLED NEW FLOOR PANEL IAW AMM 53-21-02, RII Ãâ¬ÅOK TO INSTALLÃâ¬? GIVEN ON BARCODE T3F18E005CL38.
DENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE.REMOVED THE DAMAGED SKIN,MEASURE THE CUTOUT (DIA:0.8", 10.75" FROM OUTBD EDGE I.A.W. 747-400F SRM 57-53-01-2R-1.PERFORMED NDT/ET FOR CUTOUT AREA I.A.W. 747 NTM PART6 51-00-00 PROCEDURE 23 REV:176 RESULT:NO CRACK INDICATION WAS FOUND
DENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE. (REPAIR) PERFORMED NDT/UT REWORKED AREA AND PLUS 8" AROUND HEATED AREA, I.A.W. 747 NDT MANUAL PART 1 51-01-01 AND 747 NDT MANUAL PART 1 51-04-00 REV.176 , RESULT: NO DEFECT FOUND. OPEN
L/H FRONT SPAR THE INTERCOSTAL LUG FITTING AT LBL 11.30, STA 1000.REMOVED AND REINSTALLED THE BOLTS AND TUBE AT STA 1000. CONDITIONS WERE NORMAL IAW AMM 20-11-28-964-010
R/H FRONT SPAR THE INERCOSTAL LUG FITTING AT RBL 11.33 STA 1000 REMOVED BOTS AT STA 1000. CKD NORMAL. REMOVED TUBE. CKD NORMAL IAW IPC 57-14-01-01A.
L/H FRONT SPAR THE SHEAR TIE AT LBL 75.92, STA 1000. REMOVED HARNESS FOR SM REWORK UNDER FLOOR PANEL IAW SWPM 20-10-12
STRINGER, L/H WING NO.7 V/C FLAP (REPLACE) INSTALL NEW PART IAW SRM 51-40-02-0G REV.101 AND BOEING DWG NO: 65B15170 SH 2 REV:H. IAW AMM 27-81-02-404-010, REV110, STEP A~5(E), INSTALL NO.7 VARIABLE CAMBER FLAP IAW AMM 27-81-02-404-010 REV.110 STEP E(6) TO E(33) ADJUST NO.7 V.C FLAP. CONDITION CHECK SATISFIED.
NUMBER 14 INBOARD MOST RIGHT WING KRUGER FLAP HAS 2 DENTS VERIFIED CORRECT CLEARANCES AND OPS CHECK OF THE #14 KRUEGER FLAP IAW AMM 27-81-01. ALL CHECKS GOOD AT THIS TIME.
HFEC REINSPECT REVEALED CRACK INDICATION AND NEW DAMAGED IDENTIFIED VISUALLY (T3F18E001Y856 CLOSED IN ERROR) FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01-2R. MATERIAL ID FOR FILLER IS .100" 2024-T3 PO.#SP2586586, AND FOR DOUBLER .125" 2024 T-3 PO.#SP2555900. PERFORMED PERMANENT REPAIR IAW EO-87268-REQ3.
LH I/B AFT FLAP HAS A PUNCTURE APPROX 26.75Ãâ¬? FROM TRAILING EDGE & 63Ãâ¬? FROM I/B EDGE. MARKED WITH TAPE.***SM36/LMX4/HGR*** ACCOMPLISHED STEPS 1-14 OF EO-87186-REQ3 PERMANENT REPAIR. THIS CLEARS DEFERRAL MOC 2500762.
L1 CREW ENTRANCE DOOR LATCH TO HOLD OPEN IS BROKEN CLEANED AND CHECKED HOLD OPEN MECHANISM IAW AMM 52-11-00-201 REV. 106.01. FOUND SATIS
**SUPPLEMENTAL SDR**FAULT FOUND THE MAIN DECK L1 DOOR AREA EMERGENCY LIGHT INOP (REPLACE) TASK COMPLETED IAW AMM 33-51-01 REV39.00
FAULT - BROKEN - LEFT WING OUTBOARD FORE FLAP ACCESS PANEL WBL 754 (REPAIR) TASK COMPLETED
FAULT - CORROSION - SUPPORT, RH AIR CONDITION COMPARTMENT ACCESS DOOR, MIDDLE SUPPORT. (REPLACE) TASK COMPLETED
INSPECTION TYPE:N/AUPPER FACE SHEET OF FLOOR PANEL POS 9L DELAMINATEDFABRICATE NEW FLOOR PANEL PER EO B747-5320-42648-A
INSPECTION TYPE:N/AMAIN DECK FLOOR PANEL POS 9L HAS DAMAED UPEPR FACE SHEETFABRICATE REPLACEMENT FLOOR PANEL PER EO B747-5320-42648-A
INSPECTION TYPE:N/AFUSELAGE FRAME WEB DAMAGE REPAIR AT STA 2034, S-38R - S-39R.REPAIRED PER E.O. B747-5310-82695-A.
INSPECTION TYPE:NAFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 1960, S-47R - S-48R, S-49L - S-46LREPAIRED PER EO B747-5310-82668-A
INSPECTION TYPE:NAFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 1960, S-47R - S-48R, S-49L - S-46LREPAIRED PER EO B747-5310-82670-A
INSPECTION TYPE:NAFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 2000, S-46L - S-51L, S-49R - S-47REPAIRED PER EO B747-5310-82671-A
INSPECTION TYPE:NA FUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 2020, S-45L - S-50L, S-49R - S-46RREPAIRED PER EO B747-5310-82672-A
INSPECTION TYPE:NAFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 2040, BETWEEN S-46L - S-46RREPAIRED PER EO B747-5310-82673-A
INSPECTION TYPE:NAFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 2100, BETWEEN S-46L - S-46RREPAIRED PER EO B747-5310-82676-B
INSPECTION TYPE:NAFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 2120, S-48R - S-46RREPAIRED PER EO B747-5310-82677-A
INSPECTION TYPE:NAFUSELAGE DOUBLERS MULTIPLE DAMAGES REPAIR AT STA 1954 - 1960, WL 103, S-47L - S-47RREPAIRED PER EO B747-5310-82526-A
INSPECTION TYPE:N/A FUSELAGE SKIN REPLACEMENT AT STA 1961 - 2181, S-46L - S-46R.REPAIRED PER E.O. B747-5310-82552-A.
INSPECTION TYPE:N/ALEFT FUSELAGE SKIN PANEL DAMAGE REPAIR BETWEEN STA 1961 - 2181, S-44L - S-46L.REPAIRED PER E.O. B747-5330-82692-A.
INSPECTION TYPE:N/AFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 1940, S-48R - S-47R, S-49L.REPAIRED PER E.O, B747-5310-82521-A.
INSPECTION TYPE:N/AFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 2060, S-46L - S-48L.REPAIRED PER E.O. B747-5310-82674-A.
INSPECTION TYPE:N/AFUSELAGE FRAME WEB DAMAGE REPAIR AT STA 1940, WL 110, S-47L - S-48L.REPAIRED PER E.O. B747-5310-82524-A.
INSPECTION TYPE:N/AFUSELAGE FRAME WEB DAMAGE REPAIR AT STA 2120, S-46R - S-47R.REPAIRED PER E.O. B747-5310-82522-A.
INSPECTION TYPE:N/AFUSELAGE FRAME REPAIR AT STA 2040, S-28R - S-44R.REPAIRED PER E.O. B747-5310-82523-A.
INSPECTION TYPE:N/ARIGHT FUSELAGE SKIN PANEL DAMAGE REPAIR BETWEEN STA 1961-2181, S-44R-S-46R.REPAIRED PER E.O. B747-5330-82520-A.
INSPECTION TYPE:N/AFUSELAGE LOWER FRAME WEB REPAIR AT STA 2140, S-48R - S-50R.REPAIRED PER E.O. B747-5310-82525-A.
INSPECTION TYPE:N/AFUSELAGE SKIN DAMAGE REPAIR BETWEEN STA 1900 - 1961, S-46L - S-46R.REPAIRED PER E.O. B747-5330-82519-A.
INSPECTION TYPE:N/AFUSELAGE FRAME FAIL SAFE CHORD DAMAGE REPAIR AT STA 2080, S-46L - S-47L, S-47R - S-46R.REPAIRED PER E.O. B747-5310-82675-A.
INSPECTION TYPE:NAAFTER TAKEOFF GEAR LEVER WOULD NOT MOVE TO THE UP POSITION. NO EICAS MESSAGES COMPLIED WITH QRH. REPEAT WRITE UP FROM PREVIOUS FLIGHT.ONLY REPLACED NEW GEAR LEVER ACTUATOR MODULE ASSY PER AMM 32-31-01/401 P/N ON & OFF: 257U0002-34, S/N ON & OFF: D00333/D00812. PERFORMED OPERATIONAL CHECK OF GEAR LEVER ACTUATOR MODULE ASSY PER AMM 32-31-01 AND TEST NORMAL IPC: 32-31-01-01-022V.
INSPECTION TYPE:N/A**ATB** - GEAR HANDLE WOULD NOT RAISE AFTER T/O. RAN CHECK LIST USED LOCK OVERIDE TO RAISE GEARFOUND CMC MSG 32555 & 32575. PERFORMED FIM TASK 32-61-00-812-810. GRD TEST OF PSEU, PRI L/G SYS AND ALT L/G SYS ALL PASSED. NO PLF & EXISTING FAULT NOTED. A/C OK FOR SVC. NOTIFIED AMC
INSPECTION TYPE:18FODAMAGE ON MAIN DECK FLOOR PANEL ASSY (P/N : 144U5803-28) BETWEEN STA 1235 AND STA 1265 , AND BETWEEN RBL 98.58 AND RBL 117.40 , PANEL NO. 242AGFABRICATE A NEW FLOOR PANEL I.A.W UPS EO B747-5320-42648-A
INSPECTION TYPE:N/A**ATB** DURING CLIMB OUT EICAS MESSAGE "WAI VALVE RIGHT" COMPLETED QRH. RIGHT WING ANTI-ICE VALVE WOULD NOT CLOSE. AIR TURN BACK. FUEL JETTISON.CMC SHOWS WAI VALVE RIGHT AT FAULT. R/R RH WING ANTI-ICE VALVE IAW AMM 30-11-03-404-008 REV 102.00. LEAK CHECKED SATIS. OPS TEST C/O SEVERAL TIMES. FOUND SATIS. P/N OFF-ON: 67-2985-003, S/N OFF: 487, S/N ON: 524. EFF REF IPC: 30-11-03-02 ITEM 085L REV 47.01.
NO EMERG DECL'D - NO EQUIP USED - LANDED UNEVENTFULLY, DUE TO EQUIP COOLING EICAS. PER MEL 36-11-4.L/H ISOLATION VALVE FAILED IN FLIGHT WILL BE SECURED OPEN.DMP PROCEEDURES PER MEL 36-11-4 COMPLIED WITH.DMI NO.M747173 PLACARD UINSTALED.CREW REPORTED VALVE L/H ISLN HAD TO BE SELECTED OFF IN FLT.REVERSED DMP 36-11-4. R/R'D LEFT WING ISOLATION VALVE PER MM 36-11-07-404-015. NO LEAKS NOTED OPS CHECKED GOOD. M747173 CLOSED. ESR IPC 36-11-57-01 S400.
INSPECTION TYPE:NAOVHD EMERGENCT HATCH LEFT STAINLESS TRIM PIECE IS SEVERLY BENT HATCH DOOR CATCHESCOLD WORKED TRIM PIECE BACK TO CONTOUR REF EO NO M-5100-41097-E
INSPECTION TYPE: PS1, EMERGENCY LIGHT AFT BULB INOPERABLE AT L1 DOOR CEILING LIGHT. DEFERRAL OF INTEROR EMERGENCY LIGHT SYSTEM. MEL 33-51-1-0-2 M722064 PLACARD INSTALLED. RELAMPED PER MM 33-51-05. M722064.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 1400 TO STA 1500. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM BS 1300 TO 1400 , PANEL 42CF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B747-5320-42648-A.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 1380 TO STA 1500 , PANEL NO.252FF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B747-5320-42648-A.
INSPECTION TYPE:C2DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 1740 TO STA 1860 , PANEL NO.261AF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B747-5320-42648-A
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 1020 TO STA 1100. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 2140 TO STA 2240. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 2260 TO STA 2360. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 2280 TO STA 2360. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 2360 TO STA 2380. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 1400 TO STA 1500. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 1380 TO STA 1500, FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A
INSPECTION TYPE:C2, DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 1380 TO STA 1500 , PANEL NO.252BF. ABRICATED A REPLACEMENT FLOOR PANEL PER EO B747-5320-42648-A.
INSPECTION TYPE:C2, DENT WAS FOUND ON THE LOWER PANEL ASSY OF R/H INBD T.E AFT FLAP NEAR WBL 182.REPAIR I.A.W. SRID: 4-4824467363 AND EO B747-5750-77402-A.
FLIGHT COMPARTMENT SMOKE EVACUATION SHUTTER VALVE LEAKING WATEROPENED/CLOSED/CLEANED AREA AROUND VALVE. OPS CHECKED GOOD PER MM 25-64-05-202. NO LEAKS NOTED.
INSPECTION TYPE:N/A MAIN DECK FLOOR PANEL POS 11R/12R DAMAGED. FABRICATED NEW FLOORBOARD IAW EO B747-5320-42648-A.
INSPECTION TYPE:C4, FOUND L1 DOOR AREA EMERGENCY LIGHTS INOP. IAW AMM 33-51-04-902-001-001 REV 92.04, REPLACED THE EMERGENCY LIGHT BATTERY PACK AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST, RESULT WAS SATISFACTORY.
DURING A WALK AROUND, FOUND THE NR 1 INBOARD PYLON ACCESS PANEL 454DR MISSING. INSTALLED A NEW ACCESS PANEL.
UPPER DECK EMERGENCY LIGHTS L1853, L1854, AND L5735 ARE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACK M5170 IAW AMM 33-51-04-902-001-001 REV 90.02. PERFORMED A SATISFACTORY EMERGENCY LIGHT TEST.
SMOKE CURTAIN HAS A HOLE, MAIN DECK BS 420. REPAIRED IAW MM 25-59-00-308-036
SECONDARY INDICATION DROP DOWN PAGE SHOWED INTERMITTENT VIBRATION NUMBERS UP TO 5.0 ON ENGINE NR 3. INDICATIONS WERE NOTICED DURING LOW IDLE AND BELOW ONLY. PERFORMED FIM 71-00-00-101 AND FOUND HPT TCC DUCT LINK BROKEN, R & R IAW MM 75-24-03. ALSO FOUND LPT BUSHING WORN, R & R IAW MM 75-24-03.
MCD FLOOR PANEL POS 8L INBD DAMAGED FABRICATED A NEW FLOOR PANEL IAW EO B747-5320-42648-A.
MAIN DECK FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE:N/A, L1 DOOR FWD EMERGENCY LIGHT INOP DURING TEST. RELAMPED L1 DOOR FWD EMERGENCY LIGHT. OPS CHECK GOOD. REF MM 33-51-00-5
AFT EMERGENCY LIGHT INSIDE L1 DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT INSIDE L1 DOOR. OP CHECK GOOD, REF AMM 33 51 00.
INSPECTION TYPE: PR/H, INBD AILERON HAS NUMEROUS DEEP GOUGES ON L/E SKIN. REMOVED AND REPLACED THE AILERON IAW AMM 27-11-01-004-001 AND 27-11-01-404-008.
INSPECTION TYPE: PL/H, INBD AILERON HAS NUMEROUS DEEP GOUGES ON L/E SKIN. REMOVED AND REPLACED THE LT AILERON IAW AMM 27-11-01-004-001 AND 27-11-01-404-008.
F/O EVAS INOPERATIVE. R & R THE EVAS IAW TC25-060-01-03.
MCD FLOOR PANEL DAMAGED AT ENTRY DOOR. DAMAGE IS LESS THAN .7500" IN DIAMETER. THIS IS MAJOR REPAIR TRANSFERRED TO NR 585778, BH 2020270. FABRICATED NEW PANEL IAW EO B747-5320-60339-A. THIS CLEARS DEF 573369.
MAIN DECK FLOOR PANEL, PN 14145876-94 DAMAGED REF D573368, 573369 AND 573370, FOR DAMAGES FABRICATED NEW BOARD, REF EO B747-5320-60339-A.
MAIN DECK FLOOR PANEL MIDDLE POSITION AT BS 1736 DAMAGED. REPAIRED, IAW SRM 53-00-50-2R.
FLOOR PANEL AT MIDDLE POSITION AT BS 1695 DAMAGED, REPAIRED IAW SRM 53-00-50-2R.
COCKPIT PBE DAMAGED ON TOP CORNER. R & R COCKPIT PBE OK FOR SERVICE REF MM 25-60-00 25-61-01-05D I 80 CTR CS.
NR 2 ENGINE LEAKING OIL DURING CRUISE. CREW DETERMINED NR 2 ENG LOSING 1 QT OIL EVERY 30 MINS. R & R NR 2 ENGINE IAW TC 71-000-00-01. OPS & LEAK CHECKED GOOD.
EMERGENCY DECLARED ON ARRIVAL, PASSING THROUGH 1500' AGL, ACFT EXPERIENCED MULTIPLE ELEC FAULT INDICATIONS. FLAPS FAULTED TO 20 DEGREE, A/T DISENGAGED; LOST CAPTAIN AUDIO PANEL. AUTO BRAKES DISENGAGED. FOUND CMC. MSG 24725: RCCB C8841 OR C8843 OPEN. ACCOMPLISH BOW: TS 2938 IAW FIM 24-60-00-812-808, AMM 24-60-00-715-001, DC ELECTRICAL LOAD SYS TEST SATISFACTORY, AMM 24-31-01-705-035 C/W MAIN BATTERY TEST-OK. R & R BATTERY TRANSFER RELAY R7224.
INSPECTION TYPE:CRT, WING SLAT NR 9 INBD TRACK ON THE INBD COVE SKIN PANEL HAVE CRACKS. REMOVED AND INSTALLED NEW FABRICATED SKIN, COVE PANEL IAW DWG 114N4003-18, MATERIAL 7075-T6, .050.
INSPECTION TYPE:D, RT WING INBD AFT FLAP L/E FAIRING PUNCH. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 71.
INSPECTION TYPE:D, LT WING INBD AFT FLAP L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 71.
INSPECTION TYPE: D, RT WING OTBD AFT FLAP UPPER T/E DELAMINATED. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 71.
INSPECTION TYPE:D, RT WING OTBD FORE FLAP L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 71.
INSPECTION TYPE:D, RT WING OTBD FORE FLAP L/E FAIRING INBD AREA DELAMINATED. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-01, PAR 5A(1), FIG 5, REV 71.
INSPECTION TYPE:D, LT WING INBD MID FLAP UPPER T/E PANEL PUNCH FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 71.
INSPECTION TYPE:D, LT WING INBD FORE FLAP LWR T/E DELAMINATED. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 71.
INSPECTION TYPE:D, RT WING INBD FORE FLAP LOWER T/E PUNCH. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 71.
INSPECTION TYPE:D, LT WING INBD FORE FLAP L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 71.
INSPECTION TYPE:D, LEFT WING OTBD MID FLAP L/E FAIRING DELAMINATED FIBERGLASS PREPREG LAYUP. REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 71.
INSPECTION TYPE:D, LT WING OTBD MID FLAP L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 71.
INSPECTION TYPE: DM/D, NEAR L1 DOOR OVERHEAD EMERGGENCY LIGHT DIM NEAR L1 DOOR OVERHEAD EMERGENCY LIGHT ASSY, 1 EA LAMP REPLACED AND EMERGENCY LIGHT TESTED NORMAL IAW AMM 33-51-07.
FLOOR PANEL AT BS 1920 DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52751-A.
BS 1990 FLOOR PANEL HAS A HOLER. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52750-A.
MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED FLOOR PANEL BETWEEN BS 2280-2360 IAW EO B747-5320-52752-A.
MAIN CARGO DECK FLOOR PANEL AT BS 490, DAMAGED AND DELAMINATED. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52745-A.
MAIN CARGO BAY FLOOR PANEL DAMAGED . FABRICATED NEW FLOOR PANEL BETWEEN BS 1620-1720, RBL 33-75 IAW EO B747-5320-52748-A.
HOLE IN MAIN CARGO DECK FLOORBOARD BS 1500. FABRICATED NEW FLOORBOARD IAW EO-B747-5320-43835-C.
MAIN CARGO BAY FLOOR PANEL DAMAGE, BS 480- 520, RBL 67 - 112. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-53305-A.
MAIN CARGO DECK LT FLOOR PANEL, BS 563 HAS TWO HOLES. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52724-A.
MAIN CARGO DECK LT FLOOR PANEL BS 543 HAS TWO HOLES. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52724-A.
FLOORBOARD DAMAGED AT LT BS 1650, FABRICATED NEW FLOORBOARD IAW EO B747-5320-52747-A.
MAIN CARGO DECK LT FLOOR PANEL BS 520 DAMAGED HOLE 1 X .8. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52724-A.
BS 1720, LT FLOOR PANEL DAMAGED, FABRICATED NEW FLOOR PANEL IAW EO-B747-5320-52749-A.
BS 1175, MCD LT FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52754-A.
BS 1780 FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52749-A.
MAIN CARGO DECK BS 1650, LT FLOORBOARD DAMAGED BEYOND ALLOWABLE LIMITS. FABRICATED NEW FLOORBOARD IAW EO B747-5320-52747-A.
MAIN CARGO DECK FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50-2R-1.
RIGHT INBD MIDFLAP LOWER SKIN ON COVE PANEL PUNCTURED 41 INCHES FROM INBD AND 3.1 INCHES FROM T/E. REPAIRED IAW EO B747-5750-52693-A.
RIGHT INBD MIDFLAP LOWER SKIN HAS FOUR DAMAGED AREAS. REPAIRED IAW EO B747-5750-52574-A.
MAIN CARGO DECK FLOOR PANEL, BS 2010 PUNCTURED. REPAIRED IAW SRM 53-00-50-2R-1.
MAIN CARGO DECK FLOOR PANEL BS 1700 DAMAGED. REPAIRED IAW SRM 53-00-50-2R-1.
BS 1250, MAIN CARGO DECK FLOOR PANEL HAS TWO HOLES. REPAIRED IAW SRM 53-00-50-2R-1.
FLOOR PANEL DAMAGED BS 280-300, LBL37-RBL37. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52569-A.
FLOOR PANEL STA 370 HAS THREE PUNTURES .3,.25, AND .4 INCHES BETWEEN BS 360-400, LBL 12-55, FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52571-A.
MAIN CARGO DECK FLOOR PANEL HAS A .6 DIA PUNCTURE PANEL BETWEEN BS 320-360 AND RBL12-47. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-52570-A.
BS 1662, MAIN CARGO DECK LT FLOOR PANEL DENTED. REPAIRED IAW SRM 53-00-50-2R-1.
RT INBD FLAP COVE PANEL LOWER SKIN PUNCTURED 53 INCHES FROM INBD AND 27 INCHES FROM T/E. REPAIRED IAW EO B747-5750-52297-A.
MAIN CARGO DECK FLOOR PANEL, BS 1280 SECOND FROM RT, HAS TWO DENTS. REPAIRED IAW SRM 53-00-50-2R-1.
FLOOR PANEL BS 450 HAS ONE GOUGE AND SCRATCH IN TOP SKIN. FABRICATED FLOOR PANEL IAW EO B747-5320-52572-A.
MAIN CARGO DECK FLOOR PANEL BS 1100 HAS A HOLE. REPAIRED IAW SRM 53-00-50-2R-1.
BS 1200, MAIN CARGO DECK FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50-2R-1.
DAMAGE TO LT INBD MID FLAP LOWER COVEL PANEL SKIN 8.5 INCHES FROM T/E AND 11 FT FROM OTBD EDGE. REPAIRED IAW EO B747-5750-52575-A.
DURING C INSPECTION, LEFT WING OTBD FORE FLAP INBD L/E AREA DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 67.
DURING C INSPECTION, LEFT WING OTBD FORE FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 67.
DURING C INSPECTION, RT INBD T/E FLAP DENTED INBD IF OTBD EDGE. PERFORMED METAL HOT BOND REPAIR IAW RI-57-55-10320, REV A AND EO B747-5750-51963-A.
INSPECTION TYPE: PS, EMERGENCY EXIT LIGHT ON CEILING OF MAIN CARGO DECK JUST FWD OF STAIRS INOPERATIVE. RELAMPED IAW AMM 33-51-07-962-001. OPS CHECKED GOOD.
EMERGENCY LIGHT SWITCH GUARD ON O/H PANEL WILL NOT RETAIN SWITCH WHEN ON. R & R SWITCH GUARD OIL FOR SERVICE IN REF TO AMM 33-51- 00-5.
INSPECTION TYPE:C, RT WING NR 15 KRUEGER FLAP DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 60.
INSPECTION TYPE: C, RT WING INBD AFT FLAP L/E FAIRING PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 60.
RT INBD MIDFLAP COVE PANEL DAMAGED UPPER AND LOWER SKIN/ CORE. REPAIRED REF EOB747-5750-42086-D.
MAIN CARGO COMP FLOOR POS NR 20 LT HAS HOLE. REPAIRED IAW SRM 53-00-50 REPAIR 1.
FLOOR POS 19RT DAMAGED UPPER SKIN AND CORE. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK POS NR 19R DELAM 11.5" X 10 " ON TOP SURFACE. 61" AFT OF PANEL L/E. REPAIRED IAW SRM 53-00-50 REPAIR 1.
MAIN CARGO COMP FLOOR POS NR 20 LT HAS SMALL HOLE 20" FWD OF AFT EDGE. REPAIRED IAW SRM 53-00-50 REPAIR 1.
FUSELAGE STA 720, 2.5" OTBD OF STR 47R HAS LIGHTNING DAMAGE. REMOVED DAMAGE AND REPAIRED IAW EO B747-5330-42346-A.
FUSELAGE SKIN DAMAGE BY LIGHTENING STRIKE AT STA 780, STR 47R, SKIN IS . 074 THICK (2) 1" DIA HOLE. REPAIRED REF EOB747-5330-42360-A.
EICAS MSG DET FIRE/OHT 3. REPLACED UPPER AFT LOOP ASSY (TS681), LOWER AFT LOOP ASSY (TS682) AND LOWER FWD LOOP ASSY (TS683) REF AMM 26-11-02-4. OPS CHECK GOOD.
CREW RECEIVED AN ENGINE NR 3, ILLUMINATION INDICATION. DEFERRED B LOOP NR 449984 REPLACED NR 3 ENG AFOLTS AND LOOP A FIRE CARDS. REF AMM 26-10-01-4. REPLACED UPPER AFT LOOP ASSY TS681, LOWER AFT LOOP ASSY TS682, AND LOWER FWD LOOP ASSY TS683 REF AMM 26-11-02-4. OPS CHECK GOOD. THIS CLEARS DEF NR 449984.
INSPECTION TYPE:C2, LT WING OTBD FORE FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5.A, FIG 5, REV 57.
MCD FLOOR PANEL STA 1620 DAMAGED. REPAIRED IAW OE B747-5320-35924-C.
MCD FLOOR PANEL DAMAGED 1620, REPAIRED EO B747-5320-36924-C.
FORWARD LOWER CARGO DOOR AFT LOWER CORNER IS DAMAGED. REMOVED DAMAGE AND REPAIRED IAW EO B747-5230-36580-C.
INSPECTION TYPE:N/A DIVERSION - ENGINES NR 1 & NR 3 BLEEDS INOP AND LOSS OF ICING PROTECTION ON NR 3 ENGINE. REPLACED AIR SUPPLY CONT & TEST UNIT PER MM 36-11-30-4. REPLACED NR 1 ENG HP SHUT-OFF VALVE AS PER MM 36-11-05-4 & HP CONTROLLER AS PER MM 36-11-06-4. PERFOMED OPS CHECK NORMAL.
INSPECTION TYPE:C LHW - OTBD FORE FLAP INBD L/E AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 52.
INSPECTION TYPE:C LHW, INBD T/E AFT FLAP LWR SURFACE MID AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 52.
INSPECTION TYPE-C2, R/W REAR SPAR AT IB HINGE OF NR4 SPOILER PARTITION RIB ATTACH BRACKET GOUGED AND BENT. REMOVED AND REPLACED GUSSET ON SPOILER PARTITION IAW SRM 51-1-8, 51-1- 21.
INSPECTION TYPE-C2, DRILL START IN LOWER SKIN OF RT WING OB, L/E, NEXT TO A RIVET, FWD AND IB OF 3RD. PANEL FROM OB END CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 5 1-1-21, 51-2-0 FIG.7,
L1 DOOR CEILING EMERGENCY LIGHT INOP. RELAMPED, INSPECTED. CHECKS OK.