N615FE
Registered owner: FEDERAL EXPRESS CORP, TN (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
LH WING LOWER SURFACE (NEAR FOOTSTOOL FITTING) HAS SEVERAL WEAR MARKS. C/W EA 1-5730-T0387611
BRAKE OVERHEAT AFTER LANDING AT 466K LANDING WEIGHT. OVERHEATS ON #4, #7, AND #8 WITH MAX TEMP 596 DEGREES. REMOVED AND REPLACED BRAKE ASSY LEAK AND OPS CHECKED GOOD ACFT OK TO CONTINUE
DOOR 1R EVAC SLIDE , REMOTE PRESSURE LIGHT WILL NOT PRESS TO TEST . RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY : C EXPIRATION : 01NOV24 "MEL 25-61-02: R1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFYAND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY." MEL: 25-61-02 DOOR R1 EVAC SLIDE ,PRESSURE LIGHT WILL NOT PRESS TO TEST. REMOVED AND REPLACED R1 DOOR SLIDE REMOTE PRESSURE INDICATOR ASSEMBLY. OPERATIONAL TEST PASSED. IAW AMM 25-61-04-4.
R-1 DOOR SLIDE PRESS TO TEST CONTINUITY LIGHT IS INOP. FOUND R-1 DOOR SLIDE PRESS TO TEST BATTERY HOLDER WITH CORRSION ON TERMINAL BATTERY ENDS, CLEANED BATTERY HOLDER ENDS AND REMOVED AND REPLACED BOTH BATTERIES,, PER AMM REF 25-64-04-4, PRESS TO TEST CHECKS GOOD. M.E.L. CLEARED.
WHILE PERFORMING POSTFLIGHT WALKAROUND, NOTICED R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS. TRIED TO RELAMP IAW AMM 25-61-04-4, NO HELP. ITEM TRANSFERRED TO MEL DUE TO SHORT GROUND TIME. FURTHER TROUBLESHOOTING REQUIRED. MEL 17JUL24 19:19 CDG RELEASED FOR SERVICE PER MEL : 25-61-02, R1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. ITEM TRASNFERRED TO MEL, SLIDE PRESSURE VERIFIED USING MEL'S METHOD B, BOTTLE GAUGE CHECKED AND FOUND WITHIN GREEN BAND. AIRCRAFT OK TO CONTINUE. AMM: 25-61-04-5--0 VERIFIED EVAC PRESSURE BOTTLE. PRESSURE IN GREEN BAND. REPOSITIONED SLIDE COVER & TESTED PRESSURE LIGHT. LIGHT TEST GOOD. ACFT OK FOR SERVICE
TO CARRY OUT CRACK REPAIR AS PER E.A.#: 1-5310-T0368267 P2 TITLE: FUSELAGE - MAIN FRAME - MAIN DECK CARGO OVERWING FLOOR BEAM AT STA 1256.750 CRACK REPAIR. REPAIR CARRIED OUT AS PER E.A.#: 1-5310-T0368267 A P2, TITLE: FUSELAGE - MAINFRAME - MAIN DECK CARGO OVERWING FLOOR BEAM AT STA 1256.750 CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 53103203 FOR WORK DETAILS.
RIGHT HAND MAIN LANDING GEAR DOOR LOWER UPLATCH FITTIING FOUND CRACK ( 1 EACH FORWARD SIDE) AT STATION 1433.562. RIGHT HAND MAIN LANDING GEAR DOOR LOWER UPLATCH CRACKED FITTING AT STATION 1433.562 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-33-01-0G. FITTING FABRICATED IN ACCORDANCE WITH DOUGLAS DRAWIING # ANB 7089 REVISION A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD JAMB LOWER EDGE DOUBLER FOUND WITH CHAFE, LONGERON 38R - LONGERON 42R AT STATION 895. LOWER FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD JAMB LOWER EDGE DOUBLER LONGERON 38R - LONGERON 42R AT STATION 895 WORK ACCOMPLISHED AS PER EA # 1-5330-T0308320A PT5 TITLE: FUSELAGE - PLATES & SKINS - FWD CARGO DOOR CUTOUT FWD JAMB - EXISTING REPAIR AT STA 895 BETWEEN L - 38R AND L-42R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT JAMB LOWER EDGE DOUBLER FOUND WITH CHAFE, STATION 1002.3,LONGERON 39-42 RIGHT HAND SIDE. LOWER FORWARD CARGO COMPARTMENT DOOR CUTOUT AFT JAMB LOWER EDGE DOUBLER WORK ACCOMPLISHED AS PER EA # 1-5330-T0308423C PART 6. TITLE: FUSELAGE - PLATES & SKINS -FWD CARGO DOOR CUTOUT AFT JAMB - EXISTING REPAIR AT STA 1002.3, BETWEEN L - 39R AND L -42R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LANDING GEAR: WHILE ACCOMPLISHING RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING REPAIR, TRIMMED OUT CRACKED AREA, FOUND STATION 595 LONGERON CRACKED. LANDING GEAR: RIGHT HAND NOSE LANDIING GEAR TRUNNION FITTING AREA CRACKED LONGERON REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-35-01-0G AND SRM 51-33- 01-0G. LONGERON FABRICATED IN ACCORDANCE WITH DRAWIING # ACA 3796 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK - CARGO BARRIER NET LEFT HAND SUPPORT YOKE AT STATION 535 LONGERON 24- LEFT EXISTING REPAIR OUTER ANGLE FOUND CHAFFED. MAIN DECK - AT LEFT HAND FRAME STATION 535 LONGERON 24 LEFT EXISTING REPAIR, CHAFFED OUTER REPAIR ANGLE REMOVED AND REPAIR CARRIED OUT AS PER E.A.#: 1-5310- T0308273 REVISION A PART 2, TITLE: FUSELAGE - MAIN FRAME - EO 1-5100-7-5001 - FORWARD FUSELAGE - EXISTING FRAME REPAIR AT STA 535, LONGERON 24L. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK - CARGO BARRIER NET LEFT HAND SUPPORT YOKE AT STATION 535 LONGERON LONGERON 19 - LEFT EXISTING REPAIR OUTER ANGLE FOUND CHAFFED. MAIN DECK AT EXISTING REPAIR AT LEFT HAND FRAME STATION 535 LONGERON 19 LEFT CHAFED OUTER REPAIR ANGLE REMOVED AND REPAIRED AS PER MD-11 SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - LEADING EDGE LOWER ACCESS PANEL CUTOUT FORWARD EDGE DOUBLER AT STATION XOS 547 FOUND CRACK ABOUT 1". LEFT WING LEADING EDGE LOWER ACCESS PANEL CUTOUT FORWARD EDGE AT STATION XOS 547 CRACKED DOUBLER REMOVED AND REPLACED AS PER MD -11 SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 1180 REVISION Y. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - LEFT HAND SEAT TRACK AT STATION 755, X = 8.5 FOUND CROWN DAMAGED. CABIN - AT LEFT HAND SEAT TRACK STATION 755, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 745 TO STATION 765, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STATION 5-10, X = - 8.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 5-10, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 5-63 TO EXISTING SPLICE STATION 1531/5-0, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 811.623 FOUND CRACK ABOUT 0.4 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 811.623 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SURFACES - LH WING - #6 SLAT ASSY - CRACK RIBS - LOCAL FABRICATION - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STATION 1299, X = - 8.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT, AT SEAT TRACK STATION 1299, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1269 TO STATION 1311, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STATION 5-10, X = 47.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT, AT SEAT TRACK STATION 5-10, X = 47.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1531/5-0 TO STATION 5-15, X = 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STATION 1299, X = 8.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT, AT SEAT TRACK STATION 1299, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1269 TO STATION 1311, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - STATION 1887, X = 2 FLOOR SUPPORT APPROXIMATELY OF 1.5 INCH FOUND CRACK. CABIN AT STATION 1887, X = 2 CRACKED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007, X = 2 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7081 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FOR PART NUMBER EFFECTIVITY E.A.#: 1-5321- T0379171, TITLE: FUSELAGE - CRAGO COMP FLOORS - IPC 53-00-40-01 AND IPC 53-21-43-03,
LEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 837.572 FOUND CRACK ABOUT 0.2 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 837.572 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SURFACES - LH WING - #6 SLAT ASSY - CRACK RIBS - LOCAL FABRICATION - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 842.722 FOUND CRACK ABOUT 0.3 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 842.722 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SURFACES - LH WING - #6 SLAT ASSY - CRACK RIBS - LOCAL FABRICATION - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 863.325 FOUND CRACK ABOUT 0.3 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 863.325 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SURFACES - LH WING - #6 SLAT ASSY - CRACK RIBS - LOCAL FABRICATION - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - STATION 1887, X = 57.5 FLOOR SUPPORT APPROXIMATELY OF 1.50 INCH FOUND CRACK. CABIN - CRACKED FLOOR SUPPORT AT STATION 1887, X = 57.5 REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007, X = 57.5 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FOR PART NUMBER EFFECTIVITY E.A.#: 1-5321- T0379171, TITLE: FUSELAGE - CARGO COMP FLOORS - IPC 53-00-40-01 AND IPC 53-21-43-03
CABIN - STATION 1887, X = 24 FLOOR SUPPORT APPROXIMATELY OF 1.50 INCH FOUND CRACK. CABIN AT STATION 1887, X = 24 CRACKED FLOOR SUPPORT REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G AT STATION 1887 TO STATION 2007, X = 24. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7087 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FOR PART NUMBER EFFECTIVITY E.A.#: 1-5321- T0379171, TITLE: FUSELAGE - CARGO COMP FLOORS - IPC 53-00-40-01 AND IPC 53-21-43-03,
CABIN - STATION 1887, X - 2 FLOOR SUPPORT APPROXIMATELY OF 1.25 INCH FOUND CRACK. CABIN AT STATION 1887, X = - 2 CRACKED FLOOR SUPPORT REMOVED AND REPLACED AT STATION 1887 TO STATION 2007, X = - 2 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7080 REVISION S. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FOR PART NUMBER EFFECTIVITY E.A.#: 1-5321- T0379171, TITLE: FUSELAGE - CARGO COMP FLOORS - IPC 53-00-40-01 AND IPC 53-21-43-03,
LOWER CENTER CARGO COMPARTMENT STATION 1841 X 15 WEB LOWER SUPPORT FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT STATION 1841 X 15 WEB LOWER SUPPORT CORROSION REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER MD11 SRM 53-00-00- 2R FIGURE 205 REPAIR GENERAL. SUPPORT REMOVED AND REPLACED AS PER MD11 SRM 51-31- 01-0G AT STATION 1841 FROM X=-60 TO X= 60. SUPPORT REWORKED AS PER DOUGLAS DRAWING AGA 7170 REV T. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - INBOARD FLAP OUTBOARD LOWER SEGMENT UPPER SURFACE SKIN AT XIFH 249.5 FOUND CRACK ABOUT 1 INCH. LEFT WING - INBOARD FLAP OUTBOARD LOWER SEGMENT UPPER SURFACE SKIN CRACK AT XIFH 249.5 REPAIR CARRIED OUT AS PER EA 1-5750-T0379218 P1 TITLE - WINGS - FLIGHT SURFACES - ACCOMPLISHED SRM REPAIR ON LHW INBD FLAP ASSEMBLY - FOR CRACK UPPER SKIN - RSC TRACKING.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LANDING GEAR: WHILE ACCOMPLISHING LEFT HAND NOSE LANDING GEAR TRUNNION FITTING REPAIR, 01 EACH HOLE FOUND CRACKED AT STATION 594 AFT BULKHEAD WEB DOUBLER. LANDING GEAR - LEFT HAND NOSE LANDING GEAR TRUNNION FITTING REPAIR AFT CRACKED BULKHEAD WEB DOUBLER AT STATION 594 CARRIED OUT REPAIR IN ACCORDANCE WITH EA # 1- 5310-T0378563P1 TITLE: FUSELAGE - MAIN FRAME - CRACK REPAIR ON LH NOSE LANDING GEAR TRUNNION FITTING, STA 595. AND SRM 51-73-00-0G. GENERAL.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR IS CLASSIFIED AS CATEGORY A.
LANDING GEAR : WHILE ACCOMPLISHING LEFT HAND NOSE LANDIING GEAR TRUNNION FITTING REPAIR FOUND 01 CRACK AT STATION 595 EXTEND FROM LONGERON HOLE. LANDING GEAR: LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AREA CRACKED AT STATION 595 LONGERON REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-31-01-0G & SRM 51-33- 01-0G. LONGERON FABRICATED IN ACCORDANCE WITH DOUGLAS DRAWIING # ACA 3796 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - STATION 635, X = 27.5 SEAT TRACK ASSEMBLY APPROXIMATELY OF 1.0 INCH FOUND CRACK. CABIN AT STATION 635, X = 27.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 625 TO STATION 645, X = 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
DURING ACCOMPLISHING WORK CARD 57.20.01.2 FOUND CRACK ON CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW -45. CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW -45 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
DURING ACCOMPLISHING WORK CARD 57.20.01.2, FOUND CRACK ON CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW 17. CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW 17 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
DURING ACCOMPLISHING WORK CARD 57.20.01.2, FOUND CRACK ON CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW -17. CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW -17 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - NUMBER 6 SLAT LOWER SURFACE INNER RIB AT STATION XOS 816.823 FOUND CRACK ABOUT 0.4 INCHES. LEFT WING NUMBER 6 SLAT LOWER SURFACE INNER CRACKED RIB AT STATION XOS 816.823 REPAIR CARRIED OUT AS PER EA 1-5750-T0379098 PART 1. TITLE: WINGS-FLIGHT SURFACES - LH WING - #6 SLAT ASSY - CRACK RIBS - LOCAL FABRICATION - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - STATION 1663 X = 8.5 SEAT TRACK ASSEMBLY APPROXIMATELY 1.0 INCH FOUND WITH CRACK. CABIN - CRACKED SEAT TRACK AT STATION 1663, X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1631 TO STATION 1691, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - STATION 755, X = 27.5 SEAT TRACK ASSEMBLY OF APPROXIMATELY 1.0 INCH FOUND CRACK. CABIN - CRACKED SEAT TRACK AT STATION 755, X = 27.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 745 TO STATION 765, X = 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - STATION 755, X = - 8.5 SEAT TRACK ASSEMBLY APPROXIMATELY OF 1.0 INCH FOUND CRACK. CABIN - AT STATION 755, X = - 8.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 745 TO STATION 765, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN - STATION 635 , X - 47.5 SEAT TRACK ASSEMBLY APPROXIMATELY OF 0.75 INCH FOUND CRACK. CABIN AT STATION 635, X = - 47.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X = - 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
DURING ACCOMPLISHING WORK CARD 57.20.01.2, FOUND CRACK ON CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW 46. CENTER UPPER AUXILLARY TANK STRINGER 47 AT STATION XCW 46 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 792 FOUND CRACK ABOUT 0.4 INCHES. RIGHT WING FIXED LEADIING EDGE CRACKED BEADED DOUBLER AT STATION XOS 792 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING - FIXED LEADING EDGE UPPER FORMER AT STATION XOS 584 FOUND CRACK ABOUT 1 INCH. RIGHT WING FIXED LEADING EDGE CRACKED UPPER FORMER AT STATION XOS 584 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK ABOUT 1 INCH. RIGHT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 789 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G . RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING, LEADING EDGE NO 14 SLAT TRACK CUTOUT OUTBOARD LOWER CORNER AT STATION XOS 891 FOUND CRACK. RIGHT WING LEADING EDGE NUMBER 14 SLAT TRACK CUT OUT OUTBOARD LOWER CORNER AT STATION XOS 891 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 863 FOUND CRACK ABOUT 0.5 INCHES. RIGHT WING FIXED LEADIING EDGE CRACKED BEADED DOUBLER AT STATION XOS 863 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOOR PER GMM 6-2-100.
LEFT WING - FIXED LEADING EDGE FORMER AT STATION XOS 584 FOUND CRACK ABOUT 2 INCHES. LEFT WING FIXED LEADIING EDGE CRACKED FORMER AT STATION XOS 584 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 785 FOUND CRACK ABOUT 0.2 INCHES. LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 785 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 587 FOUND CRACK ABOUT 0.5 INCHES. LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 587 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK ABOUT 0.2 INCHES. LEFT WING FIXED LEADIING EDGE CRACKED BEADED DOUBLER AT STATION XOS 655 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 640 FOUND CRACK ABOUT 0.3 INCHES. LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 640 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 631 FOUND CRACK ABOUT 0.3 INCHES. LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 631 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 FOUND CORROSION. RIGHT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1. DOUBLER REPAIR CARRIED OUT AS PER DOUGLAS DRAWING # SG11570014 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 FOUND CORROSION. LEFT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1. DOUBLER REPAIR CARRIED OUT AS PER DOUGLAS DRAWING # SG11570014 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING - FIXED LEADING EDGE FORMER AT STATION XOS 584 FOUND CRACK ABOUT 2 INCHES. LEFT WING FIXED LEADIING EDGE CRACKED FORMER AT STATION XOS 584 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ( NOTE: SAME CONTROL NUMBER, DIFFERENT REPORT, SENT AS A SUPPLEMENTAL)
HIGH FREQUENCY EDDY CURRENT INSPECTION ON NOSE LANDING GEAR LEFT HAND SIDE TRUNNION FITTING STATION 595 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATELY 0.35". NOSE LANDING GEAR LEFT HAND SIDE TRUNNION FITTING STATION 595 CRACKED AREA CARRIED OUT REPAIR IN ACCORDANCE WITH EA # 1-5310-T0378563 P1 TITLE : FUSELAGE - MAINFRAME -CRACK REPAIR ON LH NOSE LANDING GEAR TRUNNION FITTING, STA 595. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LANDING GEAR : NOSE LANDING GEAR RIGHT HAND SIDE TRUNNION FITTING STATION 595 AREA FOUND CRACKED. LANDING GEAR: NOSE LANDING GEAR RIGHT HAND SIDE TRUNNION FITTING CRACK AT STATION 595 CARRIED OUT REPAIR IN ACCORDANCE WITH EA # 1-5310-T0379130P1 TITLE: FUSELAGE - MAIN FRAME - CRACK REPAIR ON RH NOSE LANDING GEAR TRUNNION FITTING, STA 595. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
L1 CABIN DOOR WOULD NOT OPEN PNEUMATICALLY WHEN TRYING TO LEAVE AIRCRAFT WITH NO POWER TO THE DOOR. INSPECTED L1 DOOR,OPERATES NORMALLY AND ARMS WITHOUT ISSUE,L1 DOOR BOTTLE IS SERVICED AND PRESSURE TEST OF SLIDE PASSES,FURTHER TS REQUIRED
ON WALK AROUND FOUND R1 DOOR SLIDE PRESSURE LIGHT INOP. REMOVED AND REPLACED R1 DOOR SLIDE PRESSURE INDICATOR LIGHT BATTERIES IAW M/M 25-61-04-4. R1 DOOR SLIDE PRESSURE INDICATOR LIGHT OPS CHECK NORMAL IAW M/M 25-61-04-5
APPROXIMATELY 2:00 HOURS OUT OF KONT, PAST OUR ETP, RECEIVED LVL 1 CRG FLOW FWD DISAG AND SINGLE AMBER TRIANGLE IN THE LOWER FWD AIR SYNOPTIC PAGE. WHILE REVIEWING THE QRH, 2-5 MIN AFTER INITIAL ALERT, CREW RECEIVED RED CARGO FIRE LOWER. COMPLIED WITH QRH AND FIRE WARNING EXTINGUISHED WITHIN 60 SECONDS. DECLARED AN EMERGENCY AND DIVERTED TO LAND AT THE NEAREST AIRPORT. DISCHARGED 2ND BOTTLE. INSTALLED 5 SERVICEABLE CARGO SMOKE DETECTORS IN FWD CARGO COMPARTMENT REF AMM 26-14-01-4, ALL OPS CHECK GOOD. AS A PRECAUTION, ALSO REMOVED & REPLACED MSC REF AMM 31-42-01-4, OPS CHECK GOOD. INSTALLED SERVICEABLE SYSTEM 1 CARGO FIRE BOTTLE IAW AMM 26-22-01-4, OPS CHECK GOOD.
NOSE GEAR STEERING COLLAR HAS BROKEN LUG. PART MISSING IS 2 3/4 " LONG. FOUND DURING B140 CHECK. WRITTEN ON NONROUTINE 12. REMOVED AND REPLACED NLG STEERING COLLAR IAW AMM 32-21-01-8 AND CMM 32-21-11. REF EA 1-3220-T0374219 REV.A 0000302834. REF WO 00085702 N00012.
PDIS 615 33-50 2050 07JAN23 ANC OPEN U EMER LT BAT 1 LO ALERT DURING EMER LT TEST MEL 07JAN23 00:26 ANC U RELEASED FOR SERVICE PER MEL : 33-50-04 CATEGORY : C EXPIRATION : 17JAN23 "MEL 33-50-04: EMER LIGHTS - INOP." C/7346727 SHGN 07JAN23 00:35 ANC U EA: 4 UPADATED WRI TO INCLUDE A "SDR". UPDT 07JAN23 00:37 ANC U CMM: 6 UPDATED WRI TO INCLUDE A "SDR". FACT 16JAN23 13:03 ORD AMM: 33-51-01-4 REMOVED AND REPLACED POWER SUPPLY, EMERGENCY LIGHTING BATTERY (MFR. GRIMES,P/N 60-411-5,S/N 0068) IAW AMM 33-51-01-4. OPS CHECKS NML. THIS CLEARS MEL, AND PLACARD REMOVED.
LEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1-5750-T0325650 C PART 2 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1-5750-T0325648 C PART 2 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING - LEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1-5750-T0325648 C PART 2 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57501022 FOR DETAILS).
LEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1-5750-T0325650 C PART 2 STEP 1F(1) AND STEP 1F(2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CRACK FOUND APPROXIMATE 0.75" IN LENGTH AS MARKED DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE OVERWING FLOORBEAM WEB AT UPPER FLANGES STATION 1256 , X=-107. CRACK FOUND APPROXIMATELY 0.75" IN LENGTH REPAIRED AS PER EA # 1-5310- T0368267 P1 TITLE : FUSELAGE - MAINFRAME - MAIN DECK CARGO OVERWING FLOOR BEAM AT STA 1256.750 CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING - RIGHT HAND AFTER (FLAP) INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-162344 F PART 3 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND AFTER (FLAP) INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-162344 F PART 3 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING - LEFT HAND AFT (FLAP) INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND COROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-162343 H PART 3 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING - LEFT HAND AFT (FLAP) INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE FOUND COROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-162343 H PART 3 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING - RIGHT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57- 44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1-5750-T0325650 C PART 2 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING - LEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57- 44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1-5750-T0325648 C PART 2 STEP 1F(1) AND STEP 1F(2).
LEFT HAND WING LEADING EDGE CAVITY STRINGER AT STATION XOS = 667. FOUND CRACK LEFT HAND WING LEADING EDGE CAVITY STRINGER AT STATION XOS = 667 REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 667 FOUND CRACK LEFT HAND WING LEADING EDGE CAVITY CRACKED DOUBLER AT STATION XOS = 667 REMOVED AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AS PER SRM 51-33-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.
UPON FLAPS 35 SELECTION, RECEIVED LEVEL 2 SLAT DISAG. ALERT. INITIATED GO AROUND, AND THEN RECEIVED LEVEL 2 FLAP DISAG. ALERT. AIRSPEED WAS 146 IAS. ACFT DID NOT HAVE ANY ROLL MOMENT WHEN GETTING THE ALERTS. UPON RETRACTION OF FLAPS AND SLATS ALERTS WENT AWAY. ACCOMPLISHED CHECKLIST. SECOND APPROACH AT FLAPS 22/EXT. NO ALERT PRESENT AT THIS SETTING. EMERGENCY DECLARED. EMERGENCY DECLARED. SLC RANS FLAPS THROUGH ALL PHASES AND COULD NOT DUPLICATE DISCREPANCY. NO FAULTS LAST FLIGHT LEG PERTAINING TO SLATS OR FLAPS. RAN SLAT AND FLAPS RTS VIA FCC-1 AND FCC-2. NO FAULTS. CHECKED SLAT SENSOR READOUTS VIA PSEU AND ALL WERE WITHIN RANGE IAW SLAT POSITION SENSORS ADJ/TEST REF M/M 27-84-02-5.
EMPENNAGE - AFT FUSELAGE AT STATION 2164 BULKHEAD LOWEST STIFFENER LEFT HAND CORNER FOUND CRACK 0.5 INCH. AFT FUSELAGE AT STATION 2164 BULKHEAD LOWEST AREA CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-33-01-0G. STIFFENER REWORKED AS PER DOUGLAS DRAWING AJC7001 REVISION DT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
MAIN DECK CARGO COMPARTMENT FLOOR LEFT HAND SEAT TRACK ALONG X = 27.50 AT STATIOMAIN DECK CARGO COMPARTMENT FLOOR LEFT HAND SEAT TRACK ALONG X = 27.50 AT STATION 1841 FOUND WITH CORROSION MAIN DECK CARGO COMPARTMENT FLOOR LEFT HAND SEAT TRACK ALONG X = 27.50 AT STATION 1841 CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1811 TO STATION 1887 X = 27.50 END POINT AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.N 1841 FOUND WITH CORROSION
HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATE 0.15" IN LENGTH AT LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 13 SLAT TRACK #10 CUTOUT AFT INBOARD CORNER AT APPROXIMATE XOS 659.717. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AFTER LANDING CABIN DOOR 1L MISTAKENLY OPENED WITH EMERGENCY HANDLE. RAFT FELL OUT BUT DID NOT INFLATE. REMOVED 1L DOOR SLIDE RAFT AND INSTALLED 10 MAN LIFE RAFT P/N 5A3210-40621 AS PER MEL 52-10-03-03. PLEASE INSTALL CREW STAIR AT 1R DUE 1L DOOR AND RAFT INOP.
PDIS 615 05-50 1092 10FEB22 MEM FACT U REJECT AT 65 KNOTS DUE TO MASTER CAUTION. ALERT APPEARED WITH MASTER CAUTION BUT CLEARED WHEN THROTTLES REDUCED BEFORE WE HAD TIME TO READ. OAT 18 C. GROSS WEIGHT 408.0 UPDT 11FEB22 03:00 MEM U SINCE TAKE OFF REJECTED AT 65 KNOTS, NO HIGH ENERGY STOP INSPECTION REQUIRED. REF FOM 4.54. REOP 11FEB22 05:06 U DSCRP IS REOPEN FOR WORK. AMT MECHANIC: 5136900 FACT 11FEB22 05:14 MEM U REPLACED ESC. OPS CHECK GOOD. NO FAULTS NOTED. AVIONICS FLOW LIGHT ILLUMITED DURING TO, FLOW LIGHT IS EXTINGUISHED . REF MD-11 AMM 21-08-01-4 & 21-08-21-5. AC OK FOR SERVICE REFERNCE WRI 36-10 0928 FOR PARTS INSALLATION
HFEC INSPECTION FOUND CRACK ON OUTER EXISTING REPAIR DOUBLER AT CENTER CARGO DOOR AFT JAMB AREA STATION 1781 LONGERON 40 RIGHT HAND TO LONGERON 41 RIGHT HAND. CENTER CARGO DOOR AFT JAMB AREA STATION 1781 LONGERON 40 RIGHT HAND TO 41 RIGHT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH EA # 1-5330-T0308422A PT4 TITLE: " FUSELAGE - PLATES & SKINS - MD11 SRM 53-00-15 REPAIR 8 ON CENTER CARGO DOOR CUTOUT AFT JAMB AT STA 1781, BETWEEN L-40R TO L-41R". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 . REFER SNRM # N00112 FOR REPAIR DETAILS.
HFEC INSPECTION FOUND CRACK ON OUTER EXISTING REPAIR DOUBLER AT CENTER CARGO DOOR AFT JAMB AREA STATION 1781 LONGERON 40 RIGHT HAND TO LONGERON 41 RIGHT HAND. CENTER CARGO DOOR AFT JAMB AREA STATION 1781 LONGERON 40 RIGHT HAND TO 41 RIGHT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH EA # 1-5330-T0308422A PT4 TITLE: " FUSELAGE - PLATES & SKINS - MD11 SRM 53-00-15 REPAIR 8 ON CENTER CARGO DOOR CUTOUT AFT JAMB AT STA 1781, BETWEEN L-40R TO L-41R". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 . REFER SNRM # N00112 FOR REPAIR DETAILS.
HFEC INSPECTION FOUND CRACK ON OUTER EXISTING REPAIR DOUBLER AT CENTER CARGO DOOR AFT JAMB AREA STATION 1781 LONGERON 40 RIGHT HAND TO LONGERON 41 RIGHT HAND. CENTER CARGO DOOR AFT JAMB AREA STATION 1781 LONGERON 40 RIGHT HAND TO 41 RIGHT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH EA # 1-5330-T0308422A PT4 TITLE: " FUSELAGE - PLATES & SKINS - MD11 SRM 53-00-15 REPAIR 8 ON CENTER CARGO DOOR CUTOUT AFT JAMB AT STA 1781, BETWEEN L-40R TO L-41R". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 . REFER SNRM # N00112 FOR REPAIR DETAILS.
CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231LF FOUND TOP SURFACE DAMAGED AT STATION 675 TO STATION 735 . DAMAGED FLOOR PANEL #231LF AT CABIN STATION 675 TO STATION 735 (LEFT HAND) REMOVED AS PER AMM 53-21-04 . FABRICATED FLOOR PANEL #231LF AS PER FEDEX DRAWING SRZ - 25 - 005 REVISION R . FABRICATED FLOOR PANEL #231LF INSTALLED AS PER AMM 53-21-04 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231HF FOUND TOP SURFACE DAMAGED AT STA 595 TO 675 . DAMAGED FLOOR PANEL #231HF AT CABIN LEFT HAND STATION 595 TO STATION 675 REMOVED AS PER AMM 53-21-04 . FABRICATED FLOOR PANEL #231HF AS PER FEDEX DRAWING SRZ-25-005 REVISION R . FABRICATED FLOOR PANEL #231HF INSTALLED AS PER AMM 53-21-04 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AS PER EARN NR - 0015 REQUEST ON ALL FASTENER HOLES AT LEFT HAND BANJO FITTING FORWARD AND AFT REPAIR AREA STATION Y = 2164 AND FOUND NUMBER 4 HOLE FROM BOTTOM UP AT AFT ROW WITH DAMAGE INDICATION. LEFT HAND BANJO FITTING AFT EXISITING REPAIR AREA STATION Y = 2164 NUMBER 4 HOLE FROM BOTTOM UP AT AFT ROW AREA 01 EACH DAMAGE FASTENER HOLE REPAIR CARRIED OUT AS PER ENGINEERING AUTHORIZATION 1-5530-T0354042 PART 1 TITLE : STABILIZERS - VERTICAL STABILIZER - CRACK REPAIR ON VERTICAL STABILIZER REAR SPAR LT FWD AND AFT FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SPECIAL NONROUTINE MAINTENANCE FORM N01287 FOR WORK DETAILS.
FUSELAGE : FORWARD AVIONICS COMPARTMENT MAIN DECK FLOOR SUPPORT APPOXIMATELY STATION 392 TO STATION 401 X = 30 FOUND CRACKED . FUSELAGE : FORWARD AVIONIC COMPARTMENT , CRACKED MAIN DECK FLOOR SUPPORT AT APPROXIMATELY STATION 392 TO STATION 401 X = 30 , REMOVED AND REPLACED FROM STATION 421.578 TO STATION 385 X = 30 AS PER SRM 51-31-01-0G . FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING ABA 8304 REVISION B . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
RIGHT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLES CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND EA 1-5750-T0353924 PART 1 STEP 1A. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT CORROSION REPAIR. FABRICATED OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
ULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER #4 BANJO FITTING LEFT HAND SIDE FORWARD FLANGE REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATELY STATION Y = 2164
AGING AIRCRAFT - EXISTING REPAIR AT AFT CARGO STATION 1841 BEAM WEB RIGHT HAND X = -0 TO -13 EXISTING REPAIR AT AFT CARGO STATION 1841 BEAM WEB RIGHT HAND X=-0 TO X=-13 FOUND WEB DAMAGED. REPAIR CARRIED OUT AT AFT CARGO STATION 1841, X=-0 TO X=-17 AS PER SRM 53-00-00-2R FIGURE 211 REPAIR GENERAL. EO 1-5100-7-5001 B6 PART1 TITLE: STRUCTURE- REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENT 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
ULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER # 4 BANJO FITTING LEFT HAND SIDE FORWARD FLANGE REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATE STATION Y = 2164 EXISTING CRACK FOUND DURING ULTRASONIC INSPECTION ON LOWER VERTICAL STABILIZER # 4 BANJO FITTING LEFT HAND SIDE FORWARD FLANGE PREVIOUSLY REPAIRED AREA AT APPROXIMATE STATION Y = 2164 REPAIRED AS PER ENGINEERING AUTHORIZATION # 1-5530- T0354042 PART1 TITLE : STABILIZERS - VERTICAL STABILIZER - CRACK REPAIR ON VERTICAL STABILIZER REAR SPAR LHS FWD AND AFT FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLE CORROSION.
LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" FOUND MOUNT HOLE CORROSION.
LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND E.A. # 1-5750-T0325479 A PART 2 STEP 2.D. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORTS REWORK. FABRICATED OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM N00486 ATTACHED E.A.# 1-5750-T0325479 A PART 2 FOR WORK DETAILS.
LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND E.A. # 1-5750-T0325479 A PART 2 STEP 2.B. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORTS REWORK. FABRICATED OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM N00486 ATTACHED E.A.# 1-5750-T0325479 A PART 2 FOR WORK DETAILS.
LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "B" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "B" REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND EA 1-5750-T0325479 A PART 2 STEP 2A. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LT WING- OUTBD FLAP VANE ASSY- TRACK SUPPORTS REWORK. FABRICATED OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE FORMER AT STATION XOS 1025 FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DRAWING ARB 2920 REVISION BB. INSTALLED FABRICATED FORMER AT LEFT HAND WING FIXED LEADING EDGE AT STATION XOS 1025 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "C" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "C" REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND EA 1-5750-T0325479 A PART 2 STEP 2C. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LT WING- OUTBD FLAP VANE ASSY- TRACK SUPPORTS REWORK. FABRICATED OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM N00486 ATTACHED EA 1-5750-T0325479 A PART 2 FOR WORK DETAILS.
RIGHT HAND WING FIXED LEADING EDGE FORMER AT STATION XOS 1025 FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DRAWING ARB 2920 REVISION BB. INSTALLED FABRICATED FORMER AT RIGHT HAND WING FIXED LEADING EDGE AT STATION XOS 1025 AS PER SRM 51-33-01-0G. REPAIR C CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT STATION XOS 667 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER AS PER DRAWING ARB 3954 REVISION K. INSTALLED FABRICATED DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE AT STATION XOS 667 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1641 LONGERON 11 RIGHT HAND SIDE . EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1641 LONGERON 11 RIGHT HAND SIDE EVALUATED AND FOUND REPAIR DOUBLER DAMAGED / DENTED. MAIN DECK CARGO FRAME STATION 1641 LONGERON 11 RIGHT HAND SIDE CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-00-07-2R FIGURE 201 REPAIR 2. EO # 1-5100-7-5001 B6 PART 1 TITLE: " STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B' REPAIR. INITIAL INSPECTION REQUIRED AT 14500 FLIGHT CYCLE, REPETITIVE INSPECTION AT EVERY 9500 FLIGHT CYCLE AS PER SRM 53-00-07-2R TABLE 201/REPAIR 2.
RIGHT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 760 FOUND CRACK
RIGHT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 854 FOUND CRACK
LEFT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 621 FOUND CRACK
LEFT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 611 FOUND CRACK
AFT CARGO COMPARTMENT STATION 1841 BEAM WEB LEFT HAND X = 0 TO X = 9 FOUND DENT
AGING AIRCRAFT, EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1681 LONGERON 12 RIGHT HAND SIDE. EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1681 LONGERON 12R RIGHT HAND SIDE EVALUATED AND FOUND REPAIR DOUBLER DAMAGED / DENTED. MAIN DECK CARGO FRAME STATION 1681 LONGERON 12R RIGHT HAND SIDE CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-00-07-2R FIGURE 201 REPAIR 2. EO 1-5100-7-5001 B6 PART 1 TITLE: "STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B' REPAIR. INITIAL INSPECTION REQUIRED AT 14,500 FLIGHT CYCLE, REPETITIVE INSPECTION AT EVERY 9,500 FLIGHT CYCLE AS PER SRM 53-00-07-2R TABLE 201 / REPAIR 2.
AGING AIRCRAFT, EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STATION 765 , X = 8.5 LEFT HAND SIDE. CABIN SEAT TRACK EXISTING REPAIR EVALUATED AND FOUND REPAIR SLICE BETWEEN STATION 745 - STATION 765 X = 8.5 LEFT HAND SIDE 02 EACH FOUND CRACK. CABIN MAIN DECK DECK CARRIED OUT SEAT TRACK REPAIR BETWEEN STATION 745 AND STATION 765 X = 8.5 LEFT HAND SIDE IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B6 PART 1 TITLE : "STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO - R3 DOOR FORWARD JAMB LOWER WEB BOX STATION 1250.75 TO STATION 1256.75 LONGERON 26 RIGHT HAND TO LONGERON 27 RIGHT HAND . EXISTING REPAIR AT MAIN DECK CARGO - R3 DOOR FORWARD JAMB LOWER WEB STATION 1250.75 TO STATION 1256.75 LONGERON 26 RIGHT HAND TO LONGERON 27 RIGHT HAND EVALUATED AND FOUND NEW CRACK AT WEB. MAIN DECK CARGO - R3 DOOR FORWARD JAMB LOWER WEB BOX STATION 1250.75 TO STATION 1256.75 LONGERON 26 RIGHT HAND TO LONGERON 27 RIGHT HAND CARRIED OUT REPAIRED IN ACCORDANCE WITH EA # 1-5310 - T0353972 PART 1 TITLE: FUSELAGE - MAINFRAME - R3 DOOR CUTOUT INSIDE FWD JAMB - CRACKS ON INNER SKIN. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO - L3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 TO STATION 1315.42 LONGERON 26 LEFT HAND TO LONGERON 27 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO - L3 DOOR AFT JAMB WEB STATION 1305.25 TO STATION 1315.42 LONGERON 26 LEFT HAND TO LONGERON 27 LEFT HAND EVALUATED AND FOUND NEW CRACK AT WEB. MAIN DECK CARGO - L3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 TO STATION 1315.42 LONGERON 26 LEFT HAND TO LONGERON 27 LEFT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-40-15-2R FIGURE 201 REPAIR 3. EO # 1-5100-7-5001 B6 PART 1 TITLE: " STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD INNER FINGER DOUBLER DETACHED AT XW 377 - XW 385 REPAIR CARRIED OUT AT LEFT HAND WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD INNER FINGER DOUBLER AT XW 377 - XW 385 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD INNER FINGER DOUBLER DETACHED AT XW 377 - XW 385 REPAIR CARRIED OUT AT RIGHT HAND WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD INNER FINGER DOUBLER AT XW 377 - XW 385 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - CABIN SEAT TRACK EXISTING REPAIR AT RIGHT HAND STATION 745 - STATION 765 , X = - 27.5. EXISTING SEAT TRACK REPAIR BETWEEN STATION 745 - STATION 765 X = -27.5 RIGHT HAND EVALUATED AND FOUND EXISTING REPAIR SPLICE 02 EACH CRACK. CABIN MAIN DECK SEAT TRACK REPAIR CARRIED OUT BETWEEN STATION 745 AND STATION 765, X = -27.5 RIGHT HAND AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO # 1-5100-7-5001 B6 PART 1 TITLE : "STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO - L3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 TO STATION 1315.42 LONGERON 26 LEFT HAND TO LONGERON 27 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO - L3 DOOR FORWARD JAMB WEB STATION 1305.25 TO STATION 1315.42 LONGERON 26 LEFT HAND TO LONGERON 27 LEFT HAND EVALUATED AND FOUND NEW CRACK AT WEB. MAIN DECK CARGO - L3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 TO STATION 1315.42 LONGERON 26 LEFT HAND TO LONGERON 27 LEFT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-40-15-2R FIGURE 201 REPAIR 3. EO # 1-5100-7-5001 B6 PART 1 TITLE: " STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RIGHT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 854 FOUND CRACK REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT STATION XOS 854 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
RIGHT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 860 FOUND CRACK REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT STATION XOS 860 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
RIGHT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 760 FOUND CRACK REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT STATION XOS 760 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
AGING AIRCRAFT - CABIN SEAT TRACK EXISTING REPAIR AT LEFT HAND STATION 869 , X = 47.5. EXISTING SEAT TRACK REPAIR BETWEEN STATION 869 TO STATION 929, X= 47.5 LEFT HAND SIDE EVALUATED AND FOUND EXISTING REPAIR SPLICE (02 EACH) CRACK. CABIN SEAT TRACK AT STATION 869 AND STATION 929, X= 47.5 LEFT HAND SIDE REPAIR CARRIED OUT AS PER SRM 53- 00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - CABIN SEAT TRACK EXISTING REPAIR AT LEFT HAND STATION 869 , X = 27.5. EXISTING SEAT TRACK REPAIR BETWEEN STATION 869 - STATION 929, X= 27.5 LEFT HAND SIDE EVALUATED AND FOUND EXISTING REPAIR SPLICE (02 EA) CRACK. CABIN SEAT TRACK AT STATION 869 AND STATION 929, X= 27.5 LEFT HAND SIDE REPAIR CARRIED OUT AS PER SRM 53- 00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AFT CARGO COMPARTMENT STATION 1841 BEAM WEB LEFT HAND X = 0 TO X = 9 FOUND DENT AFT CARGO COMPARTMENT STATION 1841 BEAM WEB LEFT HAND X = 0 TO X = 9 REPAIR CARRIED OUT AS PER MD-11 , SRM 53-00-00-2R FIGURE 211 REPAIR GENERAL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 611 FOUND CRACK REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE DOUBLER AT STATION XOS 611 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.
LEFT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 621 FOUND CRACK REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE DOUBLER AT XOS 621 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
AGING AIRCRAFT - CABIN SEAT TRACK EXISTING REPAIR AT RIGHT HAND STATION 745 - STATION 765 , X = -8.5. EXISTING SEAT TRACK REPAIR BETWEEN STATION 745 - STATION 765, X = -8.5 RIGHT HAND SIDE EVALUATED AND FOUND EXISTING REPAIR SPLICE 02 EACH FOUND CRACK. MAIN DECK SEAT TRACK REPAIR CARRIED OUT BETWEEN STATION 745 AND STATION 765, X = -8.5 RIGHT HAND AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO # 1-5100-7-5001 B6 PART 1 TITLE : "STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.
RIGHT HAND WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 860 FOUND CRACK
RIGHT HAND WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD INNER FINGER DOUBLER DETACHED AT XW 377 - XW 385
LEFT HAND WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD INNER FINGER DOUBLER DETACHED AT XW 377 - XW 385
CABIN - SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 750 , X = 75.25 . CABIN - SEAT TRACK AT LEFT HAND STATION 750 , X = 75.25 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 725 TO EXISTING SPLICE STATION 765 X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
CABIN SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 5-11 , X = 27.5. SEAT TRACK CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1531/5-0 TO STATION 5-63 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CABIN SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 1421, X = 47.5 . SEAT TRACK CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1391 TO STATION 1451 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100
CABIN SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 5-2, X = 8.5. SEAT TRACK CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-83 TO EXISTING SPLICE STATION 5-0/1531 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100
PDIS 615 32-42 8675 03FEB20 CDG FACT U LOGPAGES:3206022 DECELLERATION THROUGH 80 KTS TIRE PRESS DIFF LEVEL 1 ALERT UPON EXITING RUNWAY LEVEL 2 TIRE FAIL ALERT. #8 PRESSURE WENT TO ZERO. INSPECTED BY MAINT. R/I 04FEB20 01:28 CDG U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: ARG7755-503 POS: 8 SRL: B0422 TAG NBR: 3183F2 ON MPN: ARG7755-503 CPN: 3200402 SRL: B4017 TAG NBR: G88881 REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: ARG7755-503 POS: 7 SRL: B3531 TAG NBR: 6759F1 ON MPN: ARG7755-503 CPN: 3200402 SRL: B4916 TAG NBR: 1388E1 FACT 04FEB20 01:28 CDG U IAW AMM 32-40-00-6 WHEEL #8 INSPECTED AND FOUND PRESSURE AT 0 PSI. NEED TO REPLACE WHEEL #8 AND OPPOSITE WHEEL #7. REMOVAL INSTALLSATION OF WHEEL #8 AND #7 PERFORMED IAW AMM 32-41-01-4. ALL WHEEL INSPECTED IAW AMM 32-40-00-6 NO DEFFECT FOUND.
"EMG BAT 1 LO" DURING PREFLIGHT. REPLACED THE EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECKED GOOD.
FIRE AT EXTERNAL POWER CONNECTION BURNED AND MELTED AIRCRAFT EXTERNAL POWER RECEPTACLE AND COMPONENTS. INSTALLED EXTERNAL POWER RECEPTACLE REFERENCE AMM 24-41-03-4. COMPLETED INSTALLATION OF EXTERNAL POWER PANEL REFERENCE DRAWING AAN7220 AND AMM 20-50-02-2. APPLIED EXTERNAL POWER REFERENCE MD-11 AMM 24-40-00-2 WITH NO DEFECTS NOTED. STARTED APU REFERENCE JRH AND ACCOMPLISHED MULTIPLE POWER TRANSFERS WITH NO DEFECTS NOTED. INSTALLED FLOOR PANEL 123HF REFERENCE AMM 53-21-04-4. STILL REQUIRES INSTALLATION OF NYLON CORD AND SEALANT. INSTALLEDD NYLON CORD AND SEALED TO FLOOR BOARD. REF AMM 53-21- 04-4.
POST FLIGHT CHECK FOUND EMERGENCY POWER TEST FAIL. DURING T-S FOUND FAULTED BATTERY CHARGER. REPLACED BATTERY CHARGER PER AMM 24-34-03-4 AND FOR PRECAUTIONARY, REPLACED BOTH MAIN BATTERIES PER AMM 24-34-02-4, ALL CHECK SATISFACTORY. SET ELECTRONIC CHRONOMETER PER AMM 31-21-02-5. A/C OK FOR SERVICE.
AFTER TAKEOFF HYD 2 FAILURE. LOSS OF ALL FLUID. RCM CHECKLIST AND RETURNED FOR LANDING. CHECKED THE HYD LEAK FROM #2 ENG R HYD PUMP. REMOVED AND REPLACED THE 2R EDP PER AMM 29-11-20-4-1. LEAK CHECKED NORMAL .BUT THE L AND R PUMP ALWAY DISPLAY LOW HYD PRESSURE DURING #2 ENGINE RAN. REMOVED AND REPLACED THE RELAY R2-5258.NO HELP.REMOVED AND REPLACED THE L&R LOW PRESSURE SWITCHS AS PER AMM 29-12-34-2-1. ALL INDICATION NORMAL.RAN #2 ENGINE PER MD11 JRH ,TEST NORMAL PER AMM 29-11-20-5. A/C OK FOR SERVICE
HYD 3 ELEV OFF ALERT, HYD 3 QUANTITY 4.9 GAL. HYD 3 QUANTITY CONTINUED TO 3.6 GAL AND TURNED ENG PUMPS OFF TO CONSERVE FLUID. TURN BACK ON PUMPS FOR LANDING AND RECEIVED HYD 3 QTY LO. FINAL QTY 1.6 GAL. REPLACED DAMAGED 'O' RING AND RING REF AMM 27-43-40-4 . LEAK AND OPS CHECK GOOD. A/C OK FOR SERVICE.
LEVEL 2 "TIRE FAIL" FOR RT FWD NOSE TIRE WITH TIRE PRESSURE DROPPING TO "0" THEN THAT ENTIRE GEAR (RT SIDE) WENT AWAY. IT CAME BACK LATER IN FLIGHT BUT WENT AWAY AGIN WITHOUT ANY ALERT. RPL RT NOSE TIRE PRESSURE TRANSDUCER. OPS AND LEAK CHECK GOOD. REF MM32-46-04-4.
LEFT WING FIXED LEADING EDGE LOWER PANEL 519AB, FWD CUTOUT FOUND DOUBLER CRACKED AT XOS 600, INBOARD OF REFUELING PANEL. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G, AND DRAWING ARB2933, REV AJ. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE LOWER PANEL 518DB FWD CUTOUT FOUND DOUBLER CRACKED AT XOS 490. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G, DRAWING ARB2933, REV AJ. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE LOWER PANEL 518GB, OUTBOARD CUTOUT FOUND A STIFFENER CRACKED AT XOS 542 OUTBOARD SIDE OF SLAT DRIVE MECHANISM DOOR. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG ARB2918, REVISION G AND SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 693. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE BEADED DOUBLER WAS FOUND CRACKED AT XOS 705. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
BS 1880 RBL 27.5 SEAT TRACK FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED FROM BS 1811 TO 1887 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 762. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LEADING EDGE BEADED DOUBLER WAS FOUND CRACKED AT XOS 616. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
CARGO TRACK CROWN DAMAGED AT 5-10, X= 27.5 UPPER CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
TWO HOURS 20 MINUTES INTO FLT, THE HYD 3 OFF WITH 2.5 GALLONS ON CONFIGURATION OF GEAR HYD 3 FAILED. TROUBLESHOT IAW FIM 29-10-08, HYD QTY LEVEL 1.8 IN SYS 3, FOUND A LARGE AMOUNT OF HYD FLUID LEAKING FROM TAIL. AFTER FURTHER INVESTIGATION. FOUND THE NR 3 SYS HORIZONTAL STAB PRIMARY CONTROL VALVE FITTING LEAKING , REPLACED THE O-RING AND BACK-UP RING. SERVICED THE NR 3 HYD SYS IAW MM 12-13-02. LEAK AND OPS CHECKED GOOD IAW MM 27-43-00-5.
LEVEL 2 ENG 2 ICE DUCT FAIL WARNING AFTER T/O PASSING 3000', PER QRH SHUT DOWN NR 2 ENG AND RETURNED TO BASE. DISCOVERED THAT THE DUCT GOING AFT IS CRACKED.
R1 DOOR SLIDE PRESS TO TEST INDICATOR IS INOP. REMOVED AND REPLACED EMERGENCY SLIDE PRESS TO TEST LIGHT BULBS AS REQUIRED. OPS CHECKED NORMAL PER MM 25-61-04-5. OK FOR SERVICE.
UPON RAISING THE GEAR AFTER TAKEOFF, THE LEFT MAIN GEAR DID NOT SHOW UP SAFE. THE PRIMARY AND SECONDARY INDICATORS BOTH INDICATED RED UNSAFE. CHANGED THE PROXIMITY SWITCH ELECTRONIC UNIT.
ON TAKEOFF ROLL AT 80 KTS HAD "ALT" MISCOMPARE ALERT AND REJECTED TAKEOFF. COMPLIED WITH QRH. ALERT CLEARED AT 60 KTS. ATTEMPTED SECOND TAKE OFF WITH SAME RESULTS AND A MOMENTARY LEVEL 1 WINDSHEAR DETECT FAIL MESSAGE. COMPLIED WITH QRH AND TAXIED BACK TO RAMP. R&R FCC 2 IAW AMM 22-01-03-4. OPS NORMAL.
FUME EVENT, CAPTAIN AND BOTH JUMPSEATING PILOTS SMELLED STRONG ELECTRICAL BURNING ODOR ON ARRIVAL AT AIRCRAFT. 3RD WRITE-UP OLD DISCREPANCY: 615-24-00-0003950. ACCOMPLISHED GVI OF FLIGHT DECK WINDOWS, FOUND L1 WINDOW UPPER CTR TERMINAL STRIP HAS EVIDENCE OF OVERHEAT.
L-1 DOOR UPPER LINING SLIDING CLOSEOUT PANEL SPRING BROKEN AND PANEL DAMAGED. NO RESTRICTION, IAW 25-23-23-2 L1 DOOR UPPER LINING SLIDING CLOSEOUT PANEL SPRING BROKEN AND PANEL DAMAGED. REMOVED L1 DOOR SLIDING CEILING AND EXIT LIGHT PANEL ASSY IAW MM 25-23-23-2, PARA 2D. TERMINATED WIRES AT LT FORWARD DOOR EXIT SIGN, L2-721, IAW SWPM, AND WDM 33-52-01. TESTS NORMAL IAW AMM 33-52-01-5. TERMINATING ACTION ACCOMPLISHED FOR 25-23-23-2 AT 66,063:27 HR, 15,552 CYCLES, L1 DOOR UPPER LINING SLIDING CLOSEOUT PANEL. INSTALLED NEW SPRING, OPS CHECKED GOOD IAW MM 25-23-23-4.
L1 DOOR FOLLOWER CEILING PANEL EMERGENCY EXIT LIGHT FRAME ASSY BROKEN.
LEFT WING OTBD FLAP INBD FWD HINGE BRACKET, WING SIDE, SIDE ATTACH SURFACE FOUND CORROSION. REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.402", LOWER 0.378", MATERIAL REMOVED: UPPER 0.010", LOWER 0.010" AND REMAINING THICKNESS: UPPER 0.392", LOWER 0.368". NEW REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750- T0325538, PT 1, STEP 1, TITLE: WINGS. FLIGHT SURFACES. EO 1-5750-7-5002, LT WING, OTBD FLAP, INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503739 FOR WORK DETAILS.
RIGHT WING OTBD FLAP INBD FWD HINGE BRACKET, WING SIDE, SIDE ATTACH SURFACE FOUND CORROSION. REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.392", LOWER 0.353", MATERIAL REMOVED: UPPER 0.010", LOWER 0.010" AND REMAINING THICKNESS: UPPER 0.382", LOWER 0.343". NEW REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750, T0325540, PT 1, STEP 1, TITLE: WINGS. FLIGHT SURFACES, EO 1-5750-7-5002. RT WING, OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO WRI 57503737 FOR WORK DETAILS.
RIGHT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.285" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-162344B, PT 4, STEPS 1A & 1C TITLE: WINGS, FLIGHT SURFACES, RT WING, INBD FLAP, OTBD HINGE BRACKET ASSY, CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO NR 57503746 FOR WORK DETAILS.
RIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.313", FINAL HOLE DIA: 1.326" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-162344B, PT 4 STEPS, 1A & 1C TITLE: WINGS. FLIGHT SURFACES, RT WING, INBD FLAP-OTBD HINGE BRACKET ASSY, CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO 57503746 FOR WORK DETAILS.
LEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.2834", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-162343D PT 4 STEPS 1A & 1C TITLE: WINGS, FLIGHT SURFACES, LT WING, INBD FLAP, OTBD HINGE BRACKET ASSY-CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO 57503744 FOR WORK DETAILS.
LEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-162343D, PT 4, STEPS 1A AND 1C. TITLE : WINGS FLIGHT SURFACES, LT WING, INBD FLAP, OTBD HINGE, BRACKET ASSY, CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100. REFER TO NR 57503744 FOR WORK DETAILS.
RIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.408", MATERIAL REMOVED: FWD 0.008", AFT 0.025", REMAINING THICKNESS: 0.375" AND MINIMUM ALLOWABLE THICKNESS: 0.408". NEW REPAIR SHIM FABRICATED AND INSTALLED IAW EA NR 1-5750-T0325483, PT 1, STEP 1, TITLE: WINGS FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO NR 57503738 FOR WORK DETAILS.
RIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.613" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW SHOULDER BUSHING, FABRICATED AND INSTALLED IAW EA 1-5750-T0325483, PT 1 STEP, 1A. TITLE: WINGS FLIGHT SURFACES, EO 1-5750-7-5002. RT WING, OTBD FLAP, OTBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO NR 57503738 FOR WORK DETAILS.
RIGHT WING, OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.612" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW SHOULDER BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0325483 PT 1, STEP 1A, TITLE: WINGS FLIGHT SURFACES, EO 1-5750-7-5002. RIGHT WING OTBD FLAP, OTBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO NR 57503738 FOR WORK DETAILS.
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.248", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750- T0325538, PT 1, STEP 1C, TITLE: WINGS FLIGHT SURFACES, EO NR 1-5750-7-5002, LT WING, OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO NR 57503739 FOR WORK DETAILS.
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-T0325538, PT 1, STEP 1C, TITLE: WINGS, FLIGHT SURFACES. EO 1-5750-7-5002, LT WING - OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO NR 57503739 FOR WORK DETAILS.
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325538, PT 1, STEP 1B, TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002. LT WING, OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO NR 57503739 FOR WORK DETAILS.
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325538, PT 1, STEP 1B, TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, LT WING, OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO NR 57503739 FOR WORK DETAILS.
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, PIVOT BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.316" AND MAXIMUM ALLOWABLE HOLE DIA: 2.3135". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325538, PT 1 STEP 1A TITLE: WINGS, FLIGHT SURFACES EO NR 1-5750-7-5002, LT WING, OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO NR 57503739 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.399", MATERIAL REMOVED 0.009", REMAINING THICKNESS 0.390" & MINIMUM ALLOWABLE THICKNESS 0.408". NEW REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0325482 PT 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503736 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW MM 57-44-09. EXISTING THICKNESS 0.421", MATERIAL REMOVED, FWD FACE 0.009" & AFT FACE 0.009", REMAINING THICKNESS 0.403" & MINIMUM ALLOWABLE THICKNESS 0.408". NEW REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0325482 PT 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503736 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. NR 3 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.581", FINAL HOLE DIAMETER 0.589" & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584". NEW SHOULDER BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325482 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503736 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. HOLE 3 CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.596", FINAL HOLE DIAMETER 0.598" & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584". NEW SHOULDER BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325482 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503736 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.218", FINAL HOLE DIAMETER 1.224" & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325482 PT 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO WRI 57503736 FOR WORK DETAILS.
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.219", FINAL HOLE DIAMETER 1.224" & MAXIMUM ALLOWABLE HOLE DIAMETER 1.220". NEW REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325482 PT 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503736 FOR WORK DETAILS.
RIGHT WING FIXED LE SKIN CUT OUT, AT STATION 659.7174, TRACK 10, CORNER 13, FOUND CRACK APPROX 3/16 INCH IN LENGTH. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
CENTER CARGO COMPARTMENT, STATION 1701 - 1721 RT SIDE, LONGERON 49R, FOUND CORRODED. CARRIED OUT REPAIR IAW EA 1-5310-T0325527 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53103729 FOR WORK DETAILS.
LEFT WING FIXED LE COMPARTMENT AT APPROX STATION XOS 675, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 795, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE COMPARTMENT, STATION XOS 768, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.
RIGHT WING FIXED LE COMPARTMENT, AT APPROX STATION XOS 697, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 665, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 656, BEADED DOUBLER FOUND CRACKED. REPAIR CLASSIFIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
RIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 614, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE COMPARTMENT AT APPROX STATION XOS 545, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
RIGHT WING OTBD FUEL DUMP ISLAND, UPPER SKIN FWD EDGE FOUND TORN AT STATION XOFH 799.865. CARRIED OUT REPAIR IAW EA 1-5730-T0325572 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57303742 FOR WORK DETAILS.
MAIN DECK FLOOR SEAT TRACK AT STATION 1288, X=8.5, FOUND CROWN DAMAGED. REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1263 - 1312, X= 8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 1288, X=-8.5, FOUND CROWN DAMAGED. REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1263 - 1312, X=-8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 1288, X=-47.5, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1248 TO 1312, X = -47.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 5 - 7, X= 47.5, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 5-0 TO 5-23, X=47.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 5 - 7, X=-47.5, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 5-0 TO 5-63, X = -47.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
LEFT WING FIXED LE INTERIOR AT APPROX STATION XOS 862, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 635, X=-8.5, FOUND CRACKED. CRACKED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 1802, X= 8.5, FOUND CORRODED SEAT TRACK. REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1771 - 1831, X =8.5 IAW 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 1802, X=-8.5, FOUND CORROSION. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1771 - 1831, X = -8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK FLOOR SEAT TRACK AT STATION 6-80, X=47.5, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 6-60 - 6-100, X=47.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX AT STATION 1250.75 - 1256.75, LONGERON 26R - 27R, FOUND CRACKED. MAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK L3 DOOR FWD JAMB, LOWER WEB BOX AT STATION 1250.75 - 1256.75, LONGERON 26L - 27L, FOUND CRACKED. MAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED IAW MAJOR IAW GMM 6-2-100.
MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 - 1315.42, LONGERON 26R - 27R, FOUND CRACKED. MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R. FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 - 1315.42, LONGERON 26L - 27L, FOUND CRACKED. MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
DURING CLIMB OUT, FCC 2 B DATA FAULT, LEVEL TWO ALERT DISPLAYED. QRH PROCEDURE APPLIED. CURRENT FAULT ON SENSOR READ OUT SHOWS FCC 2 FAULTED. FCC 2 CURRENT FAULT SHOWS FCC 2 FAULTED. CARRIED OUT INSPECTION AT FCC 2 AVIONICS RACK BACK SHELL SOCKET PINS & WIRES CONDITIONS, NO FAULT FOUND. R & R FCC 2 ASSEMBLY IAW AMM 22-01-03-4. PERFORMED FCC -1 & FCC-2 AFS CAT III B, RTS TEST IAW AMM 22-00-00-5, ALL TEST PASSED. ACFT OK FOR SERVICE.
MOMENTARY STICK SHAKER ACTIVATION AT FL 360, 242KIASDUE TO MODERATE TURBULENCE. AUTOPILOT WAS ENGAGED & AUTO THROTTLES WERE ENGAGED. CLEAN CONFIGURATION. COMPLIED WITH TURBULENCE INSPECTION IAW AMM 05-51-01-6, NO DEFECTS NOTED.
RIGHT OTBD FLAP INBD TE UPPER SURFACE FOUND DELAMINATED AT XOFH 477.69 - 497. REPAIRED IAW SRM 57-50-80 PARAGRAPH 4A 1B. REPAIR 1 REVISION 55 & EA 1-5750-T0308362 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.
MAIN DECK CARGO DOOR FOUR FWD HINGE PIN LOBE HOLES FOUND ELONGATED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 52-34-04 PARAGRAPH 2Y REVISION 78 AND EA1-5230-T0308187 PART1 STEP 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 121.
BS 1315, LONGERON 28R FOUND CRACKED. REMOVED AND REPLACED LONGERON IAW SRM 51-33-01 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.
SKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RT WING LOWER SKIN ACCESS PANEL CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.
MAIN DECK CARGO FLOOR PANEL 293DF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.
MAIN DECK CARGO FLOOR PANEL 233DF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.
MAIN DECK CARGO FLOOR PANEL 273HF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.
LEFT WING, SLAT TRACK NR 12 LOWER CUT OUT SKIN AT XOS 776 FOUND CRACKED. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.
RIGHT OTBD FLAP INBD LOWER TE FOUND DELAMINATED. REPAIRED IAW SRM 57-50-80 PARA 4 1B REPAIR 1 REVISION 55 AND EA 1-5750-T0308362 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.
AFTER TAKEOFF NR 1 ENGINE FAILED & OVER TEMPED. MAX POWER TAKEOFF COMPLETED CHECKLIST. CREW FIRED ONE EACH FIRE BOTTLE. R & R NR 1 ENGINE. OPS & LEAK CHECKED GOOD, OK FOR SERVICE.
FOUND NR 8 LT SLAT SKIN MISSING TOP SIDE MIDDLE TO T/E AREA ABOUT CENTER OF SLAT. INSTALLED LT NR 8 SLAT IAW AMM 27-80-30-4.
SHORTLY AFTER T/O WITH ALL ENG A/I SELECTED ON, GOT "ENG 2 A-ICE OFF" ALERT. CONSULTED QRH AND DIVERTED IAW GOC. FOUND DUCT CRACKED AT FLANGE NEAR FWD END. R & R DUCTING 2, ENGINE 2 ANTI-ICE. OPS CHECK GOOD, NO LEAK NOTED AND MESSAGE CLEARED.
RECEIVED LEVEL 1 "BUSS R EMER AC OFF" ALERT, 2 HOURS INTO FLIGHT. SELECT FADEC ALT,TANK 2 AFT PUMP LO, SINGLE LAND, FO PITOT HEAT, GPWS FAULT, SEL ALT CADC. FAILURE WENT AWAY AND ALL SYS NORMAL AFTER APPROX 20 MIN, DIVERTED AND LANDED WITHOUT INCIDENT. TRIED TO DUPLICATE THE PROBLEM WITH CIRCUIT BREAKER B1-139 PULLED. RECEIVED SAME ALERTS BUT COULD NOT RESET RCCB B1-138 WITH CIRCUIT BREAKER B1-139. COMPLIED WITH MTSI 2422/8464 LINE 11-15 AND FOUND NORMAL. REPLACED R2-5157 IAW SMP. REPLACED RCCB B1-138 AND ALSO REPLACED B1-139 DUE TO BEING STIFF IAW MM 24-50-01-4 AND SMP. EPCU R-T-S TEST PASSED IAW MM 24-08-01-5. ACFT OK FOR SERVICE.
AT 118 INTO FLIGHT AT FL 320 GOT LVL 1 "HYD 3 ELEV OFF" ALERT. FLUID LEVEL IN NR 3 WAS 4.3 GALS AND STARTED DECREASING AT A RATE OF .1 GAL EVERY 3 MINUTES. WHEN 3.5 WAS REACHED;, TURNED HYD SYSTEM TO MANUAL AND TURNED OFF HYD 3 LT AND RT PUMPS AND ALSO THE 1-3 AND 2-3 RMPS. FLUID LEVEL STABILIZED AND CLIMBED BACK TO 3.9 GAL. GEAR WAS LOWER BY ALTERNATE MEANS. NR 3 HYD WAS REPRESSURIZED AND QTY WENT TO 1.2, HYD NR 3 WAS DEPRESSURIZED, UNEVENTFUL LANDING AND TAXI IN, TOWED INTOP THE GATE. R & R BAD UNION, PACKING AND O-RING ON UPPER HORIZONTAL STAB PRIMARY-TRIM CONTROL-VALVE REF AMM 27-43-40-4. LEAK AND OPS CHECK GOOD.
RAN NR 3 ENG FOR IDG DISCONNECT IDG CAME APART DURING RUN. ENGINE NR 3 FIRE INDICATION IN FLIGHTDECK AND 1EA FIRE BOTTLE DISCHARGED, AFTER FURTHER INSPECTION IDG FOUND CRACKED AND INSPECTION ON WIRING AND GEARBOX INWORK. R & R IDG, AIR/OIL HEAT EXCHANGER FLUSHED IDG OIL SYS. THE ALSO R & R THRUST REVERSER HEAT BLANKET.
AT 5000' 200 KNOTS "BUS RT EMERG AC" ILLUMINATED, RT EMERGENCY AC BUSS FAILED. SELECTED "FADEC ALT", F/O CADC ON 1, TRANSPONDER 1, RAN LEVEL 1 ALERT DUE TO NO APPLICABLE CHECKLIST. TROUBLESHOT IAW FIM: 25-25-01-00 AND WDM: 24-61-51 FOUND RELAY (R2-5157)AT FAULT, REPLACED RELAY IAW WDM: 24-61-51.
DURING ACCOMPLISHMENT OF VERTICAL STABILIZER NR 4 BANJO FITTING REPAIR AT RT SIDE FORWARD FLANGE LOWER FITTING EXISTING FASTENER AREA FOUND SHORT WITH 1 EA FASTENER AT REPAIR FITTING IAW REPAIR DWG: SR10550013. REPAIRED AS PER E.A. 1-5530-159861 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LOWER VERTICAL STABILIZER, NR4 BANJO FITTING, RT SIDE FWD FLANGE. CARRIED OUT REPAIR AS PER DRAWING SR10550013 SHEET 7, 8, AND 9 REVISION P.
FRAME AT BS 1641, LONGERON 11, FOUND DENTED. CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.
FRAME AT BS 1661, LONGERON 11R FOUND DENTED. REPAIRED IAW 51-33-01 REVISION 49 AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.
FRAME AT BS 1721, LONGERON 11R FOUND DENTED. REPAIRED IAW SRM 51-33-01 REVISION 49 AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.
FRAME AT BS 1661, LONGERON 11L, FOUND DENTED. REPAIRED IAW SRM SRM 51-33-01 REVISION 49. AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LOWER VERTICAL STABILIZER NR 4, BANJO FITTING, LT SIDE, FORWARD FLANGE. CARRIED OUT REPAIR AS PER SRM 55-30-02 FIGURE 201 REPAIR 3 REVISION 49.
LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.255", REWORKED HOLE DIAMETER 1.2834", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHED AS PER FEDEX E.A. 1-5750-162343 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
FRAME BS 535, 9G NET UPPER SUPPORT YOKE FOUND CHAFED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49.
LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.2215", REWORKED HOLE DIAMETER 1.250", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHED AS PER FEDEX E.A. 1-5750-162343 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
CENTER CARGO COMPARTMENT LONGERON 42L SPLICE FOUND CRACKED AT STATION 5-113 TO 1541. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7115 REVISION D. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
BS 765, X= 8.5 SEAT TRACK FOUND DAMAGED. SEAT TRACK REMOVED AS PER SRM 51-33- 01 REVISION 49. NEW REPAIR SEAT TRACK AND SPLICE REWORKED AS PER SRM 53-00-52 REVISION 49 AND INSTALLED AS PER SRM 51-33-01 REVISION 49. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
FRAME BS 535, 9G NET LOWER SUPPORT YOKE FOUND CHAFED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49.
CENTER CARGO COMPARTMENT LONGITUDINAL SPLICE FOUND CRACKED AT STATION 5-113 TO STA 1551, LONGERON 47RT. LONGERON REMOVED AS PER SRM 51-31-01 REVISION 49 AND REPLACED WITH NEW FABRICATED SPLICE AS PER DRAWING A5A7116 REVISION D AND INSTALLED AS PER SRM 51-33-01 REVISION 49. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
03 EA FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. CARRIED OUT REPAIR AS PER EA 1-5710-162348. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 115.
THREE FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. CARRIED OUT REPAIR AS PER EA 1-5710-162349. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 115.
RT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.228", REWORKED HOLE DIAMETER 1.250", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHED AS PER EA 1-5750-162344 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
RT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.2865", REWORKED HOLE DIAMETER 1.313", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHED AS PER EA 1-5750-162344 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
CENTER CARGO COMPARTMENT LONGERON 40R SPLICE FOUND CRACKED AT STA 5-113 TO 1541. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49. SPLICE FABRICATED AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
RECEIVED LEVEL 1 ALERT REV 3 PRESS FAULT PRIOR TO 80 KTS ON TAKEOFF ROLL. WIRE HARNESS FOUND DAMAGED AND REPLACED.
NR 1 N1 ROLLED BACK TO 25-35 % JUST PRIOR TO DECENT. A NOTICABLE AND AUDIBLE BUMP IN AIRFRAME, LT YAW, & CONFIRM ENGINE OUT ON MCDU'S. SHUTDOWN ENGINE IAW QRH. ELECTED TO LEAVE ENGINE SHUTDOWN DUE TO POSSIBLE DAMAGE. EGT & N2 SLIGHTLY LOWER THAN NR 2, 3. FF 770 PPH PRIOR TO SHUTDOWN . NR 1 THROTTLE UNRESPONSIVE . NR 1 ENG LOW PRESSURE BLEED AIR CHECK VALVE, FOUND STUCK OPEN. R & R PER MM 36-11-01-4-1, PERFORMED FULL BORESCOPE & CHECKED WITHIN LIMITS PER MM 72-00-07-06-1. R & R NR 1 ECU PER MM 73-21-02-4-1, R & R NR 1 ENGINE HMU PER AMM 73-21-01-4 RAN NR 1 & 3 ENGINES PER JRH, PERFORMED NR 1 ENGINE 40% POWER ASSURANCE TEST PER AMM 71-00-00-5-1.
8 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. CARRIED OUT REPAIR AS PER EA 1-5710-132467. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 110.
CRACK INDICATION APPROX 0.5" IN LENGTH FOUND DURING X-RAY INSP AT STA 6-100, LONGERON -4R FWD SECTION EDGE. CRACKED LONGERON-4R AT FORWARD SECTION EDGE STATION 6-100, REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110.
CRACK INDICATION APPROX 4" IN LENGTH DURING X-RAY INSP AT STA 6-100, LONGERON -3R FWD SEC EDGE. CRACKED LONGERON-3R AT FORWARD SECTION EDGE STATION 6-100, REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 44 AND EA 1-5310-140453. REPAIR IS CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REVISION 110.
CRACK INDICATION APPROX 1" IN LENGTH FOUND DURING X-RAY AT STA 6-100, LONGERON -2R FWD SECTION EDGE. REPAIRED AS PER SRM 53- 00-05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110.
CRACK INDICATION APPROX 1" LENGTH FOUND DURING X-RAY INSP AT STA 6-100, LONGERON -2L FWD SECTOR. REPAIRED AS PER SRM 53-00- 05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110.
(10EA) FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. CARRIED OUT REPAIR AS PER EA 1-5710-132468. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 110.
LT WING L/E LOWER ACCESS PANEL 519CB CUTOUT FWD INBD CORNER SUSPECTED CRACK. TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-40-02 FIG. 201 REPAIR 7 REVISION 44. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 110
MAIN DECK CARGO RT STA 5-53 L-12 FRAME FOUND DAMAGED. REPAIRED IAW SRM 53-00-07, FIG 201 REPAIR 4, REV 44. REPETITIVE INSP REQUIRED INITIAL AT 12,000 CYCLES AND REPETITIVE AT 8,000 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 4 REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO RT STA 5-33 L-12 FRAME FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00-07, REPAIR 2 FIG 201, REV 44. INITIAL INSP TO BE CARRIED OUT ON 14,500 FLT CYCLE AND REPETITIVE INSP ON 9,500 FLT CYCLE IAW SRM 53-00-07, REPAIR 2, TABLE 201, REV 44. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO SEAT TRACK, STA 1561 X=-8, CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1531 TO STA 1571 X=-8 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 43. REPAIR CLASSIFIED AS MAJOR AS GMM 6-2-100 REV 110.
CENTER ACCESSORIES COMPT. LT SIDE LONGERON 37L SUSPECT CRACK AT 2 PLACES. FASTENER TO FASTENER APROX 4" IN AFT OF FUSLAGE STA Y=1129/6-100. CRACK LONGERON 37L IN CTR ACCESORY COMPARTMENT IN AFT OF FUSELAGE STA Y=1129/6-100 REMOVED AND REPLACED WITH A FABRICATED LONGERON AS PER SRM 51-33-01 REV 44. LONGERON FABRICATED BY MACHINE AS PER DRAWING AGA7121 REV A. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.
MAIN DECK CARGO AT STA 1887 X=-57, BELOW FLOOR SUPPORT BEAM END FOUND CRACKED AS MARKED. R & R IAW SRM 51-31-01, REV 44. NEW FLOOR SUPPORT FABRICATED BY MACHINING IAW DWG AGA7551, REV G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
MAIN DECK CARGO LT STA 1761 L-12 FRAME FOUND DENT. MAIN DECK CARGO STA 1761 L-12 FRAME FOUND DENT. REPAIR CARRIED OUT AS PER SRM 53-00-07 REPAIR 2 FIG 201 REV 43. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 110. INITIAL INSPECTION TO BE CARRIED OUT ON 14,500 FLT CYCLE AND REPETITIVE INSPECTION ON 9,500 FLT CYCLE AS PER SRM 53-00-07 REPAIR 9 TABLE 201 REV 44.
MAIN DECK CARGO RT STA 1601, L-12 FRAME FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07 REPAIR 2 FIG 201 REV 43. INITIAL INSPECTION TO BE CARRIED OUT ON 14,500 FLT CYCLE AND REPETITIVE INSPECTION ON 9,500 FLT CYCLE AS PER SRM 53-00-07 REPAIR 2 TABLE 201 REV 43. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 110.
MAIN DECK CARGO RT STA 1761 L-12 FRAME FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07 REPAIR 2 FIG 201 REV 44. INITIAL INSPECTION TO BE CARRIED OUT ON 14,500 FLT CYCLE AND REPETITIVE INSPECTION ON 9,500 FLT CYCLE AS PER SRM 53-00-07 REPAIR 2 TABLE 201 REV 44. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 110.
ON TAKEOFF ROLL AT 75 KTS GEN 1 & GEN 3 FLASHED OFF. REJECTED TAKEOFF. GENS BOTH RESET AUTOMATICALLY. TRIED SECOND T/O. AT 52 KTS GEN 1,2,3 ALL OFF. REJECTED TAKEOFF. ALL 3 GENS CAME BACK ONLINE THEIR OWN. WX 040/4 KTS,15 DEG C. LIGHT RAIN. ACFT WAS LOADED IN RAIN. INTERROGATED EPCU FOR FAULT REVIEW, FOUND ON LEG 2 MAIN EXT PWR/INTFC PHASE C SENSE/EXT PWR WAS LOGGED. CHECKED ALL IDG FLUID LEVEL, FOUND SATISFACTORY ON ALL IDG. ALSO VISUALLY CHECKED WIRING CONDITION AT BACK SIDE OF EPCU RACK, NO DEFECT FOUND. R & R EPCU IAW AMM24-08-01-4, R-T-S TEST WAS SATISFACTORY. ACFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION.
RECEIVED "HYD 3 OFF" ALERT AT CRUISE, WITHIN 35 MINS HYD SYS 3 QTY WENT FROM 4.0 TO 2.6 GALLONS. DURING LANDING, GEAR EXTENSION RECEIVED " HYD 3 FAIL" ALERT. REMOVED AND REPLACED, HORIZ STAB PRIMARY CONTROL VALVE "PRESSURE FITTING UNION ASSY" OPS CHECK NORMAL, NO LEAKS NOTED. SERVICED NR 3 HYD SYS TO SERVICE, CHECK LIMITS .
ON TAXI INTO CAN TX RAMP, HAD CARGO FIRE LWR FWD LEVEL 3 ALERT. COMPLIED QRH CALLED FIRE DEPT, ASKED FOR FX MECHANIC TO INSPECT EXTERIOR AIRCRAFT, NO FIRE ACTUALLY OBSERVED. REMOVED AND REPLACED LOWER CARGO NR 1 FIRE BOTTLE AS PER AMM 26-22-01-4, AND ALSO REMOVED AND REPLACED TWO DISCHARGE CARTRIDGES AS PER AMM 26-22-04-801. PERFORMED THE OPS TEST OF THE LOWER CARGO SMOKE DETECTOR IAW AMM26-14-01-5, FOUND NORMAL. SO REPLACED THE 5 EA DETECTORS OF FWD LOWER CARGO (JUST REQUIRED IN THE TSI 26-12/4016) IAW AMM 26-14-01-4, AND PERFORMED THE OPS TEST IAW AMM26-14-01-5, FOUND NORMAL.
RT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATION. RT WING INBOARD FLAP VANE REMOVED AND REPLACED AS PER AMM 27-50-22-4. FLAP VANE ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5 FOUND SATISFACTORY.
MAIN DECK CARGO, CENTER AUXILIARY TANK UPPER SURFACE FOUND CORROSION AT STA 1229 X = 6. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. FOUND TO EXCEED LIMIT AS PER SRM 57-20-00 FIGURE 13 VOLUME I. REPAIR CARRIED OUT AS PER EA 1-5710-122666. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
MAIN DECK CARGO RT FRAME STATION 1741 AT LONGERON 11 FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. DAMAGE TOLERANCE INSPECTION REQUIRED AT INITIAL FLIGHT CYCLE 14,500 AS PER SRM 53-30-00 FIGURE 1 VOLUME I.
MAIN DECK CARGO - LT FRAME STATION 1741 AT LONGERON 11 FOUND DENT. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. DAMAGE TOLERANCE INSPECTION REQUIRED AT INITIAL FLIGHT CYCLE 14,500 AS PER SRM 53-30-00 FIGURE 1 VOLUME I.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB, NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. AT MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
EMPENNAGE, RIGHT AFT FUSELAGE SKIN COMMON TO AFT BODY FAIRING NR 347DF LOWER MATING SURFACE FOUND WITH SURFACE CORROSION. SURFACE CORROSION ON EMPENNAGE RT AFT FUSELAGE SKIN COMMON TO AFT BODY FAIRING 347DF LOWER MATING SURFACE REMOVED AS PER SRM 51-21-01 VOLUME II. FOUND EXCEEDED LIMIT AS PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER ATTACH INBOARD HOLE FORWARD AND AFT SURFACE FOUND WITH CORROSION. REWORKED AS PER EA 1-5750-127701. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER ATTACH INBOARD HOLE FOUND WITH CORROSION. REWORKED AS PER EA 1-5750-127701. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR ATTACH OUTBOARD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-122667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR ATTACH INBOARD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-122667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 3 SUPPORT FITTING AT HOLE NR A. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLES NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 6 SUPPORT FITTING AT HOLES A, B AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 1 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CENTER CARGO DOOR LOWER FORWARD CORNER FOUND DOOR SKIN DAMAGED. REPAIR CARRIED OUT AS PER E.A. NO. 1-5230-127702 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CENTER CARGO DOOR LOWER FORWARD CORNER FOUND DOOR SKIN DAMAGED. CENTER CARGO DOOR LOWER FORWARD CORNER, DOOR SKIN DAMAGED AREA REPAIR CARRIED OUT AS PER EA 1-5230-127702. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
CENTER LANDING GEAR WHEEL WELL, FOUND RIGHT FORWARD MOST CORNER CUTOUT DOUBLER CRACKED. CENTER MLG WW, RIGHT FORWARD MOST CORNER CUTOUT CRACKED. DOUBLER REMOVED AS PER SRM 51-33-01 VOLUME II. FASTENER HOLES PICKED UP ON NEW DOUBLER AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE ACCESS PANEL NR 619CB CUTOUT FOUND CRACKED. RIGHT WING FIXED LEADING EDGE ACCESS PANEL 619CB CUTOUT CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
EMPENNAGE: AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD STA 2007 QUANTITY 01 STIFFENER X = -15.25 FOUND CRACKED APPROX 0.35 INCH AT UPPER CORNER AREA. AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD STATION 2007 X = -11.25 STIFFENER CARRIED OUT REPAIR AS PER EA 1-5310-122664 PART 1. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RT WING FIXED LEADING EDGE SLAT TRACK 16 INBD RIB FOUND CRACKED. RIB REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RIGHT WING FIXED LEADING EDGE SLAT TRACK 12 SKIN FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CENTER CARGO COMPT: DOORWAY CEILING AREA MAIN DECK CARGO FLOORBEAM LOWER FLANGE AT STA 1761, X = -100 FOUND DENTED. [07-25-07] REPAIRED AS PER EA 1-5310-112358.
LT WING FUEL TANK AT STRINGER 15 FOUND CRACKED. [07-24-07] SLOTTED OUT AND REPAIRED AS PER SRM 57-20-00, FIG 11, VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
CTR CARGO COMPT, FLOORBEAM STA 1781 FWD FLANGE AT X = -50 CRACKED. [07-24-07] REPAIRED AS PER FEDEX EA 1-5310-112354. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
NOSE LANDING GEAR LT TRUNNION FOUND CRACKED. [07-24-07] REPAIR CARRIED OUT AS PER SRM 53-40-00 VOL.I. FIG. 23. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
ENG 1 OIL FILTER ALERT CAME ON DURING CRUISE, ACCOMPLISHED QRH CHECKLIST, SHUTDOWN ENG 1. DUMPED 20K AND LANDING IN TPE. ENG 1 OIL FILTER ALERT CAME ON DURING CRUISE. ACCOMPLISHED CHECKLIST SHUTDOWN ENG 1. DUMPED 20K OF FUEL AND LANDING IN TPE. DUE TO THE NR 1 ENGINE HAS METAL FLAKES IN THE FILTER AND CHIP DET. POWERPLANT ENGINEER HAS GIVEN THE APPROVAL FOR ENGINE CHANGE. DUE TO THE NR 1 ENGINE HAS METAL FLAKES IN THE FILTER AND CHIP DET. COMPLIED WITH NR 1 ENG CHANGE PER T CARD 71T0001-GE AND 71T0901-GE.
RECEIVED "ENG 1 OIL FILTER". PROCEEDED VIA QRH PROCEDURES, SHUT DOWN ENGINE AND DESCENDED TO 300 (FROM 360). ALL ENGINE PARAMETERS NORMAL OTHER THAN THE ALERT. DECLARED EMERGENCY AND LANDED AT PANC. INSPECTED MASTER CHIP DETECTOR AND SCAVANGE FILTER ELEMENT WITH NO CONTAMINATION FOUND. INSTALLED NEW FILTER PER MM 79-22-05-4. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL SWITCH PER MM 79-35-01-4. RUN ENGINE PER JRH (271982). NO FAULTS NOTED. LEAK CHECK GOOD. OK FOR SERVICE.
ENG 2 A/I OFF ALERT AT FL 050 WITH A/I ON IN MODERATE ICING. DEPARTED ILE RETURNED CDG. R&R HARNESS ON ENG 2 PER AMM 71-50-04-4 AND INSTALLED ANTI ICE VALVE NEW ONE PER AMM 30-22-01-4 AND INSTALLED ALL PLUGS. REMOVED BEFORE PER ESMP AND RECONNECTED SENSE LINE AND IDG PLUG TIGHTENED PERFORMED ENG 2 RAN UP PER JRH, ALL PARAMETERS ARE OK AND NO ALERT DISCOVERED DURING ENG RUN UP. ENG 2 COWLING SECURED CLOSED, TAIL CONE AND AFT PLATFORM SECURED CLOSED PER AMM 71-10-00-2 AND 52-46-1-2. A/C OK FOR SERVICE.
ON CLIMB-OUT AT APPROX 8,000 FT RECEIVED ENGINE 2 A/ICE DUCT ALERT. COMPLIED W/CHECKLIST LIGHT WENT OUT AT IDLE. RTB FOR UNEVENTFUL LANDING. PERFORMED FIM 30-22-05, NO LEAK DETECTED ON ENG NR 2 ANTI-ICE DUCT. ENG NR 2 COWL ANTI-ICE SHUTOFF VLV, FOUND DEFERRED OPEN. REMOVED AND REPLACED ENG NR 2 INLET COWL ANTI-ICE SHUTOFF VALVE AS PER MD11 MM 30-22-01-41. PERFORMED INSPECTION OF PICCOLO TUBES FOUND NIL ABNORMALITIES. PERFORMED ENG RUN-UP AS PER JRH FOR APU AND ENG NR 2 PNEUMATIC SYS DECAY CHECK, DONE. PASSED. ALSO, PERFORMED HIGH POWER ENG RUN-UP AS PER JRH. OPS CHECKED, NORMAL.
RIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACKED AT XORS=562. RIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER AT XORS=562 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE INTERNAL RIB DOUBLER FOUND CRACKED AT XORS=562. LEFT HAND WING FIXED LEADING EDGE INTERNAL RIB DOUBLER AT XORS=562 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACKED AT XORS=683. RIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER AT XORS=683 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
UPON REMOVAL OF LT WING UPPER STRINGER 13 STRINGER END FOUND TWO FASTENER HOLES ELONGATED AT XORS 562 AND XORS 550. REPAIR CARRIED OUT IAW FEDEX EA 1-5710-90767.
MAIN DECK CARGO L3 DOOR CUTOUT FRAME FOUND SURFACE CORRODED AT AFT BOTTOM CORNER.
RIGHT WING OUTBOARD FLAP OUTBOARD HINGE FAIRING 636BR SUPPORT ANGLE FOUND CRACKED. RT WING OUTBOARD FLAP OUTBOARD HINGE FAIRING 636BR SUPPORT ANGLE REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. NEW ANGLE FABRICATED AS PER DRAWING ARC0752 AND FEDEX EA 1-5750-90762.
RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FITTING AFT STRUT (ARC2128) FORWARD BOLT HOLE FOUND CORROSION. REPAIR CARRIED OUT AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FITTING AFT STRUT (ARC2128) FORWARD BOLT HOLE AS PER FEDEX EA 1-5750-90760.
LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE FITTING (ARC1991) OUTBOARD NR 3 BOLT HOLE FOUND CORROSION.
LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT, (ARC2126) FORWARD BOLT HOLE FOUND CORROSION.
RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT, (ARC2126) AFT BOLT HOLE FOUND CORROSION.
MAIN DECK CARGO SEAT TRACK AT STA 6/10, RIGHT HAND X=8.5 FOUND EDGE BROKEN. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I FROM STATION 1129 TO STATION 1149, X=8.5. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
RIGHT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1044 TO 1047. REPAIR CARRIED OUT AT RIGHT HAND WING REAR SPAR UPPER CAP AT XORS 1044 TO 1047 CORROSION AREA AS PER FEDEX EA 1-5710-90756, TITLE: WINGS - RIGHT HAND REAR SPAR UPPER CAP CORROSION AT STATIONS XORS = 1041 THROUGH XORS = 1047 - REPAIR. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
LEFT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT CRACKED AREA REPAIRED AS PER FEDEX EA 1-5730-90744, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
RIGHT HAND WING FIXED LEADING EDGE TELESCOPING DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPING DUCT CUTOUT CRACKED AREA AS PER FEDEX EA 1-5730-90745, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
RIGHT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1041 TO 1044. REPAIR CARRIED OUT AT RIGHT HAND WING REAR SPAR UPPER CAP AT XORS 1041 TO 1044 CORROSION AREA AS PER FEDEX EA 1-5710-90756, TITLE: WINGS - RIGHT HAND REAR SPAR UPPER CAP CORROSION AT STATIONS XORS = 1041 THROUGH XORS = 1047 - REPAIR. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
LEFT HAND WING OUTBOARD FLAP INBOARD HNGE SUPPORT FITTING (ARC4009) OUTBOARD NR 3 BOLT HOLE FOUND CORRODED.
SNRM N0999: RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING (ARC4009) OUTBOARD NR 3 BOLT HOLE FOUND CORRODED.
LEFT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1044-1047. LEFT HAND WING REAR SPAR UPPER CAP CORROSION AT XORS 1044-1047 AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-90754, TITLE: WINGS - LEFT HAND REAR SPAR UPPER CAP CORROSION AT STATIONS XORS = 1044 THROUGH XORS = 1047 - REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
RT FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 538. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE BEADED DOUBLER AT XORS 538 CRACKED AREA AS PER FEDEX EA 1-5730-90750.
HFEC INSPECTION FOUND CRACK ON OUTBOARD END OF STRINGER S-10L AT LEFT WING TANK. REPAIR CARRIED OUT AT LEFT HAND WING TANK END OF STRINGER S-10L CRACKED AREA AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON OUTBOARD END OF STRINGER S-9L AT LEFT HAND WING TANK. CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON OUTBOARD END OF STRINGER S-38R AT RIGHT WING TANK. REPAIR CARRIED OUT AS PER FEDEX EA 1-5720-90755.
HFEC INSPECTION FOUND CRACK ON OUTBOARD END OF STRINGER S-13R AT RIGHT WING TANK.CRACKED AREA REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON OUTBOARD END OF STRINGER S-44L AT LEFT HAND WING TANK. REPAIR CARRIED OUT IAW SRM 57-20-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.
HFEC INSPECTION FOUND CRACK ON OUTBOARD END OF STRINGER S-14L AT LEFT HAND WING TANK. REPAIR CARRIED OUT IAW SRM 57-20-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
HFEC INSPECTION FOUND CRACK ON OUTBOARD END OF STRINGER S-13L AT LEFT HAND WING TANK. REPAIR CARRIED OUT IAW SRM 57-20-00.
RIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 663. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE BEADED DOUBLER AT XORS 663 CRACKED AREA AS PER FEDEX EA 1-5730-90749.
RIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 658. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 658 CRACKED AREA AS PER FEDEX EA -5730-90749.
FOUND RIGHT FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 590. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 590 CRACKED AREA AS PER FEDEX EA 1-5730-90751.
RIGHT FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 563. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 563 CRACKED AREA AS PER FEDEX EA 1-5730-90751.
LEFT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 522. CRACKED AREA REPAIRED AS PER FEDEX EA 1-5730-90748, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
LEFT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 600. REPAIR CARRIED OUT AT LEFT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 600 CRACKED AREA AS PER FEDEX EA 1-5730-90747.
SNRM N0754: RIGHT HAND WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED.
UPPER FUSELAGE EXTERIOR FOUND SKIN WITH BURN MARK BETWEEN STATION 576 AND STATION 595 L-2LAND L3L. REPAIRED AS PER SRM 53-20-00 FIGURE 6 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100.
DURING WALK AROUND FOR TEST FLIGHT, FOUND HYDRAULIC FLUID LEAKING FROM STAB ACCESS PANEL ENT BY: 497948 RPT BY: 096450. HORIZONTAL STABILIZER NR 2 HYDRAULIC MOTOR AND BRAKE REMOVED AND REPLACED AND LEAK CHECK AND FUNCTIONAL TEST SATISFACTORY.
TO COMPLY WITH FEDEX EA 1-5510-80350, TITLE: STABILIZERS - HORIZONTAL STABILIZER - MASTER EA - REWORK TO BARREL NUT BORES IN EXCESS OF FEDEX EO 1-5510- 7-5000 (BOEING SB MD11-55-023 REV 2.) FAA AD 2003-22-08 (AMENDMENT 39-13356). COMPLIED WITH FEDEX EA 1-5510-80350, TITLE: STABILIZERS - HORIZONTAL STABILIZER - MASTER EA - REWORK TO BARREL NUT BORES IN EXCESS OF FEDEX EO 1-5510- 7-5000 (BOEING SB MD11-55-023 REV 2.) FAA AD 2003-22-08 (AMENDMENT 39-13356).
ENG 1R T/R TRANSLATING SLEEVE UPPER SLIDING TRACK AFT EDGE FOUND CRACKED. CRACK REPAIRED REFER FAA FORM 8130-3 NO 5488(J009681-000) FOR WORK DETAILS.
ENG 2L T/R TRANSLATING SLEEVE UPR SLIDING TRACK AFT EDGE FOUND CRACKED. CORRECTIVE ACTION: SNRM N0308: CRACK REPAIRED REFER FAA FORM 8130-3 NO 5489(J009682-000) FOR WORK DETAILS.
CORROSION REMOVED ON NR 14 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REPLACED AS PER SRM 51-33-01 VOL 2.
CORROSION REMOVED ON NR 1 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 C3 PT1 FIGURE 03. CORROSION REPAIRED AS PER EA 1-5510-80352 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 1L, CORROSION REMOVAL AND REPAIR.
CORROSION REMOVED ON NR 19 LT BARREL NUT BORE EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 19L. REPAIRED AS PER EA NR 1-5510-80357, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 19L, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 20 RT BARREL NUT BORE EXCEEDED LIMITS. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 20R, REPAIRED AS PER EA NR 1-5510-80359, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 20R, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 18 LT BARREL NUT BORE EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 18L. REPAIRED AS PER EA NR 1-5510-80360, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 18L, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 16 RT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 16R. REPAIRED AS PER EA NR 1-5510-81543, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 16R, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 25 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. CORROSION REPAIRED AS PER EA 1-5510-81558 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 25L, REWORKED BEYOND SB MD11-55-023 REV2 LIMIT.
CORROSION REMOVED ON NR 4 LEFT BARREL NUT BORE FOUND EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 4L. REPAIRED AS PER EA NR 1-5510-81545, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 4L, REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 3 LEFT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 3L. REPAIRED AS PER EA NR 1-5510-81562, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 3L. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 23 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 23L. REPAIRED AS PER EA NR 1-5510-81551, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 23L. REWORKED BEYOND S/B MD11-55-023 REVD 2 LIMITS.
CORROSION REMOVED ON NR 20 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 20L, REPAIRED AS PER EA 1-5510-81552.
CORROSION REMOVED ON NR 28 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 28L, REPAIRED AS PER EA 1-5510-81548
CORROSION REMOVED ON NR 33 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33L, REPAIRED AS PER EA 1-5510-81550.
CORROSION REMOVED ON NR 32 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 32L, REPAIRED AS PER EA#1-5510-81549.
CORROSION REMOVED ON NR 30 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 30L, REPAIRED AS PER EA 1-5510-81554.
CORROSION REMOVED ON 31R BARREL NUT BORE FOUND EXCEEDED LIMIT IAW EO 1-5510-7-5000 C3 PT1 FIG 03. RT HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 31R, REPAIRED AS PER EA 1-5510-81555.
CORROSION REMOVED ON NR 35 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 35L, REPAIRED AS PER EA 1-5510-81556.
CORROSION REMOVED ON NR 36 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. REPAIRED AS PER EA 1-5510-81553, HORIZONTAL STABILIZER-BARREL NUT BORE 36L - REWORKED BEYOND S/B MD11-55-023 REV. 2 LIMITS.
CORROSION REMOVED ON NR 33 RT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33R, REPAIRED AS PER EA 1-5510-81547.
CORROSION REMOVED ON NR 24 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. CORROSION REPAIRED AS PER EA 1-5510-81561.
CORROSION REMOVED ON NR 8 RIGHT HAND BARREL NUT BORE, FOUND EXCEEDED LIMIT. CORROSION REPAIRED AS PER EA 1-5510-80349 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 8R, CORROSION REPAIR SB MD11-55-023 REV2 AND EO 1-5510-7-5000.
CORROSION REMOVED ON NR 29 LEFT BARREL NUT BORE FOUND EXCEEDED LIMIT. SNRM N1061: CORROSION REPAIRED AS PER EA 1-5510-80355 HORIZONTAL STABILIZER. BARREL NUT BORE 29L. REWORKED BEYOND SB MD11-55-023 REV2 LIMIT.
CORROSION REMOVED ON NR 13 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT.
CORROSION REMOVED ON NR 15 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 15L. REPAIRED AS PER EA NR 1-5510-81560, TITLE: HORIZONTAL STABILIZER-BARREL NUT BORE 15L. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 31 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 31L. REPAIRED AS PER EA NR 1-5510-80358, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 31L. REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 36 RIGHT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 36R. REPAIRED AS PER EA NR 1-5510-81544, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 36R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS.
CORROSION REMOVED ON NR 32 RIGHT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 32R. REPAIRED AS PER EA NR 1-5510-81559, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 32R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS.
MAIN DECK, RT SIDEWALL STRUCTURE FRAME'S INNER CHORD DENT AT STA 1721, L-12R. FRAME AT STA 1721 RT SIDEWALL L-12R DENTED AREA REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. REPAIR IS CAT B INITIAL INSPECTION AT 14,500 AND REPETITIVE INSPECTION REQUIRED AT 9,500 LANDINGS. REFER TO EA NR 1-5310-76835, TITLE:FUSELAGE MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1721, LONGERON 12R.
MAIN DECK, LT SIDEWALL STRUCTURE FRAME'S INNER CHORD DENT AT STA 1701, L-12L. FRAME AT STA 1701 L-12L DAMAGED DOUBLER REMOVED AND REPLACED AS PER SRM 53-00-00 VOL I FIG 1.
LEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442-443, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.256 INCH AND REPAIRED AS EA NR 1-5750-80342, TITLE: WINGS, TRAILING EDGE FLAPS, LEFT HAND INBOARD FLAP (FLAP SIDE), PIVOT BORE REPAIR.
RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.227 INCH, AND REPAIRED AS PER EA NR 1-5750-80343, TITLE: WINGS TRAILING EDGE FLAPS, RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR.
RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.285 INCH, AND REPAIRED AS PER EA NR 1-5750-80343, TITLE: WINGS TRAILING EDGE FLAPS, RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR.
SNRM N0453: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
RT WING-OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
SNRM N0456: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
SNRM N0455: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
RT WING-OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
SNRM N0442: LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.191 INCH AND REPAIRED AS PER EA 1-5750-80344, TITLE: WINGS - LEFT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.400 INCH, MATERIAL REMOVED=0.006 INCH, REMAINING THICKNESS=0.394 INCH AND REPAIRED AS PER EA 1-5750- 80344, TITLE: WINGS - LEFT OUTBOARD FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR.
LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.394 INCH, MATERIAL REMOVED=0.004 INCH, REMAINING THICKNESS=0.390 INCH AND REPAIRED AS PER EA 1-5750-80344, TITLE: WINGS - LEFT OUTBOARD FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR.
LT WING - OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.190 INCH AND REPAIRED AS PER EA 1-5750-80344, TITLE: WINGS - LEFT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR.
LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
ENG NR 2, LEFT THRUST REVERSER TRANSLATING SLEEVE TOP SLIDE TRACK AFT EDGE FOUND WITH SUSPECTED CRACK AT AFT EDGE.
LT WING O/B FLAP STOP FITTING FOUND CRACKED. LEFT WING O/B FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II.
LEFT WING UPPER SURFACE XIS=247 FWD SIDE FOUND CORROSION. LEFT WING UPPER SURFACE XIS=247 FWD SIDE REPAIRED AS PER EA NR 1-5710- 81539, TITLE: WINGS LT WING UPPER SURFACE, CORROSION BLEND OUT AT XORS 144.25.
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.125 INCH, AND REPAIRED AS PER EA NR 1-5750-80340, TITLE: WINGS, RT OUTBOARD FLAP, I/B (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.077 INCH AND REPAIRED AS PER EA NR1-5750-80344, TITLE: WINGS, LT OUTBOARD FLAP, I/B FLAP SIDE HINGE. BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 INCH AND REPAIRED AS PER EA NR 1-5750-80344, TITLE: WINGS , LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. SNRM N0448: LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKNESS=0.514 INCH, MATERIAL REMOVED=0.009 INCH, REMAINING THICKNESS=0.505 INCH AND REPAIRED AS PER EA NR 1-5750-80344, TITLE: WINGS, LEFT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
LT WING , O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKNESS=0.503 INCH, MATERIAL. REMOVED=0.006 INCH, REMAINING THICKNESS=0.497 INCH AND REPAIRED AS PER EA NR 1-5750-80344, TITLE: WINGS, LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES. CORROSION REMOVAL AND REPAIR.
LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
SNRM N0454: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.502 INCH, MATERIAL REMOVED=0.002INCH, REMAINING THICKNESS=0.500 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.221 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.221 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.392 INCH, MATERIAL REMOVED=0.003 INCH, REMAINING THICKNESS=0.389 INCH AND REPAIRED AS PER EA NR 1-5750- 80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.408 INCH, MATERIAL REMOVED=0.006 INCH, REMAINING THICKNESS=0.402 INCH AND REPAIRED AS PER EA NR 1-5750- 80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.497 INCH, MATERIAL REMOVED=0.004 INCH, REMAINING THICKNESS=0.493 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.125 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.094 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR.
FORWARD CABIN SEAT TRACK AT STA.487, RIGHT SIDE 27.5 INCHES WITH CORROSION.
CABIN SEAT TRACK AT LT X=27.5 STA 420-495 FOUND CORRODED.
MAIN DECK CARGO BAY DOORWAY FLOOR CARGO TRACK AT LT SIDE STA 635, 8.5 INCHES FOUND CRACKED.
LT WING OUTBOARD FLAP FOUND OUTBOARD MOST HINGE FITTING HOLE QTY. 02 EACH WITH CORROSION. LT WING OUTBD FLAP, OUTBD MOST HINGE FITTING CORROSION CARRIED OUT REPAIR IAW FEDEX EA 1-5750-67577
MAIN DECK CARGO BAY DOORWAY FLOOR SEAT TRACK AT LT SIDE STA. 635, 27.5 INCHES FOUND CRACKED. CABIN STA 635, 27.5 INCHES, LT SIDE SEAT TRACK REPAIRED AS PER SRM 53-70-00, FIG.1, VOL.I.
LT WING LE CAVITY, FOUND NR 16 TRACK ATTACH FITTING INBOARD SIDE CRACKED. LT WING L/E CAVITY NR 16 TRACK I/B CRACKED FITTING REMOVED AS PER SRM 51- 33-01, VOL. II AND NEW FITTING INSTALLED AS PER SRM 51-31-01, VOL. II.
EN ROUTE FL370 GOT CABIN SMOKE ALERT, CAME ON THEN WENT OUT THEN CAME BACK ON. FOLLOWED RED TABS AND DIVERTED TO PDX. TEST OF SMOKE DETECTOR PER MM26-14-01-5. MSC FAULTED ITSELF ON LEG 10, 20, & 30. INSPECTED SMOKE DETECTORS & WIRING & CEILING AREA FROM SMOKE CURTAIN TO AFT PRESSURE BULKHEAD. INSPECTED HF COUPLERS FOR DAMAGE. ALL CHECKS NORMAL. R&R MSC PER M-M 31-42-01-4. OPS CHECK NORMAL.
CENTER LAND GEAR LT TRUNNION BOLTS LOOSE. REMOVED AND REPLACED BOLTS PER MM 32-15-01-4.
CENTER LAND GEAR RT TRUNNION BOLTS LOOSE. REMOVED AND REPLACED BOLTS PER MM 32-15-01-4.
DURING CLIMB GOT BUS R EMER OFF LEVEL 1 ALERT. DUMP 65,000 LBS FUEL. DOWN POWERED AND POWERED UP A/C, AC RETURN TO NORMAL. AS PRECAUTION REPLACED B1-138 R EMER A/C FEED RCCB3 PER MM 24-50-01-4 & EPCU RTS TEST PASSED PER MM 24-08-01-5.
ON CLIMBOUT WITH NR 2 NOSE COWL A/I VLV INOP, AND WIRED OPEN PER MEL 30-6D GOT NR 2 ENG A/I OFF ALERT CONSULTED RED TABS. REMOVED AND REPLACED ALL 3 SENSING ELEMENT D1-89, D1-90 & D1-91 PER MM 30-22-11-4. REMOVED AND REPLACED ENG A/I VALVE PER MM 30-22-00.
NR 2 ENG COWL ANTI-ICE DUCT O/H IND CAME ON IN CLIMB.
ON LEVEL OFF RECEIVED DEFLECT AILERON ALERT, CK SYS DISPLAY SHOWED AILERON DEFLECTED IN CR AT .84. MEL 27-2 DEFLECTION AILERON SYS - INOP PER METHOD A ALL. AILERONS CONFIRM NOT DEFLECTED. *S/D* REACTIVATED DEFLECTION AILERON SYS PER MXP:27-2 IAW MD-11 WDM 27-16-01. CHECK WIRING NORMAL.
AIL DEFLECT DISAG LEVEL 2 CATUION DURING FLAPS RETRACTION. *S/D* REMOVED AND REPLACED AILERON ACTUATOR ASSY IAW MD 11, RIG AND ADJUSTMENT PER MD11 MM 27-16-02-4. OK FOR SERVICE.
TWO MINUTES AFT T/O, NR 1 & 2 ENG FADEC MAINT L-1 ALERT. A/C RETURNED TO MEM.
MAIN DECK UPPER FUSELAGE SEAT TRACK CRACK AT BS 635, X=27.5 RT , BS 635, X-8.5 RT - 135, BS 635, X=47.5 LT-136. *S/D* CARRIED OUT REPAIR IN ACCORD WITH SRM 53-70-00 FIG 1 VOL 1.
99-199 - AFT T/O NORMAL, FLAP/SLAT RETRACTION DEF AIL ALERT CAME ON.