N604FE

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

AFT CARGO COMPARTMENT STATION 1902 RIGHT HAND X=-25 TO -40 FLOOR PANEL 187HF SUPPORT FOUND CORRODED. AFT CARGO COMPARTMENT STATION 1902 RIGHT HAND X = -25 TO -40 FLOOR PANEL SUPPORT REPAIR CARRIED OUT AS PER E.A. # 1-5321-T0360340 PART 1 . TITLE : FUSELAGE - CARGO COMP FLOORS - CORROSION , AFT CARGO FLOOR BEAM ANGLE REPAIR , STA 1902.150 BETWEEN X = 10 TO X -40 . REPAIR CLASSIFEID AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

AFT CARGO COMPARTMENT STATION 1902 RIGHT HAND X= -2 TO -16 FLOOR PANEL 187 FF SUPPORT FOUND CORRODED. AFT CARGO COMPARTMENT STATION 1902 RIGHT HAND X = - 2 TO -16 FLOOR PANEL SUPPORT REPAIR CARRIED OUT AS PER E.A. # 1-5321-T0360340 PART 1 TITLE : FUSELAGE - CARGO COMP FLOORS - CORROSION , AFT CARGO FLOOR BEAM ANGLE REPAIR , STA 1902.150 , BETWEEN X = 10 TO X = -40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — UNKNOWN (LT WING) · airframe 86,707 hrs · 21,184 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING - FIXED LEADING EDGE COMPARTMENT COMPARTMENT BEADED DOUBLER STATION XOS 640. EXISTING REPAIR AT LEFT HAND WING - FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 640 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57- 57-40-02-2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

FORWARD CABIN - FLOOR SEAT TRACK AT STATION 440 TO STATION 446 X = 107 FOUND CORROSION. FORWARD CABIN - FLOOR SEAT TRACK AT STATION 440 TO STATION 446 X = 107, CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED FROM EXISTING SPLICE STATION 484.784 TO END OF PART STATION 393, X = 107 AS PER SRM 51-31-01-0G. SEAT TRACK FABRICATED AS PER DOUGLAS DRAWING ABA 7680 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 86,707 hrs · 21,184 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS 584 FORMER FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB2931 REVISION H. INSTALLED FABRICATED FORMER AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS 584 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAIN DECK CARGO DOOR HINGE ( FUSELAGE SIDE ) PART NUMBER : ACA 7223-513 FOUND LOBE NUMBER 1 TO NUMBER 17 GREATER THAN 0.395". CABIN - MAIN DECK CARGO DOOR HINGE ( FUSELAGE SIDE ) PART NUMBER : ACA 7223-513 LOBE NUMBER 1 TO NUMBER 17 REWORKED AND FOUND NUMBER 14 TO NUMBER 17 EXCEED LIMIT AS PER MD-11 SRM 52-30-16-1A FIGURE 101 SHEET 3. OVERSIZED REPAIR BUSHINGS 17 EACH FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 52-34-04 REPAIR GENERAL, PARAGRAPH Y AND EA # 1-5310-T0360205 PART 1 STEPS 2 AND 5. TITLE: FUSELAGE- MAINFRAME- MAIN DECK CARGO DOOR FORWARD SUPPORT HINGE (FUSELAGE SIDE) - WORN HINGE LOBE BORES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - DROOPED LEADING EDGE EXTERIOR UPPER SURFACE FOUND CRACKED.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

MAIN DECK STATION 1737 X = -107.25 SEAT TRACK FOUND CORRODED. MAIN DECK AT SEAT TRACK STATION 1737 , X = - 107.25 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1691 TO EXISTING SPLICE STATION 1751 , X = - 107.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

WHILE ACCOMPLISHING SNRM: N01008 FOUND MAIN DECK CARGO FLOOR SUPPORT AT STATION 1940 TO STATION 1943 X = -25 CORROSION AS MARKED. MAIN DECK CARGO FLOOR SUPPORT AT STATION 1940 TO STATION 1943 , X = - 25 , CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE. CORRODED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = - 25 AS PER SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA7087 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

WHILE ACCOMPLISHING SNRM: N01183 FOUND MAIN DECK CARGO FLOOR SUPPORT AT STATION 1900 TO STATION 1904 X = - 20 FOUND CORROSION AS MARKED. MAIN DECK CARGO FLOOR SUPPORT AT STATION 1900 TO STATION 1904 , X = - 20 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE. CORRODED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1913 TO STATION 2007 X = - 20 AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

CABIN - MAIN DECK CARGO COMPARTMENT STATION 1716 X = - 107.25 SEAT TRACK FOUND CORRODED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1716 , X = -107.25 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1691 TO EXISTING SPLICE STATION 1751 , X = - 107.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N01430 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (LT WING) · airframe 86,707 hrs · 21,184 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 646 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER STATION XOS 646 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 645 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 645 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE COMPARTMENT FORMER AT APPROXIMATELY STATION XOS XOS 1018 FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB2920 REVISION BB. INSTALLED FABRICATED FORMER AT RIGHT WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 1018 AS PER SRM 51- 33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 86,707 hrs · 21,184 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 706 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER STATION XOS 706 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 86,707 hrs · 21,184 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 622 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER STATION XOS 622 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 86,707 hrs · 21,184 cycles

LEFT HAND WING FIXED LEADING EDGE LOWER SKIN CRACK AT STATION XOS 991. LEFT HAND WING FIXED LEADING EDGE LOWER SKIN AT STATION XOS 991 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 9 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 6-2-100. INITIAL INSPECTION TO BE CARRIED OUT 24 MONTHS FROM TIME OF REPAIR AND REPETITIVE AT EVERY 24 MONTHS PER SRM 57-40-01-2R TABLE 201/REPAIR 9.

Part: DOUBLER — CRACKED (LT WING) · airframe 86,707 hrs · 21,184 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 760 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER STATION XOS 760 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE PANEL FORMER AT APPROXIMATELY STATION XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB2920 REVISION BB. INSTALLED FABRICATED FORMER AT RIGHT WING FIXED LEADING EDGE PANEL AT APPROXIMATELY STATION XOS 1025 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 499 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 499 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 86,707 hrs · 21,184 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER STATION XOS 630 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER STATION XOS 630 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 787 FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 787 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 789 FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT RIGHT WING FIXED LEADING EDGE AT APPROXIMATELY STATION XOS 789 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 735 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 735 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 614 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 614 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CRACKED (L3 DOOR) · airframe 86,707 hrs · 21,184 cycles

CABIN - L3 DOOR FORWARD #5 STOP BEAM FOUND CRACK. CABIN - AT L3 DOOR CRACKED #5 STOP BEAM REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 637 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 637 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CRACKED (L3 DOOR) · airframe 86,707 hrs · 21,184 cycles

CABIN - L3 DOOR AFT #2 STOP BEAM FOUND CRACK. CABIN - AT L3 DOOR CRACKED #2 STOP BEAM REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 545 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 545 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 990 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 990 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 86,707 hrs · 21,184 cycles

RIGHT WING - FIXED LEADING EDGE FORMER AT APPROXIMATELY STATION XOS 584 FOUND CRACK. RIGHT WING - FIXED LEADING EDGE CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FROMER PER DOUGLAS DRAWING ARB2931 REVISION H. INSTALLED FARICATED FORMER AT RIGHT WING FIXED LEADING EDGE AT APPROXIMATELY STATION XOS 584 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAINDECK FLOOR PANEL NUMBER 271EF AT STATION 1381 TO STATION 1481 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 271EF AT CABIN STATION 1381 TO STATION 1481 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 271EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 271EF INSTALLED AS PER AMM 53- 21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAINDECK FLOOR PANEL NUMBER 291DF AT STATION 1914 TO STATION 2007 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 291DF AT CABIN STATION 1914 TO STATION 2007 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 291DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 291DF INSTALLED AS PER AMM 53-21- 04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAINDECK FLOOR PANEL NUMBER 291EF AT STATION 1914 TO STATION 2007 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 291EF AT CABIN STATION 1914 TO STATION 2007 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 291EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 291EF INSTALLED AS PER AMM 53-21- 04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAINDECK FLOOR PANEL NUMBER 292DF AT STATION 1914 TO STATION 2007 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 292DF AT CABIN STATION 1914 TO STATION 2007 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 292DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 292DF INSTALLED AS PER AMM 53-21- 04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAINDECK FLOOR PANEL NUMBER 293HF AT STATION 1914 TO STATION 2007 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 293HF AT CABIN STATION 1914 TO STATION 2007 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 293HF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 293HF INSTALLED AS PER AMM 53-21- 04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAINDECK FLOOR PANEL NUMBER 293EF AT STATION 1909 TO STATION 2007 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 293EF AT CABIN STATION 1909 TO STATION 2007 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 293EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 293EF INSTALLED AS PER AMM 53-21- 04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 86,707 hrs · 21,184 cycles

FORWARD CABIN - MAINDECK FLOOR PANEL NUMBER 221GF AT STATION 423 TO STATION 459 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 221GF AT CABIN STATION 423 TO STATION 459 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 221GF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 221GF INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAINDECK FLOOR PANEL NUMBER 282HF AT STATION 1661 TO STATION 1741 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 282HF AT CABIN STATION 1661 TO STATION 1741 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 282HF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 282HF INSTALLED AS PER AMM 53- 21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 86,707 hrs · 21,184 cycles

CABIN - MAINDECK FLOOR PANEL NUMBER 292EF AT STATION 1909 TO STATION 2007 FOUND DELAMINATED. DELAMINATED FLOOR PANEL NUMBER 292EF AT CABIN STATION 1909 TO STATION 2007 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL NUMBER 292EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL NUMBER 292EF INSTALLED AS PER AMM 53- 21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

MAIN DECK STATION 1942 TO 1964 RIGHT HAND X = - 107.25 SEAT TRACK FOUND CORRODED. MAIN DECK AT SEAT TRACK STATION 1942 TO STATION 1964 , X = - 107.25 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1751 TO END OF PART STATION 2007 X = - 107.25 AS PER SRM 53- 53-00-52-2R REPAIR 6 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

MAIN DECK STATION 1977 TO STATION1987 RIGHT HAND X = - 107.25 FLOOR SEAT TRACK FOUND FOUND CORRODED. MAIN DECK AT SEAT TRACK STATION 1977 TO STATION 1987 RIGHT HAND X = - 107.25 , CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1751 TO END OF PART STATION 2007 X = - 107.25 AS PER PER SRM 53-00-52-2R REPAIR 6 FIGURE 201. REFER TO SNRM N01426 FOR WORK DETAILS. REPAIR REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (MAIN DECK) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

MAIN DECK STATION 1964 TO STATION 2000 RIGHT HAND X = - 56 FLOOR SUPORT FOUND CORRODED. MAIN DECK STATION 1964 TO STATION 2000 RIGHT HAND X = - 56 AT FLOOR SUPPORT , CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE. CORRODED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = - 56 AS PER 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.

Part: CARGO TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1153 TO STATION STATION 1163 X = - 8.5 FOUND CORROSION. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1153 TO STATION STATION 1163 , X = - 8.5 CORRROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52- 1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1189 TO EXISTING SPLICE STATION 1129 , X = - 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: FLOOR SUPPORT — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

MAIN DECK STATION 1967 TO STATION 1984 RIGHT HAND X = - 2 FLOOR SUPPORT FOUND CORRODED. MAIN DECK STATION 1967 TO STATION 1984 RIGHT HAND X = - 2 AT FLOOR SUPPORT CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE. CORRODED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = - 2 AS PER 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.

Part: FLOOR SUPPORT — CORRODED (MAIN DECK) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

MAIN DECK STATION 1921 TO 1941 LEFT HAND X = 57 FLOOR PANEL SUPPORT FOUND CORRODED. MAIN DECK STATION 1921 TO STATION 1941 LEFT HAND X = 57 AT FLOOR PANEL SUPPORT , CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE. CORRODED FLOOR PANEL SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007, X = 57 AS PER SRM 51-31-01-0G. FLOOR PANEL SUPPORT FABRICATED BY MACHINIG AS PER DOUGLAS DRAWING AGA 7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK X = - 27.5 AT STATION 790 TO STATION 795 FOUND CORROSION. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 790 TO STATION 795 , X = - 27.5 CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 785 TO STATION 832 X = - 27.5 AS PER SRM 53- 00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (MAIN DECK) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

MAIN DECK STATION 1967 TO STATION 1984 LEFT HAND X = 2 FLOOR PANEL SUPPORT FOUND CORRODED. MAIN DECK STATION 1967 TO STATION 1984 LEFT HAND X = 2 AT FLOOR PANEL SUPPORT , CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE. CORRODED FLOOR PANEL SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = 2 AS PER SRM 51-31-01-0G. FLOOR PANEL SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7081 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 86,707 hrs · 21,184 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1159 TO STATION STATION 1163 X = 8.5 FOUND CORROSION. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1159 TO STATION STATION 1163 X = 8.5 ,CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK TRACK REPLACEMENT FROM STATION 1189 TO EXISTING SPLICE STATION 1129 , X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 86,707 hrs · 21,184 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON RIGHT HAND NOSE LANDING LANDING GEAR TRUNION FITTING AND FOUND 01 EACH CRACK APPROXIMATELY 0.1 INCH PROPAGATE PROPAGATE FROM THE SLOT AREA AT STATION Y=595. RIGHT HAND NOSE LANDING GEAR TRUNION FITTING AT STATION Y=595 CARRIED OUT REPAIR IN ACCORDANCE WITH EA NUMBER 1-5310-T0315112 A PART 3. TITLE: " FUSELAGE - MAIN FRAME - RH NLG TRUNION FITTING CRACK INSPECTION". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (LT NLG) · airframe 86,707 hrs · 21,184 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AND FOUND 01 EACH CRACK APPROXIMATELY 0.25" PROPAGATE FROM THE SLOT AREA AT STATION Y=595. LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AT STATION Y = 595 CARRIED OUT REPAIR REPAIR IN ACCORDANCE WITH EA # 1-5310-T0315111 A PART 3 TITLE : " FUSELAGE - MAIN FRAME - LH NLG TRUNNION FITTING CRACK REPAIR" REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: GEARBOX — MALFUNCTIONED (FIRE WARNING) · airframe 82,150 hrs · 19,954 cycles

INTERMITTENT "FIRE DET 2 FAULT" DISPALYED ON STATUS MAINT PAGE. OBSERVED 3 HRS INTO FLIGHT. REMOVED AND REPLACED THE ENGINE FIRE DETECTOR GEAR BOX, REF AMM 26-11-03-4-1. REMOVED AND REPLACED THE ENGINE FIRE DETECTOR UPPER RT TURBINE, REF AMM 26-11-03-4-1. PERFORMED ENGINE RUN PER JRH SECTION 5. NO FAULT SHOWN. OPS CHECK GOOD.

Part: FUEL CELL — CORRODED (CENTER) · airframe 82,150 hrs · 19,954 cycles

MAIN DECK APPROX STA.1229, RBL X=47.50 CENTER FUEL TANK UPPER SKIN IS CORRODED. REMOVED CORROSION REF. STEP 2 OF EA 1-5730-T0345575 P2. INSTALLED FASTENERS REF. STEP 11 OF EA 1-5730-T0345575 P2 ( WING-PLATES AND SKINS- CENTER WING UPPER SKIN- REWORK)

Part: FUEL CELL — CORRODED (CENTER) · airframe 82,150 hrs · 19,954 cycles

MAIN DECK APPROX STA.1229 LBL X-8.50 CENTER TANK UPPER SKIN HAS CORROSION. REMOVED CORROSION REF. STEP 2 OF EA 1-5730-T0345575 P1.INSTALLD FASTENERS REF.STEP 8 EA 1-5730-T0345575 P1.

Part: FRAME — CRACKED (TAILCONE) · airframe 82,150 hrs · 19,954 cycles

TAILCONE, L/H MIDDLE ALIGNMENT PIN, HOLE WORN ON FRAME P/N AKC 7520-3. INSTALLED REPAIR DOUBLER PER SRM 53-80-07 FIG 201 VOL 2.

Part: PIN — WORN (TAILCONE) · airframe 82,150 hrs · 19,954 cycles

[TAILCONE - L/H, TOP ALIGNMENT PIN IS WORN ON P/N AKC7520......, 2019-04-10] REPAIRED IN REF TO SRM 53-80-07 FIG 201

Part: SEAT TRACK — CORRODED (BS 1139-1179) · airframe 82,150 hrs · 19,954 cycles

SEAT TRACK CORRODED @ STA.1159 LL 10 REPLACED DAMAGED SEAT TRACK AT STA. 1159 LBL 10 REF. MD-11 51-41-01-OG AND 53-00-52- 2R

Part: SEAT TRACK — CORRODED (BS 1109-1149) · airframe 82,150 hrs · 19,954 cycles

STA.1129/6-0 RBL 10 SEAT TRACK CORRODED. REPLACED DAMAGED SEAT TRACK AT STA 1129/6-0 RBL 10 REF.MD-11 SRM 51-41-01-0G AND 53- 00-52-2R.

Part: SPAR CAP — CORRODED (LT WING) · airframe 82,150 hrs · 19,954 cycles

L/H WING REAR SPAR UPPER CAP UPPER SURFACE FROM I/B OF O/B OF FLAP TO O/B OF O/B AILERON SHOW NUMEROUS OF SURFACE CORROSION (MARKED) REMOVED CORROSION PER E.A1-5710-T034511 PART 1 FROM XORS=486.600 - XORS=827.000. REMOVED CORROSION PER E.A.1-5710-T034511PART 2 FROM XORS=843.000-XORS=1070.000

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,150 hrs · 19,954 cycles

FLOOR BOARD SUPPORT CORRODED @ STA. 6-70 CENTER LINE. REMOVED AND REPLACED FLOOR BOARD SUPPORT PN ACA 3140-11 AT STA 6-70 CENTERLINE REF DWG ACA 3140. MAJOR REPAIR

Part: BULKHEAD WEB — CRACKED (BS 595) · airframe 82,150 hrs · 19,954 cycles

L/H STA. 595 BULKHEAD WEB -85 DOUBLER LOWER EDGE IS DAMAGED/TORN AT LONG 44L REPAIRED PER EA# 1-5310-T0344724

Part: BULKHEAD WEB — CRACKED (BS 595) · airframe 82,150 hrs · 19,954 cycles

INSIDE L/H ACM COMPARTMENT, AT STA. 595 BULKHEAD, LOWER WEB AND "T" CHORD, FOUND ELEVEN FASTENERS HOLES WITH INDICATION. REPAIRED PER EA#1-5310-T0344724

Part: SEAT TRACK — CORRODED (BS 1129) · airframe 82,150 hrs · 19,954 cycles

[MAIN CABIN SEAT TRACK AT STA 1129 AND RBL 10 SHOWS EVIDENCE OF CORROSION IN THE CENHTER OF THE TRACK, (PEELING UP), 2019-03-29] REMOVED LIGHT SURFACE CORROSION AT STA.1129 RBL10 SEAT TRACK REF SRM 51-21-01. MATERIAL REMOVED .014 INCH AND FOUND WITHIN LIMITS REF 53-00-52-1A FIG.101 SHEET 2 PAGE2.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 82,150 hrs · 19,954 cycles

RT STA. 595 BULKHEAD WEB FOUND 11 EA. OPEN HOLES IN BULKHEAD, 7 EA OPEN HOLES COMMOM TO TEE CAP VERT. LEG AND 1 EA. OPEN HOLE ON TEE CAP FWD HOZ. LEG HAVE CRACK INDICATION. BUSHED HOLES PER EA # 1-5310-T0344771 - PART 1.

Part: SKIN — GOUGED (RT WING) · airframe 82,150 hrs · 19,954 cycles

[2 IN. GOUGE FOUND ON LE OF RT WING NEAR SLAT TRACK NR 3, 2019-03-09] REPAIRED IN REF TO SRM 57-40-02-2R, FIG 201, SHEETS 1 & 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 82,150 hrs · 19,954 cycles

MAIN CABIN RT OUT/BRD SEAT TRACK ASSY AT STA 635 TO STA 825 HAS HEAVY CORROSION. REMOVED AND REPLACED RT O/B SEAT TRACK ASSY REF DAC DWG ACA7458.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,150 hrs · 19,954 cycles

MAIN DECK FLOOR SUPPORT ASSY AT STA 615 BETWEEN RBL 48 AND RBL 75, HAS HEAVY CORROSION THRU OUT ASSY. REMOVED AND REPLACED FLOOR SUPPORT ASSY REF SRM 51-31-01. DAC DWG ACA7664.

Part: SEAT TRACK — CORRODED (BS 755-808) · airframe 82,150 hrs · 19,954 cycles

MAIN DECK SEAT TRACK AT STA.755 TO STA.808 @ RBL 75.25 HAS CORROSION ON LANDS AND ON LUG SECTIONS. REPLACED DAMAGED/CORRORED SEAT TRACK ON MAIN DECK FROM STA.755 TO STA.808 @ RBL 75.25. REFERENCE SRM-53-00-52, REPAIR-1, FIG-201.

Part: SPAR CAP — CORRODED (LT WING) · airframe 82,150 hrs · 19,954 cycles

EXFOLIATION CORROSION LT WING AFT SPAR LWR CAP AT STA XORS 593. REMOVED CORROSION ON LT WING AFT SPAR LOWER CAP. CORROSION T STA XORS 593 REF SRM 51-21-01-06. COMPLIED WITH EA 1-5710-T0344783.

Part: SPAR CAP — CORRODED (LT WING) · airframe 82,150 hrs · 19,954 cycles

EXFOLIATION CORROSION AT LT WING AFT SPAR LWR CAP AT STA XORS 738. REMOVED CORROSION ON LT WING AFT SPAR LOWER CAP AT STA XORS 738. REF SRM 51-21-01-06. COMPLIED WITH EA 1-5710-T0344783.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 82,150 hrs · 19,954 cycles

EXFOLIATION CORROSION LT WING SPAR LWR CAP AT STA XORS 593. REMOVED CORROSION ON LT WING AFT SPAR LOWER CAP CORROSION AT STA XORS 593. REF SRM 51-21-01-06. COMPLIED WITH EA 1-5710-T0344783.

Part: VANE — DELAMINATED (TE FLAP) · airframe 82,150 hrs · 19,954 cycles

LT OB FLAP VANE OB LOWER SURFACE IS DAMAGE (CHIP) AND DELAMINATED. REPAIRED LT O/B FLAP VANE O/B EDGE LOWER SURFACE DAMAGE IAW SRM 57-50-80-2 REPAIR 2.

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 82,150 hrs · 19,954 cycles

PUNCTURE IN UPPER SURFACE LT DETACHABLE ELEVATOR, 1" X .50". REPAIRED PUNCTURE ON UPPER SURFACE LT I/B DETACH ELEV AS REQ REF SRM 55-20-80-2R AND DWG ALC8942.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,150 hrs · 19,954 cycles

NR 1 ACM COMPT, AFT BULKHEAD STA 595 LOWER WEB CRACKED AT APPROX LONGERON 44-46L. (MRKD), 2019-01-31] REPAIRED PER EA # 5310-T0344724

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,150 hrs · 19,954 cycles

NR 1 ACM COMPT AFT BULKHEAD STA 595 LOWER WEB CRACKED AT APPROX LONGERON 44-46L. REPAIRED RT STA. 595 BULKHEAD PER EA# 1-5310-T0344771, P1.

Part: ANGLE — CRACKED (TE FLAP) · airframe 82,150 hrs · 19,954 cycles

RT WING, I/B FLAP, I/B ENVELOPE HAS DAMAGED TEE CAP, BOTTOM TEE CAP O/B EDGE PN ARC2736-7. REMOVED TEE ANGLE, PER DWG S2931069, REPLACED WITH FABRICATED TEE ANGLE, PER DWG S2931069.

Part: SKIN — DENTED (TE FLAP) · airframe 82,150 hrs · 19,954 cycles

RT I/B FLAP, HAS A DENT AT STA. XIFH 133.9 AND YIFH OUT OF LIMITS. REPAIRED PER EA # T1-5750-T 0344815 AND SRM 51-50-01-2R.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 82,150 hrs · 19,954 cycles

[AFT CARGO COMPARTMENT BILGE AREA LT SLANT PANEL LOWER FLOOR SUPPORT CORRODED UNDER NUT PLATES BETWEEN STA 1841 TO 1967. (DOT 5), 2019-01-24] REMOVED AND REPLACED THE FLOOR SUPOPORT IN THE AFT CARGO BAY BETWEEN STA 1841 & STA 1967 AT LBL 56 IN REF TO DWG # AGA 3857.

Part: FITTING — CORRODED (ZONE 100) · airframe 82,150 hrs · 19,954 cycles

LT INBD FLAP ROLLER FITTING ASSY P/N ANB7016-1 ATTACHMENT HOLES MARKED IN RED SHOWS SIGNS OF CORROSION REAMED 2 EA. FLAP ROLLER SUPPORT FITTING BOLT HOLES TO .5755 AND 2 EA. BARREL NUT BOLT HOLES TO .939 TO REMOVE CORROSION REF EA 1-5300-T0344984.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 82,150 hrs · 19,954 cycles

RT MLG SUPPORT FITTING ARB7118 NEEDS ACCOMPLISHMENT OF PERMANENT REPAIR PER EA 1-5720-T0326795. REPAIRED RT MLG SUPPORT FITTING IAW EA 1-5720-T0326795E. REMOVED INSTALLED REPAIR BUSHINGS, INSTALLED NEW BUSHINGS IN REF TO EA 1-5720-T0326795E. REAM 4 EA ATTACH HOLES TO COLD WORK HOLE SIZE. FOUND HOLES ALREADY AT 1.083 4 EA. REQUIRED FOR COLD WORK PER SRM 57-20-14-2R PG 1. COLD WORKED 4 EACH ATTACH HOLES IN REF TO DPS 3.67-74 AND SRM 57-20-14-2R TO COMPLY WITH EA 1-5720-T0326795. REAMED 4 EA RT MLG SUPPORT FITTING ATTACH HOLES TO 1.125 REF SRM 57-20-14-2R. FABRICATED REPAIR (4 EA) BUSHINGS IN REF WITH SRM 57-20-14-2R PG 1 OF 6.

Part: SKIN — GOUGED (LT WING) · airframe 82,150 hrs · 19,954 cycles

LEFT HAND WING UPPER LEADING EDGE SKIN INBOARD OF SLAT TRACK NR 18 GOUGED FROM NR 8 SLAT COVE DOUBLER. ACCOMPLISHED EA 1-5730-T0345111 WINGS - PLATES AND SKINS - LT WING FIXED LEADING EDGE - REWORK. MAJOR REPAIR.

Part: SKIN — CORRODED (FAN COWL) · corrosion level 2 · airframe 82,150 hrs · 19,954 cycles

#2 ENG RH FAN COWL, UPPER FWD JAMB (APPROX 24 INCHES ON PICKLE BARREL) CORRODED, MARKED. REAIRED #2 R/H FAN COWL DOOR JAMB AJC7415-4 REF SRM 54-20-15-2R FIG 201 SH 3. MAJOR REPAIR

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 82,150 hrs · 19,954 cycles

LT LOWER WING SKIN PLANK AT FUEL ACCESS PANEL 536AB (XORS 695) HOLES NR 6, 13, 15 AND 17 HAVE CRACK INDICATIONS. INSTALLED 4 EA REPAIR BUSHINGS IN FUEL ACCESS FOR PANEL 536 AB REF SRM 57-20-02-2R REPAIR 7 MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,150 hrs · 19,954 cycles

MAIN DECK SEAT TRACK AT STA 1250 RBL 48 HAS TWO AREAS DAMAGED. (MKD) 0000721523 : REPAIRED DAMAGED SEAT TRACK REF SRM 53-00-52-2R FIG 201 REPAIR 7, SRM 51-41-01, AND DWG SR10-53-002. "MAJOR REPAIR" 0000225357.

Part: BRAKE — OVERTEMP (MLG) · airframe 82,037 hrs · 19,911 cycles

ABOUT 5 MIN AFTER DEPARTING KDEN RECEIVED LEVEL 2 BRAKE OVERHEAT ALERT. THE RIGHT CENTER GEAR BRAKE SHOWED 550 DEG, REST OF THE BRAKES WERE 90 DEG. IAW CHECKLIST LOWERED GEAR AND COOLED BRAKE DOWN TO 300 DEG BEFORE RETRACTING. ENROUTE BRAKE CONTINUED TO SLOWLY COOL DOWN. ON FINAL BRAKE TEMP WAS 90 DEG AFTER LANDING INCREASED TO 330 DEG REST OF BRAKES PEAKED AT 120 DEG. REMOVED AND REPLACED NR 10 BRAKE ASSY IN REF TO AMM 32-43-20-4. LEAK AND OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: TIRE — FAILED (MLG) · airframe 81,946 hrs · 19,877 cycles

TIRE FAIL LEVEL 1 ALERT AT APPROX 80 KTS WITH AUDIBLE BANG DURING ROLLOUT FROM CAT 3 ILS AUTO LAND. CLEARED RUNWAY AND WAITED FOR MAINTENANCE INSPECTION. LATER ANNUNCIATORS, BRAKE DIFF TEMP AND ANTI-SKID ILLUMINATED. MAINTENANCE ADVISED TO TAXI SLOW. TAXIED TO RAMP. REMOVED AND REPLACED NR 7 T/W ASSY IAW AMM 32-41-01-4.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 81,750 hrs · 19,829 cycles

UNSUCCESFUL AUTOLAND 36L MEMPHIS WIND 240/4, AUTOPILOT FLARE AT 40 FT AGL, AUTOPILOT AGGESSIVELY PITCHED OVER AT 15 FT AGL CAUSING A HARD LANDING, BOUNCE X 2, PORPOSE X 2 AND POSSIBLE NOSE WHEEL FIRST CONTACT WITH RUNWAY, DURING G0-AROUND. R/R NR 1 FCC REF MM 22 01 03 4 MAINT HISTORY ERASED, NAV DATABASE CURRENT. STILL NEEDS RTS NO RTS PERFORMED OTHER MAINT ON A/C.

Part: WEB — DAMAGED (TE FLAP) · airframe 81,740 hrs · 19,825 cycles

LT INBD FLAP SKIN PANEL DAMAGED. REPLACED -3 WEB ASSY WITH A -23 WEB ASSY IAW PRODUCTION DWG ARC2305. COMPLIED WITH EA1-5730-T0343042.

Part: WIRE — BROKEN (TEST SWITCH) · airframe 81,307 hrs · 19,662 cycles

DURING A PREFLIGHT CHECK, THE R1 DOOR SLIDE PRESSURE TEST LIGHT FAILED TO TEST. FOUND A BROKEN WIRE AT THE SWITCH. TERMINATED THE WIRE. OPS CHECKED NORMAL.

Part: CYLINDER — FAILED (NLG) · airframe 80,305 hrs · 19,332 cycles

DURING CLIMBOUT, A LOUD BANG UNDER OUR FEET, RECEIVED A HYD 3 FAIL. IAW CHECKLIST, MANUAL EXTENSION OF LANDING GEAR, ON EXTENSION, NOSE GEAR FELL OUT WITH A LOUD BANG. NOSE GEAR UNSAFE INDICATION. REPLACED NOSE GEAR RETRACT CYLINDER IAW AMM 32-35-02-4.

Part: AOA — MALFUNCTIONED (LEFT) · airframe 78,892 hrs · 19,002 cycles

AFTER DEPARTURE, FELT TURBULENCE AND RECEIVED A STICK SHAKER, BOTH AUTOPILOTS, AND AUTO THROTTLES DISCONNECTED. FCP SHOWED ALL DASHES. RECEIVED SEL ELEV FEEL LEVEL 2 ALERT, RECEIVED WINDSHEAR DETECT FAIL, AND AOA HEAT LEFT FAIL LEVEL 1 ALERTS. NOTICED AIR SPEED SPLIT, RAN THE AIR SPEED ERRATIC CHECKLIST, CAPTAIN'S AIR SPEED WAS BAD, SELECTED CADC CAPTAIN ON 2 AND FLT DIR CAPTAIN ON 2 AND STATIC AIR ALTERNATE. AOA WAS PEGGED AT 25 DEG IN ERROR. STICK SHAKER NEVER WENT AWAY. USED FLAP OVERRIDE MANUAL AND ELEV FEEL MANUAL. FLEW A VISUAL TO RWY. REMOVED AND REPLACED THE LT ANGLE-OF ATTACK SENSOR IAW AMM 27-35-02-4. PERFORMED LLM R-T-S ON AUTO FLIGHT AND AUTOLAND SYSTEM, ALL TESTS PASSED IAW MM 22-00-00-5-0.

Part: DOOR — DAMAGED (NR 2 NACELLE) · airframe 78,208 hrs · 18,832 cycles

ON AIRCRAFT ARRIVAL AT GATE, MX INFORMED CREW THAN THE NR 2 ENGINE PLATFORM FOR ACCESS ON ENGINE WAS OPEN. NO COCKPIT INDICATIONS, NO UNUSUAL FLIGHT CHARACTERISTIC DURING ANY PHASE OF FLIGHT. INSPECTED ALL DAMAGE TO THE NR 2 ENGINE PATIO DOORS AND WORK PLATFORM. REMOVED DAMAGED MECHANISM PARTS TO ACFT PFM BOX. VISUAL INSPECTED PATIO DOOR LATCHING MECHANISM UNDAMAGE AND CHECKED THE EXTERIOR AND INTERIOR HINGE LINE BETWEEN THE PATIO DOOR AND TAILCONE, NO DAMAGE NOTED. CLOSE AND LATCH THE DOOR IAW AMM 52-46-01-02.

Part: TRANSMITTER — FAILED (SLATS) · airframe 77,862 hrs · 18,738 cycles

DURING CLIMBOUT AT SLAT RETRACTION, RECEIVED AN AUDIBLE WARNING FOR THE LANDING GEAR. WARNING CONTINUED UNTIL CAWS TO/LDG/CABIN ALT, CIRCUIT BREAKER WAS PULLED. CYCLED LANDING GEAR PRIOR TO PULLING CIRCUIT BREAKER. THE WARNING STOPPED, BUT WHEN GEAR WAS RETRACTED, RECEIVED WARNING AGAIN. NO OTHER VISIBLE FLAP SLAT OR LANDING GEAR LIGHTS OR WARNINGS. REMOVED AND REPLACED THE LT, OTBD FLAP POSITION IAW AMM 27-54-02-4. DURING OPS CHECK AT 28 DEGREES, TRANSMITTER READ 0.0. DEGREES INDICATED, THE PREVIOUS TRANSMITTER WAS INSTALLED AND CLOCKED 90 DEGREES OUT. ADJUSTED NEW TRANSMITTER IAW AMM 27-50-00-5. FOUND LT INBD TRANSMITTER HIGH 1 DEGREE, AND RT INBD TRANSMITTER HIGH 1.5 DEGREE, ADJUSTED TRANSMITTERS IAW AMM 27-50-00-5. ALL TRANSMITTERS OPS CHECKED GOOD IAW AMM 27-54-00-5. REMOVED AND REPLACED RT INBD FLAP TRANSMITTER IAW AMM 27-54-04-4. OPS CHECKED GOOD IAW AMM 27-50-00-5.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 77,361 hrs · 18,583 cycles

LEFT WING- INBD FLAP OTBD FWD HINGE BRACKET PIVOT BORE FOUND CORRODED. CORROSION REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-07 AND EA 1-5750-T0330593 A, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING TE FLAP) · airframe 77,361 hrs · 18,583 cycles

RIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE BRACKET PIVOT BORE FOUND CORRODED. CORROSION REWORKED AND FOUND WITHIN LIMITS IAW 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW 57-44-07 AND EA 1-5750-T0330596A, PART 1, STEP 1F. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1405-1412) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1405 TO 1412, LBL 8 SEAT TRACK FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1, THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

AFTER FLOOR PANEL REMOVAL, FOUND STA 1790, X=75 SEAT TRACK CORRODED AT FLOOR PANEL CONTACT AREA. CORROSION REMOVED AS PER SRM 51-21-01-0G AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101. REPAIR CARRIED OUT PER SRM 53-00-52-2R FIGURE 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 5-45 TO 5-53, LBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 5-40 TO 5-46, RBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1407-1417) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1407 TO 1417, RBL 47 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 615) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

FOUND BS 615, RBL 47 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-21- 01-0G AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A ALLOWABLE DAMAGE 1, FIGURE 101. REPAIR CARRIED OUT ON SEAT TRACK AT STA 605, X = -47 AS PER SRM 53-00-52-2R, FIGURE 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1432-1440) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1432 TO 1440, RBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 655) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

FOUND BS 655, RBL 47 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, ALLOWABLE DAMAGE 1, FIGURE 101. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1276) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK SEAT TRACK BS 1276, LBL 8 FOUND WORN. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE ATTACH LOWER BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09. OVERSIZE BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789, PART 1, STEP 1C.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET UPPER INBOARD MOUNT BORE CORRODED. EXCEEDS LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1A.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET LOWER OUTBOARD MOUNT BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789 PART 1 STEP 1B AND STEP 1.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP OTBD FWD HINGE BRACKET, UPPER OTBD MOUNT BORE FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789 PART 1 STEP 1A.

Part: SEAT TRACK — CORRODED (BS 1276) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1276, RBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG. 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM-6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, INBOARD FWD HINGE BRACKET LOWER OTBD MOUNT BORE CORRODED. EXCEED LIMITS IAW CMM 57-44-08. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1C, AND STEP 1.

Part: SEAT TRACK — CORRODED (BS 1254-1259) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1254 TO 1259, RBL 8 SEAT TRACK FOUND CORRODED. FOUND EXCEEDED LIMITS SRM 53-00-52-1A, FIGURE 101. REMOVED AND REPLACED IAW SRM 51-21-01-0G, AND SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OUTBD FLAP, INBD FWD HINGE BRACKET ACTUATOR INBOARD LUG BORE FOUND CORRODED. EXCEEDED LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1D.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET LOWER INBOARD MOUNT BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789 PART 1 STEP 1B AND STEP 1.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT HAND WING OUTBD FLAP OUTBD FWD HINGE BRACKET ACTUATOR OUTBOARD LUG BORE FOUND CORROSION. CORROSION. AT LEFT HAND WING OUTBD FLAP OUTBD FWD HINGE BRACKET ACTUATOR OUTBOARD LUG BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. EXISTING HOLE DIA. 1.252", FINAL HOLE DIA. 1.258", MAXIMUM ALLOWABLE HOLE DIA. 1.220", OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER EA #: 1-5750- T0330789 PART 1 STEP 1D TITLE: WINGS-FLIGHT SURFACES - E.O. 1-5750-7-5002-LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO WRI: 57505637 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET PIVOT BORE FOUND CORROSION. EXCEEDED LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806 PART 1 STEP 1B.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE ATTACH UPPER BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789, PART 1, STEP 1C.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET UPPER INBOARD MOUNT BORE CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789 PART 1 STEP 1A.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET UPPER OUTBOARD MOUNT BORE CORRODED. EXCEEDS LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED EA 1-5750-T0330806, PART 1, STEP 1A.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET ACTUATOR INBOARD LUG BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330789, PART 1, STEP 1D.

Part: SUPPORT — CRACKED (LT WING) · airframe 77,361 hrs · 18,583 cycles

LEFT WING FIXED LEADING EDGE XOS 546 ACCESS PANEL FWD SUPPORT STRUCTURE FOUND CRACKED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, AND DWG ARB2933 REV T & AJ. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET LOWER INBOARD MOUNT BORE CORRODED. EXCEEDS LIMITS IAW CMM 57-44-08. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1C, AND STEP 1.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING OUTBD FLAP, INBD FWD HINGE BRACKET ACTUATOR OUTBOARD LUG BORE FOUND CORRODED. EXCEEDED LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1D.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING OTBD FLAP FWD HINGE BRACKET ACTUATOR INBD LUG BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330808 PART 1 STEP 1B.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE BRACKET UPPER OUTBOARD MOUNT BORE FOUND CORROSION. HINGE BRACKET REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.943", FINAL HOLE DIA 0.952" MAXIMUM ALLOWABLE HOLE DIA 0.944 OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0330790 PART 1 STEP 1A TITLE: WINGS-FLIGHT SURFACES EO 1-5750-7-5002 - RT WING - OUTBD FLAP OUTBD HINGE (WINGSIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE BRACKET UPPER OTBD MOUNT BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHING FABRICATED AND INSTALLED EA 1-5750-T0330808 PART 1 STEP 1A.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE BRACKET UPPER INBD MOUNT BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHING FABRICATED AND INSTALLED EA 1-5750-T0330808 PART 1 STEP 1A.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING OTBD FLAP OTBD FWD HINGE, LOWER OTBD MOUNT BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330790 PART 1 STEP 1B AND STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RT WING OUTBD FLAP OUTBD FWD HINGE BRACKET SIDE ATTACH LOWER BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 0.389", FINAL HOLE DIA. 0.409" MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0330790 PART 1 STEP 1C. TITLE: WINGS- FLIGHT SURFACES-EO 1-5750-7-5002-RT WING-OUTBD FLAP OUTBD HINGE (WINGSIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RT WING OUTBD FLAP OUTBD FWD HINGE BRACKET SIDE ATTACH UPPER BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330790 PART 1 STEP 1C.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET LOWER INBD MOUNT BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330790 PART 1 STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET ACTUATOR INBD LUG BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330790 PART 1 STEP 10.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RT WING OUTBD FLAP OUTBD FWD HINGE BRACKET ACTUATOR OUTBD LUG BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 1.248", FINAL HOLE DIA 1.256" MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0330790 PART 1 STEP 10. TITLE: WINGS- FLIGHT SURFACES-EO 1-5750-7-5002-RT WING-OUTBD FLAP OUTBD HINGE (WINGSIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING OTBD FLAP FWD HINGE BRACKET FOR ACTUATOR OTBD LUG BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330808 PART 1 STEP 1B.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RT HAND WING OUTBD FLAP OUTBD FWD HINGE BRACKET UPPER INBOARD MOUNT BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER INBD MOUNT BORE NR 2 HOLE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 0.943", FINAL HOLE DIA. 0.952" MAXIMUM ALLOWABLE HOLE DIA 0.944 OVERSIZE BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER EA 1-5750-T0330790 PART 1 STEP 1A TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002 - RT WING - OUTBD FLAP OUTBD HINGE (WINGSIDE). CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING, INBD FLAP FWD HINGE BRACKET PIVOT SPOT FACE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. REPAIRED IAW EA 1-5750-T0330593 A, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (BS 2140-2164) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

AFT ACCESSORY BAY , FOUND FUSELAGE SKIN WITH CORROSION BETWEEN BS 2140 AND 2164, AT LONGERON 33 TO LONGERON 35R. FUSELAGE SKIN RH STA 2140 TO STA 2164, LONGERON 33 TO LONGERON 35 CARRIED OUT REPAIR AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-1A FIGURE 202.

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING, INBD FLAP INBD AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74277 D, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING, INBD FLAP AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74282 C, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

RIGHT WING INBD FLAP INBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74277, D, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

LEFT WING, INBD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74282 C, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 77,361 hrs · 18,583 cycles

DURING HFEC INSPECTION CARRIED OUT AT LT WING FIXED LEADING EDGE AT TRACK NR 10 OF XOS 659.7174. FOUND CRACK AT CORNER NR 13 APPROXIMATELY 1/8" IN LENGTH. REPAIRED IAW SRM 57-40-02-2R FIG. 201 REPAIR 7. REPAIR CLASSIFICATION IS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 77,361 hrs · 18,583 cycles

DURING HFEC INSPECTION, CARRIED OUT AT LT WING FIXED LEADING EDGE AT TRACK NR 10 OF XOS 659.7174. FOUND THE CRACK AT CORNER NR 14 APPROXIMATELY 1/4" IN LENGTH. REPAIRED IAW SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT — CRACKED (RT WING) · airframe 77,361 hrs · 18,583 cycles

RIGHT WING LEADING EDGE AT XOS 912.02. ACCESS PANEL SUPPORT FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,361 hrs · 18,583 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT AT STA XOS 995 ACCESS PANEL FORWARD DOUBLER FOUND CRACKED. RIGHT HAND WING LEADING EDGE COMPARTMENTAT XOS 995. ACCESS PANEL FORWARD CRACKED DOUBLER CARRIED OUT REPAIR AS PER SRM 57-40-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 628) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 628, LBL 47, SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1272) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1272, RBL 75 SEAT TRACK FOUND WORN. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1669) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1669, LBL 47 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 604) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 604, RBL 75 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,361 hrs · 18,583 cycles

LEFT WING LEADING EDGE AT XOS 544 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. THE REPAIR WAS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1411-1421) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1411 TO 1421, LBL 47 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 5-5 TO 5-21, X=8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 755) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 755, RBL 27 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,361 hrs · 18,583 cycles

LEFT WING LEADING EDGE AT XOS 769, BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 635) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 635, RBL 27, SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1243) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1243, LBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 77,361 hrs · 18,583 cycles

LEFT WING LEADING EDGE AT XOS 666, STRINGER FOUND CRACKED. REPAIRED IAW SRM 57-40-03-2R FIG 202 REPAIR 2. THE REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 755) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 755, LBL 27, SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 77,361 hrs · 18,583 cycles

RIGHT WING LEADING EDGE COMPARTMENT AT XOS 666 STRINGER FOUND CRACKED. REPAIRED IAW SRM 57-40-03-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1276) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1276, RBL 47 SEAT TRACK FOUND WORN. WORN AREA REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1809) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1809, RBL 8 SEAT TRACK FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND WITHIN LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.

Part: SKIN — CRACKED (LT WING) · airframe 77,361 hrs · 18,583 cycles

LEFT HAND WING NR 14 SLAT TRACK DOOR CUTOUT LOWER OUTBOARD CORNER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 201, REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,361 hrs · 18,583 cycles

RIGHT WING LEADING EDGE AT XOS 627, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG. 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1541) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1541, LBL 47 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 630) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 630, RBL 8, SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1809) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1809, RBL 27 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R, FIG. 201, REPAIR 1. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1541-1561) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1541 TO 1561, RBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1525) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1525, LBL 8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG. 201 REPAIR 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 5-5, RBL 47 SEAT TRACK FOUND WORN. WORN AREA REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,361 hrs · 18,583 cycles

RIGHT WING LEADING EDGE AT XOS 547 ACCESS PANEL LOWER DOUBLER FOUND CRACKED. DOUBLER REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE NEW DOUBLER WAS FABRICATED IAW DWG ARB2933 REV T AND AJ. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 5-5 TO 5-21, X=-8 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG. 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1669) · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1669, RBL 47 SEAT TRACK FOUND WORN. REPAIRED IAW SRM 53-00-52-2R, FIG. 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1351) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

MAIN DECK BS 1351, RBL 47 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 360) · airframe 77,361 hrs · 18,583 cycles

FAC CEILING , CENTER OBSERVER SEAT MECHANISM ACCESS HOLE SKIN FOUND CRACK. REPAIRED IAW EA 1-5320-T0330845 PART1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. A

Part: LONGERON — CORRODED (CABIN) · corrosion level 2 · airframe 77,361 hrs · 18,583 cycles

CAC BAY, LONGERON 46R FOUND CORRODED BETWEEN BS 6-90 AND 6-100. LONGERON 46R CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-00-2R FIG. 205. REPAIRED IAW EA 1-5310-T0330770 PART 1. REPAIR CLASSSIFIED MAJOR IAW GMM 6-2-100.

Part: QUICK DISCONNECT — BURNED (MAIN BATTERY) · airframe 77,185 hrs · 18,535 cycles

ON PREFLIGHT, FOUND THE BAT CHARGING CAPTION ON AFTER 30 MINUTES, LIGHT REMAINED ON. FOUND LEFT BATTERY QUICK DISCONNECT TERMINALS BADLY BURNED AND DISCONNECT ALSO BURNED. REPLACED LEFT BATTERY AND REPLACED QUICK DISCONNECT. OPS CHECKS NORMAL

Part: BRACKET — BROKEN · airframe 75,007 hrs · 17,844 cycles

WHILE PERFORMING MX, FOUND UPPER & LOWER BRACKETS HOLDING SEM BROKEN, & SEM LAYING LOOSE ON FLOOR OF COMPARTMENT. REMOVED BROKEN SUPPORT BRACKETS, AND REPLACED IAW SERVICE BULLETIN MD11-57-043

Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 74,747 hrs · 17,761 cycles

EMERGENCY POWER CAME ON DURING CRUISE WITH BATTERIES BEING DRAINED. ADG WAS DEPLOYED. BATTERY CHARGER & BATTERIES WERE REPLACED. FOUND BATTERY SHUNT IN CAC CORRODED CAUSING A FALSE INDICATION TO THE EPCU.

Part: RCCB — MALFUNCTIONED (ELECTRICAL SYS) · airframe 74,751 hrs · 17,762 cycles

TWO HOURS INTO FLIGHT, EMER POWER ON, LIGHT CAME ON. FOLLOWED QRH & DEPLOYED ADG & SELECTED ADG ELEC. UPON ARRIVAL FOUND LT EMER DC BUS UNPOWERED. CHECKED EPCU & NO FAULT FOUND IAW SSM 24-34-0. RECYCLED LT EMER DC FEED RCCB, B1-1754, CB & BACK TO NORMAL. IAW AMM 24-24-00-4 R & R B1-1754 RCCB AS PRECAUTION IAW AMM 24-24-00-5. PERFORMED EMER POWER SYS TEST PASSED. ADG STOWED & SECURED IAW AMM 24-25-01-4. ACFT OK FOR SERVICE.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 744 hrs · 17,656 cycles

RECEIVED A LEVEL 1 TAIL PUMP OFF REPLACED S3-438 BLOCK RAIL REF SWPM. CUT OUT 2 INCHES OF DAMAGED WIRE AND RETERMINATED AT S3-438 BLOCKS 17L, 18L AND 19L REF WDM 28-22-05 AND SWPM. ALSO REPLACED BLOCKS 15CC, 17L, 18L, 19L AND 20L AT S3-438 REF SWPM. ADJACENT WIRE BUNDLES INSPECTED AND SECURED REF SWPM. NO FURTHER DAMAGE NOTED. REMOVED AND REPLACED RT TAIL TRANSFER PUMP IAW AMM 28-22-01-2. FUEL SYSTEM TEST CHECKS GOOD IAW AMM 28-22-01-5. LEAK CHECKS GOOD. THIS CLEARS MEL. A/C OK FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 727 hrs · 17,122 cycles

DURING CLIMB OUT AT 16K FEET, ENGAGED AP 1 & RECEIVED STAB OUT OF TRIM LEVEL 2. RAN QRH & LEVEL 2 DID NOT GO AWAY. TRIM SEEMED TO BE MOVING ON AP1, BUT LEVEL 2 WAS STILL THERE, ON AP 2 THE AUTOPILOT WOULD DISENGAGE. AFTER LANDING LEVEL 1 SEL LSAS RIB OFF & SEL LSASL LOB OFF CAME ON. REPLACED BOTH FCC 1 AND FCC 2 IAW MM 22-01-03-4. PERFORMED AUTOFLIGHT SYSTEM CAT RETURN TO SERVICE IAW MM 22-00-00-5.

Part: REPAIR — CRACKED (RT NACELLE) · airframe 726 hrs · 17,076 cycles

AGEING ACFT INSPECTION, AT THE TIME OF ACFT INSPECTION, FOUND AN EXISTING FLUSH REPAIR IS DAMAGED & CRACKED ON NR 2 ENG, RT FAN COWL FWD LANDING FRAME BETWEEN 5:00 & 5:30 O CLOCK POSITION. DOT 22 REPAIR REQUIRES EVALUATION FOR MAJOR & MINOR DETERMINATION & IF THE REPAIR WAS ACCOMPLISHED USING APPROVED DATA. REPAIRED IAW EA T1-5410-T0315591 & SRM 54-20-15-2R.

Part: SPAR — CORRODED (LT WING) · airframe 726 hrs · 17,076 cycles

LEFT WING REAR SPAR UPPER CAP XORS 780 TO 1042 UPPER SURFACE OF CAP AFT FLANGE HAS EXFOLIATION CORROSION & EVALUATE IF WITHIN LIMITS. REMOVED CORROSION IAW SRM 51-21-01 & DPS 3.14. COMPLIED WITH EA 1-5710-TO315380 PART 1.

Part: FEEDER CABLE — BURNED (CARGO BAY) · airframe 726 hrs · 17,076 cycles

LOWER FWD LOBE EXTERNAL FEEDER CABLE HAS ARCED FROM BILGE PANEL AT STATION 959. R & R CABLE FEEDER WIRE IAW 20-10-03 PAGE 247.

Part: BEAM — CRACKED (FUSELAGE) · airframe 726 hrs · 17,076 cycles

FORWARD CARGO, STATION 595 BULKHEAD XX= -4 - 6, Z= -81 TRANSVERSE BEAM HAS A 2 INCH CRACK, LOWER LEG ADJACENT TO RADIUS DOT 16. 16 INCHES ABOVE CARGO FLOOR REPAIRED IN IAW SRM 53-20-08 PAGES 202 - 205.

Part: KEELBEAM — DENTED (FUSELAGE) · airframe 726 hrs · 17,076 cycles

CENTER LG WW KEEL BEAM WEB X=31.50, STATION 1427 - 1441, RT Z= -70.00 - 90.00 OIL CANNING IS OUT OF LIMITS. MEASUREMENT IS .220 MAXIMUM ALLOWABLE LIMIT IS .190. COMPLIED WITH EA 1-5310-T0315234 PART 1.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 726 hrs · 17,076 cycles

NUMBER 2 ENG, LT TORQUE BOX FWD FLANGE CRACKED APPROX 1 INCH. STOPPED DRILLED CRACK IAW CF6-80C2. SERVICE BULLETIN 78-061 REV 7 STEP 1 D 2.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 69,971 hrs · 16,236 cycles

ELEVATOR OFF THREE HOURS INTO FLIGHT. HYD QTY 4.6, SLOW LEAK NR 3 HYD SYS TO A HYD 3 OFF LEVEL 1 ALERT. HYD 3 FAIL ON GEAR EXTENSION, FOUND RT AILERON B-NUT LEAKING. TIGHTENED B-NUT AND LEAK CHECKED, NO LEAKS NOTED. OK FOR SERVICE. FOUND HYDRAULIC LINE ON AFT WALL IN CENTER WHEEL WELL CRACKED, REMOVED AND REPLACED HARD LINE IAW SMP 20-10-01-2, LEAK CHECKED GOOD.

Part: FLEX LINE — LEAKING (HYDRAULIC SYS) · airframe 69,767 hrs · 16,162 cycles

PDIS 604 29 - 02 0000711 30NOV13 SLC OPEN R LOG PAGES 02156071. HYD 3 ELEV OFF ALERT FOLLOWED BY HYD 3 QTY LOW ALERT. FLUID LEAK FROM RESERVOIR 3, FLUID REDUCED TO APPROXIMATELY 2.0. FLEX LINE INSTALLED NR 10 BRAKE CTR WW FUSE TO SWIVEL CTR LG IAW MM 20-10-01-2, NO LEAKS NOTED.

Part: ELECTRICAL SYS — MALFUNCTIONED · airframe 68,291 hrs · 15,705 cycles

EMERGENCY POWER ON ALERT 1:15 INTO FLIGHT IAW QRH CYCLED SWITCH OFF THEN BACK TO ARM. EMERGENCY POWER ON LIGHT REMAINED. NO OTHER ALERTS DISPLAYED. DEPLOYED ADG IAW QRH. STOWED ADG (WRI 24-00/9915) ELECTRICAL SYS RETURNED TO NORMAL. RAN ALL THREE ENGINES IAW JRH. NO FAULTS FOUND DURING ENGINE RUN. EPCU PASSED RETURNED TO SERVICE REF AMM 24-08-01-5. EMERGENCY POWER TEST PASSED REF AMM 24-24-00-5. CANNOT DUPLICATE FAULT, ACFT OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,127 hrs · 15,647 cycles

BS 1937 TO 1987, LBL 27 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED IAW AMM 20-50-02 REVISION 75.0. NEW FLOOR SUPPORT FABRICATED IAW DRAWING AGA7088 REVISION B. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,127 hrs · 15,647 cycles

BS 1938 TO 1982, RBL 4, FLOOR SUPPORT CORRODED. REMOVED AND REPLACED IAW AMM 20-50-02 REVISION 75.0. NEW FLOOR SUPPORT FABRICATED IAW DRAWING AGA7080 REVISION S. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: DOOR FRAME — CRACKED (L3 DOOR) · airframe 68,127 hrs · 15,647 cycles

BS 1239 TO 1259 L3 DOOR FORWARD FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: BEAM — CRACKED (L3 DOOR) · airframe 68,127 hrs · 15,647 cycles

L3 DOOR PLUG LOWER BEAM FITTING FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SEAT TRACK — CORRODED (BS 1541-1561) · corrosion level 2 · airframe 68,127 hrs · 15,647 cycles

BS 1541 TO 1561, X= 8.5 SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,127 hrs · 15,647 cycles

BS 5-33 TO 5-100 X= -75 SEAT TRACK FLANGE CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 68,127 hrs · 15,647 cycles

BS 1301 TO 1321 L3 DOOR AFT FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: DOOR FRAME — CRACKED (R3 DOOR) · airframe 68,127 hrs · 15,647 cycles

BS 1239 TO 1259 R3 DOOR FORWARD FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: DOOR FRAME — CRACKED (BS 1301-1321) · airframe 68,127 hrs · 15,647 cycles

BS 1301 - 1321, R3 DOOR AFT FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: LONGERON — CORRODED (BS 1270-1289) · corrosion level 2 · airframe 68,127 hrs · 15,647 cycles

R3 DOOR, LONGERON 28 FOUND CORRODED AT APPROX BS 1270 TO 1289. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 68,127 hrs · 15,647 cycles

RIGHT WING L/E LOWER ACCESS PANEL 619CB CUTOUT FORWARD INBD CORNER FOUND CRACKED AT XOS 612. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,127 hrs · 15,647 cycles

LOWER CENTER CARGO COMPARTMENT, LONGERON SPLICE AT BS 5-123, LONGERON 43 RT FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-33-01 REVISION 52. FABRICATED IAW DRAWING A5A7114 REVISION J. REPAIR CLASSIFED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: DOOR FRAME — CRACKED (BS 1750) · airframe 68,127 hrs · 15,647 cycles

LOWER CENTER CARGO DOOR UPPER FRAME CENTER SECTION FOUND CRACKED. REPAIRED IAW EA 1-5310-167407. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: BULKHEAD WEB — CRACKED (CARGO BAY) · airframe 68,127 hrs · 15,647 cycles

LOWER CENTER CARGO COMPARTMENT, SUMP PANEL AREA FOWARD BULKHEAD RT UPPER WEB FOUND CRACKED AT STATION 1701, "X" = -32. REPAIRED IAW EA 1-5310-166105. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: INTAKE — CRACKED (NR 2 ENGINE) · airframe 68,127 hrs · 15,647 cycles

NR 2 ENGINE INTAKE DUCT RT ON PANEL NR 364RR STATION 2140, REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: DOUBLER — CRACKED (RT WING) · airframe 68,127 hrs · 15,647 cycles

RIGHT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIRED IAW SRM 57-40-40-02 REPAIR 15 FIGURE 203 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 68,127 hrs · 15,647 cycles

RT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 870 FOUND CRACKED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIGURE 203 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: WEDGE — DELAMINATED (LT WING AILERON) · airframe 68,127 hrs · 15,647 cycles

LEFT WING - OTBD AILERON T/E WEDGE INBD EDGE FOUND DELAMINATED. REPAIRED IAW EO 1-5100-7-5001 B2 PT 1AND SRM 57-60-80 REPAIR 1 PARA 4A: 1.A REVISION 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 68,127 hrs · 15,647 cycles

LEFT WING NR 8 L/E SLAT LOWER SURFACE SKIN FOUND CRACKED AT XOS 1178. REPAIR CARRIED OUT IAW SRM 57-40-01 REPAIR 3 FIGURE 201 REVISION 52 AND E.A. 1-5750-167409. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 68,127 hrs · 15,647 cycles

RT WING OTBD FLAP T/E WEDGE INBD EDGE FOUND DELAMINATION. REPAIRED IAW EA 1-5750-165912. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: CONTROL CABLE — FAILED (MLG DOOR) · airframe 65,648 hrs · 14,935 cycles

RT MAIN GEAR DOOR WAS DOWN AND OPEN AT BLOCK IN. REPLACED RT MLG DOOR FOLLOW UP CABLE IAW AMM 32-31-00-5. ACFT OK FOR SERVICE.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 64,278 hrs · 14,577 cycles

ON CLIMBOUT PASSING FL 260 ENGINE NR 1 COMPRESSOR STALLED, EVM COMP STARTED VIBRATION 4.8 UPD TO 5.0,N1 DROPPED FROM 102.5 TO 96, EGT RISE TO 580. ON ACFT ARRIVAL FIRST INSP FOUND ALL TURBINE BLADES DAMAGED MOCC P/P CONSULTED. REMOVED AND REPLACED NR 1 ENGINE.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 63,784 hrs · 14,436 cycles

3.1875 INCH CRACK EXIST ON THE UPPER SURFACE OF THE INBD FLAP AT APPROX STA 25.875 COMPLIED WITH PT1 OF EA 1-0550-153068 ON 7/22/11 AT AREA FLAP. EA 1-5750-153138. CLEANED UP DAMAGED AREA AS REQUIRED AND FABRICATED DOUBLER. ALODINE, AND PRIMED IAW SRM 57-50-01, FIG 201. COMPLETED REPAIR OF RT INBD FLAP TOP SKIN IAW REF 57-00-01, FIG 201 OF SRM.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,244 hrs · 14,304 cycles

UPON REMOVAL OF FLOOR PANEL FOUND SEAT TRACK AT STATION 1661 TO 1721 X=-75 CORRODED. CORRODED SEAT TRACK AT STATION 1661TO 1721 X=-75 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 1751 X=-75 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REVISION 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 1661-1721) · corrosion level 2 · airframe 63,244 hrs · 14,304 cycles

UPON REMOVAL OF FLOOR PANEL, FOUND SEAT TRACK CORRODED AT STA 1661-1721, X=-75. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 1751 X=-75 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REVISION 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,244 hrs · 14,304 cycles

UPON REMOVAL OF STRINGER SPLICE 9L, HFEC FOUND CRACK APPROX 0.1" LENGTH AT CABIN STA 5-0 ON LONGERON 9L FWD SECTION. REPAIRED AS PER SRM 53-00-05 FIG 202 REPAIR 1 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112. REPAIR LONGERON SEGMENT FABRICATED AS PER EA 1-5310-143570.

Part: SEAT TRACK — CORRODED (BS 1761-1821) · corrosion level 2 · airframe 63,244 hrs · 14,304 cycles

UPON REMOVAL OF FLOOR PANEL FOUND CURVE SEAT TRACK FLANGE CORRODED AT STA 1761 TO STATION 1821 X=-75.25. REPAIRED BY SECTIONAL SEGMENT REPLACEMENT AS PER SRM 53-00-52 FIG 201 REPAIR 1 AND REPAIR 6 REVISION 46. NEW CURVED SEAT TRACK SEGMENT UTILIZED AS PER EA 1-5310-143574. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 63,244 hrs · 14,304 cycles

FUSELAGE - CAC COMPARTMENT LONGERON SPLICE AT STA 6-85, LONGERON 52 FOUND CRACKED. REMOVED AS PER SRM 51-31-01 REVISION 46. NEW LONGERON SPLICE MACHINED FABRICATED AS PER DRAWING AAA7088-1 REVISION NEW. NEW MACAHINED FABRICATED LONGERON SPLICE INSTALLED PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: STRINGER SPLICE — CRACKED (ZONE 200) · airframe 63,244 hrs · 14,304 cycles

DURING X-RAY INSP AT STA 5-0, LONG -9L, STRINGER SPLICE FOUND CRACKED, CRACK LENGTH APPROX 0.1 INCH. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISON 46. NEW STRINGER SPLICE FABRICATED BY MACHINING AS PER DRAWING AEA7633 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 63,244 hrs · 14,304 cycles

LONGERON SPLICE AT STATION 6-85, LONGERON 51R FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. NEW LONGERON SPLICE FABRICATED PER DRAWING AAA7088 REVISION NEW. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: SKIN — CRACKED (ZONE 600) · airframe 63,244 hrs · 14,304 cycles

HFEC OPEN HOLE INSP CARRIED OUT AND FOUND 05 EACH HOLES WITH CRACK INDICATION AT RT OUTER WING LOWER ACCESS DOOR CUT-OUT AT STA XORS 696.730. REPAIR CARRIED OUT PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 112.

Part: SKIN — CRACKED (RT WING LE) · airframe 63,244 hrs · 14,304 cycles

RT WING DROOP LEADING EDGE EXTERNAL SURFACE INBOARD EDGE FOUND CRACKED. RIGHT HAND WING DROOP LEADING EDGE EXTERNAL SURFACE INBOARD SIDE CARRIED OUT REWORKED AS PER EA 1-5740-143564. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 112.

Part: SKIN — CRACKED (ZONE 500) · airframe 63,244 hrs · 14,304 cycles

HFEC OPEN HOLE INSP CARRIED OUT AND FOUND 08 EACH HOLES WITH CRACK INDICATION AT LT OUTER WING LOWER ACCESS DOOR CUTOUT AT STA XORS 696.730. REPAIR CARRIED OUT AT LEFT WING OUTER WING LOWER ACCESS DOOR CUTOUT AT XORS 696.730 AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 112.

Part: LONGERON SPLICE — CRACKED (BS 1529 L31R) · airframe 63,244 hrs · 14,304 cycles

STATION 1529 LONGERON 31R EXTERIOR LONGERON END FITTING CRACKED. CRACKED LONGERON END FITTING (SPLICE) AT FUSELAGE STATION 1529 L319R EXTERIOR AREA REMOVED AS PER SRM 51-31-01 REVISION 46. NEW LONGERON END FITTING (SPLICE) MACHINED FABRICATED AS PER DRAWING AEA7643 REVISION B. NEW MACHINED FABRICATED LONGERON END FITTING (SPLICE) INSTALLED AT FUSELAGE STATION 1529 L31R EXTERIOR AREA AS PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: LONGERON — CRACKED (ZONE 100) · airframe 63,244 hrs · 14,304 cycles

FUSELAGE - STA 1529, LONGERON 30R EXTERIOR LONGERON END FITTING CRACKED. REMOVED AS PER SRM 51-31-01 REVISION 46. NEW LONGERON END FITTING (SPLICE) MACHINED FABRICATED AS PER DOUGLAS DRAWING AEA7644-1 REVISION B. NEW MACHINED FABRICATED LONGERON END FITTING(SPLICE) INSTALLED AT FUSELAGE STATION 1529 L30R AREA AS PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: SHOULDER BELT — MALFUNCTIONED (COCKPIT) · airframe 62,500 hrs · 14,121 cycles

CAPTAINS SHOULDER HARNESS VERY DIFFICULT TO UNLOCK. OPS CHECKED THE CAPTAINS SHOULDER HARNESS WITH CAPTAIN WATCHING AND SHOULDER HARNESS, OPS CHECKED NORMAL. ACFT OK TO CONTINUE.

Part: SKIN — CRACKED (ZONE 100) · airframe 60,426 hrs · 13,690 cycles

LOWER FUSELAGE - NR 1 AIR CONDITION COMPARTMENT DOOR CUT OUT AFT UPPER CORNER EXTERIOR SKIN FOUND CRACKED. REPAIRED IAW EA1-5330-140315.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

RT WING INBD FLAP AFT OTBD SEGMENT LWR SURFACE FOUND 1EA EXISTING DOUBLER NOT REPAIRED IAW SRM AT XIFH 276. REPAIRED AS PER SRM57-10-00 FIG3 VOL1 REV 40.

Part: TEE FITTING — CORRODED (TE FLAP VANE) · airframe 57,749 hrs · 13,121 cycles

LTW OTBD FLAP, FLAP VANE NR 2 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132676. (MAJOR REPAIR)

Part: SUPPORT FITTING — CORRODED (TE FLAP VANE) · airframe 57,749 hrs · 13,121 cycles

LT WING OTBD FLAP VANE NR 3 SUPPORT FITTING FWD FASTENER HOLE FOUND CORRODED. REPAIRED AS PER EA1-5750-132677. (MAJOR REPAIR)

Part: TEE FITTING — CORRODED (FLAP VANE) · airframe 57,749 hrs · 13,121 cycles

RTW OTBD FLAP, FLAP VANE NR 2 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132679. (MAJOR REPAIR)

Part: TEE FITTING — CORRODED (TE FLAP VANE) · airframe 57,749 hrs · 13,121 cycles

LTW OTBD FLAP, FLAP VANE NR 4 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132678. (MAJOR REPAIR)

Part: STRUCTURE — CORRODED (FUEL TANK) · airframe 57,749 hrs · 13,121 cycles

MAIN DECK CARGO UNDERFLOOR CTR AUX FUEL TANK UPPER SURFACE CORROSION FOUND ALONG STA 1227 AT X=77.00. REPAIR CARRIED OUT AS PER EA 1-5710-132666.

Part: SKIN — MISREPAIRED (NR 7 SLAT) · airframe 57,749 hrs · 13,121 cycles

LT WING EXISTING REPAIR FOUND ON NR 7 SLAT. REPAIRED AS PER EA1-5750-132686. (MAJOR REPAIR)

Part: FUEL TANK — CORRODED · airframe 57,749 hrs · 13,121 cycles

MAIN DECK CARGO UNDERFLOOR CTR AUX FUEL TANK UPPER SURFACE CORROSION FOUND AT STA 1233 X=46.00. REPAIR CARRIED OUT AS PER EA 1-5710-132666.

Part: SKIN — MISREPAIRED (BS 1921) · airframe 57,749 hrs · 13,121 cycles

EXISTING REPAIR AT AFT CARGO FWD LOWER DOOR JAMB AT STA 1921, LONGERON 42-L. REPAIRED AS PER SRM53-50-00 FIG17 VOL1 REV40 (MAJOR REPAIR).

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

LT WING O/B FLAP I/B HINGE (WING SIDE) O/B ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132674. (MAJOR REPAIR)

Part: BUSHING — LOOSE (TE FLAP HINGE) · airframe 57,749 hrs · 13,121 cycles

LHW O/B FLAP O/B HINGE (WING SIDE) I/B ACTUATOR HOLE BUSHING FOUND LOOSE. BUSHING REPLACED AS PER CMM 57-44-09 REV 64.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

RT WING O/B FLAP I/B HINGE (WING SIDE) I/B ACTUATOR HOLE FOUND CORROSION. REPAIR AS PER EA1-5750-132673. (MAJOR REPAIR)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

LT WING O/B FLAP I/B HINGE (WING SIDE) LOWER MOUNT I/B HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132674. (MAJOR REPAIR)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

LT WING OTBD FLAP OTBD HINGE (WINGSIDE) OTBD ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132671. (MAJOR REPAIR)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

LT WING O/B FLAP O/B HINGE (WING SIDE) UPPER MOUNT I/B HOLE FOUND CORROSION. REPAIR AS PER EA1-5750-132672 (MAJOR REPAIR).

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

LT WING O/B FLAP I/B HINGE (WING SIDE) I/B ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132674. (MAJOR REPAIR)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

LT WING O/B FLAP I/B HINGE (WING SIDE) PIVOT HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132674. (MAJOR REPAIR)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 57,749 hrs · 13,121 cycles

RT WING O/B FLAP O/B HINGE (WING SIDE) I/B ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132671. (MAJOR REPAIR)

Part: SEAT TRACK — CRACKED (BS 635) · airframe 57,749 hrs · 13,121 cycles

MAIN DECK STA 635, X= 27.5 SEAT TRACK FOUND CRACKED. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL 1 REV 40 (MAJOR REPAIR).

Part: LONGERON — CRACKED (NLG) · airframe 57,749 hrs · 13,121 cycles

CRACK INDICATION FOUND APPROX 0.2" IN LENGTH DURING HFEC INSPECTION ON THE LT NOSE LANDING GEAR TRUNNION FITTING LONGERON. REPAIRED AS PER DRAWING ACA3796 REV A (MAJOR REPAIR).

Part: LONGERON — CRACKED (NLG WW) · airframe 57,749 hrs · 13,121 cycles

CRACK INDICATION FOUND APPROX. 0.3" IN LENGTH ON THE LONGERON DURING HFEC INSPECTION ON THE RT NOSE LANDING GEAR TRUNNION FITTING AREA. REPLACED AS PER SRM51-31-01 VOL2 REV40 (MAJOR REPAIR)

Part: TRUNNION — CRACKED (NLG) · airframe 57,749 hrs · 13,121 cycles

NLG SUSPECT CRACKED RT TRUNNION FITTING. REPAIRED AS PER SRM 53-40-00 FIG 23 VOL 1 REV 40 (MAJOR CAT B REPAIR).

Part: TRUNNION — CRACKED (NLG) · airframe 57,749 hrs · 13,121 cycles

NLG SUSPECT CRACKED ON LT TRUNNION FITTING. REPAIRED AS PER SRM 53-40-00 FIG 23 VOL 1 REV 40 (MAJOR CAT B REPAIR).

Part: FITTING — CRACKED (ZONE 200) · airframe 53,414 hrs · 12,209 cycles

MAIN DECK, CARGO DOOR LOWER JAMB WHILE CARRYING OUT HFEC ON NR 3 SPOOL BRACKET BOLT BORE, FOUND ON 1 CRACK ON SUPPORT FITTING BORE HOLE "A". REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 53,414 hrs · 12,209 cycles

CRACK FOUND DURING X-RAY INSPECTION AT STATION 6-100, LONGERON NR 3R STRINGER SPLICE. FOUND CRACK LENGTH APPROXIMATELY 1 INCH. CRACKED SPLICE AT STATION 6-100, LONGERON 3R REMOVED AS PER SRM 51-31-01, VOL.2. NEW SPLICE FABRICATED AS PER DRAWING A6A7112 AND INSTALLED AS PER SRM 51-31-01, VOL.2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 53,414 hrs · 12,209 cycles

CRACK FOUND DURING X-RAY INSPECTION AT STATION 6-0, LONGERON NR 6R STRINGER SPLICE. CRACK LENGTH APPROXIMATELY 1 INCH. CRACKED SPLICE AT STATION 6-0 LONGERON 6R REMOVED AS PER SRM 51-31-01, VOL 2. NEW SPLICE FABRICATED AS PER DRAWING ADA 8413 AND INSTALLED AS PER SRM 51-31- 01,VOL.2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 53,414 hrs · 12,209 cycles

HFEC INSPECTION CARRIED OUT AND FOUND CRACK AT LONGERON NR 2 SPLICE WITH CRACK LENGTH OF APPROXIMATELY 1 INCH AT STATION 6-100. CRACKED LONGERON SPLICE AT STATION 6-100, REMOVED AS PER SRM 51-31-01, VOL 2. NEW LONGERON SPLICE FABRICATED AS PER DRAWING A6A7112 AND INSTALLED AS PER SRM 51-31-01, VOL 2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 53,414 hrs · 12,209 cycles

HFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 10 HOLES WITH CRACK INDICATION AT RIGHT WING ACCESS DOOR 636AB CUT OUT. (BETWEEN STATION XORS 683.4 AND XORS 713.6). REPAIR CARRIED OUT AS PER EA 1-5710-109926, PART 1 REPAIR CLASSIFIED AS MAJOR AS PER PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1841-1861) · corrosion level 2 · airframe 53,414 hrs · 12,209 cycles

CABIN BETWEEN STATION 1841 TO 1861, X = -8.5, SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,414 hrs · 12,209 cycles

LEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATISFACTORY' AS PER AMM 27-50-22-5.

Part: FLANGE — CORRODED (ZONE 500) · airframe 53,414 hrs · 12,209 cycles

LEFT WING LEADING EDGE APPROXIMATELY STATION XOS = 900 AT HINGE PANEL NR 526FB, INBOARD MOST LATCH MATING SURFACE FLANGE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOL.II, FOUND OUT OF LIMIT AS PER SRM 57-20- 00, FIG.17, VOL I. ORIGINAL THICKNESS 0.200", MATERIAL REMOVED 0.125" AND REMAINING THICKNESS 0.075". REPAIRED AS PER EA 1-5710-112584, PART 1. REPAIR CLASSIFIED AS CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 53,414 hrs · 12,209 cycles

HFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 7 HOLES WITH CRACK INDICATION AT LT WING ACCESS DOOR 536AB CUT OUT. REPAIR CARRIED OUT AS PER EA 1-5710-109925, PART 1. REPAIR CLASSIFIED AS MAJOR AS PER PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,414 hrs · 12,209 cycles

CABIN BETWEEN STATION 1841 TO 1854, X = 8.5 , SEAT TRACK FOUND SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1524) · corrosion level 2 · airframe 53,414 hrs · 12,209 cycles

CABIN NEAR STATION 1524, X = -75.25, SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 53,414 hrs · 12,209 cycles

MAIN DECK, MID CABIN, SEAT TRACK AT STA 6-10 TO STA 6-50, X = 8, 02 EACH CRACK FOUND ON CHANNEL. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 53,414 hrs · 12,209 cycles

MAIN DECK, MID CABIN, SEAT TRACK AT STA 6-10, X = -8, 01 EACH CRACK FOUND ON CHANNEL. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: POSITION SENSOR — MALFUNCTIONED (L/E SLAT) · airframe 48,778 hrs · 11,205 cycles

RIGHT AFTER T/O FROM RWY 25, A LEVEL 1 ALERT SLAT DISAGREE ILLUMINATED WHILE STILL IN T/O CONFIG. THE A/C WAS CLEANED UP WITH 25 KTS CLIMB-OUT, THEN THE F/O NOTICED AN OUTBOARD FLAP DISAGREE INDICATION ON THE RIGHT WING. THE LEFT BOX WAS BLANK, THE RIGHT WAS "0" WITH AUTO PILOT OFF A/C ROLLED TO THE RIGHT. DIVERTED TO MANILA, DURING LANDING CONFIG SLAT DISAGREE CAME ON AGAIN LANDED USING 0DEG/28DEG EXT AS PER QRH. REMOVED AND REPLACED RT WING INBOARD FLAP POSITION TRANSMITTER PER AMM 27-54-04-4. REMOVED AND REPLACED LT WING 4A(D1-13) SLAT POSITION SENSOR PER AMM 27-84-03-4 AND FUNCTIONAL TEST OF THE SLAT POSITION INDICATION SATIS.

Part: SKIN — DAMAGED (ZONE 600) · airframe 48,748 hrs · 11,195 cycles

RT WING I/B FLAP L/E SKIN EXISTING REPAIR. REPAIR CARRIED OUT AT RT WING I/B FLAP L/E SKIN AS PER FEDEX EA NR 1- 5750-104818,TITLE: "WINGS, FLIGHT CONTROLS, I/B RT TRAILING EDGE FLAP. PERMANENT REPAIR, EA 1-5750-102907". REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: DOOR FRAME — DENTED (BS 775) · airframe 48,748 hrs · 11,195 cycles

M/D CARGO DOOR AFT DOOR JAMB (STA 775, L12-13) FOUND SURFACE DENT. REPAIR CARRIED OUT AT M/D CARGO DOOR AFT DOOR JAMB (STA 775, L12-13) AS PER FEDEX EA 1-5310-104820, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,748 hrs · 11,195 cycles

M/D CARGO SEAT TRACK (STA 5/23, RH X=75.25) FOUND EDGE UNDER FLOOR CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 5/23 RH X=75.25 AS PER SRM 53-70- 00 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,748 hrs · 11,195 cycles

M/DECK STA 5-53 X=-48 SEAT TRACK SPLICE FITTING LOWER SIDE FOUND CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 5-53 X=-48 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,748 hrs · 11,195 cycles

FOUND EDGE UNDER FLOOR CORRODED, CARGO SEAT TRACK (STA 1316, RH X=75.25). REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1316 RH X=75.25 AS PER SRM 53-70- 00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,748 hrs · 11,195 cycles

FOUND EDGE UNDER FLOOR CORRODED, CARGO SEAT TRACK (STA 1259, RT X=75.25). REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1259 RH X=75.25 AS PER SRM 53-70- 00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,748 hrs · 11,195 cycles

M/DECK STA 5-11 X=-48 SEAT TRACK SPLICE LOWER SIDE FOUND CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 5-11 X=-48 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1751) · airframe 48,748 hrs · 11,195 cycles

MAIN DECK STA 1751 X=-9 SEAT TRACK FOUND CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1751 RT X=8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 600) · airframe 48,748 hrs · 11,195 cycles

RT WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1043. REPAIR CARRIED OUT AT RT WING REAR SPAR UPPER CAP, XORS 1043 AS PER FEDEX EA 1-5710-104817, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,748 hrs · 11,195 cycles

CARGO SEAT TRACK (STA 475, LT X=27.5) FOUND CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA475 LT X=27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: KEELBEAM — CRACKED (ZONE 100) · airframe 48,748 hrs · 11,195 cycles

CENTER LANDING GEAR WHEEL WELL RH KEEL WEB DOUBLER FOUND CRACK AT STA 1361. REPAIR CARRIED OUT AT CENTER LANDING GEAR WHEEL WELL RH KEEL WEB DOUBLER AT STA 1361 AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: WEB — CRACKED (ZONE 100) · airframe 48,748 hrs · 11,195 cycles

CENTER LANDING GEAR WHEEL WELL LT KEEL WEB DOUBLER FOUND CRACK. REPAIR CARRIED OUT AT CENTER LANDING GEAR WHEEL WELL LT KEEL WEB DOUBLER AT STA 1361 AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,748 hrs · 11,195 cycles

CRACK FOUND DURING HFEC INSPECTION AT RT WING TANK END OF STRINGER 11. REPAIR CARRIED OUT AT RT WING TANK END OF STRINGER 11, XORS 704 AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 48,748 hrs · 11,195 cycles

M/D CARGO SEAT TRACK AT STA 1029 RT X=47.5 FOUND CHANNEL EDGE CHAFED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1029 RH X=47.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 48,748 hrs · 11,195 cycles

LT WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XOS 636-643. REPAIR CARRIED OUT AT LT WING FIXED L/E BEADED DOUBLER, XOS 636-643 AS PER FEDEX EA 1-5730-104811, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,748 hrs · 11,195 cycles

CRACK FOUND DURING HFEC INSPECTION AT RT WING TANK END OF STRINGER 10.REPAIR CARRIED OUT AT RT WING TANK END OF STRINGER 10, XORS 760 AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 48,748 hrs · 11,195 cycles

M/D CARGO SEAT TRACK AT STA 1010 LT X=47.5 FOUND CHANNEL EDGE GOUGED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1010 LT X=47.5 AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 48,748 hrs · 11,195 cycles

M/D CARGO SEAT TRACK AT STA 1089 LT X=47.5 FOUND CHANNEL EDGE BROKEN. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1089 LT X=47.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,748 hrs · 11,195 cycles

CRACK FOUND DURING HFEC INSPECTION AT RT WING TANK END OF STRINGER 14. REPAIR CARRIED OUT AT RT WING TANK END OF STRINGER 14, XORS 521 AS PER SRM 57-20- 00 FIGURE 10 COLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,748 hrs · 11,195 cycles

CRACK FOUND DURING HFEC INSPECTION AT LT WING TANK END OF STRINGER 43. REPAIR CARRIED OUT AT LT WING TANK END OF STRINGER 43, XORS 565 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 48,748 hrs · 11,195 cycles

M/D CARGO SEAT TRACK AT STA 785 LT X=47.5 FOUND CHANNEL EDGE GOUGED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK, STA 785 LH X=47.5 AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 48,748 hrs · 11,195 cycles

LT WING FIXED L/E NR 12 SLAT TRACK LOWER CUTOUT FOUND CRACKED AT XOS 636-643. REPAIR CARRIED OUT AT LH WING FIXED L/E NR 12 SLAT TRACK LOWER CUTOUT, XOS 636-643 AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,748 hrs · 11,195 cycles

CRACK FOUND DURING HFEC INSPECTION AT RT WING TANK END OF STRINGER 13. REPAIR CARRIED OUT AT RT WING TANK END OF STRINGER 13, XORS 577 AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 600) · airframe 48,748 hrs · 11,195 cycles

RT WING FIXED L/E TELESCOPE DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING FIXED L/E TELESCOPING DUCT CUTOUT AS PER FEDEX EA 1- 5730- 104809, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 500) · airframe 48,748 hrs · 11,195 cycles

LT WING FIXED L/E TELESCOPE DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT LT WING FIXED L/E TELESCOPING DUCT CUTOUT AS PER FEDEX EA 1-5730-104808, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: DOOR — CRACKED (ZONE 700) · airframe 44,179 hrs · 10,267 cycles

REFER TO EA 1-5280-57095, LT MLG FLIPPER DOOR ASSY, EXISTING CRACK HAS PROPAGATED PAST STOP-DRILL HOLE. LT MLG FLIPPER DOOR ASSY R & R PER AMM 32-14-10-4. ADJUSTMENT AND TEST OF THE LT FLIPPER DOOR CARRIED OUT PER AMM 32-31-700-803.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

DURING ACCOMPLISHEMENT OF EA 1-5750-87541, LT WING OUTBOARD FLAP INBOARD HINGE FITTING (FLAP SIDE) INBOARD FORWARD BOLT HOLE FOUND CORRODED. LT WING OUTBOARD FLAP ASSY R & R PER AMM 27-50-30-4.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

LT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FOUND COROSSION EXCEEDED LIMITS. LT WING OUTBOARD FLAP ASSY R & R PER AMM 27-50-30-4. REMOVED AND REPLACED PER AMM 27-50-30-4. (CLOSED)

Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

NR 3 LT MAIN ENTRY DOOR AFT JAMB CUTOUT BETWEEN LONGERONS 24L AND 25L , LOWER INTERNAL DOUBLER (AEA7539) FOUND WITH CORROSION. REPAIRED PER SRM VOLUME I, FIGURE 17 (SHEET 3) PAGE 62. (OPEN)

Part: HINGE — CORRODED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) FORWARD HINGE FITTING INBOARD MID BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4.

Part: HINGE — CORRODED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING FORWARD BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4.

Part: HINGE — CORRODED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

DURING ACCOMPLISHMENT OF EA 1-5750-87541. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. FLAP RIGGING CARRIED OUT PER AMM 27-50-30-5.

Part: HINGE — CORRODED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

DURING ACCOMPLISHMENT OF EA 1-5750-87541. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD MID BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. (CLOSED)

Part: HINGE — CORRODED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 44,179 hrs · 10,267 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING FORWARD STRUT HOLE FOUND CORRODED STRUT. COMPLIED WITH FEDEX EA 1-5750-87545. (CLOSED)

Part: HINGE — CORRODED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

LT WING, OUTBOARD FLAP INBOARD HINGE AFT HINGE FITTING AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-87551.

Part: HINGE — CORRODED (ZONE 600) · airframe 44,179 hrs · 10,267 cycles

RT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) FORWARD HINGE. COMPLIED WITH FEDEX EA 1-5750-87546.

Part: SUPPORT FITTING — CRACKED (ZONE 600) · airframe 44,179 hrs · 10,267 cycles

RT WING, WHILE ACCOMPLISHING EA NR 1-5750-87541, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. REMOVED AND REPLACED PER AMM 27-50-30-4. FLAP RIGGING CARRIED OUT PER AMM 27-50-30-5.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 44,179 hrs · 10,267 cycles

NR 2 ENGINE, RT THRUST REVERSER COWL, UPPER SLIDER TRACK END SUSPECTED CRACKED. THRUST REVERSER COWL REMOVED AND REPLACED.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 44,179 hrs · 10,267 cycles

NR 3 ENGINE, LT THRUST REVERSER COWL, FORWARD FRAME UPPER RADIUS SUSPECTED CRACKED. THRUST REVERSER COWL REMOVED AND REPLACED.

Part: SKIN — BULGED (RT WING) · airframe 44,179 hrs · 10,267 cycles

RT WING TRAILING EDGE UPPER SURFACE AT XORS 826.50, OUTBOARD OF NR 5 SPOILER, FOUND BULGING. CORROSION REMOVED PER SRM 51-21-01 VOLUME II.

Part: SPLICE — CRACKED (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, LT LONGERON L-11 SPLICE BETWEEN STA 1641 TO STA 1661, FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-33-01- VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 635 , X= 8 FOUND WORN. REMOVED AND REPLACED PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 625, X= 47 FOUND WORN ACA7399-501. REMOVED AND REPLACED PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,179 hrs · 10,267 cycles

LEFT WING, FUEL TANK UPPER STRINGER END S-10 BETWEEN XORS 799 TO XORS 827. FOUND WITH APPROXIMATELY 10 INCH CRACKED. TRIMMED OUT PER SRM 57-20-00 VOLUME I, FIGURE 10. FABRICATED REPAIR DOUBLER INSTALLED PER SRM 51-33-01 VOLUME II.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 1491, X= 47 FOUND WORN. REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 1199, X= 47 FOUND WORN AEA7579-1. REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SLEEVE — CRACKED (THRUST REVERSER) · airframe 44,179 hrs · 10,267 cycles

NR 1 ENGINE, LT THRUST REVERSER TRANSLATING SLEEVE, UPPER SLIDER TRACK END SUSPECTED CRACKED. LT THRUST REVERSER COWL REMOVED AND REPLACED.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, SEAT TRACK CROWN FROM STA 1059 TO STA 1119 , X= -47 FOUND WORN. SEAT TRACK CUT AND REMOVED PER SRM 51-33-01 VOLUME II. REPAIR PARTS INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, SEAT TRACK BASE AT STA 6 - 10, X= -8 FOUND WITH CORROSION. REMOVED AND TREATED AS PER SRM 51-21-01 VOLUME II.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 799, X= -47 FOUND WORN.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,179 hrs · 10,267 cycles

MAIN DECK, SEAT TRACK CROWN FROM STA 899 TO STA 923, X= 47 FOUND WORN.

Part: LINER — DAMAGED (NR 1 NACELLE) · airframe 42,058 hrs · 9,801 cycles

POST FLIGHT WALK AROUND FOUND SEVERAL AFT LINER SEGMENTS WITH UPPER SKIN GONE AND HONEYCOMB MATERIAL DAMAGED. ALMOST EVERY SEGMENT DAMAGED ON NR 1 ENGINE. NR 3 ENGINE FOUND AFT LINER SEGMENT OUTER SKIN DELAMINATED AND HONEYCOMB MATERIAL DAMAGED ALMOST COMPLETED AROUND THE ENGINE. INSPECTED NR 2 ENGINE, FOUND 6 INCH SECTION OF SEGMENT AT THE 4 O'CLOCK POSITION DAMAGED. TRIPLE ENGINE CHANGE IN PROGRESS.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

CABIN - PREVIOUS FRAME REPAIR AT RIGHT STA 1541 STR 12 - 13 WAS FOUND SECURED WITH RIVETS, INSTEAD OF HI-LOKS. CABIN - PREVIOUS FRAME REPAIR AT RT STA 1541 STR 12 - 13 DOUBLER REMOVED AND REPLACED IAW SRM 53-30-00 FIG 1 VOL I WITH REF TO EA 1-5310-74305, FUSELAGE - MAIN FRAME - TRACKING OF CATEGORY-B REPAIRS ON FRAME.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 39,294 hrs · 9,166 cycles

TAIL TANK, TO ACCOMPLISH E1-5510-7-5000 PT 1. LT NR 36 BARREL NUT HOLE CORROSION REMOVAL, WEB CUTTING REQUIRE FOR ACCESS. HORIZONTAL STABILIZER, TAIL TANK, WEB CUT OUT FOR ACCESS OF LT NR 36 BARREL NUT HOLE. CORROSION REMOVAL AND REPAIR CARRIED OUT AS PER EA 1-5320-74276 (TITLE: FUSELAGE - AUXILLIARY STRUCTURE - ACCESS FROM PANEL FOR 36LR - BARREL NUT MOD).

Part: STRUCTURE — CORRODED (MAIN DECK) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RT STA 1821 TO STA 1831 FLANGE AREA HAS CORROSION IN TWO PLACES. MAIN CARGO DECK RT STA 1821 TO STA 1831 FLANGE AREA, CORRODED AREA CARRIED OUT REPAIR IAW SRM 53-70-00, FIG. 5, VOL.I.

Part: HINGE — MISALIGNED (ZONE 300) · airframe 39,294 hrs · 9,166 cycles

RIGHT HORIZONTAL STABILZER SLOT DOOR 344AB FASTENER HOLES FOUND MISALIGNED. RT HORIZONTAL STAB SLOT DOOR 344AB FASTENER HOLES MISALIGN AREA CARRIED OUT REPAIR IAW EA 1-5510-74301, STABILIZERS - HORIZONTAL STABILIZER - RT NR 1 SLOT DOOR ASSEMBLY REPAIR.

Part: FITTING — WORN (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LT IB FLAP VANE NR 3 TEE FITTING BUSHING BORES DIAMETER FOUND WORN, OUT OF LIMIT. LT INBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA# 1-5750-74292, WINGS - LT AND RT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR.

Part: FITTING — WORN (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT IB FLAP VANE NR 1 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. RH INBD FLAP VANE NR 1 TEE FITTING REPAIRED AS PER EA# 1-5750-74292, WINGS- LEFT AND RIGHT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RT STA 795 SEAT TRACK REF. X = 27.5 SEAT TRACK DAMAGED IN TWO PLACES. MAIN CARGO DECK RT STA 795 SEAT TRACK REF = X =27.5 DAMAGED SEAT TRACK CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1.

Part: FITTING — WORN (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LT IB FLAP VANE NR 1 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. LT INBD FLAP VANE NR 1 TEE FITTING REPAIRED AS PER EA 1-5750-74292, WINGS - LT AND RT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR.

Part: FITTING — WORN (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

SNRM N1201 : RT IB FLAP VANE NR 3 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. RT INBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA 1-5750-74292, WINGS -LT AND RT INBD FLAP VANE -NR 1 & 3 TEE FITTING WEAR REPAIR.

Part: STRAP — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LT IB FLAP OB HINGE (FLAP SIDE), OB PIVOT HOLE FOUND CORRODED AT STRAP FACE. LT INBD FLAP OUTBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE ATTACH O/B STRAP REMOVED AND REPALCED AS PER SRM 51-33-01 VOL II & AMM 20-50-02. FABRICATED NEW STRAP AS PER DWG ARC2518.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RT FLOORBEAM 53.5 INCHES FROM CENTER LINE HAS EVIDENCE OF CORROSION. RT DAMAGED FLOOR SUPPORT STA 1891TO STA 2007, 53.5 INCHES FROM CENTER LINE REMOVED AS PER PER MM 20-50-02. FABRICATED AS PER DWG NR AGA7551. FABRICATED SUPPORT INSTALLED AS PER MM 20-20-02

Part: RIB — CHAFED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

FOUND DEEP CHAFING MARK ON LEFT INBOARD FLAP OUTBOARD VANE TRACK OUTBOARD SUPPORT RIB AT LEADING EDGE AREA. DEEP CHAFING REWORKED AS PER SRM 51-21-01, VOL.II AND EA 1-5750- 74284. WINGS - LEFT INBOARD FLAP VANE SUPPORT - RIB CHAFED ) AT LT INBD FLAP, OUTBD VANE TRACK OUTBD SUPPORT RIB LEADING EDGE AREA.

Part: SKIN — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT WING - UPPER SURFACE, FASTENER (1 EA) POPPED UP AT XORS 230, STA 1413.

Part: TRACK — GOUGED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT INBOARD FLAP CENTER VANE TRACK CUTOUT FOUND GOUGES AT 4 PLACES. COMPLIED WITH FEDEX EA 1-5750-74283, WINGS - LEFT INBOARD FLAP VANE SUPPORT RIB CHAFED.

Part: SKIN — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS STA XOS 510 UNDER REFUEL ACCESS PANEL. LT WING : LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I.

Part: SKIN — CRACKED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT WING LEADING EDGE PANEL INTERIOR SEVERAL CRACKS AT XOS 546 OUTBD OF REFUELING PANEL. RT WING LEADING EDGE XOS 546 INNER DOUBLER. REPAIRED AS PER SRM 57-10-00 FIG 25 V1.

Part: SKIN — CORRODED (ZONE 100) · airframe 39,294 hrs · 9,166 cycles

CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION FROM STA 1235 LT X =13 TO RT X =5. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK STA 1235 LH X = 13 TO RT X = 5. CORRODED AREA CARRIED OUT REPAIR IAW EA 1-5710-74294, WINGS - CENTER WING UPPER PANEL SKIN CORROSION.

Part: SKIN — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT WING - LEADING EDGE PANEL INTERIOR HAS SEVERAL CRACKS AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK. LT WING LEADING EDGE PANEL INTERIOR AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 39,294 hrs · 9,166 cycles

TAIL TANK - RIGHT NR 36 BARREL NUT HOLE, BEARING SURFACE AND BOTTOM SURFACE FOUND CORRODED. REQUIRE CUTTING OF WEB FOR REAMING. HORIZONTAL STABILIZER, TAIL TANK, WEB CUT OUT FOR ACCESS OF RT NR 36 BARREL NUT HOLE. CORROSION REMOVAL AND REPAIR CARRIED OUT AS PER EA 1-5320-74276 (TITLE: FUSELAGE - AUXILLIARY STRUCTURE - ACCESS FROM PANEL FOR 36LR - BARREL NUT MOD)

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 39,294 hrs · 9,166 cycles

CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235 RT X =30. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RT X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PANEL - SKIN CORROSION

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RT STA 1912 FLOORBEAM CORRODED BETWEEN FLOOR SUPPORT AT 53.5 FROM CENTER LINE AND SEAT TRACK 89.5. CORRODED FLOORBEAM SUPPORT BETWEEN FLOOR SUPPORT AT 53.5 FROM CENTER LINE AND SEAT TRACK 89.5 AT MAIN CARGO DECK RT STA 1912 REMOVED AND REPLACED WITH NEW SUPPORT AND INSTALLED AS PER SRM 51-31-01, VOL.II.

Part: SKIN — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT WING LEADING EDGE 2 CRACKS AT RIVETS STA XOS 630 LEADING EDGE PANEL INTERIOR. LT WING LEADING EDGE : STA XOS 630 LEADING EDGE PANEL INTERIOR, 02 EACH CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RIGHT STA 1896 TO STA 2007 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. RT STA 1896 TO STA 2007 FLOOR SUPPORT (01 EACH) REMOVED AND REPLACED IAW SRM 51-31-01 VOL II

Part: SKIN — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT WING LEADING EDGE PANEL INTERIOR MANY CRACKS FROM EOS 560 TO 620 BETWEEN SLAT TRACKS 10 AND 11. LT WING LEADING EDGE SKIN PANEL INTERIOR STA XOS 560 TO XOS 620 BETWEEN SLAT TRACK 10 AND 11, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 39,294 hrs · 9,166 cycles

LEFT CENTER CARGO CHANNEL GUIDE RAIL FOUND WITH CORROSION BETWEEN STA 1541 TO STA 5-113. CORROSION BETWEEN STA 1541 TO STA 5-113 GUIDE RAIL UPPER FLANGE, CORROSION REMOVED. ORIGINAL THICKNESS 0.090. MATERIAL REMAINING 0.082. WITHIN LIMIT PER SRM 53-00-01, FIG.3, VOL.I.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK LT STA 1341 TO STA 1361 SEAT TRACK REF X =75.25 SEAT TRACK HAS SURFACE CORROSION. MAIN CARGO DECK RH STA 1341TO STA 1365 SEAT TRACK REF. X =75.25 SEAT TRACK FLANGE CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 5 V1.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT BORE AREA. LT INBD FLAP OTBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION. REMOVED AND REPAIRED AS PER EA 1-5750-74282, WINGS - LEFT INBD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. RT OUTBD FLAP OUTBD HINGE (WING MOUNTED), OUTBD ACTUATOR LUG HOLE BORE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5740-74286, WINGS - LT & RT OUTBD FLAP OUTBD HINGE BRACKET ASSY CORROSION.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RIGHT STA 1922 TO STA 2007 SEAT TRACK REF X = 20.0, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1922 TO STA 2007 SEAT TRACK REF. X = 20.0, FLOOR SUPPORT 01 EA REMOVED AND REPLACED AS PER MM 20-50-02 (AGA7088-2). SUPPORT AGA7087 FABRICATED AS PER DWG NR AGA7087 ANS INSTALLED AS PER MM 20-50-02.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE CORRODED AT BORE AREA. LT INBD FLAP OTBD HINGE (FLAP SIDE), OUTBD PIVOT HOLE BORE CORROSION. REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74282, WINGS - LT INBD TE FLAP HINGE BRACKET CORRODED.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 39,294 hrs · 9,166 cycles

RT CENTER CARGO CHANNEL GUIDE RAIL FOUND WITH CORROSION BETWEEN STA 1541 TO STA 5-113. GUIDE RAIL UPPER FLANGE BETWEEN STA 1541 TO STA 5-113 CORROSION REMOVED. ORIGINAL THK 0.090 MATERIAL REMAINING 0.078 MIN. WITHIN LIMITS PER SRM 53-00-01 FIG 3 VOL 1

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE. RT OUTBD FLAP OUTBD HINGE (WING MOUNTED), INBD ACTUATOR LUG HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSY CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. RT OTBD FLAP OTBD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, WINGS - LT AND RT OTBD FLAP - OTBD HINGE BRACLET ASSEMBLY CORROSION. AND DWG ARC0503 AND CMM 57-44-08 AND FOUND WITHIN LIMITS.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RIGHT STA 1169 BETWEEN SEAT TRACK REF X = 27.5 AND X = 47.5 STIFFENER CRACKED. MAIN CARGO DECK RT STA 1169 BETWEEN SEAT TRACK REF. X = 27.5 AND X = 47.5 CRACKED STIFFENER REMOVED AS PER SRM 51-31-01, VOL.II. STIFFENER FABRICATED IAW DRAWING NR NPB 6272. FABRICATED STIFFENER PROTECTED AND PAINT TOUCHED UP AS PER SRM 51- 21-01, VOL. II. PART MARKED AS PER GMM 7-0-1001. FABRICATED STIFFENER INSTALLED I.A.W SRM 51-33- 01, VOL.II.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RIGHT STA 1250 TO 1361 SEAT TRACK REF X = 75.25, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1250 TO 1361 SEAT TRACK REF. X = 75.25. CORROSION ON SEAT TRACK REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL. II. MATERIAL THK: 0.080, THK REMAINED: 0.074 WITHIN LIMIT AS PER SRM 53-70-00 VOL. I.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), PIVOT HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1-5740-74285, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

FLOOR SUPPORT CORRODED AT STA 1887 CENTER SECTION X = -8.5 TO 8.5. FLOOR SUPPORT CORRODED AT STA 1887 CENTER SECTION X = -8.5 TO 8.5 P/NO AGA7559-3N REMOVED AND REPLACED IAW MM 20-50-02. AGA7080 SUPPORT FABRICATEF AS PER DWG AGA7080 AND INSTALLED AS PER MM 20-50-02.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RIGHT STA 1169 BETWEEN SEAT TRACK REF X = 47.5 AND X = 75.25 STIFFENER CRACKED. MAIN CARGO DECK RT 1169 BETWEEN SEAT TRACK REF X = 47.5 AND X = 75.25 CRACKED STIFFENER REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED STIFFENER AS PER DWG NR NPB6272. FABRICATED STIFFENER PROTECTED AND PAIN TOUCH UP AS PER SRM 51-21-01 VOL II. PART MARK AS PER GMM 7-0-1001. FABRICATED STIFFENER INSTALLED AS PER SRM 51-33- 01 VOL II.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

MAIN CARGO DECK RIGHT STA 1250 SEAT TRACK REF X = 75.25, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1250 SEAT TRACK REF - X = 75.25 SEAT TRACK CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01, VOL.II. MATERIAL THICKNESS : 0.080 , THICKNESS REMAINED: 0.076, WITHIN LIMIT AS PER SRM 53-70-00, VOL.I. REWORKED AREA PAINT TOUCHED UP AS PER SRM 51-21-01, VOL. II.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT SPOT FACES. LT INBD FLAP OTBD HINGE (FLAP SIDE), INBD PIVOT HOLE SPOT FACES CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74282, WINGS - LT INBD TE FLAP HINGE BRACKET CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT OD FLAP IB HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE. LT OUTBD FLAP OUTBD HINGE (WING MOUNTED), INBD ACTUATOR LUG HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT OB FLAP IB HINGE (WING MOUNTED), LOWER OB ATTACH HOLE (SPAR MOUNTED) CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: FITTING — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT OB FLAP VANE TEE FITTING NR 2 (COUNTING FROM IB) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OUTBD FLAP VANE TEE FITTING NR 2 REPAIRED AS PER FEDEX EA 1575074288, WINGS, LT & RT OUTBD FLAP, NR 2 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

CABIN - SURFACE CORROSION FOUND ON FLOOR SUPPORT AT STA 5-0 (APPROXIMATELY STA 1531) RT X = 8.5. SURFACE CORROSION AT CABIN FLOOR TRACKS STA 5-0 (APPROXIMATELY STA 1531) RT X=8.5 REMOVED AS PER SRM 51-21-01 VOL 2, MATERIAL THICKNESS, 0.080 INCH, THICKNESS REMAINED 0.075" & FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), UPPER INBOARD ATTACH HOLE (SPAR MOUNTED) CORRODED AT BORE. LT OTBD FLAP OTBD HINGE (WING MOUNTED) UPPER INBD ATTACH HOLE (SPAR MOUNTED) BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT OB FLAP IB HINGE (WING MOUNTED), OB ACTUATOR LUG HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. LT OTBD FLAP OTBD HINGE (WING MOUNTED), OTBD ACTUATOR LUG HOLE BORE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5740-74286, WINGS - LT & RT OTBD FLAP, OTBD HINGE BRACKET ASSY CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

CABIN - FLOORBEAM CORRODED AT STA 5/73 RIGHT X = 47.5 TO 75.25. CORRODED FLOOR SUPPORT AT CABIN STA 5/73 RT X = 47.5 TO 75.25 REMOVED AND REPLACED WITH FABRICATED FLOOR SUPPORT AS PER DWG AEA736 AND AS PER SRM 51-35-01 VOL II.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), LOWER INBOARD ATTACH HOLE (SPAR MOUNTED) CORRODED AT SPOT FACES. RT OUTBD FLAP INBD HINGE (WING MOUNTED), LOWER INBD ATTACH HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP, INBD HINGE BRACKET ASSEMBLY CORROSION

Part: FITTING — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP VANE TEE FITTING NR 4 (COUNTING FROM INBOARD) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OTBD FLAP VANE NR 4 TEE FITTING REPAIRED AS PER EA 1-5750-74290, LT AND RT OUTBOARD FLAP - NR 4 FITTING SUPPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD ACTUATOR LUG BORE. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: FITTING — CORRODED (T/E FLAP VANE) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP VANE TEE FITTING NR 5 (COUNTING FROM INBOARD) FOUND CORROSION ON FWD HOLE BORE AREA. LT OTBD FLAP VANE TEE FITTING NR 5 REPAIRED AS PER EA 1-5750-74291, WINGS - LT AND RT OUTBOARD FLAP - NR 5 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. LT OTBD FLAP INBD HINGE (FLAP SIDE), OTBD ACTUATOR LUG SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP VANE TEE FITTING NR 4 (COUNTING FROM INBOARD); FOUND CORROSION ON FWD HOLE BORE AREA. LT OTBD FLAP VANE TEE FITTING NR 4 REPAIRED AS PER EA 1-5750-74290, WINGS - LEFT AND RIGHT OUTBOARD FLAP - NR 4 FITTING SUPPORT VANE TO TRACK CORROSION

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74277, WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HINGE FOUND CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HINGE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED ON SPOT FACES AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES. LT OTBD FLAP INBD HINGE (FLAP SIDE), INBD ACTUATOR LUG SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT ATTACH PIN LOCK PLATE BOLT HOLE FOUND CORRODED ON BORE AND SPOT FACES. RT OTBD FLAP INBD HINGE (FLAP SIDE), PIVOT ATTACH PIN LOCK PLATE BOLT HOLE BORE AND SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD ACTUATOR LUG CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: FITTING — CORRODED (T/E FLAP VANE) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP VANE TEE FITTING NR 5 (COUNTING FROM INBOARD) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OTBD FLAP VANE TEE FITTING NR 5 REPAIRED AS PER EA 1-5750-74291, WINGS - LT AND RT OUTBOARD FLAP - NR 5 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. LT OTBD FLAP INBD HINGE (FLAP SIDE), OUTBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP, UP STOP RIB SUPPORT ISLAND FOUND 01 CRACK APPROX 0.25 INCH LONG AT OUTBOARD SIDE.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: FITTING — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP VANE T-FITTING NR 3 (COUNTING FROM INBOARD); FOUND CORROSION ON FWD HOLE BORE AREA. LT OUTBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA 1-5750-74289, WINGS - LEFT OUTBOARD FLAP - NR 3 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE), OUTBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. LT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: SKIN — CORRODED (CENTER WING) · airframe 39,294 hrs · 9,166 cycles

CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235, RIGHT X = 30. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RH X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PANEL - SKIN CORROSION

Part: HINGE — CORRODED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. RT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: SUPPORT — CRACKED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

RIGHT OUTBOARD FLAP, UP STOP RIB SUPPORT ISLAND FOUND 01 CRACK APPROX 0.25 INCH LONG AT OUTBOARD SIDE. RT OTBD FLAP, UP STOP RIB SUPPORT ISLAND REPAIRED AS PER EA 1-5750-74278, OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE SPOT FACES. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: SPLICE — CRACKED (ZONE 100) · airframe 39,294 hrs · 9,166 cycles

RIGHT CENTER CARGO NR 47 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5- 113 TO STA 1541. CRACKED LONGERON SPLICE AT RT CTR CARGO NR 447, STA 5-113 TO STA 1541, REMOVED AND REPALCED WITH NEW SPLICE AS PER SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 39,294 hrs · 9,166 cycles

RT CENTER CARGO NR 45 LONGERON SPLICE FOUND CRACKED BETWEEN STA 1661 TO 1681. CRACKED NR 45 LONGERON SPLICE AT RT CENTER CARGO BETWEEN STA 1661 TO 1681 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING AFA7113 AND INSTALLED AS PER SRM 51-33-01, VOL.II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 39,294 hrs · 9,166 cycles

LEFT CENTER CARGO NR 49 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5- 113 TO STA 1541. CRACKED NR 49 LONGERON SPLICE AT LT CENTER CARGO BETWEEN STA 5-113 TO STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01, VOL. II.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

CABIN - FLOOR TRACKS CRACKED AT STA 635 RIGHT X=47.5. FLOOR TRACKS CRACKED AT STA 635 RT X=47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I.

Part: HINGE BRACKET — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. LT INBD FLAP OUTBD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II.

Part: HINGE BRACKET — CRACKED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT WING - OUTBOARD FLAP INBOARD HINGE BRACKET (WING SIDE) SIDE LINK CRACKED. OUTBOARD FLAP INBOARD HINGE BRACKET (WING SIDE) SIDE LINK TENSION STRAP SUPPORT REMOVED AND REPLACED AS PER DAC SB57-10.

Part: SPLICE — CRACKED (ZONE 100) · airframe 39,294 hrs · 9,166 cycles

RT CENTER CARGO NR 49 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5-113 TO STA 1541. CRACKED NR 49 LONGERON SPLICE AT RT CENTER CARGO BETWEEN STA 5-113 TO STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING A5A 7114 AND INSTALLED AS PER SRM 51-33-01, VOL. II.

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT WING LEADING EDGE - NR 16 SLAT TRACK INTERNAL STRUCTURE CRACKED AT INBOARD TRACK BRACKET. LT WING LEADING EDGE NR 16 SLAT TRACK INTERNAL STRUCTURE I/B RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II AND EA 1-5750-74279, WINGS - LEFT HAND SLAT - FABRICATION OF RIB FOR NR 16 SLAT TRACK.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

CABIN - FLOOR TRACKS CRACKED AT STA 635 RIGHT X=8.5. CRACKED FLOOR TRACKS AT STA 635 RT X=8.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 VOL. I

Part: HINGE BRACKET — CRACKED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. RT INBD FLAP OUTBD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 V2.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

CABIN - FLOOR TRACKS CRACKED AT STA 5-78 RIGHT X=8.5. FLOOR TRACKS CRACKED AT STA 5-78 RT X=8.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 V1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,294 hrs · 9,166 cycles

CABIN - FLOOR TRACKS CRACKED AT STA 635 LEFT X=47.5. CABIN, CRACKED FLOOR TRACKS AT STA 635 LT X=47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I

Part: SKIN — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS, STA XOS 510 UNDER REFUEL ACCESS PANEL. LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 39,294 hrs · 9,166 cycles

RIGHT WING - NR 16 SLAT TRACK LEADING EDGE INBOARD BRACKET CRACKED. RT WING NR 16 SLAT TRACK LEADING EDGE INBD BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II

Part: VANE — CORRODED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT OUTBOARD FLAP VANE NR 2, 3, 4 AND 5 T-FITTING (COUNTING FROM INBOARD) FOUND FWD HOLE CORRODED AT BORES. LT OUTBOARD FLAP VANE NR 2 TEE FITTING REPAIRED AS PER EA 1-5750-74288, LT & RT OUTBD FLAP - NR 2 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE BRACKET — CRACKED (ZONE 500) · airframe 39,294 hrs · 9,166 cycles

LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FOUND 01 EA BRACKET CRACKED AT OUTBOARD SIDE APPROX 12 INCHES FROM FLAP LOWER SURFACE, 24 INCHES FROM FWD EDGE OF HINGE. LT INBD FLAP OTBD HINGE (FLAP SIDE) OTBD SIDE LOWER AREA 01 BRACKET EDGE CRACK TRIMMED OUT FOUND WITHIN LIMIT AS PER SRM 57-00-01 V1.

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 38,014 hrs · 8,859 cycles

ON TAKEOFF RECEIVED LEVEL 2 "FLAP DISAGREE" ALERT. RIGHT INBOARD FLAP WENT TO 30 DEG., OTHER FLAPS WERE 25 DEG. RAN CHECKLIST AND RETURNED TO RPLB. ACN RELEASED FOR SERVICE PER MEL/CDL: 27-54-01CATEGORY: C EXPIRATION: 05SEP03 "MEL 27-54-01: FLAP POSITION INDICATOR - INOP. VERIFY SYMMETRICAL FLAP MOVEMENT PRIOR TO TAXI FOR EACH B LOCKOUT." (RIGHT INBOARD FLAP). R&R RIB FLAP POSITION TRANSMITTER PER MD 11 MM 27-54.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 34,649 hrs · 8,039 cycles

LT WING OUTBOARD FLAP INBOARD HINGE FITTING LOWER MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BRACKET ASSY PER MM 57-53-01-4.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 34,649 hrs · 8,039 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE FITTING LWR MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BRACKET ASSY PER MM 57-53-01-4.

Part: BRACKET — CORRODED (T/E FLAP) · airframe 34,649 hrs · 8,039 cycles

RT WING OUTBOARD FLAP HINGE FITTING LWR MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BRACKET ASSY PER MM 57-53-01.

Part: BRACKET — CORRODED (T/E FLAP) · airframe 34,649 hrs · 8,039 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING LWR MOUNTING SIDE, FOUND HINGE FITTING & WASHERS CORRODED AFTER SEALANT REMOVAL. R&R BRACKET ASSY PER MM 57-53-01.

Part: ACTUATOR — FAILED (AILERON) · airframe 33,920 hrs · 7,861 cycles

ON TAKEOFF AFTER SLATS RETRACTED LVL 2 AIL DEFLECT DISAGREE ALERT ILLUM'D. REMOVED AND REPLACED LT & RT INBOARD DEFLECT AILERON ACTUATORS PER MM 27-16-01-4. RIGGED, ADJUSTED AND TESTED OK.

Part: CONTROL UNIT — FAILED (ANTI SKID SYS)

LEFT ANTI SKID FAIL ALERT ON SHORT FINAL TO SFS HEAVY RAIN AND WET RUNWAY. EXERCISED GO-AROUND AND DIVERTED TO RPLL. GOT SAME A/S ALERT. RAN RED TAB AND LANDED AT RPLL. REMOVED AND REPLACED A/S CONTROL UNIT PER MM 32-45-01-4 & PERF'D R-T-S TEST PER MM 32-45-01-5, ALL PASSED.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 31,119 hrs · 7,237 cycles

CENTER LG LT BULKHEAD DOUBLER BETWEEN BS 1360 - 1380 FOUND CRACKED. *S/D* REMOVED AND REPLACED DOUBLER PER SRM 51-31-01, 51-21-02 VOL 2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 31,119 hrs · 7,237 cycles

NR 2 SEAT TRACK DAMAGED AT BS 1421 MAIN DECK COMPT. *S/D* SMOOTHED AND FOUND WITHIN LIMITS PER SRM 53-70-00 FIG 3.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 31,119 hrs · 7,237 cycles

DAMAGED NR 3 SEAT TRACK BS 1059 MAIN CARGO COMPT. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 31,119 hrs · 7,237 cycles

CENTER LG RT BULKHEAD DOUBLER BETWEEN BS 1360 - 1380 FOUND CRACKED. *S/D* REMOVED AND REPLACED DOUBLER PER DWG AEA0526.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 31,119 hrs · 7,237 cycles

DAMAGED SEAT TRACK NR 8 BS 1361 TO 1401 8 IN AT MAIN CARGO DECK. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,119 hrs · 7,237 cycles

CABIN CORROSION FOUND ON SEAT TRACK CAVITY AROUND BS 540 & X=-8. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,119 hrs · 7,237 cycles

AFT FX INTERNAL FOUND CREW REST FWD BULKHEAD AT BS 2014.982 WITH FITTING QTY 1 CRACKED AT RBL 20. *S/D* REMOVED AND REPLACED BULKHEAD AND FITTING PER SRM 51-33-01, DWG AJL7140.

Part: FUEL TANK — FLAMED OUT (#2 ENGINE)

01-051 #2 ENG FLAMED OUT ABOUT 1 PLUS 15 MIN OUT OF LAX. #2 TANK WAS FUELED TO KNOW QTY DUE TO INOP FUEL IND THE ENG WAS RESTART WITH FUEL CROSSFEED. FUEL SLIP RECK AND SHOW RELEASE FUEL HOWEVER #2 WAS UNDERFUELED BY 20,000 #. THE FUEL CREW DEBRIEF- #2 TANK RAN DRY CAUSING FLAMEOUT. NO MAINT ACTION REQD INF NOTED. ** S/D ** COMING

Part: WARNING SYSTEM — ACTIVATED (AILERON) · airframe 28,979 hrs · 6,750 cycles

DURING R/O CHECK GOT A DEFLECTED AILERON DISAGREE LEVEL 2 ALERT.

Part: CYLINDER — CORRODED (RT MLG) · airframe 26,413 hrs · 6,192 cycles

RT MLG RETRACT ACTUATOR ROD END, INTERNAL BORE THREADS HAS CORROSION WITH PITTING NOTED. *S/D* REMOVED AND REPLACED PER MM 32-33-20-4. REFER TO WORK CARD 32 X 1701 PG 14 OF 42 FOR INSTALL.

Part: CYLINDER — CORRODED (LT MLG) · airframe 26,473 hrs · 6,192 cycles

LT MAIN GEAR RETRACT CYLINDER, UPON REMOVAL OF ACTUATOR ROD END, FOUND INTERNAL BORE THREADS CORRODED AND PITTED. *S/D* REMOVED AND REPLACED PER MM 32-33-20-4. WORK CARD 32 X 1702 14 OF 42 FOR INSTALL LT MAIN GEAR.

Part: ACCESS DOOR — DAMAGED (R7 WING)

RT WING LEAD EDGE, SLAT DRIVE MECH ACCESS DOOR OPEN DURING AC TEST FLT CAUSING DAMAGE TO THE DOOR, SLAT NR 3 RT AND THE WING LEAD EDGE ADJACENT TO SLAT NR 3. REMOVED AND REPLACED SLAT DRIVE MECH PER MM 20-50-02-2. SKIN REPAIRED PER 57-10-00, RIB REPAIR STA 526.18 PER 57-00-01.

Part: PSEU — MALFUNCTIONED (RT MLG)

AFTER TAKEOFF, RT MLG UNSAFE LIGHT ON BOTH PRIMARY AND SECONDARY GEAR INDICATION. CHECKED DOOR CYLINDER PISTON LENGTH IS WITHIN M/M LIMITS. REMOVED AND REPLACED PROX SWITCH ELECTRONICS UNIT. REMOVED AND REPLACED BOTH PRIMARY AND SECONDARY GEAR UP AND LATCHED PROXIMITY SENSOR. PERFORMED GEAR SWING, A/C OPS CHECKED GOOD FOR BOTH INDICATION. PERFORMED RIG AND ADJUSTMENT PER M/M 32-61-15 RII PERFORMED BY 136485.

Part: FRAME — CRACKED (RT CTR GEAR DOOR)

RT/CENTER GEAR DOOR, 1B FWD CORNER ON INSIDE FRAME CRACKED APPROX 2. VERIFIED CRACK W/EDDY CURRENT, REMOVED DAMAGED SECTION OF DOOR FRAME, INSTALLED NEW SECTION OF FRAME (P/N AW87376-2) PER 53-00-7.

Part: COWL WEB — CRACKED (NR 2 ENGINE)

NR 2 ENG INTERNAL NOSE COWL FWD BULKHEAD WEB AND LOWER CHORD IS CRACKED AT 4 O'CLOCK POS APPROX 1, PANEL 362GR. REMOVED AND REPLACED LOWER CHORD WEB PER SRM 51-00-00 (P/N AJC7564-45).

Part: BLKHD SKIN — DAMAGED (BS 62)

EA 1-5330-24396 SPLICE REPAIRED SKIN AT STA 62 LONGERON 36 TO 48 LT AND RT. PERMANENT REPAIR EA 1-5310-25112 REPAIRED PRESSURE BULKHEAD AT BS 595.