N855GT
Registered owner: ATLAS AIR INC, NY (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
TIRE PRESSURE EICAS & STS MSG OCCURRED AFTER T/O. PERFORMED CONDITIONAL INSPECTION ON MLG 11 & 12 AXLE IAW AMM 05-51-25 (1-8) & AMM 32-45-04-206-011, NO DAMAGE NOTED TO RH BODY GEAR. BRAKE SYS TEST PASS. NO LEAKS NOTED. OPS CHK GOOD AT THIS TIME. R & R MLG 11 & 12 TIRE WHEEL ASSY IAW AMM 32-45-01 & IPC 32-45-03-07. OPS & LK CHK OK.
CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S 50877 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-7L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50878 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-9L, AT STA 930. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 60010 (SRM 53-20-03-2R-1 REV 47) AND EI NO: T2026A53M-050 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG 142U0920 SHEET 37 REV, DWG 142U3725 SHEET 14 REV C. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER AND STRINGER SPLICES S-10R, AT FWD AND FWD SIDE OF STA 2180. REPAIR DAMAGE AREA IAW W/S NO: 50871 (SRM 53-60-03-2R-3 REV: 47) AND EI NO: T2026A53M-076 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-3L, AT AFT SIDE OF STA 2360.(<P>1. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-034 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-6R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50868 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50869 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-5L, AT AFT SIDE OF STA 2360.(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. 2. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-033 REV 1. 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG NO: 148U2377 SHEET 22 REV A. 4. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
FOUND EXTERIOR EMER LT (L6690) INOP. PERFORM WIRING CONTINUITY CHECK AND SYSTEM TROUBLESHOOTING IAW WDM 33-51-72 REV 35, FOUND M5168 BATTERY FUNCTION FAILED. PERFORM BATTERY REPLACEMENT AT M5168 IAW AMM 33-51-04-900-803 REV 49. CONDITION CHECK NORMAL AND PERFORM POWER SUPPLY TEST, RESULT WAS SATISFACTORY.
CRACK DAMAGE ON THE STRINGER S-8R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50870 (SRM 53-80-03-2R-2 REV: 47) JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-5L, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50867 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-20R, AT AFT SIDE OF STA 2360. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 50872 (SRM 53-80-03-2R-3 REV 47). INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG NO: 148U2377 SHEET 24 REV A, SHEET 25 REV A. JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-2L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50876 (SRM 53-60-03-2R-8 REV: 47) AND EI T2026A53M-087 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.
EMP - RH HORIZONTAL STAB TIP FAIRING CLOSURE WEB LWR CHORD CRACK.(<P>LWR CHORD REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.</P>)
FUSELAGE SECTION 46 - FUSELAGE SKIN (P/N: 146U3867-5) - PUNCTURE BETWEEN STA 2000 AND S38L TO S39L - CATEGORY B REPAIR.(<P>SHEAR TIE REPLACED AS PER SRM 51-10-02. NEW SHEAR TIE HOLES TRANSFERRED AS PER SRM 51-40-05. NEW SHEAR TIE INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)
#8 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
#9 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
LHW NO.11 K-FLAP AT WS 569 D-BEAM LWR ATT BOLT AREA, FOUND CRACK.(<P>CRACK AREA REPAIRED AS PER RI NO: RI-57-41-17558 REV A. NO FURTHER DEFECTS NOTED.</P>)
LH HORIZONTAL STAB TIP T/E FAIRING FWD U CHANNEL CRACK.(<P>U CHANNEL REPLACED AS PER RI NO: RI-55-10-17562 REV A. NO FURTHER DEFECTS NOTED.</P>)
EMP - RH HORIZONTAL STAB TIP FAIRING I/B CLOSURE WEB, FOUND CRACK.(<P>CRACK - WEB REPLACED AS PER SRM 51-10-01. NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05. NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)
M/D STA 1510, 1530, 1550 LBL 11 SEAT TRACK SLOT HOLE ELONGATED.(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-9 REPAIR 9 FIG 201 AND RI NO: RI-53-65-17570 REV A. NO FURTHER DEFECTS NOTED.</P>)
#19 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
#18 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
#7 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
#20 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
#21 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
RHW ILE 450 I/B SUPPORT BEAM UPPER FTG FOUND HOLE ELONGATED.(<P>SUPPORT BEAM REPAIRED AS PER SRM 57-41-09-2R-2 REPAIR 2 FIG 203 DETAIL IV AND RI-57-41-17586 REV A. NO FURTHER DEFECTS NOTED.</P>)
RHW I/B L/E D-BEAM AT I/B PDU AREA O/B FOUND CRACK ILES 520.(<P>CRACK AREA REPAIRED AS PER RI-57-41-17559 REV A. NO FURTHER DEFECTS NOTED.</P>)
EMP - RH HORIZONTAL STAB TIP FAIRING INTERNAL AREA MOST AFT RIB, FOUND CRACK.(<P>RIB REPLACED AS PER SRM 51-10-02. NEW RIB HOLES TRANSFERRED AS PER SRM 51-40-05. NEW RIB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)
REJECTED TAKE OFF @ 110 KNOTS MASTER WARING ON EICAS.(<P>REMOVED & REPLACED MAWEA PRINTED CIRCUIT CARD (MASTER MONITORS) AMM 31-51-02/401, HIGH ENERGEY STOP INSPECTION C/W IAW AMM 05-51-10-202-001</P>)
LOW AIRSPEED REJECT DUE TO "CONFIG SPOILER" AT 40 KTS(<P>CMC SHOWED NO EXISTING FAULT. PERFORMED SPOILER TEST AND T/O CONFIG GND TEST, TEST PASSED. NO MAINT MSG IAW 27-61-00/501 AND 31-52-00/501. HIGH ENERGY STOP INSPECTION NOT REQUIRED PER AMM 05-51-10.</P>)
SPEED BRAKE HANDLE POPPED UP DURING TAKEOFF ROLL. LOW SPEED. TAKEOFF CONFIG WARNING APPEARED. AUTOSPOILER SYSTEM DEACTIVATED. R & R ACTUATOR IAW AMM 27-62-00, OPS CHECKED GOOD.
RTO AT APPROXIMATELY 140 KTS DUE TO "CONFIG SPOILERS" WARNING MSG AND SIREN. GROSS T/O WT 442.0(<P>PERFORMED HIGH ENERGY STOP INSPECTION IAW B747 AMM 05-51-10, NO DEFECTS NOTED. SPEEDBRAKE HANDLE SWITCH REPLACED IAW AMM 27-62-10, OPS CHECK GOOD.&NBSP;</P>)
SB 747-57-2369 NO.1 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION.(<P>SB 747-57-2369 NO.1 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION AREA ACCOMPLISHED IAW RI-57-50-16189 REV.A&NBSP;</P>)
SB 747-57-2369,ÃÂ NO.8 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION.(<P><SPAN>SB 747-57-2369,&NBSP;</SPAN><SPAN>NO.8 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION AREA ACCOMPLISHED IAW RI-57-50-16190 REV A</SPAN></P>)
RH WING NO.20 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(<P>REPAIRED WITH ADHESIVE PASTE AS PER&NBSP;CMM 57-55-42</P>)
RH WING NO.19 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(<P>REPAIRED WITH ADHESIVE PASTE AS PER&NBSP;<SPAN>CMM 57-55-42</SPAN></P>)
RH WING NO.21 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(<P>REPAIRED WITH ADHESIVE PASTE AS PER&NBSP;<SPAN>CMM 57-55-42</SPAN></P>)
LHW REFUEL PANEL O/B ROD CLEVIS PN: 116U4252-157 FOUND ELONGATED(<P><SPAN>LHW REFUEL PANEL O/B ROD CLEVIS PN: 116U4252-157 FABRICATED AND REPLACED IAW RI-52-49-16199 REV A</SPAN></P>)
L/H WING I/B L/E CAVITY NO.7 V LINK (COUNT FROM I/B) UPPER BRACKET FOUND ELONGATED.(<P>LHW ILES 442.84 RIB SUPPORT BEAM ATTACHMENT FLANGE FASTENER HOLE ELONGATION AREA REPAIRED IAW RI-57-00-16173 REV.A.</P>)
LHW O/B REFUEL PNL 521CB FWD HINGE P/N: 116U4152-5 FOUND WORN.(<P><SPAN>LHW O/B REFUEL PNL 521</SPAN>CB FWD HINGE P/N: 116U4152-5 WORN AREA TIME-LIMIT REPAIRED IAW RI-52-00-16187 REV.A.</P>)
APU COMPARTMENT LH STA 2664.19 FRAME FOUND CRACKED (AT ELECTRICAL CABLE ATT BRACKET AREA).(<P>APU COMPARTMENT LH STA 2664.19 FRAME WL 305 CRACK AREA REPAIRED IAW RI-53-82-16186 REV.A.&NBSP;</P>)
RH WING NO.18 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(<P><SPAN>REPAIRED WITH ADHESIVE PASTE AS PER&NBSP;</SPAN><SPAN>CMM 57-55-42</SPAN></P>)
LHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-159 FOUND ELONGATED.(<P>LHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-159 FABRICATED AND REPLACED IAW RI-52-49-16198 REV.A</P>)
RHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-157 FOUND ELONGATED.(<P>RHW REFUEL PANEL I/B ROD CLEVIS PN: <SPAN>116U4252-157 FABRICATED AND REPLACED IAW RI-52-49-16197 REV.A</SPAN></P>)
LH HORI. STAB. TIP FAIRING AFT WEDGE U CHANNEL FOUND CRACK(<P>U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16182 REV.A</P>)
RH HORI. STAB. TIP FAIRING AFT WEDGEÃÂ U CHANNEL FOUND CRACK(<P>U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16183 REV.A</P>)
LOGPAGE 1669079 ITEM 6, AIRCRAFT WAS STRUCK BY A CARGO CONTAINER @ APPROX STATION STRINGER 44 AFT OF CARGO DOOR(<P>LOGPAGE 1669079 M6: EVALUATING DAMAGE AT STA 2100 TO STA 2120 STR 44 AFT OF BULKHEAD CARGO DOOR; REMOVED "BKND-OUT" GOUGE AT FUSELAGE AND ELEVATED DENT. AFTER FURTHER INSPECTION, FOUND DAMAGE TO BE OUT OF LIMITS IAW B747 SRM 53-00-01. (WAITING ON FURTHER INSPECTION PER ENGINEERING).</P> / <P>LOGPAGE 1669080 M9: PERFORMED HFEL ISPECTION OF BLEND REPAIR AREA ON R/H FUSELAGE STATION 2120 STR 44R AFT OF CARGO DOOR. IAW B747 NOT MANUAL PART 6 51-00-00, NO DEFECTS NOTED AT THIS TIME. TOLEDO JET CENTER CRS 2TJR420B W/O 83165 S.S. 2855439. SEE LP 1669083 IEM 18 FOR CONTINUED INSPECTION.</P> / <P>LOGPAGE 1669081 M13: C/W BLEND REPAIR IAW 63-00-01-1A-1 SHARP EDGES BROKEN PER BAC 5330 HFL C/W ON LP 1669080 ITEM 9. NO FURTHER DEFECTS NOTED.</P> / <P>LOGPAGE 1669082 M17: COMPLIED WITH ATLAS AIR E.O. 4853A156 PART 1 PERMANENT REPAIR.</P> / <P>LOGPAGE 1669083 M18: PERFORMED CONDITIONAL INSPECTION (GROUND HANDLING EQUIPMENT HITS THE AIRPLANE INSPECTION) IAW AMM TASK 05-51-59. FOR DAMAGE AT STA2100 TO 2120 STR 44 AFT OF BULK CARGO DOOR FOUND DAMAGE TO BE OUT OF LIMITS PER SRM 53-00-01. REFRENCE LP 1669082 M17 FOR CONTINUED ACTION.</P>)
MAIN CARGO SMOKE DETECTOR MID 11 INOP(PLACED ON MDR 165471 IAW MEL 26-14-01-04A, CAT C.REMOVED AND REPLACED MAIN DECK MID SMOKE DETECTOR #11 IAW AMM 26-14-01/401. OPS CHECK NORMAL. THIS CLEARS MDDR 165471.)
EICAS "GEAR TILT." UNABLE TO RETRACT LANDING GEAR AFTER TAKE OFF.(<P>FOUND THE RIGHT HAND BODY GEAR TRUCK POSITION ACTUATOR BROKEN. REMOVED AND REPLACED RIGHT HAND BODY GEAR TRUCK POSITION ACTUATOR IAW 32-13-15.</P>)
CRACK ON RIB OF RH WING OF FIXED TRAILING EDGE AT WBL 448.7(<P>ACCOMPLISHED EI NO T2021A57M-861 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)
DEVIATION FOUND DURING PERFORM 747-8F SRM 53-00-01 REPAIR 1 ON FUSELAGE SKIN NEAR STA 680 BETWEEN S-31R AND S-33R.(<P>ACCOMPLISHED EI NO T2021A53M-1021 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
DENT - PNL, V-STAB, LH SURFACE, FS 130, BSTA 2130(<P>CUT OUT THE DAMAGED AREA AND CLEAN. MEASURE THE DAMAGED AREA (DIA = 2", D = 0.01", 28.5" FROM FWD EDGE, 10" FRO UPR EDGE AT V-STAB, L/H SURFACE. FS130 BSTA 2130) BOND FILLER AND REPAIR DOUBLER (DIA&NBSP; = 5", AS A CIRCLE) WITH FILM ADHESIVE. CURE AT 250 DEGREES F FOR 120 MINUTES AND MAINTAIN A MINIMUM VACUUM AT 20 IN/HG IAW B747-8F SRM 55-30-01-1A-1 REFER TO SRM 51-70-10-2R-0 AND SRM 51-70-10-2R-4 REV. 33. CONDITION CHECK IS SATISFACTORY.</P>)
CRACK DAMAGE ON THE STRINGER S-8R BETWEEN STA 830 AND STA 910.(<P>ACCOMPLISHED EI NO T2021A53M-871 REV 1 AND ITS ATTACHING WITH WO 5672202. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
FOUND WIRE WS95-328-20R / W895-329-20B / WS95-330-20Y AND W895-334-20R / W895-335-20B / W895-336-20Y WIRE TOUCH WITH STRUCTURE AND DAMAGE NEAR CONNECTOR DV 744 #2 RAM AIR INLET ACTUATOR(<P>IAW SMM 21-622-03-00-801 / 21-62-03-400-801 REV 35, WDM 21-62-21 REV 23, SWPM 20-30-12, 20-63-21, 20-30-11, 20-60-06, 20-10-11, 20-10-12 REV 76 REPLACED WIRE W895-318-20R / 329-20B / 330-20Y AND W895-334-20R-335-20B / 336-20Y, CONDITION CHK NORMAL. IAW WDM 21-62-21 REV 33 PERFORM WIRING CONTINUITY CHK AND THE RESULT WAS SATISFACTORY. IAW AMM 21-62-03-400-801 REV35 PERFORM TEST OF #2 RAM AIR INLET DOOR ACTUATOR, THE RESULT WAS SATISFACTORY.</P>)
CRACK DAMAGE ON THE STRINGER S-20R, AT AFT SIDE OF STA 2180(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-935 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U2181 SH 392 REV A AND 146U2200 SH 164 REV -. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK ADAMAGE ON THE STRINGER S-12R, AT FWD SIDE OF STA 1960(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-922 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1961 SHEET 465 REV B AND 146U1312 SH 123 REV -. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-22R, AT FWD SIDE OF STA 1960(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-924 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1323 SH 105 REV -, AND 146U1961 SH 615, 614 - . CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGERS S-9R, AT AFT SIDE OF STA 2180(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-934 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U3481 SH63 REV -, 146U3922 SH 21 REV - AND 146U2200 SH 120 REV C. CONDITION CHK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER -19R, AT FWD SIDE OF STA 1960.(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-923 REV 1. REINSTALL THE FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U3732 SH 36 REV A, 146U1961 SH 614 REV -, 146U1961 SH 615 REV - 146U1940 SH 179 REV -. CONDITION CHK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-23R, AT FWD SIDE OF STA 1960.(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-925 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1323 SH 105 REV - AND 146U1961 SH 484 REV -. CONDITION CHK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-20R, AT FWD AND AFT SIDE OF THE STA 1740(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-915 REV 1. REINSTALL FASTENER IAW SRM 51-40-02 REV 33 AND DWG NO 146U1741 SH 324, 325, 326 REV -, 146U1720 SH 80 REV B AND 146U1323 SH 96 REV -. CONDITION CHK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-21R, AT FWD AND AFT SIDE OF STA 1740(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-916 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1741 SH 324 REV -. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON STRINGER S-25R, AT FWD AND AFT SIDE OF STA 1740(<P>REPAIRED DAMAGE AREA IAW EI NO T2021A53M-919 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1741 SHEET 327 REV A. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-13R, AT AFT SIDE OF STA 740.(<P>ACCOMPLISHED EI NO T2021A53M-878 REV 1. INSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND BOEING DWG NO 142U0741 SHEET 423 REV - AND BOEING DWG NO 142U1312 SHEET 1 REV A. CONDITION CHK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-15R AT AFT SIDE OF STA 740.(<P>ACCOMPLISHED EI NO T2021A53M-879 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND BOEING DWG NO 142U3736 SHEET 24 REV -. CONDITION CK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-22R, AT FWD SIDE OF STA 1740(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-917 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1741 SH 324, 325 REV -, 146U1720 SH 79 REV B. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-23R, AT FWD SIDE OF STA 1740.(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-918 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02, REV 33 AND DWG NO 146U1741 SH 324, 325 REV - AND DWG NO 146U1720 SH 79 REV B. CONDITION CHK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER 2-9R, AT FWD SIDE OF STA 1960(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-920 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1961 SHEET 511 513 REV B, 146U1940 SHEET 173 REV -. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-19L, AT AFT SIDE OF STA 1960.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33, ACCOMPLISHED EI NO T2021A53M-929 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1980, SHEET 86 REV B. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-13L, AT AFT SIDE OF STA 2180(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-937 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U2181 SHEET 368 REV C. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-17L, AT AFT SIDE OF STA 2180.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-938, REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U2200 SHEET 154 REV -. JOB COMPLETED AND CONDITION CHK NORMAL</P>)
CRACK DAMAGE ON THE STRINGER S-23L, AT FWD SIDE OF STA 1960.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-933 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1365 SHEET 20 REV A AND 146U1365 SHEET 30 REV A. JOB COMPLETD AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON STRINGER S-20L, AT FWD SIDE OF STA 1960.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-930 REV 1. REINSTALLED FASTENER IAW SRM 51-40-02 REV 33 AND DWG NO 146U1940 SHEET 206 REV -. JOB COMPLETED AND CONDITION CK NORMAL.</P>)
CRACK DAMGE ON THE STRINGER S-21L, AT AFT SIDE OF STA 2180(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-939 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U2200 SHEET 153 REV -. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-11R, AT FWD SIDE OF STA 1960(<P>REPAIRED DAMAGE AREA IAW EI NO T2021A53M-921 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1961 SH511, 513, REV B AND 146U1961 SH465 REV B. CONDITION CHK NORMAL AND JOB COMPLETED.</P>)
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 930 - STA 950, S-9L(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-872, REV 1. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 950 - STA 980+30, S-9L(<P>ACCOMPLISHED EI NO T2021A53M-872, REV 1 AND EI ATTACH TO WO NO 5670098 (367). JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGES ON THE STRINGER AT S-46R STA 2604(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-1016 REV 1. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGES ON THE STRINGER S-42L NEAR STA 2606.(<P>REPAIR DAMAGE AREA IAW EI NO 52021A53M-1013 REV 1. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGES ON THE STRINGER S-42R NEAR STA 2605.(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-1015, REV 1. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER AT S-46L, STA 2604(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-1014 REV 1. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON STRINGER S-21L AT FWD SIDE OF STA 1960.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-931 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1365 SHEET 20 REV A AND 146U1365 SHEET 30 REV A. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-10L, AT FWD SIDE OF STA 1960.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-926 REV 1. REINSTALLED FASTENER IAW SRM 51-40-02 REV 33 AND DWG NO 146U1940 SHEET 206 REV -. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-12L, AT FWD SIDE OF STA 1960.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-927 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1940 SHEET 206 REV -. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-23L, AT FWD SIDE OF STA 2180.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 22. ACCOMPLISHED EI NO T2021A53M-940 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U2160 SHEET 158 REV C. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON STRINGER, S-22L, AT FWD SIDE OF STA 1960.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-932 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1961 SHEET 470 REV A AND 146U1961 SHEET 556 REV - AND 146U1961 SHEET 558 REV -. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK DAMAGE ON STRINGER S-17L, AT FWD SIDE OF STA 1960(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 22. ACCOMPLISHED EI NO T2021A53M-928 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1940 SHEET 206 REV -. JOB COMPLETD AND CONDITION CHK NORMAL.</P>)
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 870 - STA 890, S-7L(<P>REPAIR DAMAGED AREA IAW EI NO T2021A53M-867, REV 1. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 850 - STA 890, S-10L(<P>REPAIR DAMAGED AREA IAW EI NO T2021A53M-874, REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 870 - STA 910, S-11L(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-876, REV 1. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 930 - STA 970, S-8L(<P>ACCOMPLISHED EI NO T2021A53M-870, REV 1 AND EI ATTACHING WITH WO NO. 5670088 (365). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 870 - STA 890, S-8L(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-870 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-12L, AT AFT SIDE OF STA 2180.(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-936 REV 1. REINSTALLED FASTENER IAW SRM 51-40-02 REV 33 AND DWG NO 146U1312 SHEET 113 REV - . JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-18R, AT FWD SIDE OF STA 1740(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-914 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1741 SHEET 325, REV - AND DWG NO 146U11620, SH80 REV B. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-8R BETWEEN STA 930 AND STA 980+30(<P>ACCOMPLISHED EI NO T2021A53M-871 REV 1 AND ITS ATTACHING WITH WO 5672202. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-8R BETWEEN STA 790 AND STA 810(<P>ACCOMPLISHED EI NO T2021A53M-871 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-10R BETWEEN STA 870 AND STA 890(<P>ACCOMPLISHED EI NO T2021A53M-875 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-9R BETWEEN STA 930 AND 950(<P>ACCOMPLISHED EI NO T2021A53M-873 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-9R BETWEEN STA 870 AND STA 910.(<P>ACCOMPLISHED EI NO T2021A53M-873 REV 1 AND ITS ATTACHING WITH WO 5671454 (372). CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-11R BETWEEN STA 810 AND STA 890(<P>ACCOMPLISHED EI NO T2021A53M-877 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-7R BETWEEN STA 930 AND STA 970(<P>ACCOMPLISHED EI NO T2021A53M-869 REV 1 AND ITS ATTACHING WITH WO NO 5672759. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-7R BETWEEN STA 850 AND 890(<P>ACCOMPLISHED EI NO T2021A53M-869, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK DAMAGE ON THE STRINGER S-6R BETWEEN STA 770 AND STA 790(<P>ACCOMPLISHED EI NO: T2021A53M-866 REV. 1. CONDITION CHECK NORMAL AND JOB COMPLETED,</P>)
BIRD STRIKE HALFWAY DOWN RW 27 JUST PRIOR TO ROTATE. MCC DIRECTED TO RETURN TO CVG FOR MX INSPECTION. BIRD STRIKE AREA IS NOSE/CARGO DOOR (RT SIDE) STA 200/RWL 250 AND RWL 312. AFFECTED AREA HAS BEEN CLEANED AND INSPECTED, NO DAMAGE FOUND. ENGINES AND AIRCRAFT WALKAROUND (DVI) HAS BEEN PERFORMED. NO DAMAGE FOUND IAW B747-8 AMM 05-51-19-202-001.
FLIGHT CREW REPORTED TO HKG MX THAT NR 3 ENGINE DID NOT SPOOL UP ON TAKE OFF, BUT SECOND TRY WAS NORMAL. DISCUSSED WITH PPE, AND DOWNLOADED QAR DATA FOR REVIEW.
REPEAT WRITEUP - REF LOG PAGE 1127088. DURING TAKEOFF ROLL AND ENGINES ACCELERATING TO TAKEOFF&NBSP;THRUST, COMPRESSOR STALL EITHER #1 OR #2 AT A LOW SPEED 30 KNOTS. A FLASH OF LIGHT WAS VISABLE ALSO.(<P>ENGINE 1 REMOVED AND REPLACED&NBSP;IAW GE 8130 FORM 20398. OPS CHECK ACCOMPLISHED IAW PRE-TESTED ENGINE AMM 71-00-00-710-802-GOO. ALL TESTS PASSED.</P>)
DURING TAKE OFF ROLL AND ENGINE ACCELERATING TO THRUST, SUSPECT COMPRESSOR STALL ON EITHER 1 OR 2.(<P ><SPAN>C/W ECM #2020P-176 AND / 2020P-174. NO DEFECTS NOTED.</SPAN></P>)
APU COMPARTMENT R/H STA 2696 CONDUIT SUPPORT BRACKET MOUNTED FRAME CRACKED.(<P>APU COMPARTMENT R/H STA 2696 WL 292, LOWER SUPPORT FRAME CRACK AREA REPAIRED IAW RI-53-82-13469 REV. A.&NBSP;&NBSP;</P>)
LHW L/E CAVITY SUPPORT STRUT UPPER MOUNTING HOLE FOUND ELONGATE AT ILES 398, UPPER BEAM.(<P>LHW L/E CAVITY SUPPORT STRUT AT ILES 398 - 404.55 RIB FASTENER HOLES ELONGATION AREAS REPAIRED IAW RI-53-82-13469 REV. A.&NBSP;</P>)
LHW L/E CAVITY SUPPORT STRUT UPPER MOUNTING HOLE FOUND ELONGATE AT ILES 440, UPPER BEAM.&NBSP;(<P>LHW L/E CAVITY SUPPORT STRUT AT ILES 440 - 442.84 RIB FASTENER HOLES ELONGATION AREA REPAIRED IAW RI-53-82-13469 REV. A.&NBSP;&NBSP;</P>)
NO.2 PYLON CAVITY REAR SPAR BOTTOM AREA WING FIXED LEADING EDGE VAPOR BARRIER CRACK AT I/B NACELLE AREA.&NBSP;(<P>NO.2 PYLON CAVITY REAR SPAR BOTTOM AREA WING FIXED LEADING EDGE VAPOR BARRIER CRACK AT I/B NACELLE AREA REPAIRED IAW SRM 57-41-01-2R-6 REPAIR 6, TEMPORARY REVISION 57-105.</P>)
UPPER DECK PORTABLE ELT ROPE DAMAGED. THE PORTABLE ELT WAS REMOVED AND REPLACED IAW AMM 25-63-03.
NR 3 PYLON CAVITY VAPOR BARRIER FWD OTBD SUPPORT, CRACKED. REPAIRED IAW RI-57-41-10697, REV A.
RIGHT WING NR 5 FLAP TRACK, FWD UPPER FIXED PANEL OTBD CHANNEL AFT SIDE FOUND CRACKED. REPAIRED IAW RI-57-22-11773, REV A.
STATUS HYDRAULIC PRESSURE ENGINE 2 AND EICAS HYDRAULIC QTY LOW 2. REMOVED ENGINE 1 EDP AND INSTALLED ON 2 ENGINE IAW AMM 29-11-05. OPS CHECK AND LEAK CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.
AFTER TAKEOFF HYDRAULIC QTY LOW 4 EICAS MESSAGE. RAN ECL NR 4, SYSTEM OFF. REF LP 812459, ITEM 11. FOUND NR 4 ADP HYDRAULIC PUMP LEAKING. R & R NR 4 ADP AND OPS AND LEAK CHECKS OK IAW MM 29-11-17.
DURING TAKEOFF ROLL RECEIVED AURAL WARNING, MASTER CAUTION LIGHT & EICAS ALERT MSG CONFIG. PERFORMED REJECTED TAKEOFF AT APPROX 145 KNOTS. FOUND CMC MSG 277791. PERFORMED TROUBLESHOOTING IAW AMM 27-00-00 & FOUND JUMPER AT LE PANEL OPEN. R & R JUMPER WERE PERFORMED LE & FAILURE INDICATION TEST IAW AMM 27-89-00, FOUND SATISFACTORY.
REJECTED TAKEOFF AT 60KTS DUE TO CONFIG SPOILER EICAS WARNING. CUT OUT INSPECTION OF SPOILERS & CARRIED OUT OPERATIONS CHECK OF SPOILERS IAW AMM 27-61-00-715-001 & ALL SATISFACTORY.
ENGINE NR 1 OIL QTY GRADUALLY WENT DOWN TO ZERO, ALL OTHER INDICATIONS, OIL PRESS & TEMP WERE NORMAL. PERFORMED OPEN & CLOSED COWL INSPECTION IAW AMM 79-00-00, NO LEAKS NOTED AT THIS TIME. PERFORMED ENG DRY MOTOR IAW AMM 71-00-00 TEST 2, NO LEAKS NOTED AT THIS TIME. IAW MCC & TASK 71-71-00 CAPPED IDG PAD DRAIN.
DENT ON FUSELAGE SKIN AT STATION 516 BETWEEN STRINGER 35R - 36R. REPAIRED DAMAGE AREA IAW EI NO T2015A53B-390 REV 1. JOB COMPLETED & CONDITION CHECKED NORMAL.
NUMBER 1 PACK PRODUCES AN ODD SMELL AS IF THERE IS ELEC BURNING. VISUAL INSPECTION AT PACKS INLET & OUTLET AT PACK 1 BAY, NO ABNORMALITIES NOTED. REF ITEM 3 DETAILED INSPECTION ACCOMPLISHED & FOUND EE SUPPLY FAN AT FAULT. FAN DEACTIVATED & OPERATIONS CHECKED OF ALL PACKS NORMAL. NO BAD ODOR OR SMOKE NOTICE. EE SUPPLY FAN TRANSFERRED TO MDDR 54582 IAW DDG 21-58-06 CAT C.
GEAR TILT STATUS MSG, GEAR WOULD NOT RETRACT AFTER TAKE TAKEOFF, QRH CHECKLIST ACCOMPLISHED. R & R L/B TRUCK TILT LEVER LOCK PROX SENSOR S2653 IAW AMM 32-61-12. ADJUSTED SENSOR IAW AMM 32-61-12. OPERATIONS NORMAL IAW AMM 32-61-00 & 32-31-00.
INADVERTENT ENCOUNTER WITH ICE CRYSTALS, NR 2 ENG ROLLED BACK. PERFORMED BORESCOPE INSPECTION OF ALL HIGH PRESS COMPRESSOR BLADE AIRFOILS OF THE NR 2 ENG IAW AMM TASK 71-00-00-200-816-G00, AWL 30-099-01 & AD 2013-24-01 PARA J I & SATISFACTORY.