N858GT
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (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
REJECT AT 62 KTS FOR CONFIG WARNING 421.6 KG. SPEED BRAKE ARMED EICAS AND COULD NOT BE RESET AFTER REJECT. VERIFIED INTERNAL SHORT IN SPEED BRAKE ARM SWITCH IAW WDM 32-41-31 & AMM 20-11-00. R & R SPEED BRK ARM SWITCH IAW AMM 27-62-10. OPS CHECK NORMAL. THIS CLEARS DMI 251286, PLACARD REMOVED.
#8 TIRE PRESSURE ADVISORY MESSAGE - TIRE PRESSURE DECREASING.(<P>FOUND #8 MAIN TIRE PRESSURE LOW. REMOVED AND REPLACED #8 MAIN WHEEL ASSY PER AMM 32-45-01. ALSO, REPLACED #7 MAIN WHEEL ASSY PER AMM 32-45-01. OPS & LK CHK OK</P>)
MULTIPLE GEAR MESSAGES INCLUDING GEAR MONITOR, GEAR DISAGREE, AND GEAR DOOR AND GEAR WOULD NOT RETRACT. R & R PSEU & PERFORMED CMC GND TEST & ZONAL INSPECTION OF NOSE LANDING GEAR & NOSE LANDING GEAR DOOR IAW AMM 32-09-03/401 & AIPC 32-61-01-01, OPS CHK GOOD. NO FURTHER DEFECTS NOTED.
AT FLT 310, CABIN PRESSURE BECAME UNCONTROLLABLE. OUTFLOW VALVES WERE INDICATING FULLY CLOSED. CABIN ALTITUDE WAS CLIMBING 200 FPM.(<P>COMPLETED THE FOLLOWING CHECKS PER BOEING SR: CABIN SYSTEM CONTROL PRESSURE TEST AMM TASK 21-31-00-735-011 AND EXCESSIVE CABIN PRESSURE LEAKAGE TEST PER AMM 05-51-08-702-001. PARTS REPLACED. REF AMM 21-26-15/401. R & R FWD CARGO OVERBOARD VALVE.
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 892, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50659 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50659 ATTACH WITH T/C: 11454336. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880, S-10R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50669 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 866, S-10R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50669 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50669 ATTACH WITH T/C: 11454311 (098) 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 840, S-11L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 860, S-11L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50664 ATTACHING WITH THE T/C 11454296. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT AFT OF STA 1660, S-10R.(<P>1. ACCOMPLISHED EI NO. T2025A53M-1965 REV 1. 2. ACCOMPLISHED EI NO. T2025A53M-1965 REV 2. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880 S-10L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50671 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 780 S-10L.(<P>1. PERFORMED EI NO. T2025A53M-1973 REV 1 SEQUENCE A & B. 2. ACCOMPLISHED EI NO. T2025A53M-1973 REV 2 & T2025A53M-1909 REV 1. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 760 S-8L.(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 46. 2. PERFORM EI NO. T2025A53M-1990 REV 1 SEQUENCE B. 3. INSTALL AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 46 AND DWG NO. 142U3625 SH 13 REV - & 142U3440 SH 14 REV B & 142U3725 SH 10 REV B. 4. ACCOMPLISH EI NO. T2025A53M-1990 REV 2. 5. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK BETWEEN STA 2177 AND STA 2185 S-8R.(<P>1. PERFORM STRINGER REPAIR IAW W/S NO. 50672 AND SRM 53-60-03-2R-3 REV 46/ TR: 53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER CRACK FRAME FWD SIDE BETWEEN STA 1957 AND STA 1966 S-9R.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50674 AND SRM 53-60-03-2R-4 REV 46/ TR: 53-155. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT AFT OF STA 2180, S-11R.(<P>1. PERFORMED STRINGER REPAIR IAW W/S NO. 50658 AND SRM 53-60-03-2R-3 REV 46/ TR: 53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
FOUND STRINGER CRACK ON S-11L STA 885. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S 50664 ATTACHING WITH THE T/C 11454296. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
FOUND EMERGENCY LIGHT BATTERY (M5169) FUNCTION FAIL AND CAN NOT RE-CHARGE.(<P>REPLACED POWER SUPPLY ASSY AND PERFORM POWER SUPPLY INSTALLATION TEST IAW AMM 33-51-04-000-803, AMM 33-51-04-400-803 AND AMM 33-51-04-900-803 REV 48A. THE RESULT WAS SATISFACTORY.</P>)
FOUND RH WLG ALTERNATE EXTENSION ACTUATOR FUNCTION ABNORMAL.(<P>1. REPLACED RH WLG ALTERNATE EXTENSION ACTUATOR IAW AMM 32-36-01-004-001 REV 48A AND AMM 32-36-01-404-009 REV 48A. 2. PERFORMED R/H WLG ALTERNATE EXTENSION TEST IAW AMM 32-36-00-705-009 REV 48A, TEST RESULT WAS PASS. 3. CONDITION CHECK SATISFACTORY.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 860, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50667 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FOUND STRINGER HAVE CRACK AT FWD OF STA 2598 S-6R.(<P>1. REMOVED FASTERNERS IAW SRM 51-40-02-0G-0 REV 46. 2. REPAIR STRINGER IAW W/S NO. 50660 AND SRM 53-80-03-2R-2 REV 46/ TR:53-152. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FOUND STRINGER HAVE CRACK AT FWD OF STA 2598 S-8L.(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 46. 2. REPAIR STRINGER IAW SRM 51-40-02-0G-0 REV 46 & W/S NO. 50661 AND SRM 53-80-03-2R-2 REV 46/ TR:53-152. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER CRACK BETWEEN STA 2177 AND STA 2185 S-10R.(<P>1. PERFORM STRINGER REPAIR IAW W/S NO. 50673 AND SRM 53-60-03-2R-3 REV 46/ TR:53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
FOUND CROWN STRINGER HAVE CRACK AT STA 920, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50666 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
FOUND CROWN STRINGER HAVE CRACK AT STA 905, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50666 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50666 ATTACH WITH T/C:11454301 (095). 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND FUSELAGE CROWN STRINGER HAVE CRACK AT STA 780, S-12R.(<P>1. REPAIR STRINGER AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 746, S-12R.(<P>1. REPAIR STRINGER CRACK AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50663 ATTACH WITH T/C:11454292. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 793, S-12R.(<P>1. REPAIR STRINGER CRACK AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50663 ATTACH WITH T/C:11454292. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880, S-8R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50668 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 980+15, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50670 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 882, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50659 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
AIR TURNBACK DUE TO LOSS OF CABIN PRESSURE.(<P>R+R SMOKE OVERIDE VALVE PER AMM 21-58-06, OPS CHECK GOOD.</P>)
HYD PRESS SYS 4 EICAS. #4 HYD QTY 40%(<P>INSPECTION FOUND #4 HYDRAULIC RETURN FLEX LINE IN THE R/H HORIZONTAL STABILIZER, CLOSE TO THE R/H INBOARD ELEVATOR PCU HAD RUPTURED. REMOVED THE DAMAGED LINE. INSTALLED TEMPORARY FLEX LINE, WITH RE-INSPECTION DUE EVERY 25 FC, AND PERMANENT REPAIR DUE AT NEXT "A" CHECK IN ACCORDANCE WITH GMM 3.24.1.</P>)
#7 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
FLIGHT COMPARTMENT L1 WINDOW STRUCTURE UPPER CHORD CORNER CHORD AT STA 288 BL 1.0 FOUND SLOT(<P>SLOT WAS CONFIRMED A PRODUCTION GAP BETWEEN THE CHORD AND THE CENTER WINDSHIELD POST AS PER ATLAS AIR EO #4853A118 REV 3&NBSP;</P>)
LH I/B ELEVATOR UPPER L/E PANEL DAMAGE 4EA LOCATION(<P>DAMAGE AREA REPAIRED AS PER RI #RI-55-20-16459 REV A. NO FURTHER DEFECTS NOTED</P>)
LH I/B ELEVATOR L/E SKIN ELEV. STA 119.358 PER EA 4855A0004 HAS BEEN REVISED EA 4855A005 PERMANENT REPAIR WITHIN 500 FC PER EA(<P>L/E SKIN REPAIRED AS PER RI #RI-55-20-16459 REV A. NO FURTHER DEFECTS NOTED</P>)
RH HORIZONTAL STAB TIP FAIRING I/B RIB UPPER CHORD CRACK(<P>UPPER CHORD REPLACED AS PER SRM 51-10-02 NEW CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW CHORD INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023 ). NO FURTHER DEFECTS NOTED</P>)
RHW MOST I/B LOWER FIXED PANEL AFT SUPPORT BEAM WBL 128-212 FOUND WORN(<P>SUPPORT BOTH WORN AREA REPAIRED AS PER RI #RI-57-22-16462 REV A. NO FURTHER DEFECTS NOTED</P>)
RH WLG I/B STRUT DOOR FWD EDGE LOWER FITTING WORN AND CRACK(<P>WORN AND CRACK FITTING REPAIRED AS PER RI #RI-52-80-16471 REV A. NO FURTHER DEFECTS NOTED</P>)
LHW MOST I/B T/E LOWER FIXED PANEL AFT SUPPORT AT WBL 128-212 WORN.(<P>SUPPORT WORN AREA REPAIRED AS PER RI #RI-57-00-16461 REV A. NO FURTHER DEFECTS NOTED</P>)
LH WLG I/B STRUT DOOR FWD EDGE LOWER FITTING WORN(<P>WORN FTG REPLACED AS PER SRM 51-10-02 AND NEW FTG HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FTG INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023 ). NO FURTHER DEFECTS NOTED</P>)
M/D STA 1480 +20 - 1480 +40 RBL 75" HAT SECTION FOUND CRACK(<P>HAT SECTION CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-10 REPAIR 10 FIG 201 REV 40, DATE 20 JUN 2023. NO FURTHER DEFECTS NOTED</P>)
APU COMPT LH FRAME STA 2685 CRACKED(<P>FRAME CRACK AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201 REV 40 DATE 20 JUN 2023. NO FURTHER DEFECTS NOTED</P>)
APU COMPARTMENT LH FRAME STA 2664 CRACKED(<P>&NBSP;FRAME CRACK AREA REPAIRED AS PER RI #RI-53-80-16456 REV A. NO FURTHER DEFECTS NOTED</P>)
APU BATTERY COMPT STA 2598 - STA 2618 STR 42R FOUND CRACK(<P>CRACK STRINGER REPLACED AS PER RI #RI-53-80-16468 REV A. NO FURTHER DEFECTS NOTED</P>)
APU COMPT STA 2664 WL 310 R//H FRAME FOUND CRACK(<P>FRAME CRACK AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201 REV 40 DATE 20 JUN 2023. NO FURTHER DEFECTS NOTED</P>)
RH I/B ELEVATOR I/B AFT UPPER SURFACE FOUND DENT MARK(<P>PERFORMED COMPOSITE WET LAYUP REPAIR AS PER SRM 51-70-04 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)
#9 VC FLAP BULL NOSE O/B EDGE FOUND DELAM MARKED(<P>PERFORMED COMPOSITE WET LAYUP REPAIR AS PER SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED</P>)
RHW L/E #3 PYLON TO WING CAVITY VAPOUR BARRIER FOUND CRACK(<P>VAPOUR BARRIER PANEL CRACK AREA REPAIRED AS PER SRM 57-41-01-2R-6 REPAIR 6 FIG 201 TO FIG 204 REV 40 DATE : 20 JUN 2023. NO FURTHER DEFECTS NOTED</P>)
#6 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
LHÃÂ HORIZONTAL STAB O/B T/E WEDGE FWD ATTACH U-CHANNEL CRACK(<P>U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16446 REV A. NO FURTHER DEFECTS NOTED</P>)
#21 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
#19 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER&NBSP;&NBSP;CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
#8 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER&NBSP;&NBSP;CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
#9 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER&NBSP;&NBSP;CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
LWR RUDDER - FX, L/H AFT SEAL TORN(<P>LOCALLY FABRICATE REPAIR IAW RI #RI-53-00-16472 REV A. NO FURTHER DEFECTS NOTED</P>)
STATUS MESSAGE ENG 2 OIL SYS(<P>COMPLETED LOW PRESSURE INSP PER AMM 71-00-00 NO DEFECT. GBX INSP COMPLETED PER 72-60-00 NO DEFECT.</P> / <P>ADDITIONAL INSP FPI OF #2 ENG OIL SUPPLY TUBE PER BOEING SPM 70-11-06 NO DEFECTS. OIL CAP INSP PER AMM 12-13-03 NO DEFECTS. REPLACED OIL FILTER PER AMM 79-21-07.</P>)
ATB - AFTER TAKE-OFF NOSE GEAR FAILED TO RETRACT.(<P>TRANSFERRED TO MDDR 155894 IAW MEL 32-30-01, CAT B.</P>)
LHW NO.7 V/C FLAP TRANSLATING WIRE LINK BRACKET FOUND DAMAGED(<P>LHW NO.7 V/C FLAP WIRE LINK BRACKET REPLACED AS PER RI-57-00-15033 REV. A.</P>)
EMP - RH HORI STAB TIP FAIRING T/E SUPPORT CHANNEL 2 PLACES CRK(<P>REPLACE THE CRACKED CHANNEL IAW&NBSP;<SPAN>RI 55-10-14999.</SPAN></P>)
L/G - L/H WLG FORWARD SECONDARY DOOR L/E HEAT SHIELD ASSEMBLY EXT. SKIN FOUND DELAMINATION(<P>DELAMINATION AREA PERFORMED REPAIR AS PER RI-52-80-15004 REV A.</P>)
AFT CARGO STA 1920-1980 L/R CEILING FOUND TORN (2EA)(<P>AFT CARGO STA 1920-1980 L/R CEILING REPLACED AS PER AMM 25-52-01 , LH CEILING LINER REPLACED IAW RI-25-54-15034 REV.A</P>)
NO. 8 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)
NO. 19 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)
FWD CARGO DOOR CONTROL SWITCH CHANGE (GROUP 1) THE 4EA EXISTING CLIPS COMMON TO THE STRINGERS FOUND MISMATCH SB.(<P>4EA EXISTING CLIPS INSTALL IAW RI-52-00-14998 REV A</P>)
NO. 6 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1.</P>)
NO. 21 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)
NO. 7 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)
MAIN DECK SIDE CARGO DOOR LATCH FRAME SPLICE INTERCOSTAL WEB (146U6145-1), DOUBLER (65B17613-30), AND INNER CHORD (146U6157-10) - CRACK DAMAGE AT STA 1707 WL210 TO WL200 - CAT C REPAIR(<P ><SPAN>PERFORMED TIME LIMITED / REPAIR OF MAIN DECK SIDE CARGO DOOR IAW EO&NBSP;1952A330 PART 1, FABRICATED AND / INSTALLED&NBSP; 0.140" THICK REPAIR STRAP ON THE SHAPE OF INTERCOSTAL / INNER CHORD 146U6157-10</SPAN></P>)
BODY GEAR STRG EICAS AND STATUS. FOUND LT BODY GEAR INBOARD STEERING ACTUATOR DAMAGED. REMOVED AND REPLACED L BODY / GEAR INBOARD STEERING ACTUATOR IAW AMM 32-53-11, SYSTEM OPS CHECK / GOOD.
AFTER TAKE-OFF EICAS MESSAGE "GEAR TILT". RETURNED TO AIRPORT.(<P ><SPAN>REPLACED BODY GEAR SENSOR (OFF PART: PN 8-935-01, NSN) AND FOUND LT BODY GEAR TRUCK TILT HYDRAULIC LINE LEAKING. REPLACED FLEX LINE / WITH TEMPORARY LINE PER GMM 3.24.1. PERFORMED LEAK CHECK IAW B747 AMM 32-33-00.</SPAN></P>)
CRACK - FOUND LT HST TIP FAIRING RIB CRACKED AT STAB BL 435, YB410-YB430, TTL: 3EA. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PARTS IAW SRM 51-40-02 REV 28 AND DWG NR 65B03521 SHEET 06. JOB COMPLETED AND CONDITION CHECKS NORMAL. OFF PARTS (PN:65B03521U9, SN: NSN) & (PN:65B03521Y11, SN NSN)
CRACK - FOUND RT HST TIP FAIRING RIB CRACKED AT STAB BL 435, YB410~YB430, TTL=2 EA. REMOVED THE DAMAGE RIBS IAW SRM 51-40-02 REV 28. INSTALLED THE NEW RIBS IAW SRM 51-40-02 REV 28, DWG NR 65B03521 SH6 AND SH7. JOB COMPLETED AND CONDITION CHECK NORMAL. OFF PART (PN: 65B03521Y12, SN: NSN) CRACK LENGTH= 0.5", 5"
BROKEN - BOLT, LOWER FUSELAGE STA 1243, PRESSURE BULKHEAD FASTENER RBL 120. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PART IAW DWG NO 65B07992, SH 115 & SRM 51-40-02 REV 28. JOB COMPLETED AND CONDITION CHECKS NORMAL.
CRACK ON LOWER CHORD OF HORIZONTAL STABILIZER, RT TIP, AT STAB BL 421.5. REPAIRED DAMAGED AREA IAW EI NR T2019A55M-3713 REV 2. JOB COMPLETED AND CONDITION CHECKS NORMAL.
CRACKS ON LOWER CHORD, UPPER CHORD, AND WEB OF LT SIDE HORIZONTAL STABILIZER; TRAILING EDGE AT STAB BL 421.5. REPAIRED DAMAGED AREAS IAW EI NO T2019A55M-3727 REV 3. JOB COMPLETED AND CONDITION CHECKS NORMAL. CRACK LENGTH 0.5", 3", 5"
CRACK - FOUND RT HST TIP FAIRING RIB CRACKED AT STAB BL 435, YB 420. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PART IAW SRM 51-40-02 REV 28 AND DWG NR 65B03521 SHEET 06. JOB COMPLETED AND CONDITION CHECKS NORMAL.
CRACK - FOUND LT HST TIP FAIRING CRACKED AT STAB BL 435, YB400-YB410, 1 EACH. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PART IAW SRM 51-40-02 REV 28 AND DWG NR 65B03521 SHEET 06. JOB COMPLETED AND CONDITION CHECKS NORMAL.
BROKEN - BOLT, LOWER FUSELAGE STA 1243, PRESSURE BULKHEAD FASTENER LBL 120. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PART IAW DWG NR 65B07992, SH 113 AND SRM 51-40-02 REV 28. JOB COMPLETED AND CONDITION CHECKS NORMAL.
WORN - FASTENER HOLES ON THE RT WING, L/E RIB AT IFSS 443.67. ACCOMPLISHED EI NO T2019A57M-3618 REV 1. JOB COMPLETED AND CONDITION CHECKS NORMAL.
CORROSION - PLATE, LOWER FACE OF UNDER MAIN DECK CARGO FLOOR, STA 2359 LBL 50. ACCOMPLISHED RPL PLATE AT LWR FACE OF UNDER M/D CGO FLOOR STA 2359, LBL 50 IAW AMM 51-41-12-202-037 REV 30. CONDITION CHECKS NORMAL. ADAPTER PART OFF (PN: 65B17393-13, SN: NSN)
1 HOUR INTO FLIGHT "ENGINE 2 OIL SYSTEM" STATUS. 2 HOURS IN FLT FLT COMPACT ENG INDICATIONS DISPLAYED ON LOWER EICAS. ENGINE 2 READING NORMAL, OIL PRESSURE 27-30 PSI, APPROXIMATELY 7 HOURS INTO FLT ENG 2 OIL DISPLAYED OIL FILTER STATUS MESSAGE. ALL ENG 2 INDICATIONS STILL THE SAME. IN DESCENT GOT "OIL FILTER ENG 2" STATUS. (<P>UPON ARRIVAL CHECKED #2 ENGINE OIL TANK FILLER CAP, FOUND FILLER CAP OPENED. INSPECTED FILLER CAP & O-RING, NO DAMAGE FOUND. PER ECM ITEM 2019P-307, PERFORMED DVI #2 ENGINE OIL FILTER ELEMENT, MAG CHIP DETECTORS, OIL SYSTEM FLUID, NO CONTAMINATES, DMS SENSORS, NO TROUBLE FOUND, CLEANED DMS SENSOR, REPLACED OIL FILTER, C/W IDLE LEAK CHECK, TEST ALL OK PER AMM 71-00-00-790-804-GOO. NO EXISTING FAULTS FOUND A/C OK FOR SERVICE. MCC NOTIFIED</P>)
CABIN ALTITUDE EICAS DURING CRUISE, NO EICAS MESSAGE FOUND. STS MESSAGE, & CMC MESSAGE AFT ARR SPOT. BOTH OUTFLOW VALVE TESTED OKAY. ALL DOOR & OUTLETS OK, BOTH CPCS GND TEST PASSED AIW AMM 21-31-00/501. DOOR & SEAL INSPECTED OF ALL REVR AND OUTFLOW IAW AMM 52-11-00, 52-34-00, 52-36-00, AND 52-48-01.
EICAS MESSAGE, GEAR TILT AFTER TAKEOFF MSG, EXTINGUISHED AFTER A FEW SECONDS. GEAR RETRACTED NORMAL, FOUND CMC MSG, 32723 INTERMITTENT FAULT NOT ACTIVE PERFORMED BODY GEAR TRUCK TILT SENSOR TEST OF LT BODY GEAR IAW AMM 32-61-12-820-801 FOUND SENSOR AND TARGET AT PERMITTED MEASURED CLEARANCE AT 3.9MM. ALSO, PERFORMED PSEU CMC GROUND TEST IAW AMM 32-09-03 TEST PASS.
GEAR TILT EICAS, PERFORMED ADJUSTMENT/TEST OF THE LT BODY GEAR TRUCK TILT SENSOR IAW AMM 32-61-12-820-801. TEST SATISFACTORY. MEASURED GAP BETWEEN TILT SENSOR AND TARGET AND FOUND OK. ACCOMPLISHED OVERWEIGHT LANDING CONDITION INSPECTION IAW AMM 05-51-39/201. NO DAMAGE NOTED.
FOUND A DENT ON THE EXTERNAL SKIN, NEAR BS 1940, S34R. REPAIRED THE DAMAGED SKIN IAW EI T2015A53B-2112, REV 2. CHECKED NORMAL.
LIGHTNING STRIKE DAMAGE ON THE FASTENERS OF LT FUSELAGE EXTERNAL SURFACE AT BS 200 AND BS 220 BETWEEN S15-16L. REPAIR DAMAGE AREA IAW EI NR T2015A52B-2146, REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
LIGHTNING STRIKE DAMAGE ON THE FASTENER OF LT FUSELAGE EXTERNAL SURFACE AT BS 306, S14L. ACCOMPLISHED EI NR T2015A53B-2157, REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
OIL QUANTITY NR 2 ENGINE DECREASED TO ZERO OVER A 2 HOUR PERIOD, DIVERTED. PRESSURE AND TEMPERATURE STAYED NORMAL. FOUND NR 5 BEARING SCAVENGE TUBE B-NUT LOOSE. TORQUED B-NUT IAW AMM 79-21-09. PERFORMED GROUND RUN AND NO LEAKS NOTED.
LOW SPEED RTO; 20 KTS FOR A MASTER CAUTION MESSAGE. A/T DISCONNECTED. ENTERED RUNWAY, MESSAGE GONE. BRAKE TEMP & LT; 1.0, TAXI BACK NORMAL T/O BUT SLIGHT VARIANCE IN AIRSPEED. ACFT TRYING TO FLY AT V1. AIRSPEED INDICATION JUMPED DURING CLIMBOUT. INFO NOTED AND PASSED TO OTBD CREW. FMC LT AND RT PASS IAW AMM 22-12-00. ADIRU LT, CENTER AND RT CMC TESTS PASS IAW AMM 34-25-00, PITOT STATIC PROBE HEAT TESTS PASS IAW AMM 30-31-00. NO FAULTS OR HISTORY.
ECIAS MESSAGE, FMC AND AUTOTHROTTLE DISCONNECTED BEFORE TAKEOFF, NO PLF MESSAGE NOTED BOTH FMC & IRS SYS; ALL 3 IRU REALIGNED AND FMC LT & RT; GROUND TESTED GOOD. FMC LT & RT SERVO LOOP GROUND TEST ALSO PASSENGER IAW AMM 34-01-00.
DURING NR 5 BALLSCREW LUBRICATION, FOUND A NICK ON NR 5 BALLSCREW. REPLACED NR 5 BALLSCREW ASSY AND OPS CHECK NORMAL IAW AMM 27-51-41.
REJECTED TAKEOFF AT 65 KNOTS DUE TO TAKEOFF WARNING HORN. NO RECORDED FAULT MESSAGES AND NOT RECENT HISTORY; BITE CHECK CARRIED OUT AND SATISFACTORY IAW AMM 31-51-00. TAKEOFF WARNING TEST CARRIED OUT AND SATISFACTORY AMM 31-52-00. FUNCTIONS CHECKED, CONFIG FLAPS, CONFIG TRIM AND CONFIG PARK BRAKE. ALL NORMAL.