N605FE

Part: FRAME — DAMAGED (ZONE UNK) · airframe 97,942 hrs · 23,902 cycles

DURING REPAIR INSPECTION, REF WRI 53-10/5099, FOUND DAMAGE TO FRAME AT FR. STA. 374L@X= 38. INSTALLED SKIN DOUBLER, TRIPLER AND FILLER REF MD11 SRM 53-00-01-2R. E. A. 1-5330-T0384438 PT1 AND PT2 .FUSELAGE- PLATES & SKINS- SKI AND FRAME REPAIR AT STA 374, X= 38.

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 97,942 hrs · 23,902 cycles

DURING STORM IN DFW , TRUCK CAN PUNCTURED AIRCRAFT . DAMAGE IS 4" LONG BY 2 " WIDE . SEE PICTURES INSTALLED SKIN DOUBLER, TRIPLER AND FILLER REF MD11 SRM 53-00-01-2R. E. A. 1-5330-T0384438 PT1 AND PT2 .FUSELAGE- PLATES & SKINS- SKI AND FRAME REPAIR AT STA 374, X= 38.

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 97,785 hrs · 23,847 cycles

EMERGENCY LIGHTING SYSTEM TEST SHOWING "EMERG BAT 1 LO" MSG ,DURING COCKPIT POST FLT CHECK. RELEASED FOR SERVICE PER MEL 33-50-04. EMERG BAT 1 LOW MSG DURING TEST. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKS SATISFACTORY. OK FOR SERVICE.

Part: RELAY — FAILED (ZONE 100) · airframe 96,443 hrs · 23,529 cycles

BATT DISCHARGING LEVEL 1 CAUTION AT 28000FT DURING CLIMB. CAUTION WENT AWAY AT 2000 ON APPROACH, CAME BACK DURING TAXI IN. EMERGENCY DECLARED. R/R BATTERY CHARGER RELAY R2-24 PER AMM. OPERATIONAL TESTS PASSED.

Part: PLATE — CORRODED (LT WNG SPAR CAP) · airframe 95,379 hrs · 23,299 cycles

LEFT WING LEADING EDGE LOWER SPAR CAP STRAP PLATE FOUND WITH CORROSION AT STATION XOS 473. LEFT HAND WING LEADING EDGE LOWER SPAR CAP STRAP PLATE CORROSION AT STATION XOS 473 REPAIRED AS PER E.A.#: 1-5720-T0379764. TITLE: WING SECONDARY WING STRCT REPAIR FOR LH WING L.E LOWER SURFACE CORRODED DOUBLER P/N: ARB7188-1 BETWEEN XFS 471.450 AND XFS 482.787. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1801) · airframe 95,379 hrs · 23,299 cycles

WHILE OPENING FLOOR PANEL AT STATION 1801, FOUND SEAT TRACK X = 8.5 FOUND WITH CORROSION. CABIN - AT STATION 1801, X = 8.5 CORROSION AT SEAT TRACK EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1771 TO EXISTING SPLICE STATION 1811, X = 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1801) · airframe 95,379 hrs · 23,299 cycles

WHILE OPENING FLOOR PANEL AT STATION 1801, FOUND SEAT TRACK X = - 8.5 FOUND WITH CORROSION. CABIN - AT SEAT TRACK STATION 1801, X = - 8.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1771 TO EXISTING SPLICE STATION 1831, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1139) · airframe 95,379 hrs · 23,299 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1139, X = 8.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1139, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1189 TO EXISTING SPLICE STATION 1129/6-100, X = 8.5 AS PER MD- 11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CORRODED (CENTER CARGO) · airframe 95,379 hrs · 23,299 cycles

LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-120, LONGERON SPLICE 45 RIGHT HAND FOUND WITH CORROSION. CORROSION AT LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-120, LONGERON SPLICE 45 RIGHT HAND REMOVED AND FOUND OUT LIMIT AS PER MD-11 SRM 53-00-00-2R FIGURE 202 REPAIR / GENERAL. LONGERON SPLICE STATION 5-123 45 RIGHT HAND REMOVED AND REPLACED WITH FABRICATED LONGERON SPLICE AS PER MD-11 SRM 51-33-01-0G. LONGERON SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A 7116 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CORRODED (CENTER CARGO) · airframe 95,379 hrs · 23,299 cycles

LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-122, LONGERON SPLICE 46 RIGHT HAND FOUND WITH CORROSION. CORROSION AT LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-122, LONGERON SPLICE 46 RIGHT HAND REMOVED AND FOUND WITHIN LIMIT AS PER MD-11 SRM 53-00-00-2R FIGURE 202 REPAIR / GENERAL. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1481) · airframe 95,379 hrs · 23,299 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1481, X = - 8.5 FOUND WITH CORROSION. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1481, X = - 8.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1451 TO STATION 1531/5-0, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ACCESS PANEL) · airframe 95,379 hrs · 23,299 cycles

CRACK FOUND ON FUEL ACCESS DOOR, FORWARD INBOARD CORNER (CORNER 11). APPROXIMATE LENGTH OF CRACK IS 0.25. RIGHT HAND WING LEADING EDGE REFUELING ACCESS DOOR FORWARD INBOARD CORNER SKIN REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-01-2R FIGURE 201 REPAIR 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVE INSPECTION REQUIRED - INITIAL AT 7,500 CYCLES AND REPETITIVE INSPECTION AT 7,500 CYCLES TO BE CARRIED OUT AS PER MD-11 SRM 57-40-01-2R FIGURE 201 TABLE 204 REPAIR 18.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 95,379 hrs · 23,299 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-90, X = -8.5 FOUND WITH CORROSION. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 6-90, X = - 8.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 6-0/1129 TO STATION 6-100/1129, X = - 8.5 AS PER MD-11 SRM 53-00-52- 2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WNG LE FORMER) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 645 APPROXIMATELY 0.93 INCH. RIGHT HAND WING FIXED LEADING EDGE INTERNAL CRACKED BEADED DOUBLER AT STATION XOS 645 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (BS 755) · airframe 95,379 hrs · 23,299 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X = 47.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 755, X = 47.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 725 TO EXISTING SPLICE STATION 765, X = 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 791 APPROXIMATELY 1.2 INCH. RIGHT HAND WING LEADING EDGE INTERNAL CRACKED BEADED DOUBLER AT STATION XOS 791 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 735) · airframe 95,379 hrs · 23,299 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 735, X = - 8.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 735, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 705 TO STATION 745, X = - 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 95,379 hrs · 23,299 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 635, X = - 47.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 635, X = - 47.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 625 TO STATION 645, X = - 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WNG LE FORMER) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 663 APPROXIMATELY 0.5 INCH RIGHT HAND WING FIXED LEADING EDGE INTERNAL CRACKED BEADED DOUBLER AT STATION XOS 663 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (BS 635) · airframe 95,379 hrs · 23,299 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 635, X = 27.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 635, X = 27.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 625 TO STATION 645, X = 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WNG LE FORMER) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 768 APPROXIMATELY 0.37 INCH. RIGHT HAND WING FIXED LEADING EDGE INTERNAL CRACKED BEADED DOUBLER AT STATION XOS 768 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 735) · airframe 95,379 hrs · 23,299 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 735, X = 27.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 755, X = 27.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 745 TO STATION 765, X = 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 744 APPROXIMATELY 1.1 INCH. RIGHT HAND WING FIXED LEADING EDGE INTERNAL CRACKED BEADED DOUBLER AT STATION XOS 744 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (MAIN DECK CARGO) · airframe 95,379 hrs · 23,299 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X = - 8.5 FOUND WITH CORROSION. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 6-10, X = - 8.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 6-0/1129 TO STATION 6-100/1129, X = - 8.5 AS PER MD-11 SRM 53-00-52- 2R FIGURE 201 REPAIR 1. REFER TO SNRM N00343 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WNG LE FORMER) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK APPROXIMATELY 0.25 INCH AT STATION XOS 688 AS MARKED. RIGHT WING FIXED LEADING EDGE INTERNAL CRACKED BEADED DOUBLER AT XOS 688 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R, FIGURE 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WNG LE FORMER) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT FORMER DOUBLER FOUND CRACK AT STATION XOS 789 APPROXIMATELY 0.75 INCH RIGHT FIXED LEADING EDGE INTERNAL SUPPORT CRACKED FORMER DOUBLER AT STATION XOS 789 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DRAWING ARB 3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT FORMER FOUND CRACK AT STATION XOS 795 APPROXIMATELY 1 INCH RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT CRACKED FORMER AT STATION XOS 795 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2922 REVISION B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 95,379 hrs · 23,299 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT FORMER FOUND CRACK AT STATION XOS 808 APPROXIMATELY 4 INCH. RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT CRACKED FORMER AT STATION XOS 808 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2922 REVISION B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOAT — UNKNOWN (UNKNOWN) · airframe 93,684 hrs · 22,844 cycles

APPROXIMATELY 3 HOURS INTO FLIGHT, FL 340, RECEIVED A LEVEL 2 FUEL QTY/USED CHK. COMPLIED WITH QRH. WHEN SYSTEM WAS SWITCHED TO MANUAL AND THE TAIL TANK WAS ISOLATED, THE TAIL TANK CONTINUED TO DECREASE 400LBS IN 4 MINUTES. SUSPECT THE FUEL LEAK WAS IN OR CONNECTED TO THE TAIL TANK. EMERGENCY CREW SAW A SLOW DRIP FROM THE LEFT SIDE OF THE TAIL. THE FUEL DIFFERENTIAL AT BLOCK IN WAS 14,280LBS. REMOVED, REPLACED AND OPS CHECKED BOTH LH AND RH TAIL TANK FULL FLOAT SWITCHES REF FEDEX MD-11 AMM 28-14-01-4. OPS CHECK GOOD

Part: PUMP — LEAKING (ZONE 600) · airframe 92,191 hrs · 22,468 cycles

4 HOURS INTO FLIGHT HYD 3 ELEV OFF THEN HYD 3 FAIL. CONSULTED MOC AND COMPLIED WITH QRH. SHGN 03MAR23 17:22 KIX U AMM: 29-12-41-2 AMM: 29-11-20-4-1 T/S FOUND HYD LEAK FROM #3 ENG LOWER EDP(RIGHT PUMP) BODY. REMOVED AND REPLACED #3 ENG BOTH UPP & LWR EDP. LEAK & OPS CHECKED NORMAL.

Part: HOSE — LEAKING (NR 2 ENGINE) · airframe 90,779 hrs · 22,147 cycles

ON CLIMB OUT PASSING APPROXI 2500 FT FELT A BRIEF THUMP. APPROX 10 SECS LATER, NR 2 ENG ROLLED BACK TO BELOW IDLE. GOT LVL 2 ENGINE 2 RPM LO ALERT. ENG STILL WINDMILLING AT ABOUT 20% N1. RAN QRH & ATTEMPTED A RESTART, NO SUCCESS. SHUT ENG DOWN DECLARED AN EMERGENCY WITH ATC. RETURNED TO DFW. REPLACED #2 ENG LH FUEL MANIFOLD SUPPLY HOSE PER AMM 73-11-03-4-1, LEAK CHK GOOD. REF WRI 72-00/1669 # 2 ENG BOROSCOPED WITH NO DEFECTS NOTED PER AMM 72-00-07-6-1. PERFORMED #2 ENG STALL INSP IAW AMM 7-00-5-6-1, NO DEFECTS NOTED. PERFORMED #2 ENG MAX POWER ASSURANCE RUN IAW AMM 71-00-00-5-1, ALL PARAMETERS WITHIN LIMITS & NO FUEL LEAKS NOTED. ACFT OK FOR SVC.

Part: NONE — NONE (NONE) · airframe 90,203 hrs · 22,023 cycles

AGING AIRCRAFT - EXISTING DOUBLER REPAIR FOUND AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE NUMBER 10 SLAT TRACK CUTOUT INBOARD SIDE XOS 657. EXISTING DOUBLER REPAIR AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE NUMBER 10 SLAT TRACK CUTOUT INBOARD SIDE XOS 657 EVALUATED AND FOUND REPAIR DOUBLER WITH CHAFE MARK. EA 1-5730-T0326737 A PART 2 TITLE: WINGS - PLATES AND SKINS - REPAIR FOR RH WING FIXED L.E NO 10 SLAT TRACK CUTOUT SKIN CENTER AREA CRACK AT XOS 657 ACCOMPLISHED. E.O 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 90,203 hrs · 22,023 cycles

AT THE TIME OF AGING AIRCRAFT INSPECTION ON N605FE, CENTER CARGO CUTOUT , FORWARD JAMS LOWER (INTERNAL) STATION 1671 RIGHT HAND BETWEEN LONGERON 46-48 FOUND A REPAIR DOUBLER THAT WAS NOT DOCUMENTED, AND EVALUATION AS REQUIRED BY EO # E1-5100-7-5001 PART 1. EXISTING REPAIR AT STATION 1671 RIGHT HAND BETWEEN LONGERON 46-48 CENTER CARGO CUTOUT FORWARD JAMB EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00- 04-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 90,203 hrs · 22,023 cycles

AT THE TIME OF AGING AIRCRAFT INSPECTION ON N605FE, CENTER CARGO CUTOUT , AFT JAMS LOWER (INTERNAL) STATION 1781 RIGHT HAND BETWEEN LONGERON 46-48 FOUND A REPAIR DOUBLER THAT WAS NOT DOCUMENTED, AND EVALUATION AS REQUIRED BY EO # E1- 5100-7-5001 PT1. EXISTING REPAIR AT STATION 1781 RIGHT HAND BETWEEN LONGERON 46-48 CENTER CARGO CUTOUT AFT JAMB EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-04-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 90,203 hrs · 22,023 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 745 TO STATION 765 X = -8.5. EXISTING SEAT TRACK REPAIR AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 745 TO STATION 765 X = -8.5 EVALUATED AND FOUND SEAT TRACK FLANGE CRACK AT STATION 755 AND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101 . SEAT TRACK REPAIR CARRIED OUT AT STATION 745 TO STATION 765 X = -8.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201 . EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CRACKED (ZONE 200) · airframe 90,203 hrs · 22,023 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 745 TO STATION 830 X = -47.5. EXISTING SEAT TRACK REPAIR AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 745 TO STATION 830 X = -47.5 EVALUATED AND FOUND SEAT TRACK FLANGE CRACK AT STATION 787 AND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101. SEAT TRACK REPAIR CARRIED OUT AT STATION 745 TO STATION 830 X = -47.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD -11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED . REPAIR CLASSIFID AS MAJOR PER GMM 6-2- 100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 90,203 hrs · 22,023 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 645 TO STATION 745 X = -27.5. EXISTING SEAT TRACK REPAIR AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 645 TO STATION 745 X = -27.5 EVALUATED AND FOUND SEAT TRACK FLANGE CRACK AT STATION 695 AND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101. SEAT TRACK REPAIR CARRIED OUT AT STATION 645 TO STATION 745 X = -27.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201 . EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SKIN — CRACKED (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

RIGHT HAND #1 SLAT LOWER SURFACE SKIN FOUND CRACKS AT AROUND XIS 247. RIGHT HAND #1 SLAT LOWER SURFACE SKIN AROUND XIS 247 CRACKED AREA REPAIR CARRIED OUT AS PER EA # 1-5750-T0368776 PART 1 TITLE: WINGS Ï¿½ FLIGHT SURFACE Ï¿½ RH WING - #1 SLAT INNER SKIN SPLICE REPAIR AT STA XIS 199.447 Ï¿½ SRM 57-40-01 REPAIR 3 Ï¿½ RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

RIGHT HAND WING #6 SLAT INTERNAL RIB XOS 868.476 FOUND CRACKS DURING SLAT SKIN REMOVAL FOR WORK ACCESS. RIGHT HAND WING #6 SLAT INTERNAL XOS 868.476 CRACKED RIB REPAIR CARRIED OUT AS PER E.A. # 1-5750-T0368508 P1 TITLE: WINGS Ï¿½ FLIGHT SURFACES Ï¿½ RH WING SLAT NO. 6 Ï¿½ RIBS REPLACEMENT AT XOS 858 & XOS 868 Ï¿½ RSC TRACKING REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — NONE (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

EXISTING REPAIR FOUND AT RIGHT HAND WING STRINGER END 9 (UPPER) XORS 819. EXISTING REPAIR AT RIGHT HAND WING STRINGER END 9 (UPPER) XORS 819 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R REPAIR 3 FIGURE 201 . WING STRINGER END 9 CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 57-00-03-2R REPAIR 3 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 T REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (ZONE 500) · airframe 90,203 hrs · 22,023 cycles

EXISTING REPAIR FOUND AT LEFT HAND WING STRINGER END 9 (UPPER) XORS 819. EXISTING REPAIR AT LEFT HAND WING STRINGER END 9 (UPPER) XORS 819 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R REPAIR 3 FIGURE 201. WING STRINGER END 9 CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 57-00-03-2R REPAIR 3 FIGURE 201. EO 1-5100-7-5001 B7 PART1. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (CARGO) · airframe 90,203 hrs · 22,023 cycles

LOWER CENTER CARGO COMPARTMENT BILGE AREA BETWEEN STATION 5 - 113 TO STATION 1541 LEFT HAND LONGERON LEFT 49 FOUND CORROSION.

Part: RIB — CRACKED (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

RIGHT WING - NUMBER 6 LEADING EDGE SLAT INNER RIB FOUND CRACK AT STATION XOS 858.175. RIGHT HAND WING - NUMBER 6 LEADING EDGE SLAT INNER RIB AT STATION XOS 858.175 REPAIR CARRIED OUT AS PER E.A. # 1-5750-T0368508 P1 TITLE: WINGS Ï¿½ FLIGHT SURFACES Ï¿½ RH WING SLAT NO. 6 Ï¿½ RIBS REPLACEMENT AT XOS 858 & XOS 868 Ï¿½ RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (ZONE 800) · airframe 90,203 hrs · 22,023 cycles

CABIN - L3 DOOR #5 BEAM FROM UPPER FOUND WITH CRACK. REAMED AND REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — NONE (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

EXISTING REPAIR FOUND AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE DOUBLER XOS 906. EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE DOUBLER XOS 906 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-03-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (800) · airframe 90,203 hrs · 22,023 cycles

CABIN - L3 DOOR #1 BEAM FROM UPPER FOUND WITH CRACK. CABIN - AT L3 DOOR , CRACKED #1 BEAM REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BEAM — CRACKED (ZONE 800) · airframe 90,203 hrs · 22,023 cycles

CABIN - R3 DOOR #1 BEAM FROM UPPER FOUND WITH CRACK. REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — UNKNOWN (ZONE 500) · airframe 90,203 hrs · 22,023 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON LEFT HAND WING FIXED LEADING EDGE LOWER SURFACE NUMBER 14 SLAT TRACK CUTOUT AT STATION XOS 889. EXISTING REPAIR DOUBLER ON LEFT HAND WING FIXED LEADING EDGE LOWER SURFACE NUMBER 14 SLAT TRACK CUTOUT AT STATION XOS 889 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-02-2R REPAIR 7 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE :STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 90,203 hrs · 22,023 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS = 789 RIB DOUBLER FOUND CRACKS. DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. DOUBLER FABRICATED AS PER DRAWING ARB 3954 RIVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

RIGHT HAND FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT XOS 683. 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 (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

RIGHT HAND FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT XOS 703. 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 (200) · airframe 90,203 hrs · 22,023 cycles

CABIN - R3 DOOR CUT OUT AFT JAMB BETWEEN STATION 1305.25 AND STATION 1315.42 UPPER EDGE SKIN FOUND WITH CRACK. CABIN - R3 DOOR CUTOUT AFT JAMB BETWEEN STATION 1305.25 AND STATION 1315.42 , CRACKED UPPER EDGE SKIN REPAIRED AS PER E.A.#: 1-5310-T0368568 P1. TITLE: FUSELAGE - MAINFRAME - R3 DOOR CUTOUT INNER AFT JAMB - CRACK ON INNER SKIN. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

RIGHT HAND FIXED LEADING EDGE COMPARTMENT XOS = 667 UPPER STRINGER FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT XOS = 667 UPPER STRINGER CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 100) · airframe 90,203 hrs · 22,023 cycles

UPPER CENTER AUXILIARY TANK - STRINGER 52 RIGHT HAND XCW = - 46.5 FOUND CRACKS. UPPER CENTER AUXILIARY TANK - STRINGER 52 RIGHT HAND XCW = - 46.5 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — NONE (ZONE 600) · airframe 90,203 hrs · 22,023 cycles

EXISTING REPAIR FOUND ON RIGHT HAND WING UPPER SURFACE MAIN LANDING GEAR SUPPORT DOUBLER BETWEEN AUXILIARY SPAR AND YW 467. EXISTING REPAIR ON RIGHT HAND WING UPPER SURFACE MAIN LANDING GEAR SUPPORT DOUBLER BETWEEN AUXILIARY SPAR AND YW 467 EVALUATED AND FOUND CORROSION EXIST. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101. REPAIR CARRIED OUT AS PER DRAWING SG 11570014 AND EA 1-5730-T0368835 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 100) · airframe 90,203 hrs · 22,023 cycles

UPPER CENTER AUXILIARY TANK - STRINGER 47 LEFT HAND XCW = 46.5 FOUND CRACKS. UPPER CENTER AUXILIARY TANK - STRINGER 47 LEFT HAND XCW = 46.5 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (600) · airframe 90,203 hrs · 22,023 cycles

RIGHT WING FIXED LEADING EDGE XOS = 542 STIFFENER FOUND CRACKS. STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB 2918 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 100) · airframe 90,203 hrs · 22,023 cycles

UPPER CENTER AUXILIARY TANK - STRINGER 47 RIGHT HAND XCW = - 17 FOUND CRACKS. UPPER CENTER AUXILIARY TANK - STRINGER 47 RIGHT HAND XCW = - 17 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (N/A) · airframe 90,203 hrs · 22,023 cycles

LEFT HAND - UPPER WING MAIN LANDING GEAR SUPPORT DOUBLER SURFACE FOUND CORROSION.

Part: STRINGER CLIP — CRACKED (ZONE 500) · airframe 90,203 hrs · 22,023 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS=667 UPPER STRINGER FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS = 667 UPPER STRINGER CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CAP — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,203 hrs · 22,023 cycles

LEFT WING - TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT STATION XORS 1051. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-00-10-1A ALLOWABLE DAMAGE 1 FIGURE 101. LEFT WING TRAILING EDGE REAR SPAR LOWER CAP AT STATION XORS 1051 REPAIR CARRIED OUT AS PER EA # 1-5710-T0368526 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 90,203 hrs · 22,023 cycles

CABIN - STATION 1199 X = - 8.5 SEAT TRACK CROWN FOUND WITH CRACK. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO EXISTING SPLICE STATION 1189 , X = - 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (ZONE 500) · airframe 90,203 hrs · 22,023 cycles

LEFT WING FIXED LEADING EDGE XOS = 542 STIFFENER FOUND CRACKS . CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB 2918 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (100) · airframe 90,203 hrs · 22,023 cycles

LOWER CENTER COMPARTMENT DOORWAY STATION 1741 X = 2 TO - 2 FLOOR BEAM CRACKS. REPAIR CARRIED OUT AT LOWER CENTER CARGO COMPARTMENT DOORWAY STATION 1741 X = 2 TO - 2 FLOOR BEAM AS PER EA. #: 1-5321-T0368469 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (N/A) · airframe 90,203 hrs · 22,023 cycles

CABIN - STATION 1199 X = - 47.5 SEAT TRACK CROWN FOUND WITH CRACK. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1209 TO STATION 1249 , X = - 47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 90,203 hrs · 22,023 cycles

CABIN - STATION 1199 X = 47.5 SEAT TRACK CROWN FOUND WITH CRACK. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1169 TO STATION 1229 , X = 47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — PUNCTURED (ZONE 100) · airframe 90,203 hrs · 22,023 cycles

LOWER CENTER CARGO COMPARTMENT STATION 1841 LEFT HAND SIDE WEB FOUND PUNCTURED. DAMAGED WEB AT LOWER CENTER CARGO COMPARTMENT STATION 1841 LEFT HAND SIDE REMOVED AS PER SRM 51-31-01-OG. WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REVISION R AND INSTALLED AS PER SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CRACKED (ZONE 300) · airframe 90,203 hrs · 22,023 cycles

VERTICAL STABILIZER RIGHT HAND ACCESS PANEL 364QR CUTOUT DOUBLER ASSEMBLY FOUND CRACK AT APPROXIMATELY STATION Y 2164 CRACKED FRAME DOUBLER AT VERTICAL STABILIZER APPROXIMATELY STATION Y 2164 RIGHT HAND ACCESS PANEL 364QR CUT OUT REMOVED AND REPLACED PER MD-11 SRM 51- 31-01-OG. FRAME DOUBLER FABRICATED BY MACHINING PER DOUGLAS DRAWING AJC7593 REVISION Y. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BATTERY PACK — INOPERATIVE (SLIDE PRESS LIGH) · airframe 85,456 hrs · 20,724 cycles

DOOR 1R SLIDE PRESSURE LIGHT INOP. REMOVED AND REPLACED BATTERIES PER 25-61-04-5 AMM OPS CHECK GOOD A/C OK FOR SERVICE

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 85,360 hrs · 20,708 cycles

EMPENNAGE, HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION FOUND ADDITIONAL FASTENER HOLES NR 4 & 6 CRACKED AT NR 4 BANJO FITTING RIGHT HAND AFT FLANGE AREA STATION 2164 & ONE FASTENER HOLE OVER-COUNTERSUNKED, UNABLE TO INSTALL HLT335-8-14 AS PER SRM 55-30-02-2R FIGURE 202 REPAIR 5. TWO EACH FASTENER HOLES CRACK DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT NR 4 BANJO FITTING RT HAND SIDE AFT FLANGE 4TH AND 6TH HOLE AND 01 EACH OVERCOUNTERSUNKED FASTENER HOLE AT RT HAND SIDE AFT FLANGE AT STATION 2164 REPAIRED PER EA 1-5530-T0341085 A P3 TITLE STABILIZERS - VERTICAL STAB - CRACK REPAIR ON VERTICALSTABILIZER REAR SPAR RT FWD FLANGE. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (200) · airframe 85,360 hrs · 20,708 cycles

CABIN AFT FLOOR SUPPORT AT STATION 1887 X = - 56 FOUND CRACK . CABIN - CRACKED AFT FLOOR SUPPORT AT STATION 1887 , X = - 56 REMOVED AND REPLACED AS PER SRM 51-31-01-0G FROM STATION 1887 TO STATION 2007 X = - 56 . AFT FLOOR SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA 7551 REVISION G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK STATION 1927 TO 1947 LEFT HAND X = 56 FLOOR PANEL SUPPORT FOUND CORRODED. MAIN DECK AT FLOOR PANEL SUPPORT STATION 1927 TO STATION 1947 X = 56, CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIG 206 ALLOWABLE DAMAGE. CORRODED FLOOR SUPPORT AT STATION 1887 TO STATION 2007 X = 56 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA 7551 REVISION G. REFER TO SNRM N00807 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK STATION 1887 LEFT HAND X = 25 FLOOR PANEL SUPPORT FOUND CORRODED. MAIN DECK AT FLOOR PANEL SUPPORT STATION 1887 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 PANEL SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA7087 REVISION M. REFER TO SNRM N00811 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK STATION 1929 TO 1947 LEFT HAND X = 25 FLOOR PANEL SUPPORT FOUND CORRODED. MAIN DECK AT FLOOR PANEL SUPPORT STATION 1929 TO STATION 1947 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 DRAWING AGA 7087 REVISION M. REFER TO SNRM N00811 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK STATION BETWEEN 1721 TO 1741 RIGHT HAND X = - 75.25 SEAT TRACK FLANGE FOUND CORRODED. 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 1711 TO EXISTING SPLICE STATION 1751 X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 85,360 hrs · 20,708 cycles

LOWER CENTER CARGO COMPARTMENT RIGHT HAND TUNNEL LONGERON 34 RIGHT SPLICE FITTING FOUND CRACK BETWEEN STATION 5-113 - 1541. LOWER CENTER CARGO COMPARTMENT RIGHT HAND TUNNEL LONGERON 34 RIGHT CRACKED SPLICE FITTING BETWEEN STATION 5-113 TO STATION 1541 REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER MD-11 , SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING : A5A 7112 , REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 85,360 hrs · 20,708 cycles

LOWER CENTER CARGO COMPARTMENT RIGHT HAND TUNNEL LONGERON 38 RIGHT SPLICE FITTING FOUND CRACK BETWEEN STATION 5-113 - 1541. LOWER CENTER CARGO COMPARTMENT RIGHT HAND TUNNEL LONGERON 35 RIGHT CRACKED SPLICE FITTING BETWEEN STATION 5-113 TO STATION 1541 REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER MD-11 , SRM 51-33-01-0G . SPLICE FABRICATED AS PER DOUGLAS DRAWING : A5A7114 , REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 85,360 hrs · 20,708 cycles

LOWER CENTER CARGO COMPARTMENT RIGHT HAND TUNNEL LONGERON 35 RIGHT SPLICE FITTING FOUND CRACK BETWEEN STATION 5-113 - 1541. CRACKED SPLICE FITTING BETWEEN STATION 5-113 TO STATION 1541 REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DRAWING A5A7114, REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK STATION 1858 LEFT HAND X = 75.25 SEAT TRACK FLANGE FOUND CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK STATION 5-73 TO 5-93 LEFT HAND X = 27.5 SEAT TRACK FLANGE FOUND CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 85,360 hrs · 20,708 cycles

CABIN, UPON OPENING OF FLOOR PANEL FOR ACCESS FOUND SEAT TRACK FLANGE CORROSION AT STATION 1781, X = - 75.25. CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED AS PER EA 1-5310-T0354976 P1. TITLE FUSELAGE - MAINFRAME - CORROSION FOUND ON CURVE SEAT TRACK BETWEEN STA 1761 AND STA 1887, AT X = - 75.25 - SRM SPLICE REPAIR - ALTERNATE MATERIAL FOR SEAT TRACK REPLACEMENT SECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK BETWEEN STATION 1561 TO 1601 LEFT HAND X = 75.25 SEAT TRACK FLANGE FOUND CORRODED. 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 AT EXISTING SPLICES STATION 5-123/1531 TO STATION 1651 X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK STATION 5-73 TO 5-93 LEFT HAND X = 27.5 SEAT TRACK FLANGE FOUND CORRODED . MAIN DECK STATION 5-73 TO STATION 5-93 , X = 27.5 AT SEAT TRACK FLANGE CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-0-52-1A FIGURE 101 ALLOWABLE DAMAGE1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-63 TO EXISTING SPLICE STATION 5-123/1531 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 85,360 hrs · 20,708 cycles

LOWER CENTER CARGO COMPARTMENT RIGHT HAND TUNNEL LONGERON 34 RIGHT SPLICE FITTING FOUND CRACK BETWEEN STATION 5-113 - 1541.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

CABIN, UPON REMOVAL OF FLOOR PANEL FOR ACCESS FOUND SEAT TRACK FLANGE CORROSION AT STATION 1601 X = 75.25. 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 AT EXISTING SPLICES STATION 5-123/1531 TO STATION 1651 X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N01007 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK STATION 1561 TO 1641 RIGHT HAND X = - 107.25 SEAT TRACK FLANGE FOUND CORRODED. 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 1671 TO EXISTING SPLICE STATION 1531/5-123 X = -107.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (BS 1915) · airframe 85,360 hrs · 20,708 cycles

CABIN UPON REMOVAL OF FLOOR PANEL FOR ACCESS FOUND FLOOR SUPPORT EDGE CRACKED AT STATION 1915, X = 22. REMOVED AND REPLACED FROM STATION 1914 TO STATION 2007 X = 22 AS PER SRM 51-31-01-0G . FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7088 REVISION B . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

CABIN, UPON REMOVAL OF FLOOR PANEL FOR ACCESS FOUND FLOOR SUPPORT CORROSION AT STATION 1887 - STATION 2007, X = - 25. CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE. CORRODED FLOOR SUPPORT AT STATION 1887 TO STATION 2007 X = - 25 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA 7087 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK LEFT HAND STATION 1967 TO 1987 X = 56 FLOOR PANEL SUPPORT FOUND CORRODED. CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE. CORRODED FLOOR SUPPORT AT STATION 1887 TO STATION 2007 X = 56 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA 7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,360 hrs · 20,708 cycles

MAIN DECK LEFT HAND STATION 1987 TO STATION 2007 X = 25 FLOOR PANEL SUPPORT FOUND CORRODED. CORROSION 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 DRAWING AGA 7087 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 85,360 hrs · 20,708 cycles

02 EACH CRACKS INDICATION APPROXIMATELY 1 INCH AND 0.5 INCH IN LEGTH FOUND DURING X-RAY INSPECTION AT STATION Y = 6-100, LONGERON 7 LEFT CENTER SPLICE SECTION. CRACKED LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-31-01-0G. LONGERON SPLICE FABRICATED BY MACHINING AS PER DRAWING A6A 7112 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,360 hrs · 20,708 cycles

CABIN SEAT TRACK CROWN AREA FOUND DAMAGED AT RIGHT HAND STATION 1159, X = - 47.5. DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1129 TO STATION1209 X = - 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1239) · airframe 85,360 hrs · 20,708 cycles

CABIN - SEAT TRACK CROWN AREA DAMAGED AT STATION 1239 , X = 47.5 . CABIN - AT SEAT TRACK STATION 1239 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO EXISTING SPLICE STATION 1351 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REFER TO SNRM N00631 FOR WORK DETAILS . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,360 hrs · 20,708 cycles

CABIN SEAT TRACK CROWN AREA FOUND DAMAGED AT RIGHT HAND STATION 1169, X = - 8.5.

Part: SEAT TRACK — DAMAGED (BS 1169) · airframe 85,360 hrs · 20,708 cycles

CABIN - SEAT TRACK CROWN AREA FOUND DAMAGED AT RIGHT HAND STATION 1169 , X = - 8.5 . CABIN AT SEAT TRACK STATION 1169 X = - 8.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1189 TO EXISTING SPLICE STATION1129 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,360 hrs · 20,708 cycles

CABIN SEAT TRACK CROWN AREA DAMAGED AT STATION 1239, X = 47.5.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 85,360 hrs · 20,708 cycles

CABIN FLOOR PANEL 291CF TOP SUFACE DAMAGED AT LEFT HAND STATION 1887 - 1909. DAMAGED FLOOR PANEL REMOVED AS PER AMM 53-21-04. FLOOR PANEL 291CF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 85,360 hrs · 20,708 cycles

CABIN FLOOR PANEL 292EF TOP SURFACE DAMAGED AT RIGHT HAND STATION 1909 - 2007. DAMAGED FLOOR PANEL REMOVED AS PER AMM 53-21-04. FLOOR PANEL 292EF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 85,360 hrs · 20,708 cycles

CABIN FLOOR PANEL 292CF TOP SURFACE DAMAGED AT RIGHT HAND STATION 1887 - 1909. DAMAGED FLOOR PANEL REMOVED AS PER AMM 53-21-04. FLOOR PANEL 292CF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 85,360 hrs · 20,708 cycles

CABIN FLOOR PANEL 293EF TOP SURFACE DAMAGED AT LEFT HAND STATION 1909 - STATION 2007. DAMAGED FLOOR PANEL REMOVED AS PER AMM 53-21-04. FLOOR PANEL 293EF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 85,360 hrs · 20,708 cycles

CABIN FLOOR PANEL 291FF TOP SURFACE DAMAGED AT LEFT HAND STATION 1853 - 1887. DAMAGED FLOOR PANEL REMOVED AS PER AMM 53-21-04. FLOOR PANEL 291FF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 29IFF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CHAFED (BS 1009) · airframe 85,360 hrs · 20,708 cycles

FORWARD CARGO COMPARTMENT DOOR CUTOUT STATION 1009 LONGERON 40 RIGHT HAND TO LONGERON 41 RIGHT HAND FOUND CHAFFING. FORWARD CARGO COMPARTMENT DOOR CUTOUT REPAIR CARRIED OUT AT STATION 1009 LONGERON 40 RIGHT HAND TO 41 RIGHT HAND AS PER MD-11 SRM 53-00-15-2R , FIGURE 202 REPAIR 8. INITIAL INSPECTION TO BE CARRIED OUT AT 4000 FLIGHT CYCLES AND REPETITIVE INSPECTION EVERY 4000 FLIGHT CYCLES AS PER SRM 53-00-15-2R FIGURE 202 REPAIR 8 TABLE 201 REQUIREMENTS. METHOD BY EXTERNAL VISUAL INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (FUSELAGE) · airframe 85,360 hrs · 20,708 cycles

FORWARD CARGO COMPARTMENT DOOR CUTOUT STATION 1009 LONGERON 40 RIGHT HAND TO LONGERON 41 RIGHT HAND FOUND CHAFING.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 85,360 hrs · 20,708 cycles

CABIN SEAT TRACK CROWN AREA FOUND DAMAGED AT RIGHT HAND STATION 1421, X = - 8.5. DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1391 TO STATION 1451 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 85,360 hrs · 20,708 cycles

ULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER NR 4 BANJO FITTING RIGHT HAND SIDE FORWARD FLANGE. REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATE STATION Y = 2164. CRACK ON LOWER VERTICAL STABILIZER NR 4 BANJO FITTING RIGHT HAND SIDE FORWARD FLANGE REPAIR AREA AT STATION 2164 REPAIRED AS PER ENGINEERING AUTHORIZATION 1-5530-T0341085 A P3 TITLE : STABILIZERS - VERTICAL STABILIZER - VERTICAL STABILIZER - CRACK REPAIR ON VERTICAL STABILIZER REAR SPAR RT FWD FLANGE. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — PUNCTURED (LE SLAT) · airframe 85,360 hrs · 20,708 cycles

LEFT HAND WING NR 8 SLAT INBOARD EDGE FOUND INNER SKIN PUNCTURED AT STATION XOS 1007.5. REPAIR CARRIED OUT AS PER SRM 54-40-01-2R FIGURE 201 REPAIR 3 AND ENGINEERING AUTHORIZATION # 1-5750-T0354766 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 85,360 hrs · 20,708 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAP STATION 2164 AND FOUND CRACK INDICATION. FOUND THE BANJO FITTING CRACKED APPROXIMATE 1/4" TRIMMED AS PER SRM 55-30-02- 2R FIGURE 201 REPAIR 5 AND REPAIR CARRIED OUT ON LEFT HAND # 4 BANJO FITTING AS PER SRM 55-30-02-2R FIGURE 202 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 5400 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2700 FLIGHT CYCLES AS PER SRM 55-30-02-2R TABLE 203 REPAIR 5 FIGURE 202 REQUIREMENTS.

Part: SEAT TRACK — DAMAGED (BS 1289) · airframe 85,360 hrs · 20,708 cycles

CABIN - SEAT TRACK CROWN AREA FOUND DAMAGED AT LEFT HAND STATION 1289 , X = 47.5. DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO EXISTING SPLICE STATION 1351 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (BS 1421) · airframe 85,360 hrs · 20,708 cycles

CABIN - SEAT TRACK CROWN AREA FOUND DAMAGED AT RIGHT HAND STATION 1421 , X = - 27.5 . DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1411 TO STATION 1451 X = - 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (BS 1421) · airframe 85,360 hrs · 20,708 cycles

CABIN - SEAT TRACK CROWN AREA FOUND DAMAGED AT RIGHT HAND STATION 1421 , X = - 47.5 . DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1451 TO EXISTING SPLICE STATION 1411 X = - 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR I . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 85,360 hrs · 20,708 cycles

CABIN FLOOR PANEL 263EF TOP SURFACE DAMAGED AT CENTER STATION 1321 - 1361. DAMAGED FLOOR PANEL 263EF REMOVED AS PER AMM 53-21-04. FLOOR PANEL 263EF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 85,360 hrs · 20,708 cycles

CABIN FLOOR PANEL 232EF FOUND DAMAGED AT RH BS 495- 595.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 85,360 hrs · 20,708 cycles

CABIN - FLOOR PANEL #232EF TOP SURFACE FOUND DAMAGED AT RIGHT HAND STATION 495 - STATION 595 AND BETWEEN X= -75.5 TO X= -107.5 DAMAGED FLOOR PANEL #232EF AT CABIN RIGHT HAND STATION 495 - STATION 595 AND BETWEEN X= -75.5 TO X= -107.5 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #232 EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL #232 EF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING LE) · airframe 85,360 hrs · 20,708 cycles

LEFT HAND WING LEADING EDGE CAVITY FORMER AT STATION XOS = 733 FOUND CRACK. CRACKED FORMER REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW FORMER IAW DRAWING ARB2923, REVISION D. INSTALLED THE NEW FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 85,360 hrs · 20,708 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 624 FOUND CRACK. LEFT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 624 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 85,360 hrs · 20,708 cycles

RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 766 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 85,360 hrs · 20,708 cycles

RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 878 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 85,360 hrs · 20,708 cycles

RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 751 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 85,360 hrs · 20,708 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING, STATION Y = 595 AND FOUND 01 EACH CRACK PROPAGATE FROM THE SLOT OUT AREA APPROXIMATE 1/4 INCHES LENGTH. 01 EACH PROPAGATED CRACK FROM THE SLOT OUT AREA AT LEFT HAND NOSE LANDING GEAR TRUNNION FITTING STATION Y = 595 REPAIRED AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT EVERY 1500 FLIGHT CYCLES PER SRM 53-10-14-2R TABLE 201 FIGURE 202 REPAIR 2 REQUIREMENTS. METHOD BY HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 85,360 hrs · 20,708 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING, STATION Y = 595 AND FOUND 01 EACH CRACK PROPAGATE FROM THE SLOT OUT AREA APPROXIMATE 1/4 INCHES LENGTH.

Part: WIRE — BROKEN (CABIN) · airframe 84,480 hrs · 20,509 cycles

L1 DOOR EXIT SIGN INOP IN EMERGENGY LIGHT SYSTEM TEST. REF WDM 33-52-01 REPAIRED BROKEN WIRE TERMINALS AT LEFT FWD DOOR EXIT SIGN L2-721 7,8 PER SWPM. REINSTALLED PANEL REF M/M 25-23-23-4. EMERGENCY LIGHTING TESTS NORMAL PER M/M 33-50-00-5. OK FOR SERVICE.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 83,744 hrs · 20,239 cycles

MDIS 605 52-10 8462 31OCT19 MEM OPEN U L1 DOOR SLIDE DEPLOYED UPON OPENING MEL 31OCT19 08:07 MEM U RELEASED FOR SERVICE PER MEL : 52-10-03-03 CATEGORY : C EXPIRATION : 10NOV19 "MEL 52-10-03-03: L1 CABIN ENTRY SLIDE - INOP EXTENDED OVERWATER OPS REQUIRES TWO SLIDE/RAFTS AND/OR PORTABLE RAFTS." SLIDE WAS DEPLOYED. DEFLATED AND REMOVED TO MAIN CARGO FLOOR BEHIND 9 G NET. A/C OK TO CONTINUE C/7205893 REMOVED AND REPLACED L1 DOOR SLIDE AND CONTAINER REF MD-11 AMM 25-61-01-4.

Part: VALVE — FAULTY (L1 DOOR) · airframe 83,670 hrs · 20,207 cycles

1L DOOR BOTTLE ACCUMULATOR PRESSURE LOW AND OUT OF GREEN. REMOVED AND REPLACED RECHARGE VALVE FOR PRECAUTION WITH NEW ONE AND SERVICED ACCUMULATOR AND CYLINDER PRESSURE SHOWS IN THE MIDDLE OF GREEN AREA ON THE PRESSURE INDICATOR ON Z TIME 1900 FOUND NO LEAK REF AMM CHAP 52-11-04-04, CHAP 12-25-04. AS A PRECAUTION, SUGGEST LEAVE THIS WRI IN WORK TO MONITOR ANY POSSIBLE LEAK NEXT 8 HRS. RECHECKED L1 DOOR PNUEMATIC STORAGE RESERVOIR AND FOUND NO LEAKAGE, REF AMM12-25-04-3.

Part: CONTROL VALVE — INOPERATIVE (NLG STEERING) · airframe 82,972 hrs · 19,957 cycles

ON TAKE OFF ROLL A/C ON CENTERLINE. F/O TAKEOFF. A/C VEERED LEFT. F/O APPLIED FULL RIGHT RUDDER BUT A/C CONTINUED TO VEER LEFT. CAPTAIN TOOK A/C APPLIED RT BRAKE TO IDLE POWER TO BRING A/C TO CENTERLINE. AFTER REJECT BOTH CAPT AND FO TESTED RUDDER STEERING ON RUNWAY A/C STEERED NORMALLY. RETURNED TO GATE FOR TROUBLESHOOTING. A/C TURNED 20 DEG-30 DEG TO LEFT OF CENTERLINE, LESS THAN 50KTS PRIOR TO REJECT. REMOVED AND INSTALLED NLG STEERING CONTROL V/V PER AMM 32-52-03-4. NLG STEERING OPS CHK GOOD.

Part: QUICK DISCONNECT — UNSAFETIED (ADC) · airframe 82,491 hrs · 19,830 cycles

REJECTED TAKE OFF AT 90 KNOTS FOR NO SPEED TAPE IN CAPT HUD AND PFD. INSPECTED ALL 3 PITOT PORTS - NO OBSTRUCTION. CHECKED PITOT QD CONNECTOR AT NR 1 AIR DATA COMPUTER - FOUND IT LOOSE AND PARTIALLY BACKED OFF. RESECURED QD CONNECTOR TO NR 1 AIR DATA COMPUTER. REF: AMM 34-16-04. ACFT OK FOR SVC.

Part: INDICATOR — FAILED (L1 DOOR SLIDE) · airframe 82,295 hrs · 19,761 cycles

L-1 DOOR SLIDE ANNUNCIATOR LIGHT INOPERATIVE. R & R THE L1 DOOR REMOTE PRESSURE INDICATOR ASSY IAW AMM 25-61-04-4. OK FOR SERVICE.

Part: LONGERON — CORRODED (BS 1681) · corrosion level 2 · airframe 81,660 hrs · 19,547 cycles

FOUND CORROSION ON LONGERON 50R AT STA 1681. COMPLIED WITH E.A. 1-5310-T0343744; PART 1; REPAIR FOR LONGERON 50R STA. 1681.

Part: LONGERON — CORRODED (BS 1681) · corrosion level 2 · airframe 81,660 hrs · 19,547 cycles

FOUND CORROSION ON LONGERON 49R AT STA 1681. COMPLIED WITH E.A. 1-5310-T0343744; PART 1; MAINFRAME AFT INTERMEDIATE FUSELAGE; BOTTOM; STA. 1671-1691; R/H LONGERONS L49 & L50 CORROSION REPAIR..

Part: CONTROLLER — FAILED (FIRE DETECTION) · airframe 81,068 hrs · 19,382 cycles

AT FL330, 1:30 MINUTES INTO FLIGHT, RECEIVED LVL3 LOWER CARGO FIRE AFT ALERT, DECLARED AN EMERGENCY, RAN QRH FOR LOWER CARGO FIRE AFT AND DIVERTED TO KPHL. ON LANDING, FIRE DEPT SCANNED AIRPLANE AND REPORTED NO HOT SPOTS. R&R NR 1 & 2 LOWER CARGO FIRE EXTINGUISHER CONTAINERS PER MM REF 26-22-01-4. R&R NR 1 & 2 AFT LOWER CARGO FIREX CONTAINER DISCHARGE CARTRIDGES PER MM REF 26-22-04-4. LOWER CARGO FIRE EXTINGUISHER CONTAINER ADJ/TEST TEST OK PER MM REF 26-22-01-5. REPLACED THE FOLLOWING COMPONENTS PRECAUTIONARY REF SSM 26-14-0. R&R LOWER CTR CARGO SMOKE DETECTORS NR 1, 2, 3 & 4. R&R LOWER AFT CARGO SMOKE DETECTOR 5 REF AMM 26-14-01-4. R&R LOWER AFT CARGO OVERHEAT DETECTOR'S S1-790 & S1-791 REF AMM 26-14-02-4. R&R MISC SYSTEMS CONTROLLER U1-1114 REF AMM 31-42-01-4. R&R CARGO FIRE CONTROL PANEL P4-1029 REF AMM 26-14-10-4. PERFORMED OPS TESTS OF ALL COMPONENTS PER THE FOLLOWING REFERENCES: 26-14-01-5, 31-42-01-5, 26-14-02-5. ALL COMPONENT TESTS PASSED. NO CARGO FIRE FAULTS DISPLAYED.

Part: SUPPORT — CORRODED (LT SPOILER) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

LT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE FOUND WITH CORROSION. CORROSION AT LT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE REWORKED AS PER SRM 51-21-01-0G. EXISTING THICKNESS: 0.406", MATERIAL REMOVED I/B FACE: 0.041" , O/B FACE: 0.057". REMAINING THICKNESS 0.308", REPAIR CARRIED OUT AS PER EA 1-5750-T0341089 PART 1, TITLE: WINGS-ATTACH FITTINGS-LT WING NR 1 SPOILER SUPPORT ASSEMBLY, PART NUMBER : ARC 0391-11 ACTUATOR LOWER HINGE INBD AND OUTBD HOLE CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341089 PART 1AND SNRM NR N00652 FOR WORK DETAILS.

Part: SUPPORT — EXCESS PLAY (RT SPOILER) · airframe 80,858 hrs · 19,323 cycles

RT NR 1 SPOILER LOWER HINGE FOUND FREE PLAY. RT NR 1 SPOILER LOWER HINGE HOLE REWORKED AS PER SRM 51-21-01-0G. EXISTING HOLE DIA 0.954"-0.964", FINAL HOLE DIA 1.069", REPAIR BUSHING 01 EA FABRICATED AND INSTALLED AS PER EA 1-5750-T0341116 PT 1 STEP 4 AND STEP 5, TITLE: WINGS-ATTACH FITTINGS-RT WING NR 1 SPOILER SUPPORT ASSEMBLY, PART NUMBER: ARC0391-12 ACTUATOR LOWER HINGE INBD HOLE CORROSION REPAIR. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: SUPPORT — EXCESS PLAY (LT SPOILER) · airframe 80,858 hrs · 19,323 cycles

LT WING NR 1 SPOILER ACTUATOR FOUND LOWER HINGE FREE PLAY. LT NR 1 SPOILER ACTUATOR LOWER HINGE I/B AND O/B HOLES REWORKED AS PER SRM 51-21-01-0G. I/B HOLE EXISTING HOLE DIA 0.954"-0.970", FINAL HOLE DIA 1.069", O/B HOLE EXISTING HOLE DIA 1.500"-1.505", FINAL HOLE DIA 1.5432", I/B AND O/B BUSHINGS 02 EA FABRICATED AND INSTALLED PER EA 1-5740-T0341089 PT 1 STEP 4 AND STEP 6, TITLE: WINGS-ATTACH FITTINGS-LT WING NR 1 SPOILER SUPPORT ASSEMBLY, PART NUMBER: ARC0391-11 ACTUATOR LOWER HINGE INBD HOLE-CORROSION REPAIR. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (RT SPOILER) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

RT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE FOUND WITH CORROSION. CORROSION AT RT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE REWORKED AS PER SRM 51-21-01-0G. EXISTING THICKNESS: 0.406", MATERIAL REMOVED I/B FACE: 0.035", O/B FACE: 0.052". REMAINING THICKNESS 0.319", REPAIR CARRIED OUT AS PER EA 1-5750-T0341116 PART 1, TITLE: WINGS-ATTACH FITTINGS-RT WING NR 1 SPOILER SUPPORT ASSEMBLY, PART NUMBER ARC 0391-12 ACTUATOR LOWER HINGE INBD HOLE CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341116 PART 1AND SNRM NR N00654 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. HINGE ACTUATOR O/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.250", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2E AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: PIVOT — CORRODED (LT WING) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.630" MAXIMUM ALLOWABLE HOLE DIAMETER: 0.584" SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341019 P1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341019 P1 AND SNRM N00423 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.613", MAXIMUM ALLOWABLE HOLE DIA 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 2B AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09. EXISTING THICKNESS UPPER: 0.409", LOWER: 0.399", MATERIAL REMOVED UPPER: 0.013", LOWER: 0.013", REMAINING THICKNESS UPPER: 0.396", LOWER: 0.386". REPAIR SHIM FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 2.3159", FINAL HOLE DIA 2.321", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341052 PART 1 STEP 2A AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — WORN (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) PIVOT BUSHING WORN. RT I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE MEASURED DIA 2.500" AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. MAXIMUM ALLOWABLE HOLE DIA 2.531". NEW BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-71880 B P4 STEP 1A AND STEP 1C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) UPPER BARREL NUT BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.389", FINAL HOLE DIA 0.406", MAXIMUM ALLOWABLE HOLE DIA 0.931". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2D AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.720", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABLE HOLE DIA 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0340973 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0340973 PART 1 AND SNRM NR N00535 FOR WORK DETAILS.

Part: HINGE BRACKET — WORN (RT WING) · airframe 80,858 hrs · 19,323 cycles

LT INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) PIVOT BUSHING WORN. LT I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE MEASURED DIA 2.526" AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. MAXIMUM ALLOWABLE HOLE DIA 2.531". NEW BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-71881 B P4 STEP 1A AND STEP 1C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. ACTUATOR O/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.221", FINAL HOLE DIA 1.2245", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0340973 PART 1 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0340973 PART 1 AND SNRM NR N00535 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.597", FINAL HOLE DIA 0.613", MAXIMUM ALLOWABLE HOLE DIA 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2B AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341052 PART 1 STEP 2D AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341052 PART 1 AND SNRM NR N00390 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.221", FINAL HOLE DIA 1.248", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2E AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE FOUND WITH CORROSION. LOWER MOUNT O/B HOLE SURFACE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.434", MATERIAL REMOVED FWD FACE: 0.008", AFT FACE: 0.009", REMAINING THICKNESS: 0.417", MINIMUM ALLOWABLE THICKNESS: 0.423". REPAIR SHIM FABRICATED AND INSTALLED AS PER EA 1-5750-T0340973 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0340973 PART 1 AND SNRM NR N00535 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE LOWER MOUNT I/B HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.650", FINAL HOLE DIA 0.713", MAXIMUM ALLOWABLE HOLE DIA 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341052 PART 1 STEP 2B, 2C AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. ACTUATOR I/B HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.227", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0340973 PART 1 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0340973 PART 1 AND SNRM NR N00535 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.251", MAXIMUM ALLOWABLE HOLE DIA 1.220" . OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341019 PART 1 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP I/B AFT HINGE PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.149", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341020 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341052 PART 1 STEP 2D AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.430", MATERIAL REMOVED: 0.007", (FWD) AND 0.019" (AFT), MINIMUM ALLOWABLE THICKNESS: 0.408". REPAIR SHIM FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: BRACKET — CORRODED (TE FLAP) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. IDLER BRACKET ATTACH HOLE BORE REWORKED AS PER SRM 51-21-01-0G. EXISTING HOLE DIA 1.0", FINAL HOLE DIA 1.384", LOCAL BLEND POSITION 9 O'CLOCK POSITION, L=0.25" X W= 0.25", DEPTH=0.065". I/B BUSHING ARC 3087-1 AND O/B BUSHING ARC 3086-1 FABRICATED AND INSTALLED AS PER EA 1-5750-T0341021A PART 1 STEP 1, STEP 2 AND STEP 5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) HINGE LOWER BARREL NUT HOLE FOUND WITH CORROSION. LOWER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.384", FINAL HOLE DIA 0.409", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341019 P1 STEP 1C AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341083 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08. EXISTING THICKNESS UPPER: 0.376", LOWER: 0.373", MATERIAL REMOVED UPPER: 0.003", LOWER: 0.003", REMAINING THICKNESS UPPER: 0.373", LOWER: 0.351". REPAIR CARRIED OUT AS PER EA 1-5750-T0341052 PART 1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341052 PART 1 AND SNRM NR N00390 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE FOUND WITH CORROSION. LOWER MOUNT O/B HOLE SURFACE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS 0.425", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.417". MINIMUM ALLOWABLE THICKNESS: 0.423". REPAIR SHIM FABRICATED AND INSTALLED AS PER EA 1-5750-T0340973 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0340973 PART 1 AND SNRM NR N00535 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.389", FINAL HOLE DIA 0.406", MAXIMUM ALLOWABLE HOLE DIA 0.931". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2D AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS: 0.435". MATERIAL REMOVED: 0.007" (FWD), 0.024" (AFT). REMAINING THICKNESS: 0.404". MINIMUM ALLOWABLE THICKNESS: 0.408". REPAIR SHIM FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 P1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) UPPER MOUNT O/B HOLE BORE (2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.955", MAXIMUM ALLOWABLE HOLE DIA 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2A AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341053 PART 1 AND SNRM NR N00509 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.316", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2C AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABLE HOLE DIA 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0340973 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.627" MAXIMUM ALLOWABLE HOLE DIAMETER: 0.584" SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341019 P1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0341019 P1 AND SNRM N00423 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE UPPER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.384", FINAL HOLE DIAMETER: 0.409", MAXIMUM ALLOWABLE HOLE DIAMETER: 0.391". OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341019 P1 STEP 1C AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT HOLE BORE FOUND WITH CORROSION. CORRODED PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.124". FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T034101B PT 1 STEP 1A. REPAIR CLASSIDFIED MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 80,858 hrs · 19,323 cycles

RT O/B FLAP I/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08. EXISTING THICKNESS UPPER: 0.375", LOWER: 0.351", UPPER: 0.003", LOWER: 0.003", REMAINING THICKNESS UPPER: 0.372", LOWER: 0.348", REPAIR CARRIED OUT AS PER EA 1-5750-T0340973 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-T0340973 PART 1 AND SNRM NR N00535 FOR WORK DETAILS.

Part: PIVOT — CORRODED (LT WING) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION AT LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 2.310". FINAL HOLE DIAMETER: 2.354". MAXIMUM ALLOWABLE HOLE: DIAMETER 2.3135". OVERSIZE BUSHING FABRICATED AS PER EA 1-5750-T0341019 P1 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.582", FINAL HOLE DIAMETER: 0.630" MAXIMUM ALLOWABLE HOLE DIAMETER: 0.584" SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341019 P1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 80,858 hrs · 19,323 cycles

LT O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. HINGE ACTUATOR O/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.251", MAXIMUM ALLOWABLE HOLE DIA 1.220" . OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341019 PART 1 STEP 1D AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

LT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.254", FINAL HOLE DIA 1.2835", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-69256 C P5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO MASTER EA 1-5750-69296 C P5 AND SNRM NR N00763 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

RT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.255", FINAL HOLE DIA 1.284", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-127827 C P5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO EA 1-5750-127827 C P5 AND SNRM NR N00742 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

RT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.290", FINAL HOLE DIA 1.326", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-127827 C P5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 80,858 hrs · 19,323 cycles

LT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.1885", FINAL HOLE DIA 1.222", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-69256 C P5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RUDDER) · airframe 80,858 hrs · 19,323 cycles

UPPER AFT RUDDER ASSEMBLY LT UPPER SKIN FOUND WITH CORROSION AT APPROX ZAR 554.920. CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED ALLOWABLE LIMITS AS PER SRM 55-00-00-2R FIG 202. ORIGINAL THK 0.016", THK REMOVED 0.015", THK REMAINED 0.001". CARRIED OUT REPAIR AS PER SRM 55-40-01-2R FIG 201 REPAIR 2 AND EA 1-5540-T0341022 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 80,858 hrs · 19,323 cycles

DURING HFEC INSPECTION, 01 EA CRACK FOUND APPROX 1/2 INCH IN LENGTH AS MARKED AT LT WING CORNER NR 13 SLAT TRACK NR 10 CUTOUT, AFT INBOARD CORNER. REPAIR CARRIED OUT AT LT WING CORNER NR 13 SLAT TRACK NR 10 CUTOUT AT XOS 659 AS PER SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 80,858 hrs · 19,323 cycles

DURING HFEC INSPECTION, 01 EA CRACK FOUND APPROX 1/8 INCH IN LENGTH AT RT WING CORNER NR 5 SLAT ACTUATOR ACCESS DOOR, FORWARD INBOARD CORNER. REPAIR CARRIED OUT AT RT WING CORNER NR 5 SLAT ACTUATOR ACCESS DOOR FWD INBOARD CORNER AT XOS 490 AS PER SRM 57-40-01-2R FIG 201 REPAIR 17. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,858 hrs · 19,323 cycles

EMPENNAGE RT AFT SKIN FOUND WITH CORROSION UNDERNEATH BODY FAIRING 347DF LOWER EDGE BETWEEN STA 2146 TO 2164. CORROSION BLENDED OUT AND FOUND EXCEEDED ALLOWABLE LIMITS AS PER SRM 53-70-01-2R FIG 201 REPAIR 3. ORIGINAL THK 0.095" THK REMOVED 0.080" THK REMAINED 0.015". REPAIR CARRIED OUT AS PER SRM 53-70-01-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — WORN (CARGO DOOR) · airframe 79,275 hrs · 18,869 cycles

CARGO DOOR, MCD FWD 3 HINGE LOBES AIRCRAFT SIDE OVER CMM LIMIT. COMPLY WITH EA 1-5230-T0336800 REV NR P1 MAIN CARGO DOOR FWD HINGE AIRCRAFT SIDE HAS 17 EA LUGS OUT OF LIMITS. THE 3 FORWARD LUGS WERE WORN BEYOND CMM LIMITS REQUIRED ABOVE EA FOR REPAIR. COMPLIED WITH EA 1-5230-T0336800 FOR THE REPAIR OF THE THREE FORWARD LUGS.

Part: FRAME — CRACKED (BS 1601) · airframe 79,000 hrs · 18,789 cycles

MAIN DECK, BS 1601 LONGERON 17R, FRAME CRACKED. REPAIRED IAW SRM 53-30-00, FIG 5, SHEET 1, VOL 1.

Part: SEAT TRACK — CRACKED (BS 1521) · airframe 78,974 hrs · 18,778 cycles

MAIN CABIN SEAT TRACK DAMAGED BS 1521, RBL 27. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL. 1.

Part: PUMP — MALFUNCTIONED (ENGINE) · airframe 78,937 hrs · 18,767 cycles

DURING TAKEOFF ROLL AT 120 KIAS, ENG FAIL LIGHT ON GLARESHIELD ILLUMINATED. REJECTED TAKE-OFF AND COMPLIED WITH QRH. AS PER CREW VERBAL DEBRIEF, THEY DID NOT FEEL A ROLL DURING TIME OF EVENT AND HEARD AN ENGINE POWER BACK. REQUIRES TROUBLESHOOTING. REPLACED THE ENGINE DRIVEN FUEL PUMP

Part: HMU — MALFUNCTIONED (ENGINE) · airframe 78,916 hrs · 18,760 cycles

ENGINE FAIL LIGHT AT 120KTS. RTO COMPLIED WITH QRH. OLD DISCREPANCY 605 / 77-11. R&R HMU.

Part: SKIN — CHAFED (LT WING) · airframe 78,914 hrs · 18,759 cycles

LT WING LOWER WING ACCESS PANEL DOOR CUT OUT AT XORS 683 HAS 1 EA DAMAGE ATTACH HOLE AT 6 OCLOCK POSITION AFT REPAIR DOUBLER REF SRM 57-10-00 FIG 69A SHEET 2

Part: INDICATOR — MALFUNCTIONED (SLIDE PRESSURE) · airframe 78,286 hrs · 18,565 cycles

DURING AN A CHECK, FOUND THE R1 DOOR SLIDE REMOTE PRESSURE PRESS TO TEST INDICATOR LIGHT DOES NOT EXTINGUISH. TROUBLESHOT SLIDE, PRESSURE VERIFIED ADEQUATE. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-61-15-4. CHECKED OK.

Part: INDICATOR — FALSE ACTIVATION (DOOR SLIDE) · airframe 77,881 hrs · 18,409 cycles

RT CABIN DOOR SLIDE LIGHT ILLUMINATED. REMOVED AND REPLACED INDICATOR ASSEMBLY IAW AMM 25-61-04-4. PERFORMED AN OPS CHECK IAW AMM 25-61-04-710-801. OPS CHECK PASSED. OK FOR SERVICE.

Part: INDICATOR — DAMAGED (R1 DOOR) · airframe 77,703 hrs · 18,349 cycles

R1 DOOR SLIDE BOTTLE PRESS LIGHT STAYS ILLUMINATED. LIGHT DOES NOT SPRING BACK DURING TROUBLESHOOTING FOUND ON THE REMOTE PRESSURE INDICATOR THAT THE UPPER DOOR LINER JACK GROUNDED TO SELF PER WDM 25-61-01. REMOVED AND REPLACED REMOTE PRESSURE INDICATOR ASSEMBLY IAW MM 25-61-04-4. OPS CHECK NORMAL PER MM 25-61-04-5.

Part: SENSOR — FAILED (PNEUMATIC SYS) · airframe 77,640 hrs · 18,335 cycles

DURING CLIMB OUT AT 3000 FT, RECEIVED A LEVEL 3 AIR MANIFOLD 1 FAIL AND AURAL WARNING. LEVEL AT 5000 FT RAN QRH. DUMPED FUEL AFTER 3 MINUTES, SECOND PRV CLOSED AND BOTH SYSTEM 1 & 2 RED ON AIR SYNOPTIC. CURRENT FAULT SHOWS 'MFC MON 2 RLY'. LAST LEG FAULTS HAS 10 FAULTS. PNEU Z11 OVERHEAT, PNEU Z7B OVERHEAT, PNEU Z7B OVERHEAT, MFC PNEU 1 OUT, MFC MON 1 RELAY, PNEU 2 OUT, PNEU Z7A OVERHEAT, PNEU 1 Z4 OVERHEAT, MFC MON 2 RELAY, PNEU Z5 OVERHEAT. REPLACED THE ZONE 5 SENSING ELEMENT D1-38E IAW AMM 36-23-07-4, CHECKED GOOD. INSULATION RESISTANCE CHECKED, BOTH PASSED IN ZONE 5 AND ZONE 7B ELEMENT IAW WDM 36-23-02, PG1, SH1. APU PNEUMATIC DECAY CHECKED IN 1-2-AND 3 SYSTEM, ALL PASSED.

Part: CLAMP — LOOSE (PNEUMATIC SYS) · airframe 77,640 hrs · 18,335 cycles

DRUING CLIMB OUT AT 3000 FT, RECEIVED A LEVEL 3 AIR MANIFOLD 1 FAIL, AND AURAL WARNING. LEVELED AT 5000', RAN QRH. DUMPED FUEL AFTER 3 MINUTES, SECOND PRV CLOSED AND BOTH SYSTEM 1 & 2 RED ON AIR SYNOPTIC. RETORQUED LEAKING CLAMP. R & R THE ZONE 5 SENSING ELEMENT D1-38E, R & R THE RELAY R2-5015 AND RELAY R2-5743.

Part: PANEL — MISSING (NR 1 NACELLE) · airframe 76,696 hrs · 18,058 cycles

ON ARRIVAL, FOUND NR 1 INBOARD ENGINE MOUNT COVER WAS FOUND MISSING, ALSO FWD NUT PLATEWAS MISSING AND REAR NUT PLATE ATTACH RIVET HEAD MISSING. REPAIRED IAW 1-5450-T0328547 A PART 2, REPLACED INTERIM PANEL WITH NEW IAW AMM,SRM, IAW DRAWINGS AUB7726. OK FOR SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 76,366 hrs · 17,956 cycles

RIGHT WING, FIXED LEADING EDGE NR 10 SLAT TRACK INBOARD CUTOUT SKIN CENTER FOUND CRACKED AT XOS 657. REPAIR CARRIED OUT IAW EA 1-5730-T0326737, PART 1, TITLE: WINGS, PLATES AND SKINS. REPAIR FOR RT WING FIXED L/E NR 10 SLAT TRACK CUTOUT SKIN CENTER AREA CRACK AT XOS 657. REPAIR CLASSIIFED AS MAJOR IAW GMM 6 -2-100. REFER TO WRI 57304075 FOR WORK DETAILS.

Part: SKIN — CRACKED (TE FLAP) · airframe 76,366 hrs · 17,956 cycles

AGING AIRCRAFT, EXISTING REPAIR AT RT WING INBD FLAP SEGMENT UPPER SURFACE AT XIFH 171.3 -XIFH 177.3. EVALUATED AND FOUND CRACK COMMON TO SKIN. RIGHT WING INBD FLAP, INBD FLAP SEGMENT UPPER SURFACE XIFH 171.3-XIFH 177.3. CARRIED OUT REPAIR IAW EA 1-5750-T0326829P1, STEP 1A. EO 1-5100-5001B6, PART 1 TITLE: STRUCTURES, REPAIR CATALOG, REPAIR ID AND TRACKING REQUIREMENTS 14CFR 121.707" ACCOMPLISHED. REFER WRI 57504064 FOR WORK DETAILS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,366 hrs · 17,956 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, REPAIR 15, FIG 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,366 hrs · 17,956 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 770 FOUND CRACKED. BEADED DOUBLER REPAIRED IAW SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,366 hrs · 17,956 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 749 FOUND CRACKED. BEADED DOUBLER REPLACED IAW SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 76,366 hrs · 17,956 cycles

ON REMOVAL OF MAIN DECK FLOOR PANEL 243CF, FOUND SEAT TRACK CRACKED AT BS 755 X -27.5. REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STA 745 TO STA 765, X=-27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 76,366 hrs · 17,956 cycles

LEFT WING OUTBOARD AILERON TRAILING EDGE WEDGE UPPER SURFACE INBOARD SIDE. FOUND DELAMINATION ABOUT 4" X 4". REPAIRED IAW EA 1-5750-T0326653, PART: 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI: 57504046 FOR WORK DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,366 hrs · 17,956 cycles

MAIN DECK SEAT TRACK AT BS 1541 X 47.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1530-STA 1550X=47.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 76,366 hrs · 17,956 cycles

MAIN DECK SEAT TRACK AT BS 1480 X 47.5 FOUND TO HAVE CROWN DAMAGE. REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STA 1470 TO STA 5-0 X= 47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 76,366 hrs · 17,956 cycles

MAIN DECK SEAT TRACK AT BS 1734, X 47.5 FOUND TO HAVE CROWN DAMAGED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1730 TO STA 1750, X = 47.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 76,366 hrs · 17,956 cycles

MAIN DECK SEAT TRACK AT BS 1734 X 27.5 FOUND TO HAVE CROWN DAMAGE. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1730-STA 1750 TO STA 1750X=27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,366 hrs · 17,956 cycles

MAIN DECK SEAT TRACK AT BS 1301 X 8.5 FOUND CORRODED. REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STA 1270 TO STA 1330, X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1381) · airframe 76,366 hrs · 17,956 cycles

MAIN DECK SEAT TRACK AT BS 1381 X 47.5 FOUND TO HAVE CROWN DAMAGE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,366 hrs · 17,956 cycles

MAIN DECK SEAT TRACK AT BS 5-43 X 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-0 TO STA 5-83 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 75,557 hrs · 17,716 cycles

REPEAT WRITE UP, AT START OF TAXI, NR 2 ENG FLAMED OUT. RAMP TOWER REPORTED SMOKE COMING FROM THE ENG, SO WE SHUT IT DOWN & DISCHARGED ONE FIRE BOTTLE. SMOKE STARTED TO DISSIPATE, DID NOT FIRE SECOND BOTTLE.

Part: ENGINE — FIRE (NR 2) · airframe 75,549 hrs · 17,711 cycles

AFTER NORMAL 3 ENG START, BEGAN TAXI, GOT LVL 0 ALERTS. RAMP 1-3, RAMP 2-3, AIR 1-3 ISOL & ANTI-ICE ENG 2 DISAGREE. EXTERNAL RADIO CALLS FOR SMOKE & FLAME ON ENG 2. ALL ENG INDICATIONS NORMAL. PULLED 2 FIRE HANDLE & BLEW AGENT, STILL REPORTS OF FLAME. MOTORED 4 - 5 MIN STILL REPORT OF FLAME BLEW SECOND AGENT BOTTLE. FLAMES OUT ALL TEMPS LOW. REPLACED BOTH NR 2 FIRE BOTTLES IAW AMM 26-21-01-4. SEE WRI 26-20 3327 FOR PAR. RAN NR 2 ENG IAW JRH & TESTED NR 2 ANTI-ICE VLV IAW AMM 30-22-00-5-1. SYS TESTED NORMALLY. NR 2 ENG STARTED NORMALLY IAW JRH WITH NO ROLLBACK.

Part: SUPPORT BRACKET — CRACKED (TAILCONE) · airframe 748 hrs · 17,463 cycles

POST FLIGHT MX WALK AROUND SHOWS TAIL CONE NOT SECURED. GAP BETWEEN TAIL CONE & FUSELAGE. INSPECTION SHOWS LT SUPPORT BRACKET FOR LT UPPER LATCH CRACKED & HAS SHEARED RIVETS. UNABLE TO ACCESS TAIL CONE COMPARTMENT FOR FURTHER INSPECTION DUE TO TAIL CONE IS ONLY HELD BY SAFETY HOOK & HIGH WINDS ON RAMP IAW AMM 53-52-01-2. FOUND SUPPORT BRACKET OF LT UPPER LATCH CRACKED & HAD SHEARED RIVETS, BRACKETS & ATTACHING HARDWARE R & R. REPLACED AND REPAIRED

Part: ACTUATOR — MALFUNCTIONED (OUTFLOW VALVE) · airframe 742 hrs · 17,262 cycles

AT CRUISE FLIGHT AT FL380, RECEIVED A LEVEL 3 CABIN ALTITUDE. QRH ACTION AVIONICS FAN OVRD CORRECTED PROBLEM. AFTER APPROX 10 MINUTES PROBLEM RETURNED. HAD TO INITIATE DESCENT TO FL320 TO MAINTAIN PRESS. THERE WAS A SLIGHT VIBRATION UNDER THE CAPTAIN'S FLOOR AREA. REPLACED OUTFLOW VLV ACTUATOR.

Part: DOOR FRAME — CRACKED (LT MLG DOOR) · airframe 71,836 hrs · 16,567 cycles

LEFT MLG DOOR UPPER FRAME CTR HINGE ATTACHMENT FOUND CRACKED AT APPROXIMATE STATION Y=1438.375. AREA REPAIRED AS PER EA 1-3210-T0310973A PART 1 TITLE: "LANDING GEAR - MAIN GEAR AND DOORS - MLG LT DOOR HINGE FRAME FOUND CRACKED" WORK INSTRUCTIONS. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REFER TO WRI 32101142 FOR DETAILS.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,836 hrs · 16,567 cycles

CABIN AT LT STATION 1257 LONGERON 27 FOUND CRACKED. CABIN AT LEFT HAND STATION 1257 CRACKED LONGERON 27 REMOVED AND REPLACED AS PER SRM 51-31-01 FROM STATION 1256 TO STATION 1305 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: FRAME — DENTED (FUSELAGE) · airframe 71,836 hrs · 16,567 cycles

CABIN LT STATION 1641, LONGERON 11 - 12 FRAME FOUND DENTED. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 FLIGHT CYCLES AND REPETITIVE INSPECTION 9,500 FLIGHT CYCLES TO BE CARRIED OUT AS PER SRM 53-00-07 TABLE 201 REPAIR 2. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: WEB — CRACKED (FUSELAGE) · airframe 71,836 hrs · 16,567 cycles

CABIN L3 MAIN ENTRY DOOR FWD LOWER JAMB STATION 1254, LONGERON 26 - 27 WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: WEB — CRACKED (FUSELAGE) · airframe 71,836 hrs · 16,567 cycles

CABIN L3 MAIN ENTRY DOOR AFT LOWER JAMB STATION 1310, LONGERON 26 - 27 WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: WEB — CRACKED (FUSELAGE) · airframe 71,836 hrs · 16,567 cycles

CABIN R3 MAIN ENTRY DOOR AFT LOWER JAMB STATION 1310, LONGERON 26 - 27 WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: WEB — CRACKED (FUSELAGE) · airframe 71,836 hrs · 16,567 cycles

CABIN R3 MAIN ENTRY DOOR FWD LOWER JAMB STATION 1254, LONGERON 26 - 27 WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: SKIN — CRACKED (LT WING) · airframe 71,836 hrs · 16,567 cycles

LEFT WING LOWER FIXED LE SKIN XORS 799 ON SLAT TRACK CUT OUT FOUND CRACK. CRACKED AREA AT LEFT HAND WING LOWER FIXED LEADING EDGE SKIN AT STATION XOS 799 AREA REPAIRED AS PER SRM 57-40-02. REPAIR 7 FIGURE 201 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: SKIN — CRACKED (LT WING) · airframe 71,338 hrs · 16,408 cycles

ON WALK AROUND FOUND POSSIBLE CRACK ON LT WING AT FUELING PANEL FWD INBD CORNER. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6. TRIMED OUT CRACK AREA IAW SRM 57-40-02 REPAIR 7 FIG 202. PERFORMED HFEC OF DAMAGE CUT OUT IAW NTSPM 06-10-01.001. INSTALLED DOUBLER & FILLER IAW SRM 57-40-02 REPAIR 7 FIG 202 & EA 1-5710-T0308358 PT 1 FOR ALTERNATE FASTENERS. PAINTED REPAIR IAW SRM 51-21-02.

Part: BATTERY — INOPERATIVE (DOOR SLIDE) · airframe 69,720 hrs · 15,892 cycles

DURING SERVICE CHECK, FOUND PUSH TO TEST LIGHT ON R1 DOOR SLIDE REMOTE INDICATOR INOP. R & R PUSH TO TEST LIGHTS. NO HELP. REPLACED 2C BATTERYS ON DOOR SLIDE, OPS CHECKED DOOR IAW MM 25-61-04-4.

Part: TRUNNION — CORRODED (MLG) · airframe 69,577 hrs · 15,835 cycles

EVIDENCE OF RUST AROUND CENTER LANDING GEAR PILLOW BLOCK. REPAIRED IAW EA T1-3210-T0300244, REV F, PART 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: BUTTON — INOPERATIVE (PRESS TO TEST) · airframe 69,400 hrs · 15,756 cycles

DURING PRE DEPARTURE CHECK, R1 DOOR EVACUATION SLIDE REMOTE PRESS -TO-TEST PUSH BUTTON INOPERATIVE. REPLACED LAMPS WITH PROPER BULB 368 PER SMP OPS CHECKED GOOD.

Part: DADC — MALFUNCTIONED · airframe 69,238 hrs · 15,671 cycles

AIRSPEED, LOST SUSPECT OR ERRATIC IAS ANNUNCIATION ON BOTH PFD, W SHEAR DET FAIL ALERT SEL ELEV FEEL MAN. SEL FLAP LIM OVER RIDE IND A/S NOT CONSISTENT WITH NORMAL PITCH ATT & PWR. REF WRI 34-16-9308 FOR CADC REMOVE AND REPLACE. INSPECTED ALL 3 PITOT TUBES IAW AMM 34-11-01-6. CAPT/STBY GOOD. F/O'S DRAIN HOLES WERE CLOGGED. CLEANED DRAIN HOLES IAW AMM 34-11-01-2. CHECKS GOOD IAW AMM 34-11-00-2. CHECKED ADC'S IAW AMM 34-16-03-2. CHECKS GOOD WITH NO FAULTS. OTHER WARNINGS WHERE SET OFF BY F/O'S ERRATIC AIR SPEEDS. ACFT OK FOR SERVICE.

Part: SKIN — DELAMINATED (RT WING AILERON) · airframe 68,118 hrs · 15,292 cycles

RT WING, OTBD AILERON, INBD T/E SURFACE FOUND DELAMINATED. REPAIRED IAW SRM 57-60-80, REPAIR 1, REVISION 51 AND COMPLIED WITH EA 1-5750-165176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 68,118 hrs · 15,292 cycles

EMPENNAGE, LT LOWER VERTICAL STABILIZER REAR SPAR FRAME APPROX STATION YTN= 121 ACCESS THRU PANEL NR 363PL FOUND WEB CRACKED. REPAIRED IAW SRM 55-30-02, REPAIR 2, REV 51.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 68,118 hrs · 15,292 cycles

EMPENNAGE, RT LOWER VERTICAL STABILIZER REAR SPAR FRAME APPROX STATION YTN= 121 ACCESS THRU PANEL NR 364RR FOUND WEB CRACKED. REPAIRED IAW SRM 55-30-02, REPAIR 2, REV 51.

Part: SKIN — CRACKED (ZONE 500) · airframe 68,118 hrs · 15,292 cycles

ONE FASTENER HOLE FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. REPAIR CARRIED OUT IAW SRM 57-20-02, FIGURE 201, REPAIR 5, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

CENTER CARGO COMPARTMENT, ABOVE CEILING AREA, AT BS 1661, "X"= 75, SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPLACED FROM BS 1651 TO 1711, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR, IAW MM 6-2-100, REV 115.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 68,118 hrs · 15,292 cycles

MAIN DECK FLOOR SUPPORT AT BS 1887, "X"=0, FOUND CRACKED. R & R IAW MM 20-50-02, REV 74.1. FLOOR SUPPORT FABRICATED IAW DWG AGA7081, REVISION "M". REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

CENTER CARGO COMPARTMENT, ABOVE CEILING AREA AT BS 1701, "X" = 75, SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPLACED FROM BS 1651 TO 1711, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR PANEL SUPPORT AT STATION 1887, "X"=-60, FORWARD FLANGE CORRODED. FLOOR SUPPORT REMOVED AND REPLACED AS PER AMM 20-50-02, REVISION 74.1. NEW FLOOR SUPPORT FABRICATED IAW DRAWING AGA7551, REVISION "G". CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK BS 1541, X= -27 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACED FROM STATION 1531 TO 1571, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK, BS 1745, X= -27 FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.

Part: SKIN — CRACKED (ZONE 500) · airframe 68,118 hrs · 15,292 cycles

LT WING L/E LOWER SURFACE ACCESS PANEL 518FB CUT-OUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 202, REPAIR 7, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK BS 1827, X= 8.5 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACEED FROM BS 1791 TO 1887, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 600) · airframe 68,118 hrs · 15,292 cycles

RT WING L/E FOUND LOWER FIXED PANEL NR 11 SLAT TRACK CUT-OUT SKIN EDGE CORNER CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK BS 1661, X= -8.5 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACEED FROM BS 1531 TO 1671, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (RT WING LE SLAT) · airframe 68,118 hrs · 15,292 cycles

RT WING L/E NR 8 SLAT OTBD INNER SKIN FOUND CRACKED. REPAIRED IAW EA 1-5750-165172, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK BS 1541, X= -8.5 FOUND WITH SURFACE CORROSION. CARGOTRACK REPLACED FROM BS 1531 TO 1671, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK BS 1841, X= -27 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACED FROM BS 1791 TO 1887, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 500) · airframe 68,118 hrs · 15,292 cycles

LEFT WING NR 11 L/E SLAT TRACK CUT-OUT FOUND CRACKED AT XOS 720. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK AT BS 873, "X"= 8.5, FOUND WITH CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK AT BS 1092, "X"= 47, FOUND CROWN ELONGATED. CARGO TRACK REPLACED FROM BS 1009 TO 1109, "X"= 47, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

LEFT WING, T/E LOWER ACCESS PANEL NR 541JB CUTOUT FORWARD EDGE LOWER CAP. LOWER SURFACE FOUND CORRODED. CUTOUT FORWARD EDGE LOWER CAP DAMAGED. R & R WITH NEW CAP IAW SRM 51-31-01, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.

Part: CARGO TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK AT BS 1035, "X"= 47", FOUND CROWN ELONGATED. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,118 hrs · 15,292 cycles

MAIN DECK CARGO TRACK AT BS 873, "X"=-8.5", FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 68,118 hrs · 15,292 cycles

LEFT WING, INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED IAW MM 27-50-22-4, REVISION 74.1. ADJUSTMENT CARRIED OUT IAW MM 27-50-22-830-801, REVISION 74.1 AND FOUND SATISFACTORY. FLAP OPS TEST CARRIED OUT IAW MM 27-50-00-860-801, REVISION 74.1 AND FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.

Part: DOOR FRAME — CRACKED (BS 1743) · airframe 68,118 hrs · 15,292 cycles

CENTER CARGO DOOR, UPPER DOOR FRAME BEAM AT BS 1743, "X" =-106 CRACKED. REPAIRED IAW EA 1-5310-165169. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,735 hrs · 15,195 cycles

PRE-DISPATCH CHECK FOUND EMERGENCY LIGHT TEST FAILED. R & R THE EMERGENCY LIGHTING BATTERY POWER SUPPLY, OPS TEST PASSED .

Part: BATTERY — INOPERATIVE (ESCAPE SLIDE) · airframe 66,783 hrs · 14,918 cycles

DURING PREFLIGHT DISCOVERED DOOR R-1 EMERGENCY ESCAPE SLIDE PRESS TO TEST INDICATOR DID NOT ILLUMINATE WHEN PRESSED. REPLACED BATTERIES IAW SMP, OPS CHECKED NORMAL, OK FOR SERVICE.

Part: LAMP — FAILED (DOOR SLIDE) · airframe 66,553 hrs · 14,860 cycles

DOOR EVAC SLIDE PRESS TO TEST INDICATOR SWITCH INOPERATIVE. RELAMPED R1 DOOR REMOTE PRESSURE INDICATOR WITH CORRECT LAMPS IAW SMP. PERFOREMD OPS CHECK IAW AMM 25-61-04-5-0 WITH NO DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE AT THIS TIME.

Part: BULB — INOPERATIVE (R1 DOOR SLIDE) · airframe 65,739 hrs · 14,650 cycles

R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INOPERATIVE. REPLACED PUSH SWITCH LIGHT BULB ASSY AND OPS CHECKED NORMAL IAW MM 25-61-04-4.

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 65,702 hrs · 14,642 cycles

R1 SLIDE CONTINUITY PRESS TO TEST LIGHT INOPERATIVE ON PRE-FLIGHT. CAN RT R & R TEST LIGHT BATTERY IAW SMP. PERFORMED OPS TEST IAW MM 25-61-04-5,CHECK.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 64,944 hrs · 14,475 cycles

EMER LT TEST FAILS, GET EMER LT BAT 1 ALERT DURING TEST. R & R EMERERGENCY LIGHTING BATTERY POWER SUPPLY REF MM 33-51-01-4-0. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (ESCAPE SLIDE) · airframe 64,341 hrs · 14,310 cycles

LT MAIN ENTRY DOOR EVACUATION SLIDE PRESSURE WONT TEST. RELAMPED L1 EVACUATION SLIDE PACK PRESSURE INDICATION SWITCH IAW AMM 25-61-04-5-0, CHECKED GOOD.

Part: LIGHT — ILLUMINATED · airframe 63,067 hrs · 14,014 cycles

EMERGENCY POWER ON LIGHT CAME ON DURING FLIGHT - FOLLOWED QRH IT WENT OUT. ADJUSTMENT TEST POWER SYS EMERGENCY IAW AMM 24-24-00-5. OPS CHECKED GOOD, ACFT OK FOR SERVICE AT THIS TIME. FINAL CLOSED.

Part: LONGERON — CRACKED (ZONE 200) · airframe 62,866 hrs · 13,961 cycles

MAIN DECK STA 5-0, LONGERON 1, RT FWD SECTION EDGE FOUND 1 EA CRACKED, APPROX 0.25 INCH LONG DURING X-RAY INSP. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 45. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON — CRACKED (ZONE 200) · airframe 62,866 hrs · 13,961 cycles

MAIN DECK STA 5-0, LONGERON 1 LT, AFT SECTION EDGE FOUND 1 EACH CRACKED, APPROX 0.25 INCH LONG DURING X-RAY INSP. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REVISION 45. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON — CRACKED (ZONE 200) · airframe 62,866 hrs · 13,961 cycles

MAIN DECK STA 5-123, LONGERON 6 RT, LONGERON SPLICE CTR SECTION FOUND 2 EA CRACKED, APPROX 0.625 INCH LONG DURING X-RAY INSP. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7112 REVISION D. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON — CRACKED (ZONE 200) · airframe 62,866 hrs · 13,961 cycles

MAIN DECK STA 5-0, LONGERON 1, LT FWD EDGE FOUND 1 EACH CRACKED, APPROX 1.25 INCH LONG DURING X-RAY INSP. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 45. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (ZONE 500) · airframe 62,866 hrs · 13,961 cycles

LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, FOUND 03 EACH FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 62,866 hrs · 13,961 cycles

RT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, FASTENER HOLES 12 EA. FOUND CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 62,866 hrs · 13,961 cycles

RT WING INBD T/E FLAP VANE LOWER SURFACE DELAMINATED BETWEEN VANE CTR AND OTBD TRACK. VANE REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 69.0. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 69.0 FOUND SATISFACTORY.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 62,866 hrs · 13,961 cycles

RT WING SLAT TRACK NR8 CUT OUT OTBD AREA CRACKED. REPAIRED AS PER E.A. 1-5740-143499. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FITTING — CRACKED (LT MLG) · airframe 62,866 hrs · 13,961 cycles

LT MLG DOOR UPLATCH FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. FITTING FABRICATED AS PER DRAWING ANB7089 REVISION A. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: RIB — CRACKED (ZONE 600) · airframe 62,866 hrs · 13,961 cycles

RT WING L/E INBD RIB NR16 CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45 AND DRAWING ARB7565 REVISION C. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: FITTING — CRACKED (RT MLG) · airframe 62,866 hrs · 13,961 cycles

RT MLG DOOR UPLATCH FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. FITTING FABRICATED AS PER DRAWING ANB7089 REVISION A. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

FUSELAGE EXISTING SKIN DOUBLER REPAIR (02 LAYER) FOUND AT STATION 621 LONGERON 26 LEFT. FUSELAGE EXISTING SKIN DOUBLER REPAIR AT STATION 621, LONGERON 26 LEFT EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. EXISTING DOUBLER REPAIR (02 LAYER) AT FUSELAGE STATION 621, LONGERON 26 LEFT. REMOVED AS PER SRM 51-33-01 VOLUME II, REVISION 40 AND REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 17 VOLUME I, REVISION 40 EO NR 1-5100-7-5001 A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100, REVISION 107.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 57,345 hrs · 12,752 cycles

CRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON RIGHT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP. CRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON RIGHT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP REPAIRED AS PER SRM 55-20-00 FIGURE 3, VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 57,345 hrs · 12,752 cycles

01 FASTENER HOLE FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700. FASTENER HOLE FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS 690 AND XORS 700 REPAIRED AS PER EA 1-5710-127828, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100, REVISION 107.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 57,345 hrs · 12,752 cycles

04 FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION, AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700. FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS 690 AND XORS 700, REPAIRED AS PER EA 1-5710-127824, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100, REVISION 107.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

MAIN DECK CARGO STA 1651 LONGERON 13 RIGHT SPLICE DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. NEW SPLICE FABRICATED AS PER AFA7181 REVISION E. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 57,345 hrs · 12,752 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) PIVOT POINT BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127825, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT OUTBOARD BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127826, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT INBOARD LUG BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127827, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

MAIN DECK CARGO STA 1276 TO STA 1361, X = -75.5 SEAT TRACK FOUND WITH SURFACE CORROSION.

Part: SEAT TRACK — CORRODED (BS 1175-1257) · airframe 57,345 hrs · 12,752 cycles

MAIN DECK CARGO STA 1175 TO STA 1257, X = -75.5 SEAT TRACK FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (BS 1301-1381) · airframe 57,345 hrs · 12,752 cycles

MAIN DECK CARGO STA 1301 TO STA 1381, X = 75.5 SEAT TRACK FOUND WITH SURFACE CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 57,345 hrs · 12,752 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT OUTBOARD LUG BORE FOUND CORROSION. REPAIRED AS PER E.A. NO. 1-5750-127825, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SKIN — CHAFED (ZONE 600 TE FLAP) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING LEADING EDGE UPPER SURFACE FOUND CHAFING MARK AT APPROXIMATELY XIS 247. CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 24 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.

Part: STRUCTURE — CHAFED (ZONE 600) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING DROOP LEADING EDGE UPPER SURFACE INBOARD SIDE FOUND CHAFING MARKS. REPAIRED AS PER EA 1-5730-128683, CLASSIFIED AS MINOR REPAIR PER GMM 6-2-100, REVISION 107.

Part: SKIN — CRACKED (ZONE 600 TE FLAP) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING INBOARD FLAP UPPER SURFACE SKIN FOUND CRACKED AT 46 INCHES FROM INBOARD END AND 51.5 INCHES FROM TRAILING EDGE, AT APPROXIMATELY XIFH 171.5. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 38 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT OUTBOARD LUG BORE FOUND CORROSION. REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-127820. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT INBOARD BORE FOUND CORROSION. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-127820. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT OUTBOARD BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127820, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLE NR B AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

MAIN DECK CARGO STATION 5-40, X = -8.5 SEAT TRACK FOUND CORRODED.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLE NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SKIN — CRACKED (RT WING LE) · airframe 57,345 hrs · 12,752 cycles

RIGHT WING LEADING EDGE, ANTI-ICE TELESCOPIC DUCT DOOR CUTOUT, CRACKS FOUND AT UPPER CORNER EDGES, STA XOS 464 AND STATION XOS 470. REPAIR CARRIED OUT AS PER SRM 57- 10-00 FIGURE 43 VOLUME I, REVISION 40. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30-5, REVISION 62 AND OPERATION TEST AND LEAK CHECK OF THE TELESCOPIC DUCT CARRIED OUT AS PER AMM 30-11-01-4, REVISION 62 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE NR C AND D.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE NR A, B AND C.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

MAIN DECK CARGO STATION 1463, X = 8.5 SEAT TRACK FOUND CORRODED.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLE NR C.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,345 hrs · 12,752 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE NR A, B, C AND D.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR FRAME) · airframe 57,345 hrs · 12,752 cycles

CRACK INDICATION FOUND DURING INSPECTION ON DIAMETER: 0460 HOLE AT THE MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLE NR A AND D, FITTING. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: PAN — CRACKED (CARGO DOOR) · airframe 57,345 hrs · 12,752 cycles

UPPER CARGO DOOR CENTERING GUIDE ASSY MOUNTING STRUCTURE FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40. ADJUSTMENT OF CLOSE LIMIT WARNING SWITCH AND VENT DOOR WARNING SWITCH CARRIED OUT AS PER AMM 52-34-18 FOUND SATISFACTORY. NEW PAN FABRICATED AS PER DRAWING ACA7304 REVISION J. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SWITCH — DAMAGED (FIRE DETECTOR) · airframe 55,846 hrs · 12,441 cycles

"CRG FIRE LWR AFT" LEVEL 3 ALERT AND AURAL WARNING ON TAKEOFF ROLL. ABORTED TAKEOFF AND DISCHARGED BOTH FIRE BOTTLES. PERFORMED AFT AND FWD CARGO COMPT INSPECTION, NO DAMAGED OR FIRE CONDITION FOUND. VERIFY WITH FLT CREW THAT THEY DISCHARGED AGENT 1 (THE BIG BOTTLE) ONLY. MSC FAULT REVIEW SHOWN 'MSC' NO OTHER RELATED FAULT. REMOVED AGENT 1 FIRE BOTTLE PER AMM 26-22-01-4 AND FOUND P1-2286 CONNECTOR BROKEN OFF. SUPP, R & R LOWER CARGO FIRE EXTINGUISHER CONTAINER NR 1 PER MM 26-22-01-4, FOUND FWD & AFT AGENT 1 LOW PRESS LIGHT ON. T/S FIM 26-22-01 FOUND LOW PRESS SWITH AT FAULT ,PRESSURE SWITCH PIN "A" & "B" IN CLOSED.

Part: SWITCH — MALFUNCTIONED (FIRE BOTTLE) · airframe 55,846 hrs · 12,441 cycles

"CRG FIRE LWR AFT" LEVEL 3 ALERT AND AURAL WARNING ON TAKEOFF ROLL. ABORTED T/O AND DISCHARGED BOTH FIRE BOTTLES. PERFORMED AFT AND FWD CARGO COMPT INSPECTION, NO DAMAGE OR FIRE CONDITION FOUND. VERIFY WITH FLT CREW THAT THEY DISCHARGED AGENT 1 (THE BIG BOTTLE) ONLY. REMOVED AND REPLACED LOWER CARGO FIRE EXTINGUISHER CONTAINER NR 1 PER MM 26-22-01-4. FOUND FWD AND AFT AGENT 1 LOW PRESS LIGHT ON. T/S FIM 26-22-01 FOUND LOW PRESS SWITCH AT FAULT, PRESSURE SWITCH PIN "A" AND "B" IN CLOSED. SWITCH IS PART OF THE FIRE BOTTLE SAME P/N.

Part: SUPPORT BRACKET — CORRODED (FLAP FAIRING) · airframe 52,369 hrs · 11,713 cycles

RIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT OUTBOARD LOWER MOUNTING BORE FOUND CORROSION. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-116494. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1211-1239) · airframe 52,369 hrs · 11,713 cycles

FOUND UPPER CARGO COMPARTMENT, SEAT TRACK RBL 75 CORRODED AT STA 1211 TO BS 1239. 10-24-07 REPAIR CARRIED OUT AS PER SRM 53-70-00 FOULME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CHAFED (LT WING LE SLAT) · airframe 52,369 hrs · 11,713 cycles

LEFT WING, NR 3 LEADING EDGE SLAT O/B SUPPORT FITTING FOUND CHAFE MARK. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-115218, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — DAMAGED (LT WING LE SLAT) · airframe 52,369 hrs · 11,713 cycles

LEFT WING, NR 3 LEADING EDGE SLAT O/B SUPPORT FITTING MOUNTING HOLE ELONGATED. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-115218. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (LT WING LE SLAT) · airframe 52,369 hrs · 11,713 cycles

LEFT WING, NR 3 LEADING EDGE SLAT I/B SUPPORT FITTING FOUND CORROSION. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-115218. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (LT WING LE SLAT) · airframe 52,369 hrs · 11,713 cycles

LEFT WING, NR 3 LEADING EDGE SLAT MIDDLE SUPPORT FITTING FOUND CORROSION. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-115218, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LINK — CORRODED (LT WING LE SLAT) · airframe 52,369 hrs · 11,713 cycles

LEFT WING, NR 3 LEADING EDGE SLAT O/B TRACK LINK FOUND CORROSION. 10-24-07 REPAIR CARRIED AS PER FEDEX EA 1-5740-115219. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: TRUNNION — CRACKED (FUSELAGE) · airframe 52,369 hrs · 11,713 cycles

FASTENER HOLE FOUND CRACK AT 3 O'CLOCK POSITION AT NOSE LANDING GEAR LEFT TRUNNION FITTING LOWER LONGERON. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-115207, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 52,369 hrs · 11,713 cycles

CRACK INDICATIONS REVEALED FASTENER HOLES AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT EDGE. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115214, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 52,369 hrs · 11,713 cycles

CRACK INDICATIONS REVEALED FASTENER HOLES AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT EDGE. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115213. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 52,369 hrs · 11,713 cycles

RIGHT WING LEADING EDGE SLAT NR 6 OUTBOARD SLAT TRACK CUTOUT, SLAT TRACK NR 14, FOUND CRACK AT CORNER EDGE. 10-24-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 52,369 hrs · 11,713 cycles

LEFT WING, NR 5 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT LOWER EDGE FOUND CRACK. 10-24-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 52,369 hrs · 11,713 cycles

FASTENER HOLE FOUND CRACK AT 3 O'CLOCK POSITION AT NOSE LANDING GEAR RIGHT TRUNNION FITTING LOWER LONGERON. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-115206. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 52,369 hrs · 11,713 cycles

RIGHT WING LEADING EDGE SLAT NR 6 INBOARD SLAT TRACK CUTOUT (SLAT TRACK NR 12), FOUND CRACK AT CORNER EDGE. 10-24-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 .

Part: FITTING — DAMAGED (ZONE 700) · airframe 52,369 hrs · 11,713 cycles

NOSE LANDING GEAR RIGHT SIDE LOAD FITTING, FOUND AREA HOLE ELONGATED. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-115220, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 52,369 hrs · 11,713 cycles

NOSE LANDING GEAR MOUNTING LEFT TRUNNION FITTING FOUND WITH CRACK. 10-24-07 REPAIR CARRIED OUT AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS AS PER SRM 53- 40-00 FIGURE 23 VOLUME I.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 52,369 hrs · 11,713 cycles

FOUND NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 10-24-07 REPAIR CARRIED OUT AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS AS PER SRM 53-40-00 FIGURE 23 VOLUME I.

Part: STRUCTURE — CRACKED (ZONE 500) · airframe 52,369 hrs · 11,713 cycles

LEFT WING, NR 3 LEADING EDGE SLAT TELESCOPING DUCT CUTOUT OUTBOARD CORNER FOUND CRACK. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115224, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: CONTROL UNIT — FAILED (EMERGENCY POWER) · airframe 51,108 hrs · 11,458 cycles

AT APPROX 00:00Z GOT A MASTER WARNING LT W/A LEVEL 1 EMERGENCY POWER ON ALERT. COMPLIED W/QRH. SELECTED EMERGENCY POWER SWITCH TO OFF. GOT LVL 1 L EMERGENCY AC BUSS ALERT. SELECTED EMERGENCY POWER SWITCH BACK TO ARM , STILL HAD EMERGENCY POWER ON LEVEL ONE ALERT. CONSULTED W/GOC AND MOCC VIA SAT. BATTERY VOLT NOW DOWN TO 24V -51. WHEN VOLT DROPPED TO 22V (AMBER) DEPLOYED ADG IN ELEC BATTERY CHARGED UP TO 32V, ELECTED TO DIVERT SEA. ON NEXT POWER UP, EMERGENCY POWER TEST FAILED. REF WDM 24-61-11, REMOVED AND REPLACED LEFT EMERGENCY CONTROL RELAY (R2-17) PER SMP. REF AMM 24-24-00-5 AND EPCU R-T-S REF AMM 24-08-01-5, ALL TEST PASSED AND CHECKED NORMAL. DID NOT DUPLICATE FAULT, FINAL FIX REMOVED AND

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

RIGHT CABIN SEAT TRACK AT APPROX STA Y= 1521, X= -8.5 SEAT TRACK SLOT CHANNEL BASE AREA FOUND CORRODED. RIGHT CABIN SEAT TRACK AT APPROX STA Y= 1521, X= -8.5 CARRIED OUT. REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

RIGHT CABIN SEAT TRACK AT APPROX STA Y= 1561, X= -75.25 SUPPORT FLANGE FOUND CORRODED. RIGHT CABIN SEAT TRACK AT APPROX STA Y= 1561, X= -75.25 CARRIED OUT. REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 3. REFER TO SNRM N00759 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

AFT CARGO COMPARTMENT, FRAME STA 1841 WEB PUNCTURED AT LONGERON 42L. AFT CARGO COMPARTMENT, FRAME STA 1841 WEB AT LONGERON 42L CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5350-99693, TITLE: FUSELAGE, AFT CARGO DOOR JAMB LOWER BEAM CRACK REPAIR. REPAIR IS CLASSIFIED MINOR PER GMM 6-2-100.

Part: FITTING — DAMAGED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RIGHT HAND WING STA XORS 819 STRINGER 9, WHILE CARRYING OUT STRINGER END REPAIR FOUND CLIP P/N: ARB7192-502 UNABLE TO INSTALL. COMPLIED WITH FEDEX E.A. 1-5720-99686, REPAIR IS CLASSIFIED MINOR PER GMM 6-2-100.

Part: FITTING — DAMAGED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT HAND WING STA XORS 819 STRINGER 9, WHILE CARRYING OUT STRINGER END REPAIR FOUND CLIP P/N: ARB7192-501, UNABLE TO INSTALL. COMPLIED WITH FEDEX EA 1-5720-99685,

Part: SKIN — CHAFED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RIGHT HAND WING - FORWARD FIXED LEADING EDGE SKIN BETWEEN STA XORS 690 TO XORS 723 FOUND WITH SEVERAL CHAFED MARKS. REPAIRED AS PER SRM 57-10-00 FIGURE 15 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

RIGHT HAND CABIN SEAT TRACK AT APPROX STA Y= 1841, X= -75.25 SUPPORT FLANGE FOUND CORRODED. RIGHT HAND CABIN SEAT TRACK AT APPROX STA Y= 1841, X= -75.25 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 5 VOLUME I. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT HAND WING - UPPER SURFACE FORWARD FIXED LEADING EDGE AT APPROX STA XORS 625 FOUND 01 EA HI-LOK SKIN AREA CORRODED. CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5730-99689. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT HAND WING REAR SPAR UPPER CAP AT STA XORS 780 TO XORS 801 FOUND WITH CORROSION. REPAIRED AS PER FEDEX E.A. 1-5710-99688. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT HAND WING REAR SPAR UPPER CAP STA XORS 670 TO XORS 708 FOUND WITH CORROSION. REPAIRED AS PER FEDEX E.A. 1-5710-99688. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (T/E FLAP) · airframe 47,863 hrs · 10,773 cycles

RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE FOUND DENTED. REPAIRED AS PER SRM 57-10-00 VOLUME I FIGURE 34. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

RIGHT FUSELAGE CENTER WING BARREL AREA FOUND LONGERON 28R FOUND WITH CORROSION AT APPROX STA 1305.205. COMPLIED WITH FEDEX E.A. 1-5310-99687.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

LEFT CABIN SEAT TRACK AT APPROX STA Y= 615, X= 8.5 CHANNEL SLOT FOUND WORN. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

RIGHT CABIN SEAT TRACK AT APPROX STA Y= 1581, X= -75.25 SUPPORT FLANGE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

LEFT CABIN SEAT TRACK AT APPROX STA Y= 615, X= 47.5 CHANNEL SLOT FOUND WORN.CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

LEFT FUSELAGE CENTER WING BARREL AREA FOUND LONGERON 28L FOUND WITH CORROSION AT APPROX STA 1273. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: SUPPORT — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LT WING, LEADING EDGE CAVITY AT APPROX STA XORS 481, RIBS SUPPORT FOUND CRACKED. LEADING EDGE CAVITY AT APPROX. STA XORS 481, CRACKED RIB SUPPORT REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RT WING, LEADING EDGE CAVITY AT APPROX STA XORS 626, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5730-99676

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,863 hrs · 10,773 cycles

RT CABIN LATERAL FLOOR PANEL SUPPORT AT APPROX STA Y=1821 / X= - 107.25 TO -75.25 FOUND CORRODED AT SEVERAL FASTENER HOLE AREAS. REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. THIS REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RIGHT HAND, LEADING EDGE CAVITY AT APPROX STA XORS 534, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. COMPLIED WITH FEDEX E.A. #1-5730-99671

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RIGHT WING, LEADING EDGE CAVITY AT APPROX STA XORS 632, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. COMPLIED WITH FEDEX E.A. 1-5730-99676

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT WING, LEADING EDGE CAVITY AT APPROX STA XORS 659, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5730-99681

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LT WING, LEADING EDGE CAVITY AT APPROX STA XORS 565, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5730-99682.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RT WING, LEADING EDGE CAVITY AT APPROX STA XORS 649, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. COMPLIED WITH FEDEX E.A. 1-5730-99676

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LT WING, LEADING EDGE CAVITY AT APPROX STA XORS 534, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. #1-5730-99683

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LT WING, LEADING EDGE CAVITY AT APPROX STA XORS 774, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. #1-5730-99678

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT WING, LEADING EDGE CAVITY AT APPROX STA XORS 549, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. #1-5730-99683.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LT WING, LEADING EDGE CAVITY AT APPROX STA XORS 595, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5730-99682.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

FOUND LEFT WING, LEADING EDGE CAVITY AT APPROX STA XORS 526, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5730-99683.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RT WING, LEADING EDGE CAVITY AT APPROX STA XORS 482, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. COMPLIED WITH FEDEX E.A. #1-5730-99670

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LT WING, LEADING EDGE CAVITY AT APPROX STA XORS 625, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5730-99681.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LT WING, LEADING EDGE CAVITY AT APPROX STA XORS 655, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5730-99681.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RIGHT WING, LEADING EDGE CAVITY AT APPROX STA XORS 507, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. COMPLIED WITH FEDEX E.A. #1-5730-99671

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

FOUND RIGHT WING, LEADING EDGE CAVITY AT APPROX STA XORS 550, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. COMPLIED WITH FEDEX E.A. 1-5730-99671.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RT WING, LEADING EDGE CAVITY AT APPROX STA XORS 527, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. COMPLIED WITH FEDEX E.A. 1-5730-99671, TITLE: WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. THIS REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RIGHT WING, LEADING EDGE CAVITY AT APPROX STA XORS 524, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. COMPLIED WITH FEDEX E.A. #1-5730-99671

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT WING, LEADING EDGE CAVITY AT APPROX STA XORS 541, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. #1-5730-99683.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

RT WING, LEADING EDGE CAVITY AT APPROX STA XORS 540, BEADED DOUBLER FOUND CRACKED AT FASTENER HOLES. REPAIR CARRIED OUT AS PER FEDEX E.A. #1-5730-99671

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LT WING, LEADING EDGE CAVITY AT APPROX STA XORS 440, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. #1-5730-99680.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT WING, LEADING EDGE CAVITY AT APPROX STA XORS 649, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5730-99681, TITLE: WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — SCRATCHED (L/E SLAT) · airframe 47,863 hrs · 10,773 cycles

LEFT WING, NR 2 SLAT INNER SURFACE FOUND WITH SCRATCH MARK. REPAIRED AS PER SRM 57 -10-00 FIGURE 10 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT WING, LEADING EDGE CAVITY AT APPROX STA XORS 689, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. #1-5730-99679

Part: DOUBLER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

LEFT WING, LEADING EDGE CAVITY AT APPROX STA XORS 588, BEADED DOUBLER FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5730-99682.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 47,863 hrs · 10,773 cycles

RIGHT CABIN SEAT TRACK AT APPROX STA Y= 950 TO 970 AND X= -47.50 FOUND WITH NUT CHANNEL EDGE CHIPPED OFF AT FEW PLACES. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,863 hrs · 10,773 cycles

RIGHT CABIN SEAT TRACK AT APPROX STA Y= 1561 AND 1861, X= -75.25 SUPPORT FLANGE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 10 AT APPROX. XORS 760.

Part: STRINGER — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 13 AT APPROX XORS 577. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 41 AT APPROX XORS 685. COMPLIED WITH FEDEX E.A. 1-5720-99663. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF STRINGER 9 AT APPROX XORS 819. REPAIRED AS PER SRM 57-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF STRINGER 10 AT APPROX XORS 760. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 9 AT APPROX XORS 819. REPAIRED AS PER SRM 57-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT HAND WING TANK AT THE END OF STRINGER 10 AT APPROX XORS 760. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF STRINGER 14 AT APPROX XORS 521. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF STRINGER 12 AT APPROX XORS 642. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 47,863 hrs · 10,773 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF STRINGER 11 AT APPROX XORS 704. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 879 TO Y= 929, X= -47.50 FOUND WORN. MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 879 TO Y= 929, X= -47.50 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I.

Part: VANE — DELAMINATED (ZONE 500) · airframe 42,837 hrs · 9,749 cycles

LT HAND WING, INBOARD FLAP VANE LOWER CENTER SKIN FOUND DELAMINATED WHICH MEASURES 36.0 INCHES IN LENGTH AND 14.0 INCHES IN WIDTH AT STA 216.300 - 279.345 DELAMINATION AT LEFT HAND WING, INBOARD FLAP VANE LOWER CENTER SKIN AT STA 216.300 - 279.345 REPAIRED PER FEDEX EA 1-5750-81678.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 755 TO Y= 840, X= 47.50 FOUND WORN.CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: CHANNEL — CRACKED (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, FLOOR PANEL SUPPORT, J-CHANNEL UPPER SURFACE AT STA Y= 1381 BETWEEN X= 8.50 AND X= -8.50 FOUND CORRODED. NEW J-CHANNEL FABRICATED PER DRAWING NR.: AEA7392 AND INSTALLED PER SRM 51-35-01 VOLUME I.

Part: SKIN — CRACKED (ZONE 300) · airframe 42,837 hrs · 9,749 cycles

AFT FUSELAGE, RT SIDE BEDROOM COMPARTMENT, FORWARD MOST TOP FITTING EDGE FOUND WITH CRACKED. CRACKED FITTING REMOVED PER SRM 51-33-01 VOLUME II. NEW FITTING FABRICATED PER DOUGLAS DRAWING NR: AJC7140 AND INSTALLED PER SRM 51-33-01 VOLUME II

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK HORIZONTAL FLANGE UPPER SURFACE AT STA Y= 5-11 TO Y= 5-33, X= 75.25 FOUND FLOOR PANEL MOUNTING FOUND CORRODED AND WITH SHORT EDGE DISTANCE. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: LONGERON — DENTED (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK, LONGERON 18L AT STA Y= 535 FOUND WITH DENT. FOUND MOUNTING FASTENER LOOSE LONGERON 18L AT STA Y= 535 - LOOSE FASTENERS REMOVED AND REPLACED PER SRM 51-31-01 VOLUME I

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1781 TO Y= 1801, X= 47.50 FOUND CORRODED. REPAIRED IAW SRM 51-2101.

Part: STIFFENER — CORRODED (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK, CENTER TANK, REAR SPAR UPPER CHORD ATTACHED STIFFENER FOUND CORRODED AT STA Y= 1371, X= 117 FORWARD OF SLANT PANEL. MAIN DECK, CENTER TANK, CORROSION ON REAR SPAR UPPER CHORD AT STA Y= 1371, X= 117. REMOVED AND REPROTECTED PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS= 0.180 INCH, MATERIAL REMOVED= 0.031 INCH, REMAINING THICKNESS= 0.149, WITHIN LIMITS PER SRM 57-00-01 VOLUME 1.

Part: SPAR CAP — CORRODED (ZONE 600) · airframe 42,837 hrs · 9,749 cycles

RT WING, REAR SPAR UPPER CAP AT STA 1044 FOUND WITH CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-81590

Part: SKIN — CORRODED (ZONE 600) · airframe 42,837 hrs · 9,749 cycles

RT WING, CORROSION FOUND BETWEEN XOS= 680 TO XOS= 725 UPPER SURFACE SPAR AREA. COMPLIED WITH FEDEX EA 1-5710-81591, CORROSION REMOVAL AND REPAIR. CORROSION REMOVED AT XORS STA 714 AS PER SRM 51-21-01 VOL. II FOUND WITHIN LIMITS AS PER SRM 57-10-00 FIG. 32 VOL. I.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1099 TO Y= 1129, X= 27.50V FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK, SEAT TRACK HORIZONTAL FLANGE UPPER SURFACE AT STA Y= 5-11 TO Y= 5-53, X= -75.25 FOUND FLOOR PANEL MOUNTING HOLE SHORT OF EDGE MARGIN. REPAIRED IAW SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 710 TO Y= 715, X= -8.50 SCALLOP FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 42,837 hrs · 9,749 cycles

LT WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 FOUND CORRODED. REPAIR CARRIED OUT AT LEFT HAND WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 AS PER FEDEX EA 1-5710-81589, FOUND EXCEEDED LIMITS AS PER SRM 57-20-00 VOLUME I, FIGURE 16.

Part: SKIN — DENTED (ZONE 500) · airframe 42,837 hrs · 9,749 cycles

INNER LT WING LOWER SKIN AT XORS= 85 FOUND WITH 3.5 INCH DENT. COMPLIED WITH FEDEX EA 1-5710-81592.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1841 TO Y= 1871, X= - 8.50 FOUND CORRODED. REMOVED AND REPAIRED PER SRM SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1341 TO Y= 1401, X= - 47.50 FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1501 TO Y= 5-11, X= 8.50 FOUND WORN. SPLICED AND TRIMMED PER SRM 51-33-01 VOLUME II; AND REPAIRED PER SRM 53-70- 00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK, SEAT TRACK BETWEEN STA Y= 1219 TO Y= 1239, X= -47.50 FOUND WORN. SPLICED AND REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: THRUST REVERSER — CRACKED (ZONE 400) · airframe 42,837 hrs · 9,749 cycles

NR 3 ENGINE, LT THRUST REVERSER, TRANSLATING COWL, UPPER TRACK, MOST AFT END FOUND WITH CRACKED. THRUST REVERSER P/N 683L220G04, S/N R591-090 NR 3 ENGINE, LT THRUST REVERSER REMOVED AND REPLACED PER AMM 78-33-01-4. THRUST REVERSER DOOR ADJUSTMENT AND CHECK CARRIED OUT PER AMM 78-33-01-700-807. FUCTIONAL TEST CARRIED OUT PER AMM 78-30-00-700-801. COMPLIED WITH ROUTINE WORKCARD NOS.: 78T3003-L AND 78T3903-L

Part: THRUST REVERSER — CRACKED (ZONE 400) · airframe 42,837 hrs · 9,749 cycles

NR 3 ENGINE, RT THRUST REVERSER, TRANSLATING COWL, UPPER TRACK, MOST AFT END FOUND WITH CRACKED. THRUST REVERSER P/N 683L221G04, S/N R592-084. NR 3 ENGINE, RT THRUST REVERSER REMOVED AND REPLACED PER AMM 78-33-01-4. THRUST REVERSER DOOR ADJUSTMENT AND CHECK PER AMM 78-33-01-700-807. FUCTIONAL TEST CARRIED OUT PER AMM 78-30-00-700-801. COMPLIED WITH ROUTINE WORKCARD NOS.: 78T3003-R AND 78T3903-R

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 42,837 hrs · 9,749 cycles

MAIN DECK CARGO, SEAT TRACK AT STA Y= 791.75 TO Y= 859, X= 8.5 DAMAGED AT FLANGED AREA. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1

Part: SLAT TRACK — CRACKED (LT WING) · airframe 42,837 hrs · 9,749 cycles

LEFT HAND WING, SLAT TRACK NR 16 INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-33-01 AND SRM 51-35-01. NR 16 SLAT TRACK ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-80-00-2. OUTBOARD SLAT OPERATIONAL TEST CARRIED OUT PER AMM 27-80-00-5.

Part: CONTROL UNIT — MALFUNCTIONED (FUEL SYSTEM) · airframe 41,847 hrs · 9,543 cycles

IN CRUISE FLT, AT FL 330, AT APPROX TAKEOFF PLUS FOUR HOURS, RECEIVED (LEVEL 1 TANK 2 FUEL QTY LO) ALERT S.D. FUEL READINGS WERE: 1- 900 2- 0 3-900 AUX- 900 TAIL- 12900. FUEL INDICATIONS AND USAGE TO THAT POINT HAD BEEN NORMAL. FSC WAS IN AUTO, ALSO GOT LEVEL 1 ALERT (FUELMANF DRAIN) AND DRAIN WAS ILLUMINATED OVERHEAD IN THE GUARDED MANF SWITCH. GOT A LEVEL 2 FUEL QTY/USED CHECK ALERT AS WELL AS LEVEL 2 FUEL QTY FAULT ALERT CHECKLIST FOR FUEL MANF DRAIN DIRECTS CREW NOT TO PRESSURIZE CROSSFEED MANIFOLD AS A RESULT WE KEPT FSC IN AUTO AND DIVERTED TO KMSP. REMOVED AND REPLACED S.E.M AND FUEL QUAN. DATA CONTROL UNIT IAW M/M. SYS OP'S CHECKS NORMAL AT THIS TIME. OK TO CONTINUE.

Part: PITOT TUBE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 41,507 hrs · 9,472 cycles

ON DESCENT DURING APPROACH GOT IAS ON PFD AND SELECT ELEV FEEL MAN, LVL 2 ALERT. ALSO HAD WINDSHEAR FAIL DET ALERT ON STATUS PAGE. STANDBY A/S SHOWED F/O'S INDICATOR ACCURATE. CAPT'S 10 KNOTS SLOW. RAN READ TAB. B Y TOUCHDOWN, F/O'S INDICATOR READ 156 KNOTS, CAPTAINS READ 118 KNOTS IN YELLOW. FOLLOWED T/S PER FIM34-11-02 AND FOUND A/S TOLERANCE BET CAPT AND F/O BEYOND LIMIT REF FIG 103 TABLE. PHYSICALLY INSPECTED PITOT PROBES FOUND SMALL DEBRIS ON CAPT PROBE WHEN PURGED. REMOVED AND REPLACED CAPT PROBE & NR 1 CADC PER MM 34-16-01 AND MM 34-11-01. PERFORMED SYS TEST PER MM 34-16-01-5, SATISFACTORY. COMPLIED W/ MTSI 34-10/9654 STEPS 1-6, SATISFACTORY.

Part: PITOT HEAD — OBSTRUCTED (CAPTAIN'S) · airframe 41,505 hrs · 9,470 cycles

ON DESCENT DURING APPROACH GOT IAS ON PFD AND SELECT ELEV FEEL MAN LVL 2 ALERT. ALSO HAD WINDSHEAR FAIL DET ALERT ON STATUS PAGE. STANDBY A/S SHOWED F/O'S INDICATOR ACCURATE. CAPT'S 10 KNOTS SLOW. RAN READ TAB. BY TOUCHDOWN, F/O'S INDICATOR READ 156 KNOTS, CAPTAINS READ 118 KNOTS IN YELLOW. FACT: NUMEROUS FAULTS ON FAULT REVIEW, ADC 1 & 2, FMC 1 & 2, ELEV LD FEEL ACT AND ELEV ACT RIB AND LOB. T/S PER FIM, FOUND A/S TOLERANCE BETWEEN CAPT AND F/O BEYOND LIMIT. FOUND SMALL DEBRIS IN CAPT PITOT PROBE. PURGED, REMOVED AND REPLACED CAPT PROBE & NR 1 CADC.

Part: SHIM — OUT OF POSITION (LT WING) · airframe 37,601 hrs · 8,599 cycles

LEFT WING ROOT- STRINGER NR 1 SHIM FOUND MIGRATED 0.3 INCH DOWN. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION.

Part: SHIM — OUT OF POSITION (RT WING) · airframe 37,601 hrs · 8,599 cycles

RIGHT WING ROOT UPPER SURFACE- STRINGER NR 1 SHIM FOUND SEPARATED INTO 2 VISIBLE PIECES AND EACH WITH MIGRATION OF: (1) 0.7 INCH FWD AND 0.5 INCH DOWN AND (2) 0.6 INCH DOWN. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION.

Part: SHIM — OUT OF POSITION (LT WING) · airframe 37,601 hrs · 8,599 cycles

LEFT WING ROOT- UPPER SURFACE- STRINGER NR 4 SHIM FOUND MIGRATED 0.6 INCH DOWN AND 0.4 INCH FWD. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION.

Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · airframe 37,601 hrs · 8,599 cycles

HORIZONTAL STAB RT AFT SPAR CAP NR 36R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STABILIZER AFT SPAR CAP NR 36R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69404 - STABILIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 36 RIGHT HAND SIDE.

Part: SHIM — OUT OF POSITION (LT WING) · airframe 37,601 hrs · 8,599 cycles

LEFT WING ROOT- UPPER SURFACE STRINGER NR 3 SHIM FOUND MIGRATED 0.7 INCH DOWN. PREVIOUS RECORD IS 0.5 INCH. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION.

Part: SKIN — CORRODED (ZONE 300) · airframe 37,601 hrs · 8,599 cycles

HORIZONTAL STAB RT UPPER CENTER PLANK NR 26R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STABILIZER RT UPPER CTR PLANK NR 26R FITTING REMOVED & REPLACED AS PER FEDEX EA 1-5510-69397 - STABILIZERS - HORIZONTAL STABILIZER - FITTING ALC8107-2 FABRICATION.

Part: FITTING — CORRODED (ZONE 600) · airframe 37,601 hrs · 8,599 cycles

RT WING O/B FLAP VANE- TEE FITTING NR 2 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 2 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71878,

Part: TEE FITTING — CORRODED (T/E FLAP) · airframe 37,601 hrs · 8,599 cycles

RIGHT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71878, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RIGHT OUTBOARD FLAP NR 2, 3, 4 AND 5 VANE TO TRACK SUPPORT REWORK.

Part: FITTING — CORRODED (ZONE 600) · airframe 37,601 hrs · 8,599 cycles

RT WING O/B FLAP VANE- TEE FITTING NR 5 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 5 FROM INBOARD CORROSION IN HOLE, REPAIRED IAW EA 1-5750-71878.

Part: FITTING — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND WITH CORROSION IN HOLE. LT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71810, TITLE: WINGS TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP NR 3 AND NR 4 VANE TO TRACK SUPPORT REWORK.

Part: TEE FITTING — CORRODED (T/E FLAP) · airframe 37,601 hrs · 8,599 cycles

SNRM N1007 - RT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND WITH CORROSION IN HOLE. SNRM N1007 - RT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED IAW EA 1-5750-71878, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RT OUTBOARD FLAP NR 2, 3, 4 AND 5 VANE TO TRACK SUPPORT REWORK.

Part: FITTING — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND WITH CORROSION IN HOLE. LT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71810.

Part: BARREL NUT — CORRODED (ZONE 300) · airframe 37,601 hrs · 8,599 cycles

RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE REPAIR CARRIED- OUT AS PER FEDEX EA 1-5510-69279 - STABILIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 27 RIGHT HAND SIDE.

Part: SKIN — CORRODED (ZONE 300) · airframe 37,601 hrs · 8,599 cycles

RH HOR STAB UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69279 - STABILIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 27 RIGHT HAND SIDE.

Part: SPLICE — CRACKED (ZONE 100) · airframe 37,601 hrs · 8,599 cycles

CENTER CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 45L SPLICE FITTING FOUND CRACK. CENTER CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 45L SPLICE FITTING REMOVED & REPLACED AS PER SRM 51-33-01 VOL II.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,601 hrs · 8,599 cycles

RIGHT HORIZONTAL STABILIZER UPPER AFT PLANK NR 35R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-1-5000 LIMITATIONS. RIGHT HORIZONTAL STABILIZER UPPER AFT PLANK NR 35R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69402 - STABILIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 35 RIGHT HAND SIDE.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 37,601 hrs · 8,599 cycles

CTR CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 49L SPLICE FITTING FOUND CRACK. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II.

Part: HINGE — LOOSE (ZONE 600) · airframe 37,601 hrs · 8,599 cycles

SNRM N0934 - RT WING- O/B FLAP (FLAP SIDE) O/B HINGE O/B PIVOT HOLE AND I/B AND O/B ACTUATOR ATTACHMENT HOLES FOUND BUSHING LOOSE. ** S/D ** COMING

Part: SPLICE — CRACKED (FUSELAGE) · airframe 37,601 hrs · 8,599 cycles

CTR CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 46L SPLICE FITTING FOUND CRACK. CTR CARGO STA 5-113 THRU STA 1541 CRACK LONGERON 46L SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG A5A7114 AND SRM 51-33-01 VOL II.

Part: HINGE — CORRODED (RT WING) · airframe 37,601 hrs · 8,599 cycles

SNRM N0866 - RT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. CORRECTIVE ACTION: SNRM N0866 - RT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS IAW EA 1-5750-71806, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LT WING- O/B FLAP STOP BOLT SUPPORT ISLAND FOUND CRACKED. LT OUTBD FLAP STOP BOLT SUPPORT ISLAND REPAIRED AS PER FEDEX EA 1- 5750-69259 - WINGS - TRAILING EDGE FLAPS - LT OUTBOARD FLAP SECONDARY UP STOP REPAIR.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 37,601 hrs · 8,599 cycles

CTR CARGO LEFT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING FOUND CRACK. LEFT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 37,601 hrs · 8,599 cycles

CTR CARGO RT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING FOUND CRACK. CTR CARGO RT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING REMOVED AS PER SRM 51-33-01 VOL II. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 37,601 hrs · 8,599 cycles

CTR CARGO RT TUNNEL STA 5-123 LONGERON 38 SPLICE FITTING FOUND CRACK. CTR CARGO RT TUNNEL STA 5-123 LONGERON 38 SPLICE FITTING FABRICATED AS PER DWG A5A7114 & INSTALLED AS PER SRM 51-33-01 VOL II.

Part: HINGE — CORRODED (RT WING) · airframe 37,601 hrs · 8,599 cycles

RIGHT WING- I/B FLAP (WING SIDE) O/B HINGE PIVOT LUG I/B SURFACE CORRODED. RIGHT WING- I/B FLAP (WING SIDE) O/B HINGE PIVOT LUG I/B SURFACE REPAIRED AS PER FEDEX AE 1-5750-71880, TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES- RT INBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LT WING I/B FLAP (WING SIDE) O/B HINGE PIVOT BORE AND I/B LUG SURFACE CORRODED. LT WING I/B FLAP (WING SIDE) O/B HINGE PIVOT BORE AND I/B LUG SURFACE REPAIRED AS PER FEDEX EA 1-5750-71881 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBD FLAP OUTBD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. LT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-71807.

Part: HINGE — LOOSE (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LT WING O/B FLAP (FLAP SIDE) O/B HINGE I/B AND O/B PIVOT HOLES BUSHING FOUND LOOSE. LEFT O/B FLAP (FLAP SIDE) O/B HINGE I/B AND O/B PIVOT HOLES REPAIRED AS PER FEDEX EA 1-5750-69278 - WINGS TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (LT WING) · airframe 37,601 hrs · 8,599 cycles

LEFT O/B FLAP (WING SIDE) I/B HINGE LOWER REAR SPAR MOUNT O/B HOLE AND AFT NUT ATTACHMENT SURFACE CORRODED. LEFT O/B FLAP (WING SIDE) I/B HINGE LOWER REAR SPAR MOUNT O/B HOLE AND AFT NUT ATTACHMENT SURFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 AND DRAWING ARC0502 SHT 4.

Part: HINGE — CORRODED (LT WING) · airframe 37,601 hrs · 8,599 cycles

LEFT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. LEFT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-69406, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- LEFT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,601 hrs · 8,599 cycles

RT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. RT WING O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-69405 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBD FLAP INBD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,601 hrs · 8,599 cycles

RIGHT O/B FLAP (FLAP SIDE) I/B HINGE I/B PIVOT HOLE AND I/B PIVOT LUG INNER AND OUTER SURFACES FOUND CORRODED. RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACES REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LT I/B FLAP (FLAP SIDE) - O/B HINGE O/B PIVOT HOLE AND O/B PIVOT LUG INNER AND OUTER SURFACES CORRODED. LT I/B FLAP (FLAP SIDE)- O/B HINGE O/B PIVOT HOLE AND O/B PIVOT LUG INNER AND OUTER SURFACES REPAIRED AS PER FEDEX EA 1-5750-69256 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT INBD FLAP HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LEFT O/B FLAP (FLAP SIDE) - I/B HINGE O/B PIVOT HOLE CORRODED. SNRM N0463 - LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE O/B PIVOT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LEFT O/B FLAP (FLAP SIDE) - I/B HINGE BRACKET I/B ACTUATOR ATTACHMENT HOLE FOUND CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE BRACKET I/B ACTUATOR ATTACHMENT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,601 hrs · 8,599 cycles

RIGHT O/B FLAP (FLAP SIDE) I/B HINGE I/B AND O/B ACTUATOR HOLES CORRODED. RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE I/B AND O/B ACTUATOR HOLES REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,601 hrs · 8,599 cycles

RIGHT WING - O/B FLAP (FLAP SIDE) O/B HINGE I/B PIVOT HOLE AND I/B PIVOT LUG INNER AND OUTER LUG SURFACES FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,601 hrs · 8,599 cycles

RIGHT I/B FLAP (FLAP SIDE) - O/B HINGE O/B PIVOT HOLE AND LUG INNER AND OUTER SURFACE CORRODED. RT I/B FLAP (FLAP SIDE)- O/B HINGE, O/B PIVOT HOLE AND LUG INNER AND OUTER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69257 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RH INBD FLAP HINGE BRACKET ASSY REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,601 hrs · 8,599 cycles

RIGHT I/B FLAP (FLAP SIDE) - O/B HINGE I/B PIVOT HOLE AND LUG INNER SURFACE CORRODED. RT I/B FLAP (FLAP SIDE)- O/B HINGE I/B PIVOT HOLE AND LUG INNER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69257 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBD FLAP HINGE BRACKET ASSY REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LT O/B FLAP (FLAP SIDE) - I/B HINGE I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACE CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE- I/B PIVOT HOLE AND I/B LUG INNER AND OUTER SURFACE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS - TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,601 hrs · 8,599 cycles

RIGHT WING- O/B FLAP (FLAP SIDE) I/B HINGE O/B PIVOT HOLE CORRODED. RIGHT WING- O/B FLAP (FLAP SIDE) I/B HINGE O/B PIVOT HOLE REPAIRED AS PER FEDEX EA 1-5750-69277, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RIGHT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,601 hrs · 8,599 cycles

LEFT O/B FLAP (FLAP SIDE) - I/B HINGE O/B ACTUATOR ATTACHMENT HOLE CORRODED. LEFT WING O/B FLAP (FLAP SIDE) - I/B HINGE O/B ACTUATOR ATTACHMENT HOLE REPAIRED AS PER FEDEX EA 1-5750-69278, TITLE: WINGS - TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: SKIN — BULGED (ZONE 600) · airframe 37,601 hrs · 8,599 cycles

RT WING PANEL AT STA XORS 1042 REAR SPAR SKIN BULGE. RT WING PANEL AT STA XORS 1042 REAR SPAR SKIN BULGE REPAIRED AS PER FEDEX EA 1-5720-69399 - WINGS - OUTER WING - RH REAR SPAR/TRAILING EDGE CORROSION REWORK.

Part: HINGE FITTING — CRACKED (T/E FLAP) · airframe 37,601 hrs · 8,599 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD SIDE LINK FOUND CRACKED. CRACKED O/B SIDE LINK FITTING OF LEFT WING O/B FLAP I/B HINGE FITTING REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-33-01 VOL II.

Part: FASTENER — BROKEN (CENTER WING) · airframe 33,450 hrs · 7,658 cycles

DURING B-CHECK FOUND 1 TAPER LOCK FASTENER BROKEN ON REAR SPAR LOWER CAP OF CENTER WING REF EA 1-5314-64689. R/R FASTENER PER E.A.

Part: AILERON — ILLUMINATED · airframe 32,522 hrs · 7,453 cycles

02-67 AILERON DEFLECT DISAGREE ALERT CAME ON IN FLT. DIVERT TO RCTP DUE TO INCREASE FUEL BURN. ** S/D ** COMING

Part: WIRE HARNESS — BROKEN (NR 1 GENERATOR) · airframe 32,448 hrs · 7,437 cycles

NR 1 ENG GENERATOR FEEDER CABLE N012-2-00B (AL) BROKEN NEAR LT WING ROOT FEED THROUGH. REMOVED AND REPLACED NR 1 ENG GEN FEEDER LINE CABLE AND CLAMPS PER MM 24-22-03-5.

Part: WIRE HARNESS — BROKEN (NR 3 GENERATOR) · airframe 32,448 hrs · 7,437 cycles

NR 3 ENG GENERATOR FEEDER CABLE N117-1-00A (AL) NEAR TERMINAL STRIP S3-385R BROKEN. REMOVED AND REPLACED NR 3 ENG GEN FEEDER LINE CABLE AND CLAMPS PER MM 24-22-03-5.

Part: RIB — CRACKED (RT WING) · airframe 32,448 hrs · 7,437 cycles

RIGHT WING L/E COMPT RIB FOUND CRACKED AT STA XORS 694 APPROX 3 INCHES. REMOVED AND REPLACED RIB PER DWG ARB 2922.

Part: BEARING — OUT OF POSITION (L/E SLAT)

RT WING O/B SLAT DRIVE MECHANISM FWD BEARING MIGRATED.

Part: BEARING — OUT OF POSITION (L/E SLAT) · airframe 32,448 hrs · 7,437 cycles

RT WING O/B SLAT DRIVE MECHANISM FWD BEARING MIGRATED. REMOVED AND REPLACED WING OUTBOARD SLAT DRIVE MECH PER EA 1-2780-60721.

Part: SPAR — CORRODED (LT WING) · airframe 32,448 hrs · 7,437 cycles

LT WING UPPER FIXED T/E PANEL BULGE AT BS XOR 772.5 (O/B OF NR 5 SPOILER). REMOVED AND REPLACED OUTER WING REAR SPAR/TRAILING EDGE PER EA 1-5720-60680.

Part: SPAR — BULGED (LT WING) · airframe 32,448 hrs · 7,437 cycles

LT WING UPPER FIXED T/E PANEL BULGED AT BS XOR 674 (CTR OF NR 4 SPOILER). REMOVED AND REPLACED OUTER WING REAR SPAR/TRAILING EDGE PER EA 1-5720-60680.

Part: ACTUATOR — FAILED · airframe 31,483 hrs · 7,202 cycles

01-356 ON T/O UPON FLAP RETRACTION RECEIVED LEVEL 2 DEFLECTED AILERON DISAGREE ALERT. ** S/D ** COMING

Part: FLAP — VIBRATION (WING)

VIBRATION ON SELECTING FLAPS TO 50 DEG. NO PROBLEMS FOUND ON FLT CONTROL INSP. AC OK FOR SERVICE.

Part: O-RING — BROKEN (HYD SYSTEM)

IN CR HYD 1 OFF ILLUM. REMOVED AND REPLACED BROKEN O-RING PER SMP. LEAK CK OK.

Part: O-RING — LEAKING (HYD SYSTEM)

HYD SYS NR 1 FAIL 1 HR INTO FLT FOUND LEAKS FROM HOL STAB CONTROL VALVE NR 2 SYS NR 1 PRESS LINE ON VALVE FITTING. REMOVED AND REPLACED DELAMINATED O-RING OF FITTING.

Part: FILTER — MALFUNCTIONED (NR 2 ENGINE FUEL)

RECEIVED TANK 2 FWD PMP LO ALERT. ACCOMPLISH CKLIST. NR 2 ENG FLAMED OUT AFTERWARDS. FOR PRECAUTION REMOVED AND REPLACED NR 2 ENG FUEL FILTER AND NO LEAK PER 73-11-04-6. FUEL SHROUD DRAIN FOUND NO LEAK PER MM 28-25-00-6.

Part: EPCU — FAULTY

00-347 ON DEPART HAD MOMENTARY TOTAL ELECTRICAL PWR FAILURE. R&R EPCU PER MM 24-08-01-4, 24-20-17.

Part: WINDOW — CRACKED (COCKPIT)

00-25 - FO SLIDING WINDOW OUTER PANE OBSERVED CRACKING IN OUTER PANE, CRACK PROGRESSING APPROX 1 PER 5 MIN AT FL 330. CONTACTED ANC MAINT AND ADVISED TO RETURN TO PANC. REMOVED AND REPLACED RT CLEAR VIEW WINDOW PER MM 56-12-01-4. WINDOW OPS CK GOOD. REMOVED AND REPLACED WINDSHIELD AND WINDOW DEF OF CONTROLLER, PER MM 30-42-01-4. OPS CK GOOD. AC OK FOR SERVICE.

Part: SEAT TRACK — CRACKED (BS 635 - 755)

SNRM 263, 264, 265, 266, 268 UPPER CARGO COMPT 263-LT BS 635, LBL 28. 264- LT BS 635, LBS 48. 265- LT BS 755, LBL 28. 266- LT BS 755, LBL 48. 268- RT BS 637, RBL 48, SEAT TRACKS CRACKED. SEAT TRACKS REPAIRED AS PER SRM 53-70-00.

Part: SEAT TRACK — CRACKED (BS 970)

SNRM 159 - MAIN DECK - SEAT TRACK FOUND CRACKED AT BS 970.5 X = 47.5 RT CRACK LENGTH APPROX 2 INCHES. REPAIRED SEAT TRACK PER SRM 53-70-00 VOL 1.

Part: FIRE WIRE — FAILED (NR 2 ENGINE)

SHUTDOWN NR 2 ENG IN FLT DUE TO FIRE WARN IND, DISCHARGED FIRE-X BOTTLE. REMOVED AND REPLACED HARNESSES 420804-0000, 420896-0000, & 224W9727-517. ALSO, REPLACED FIRE-X BOTTLE (P/N 895564-10. RAN ENG, CHECK GOOD.

Part: FIRE LOOP — FAILED (NR 2 ENGINE)

99-196- WHILE CLIMB, ENG NR 2 FIRE ALERT WARNING ACTIVATED. ENG SHUTDOWN IAW FLT MANUAL. NR 2 FIRE AGENT DISCHARGED. REMOVED AND REPLACED UP RT FIRE DET ASSY A, HARNESS OF DH4 TO DH23, DH22 TO DH7, AND DH7 TO DH8 FOR MAINT PREVENTION PER MD-11. RUN ENG WITH HI PWR ALL COND NML.

Part: KEEL BEAM — DAMAGED (BS 1401-1451)

UNDERWING KEEL STRUCTURE WAS DAMAGED IN LAND INCIDENT AND HAS BEEN OPER UNDER REPETITIVE INSP PER EA 1-5330-33495 AND 1-5330-39772 BS 1401 TO 1451 Z-60 TO Z-110. *S/D* COMPLIED WITH EA 1-5310-40320 FUSELAGE - UNDERWING KEEL STRUCTURE REPAIR.

Part: SKIN — DAMAGED (BS 623)

A/C SUSTAINED DAMAGE TO FUSELAGE SKIN DURING LANDING INCIDENT BS 623 FROM L36 TO L48 LT. *S/D* COMPLIED WITH EA 1-5330-40318 FUSELAGE, SKINS-SPLICE REPAIR OF SKIN AT BS 623, L36-L48, LT AND RT.

Part: BULKHEAD — DAMAGED (BS 595)

FWD FUSELAGE WAS DAMAGED IN LAND INCIDENT AND HAS BEEN OPER UNDER REPETITIVE INSP PER EA 1-5330-39764. BULKHEAD AT BS 595 WAS STRESSED. *S/D* COMPLIED WITH EA 1-5310-40319- FUSELAGE, MAIN FRAME - REPAIR OF BS 595 PRESSURE BULKHEAD.

Part: WIRE — FAILED (LANDING GEAR)

AFTER TAKEOFF AND GEAR RETRACTION HAD 4 RED GEAR UNSAFE LIGHTS. FOLLOWED EMERGENCY PROCEDURES THAT HAD US CYCLE GEAR SEVERAL TIMES WITH NO SUCCESS. GEAR EXTENDS NORMALLY. VERIFIED PROBLEM WAS WITH INDICATION. WHILE ON GROUND INDICATION DID NOT SHIFT FROM GREEN TO RED WITH GEAR HANDLE PULLED. FOUND WIRE HARNESS INTERFERING WITH GEAR HANDLE SWITCH OPERATION. SECURED WIRING AWAY FROM HANDLE SWITCH AND HANDLE SWITCH OPERATED NORMAL.

Part: CONTROL MODULE — MALFUNCTIONED (LE SLATS)

GOT A SLATS DISAGREE WHEN SLAT HANDLE WAS IN THE RETRACT POSITION. RETURNED FLAP HANDLE TO THE 0 DEGREES/EXTEND POSITION AND SLATS INDICATED EXTENDED. FOUND SLAT CONTROL POWER A C1 RESET C/B AND ATTEMPTED TO RETRACT SLATS. GOT THE SAME SLATS DISAGREE ALERT BUT THE CB REMAINED RESET. AIRCRAFT PITCH ALTITUDE AND SLIGHT VIBRATION WITH WDM 27-85-02, FOUND S1-9242 AND S1-9241 FAILED IN THE EXTEND POSITION. REMOVED AND REPLACED FLAP/SLAT CONTROL MODULE PER M/M 27-51-01 AFTER REPLACING S1-9242 AND S1-9241. ALSO REPLACED S1-9239 AND S1-9240 AS PRECAUTIONARY, AS PER THE ABOVE M/M REF PERFORMED.

Part: SPLICE — CRACKED (BS 1465)

CENTER W/W RT AND LT TRUNNION SUPPORT BOOT STRAP SPLICES CRACKED 5 EA. 1 EA. SPLICE CRACKED 10 INCHES STA 1465, REF SNRM NR N00646. 1 EA BOOT STRAP SPLICE CRACKED 6 INCH AT Y-STA 1489, REF SNRM NR N00648. 1 EA BOOT STRAP SPLICE CRACKED 1 INCH AT Y-STA 1465, REF SNRM NR N00649. 1 EA BOOT STRAP SPLICE CRACKED 3 INCH AT Y-STA 1465, REF NR N00650. 1 EA BOOT STRAP SPLICE CRACKED 2 INCH AT Y-STA 1489, REF SNRM NR N00651. *S/D* SNRM'S NBR'S N000646, N000648, N000649, N000650 AND N000651 INSTALLED SPLICE ANGLE PER EA 1-5310-34814 REF SEQ NR 000666.

Part: SPACER — GOUGED (RT MLG)

SNRM N00514 REF: TO EO 1-3210-7-3303B-P2. THE RT MAIN GEAR FWD TRUNNION IN COMPLIANCE WITH EO DISCOVERED THAT THE INNER SPACER ASSEMBLY WAS DAMAGED BEYOND LIMITS. DEEP GOUGES AND PITS IN INNER BUSHINGS. CLOSED OFF LUBE PASSAGE. REMOVED AND REPLACED SPACER ASSY, REF M/M 32-11-01-4, CLOSED 7-7-97.

Part: SPACER — GOUGED (LT MLG)

SNRM N00517 REF: TO EO 1-3210-7-3303B-P1. LT MAIN GEAR FWD TRUNNION, IN COMPLIANCE WITH EO DISCOVERED THE INNER SPACER ASSEMBLY WAS DAMAGED BEYOND LIMITS. DEEP GOUGES AND PITS, RESTRICTED LUBE PASSAGE. INSTALLED NEW SLEEVE ASSEMBLY PER M/M 32-11-01-04. CLOSED 7-8-97.

Part: BUSHINGS — GALLED (RT MLG TRUNION)

THE RT MAIN GEAR FORWARD TRUNNION SUPPORT FITTING, BOTH FWD AND AFT BUSHINGS HAVE MINOR GALLING AND SCORING FROM REMOVAL OF PIVOT PIN AT BOTTOM I/B AREA OF BUSHINGS. TRUNNION BUSHINGS MEASURED WITH IN WEAR LIMITS 3.754 PER CMM 32-10-02.

Part: BUSHING — GALLED (LT MLG TRUNION)

LT MLG FWD TRUNNION BUSHINGS DON'T HAVE ENOUGH CLEARANCE BETWEEN THEM TO PROVIDE PROPER GREASE CHANNEL PASSAGE. INSTALLED NEW BUSHINGS PER CMM 20-20-07 AND CMM 32-10-02.

Part: BUSHINGS — GALLED (LT MLG)

SNRM N00505 REF: TO EO 1-3210-7-3303B-P1, THE LT MAIN GEAR FWD TRUNNION SUPPORT FITTING BOTH FWD AND AFT BUSHINGS HAVE SEVERE GALLING 7 SCORING DURING REMOVAL OF PIVOT PIN, INNER BORE. *S/D* INSTALLED NEW BUSHING IN FWD TRUNNION PER CMM 20-20-07 AND SEALED, CLOSED 7-8-97.

Part: BUSHING — GALLED (RT MLG TRUNION)

RT MLG FWD TRUNNION BUSHINGS DON'T HAVE ENOUGH CLEARANCE BETWEEN THEM TO PROVIDE PROPER GREASE CHANNEL PASSAGE. INSTALLED NEW BUSHINGS PER CMM 20-20-07 AND CMM 32-10-02.

Part: SKIN — WRINKLED (BS 595-615)

FUSELAGE SKIN WRINKLED AT STA 595 TO 615 LONG 27 TO 47 LEFT SIDE AND AT STA 595 TO 615 LONG 27 TO 47 RIGHT SIDE. ALSO, AT STA 475 LONG 27 RIGHT SIDE AFT OF R1 DOOR. *S/D* MEASURED DEPRESSED AREA OF SKIN DIM IS 6 X 11.080 DENT IS WITHIN LIMITS PER SRM 53-20-00 FIG 6 TABLE A SHEET 2 P32. N00092, N00086 ACCOMPLISHED EA 1-5330-33474, REF SEQ NR 000391.

Part: TRIM MOTOR — CRACKED (HORIZ STAB TRIM)

HYD SYS 3 FAIL ALERT DISPLAYED ON CLIMBOUT, TOTAL LOSS OF HYD QTY, SYSTEM AUTO SHUTDOWN. FOUND HORIZONTAL STAB TRIM MOTOR CRACKED VERTICALLY. REMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR M1-16. REMOVED AND REPLACED BOTH PUMPS AND FILTERS PER M/M.

Part: ENGINE — FAILED (NR 2)

DURING FLIGHT THE NUMBER 2 ENGINE HAD AN OIL OVER TEMP AND OIL LOST PROBLEM. THE FLIGHT CREW FOLLOWED THE FLIGHT MANUAL AND SHUT DOWN THE ENGINE IN FLIGHT. REMOVED AND REPLACED THE NUMBER 2 ENGINE.

Part: SEAL — LEAKING (NR 2 ENGINE)

NUMBER 2 ENGINE OIL QUANTITY WENT TO 5 QUARTS APPROXIMATELY 15 MINUTES AFTER TAKEOFF AND CONTINUED TO DROP. ENGINE WAS SHUT DOWN AND A/C RETURNED. FOUND OIL LEAKING FROM GENERATOR STATOR CANNON PLUG. REMOVED AND REPLACED GENERATOR STATOR ASSEMBLY AND PACKING, MOTORED ENGINE AND LEAKED CHECKED OK. THIS WAS DONE PER M/M REF 73-21-21-4, SERVICED ENGINE TO 21 QUARTS AND OPERATIONAL CHECK GOOD.

Part: FRAME — CRACKED (LT MLG WW)

LT MLG GEAR WELL DOOR UPPER FRAME CRACKED. LOCATED 12 INCHES FWD OF GEAR WELL DOOR ACTUATOR I/B STRUT FAIRING. STOP DRILLED CRACK PER SRM 52-10-00, FABRICATED REPAIR DOUBLER PARTS REF SRM 52-10-00 AND INSTALLED REPAIR DOUBLERS REF SRM 52-10-00 PAGE 46.

Part: RIB — CRACKED (RT WING)

RT WING L/E RIB HAS A VISUAL CRACK INDICATION AT THE LOWER RADIUS APPROX 1.5 INCH LONG ON XORSS562.

Part: FRAME — CRACKED (LT MLG WW)

LT MLG GEAR WELL DOOR UPPER FRAME CRACKED. LOCATED 16 AFT OF GEAR WELL DOOR ACTUATOR I/B STRUT FAIRING. CRACK GOES TO EXISTING HOLE AS PER SRM 52-10-11 FIG 13 SHEET 2. FABRICATED DOUBLERS REF SRM 52-10-00 FIG 13 SHEET 2 AND INSTALLED DOUBLERS REF SRM 52-10-00 FIG 13 SHEET 2.

Part: SKIN — BULGE (LT MLG DOOR)

LT MLG GEAR WELL DOOR EXTERNAL SKIN BULGED ADJACENT TO CENTER HINGE SEGMENT, 52 INCHES FROM L/E OF DOOR.

Part: DRAIN LINE — BROKEN (NR 3 HYD SYST)

HYD NR 3 FAIL ALERT ILLUMINATED AND NR 3 HYD WENT TO ZERO. FOUND CASE DRAIN LINE BROKEN ON NR 3 ENGINE. MADE INTERIM REPAIR BY REMOVING PUMP AND CASE DRAIN LINE, FOLLOWED MEL 29-3 PROCEDURE. INSTALLED CASE DRAIN LINE AND HYD PUMP, HYD FLUID LEAK TEST COMPLIED PER MM 29-11-20. NO HYD FLUID LEAK WAS FOUND.

Part: RESERVOIR — FAILED (NR 3 HYD SYST)

LOST NR 3 HYDRO SYS FLUID QTY, THE SYS WENT DOWN TO EMPTY AFTER GEAR RETRACTION. REMOVED AND REPLACED NR 3 SYS HYD RESERVOIR. RAN HYDRO PRESS AND CHECKED FOR LEAKS. OPS CKD GOOD, OK FOR SERVICE.

Part: AIR BLEED VALVE — MALFUNCTIONED (NR 3 HYD SYST)

SIN: LOST NR 3 HYD SYSTEM FLUID QTY. THE SYSTEM WENT DOWN TO EMPTY AFTER GEAR RETRACTION. SERVICED NR 3 HYD SYSTEM TO 8.5 GAL, TROUBLESHOT AND RAN HYD SYSTEM AND LEAK CHECKED, NO LEAKS NOTED (SUSPECT AIR BLEED VALVE PLUNGER MAY HAVE STUCK DOWN), ALSO, RAN NR 3 ENGINE TO CHECK FOR LEAKS NOTED. EXCERISED PLUNGER AND OPS CHECKS GOOD. OK FOR SERVICE.

Part: HYD SYST — REQD SERVICE (NR 3 HYD SYST)

TPE - LOST NR 3 HYDRO SYSTEM, FLUID QUANTITY WENT DOWN TO 2.8. SERVICED NR 3 HYDRO SYSTEM TO 8.5 GALLONS. TROUBLESHOT AND RAN ENGINES. NO LEAK NOTED. (SUSPECT AIR BLEED VALVE PLUNGER MAY HAVE STUCK OPEN.) EXCERISED PLUNGER AND OPS. CHECK NORMAL.