N617FE

Part: TRUNNION — CRACKED (NLG) · airframe 84,311 hrs · 21,235 cycles

LANDING GEAR: NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING FOUND CRACKED AT STATION 595 (APPROX 1.0") CRACK AT NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING STATION 595, REPAIRED PER E.A. #: 1-5310-T0380063 P1. TITLE: FUSELAGE MAINFRAME CRACK REPAIR ON RH NOSE LANDING GEAR TRUNNION FITTING, STA595. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (ZONE 200) · airframe 84,311 hrs · 21,235 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1010, X = - 8.5 CROWN DAMAGED. CABIN - MAIN DECK COMPARTMENT AT SEAT TRACK STATION 1010, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 989 TO STATION 1029, 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 — DAMAGED (ZONE 200) · airframe 84,311 hrs · 21,235 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1681, X = 27.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT, DAMAGED CROWN AT SEAT TRACK STATION 1681, X = 27.5 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 1651 TO STATION 1691, 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: SEAT TRACK — DAMAGED (ZONE 200) · airframe 84,311 hrs · 21,235 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X = - 47.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT, DAMAGED CROWN AT SEAT TRACK STATION 1541, X = - 47.5,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 1571 TO EXISTING SPLICE STATION 5-123/1531, 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: SEAT TRACK — DAMAGED (ZONE 200) · airframe 84,311 hrs · 21,235 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879, X = 47.5 CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 879, 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 STATION 869 TO STATION 909, 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: SEAT TRACK — DAMAGED (ZONE 200) · airframe 84,311 hrs · 21,235 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879, X = - 8.5 CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 879, X = - 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD- 11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 869 TO STATION 909, 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 — DAMAGED (ZONE 200) · airframe 84,311 hrs · 21,235 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1010, X = 47.5 CROWN DAMAGED CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1010, 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 STATION 989 TO STATION 1029, 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: SKIN — DAMAGED (FUSELAGE) · airframe 81,616 hrs · 20,438 cycles

HUB STRIKE BELOW AFT BULK CARGO DOOR. REMOVED DAMAGED SKIN AS REQUIRED FOR SKIN REPAIR PER SRM 53-00-01-2R REPAIR #1. ROTOPROBE HOLES AND HFEC DAMAGE CUTOUT IAW NDTSPM PT6.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 80,824 hrs · 20,233 cycles

03 EACH FASTENER HOLES # 8 , # 32 , # 33 FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 . LEFT HAND LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 03 EACH HOLES # 8 , # 32 , # 33 BUSHING REPAIR CARRIED OUT AS PER MD11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLES AFTER BUSHING REPAIR COMPLETION AND REPETITIVE INSPECTION TO BE CARRIED OUR AT EVERY 2000 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT INSPECTION METHOD PER MD11 SRM 57-20-02-2R REPAIR 5 FIGURE 202 TABLE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 80,824 hrs · 20,233 cycles

08 EACH FASTENER HOLES #6 , #8 , #11 , #14 , #33 , #34 , # 35, # 36 FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 . RIGHT HAND LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6 08 EACH HOLES #6 , #8 , #11 , #14 , #33 , #34 , # 35, # 36 BUSHING REPAIR CARRIED OUT AS PER MD11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLES AFTER BUSHING REPAIR COMPLETION AND REPETITIVE INSPECTION TO BE CARRIED OUR AT EVERY 2000 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT INSPECTION METHOD PER MD11 SRM 57-20-02-2R REPAIR 5 FIGURE 202 TABLE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR — CRACKED (ZONE 600) · airframe 80,824 hrs · 20,233 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REVISION C ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP STATION 2164 EXISTING CRACK INDICATION FOUND FROM 2ND FASTENER FROM BELOW TO LOWEST FASTENER AND UNABLE TO PROCEED FURTHER INSPECTION DUE TO WEB BLOCKAGE. RIGHT HAND LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP STATION 2164 . EXISTING CRACK INDICATION FOUND FROM 2ND FASTENER FROM BELOW TO LOWEST FASTENER . EXISTING STOP DRILL AREA TRIMMED OUT AS PER SRM 55-30-02-2R REPAIR 5 FIGURE 201,AND REPAIR CARRIED OUT ON #4 RIGHT BANJO FITTING AS PER SRM 55- 30-02-2R REPAIR 5 FIGURE 204 AND EA # 1-5530-T0369333 P1 TITLE : STABILIZERS - VERTICAL STABILIZER - REAR SPAR LEFT AND RIGHT , BOTH FORWARD AND AFT FLANGES - REPAIR . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 . 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 204 .

Part: SEAT TRACK — WORN (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - RIGHT HAND STATION 1249 X = - 47.5 SEAT TRACK CROWN FOUND WORN. CABIN - RIGHT HAND SEAT TRACK AT STATION 1249 , X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO STATION 1311 X = - 47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REFER TO SNRM N00982 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - STATION 1250.75 TO STATION 1256.75 R3 DOOR CUT OUT FORWARD UPPER JAMB WEB BOX FOUND CRACKED. CABIN AT STATION 1250.75 TO STATION 1256.75 R3 DOOR CUTOUT FORWARD UPPER JAMB WEB BOX , CRACKED AREA REPAIRED AS PER E.A.#: 1-5310-T0369327 PART 1 , TITLE : FUSELAGE - MAINFRAME - CRACK REPAIR FOR R3 CENTER FUS PAX DOOR JAMB FWD INNER SKIN , STA 1250 - 1256 , L - 15R TO L - 16R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - STATION 1250.75 TO STATION 1256.75 L3 DOOR CUT OUT FORWARD UPPER JAMB WEB BOX FOUND CRACKED. CABIN AT STATION 1250.75 TO STATION 1256.75 L3 DOOR CUTOUT FORWARD UPPER JAMB WEB BOX , CRACKED AREA REPAIRED AS PER E.A.# : 1-5310 - T0369391 PART 1 , TITLE : FUSELAGE - MAINFRAME - CRACK REPAIR FOR L3 CENTER FUS PAX DOOR JAMB FWD INNER SKIN , STATION 1250 - 1256 , L - 15L TO L - 16L. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - LEFT HAND STATION 1009 X = 27.5 SEAT TRACK CROWN FOUND WORN. CABIN - AT LEFT HAND STATION 1009 , X = 27.5 SEAT TRACK WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 989 TO STATION 1029 , X = 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - MAIN DECK CARGO RIGHT HAND STATION 1781 LONGERON -12 TO LONGERON -13 FRAME FOUND DENT. CABIN - MAIN DECK CARGO , DENT AT RIGHT HAND FRAME STATION 1781 BETWEEN LONGERON 12 RIGHT TO LONGERON 13 RIGHT REPAIRED AS PER SRM 53-00-07-2R REPAIR 2 FIGURE 201. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-00-07-2R REPAIR 2 TABLE 201.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 80,824 hrs · 20,233 cycles

LOWER AFT CARGO COMPARTMENT BETWEEN STATION 1897 AND STATION 1925 X - 57 CEILING FLOOR SUPPORT FOUND WITH CORROSION. LOWER AFT CARGO COMPARTMENT CEILING , AT FLOOR SUPPORT STATION 1897 AND STATION 1925 , X = - 57 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FUGURE 206 REPAIR GENERAL. CORRODED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 , X = - 57 AS PER SRM 51-31-01-0G. FLOOR SPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 80,824 hrs · 20,233 cycles

AFT CARGO AND WASTE TANK COMPARTMENT STATION 1990 TO STATION 2000 , X - 25 CEILING FLOOR SUPPORT FOUND WITH CORROSION. AFT CARGO AND WASTE TANK COMPARTMENT CEILING , AT FLOOR SUPPORT STATION 1990 TO STATION 2000 , X = - 25 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL CORRODED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G FROM STATION 1887 TO STATION 2007 X = - 25. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7087 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - RIGHT HAND STATION 2003 X = - 22 FLOOR SUPPORT FOUND CORRODED. CABIN - AT RIGHT HAND FLOOR SUPPORT STATION 2003 , X = - 22 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL. CORRODED FLOOR SUPPORT 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: SEAT TRACK — CORRODED (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

RIGHT HAND STATION 555 X = - 27.5 SEAT TRACK FOUND CORRODED. CABIN - AT RIGHT HAND SEAT TRACK STATION 555 , X = - 27.5 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 525 TO STATION 585 , X = - 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - RIGHT HAND STATION 1421 X = - 47.5 SEAT TRACK CROWN FOUND WORN. AT RIGHT HAND SEAT TRACK STATION 1421 , X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1411 TO STATION 1471 , 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 — CORRODED (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - LEFT HAND STATION 1721 X = 27.5 SEAT TRACK FOUND CORRODED. CABIN - AT LEFT HAND SEAT TRACK STATION 1721 , X = 27.5 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 STATION 1731 , X = 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - RIGHT HAND STATION 1411 X = - 27.5 SEAT TRACK CROWN FOUND WORN. CABIN - RIGHT HAND SEAT TRACK AT STATION 1411 , X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1391 TO STATION 1431 , X = - 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 80,824 hrs · 20,233 cycles

CABIN - RIGHT HAND STATION 1285 X = - 47.5 SEAT TRACK CROWN FOUND WORN. CABIN - RIGHT HAND SEAT TRACK AT STATION 1285 , X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO STATION 1311 , X = - 47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,824 hrs · 20,233 cycles

LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-73 , LONGERON 48 LEFT HAND FOUND WITH CORROSION . LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-73, CORROSION AT LONGERON 48 LEFT HAND REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORRODED LONGERON 48 LEFT HAND REMOVED AND REPLACED AT EXISTING SPLICES STATION 5-50 TO STATION 1541 AS PER SRM 51-31-01-0G. LONGERON 48 LEFT HAND FABRICATED AS PER DOUGLAS DRAWING A5A7032 REVISION B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,824 hrs · 20,233 cycles

LOWER CENTER CARGO COMPARTMENT BILGE STATION 1581 , LONGERON 48 LEFT FOUND WITH CORROSION . LOWER CENTER CARGO COMPARTMENT BILGE STATION 1581 , LONGERON 48 LEFT CORROSION BLENDOUT AND SMOOTHEN AND REPROTECT AS PER MD-11 SRM 51-21-01-OG . FOUND WITHIN LIMIT AS PER MD-11 SRM 53-00-00-2R . FIGURE 205 . REPAIR GENERAL . REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 80,824 hrs · 20,233 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 622 FOUND CRACK. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 622 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 80,824 hrs · 20,233 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM 2ND FASTENER FROM BELOW TO LOWEST FASTENER AND UNABLE TO PROCEED FURTHER INSPECTION DUE TO WEB BLOCKAGE. LEFT HAND LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP STATION 2164 . EXISTING CRACK INDICATION FOUND FROM 2ND FASTENER FROM BELOW TO LOWEST FASTENER . EXISTING STOP DRILL AREA TRIMMED OUT AS PER SRM 55-30-02-2R REPAIR 5 FIGURE 201,AND REPAIR CARRIED OUT ON #4 LEFT BANJO FITTING AS PER SRM 55-30- 02-2R REPAIR 5 FIGURE 204 AND EA # 1-5530-T0369333 P1 TITLE : STABILIZERS - VERTICAL STABILIZER - REAR SPAR LEFT AND RIGHT , BOTH FORWARD AND AFT FLANGES - REPAIR . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 . 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 204 .

Part: TRUNNION — CRACKED (NLG) · airframe 80,824 hrs · 20,233 cycles

DURING HIGH FREQUENCY EDDY CURRENT SURFACE REPETITIVE INSPECTION ON THE LEFT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACKS WITH LENGTH APPROXIMATELY 0.2Ï¿½ AT STATION 575. AT HIGH FREQUENCY EDDY CURRENT SURFACE REPETITIVE INSPECTION ON LEFT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA WITH 01 EACH CRACK STATION 575 REPAIRED AS PER SRM 53-10- 14-2R REPAIR 2 FIGURE 202. REPETITIVE INSPECTION REQUIRED Ï¿½ INITIAL AT 1,500 CYCLES AND REPETITIVE INSPECTION AT 1,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-10-14-2R REPAIR 2 TABLE 201 (FIGURE 202). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 80,824 hrs · 20,233 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 689 FOUND CRACK. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 689 CRACKED AREA 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 80,824 hrs · 20,233 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 545 FOUND CRACK. RIGHT WING FIXED LEADING EDGE AT XOS 545 BEADED DOUBLER CRACKED AREA REPAIRED AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — CRACKED (ZONE 500 RIB) · airframe 80,824 hrs · 20,233 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK. LEFT WING FIXED LEADING EDGE AT STATION XOS 789 CRACKED RIB DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 80,824 hrs · 20,233 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 561 FOUND CRACK. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 561 CRACKED AREA 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 500) · airframe 80,824 hrs · 20,233 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 711 FOUND CRACK. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 711 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (ZONE 600) · airframe 80,824 hrs · 20,233 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE UPPER FORMER AT XOS 584 FOUND CRACK. RIGHT WING FIXED LEADING EDGE AT XOS 584 CRACKED UPPER FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600 RIB) · airframe 80,824 hrs · 20,233 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACK. RIGHT WING FIXED LEADING EDGE AT XOS 789CRACKED RIB DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — DELAMINATED (ZONE 500) · airframe 80,824 hrs · 20,233 cycles

LEFT WING Ï¿½ TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 398 FOUND DETACHED. LEFT WING TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 398 DETACHED AREA REPAIR CARRIED OUT AS PER SRM 57-50- 01-2R REPAIR 6 FIGURE 203 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — DAMAGED (ZONE 600) · airframe 80,824 hrs · 20,233 cycles

RIGHT WING Ï¿½ TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 400 FOUND DETACHED. RIGHT WING - TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SUFACE FORWARD EDGE FINGER DOUBLER AT XW 400 DETACHED AREA REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAIR 6 FIGURE 203 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE — CORRODED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE SURFACES FOUND WITH CORROSION. LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE SURFACE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07, REPAIR EVALUATED AND FOUND PIVOT BORE SURFACE INBOARD FACE REMAINING THICKNESS : 0.463", OUTBOARD FACE REMAINING THICKNESS : 0.461", IS CORRECTED AS PER EA 1-5750-T0354715P1 STEP 1E FIGURE 2. TITTLE : WINGS- FLIGHT SURFACES- LEFT HAND WING - INBOARD FLAP - OUTBOARD FORWARD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1- ALTERNATE METHOD. REFER TO WRI : 57509345 FOR WORK DETAIL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 75,793 hrs · 18,853 cycles

RIGHT HAND WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE SURFACES FOUND WITH CORROSION. RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE SURFACE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07, REPAIR EVALUATED AND FOUND PIVOT BORE SURFACE INBOARD FACE REMAINING THICKNESS : 0.465", OUTBOARD FACE REMAINING THICKNESS : 0.496", IS CORRECTED AS PER EA 1-5750-T0354716P1 STEP 1E FIGURE 2. TITTLE : WINGS- FLIGHT SURFACES- RIGHT HAND WING - INBOARD FLAP - OUTBOARD FORWARD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1- ALTERNATE METHOD. REFER TO WRI : 57509346 FOR WORK DETAIL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — BULGED (TE FLAP VANE) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING INBOARD FLAP VANE MID LEADING EDGE ADJACENT TO VANE TRACK FOUND SKIN BULGING.

Part: FLOOR PANEL — DAMAGED (MIAIN DECK) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT BETWEEN STATION Y1561 AND Y1661, LEFT SIDE FLOOR PANEL 283AF FOUND PUNCTURED AT AFT CORNER EDGE X = 27. MAIN DECK CARGO COMPARTMENT PUNCTURED FLOOR PANEL 283AF BETWEEN STATION Y1561 TO STATION Y1661 AFT EDGE X = 27 LEFT SIDE REMOVED AS PER AMM 53-21-09-4. FLOOR PANEL FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-09-4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT LEFT STATION Y1761 OUTBOARD FLOOR PANEL 281JF FOUND SPONGY. MAIN DECK CARGO COMPARTMENT STATION Y1761 OUTBOARD FLOOR PANEL 281JF SPONGY PANEL REMOVED AND NEW FLOOR PANEL FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. NEW FLOOR PANEL PART MARK AS SR10-AFA 3240-9 PER GMM 7-0-1000. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT AFT LEFT AREA X = 78.25, STATION Y1942 OUTBOARD FLOOR PANEL 293EF FOUND SPONGY. MAIN DECK CARGO COMPARTMENT LEFT AREA SPONGY FLOOR PANEL 293EF AT STATION Y1942 X = 78.25 REMOVED AS PER AMM 53-21-09-4. FABRICATED FLOOR PANEL AS PER DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL INSTALLED AS PER AMM 53-21-09-4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — WORN (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE BUSHING FOUND WORN. WORN BUSHING PIVOT BORE REMOVED IAW CMM 20-10-7 AND FOUND LUG HOLE WITHIN LIMIT IAW CMM57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-07, AND EA 1-5750-T0354715, P1, STEP 1.F.(1), AND STEP 1.F.(3). REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100.

Part: BRACKET — WORN (RT WING) · airframe 75,793 hrs · 18,853 cycles

RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE BUSHING FOUND WORN. WORN BUSHING AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE REMOVED AS PER MD-11 CMM20-10-7 AND FOUND LUG HOLE WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND EA.#:1-5750-T0354716 P1 STEP 1.F.(1) AND STEP 1.F.(3) . TITLE: WINGS- FLIGHT SURFACES-RIGHT HAND WING-INBOARD FLAP -OUTBOARD FORWARD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1-ALTERNATE METHOD. REFER TO WRI:57509346 FOR WORK DETAIL. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: HINGE — WORN (LT WING) · airframe 75,793 hrs · 18,853 cycles

RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE BUSHING FOUND WORN.

Part: HINGE — WORN (LT WING TE FLAP) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING-INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE BUSHING FOUND WORN.

Part: FLOOR PANEL — DAMAGED (MIAN DECK) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT AFT LEFT AREA, STATION Y1901 FLOOR PANEL 291GF (SECOND FROM OUTBOARD) FOUND SPONGY. MAIN DECK CARGO COMPARTMENT AFT LEFT AREA, STATION Y1901 FLOOR PANEL 291GF REMOVED PER AMM 53-21-09-4, FABRICATED PER DRAWING SRZ-25-005 REVISION R, AND INSTALLED PER AMM 53-21-09-4. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535, OUTBOARD FLOOR PANEL 231EF FOUND WITH SEVERAL PUNCTURES. MAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535, OUTBOARD FLOOR PANEL 231EF REMOVED PER AMM 53-21-09-4, FABRICATED PER DRAWING SRZ-25-005 REVISION R AND INSTALLED PER AMM 53-21-09-4. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT AFT LEFT AREA , STATION Y1901 FLOOR PANEL #291GF (SECOND FROM OUTBOARD) FOUND SPONGY. MAIN DECK CARGO COMPARTMENT AFT LEFT AREA, X = 47.5 STATION Y1901. FLOOR PANEL #291GF REMOVED PER AMM 53-21-09-4, FABRICATED PER DRAWING SRZ-25-005 REVISION R, AND INSTALLED PER AMM 53-21-09-4. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535 , OUTBOARD FLOOR PANEL #231EF FOUND WITH SEVERAL PUNCTURES. MAIN DECK CARGO COMPARTMENT LEFT SIDE X = 78 STATION Y535, OUTBOARD FLOOR PANEL #231EF REMOVED PER AMM 53-21-09-4, FABRICATED PER FEDEX DRAWING SRZ-25-005 REVISION R, AND INSTALLED PER AMM 53-21-09-4. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT AFT LEFT AREA, STATION Y1901 FLOOR PANEL 291GF (2ND FROM OUTBOARD) FOUND SPONGY.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 75,793 hrs · 18,853 cycles

MAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535, OUTBOARD FLOOR PANEL #231EF FOUND WITH SEVERAL PUNCTURES.

Part: DOUBLER — CORRODED (RT WING) · airframe 75,793 hrs · 18,853 cycles

RIGHT WING UPPER INBD SURFACE, MAIN LANDING GEAR SUPPORT DOUBLER CORRODED NEAR TWO INBD AFT FASTENERS. CORROSION REMOVED AND FOUND EXCEED LIMITS. CORROSION REMOVAL 0.100 INCHES MAXIMUN IAW SRM 57-20-01-1A, FIGURE 101, ALLOWABLE DAMAGE 1 . REPAIRED IAW EA 1-5730-T0354739 P1. CLASSIFIED THE REPAIR AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CORRODED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT WING UPPER INBOARD SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER CORRODED NEAR INBOARD EDGE. CORROSION REMOVED AND FOUND EXCEEDED LIMITS. CORROSION REMOVAL 0.100 INCHES MAXIMUN IAW SRM 57-20-01-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED IAW EA 1-5730-T0354588A, P1. CLASSIFIED REPAIR AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CRACKED (BS 1721) · airframe 75,793 hrs · 18,853 cycles

DURING HFEC INSPECTION, FRAME AT BS 1721, BETWEEN STRINGER 12L AND 13. FOUND CRACKED ON ORIGINAL FRAME APPROXIMATE 1/2 INCH.

Part: FORMER — CRACKED (RT WING) · airframe 75,793 hrs · 18,853 cycles

RIGHT HAND WING LEADING EDGE PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643. RIGHT HAND WING LEADING EDGE REFUELING PANEL COMPARTMENT CUTOUT EDGE CRACKED AT OUTBOARD AFT CORNER AREA ( XOS 643 ) REMOVED PER SRM 51-31-01-OG. FABRICATED FORMER AS PER DRAWING ARB 2917 REVISION L. MATERIAL USE 7075-0-0.071" ALUMINIUM ALCLAD SHEET. FABRICATED FORMER INSTALLED AS PER SRM 51-31-01-OG. FABRICATED FORMER PARTS MARKED AS FX ARB 2917-12 PER GMM 7-0-1001. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 766 FOUND CRACK.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT FOUND WITH BEAD DOUBLER MINOR CRACKED AT XOS 771.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,793 hrs · 18,853 cycles

RIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 639 FOUND CRACK.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING- LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 766 FOUND CRACK LEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 766 CRACKED AREA TRIMMED OUT . REPAIR ANGLE AND DOUBLERS FABRICATED AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203 . FABRICATED REPAIR ANGLE AND DOUBLERS INSTALLED AS PER SRM 57-40-02- 2R FIGURE 203 REPAIR 15 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FORMER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT WING LEADING EDGE REFUELING PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643. REMOVED AND FABRICATED A FORMER IAW DRAWING ARB 2917, REVISION L . FABRICATED FORMER INSTALLED IAW SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 .

Part: DOUBLER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 663 FOUND CRACK.

Part: SKIN — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING LEADING EDGE REFUELING PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING-LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 663 FOUND CRACK. LEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 633 CRACK AREA TRIMMED OUT AND REPAIR CARRIED OUT PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR PARTS MATERIAL USE 7075T6-0.020" AND 7075-0-0.063" ALCLAD ALUMINIUM SHEET AND 7075T6-0.032" ALCLAD ALUMINIUM SHEET. REPAIR PARTS INSTALLED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT FOUND WITH BEAD DOUBLER MINOR CRACKED AT XOS 771 LEFT WING LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER TRIMMED OUT REPAIR ANGLE AND DOUBLERS FABRICATED AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203 . REPAIR ANGLE AND DOUBLERS FASTENERS HOLE PICKED UP AND INSTALLED 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 75,793 hrs · 18,853 cycles

RIGHT HAND WING- LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 639 FOUND CRACK RIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 639 CRACKED AREA TRIMMED OUT . REPAIR ANGLE AND DOUBLERS FABRICATED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. FABRICATED REPAIR ANGLE AND DOUBLERS INSTALLED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 AND SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 609 FOUND CRACK.

Part: SKIN — CRACKED (RT WING) · airframe 75,793 hrs · 18,853 cycles

RIGHT HAND WING LEADING EDGE PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,793 hrs · 18,853 cycles

LEFT HAND WING-LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 609 FOUND CRACK. LEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 609 CRACK AREA TRIMMED OUT AND REPAIR CARRIED OUT PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR PARTS MATERIAL USE 7075T6-0.020" AND 7075-0-0.063", 7075T6-0.032" ALCLAD ALUMINIUM SHEET. REPAIR PARTS INSTALLED 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 75,793 hrs · 18,853 cycles

AGING AIRCRAFT, EXISTING REPAIR AT RIGHT HAND WING LOWER LEADING EDGE, STRINGER DOUBLER REPAIR XOS 906. EXISTING STRINGER DOUBLER REPAIR AT RIGHT HAND WING LOWER LEADING EDGE, XOS 906 REMOVED IN ACCORDANCE WITH SRM 51-31-01-0G AND NEW REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 57-40-03-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B6 PART 1, TITLE: "STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 75,793 hrs · 18,853 cycles

EMPENNAGE - ACCESS PANEL 364QR FOUND CUT OUT CRACKED UPON PANEL REMOVAL.

Part: FRAME — CRACKED (EMPENNAGE) · airframe 75,793 hrs · 18,853 cycles

EMPENNAGE - ACCESS PANEL 363ML FOUND CUT OUT CRACKED UPON PANEL REMOVAL. AT STATION 2164 LEFT HAND , ZID = 72.0 , XID = 9.0 . ACCESS PANEL 363ML AT STATION 2164 LEFT HAND ZID = 72.0 XID = 9.0 CRACK FRAME REMOVED AND REPLACED AS PER EA # 1-5500-T0354594P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 75,793 hrs · 18,853 cycles

EMPENNAGE ACCESS PANEL 363ML FOUND CUT OUT CRACKED UPON PANEL REMOVAL. ACCESS PANEL 363ML AT STATION 2164 LEFT HAND ZID 72.0 CRACK FRAME REMOVED AND REPLACED AS PER EA 1-5500-T0354594 TITLE : STABILIZERS - GENERAL - PYLON CARRY THRU PANEL FRAME AJC 7593-51 ALTERNATE SURFACE FINISH. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — CRACKED (EMPENNAGE) · airframe 75,793 hrs · 18,853 cycles

EMPENNAGE - ACCESS PANEL 364QR FOUND CUT OUT CRACKED UPON PANEL REMOVAL. AT STATION 2164 RIGHT HAND ZID = 75.5 , XID = 9.0 . EMPENNAGE ACCESS PANEL 364QR AT STATION 2164 RIGHT HAND ZID = 75.5 , XID = 9.0 CRACKED SKIN PANEL REMOVED PER SRM 51-31-01-OG . NEW SKIN PANEL ( FRAME ) PART NUMBER AJC 7593U52 FASTENER HOLES PICKED UP AND INSTALLED AS PER SRM 51-31-01- OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: TRIM MOTOR — CRACKED (HORIZ STAB) · airframe 75,563 hrs · 18,801 cycles

2:00 INTO FLT, FLT 370 HYD 3 ELEV OFF ALER. HYD SYS 3 WAS AT 3.9 OVER NEXT FIVE MINUTES DROPPED TO 3.6. DEPRESSURIZED SYS UNTIL LANDING. AFTER LANDING QTY WAS DOWN TO 1.0 FOUND HYDRAULIC FLUID MISTING IN TAIL AREA AROUND HORIZONTAL STABILIZER TRIM MOTORS. FOUND HORIZONTAL STABILIZER TRIM MOTOR 1 BODY CRACKED AT MATING FLANGE ATTACH POINTS. REMOVED HS TRIM MOTOR SN MX-328050C. REF MD11 AMM 27-43-30-4 COMPLETE UP TO STEP 3, READY FOR TRIM MOTOR INSTALLATION. INSTALLED TRIM MOTOR. PERFORMED OPS CHECK. CHECKS NORMAL NO LEAKS NOTED. REF AMM 27-43-30-4.

Part: COMPENSATOR — INOPERATIVE (FUEL TANK) · airframe 75,245 hrs · 18,715 cycles

AT LEVEL OFF, WHEN COMBINING FUEL USED AND FUEL REMAINING, TOTAL FUEL WAS 7000 # HIGHER THAN OUR INITIAL FUEL AT BLOCK OUT. FUEL QTY NUMBERS ON FUEL SYNOPTIC WERE INTERMITTENTLY AMBER THEN WHITE, BUT FUEL TOTAL WAS ALWAYS GROSSLY INACCURATE, MAXING AT THE 7000 # OFF. RTB MEM. MX ENTRY ONLY: REPLACED #2 TANK L/H AND R/H COMPENSATORS IRW MD-11 AMM 28-41-37-4. OPS CHECK/ BITE TEST GOOD IRW MD-11 AMM 28-41-00-5. LEAK CHECK GOOD IRW MD-11 AMM 28-11-00-2. ALL WORK PERFORMED BY FFC,

Part: SKIN — CORRODED · corrosion level 2 · airframe 74,254 hrs · 18,420 cycles

AFT ACCESSORY COMPARTMENT HAS EVIDENCE OF CORROSION ON R/H SIDEWALL. REPAIR IN REF. TO MD11 SRM 53-70-01-2R; FIG. 201.

Part: SKIN — CORRODED (BS 2160-2163) · corrosion level 2 · airframe 74,254 hrs · 18,420 cycles

AFT ACCESSORY COMPARTMENT HAS EVIDENCE OF CORROSION ON THE RT SIDEWALL. REPAIRED IAW SRM 53-70-01-2R, FIG 201.

Part: ELECTRICAL SYS — UNKNOWN · airframe 73,797 hrs · 18,283 cycles

DURING SVC, FOUND EMERGENCY PWR TEST COULD NOT BE COMPLETED. ONLY BATTERY VOLTAGE DROP TO 28V AND GO UP TO 31V WITHOUT BATTERY CHARGING ALERT. EPCU NO FAULT AND RTS TEST PASSED. BAT CHARGER C/B RESET NO HELP AND CYCLED A/C PWR NO HELP. STARTED APU PER JRH AND BAT VOLTAGE DROPPED TO 20V AND CHARGED TO 31V WITH BAT CHARGING ALERT. BUT EMER RWR TEST STILL SAME RESULT. PERFORMED FURTHER T/S IAW FIM 24-30-16-00. CK'D AND INSPECTED BAT EQIPMENT AREA AND BAT AMMETER SHUNT. FOUND NO DEFECT. INSPECTED CHARGER CONNECTOR PLUG AND NO DEFECT PER MM 24-34-03-4. PERFOMRED BAT CHARGER OPERATIONAL TEST PER MM 24-34-03-5, EMER PWR SW TURNED ON FOR 5 MINS AND TURNED OFF THEN BAT CHARGING ALERT IS SHOWN. FULLY CHARGED TO 33V. THEN PERFORMED EMER PWR TEST AND TEST COMPLETED NML WITH CHARGING ALERT AND PASS SEVERAL TIMES. NO HISTORY. A/C OK FOR SVC.

Part: CHECK VALVE — LEAKING (HYD SYSTEM) · airframe 73,583 hrs · 18,223 cycles

APPROX. 1 HOUR INTO FLIGHT LEVEL 1 HYD EIU 3 OFF ALERT. HYD QTY 3.2. HYD QTY CONTINUED TO DECREASE TO 2.5 LEVEL 1 HYD 3 OFF. QTY THEN HELD SEADY AT 2.5. AT SLAT EXNTENSION, QTY IMMEDIATLY DROPPED AND RECIEVED LEVEL 2 HYD FAIL ALERT. QTY WENT TO NEAR 0. REMOVED AND REPLACED THE CHECK VALVE THAT WAS LEAKING ON THE UPPER HYD TRIM VALVE PER M/M 27-43-41-4-0. PERFORMED LEAK CHECK ON VALVE AND ALL SYSTEM ARE GOOD. THE ORING WAS FOUND TO BE SPLIT ON OLD CHECK VALVE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,339 hrs · 18,169 cycles

DURING CA CABIN PREFLIGHT, EMER LIGHTS TEST FAILED W/ "EMER LT BAT 1 LOW" FAULT. R&R'ED EMERGENCY POWER SUPPLY BAT PER MM 33-51-01-4 AND PERFORMED TEST PER MM 33-51-01-5, TEST PASSED MEL CLOSED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,339 hrs · 18,169 cycles

PDIS 617 33-50 8018 12MAY19 MEM OPEN U LOGPAGES:3111468 DURING CA CABIN PREFLIGHT, EMER LIGHTS TEST FAILED W/ "EMER LT BAT 1 LOW" FAULT. MEL 12MAY19 20:06 MEM U RELEASED FOR SERVICE PER MEL : 33-50-04 CATEGORY : C EXPIRATION : 22MAY19 "MEL 33-50-04: EMER LIGHTS - INOP." C/7185236 18MAY19 00:51 CDG R&R'ED EMERGENCY POWER SUPPLY BAT PER MM 33-51-01-4 AND PERFORMED TEST PER MM 33-51-01-5.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 72,760 hrs · 17,980 cycles

EMER LIGHT TEST ARM WOULD NOT TEST. PERFORMED RESET TO EMERGENCY LIGHT CONTROL C/B G13. OPERATIONAL CHECK OK

Part: FIRE DETECTOR — INTERMITTENT (NR 3 ENGINE) · airframe 72,216 hrs · 17,805 cycles

PDIS 617 26-10 7503 01DEC18 EWR OPEN U LOGPAGES:2733768 "FIRE DET 3 FAIL" BLINKS INTERMITTANTLY. AT TIMES SHGN 02DEC18 19:08 EWR REMOVED AND REPLACED NR 3 ENGINE UPPER TURB R LOOP A (DH4) FIRE DETECTOR AS REQUIRED IN REF TO AMM 26-11-03-4-1 FACT 03DEC18 06:58 EWR NR 3 ENGINE FIRE LOOP "A" OPS CHECK GOOD AND BITE TEST OF THE FIRE DETECTION CONTROL UNIT CHECKED GOOD WITH NO FAULTS FOR "A" LOOP ON NR 3 ENGINE AS PER AMM 26-11-02-5.

Part: FRAME — DENTED (BS 1761) · airframe 71,528 hrs · 17,607 cycles

MAIN DECK CARGO BAY FRAME WAS DENTED BS 1761, LONGERON 12L. REPAIRED THE FRAME IAW SRM 53-00-07-2R, FIGURE 201, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 71,528 hrs · 17,607 cycles

LEFT WING LEADING EDGE COMPARTMENT ALONG XOS 665, AROUND THE NR 5 SLAT AREA, FOUND LEADING EDGE PLATING STRINGER CRACKED. TRIMMED AND REPAIRED IAW SRM 57-40-03-2R, FIGURE 202, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,528 hrs · 17,607 cycles

LEFT WING LEADING EDGE COMPARTMENT ALONG XOS 708, AROUND THE NR 5 SLAT AREA, FOUND THE LEADING EDGE PLATING BEADED DOUBLER CRACKED. THE BEADED DOUBLER WAS TRIMMED OUT AND REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,528 hrs · 17,607 cycles

LEFT WING LEADING EDGE COMPARTMENT LOWER SURFACE, 518GB PANEL CUTOUT, FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TIRE — LEAKING (MLG) · airframe 71,118 hrs · 17,481 cycles

LEVEL 1 LOW TIRE PRESSURE ALERT ON NR 5 TIRE CAME ON DURING CLIMB. FOLLOWED BY LEVEL 2 TIRE FAILURE ALERT. C/W QRH AND RETURNED TO KMEM. REPLD NR 5 AND NR 6 WHEEL ASSY REF AMM 32-41-01-4. INSP WHEEL WELL AND LANDING GEAR AREA. NO DAMAGE FOUND. A/C OK FOR SVC.

Part: FLEX LINE — BROKEN (BRAKE SYSTEM) · airframe 70,973 hrs · 17,433 cycles

ON BLOCK IN, ADVISED BY GROUND THAT FLAMES WERE COMING FROM LEFT GEAR . TRYING TO CONFIRM, THE FLAMES HAD STOPPED. HIGHEST BRAKE TEMP NOTED ON CONFIG PAGE WAS 6 AT 473. ALL TEMPS ON LEFT TRUCK WERE MID 400S, ALL TEMPS ON RIGHT TRUCK MID 300S. LIGHT TO MEDIUM BRAKING ON LANDING . FOUND BROKEN BRAKE FLEX LINE NEAR QD COUPLING ON THE NR 6 BRAKE ASSY. REMOVED AND REPLACED THE FLEX LINE. CONNECTED TO COUPLING IAW AMM 32-43-21-4. INSPECTED BRAKE ASSY. NO DAMAGE NOTED IAW AMM 32-43-20-6. BRAKE SYSTEM CHECKED GOOD FOR SECURITY AND OPERATION.

Part: PITOT LINE — CLOGGED · airframe 70,748 hrs · 17,362 cycles

AT FL380, WITH THE ENGINE & WING ANTI-ICE ON, RECEIVED AN IAS COMPARITOR LIGHT. A/S STARTED DECAYING TOWARD THE LWR FOOT. STARTED AN IMMEDIATE DESCENT TO FL340. LVL 2 SEL ELEV FEEL MAN. QRH DIRECTED REFERENCE TO FLT INSTEUMENTS > EMERG NON-ALERT PROCEDURE - AIRSPEED UNRELIABLE. COMPLIED WITH QRH. CADC 2 - INOP. JT CREW DEBRIEF: WAS IN HEAVY ICING CONDITIONS AND SUSPECTED POSSIBLE ICE BLOCKAGE. CADC 2 PASSED OPS/BITE TEST. MSC AIR DATA HEATER TEST PASSED. PITOT MOISTURE TRAPS IN E/E WERE DRY. DISC 2 PITOT LINE AT CADC QD FITTING AND BLEW DRY NITROGEN BACK THROUGH SYSTEM. INITIALLY HAD NO FLOW, BUT AFTER A FEW SECONDS A COUPLE CC'S OF COLD WATER BLEW OUT OF PITOT TUBE AND HAD GOOD FLOW. VERIF'D PITOT DRAINS WERE CLEAR BY NITROGEN FLOW AND VISUALLY. VERIF'D NO DEBRIS IN PITOT TUBE. TURNED ON PITOT HEAT AND VERIF'D PITOT HEAT OPS NML, PROBE GETS HOT. PERF AUTOLAND RTS OF #2 FCC, ALL TESTS PASSED. LLM STATUS REMAINS THE SAME. NO HIST 90 DAYS. REF AMM 34-16-01-4, 22-00-00-2, 34-10-00-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,114 hrs · 16,878 cycles

CRACK ON FUSELAGE AT THE UPPER AFT CORNER OF NR 1 PACK BAY DOOR. REPAIRED IAW SRM 53-20-15-2R.

Part: COLLAR — BROKEN (NLG STEERING) · airframe 68,972 hrs · 16,837 cycles

DURING POSTFLIGHT, FOUND NOSE STRUT LOWER STEERING SUPPORT COLLAR ASSY BROKEN. REMOVAL OF NOSE STRUT LOWER LEG IN PROGRESS AS PER AMM 32-21-01-8 FROM CHAPTER 4 . INSTALLED IAW MM 32-21-01-8 FROM STEP 5.F.11. ALL TEST PASSED INCLUDING NOSE LANDING GEAR RETRACTION TEST. A/C RECONFIGURED IAW MM 32-21-01-8.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP VANE HORN FITTING-C, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. A REPAIR SLOT BUSHING WAS FABRICATED IAW EA 1-5750-T0328433 PART 1 STEP 2B AND INSTALLED IAW AMM 27-50-32-4.

Part: VANE — CORRODED (TE FLAP) · corrosion level 2 · airframe 66,872 hrs · 16,216 cycles

RT WING OTBD FLAP VANE HORN FITTING E, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R FIG.201. SLOT BUSHING FABRICATED IAW EA 1-5750-T0328433 PART 1 STEP 2A AND INSTALLED IAW AMM 27-50-32-4.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP VANE HORN FITTING-D, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. REPAIR SLOT BUSHING FABRICATED IAW EA 1-5750-T0328435 PART 1 STEP 1A AND INSTALLED IAW AMM 27-50-32-4.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP INBD TRAILING EDGE WEDGE DELAMINATED. WEDGE REPAIRED AND SMOOTHED AS PER SRM 57-50-80 REPAIR 1 PARA 4A1B. REFER TO WR1 57504399 FOR WORK DETAIL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED EA 1-5750-T0328351 PART 1 STEP 1C.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1C.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1 STEP 1A AND STEP 1.

Part: HINGE — CORRODED (TE FLAP) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75312C PART 5 STEP 4 & STEP 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,872 hrs · 16,216 cycles

CABIN, MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSIONS AT RT STA 475, X = -75.25. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 66,872 hrs · 16,216 cycles

LEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORRODED. REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75300C P5, STEP 1A & STEP 1C. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP INBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328382, PART 1, STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1B AND STEP 1.

Part: HINGE — CORRODED (TE FLAP) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75312C PART 5 STEP 2 & STEP 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1A.

Part: HINGE — CORRODED (TE FLAP) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0328400 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1A AND STEP 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

CABIN, MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSIONS AT RT STA 615, X = -8.5. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 585 TO EXISING SPLICE AT STA 625 X= -8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE. LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1B.

Part: HINGE — CORRODED (TE FLAP) · airframe 66,872 hrs · 16,216 cycles

LEFT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75300C P5, STEP 1A & STEP 1C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE UPPER BARREL NUT HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.406", FINAL HOLE: DIA 0.421", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0328318 PART 1 STEP 1B. CORROSION REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT, OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.582", FINAL HOLE: DIA 0.598", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0328318 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER BARREL NUT HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE: DIA 0.406", FINAL HOLE: DIA 0.421", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0328318 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FRAME DENTED AT LT STA 5-11, LONGERON 12L. FRAME REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE ACTUATOR OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0328318 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR WAS BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1B.

Part: HINGE — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP, INBD FORWARD HINGE, WING SIDE LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. FABRICATED A REPAIR BUSHING AND INSTALLED IAW EA 1-5750-T0328311 PART 1 STEP 1.

Part: ANGLE — DENTED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR ANGLE DENTED AT LT STA 1701, LONGERON 12L. FRAME REPAIR ANGLE REMOVED PER SRM 51-33-01-0G AND REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1310) · airframe 66,872 hrs · 16,216 cycles

R3 DOOR AFT LOWER FUSELAGE FRAME WEB CRACKED AT BS 1310, BETWEEN LONGERONS 2R AND 27R. REPAIRED IAW SRM 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1C.

Part: HINGE — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP, INBD FORWARD HINGE, WING SIDE ACTUATOR INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE: DIA 1.246", FINAL HOLE: DIA 1.250", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0328311 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME DENTED AT LT STA 1059, LONGERON 12L. FRAME REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 66,872 hrs · 16,216 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1C.

Part: HINGE — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE ACTUATOR INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE: DIA 1.249", FINAL HOLE: DIA 1.252", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0328318 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.582", FINAL HOLE: DIA 0.598", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0328318 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ANGLE — DENTED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR ANGLE DENTED AT RT STA 1681, LONGERON 12R. FRAME ANGLE REMOVED PER SRM 51-33-01-0G AND REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE LOWER MOUNT OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE: DIA 0.707", FINAL HOLE: DIA 0.729", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0328311 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

MAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 755, X 75.25. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 725 TO EXISTING SPLICE AT STA 765 X= 75.25 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

MAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 1290, X 47.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1266 TO STA 1331 X= 47.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1818) · airframe 66,872 hrs · 16,216 cycles

SEAT TRACK FLANGE FOUND CORRODED AT BS 1818, RBL 47.5. REPAIRED 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 66,872 hrs · 16,216 cycles

MAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 5-10, X -47.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-63 TO EXISTING SPLICE AT STA 5-0 X= -47.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1818-1872) · airframe 66,872 hrs · 16,216 cycles

SEAT TRACK FLANGE FOUND CORRODED AT BS 1818 - 1872, LBL 47.5. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (MAIN CARGO) · airframe 66,872 hrs · 16,216 cycles

MAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 5-113, X 8.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-83 TO STA 5-123 X= 8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 66,872 hrs · 16,216 cycles

RIGHT WING LEADING EDGE CAVITY AT OUTBOARD OF SLAT TRACK NR 16 FORMER FOUND CRACKED. FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER PER DWG ARB2920 REVISION BB. INSTALLED FORMER AT RT WING L/E CAVITY AT O/B OF SLAT TRACK 16 AT XOS 1025.289 PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

MAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 6-10, X 8.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 6-40 TO EXISTING SPLICE AT STA 6-10 X= 8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 66,872 hrs · 16,216 cycles

HFEC INSPECTION CARRIED OUT ON LEFT WING FIXED LEADING EDGE AT CORNER 11, FUEL ACCESS DOOR FWD INBD CORNER AND FOUND ONE CRACK PROPAGATE FROM THE FASTENER HOLE APPROX. 3/8 INCH IN LENGTH, AT XOS 605.844. REPAIR CARRIED OUT PER SRM 57-40-01-2R FIG 201 REPAIR 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,872 hrs · 16,216 cycles

SEAT TRACK FLANGE FOUND CORRODED AT BS 1964 - 2000, X -107. REPAIR AS PER EA 1-5310-T0328362 P1. SEAT TRACK AT X=-107.5 - SPLICE REPAIR FROM STA 1831 TO STA 2007. REFER TO WRI: 53104412 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

MAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 775, X 75.25. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 816 TO EXISTING SPLICE AT STA 765 X= 75.25 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

MAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 5-11, X -27.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-63 TO EXISTING SEAT SPLICE AT STA 5.0 X= -27.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (ZONE 200) · airframe 66,872 hrs · 16,216 cycles

MAIN DECK SEAT TRACK CROWN AREA DAMAGED AT BS 1411, X -8.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1391 TO STA 1431 X= -8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,872 hrs · 16,216 cycles

SEAT TRACK FLANGE FOUND WITH CORROSION AT BS 1811, X 27.5. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1771 TO STA 1811 X= 27.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR — CRACKED (NLG) · airframe 66,434 hrs · 16,077 cycles

LEFT FWD NOSE GEAR DOOR CRACKED THROUGH 3 RIVETS. APPROXIMATELY 6-8" FROM L/E OF DOOR. REMOVED LT FWD NOSE GEAR DOOR IAW AMM 32-23-03-4. SENT TO SHEETMETAL SHOP. REMOVED DAMAGE ON LT FWD NOSE GEAR DOOR AND REPAIRED IAW SRM 52-00-00-2R.

Part: WIRE HARNESS — CHAFED (MLG) · airframe 66,387 hrs · 16,061 cycles

DURING APPROACH, AFTER ALL CHECKLISTS COMPLETED, WE HAD A GREEN BOX ON DU NR 3, BUT THEN, LANDING GEAR, BEGAN FLICKERING IN SIDE THE BOX INTERMITTENTLY. WE LOOKED AT THE LANDING GEAR SYNOPTIC. THE LT GEAR INDICATED RED FOR UNSAFE. WENT AROUND CYCLED GEAR FOR A NORMAL APPROACH AND LANDING. DUPLICATED FAULT BY SHAKING DOWN HARNESS. REPLACED LT GEAR SECONDARY DOWN AND LOCKED PROX SENSOR AND HARNESS ASSY PER AMM 32-61-15-4. PERFORMED RTS PER AMM 31-61-15-741-802. CK GOOD. REMOVED PART SENSOR P/N IDENTIFIABLE P/N 8-636-01, S/N A2767. A/C OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 65,760 hrs · 15,847 cycles

EMERGENCY LIGHT BATTERY 1 LOW. R & R EMER EXIT LIGHTS POWER SUPPLY IAW 33-51-01-5. OPERATIONS CHECKED NORMAL AT THIS TIME. OK FOR SERVICE.

Part: TIRE — FAILED (MLG) · airframe 65,075 hrs · 15,591 cycles

DURING LANDING, RECEIVED A LEVEL 2 ALERT, TIRE FAIL, ON LATTER PART OF THE ROLLOUT. LT CTR GEAR TIRE FAILURE. R & R ANTI-SKID CONTROL UNIT IAW AMM 32-45-01-04, STILL REQUIRES OPERATIONS CHECK. PERFORMED ANTI-SKID CONTROL UNIT ADJUSTMENT & TEST IAW AMM 32-45-01-5. ALL TEST PASSED AT THIS TIME. ALSO REF AMM 32-38-00-2 EXTENDED CTR GEAR FOR REVERSAL OF MEL. STILL REQUIRES SERVICING, DUE TO OTHER MX BEING PERFORMED ON MTSI 32-44-3245. SERVICED CTR LG SHOCK STRUT IAW AMM 32-15-01-3. ACCOMPLISHED ANTI-SKID ADJUSTMENT & TESTED IAW AMM 3245-00-5. TESTED NORMAL, NO FAULTS NOTED.

Part: TIRE — BLOWN (MLG) · airframe 647 hrs · 15,474 cycles

NUMBER 10 TIRE BLEW OUT DURING LANDING ROLLOUT. NR 10 WHEEL BRAKE DISABLED. INSPECTED CTR LANDING FOR ANY ANOMALIES FOR ASSOCIATED NR 10 BLOWN TIRE. INSPECTED BOTH NR 9 & 10 AXLE & INSPECTED CTR LG AS REQUIRED, NO DAMAGE FOUND. R & R BOTH NR 9 & 10 TIRE AS REQUIRED IAW MM 32-41-01-4. TIRE PRESSURES WITHIN SERVICEABLE LIMITS IAW SERVICE CHECK. REPLACED CTR GEAR ANTI-SKID HARNESS. REINSTALLED NR 9 & 10 WHEEL SPEED TRANSDUCERS & TIRE PRESS TRANSMISSIONS. HARNESS MPN AES9307-501 IAW AMM 32-45-03-4 & PASSED OPERATIONAL TEST AMM 32-45-00-5.

Part: FIRE LOOP — BROKEN (NR 3 ENGINE) · airframe 645 hrs · 15,412 cycles

ENGINE FIRE NR 3 SHUT DOWN ENG, NO FIRE INDICATION ON N1, N2 OR EGT. ALERT OCCURRED ON CLIMB OUT PASSING FL 220. CHECKED FDCU NR 3 & FOUND CURRENT FAULT LOWER TURBINE LOOP A & FIRE LOOP A. PERFORMED TROUBLESHOOTING & FOUND LOWER TURBINE LOOP A DH5 BROKEN. REPLACED SAME PARTS, NO CURRENT FAULT & RTS TEST PASSED.

Part: STRINGER — CRACKED (RT WING) · airframe 62,077 hrs · 14,647 cycles

DURING REMOVAL OF RT WING BEADED DOUBLER FOR REPAIR, STRINGER FOUND CRACKED BETWEEN XOS 670 TO 680. REPAIRED IAW SRM 57-40-03 REPAIR 2 FIG 202. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 785) · airframe 62,077 hrs · 14,647 cycles

MAIN DECK CARGO TRACK SPLICE FITTING WEB CRACKED AT BS 785, X -8. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: BEAM — CRACKED (ZONE 200) · airframe 62,077 hrs · 14,647 cycles

MAIN DECK CARGO R3 DOOR AFT LOWER BEAM FITTING CRACKED APPROX 5/8 INCH. BEAM REMOVED AND REPLACED IAW SRM 51-35-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BEAM — CRACKED (ZONE 200) · airframe 62,077 hrs · 14,647 cycles

MAIN DECK R3 DOOR AFT UPPER BEAM FITTING CRACKED APPROXIMATELY 5/8 INCH. REMOVED AND REPLACED IAW SRM 51-35-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 62,077 hrs · 14,647 cycles

RIGHT WING FIXED LE LOWER COMPARTMENT CRACKED ON BEADED DOUBLER XOS 670. REPAIR AS PER SRM 57-40-02 FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 62,077 hrs · 14,647 cycles

RIGHT DROOP LE EXTERIOR UPPER OTBD AREA STATION XDLE 327 CRACKED. REPAIRED IAW SRM 57-40-01, FIGURE 201, REPAIR 5. REPAIR CLASSIFIED MAJOR AS IAW GMM 6-2-100.

Part: TENSION TIE — CRACKED (RT WING TE FLAP) · airframe 62,077 hrs · 14,647 cycles

RIGHT WING OTBD TE FLAP INBD HINGE OTBD TENSION TIE FITTING CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01 AND AMM 57-53-01-4. LEAK CHECK CARRIED OUT IAW AMM 12-11-04, FOUND SATISFACTORY. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 62,077 hrs · 14,647 cycles

RIGHT FIXED WING LE LOWER COMPARTMENT, BEADED DOUBLER CRACKED, XOS 771 INBD OF SLAT TRACK 12. REPAIRED IAW SRM 57-40-02 REPAIR 15, FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 62,077 hrs · 14,647 cycles

LEFT WING FIXED LE LOWER COMPARTMENT, BEADED DOUBLER CRACKED, XOS 630. REFUEL PANEL COMPARTMENT. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 62,077 hrs · 14,647 cycles

MAIN DECK CARGO TRACK AT BS 635, X = 28 FOUND CRACKED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (ZONE 200) · airframe 62,077 hrs · 14,647 cycles

NR 3 LT PLUG DOOR JAMB CUT OUT AREA LOWER FWD WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 62,077 hrs · 14,647 cycles

RIGHT FIXED WING LE LOWER COMPARTMENT, BEADED DOUBLER CRACKED, XOS 907. STRAP FABRICATED IAW DRAWING ARB3954 REVISION K. STRAP REMOVED AND REPLACED IAW SRM 51-33-01. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 62,077 hrs · 14,647 cycles

RIGHT WING LE LOWER COMPARTMENT, BEADED DOUBLER CRACKED, XOS 614. REFUEL PANEL COMPARTMENT. REPAIR IAW SRM 57-40-02 REPAIR 15 FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (ZONE 200) · airframe 62,077 hrs · 14,647 cycles

NR 3 RT PLUG DOOR JAMB CUT OUT AREA LOWER FWD WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 755) · airframe 62,077 hrs · 14,647 cycles

MAIN DECK CARGO TRACK AT BS 755, X = 9 FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 62,077 hrs · 14,647 cycles

LEFT WING FIXED LE LOWER COMPARTMENT, BEADED DOUBLER CRACKED, XOS 667 OTBD OF SLAT TRACK 10. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 62,077 hrs · 14,647 cycles

RIGHT FIXED WING LE LOWER COMPARTMENT, BEADED DOUBLER CRACKED, XOS 614. REFUEL PANEL COMPARTMENT. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 62,077 hrs · 14,647 cycles

RIGHT FIXED WING LE LOWER COMPARTMENT, BEADED DOUBLER CRACKED, XOS 697 BETWEEN SLAT TRACK 10 & 11. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 62,077 hrs · 14,647 cycles

MAIN DECK CARGO TRACK AT BS 635, X = -28 FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 62,077 hrs · 14,647 cycles

MAIN DECK CARGO TRACK AT BS 635, X 47 SEAT TRACK FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (LT WING AILERON) · airframe 58,169 hrs · 13,435 cycles

LEFT WING OTBD AILERON INBD T/E UPPER AND LOWER SURFACE FOUND DELAMINATED. REPAIRED AS PER EA 1-5750-166108. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: SKIN — DELAMINATED (RT WING AILERON) · airframe 58,169 hrs · 13,435 cycles

RT WING OTBD AILERON INBD T/E UPPER SURFACE FOUND DELAMINATED. REPAIRED IAW EA 1-5750-166107. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: TRUNNION — CRACKED (NLG) · airframe 58,169 hrs · 13,435 cycles

NOSE LANDING GEAR LEFT TRUNNION ATTACHED FITTING FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: FILTER — FAILED (FUEL SYSTEM) · airframe 57,646 hrs · 13,289 cycles

ON TAKEOFF ROLL, AS POWER STABILIZED AT TAKE OFF THRUST, HAD A NR 1 FUEL FILTER ALERT. REJECTED TAKE OFF AT APPROX 30 KNOTS. R & R NR 1 ENG FUEL FILTER IN REF TO AMM 73-11-02-4-1. LEAK CHECKED GOOD. PERFORMED NR 1 ENG ADJ/TEST IN REF TO AMM 73-34-01-4-1, AMM 71-00-00-5-1 AND JRH. ALL TESTS PASSED. ACFT OK FOR SERVICE.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 54,992 hrs · 12,555 cycles

FOUND EMERGENCY EXIT LIGHT COVER ON LEFT ENTRY DOOR BROKEN. REMOVED AND REPLACED THE FWD DOOR EXIT LIGHT IAW AMM 33-52-05-2. PERFORMED OPS TEST IAW AMM 33-52-05-700-801. TEST CHECKED GOOD.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 53,665 hrs · 12,221 cycles

EXIT LIGHT COVER OVER FORWARD RT MAIN CABIN DOOR BROKEN OFF. INSTALLED NEW EXIT LIGHT COVER OVER R1 DOOR, IAW MM SMP. (CLOSED)

Part: LIGHT — NO TEST (CABIN) · airframe 53,616 hrs · 12,211 cycles

ON PREFLIGHT CHECK EMERGENCY LIGHT WILL NOT TEST. TROUBLE SHOT PER FIM 33-51-02. R & R EMERGENCY LIGHT BATTERY POWER SUPPLY PER MM 33-51-01-4, NO HELP. RE-INSTALLED ORIGINAL PART. REMOVED AND REPLACED MSC REF AMM 31-42-01-4, NO HELP. REINSTALLED ORIGINAL. ITEM REMAINS ON MEL.

Part: LONGERON SPLICE — CRACKED (L45L) · airframe 53,145 hrs · 12,100 cycles

LOWER CENTER CARGO COMPARTMENT STATION 5-123 LONGERON 45L SPLICE FITTING FOUND CRACKED. LOWER CENTRE CARGO COMPARTMENT STATION 5-123 LONGERON 45L DAMAGED SPLICE FITTING REMOVED AND REPLACED WITH NEW SPLICE AS PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112. NEW SPLICE FABRICATED AS PER DRAWING A5A7116 REVISION D.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 53,145 hrs · 12,100 cycles

LOWER CENTER CARGO COMPARTMENT STATION 5-123 LONGERON 38LH SPLICE FITTING FOUND CRACKED. LOWER CENTRE CARGO COMPARTMENT STATION 5-123 LONGERON 38LH SPLICE FITTING FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVISION 3. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 1239-1259) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN RIGHT HAND STATION 1239 TO 1259 X=-107.25 SEAT TRACK FOUND CORRODED. CABIN RIGHT BS 1239 TO 1259 X=-107.25 SEAT TRACK REPAIRED AS PER SRM 53-00-52 FIG 201 REVISION 46. SEAT TRACK FABRICATED AS PER DRAWING AEA7532 REVISION A. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SKIN — DENTED (NR 2 INLET) · airframe 53,145 hrs · 12,100 cycles

ENGINE NR 2 INLET NOSE COWL LEADING EDGE AREA AT APPROXIMATELY 1 O'CLOCK POSITION FOUND DENTED. ENGINE NR 2 INLET NOSE COWL LEADING EDGE DENT AREA REPAIRED AS PER SRM 54-10-01 FIG 202 REVISION 46. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 112. REPETITIVE VISUAL INSPECTION REQUIRED AT 'C' CHECK PER SRM 54-10-01 PAGE 207 REVISION 46.

Part: FLOORBEAM — CORRODED (BS 495) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN RIGHT STATION 495 X=-77.25 - X=-107.25 FLOORBEAM STRUCTURE FOUND CORRODED. CABIN RIGHT STATION 495 X=-77.25 TO X=-107.25 FLOORBEAM FABRICATED AS PER DRAWING ABA7363 REVISION D. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 46. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 420-450) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN RIGHT STATION 420 TO 450 X=-107.25 SEAT TRACK FOUND CORRODED. CABIN RIGHT STATION 420 TO 450 X=-107.25 SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 730-745) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN LT STATION 730 TO 745 X=8.5 SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53-00-52 FIG 201 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: SKIN — CRACKED (LT WING) · airframe 53,145 hrs · 12,100 cycles

05 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XORS=713.6. CARRIED OUT REPAIR AS PER DRAWING SG11570004 REVISION B. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 112.

Part: LONGERON SPLICE — CRACKED (CARGO BAY) · airframe 53,145 hrs · 12,100 cycles

LOWER CTR CARGO COMPARTMENT STATION 5-123, LONGERON 38LT SPLICE FITTING FOUND CRACKED. FABRICATED AS PER DRAWING A5A7114 REVISION 3. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 745) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN RT STATION 745 X =-8.5 SEAT TRACK FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-00-52 FIG 201 REVISION 46. SEAT TRACK FABRICATED AS PER DRAWING ACA7104 REVISION A. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 590) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN RT STATION 590 X=-27.5 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-00-52 FIG 201 REVISION 46. SEAT TRACK FABRICATED AS PER DOUGLAS DRAWING ACA7105 REVISION A. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 475) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN RT STATION 475 X=-27.5 SEAT TRACK FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. SEAT TRACK FABRICATED AS PER DRAWING ABA7684 REVISION A. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: LONGERON SPLICE — CRACKED (L45L) · airframe 53,145 hrs · 12,100 cycles

LOWER CENTER CARGO COMPARTMENT STA 5-123, LONGERON 45LT SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW SPLICE AS PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112. NEW SPLICE FABRICATED AS PER DRAWING A5A7116 REVISION D.

Part: SKIN — CRACKED (RT WING) · airframe 53,145 hrs · 12,100 cycles

05 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. CARRIED OUT REPAIR AS PER DRAWING SG11570004 REVISION B. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 470-485) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN LT STATION 470 TO 485 X=27.5 SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53-00-52 FIG 201 REVISION 46. SEAT TRACK FABRICATED AS PER DOUGLAS DRAWING ABA7684 REVISION A. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 435-455) · corrosion level 2 · airframe 53,145 hrs · 12,100 cycles

CABIN LT STA 435 TO 455 X=107.25 SEAT TRACK FOUND CORRODED. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: FRAME — DENTED (BS 1741 L11R) · airframe 53,145 hrs · 12,100 cycles

CABIN RT STATION 1741 L-11 FRAME FOUND DENT. REPAIRED AS PER SRM 53-00-07 FIG 201 REVISION 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112. REPETITIVE INSPECTION AT 9500 AND INITIAL INSPECTION AT 14500 BY HFEC METHOD AS PER SRM 53-00-07 FIG 201 REVISION 46.

Part: FRAME — DENTED (BS 1721 L11R) · airframe 53,145 hrs · 12,100 cycles

CABIN RT STA 1721 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REVISION 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 112. REPETITIVE INSPECTION AT 9500 AND INITIAL AT 14500 BY HFEC METHOD AS PER SRM 53-00-07 FIG 201 REVISION 46.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (LT WINDSHIELD) · airframe 52,606 hrs · 11,959 cycles

LEFT WINDSHIELD HEAT FAILED IN ICING CONDITION, ASSOCIATED WITH SPARKS IN CAPTAIN'S FLOOR PAN. PERFORMED OPS CHECK OF LT WINDSHIELD ANTI-ICE IAW MM 30-41-01-4. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 51,618 hrs · 11,732 cycles

HYD 1 OFF ALERT IN CRUISE 2.7 G REMAINING IN TANK 1. ON FINAL HYD 1 FAIL ALERT 0.5 REMAINING IN TANK 1. ON FINAL HYD 1 FAIL ALERT 0.5 REMAINING IN TANK 1. FOLLOWED QRH PROCEDURES LANDED WITHOUT INCIDENT. REPLACED LT INBD FLAP ACTUATOR PRESSURE LINE IAW AMM 20-10-01-2-0. LEAK CHECK SATIS, ACFT OK FOR SERVICE.

Part: FITTING — CRACKED (ZONE 300) · airframe 47,748 hrs · 10,844 cycles

DURING OPEN HOLE INSP CRACKED FOUND ON LT SIDE BANJO FITTING SECOND FASTENER HOLE COMMON TO BANJO FITTING AND CARRY THROUGH STRUCTURE AFT ROW ON BANJO FITTING LAYER. REPAIR CARRIED OUT IAW EA 1-5530-132118. REPAIR CATEGORY B, ACCOMPLISH INITIAL INSP WITHIN 5400 FLIGHT CYCLES FROM EA RELEASE DATE (15 JULY 2009) AND REPETITIVELY THERE AFTER WITHIN 2700 FLIGHT CYCLE INTERVALS IAW DWG NR. SN10550000. REPAIR CLASSFIED AS MAJOR IAW GMM 6-2-100, REVISION 107.

Part: FITTING — CRACKED (ZONE 300) · airframe 47,748 hrs · 10,844 cycles

DURING OPEN HOLE INSP ON RT SIDE BANJO FITTING FASTENER HOLE COMMON TO REPAIR DOUBLER, CRACKED FOUND ON AFT FLANGE LOWEST FASTENER HOLE BANJO FITTING LAYER AT 3 AND 6 O'CLOCK POSITION. REPAIR CARRIED OUT IAW EA 1-5530-132118. REPAIR CATEGORY B, ACCOMPLISH INITIAL INSP WITHIN 5400 FLIGHT CYCLES FROM EA RELEASE DATE (15 JULY 2009) AND REPETITIVELY THERE AFTER WITHIN 2700 FLIGHT CYCLE INTERVALS IAW DWG NR SN10550000. REPAIR CLASSFIED AS MAJOR IAW GMM 6-2-100, REVISION 107.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

RIGHT WING INBOARD FLAP VANE LOWER AND UPPER SURFACE FOUND DELAMINATED AT BETWEEN NR 1 AND 2 VANE TRACK AREA. REMOVED AND REPLACED IAW AMM 27-50-22-4, REVISION 64. RT INBD FLAP VANE ADJUSTMENT AND TEST IAW WORK CARD NR E1-5750-7-5003 C3 PART 2.

Part: FITTING — CRACKED (ZONE 300) · airframe 47,748 hrs · 10,844 cycles

CRACKED INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON FIRST LAYER (SKIN) AT RT SIDE BANJO FITTING, AFT ROW LOWEST NR 4 FASTENER HOLE. REPAIR CARRIED OUT AS PER EA 1-5530-132118, REPAIR CATEGORY B, ACCOMPLISH INITIAL INSPECTION WITHIN 5400 FLT CYCLES FROM EA AND REPETITIVELY THERE AFTER WITHIN 2700 FLIGHT CYCLE INTERVALS AS PER DAC DRAWING NR SN10550000. REPAIR CLASSFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 47,748 hrs · 10,844 cycles

VERTICAL STABILIZER LT NR 4 FWD BANJO FITTING FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-20-00 FIGURE 3 VOLUME I, REVISION 40. REPAIR CATEGORY B, DAMAGE TOLERANCE INSPECTION REQUIREMENT INITIAL 5400 CYCLE, REPETITIVE 2700 CYCLE AS PER DRAWING NR SN10550000. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

CORROSION-UPPER BORE OF RT WING OTBD FLAP OTBD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT. REPAIR CARRIED OUT AS PER E.A. 1-5750-131727, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

CORROSION-BORE OF LT WING OTBD FLAP OTBD HINGE (WING MOUNTED) FWD ATTACHMENT LUG OTBD. REPAIR CARRIED OUT AS PER E.A. 1-5750-131724. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

CORROSION-OTBD BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) LWR ATTACHMENT. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

CORROSION-INBD BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) LWR ATTACHMENT. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

CORROSION-BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBD LUG. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 47,748 hrs · 10,844 cycles

CORROSION-LOWER BORE OF LT WING OTBD FLAP OTBD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT. REPAIR CARRIED OUT AS PER E.A. 1-5750-131724 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

CORROSION-BORE OF RT WING OTBD FLAP INBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBD. FOUND CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5750-131726, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 47,748 hrs · 10,844 cycles

CORROSION-UPPER BORE OF LT WING OTBD FLAP OTBD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT. REPAIR CARRIED OUT AS PER E.A. 1-5750-131724, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 47,748 hrs · 10,844 cycles

CORROSION-BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT OTBD LUG. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE — CORRODED (LT WING) · airframe 47,748 hrs · 10,844 cycles

CORROSION-BORE OF LT WING OTBD FLAP INBD HINGE (WING MOUNTED) PIVOT ATTACHMENT. REPAIR CARRIED OUT AS PER EA 1-5750-131725, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

CORROSION-BORE OF RT WING OTBD FLAP, OTBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBD LUG. REPAIR CARRIED OUT AS PER E.A. 1-5750-131727, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 47,748 hrs · 10,844 cycles

CORROSION-LWR BORE OF RT WING OTBD FLAP OTBD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT. REPAIR CARRIED OUT AS PER E.A. 1-5750-131727, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SUPPORT — CRACKED (ZONE 300) · airframe 47,748 hrs · 10,844 cycles

LT NR2 ENGINE INTAKE DUCT (INTERNAL) SUPPORT FRAME AT STA ZFR 2033 FOUND WITH CRACK. REPAIR CARRIED OUT AS PER E.A. 1-5530-132119, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: INTERCOSTAL — CRACKED (ZONE 300) · airframe 47,748 hrs · 10,844 cycles

RT NR 2 ENGINE INTAKE DUCT (INTERNAL) SUPPORT FRAME AT STA ZFR 2033 FOUND WITH CRACK. REPAIR CARRIED OUT AS PER E.A. 1-5530-132119, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: FITTING — CRACKED (ZONE 300) · airframe 47,748 hrs · 10,844 cycles

VERTICAL STABILIZER RT NR 4 FWD BANJO FITTING FOUND WITH CRACK. REPAIR CARRIED OUT AS PER SRM 55-20-00 FIGURE 3 VOLUME I, REVISION 40. REPAIR CATEGORY B DAMAGED TOLERANCE INSPECTION REQUIREMENT INITIAL 5400 CYCLE, REPETITIVE 2700 CYCLE AS PER DRAWING NR SN10550000. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SKIN — CRACKED (ZONE 700) · airframe 47,748 hrs · 10,844 cycles

CTR LANDING GEAR WHEEL WELL RT SIDEWALL DOUBLER ON CUTOUT CRACKED AT STA 1390. CUTOUT STA 1390 REPLACED AS PER SRM 51-31-01 VOLUME II, REVISION 40 AND SRM 51-33-01 VOLUME II, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.

Part: WEB — CRACKED (DOOR FRAME) · airframe 47,748 hrs · 10,844 cycles

CRACK INDICATION FOUND ON SECOND LAYER WEB AT 2 O'CLOCK POSITION DURING HFEC OPEN HOLE INSP ON 0.520 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLE NR B. MAIN CARGO DOOR LOWER JAMB NO.7 SUPPORT FITTING AT HOLE NO. B SECOND LAYER WEB REAMED TO DIAMETER 0.540 INCH AS PER SRM 51-31-01 VOLUME II, REVISION 40. REPAIR CARRIED OUT ON WEB AS PER E.A. 1-5310-132111, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6- 2-100, REVISION 107.

Part: WEB — CRACKED (DOOR FRAME) · airframe 47,748 hrs · 10,844 cycles

CRACK INDICATION FOUND ON FIRST LAYER WEB AT 5 O'CLOCK POSITION DURING HFEC OPEN HOLE INSP ON 0.520 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLE NR B. REAMED TO DIAMETER 0.540 INCH IAW SRM 51-31-01 VOLUME II, REVISION 40. REPAIR CARRIED OUT ON WEB IAW EA 1-5310-132111. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 107.

Part: WEB — CRACKED (DOOR FRAME) · airframe 47,748 hrs · 10,844 cycles

CRACK INDICATION FOUND ON FIRST LAYER WEB AT 7 O'CLOCK POSITION DURING HFEC OPEN HOLE INSP AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLE C. REPAIR CARRIED OUT ON WEB AS PER E.A. 1-5310-132111, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: STOP FITTING — CRACKED (ZONE 600) · airframe 47,748 hrs · 10,844 cycles

RT WING OTBD FLAP SECONDARY STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 47,748 hrs · 10,844 cycles

RT WING L/E LOWER ACCESS FOUND CRACKED AT APPROX XOS 612. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I, REVISION 40. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 107.

Part: FUEL TANK — VENTING (RIGHT) · airframe 46,999 hrs · 10,670 cycles

"TANK WING OVERFILL" AMBER LEVEL 2. COMPLIED WITH RED TABS. VISUALLY CONFIRMED FUEL VENTING FROM CARGO BAY WINDOW. FUEL VENTING FROM OVER TOP OF LT AILERON. RTB WITH FUEL DUMP OF APPROX 90,000 LBS. UNEVENTFUL LDG. NO FUEL VENTING AFTER FUEL DUMP. CREW ADVISED THAT AT TOP OF CLIMB FUEL APPROX 2000 LBS LESS THAN COMPUTED. COMPUTED FUEL BURN 7000 LBS EVERY 20 MIN & USING 10000 LBS IN 10 MIN. AT THE TIME THE TANK WING OVER FILL MESSAGE CAME ON NONE OF FILL VALVE ON. FUEL STILL COMING OUT OF VENT AFTER FUEL LEVEL DOWN TO 39000 LBS IN RT TANK. PER FIM 28-14 PAGE 172 PRESSURIZED MANIFOLD FOR APPROX 30 MIN NO FUEL MIGRATED BETWEEN TANKS. FILLED BOTH TANK 1 & TANK 3 TANK 1 AUTO SHUT OFF AT 39800 LBS & TANK 3 AUTO SHUT OFF AT 41500 LBS. COMPLIED WITH STEP 3 OF FIM 28-14 WITH NO DEFECTS NOTED. FILLED NR 2 TANK UNTIL FILL VALVE AUTO SHUTOFF. FILL VALVE CLOSED AT 65500 LBS. NO LEAKS NOTED OUT OF VENT. DEFUELING ACFT IN PREPARATION FOR TANK TEAM DEFUELED ACFT & MOVED TO HANGER. SUMPED FUEL TANKS. NR 2 AND 3 TANKS ARE OPEN AND VENTING.

Part: PRESSURE SWITCH — FROZEN (NR 3 ENGINE) · airframe 46,218 hrs · 10,484 cycles

LOW SPEED REJECTED T/O AT 75KT DUE TO LEVEL 2 ENGINE OIL FILTER 3 ALERT. COMPLETED RTO AND OIL FILTER CHECK LISTS. OIL TEMPS WERE ALL AT 65 DEGREES. ACFT COLD SOAKED FROM SITTING IN VERY COLD AIR FOR 2 DAYS. CONTACTED MX AND AGREED THAT PROBLEM WAS MOST LIKELY DUE TO COLD SOAK. SECOND T/O SUCCESSFUL. R&R SCAVENGE OIL FILTER ELEMENT PER MM 79-22-05-4-1 & OIL FILTER DIFFERENTIAL PRESSURE SWITCH PER MM 7 9-35-01-4 1 ON NR 3 ENGINE. NR 3 ENGINE RAN PER 340709 IAW JRH. LEAK CHECK OK

Part: PIN — INSTALLED (MLG) · airframe 43,818 hrs · 9,957 cycles

AFTER TAKEOFF AND GEAR RETRACTION. CENTER MAIN LANDING GEAR SHOWED RED. EXTENDED GEAR ALL POSITIONS GREEN. DUMPED 30K FUEL. RETURNED TO MEM LANDED UNEVENTFULLY. REMOVED CENTER LANDING GEAR SAFETY LOCK PIN. RETURNED TO SERVICE.

Part: CHAIN — FAILED (ZONE 200) · airframe 43,127 hrs · 9,806 cycles

DURING ESCAPE SLIDE/RAFT OPS CHECK, MED L1 FAILED TO DEPLOY IN EMERGENCY MODE. L1 DOOR AFT DRUM POWER DRIVE ROLLER CHAIN REMOVED AND REPLACED AS PER CMM 52-11-09. EMERGENCY OPERATIONAL TEST CARRIED OUT AS PER AMM 52-11-04-5.

Part: STRUT — CORRODED (ZONE 500) · airframe 43,127 hrs · 9,806 cycles

FOUND CORROSION, LT WING OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT AFT FASTENER HOLE. CORROSION REPAIRED AS PER EA 1-5750-117306, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 43,127 hrs · 9,806 cycles

MAIN DECK STA 755, X = 48, SEAT TRACK FOUND CRACKED. CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (TE FLAP) · airframe 43,127 hrs · 9,806 cycles

RT WING, INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 192. REPAIR CARRIED OUT AT RT WING INBOARD FLAP LOWER SURFACE DENT AREA AT XIFH 192 AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 43,127 hrs · 9,806 cycles

FOUND CORROSION, LT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT INBOARD CENTER FASTENER HOLE. CORROSION REPAIRED AS PER EA 1-5750-117305, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 43,127 hrs · 9,806 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING STRUT AFT FASTENER HOLE FOUND CORRODED. CORROSION AT LEFT WING OUTBOARD FLAP OUTBOARD HINGE AFT STRUT AFT HOLE REPAIRED AS PER FEDEX EA NR 1-5750-117303, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 43,127 hrs · 9,806 cycles

FOUND CORROSION LEFT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT INBOARD FORWARD FASTENER HOLE. MINOR CORROSION REPAIRED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER DRAWING ARC1984. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUT — CORRODED (ZONE 500) · airframe 43,127 hrs · 9,806 cycles

FOUND CORROSION, LT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT FORWARD FASTENER HOLE. CORROSION REPAIRED AS PER EA 1-5750-117306, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 43,127 hrs · 9,806 cycles

RT WING, LEADING EDGE LOWER ACCESS PANEL 618FB INBOARD FORWARD CORNER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE LOWER ACCESS PANEL 618FB INBOARD FORWARD CORNER AS PER EA 1-5740-117298, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,127 hrs · 9,806 cycles

MAIN DECK SEAT TRACK AT STA 1806 LBL 8 FOUND EXFOLIATION CORROSION. MAIN DECK SEAT TRACK REPAIR CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 43,127 hrs · 9,806 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING ARC4009 FORWARD INBOARD FASTENER HOLE FOUND CORROSION. LT WING, OUTBOARD FLAP R & R AS PER AMM 27-50-30-4. FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. TEST OF THE FLAP SYSTEM OPERATION/RANGE OF MOVEMENT CARRIED OUT AS PER AMM 27-50-00-710-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 43,127 hrs · 9,806 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING ARC4008 OUTBOARD FASTENER HOLE FOUND CORROSION. LT WING, OUTBOARD FLAP R & R AS PER AMM 27-50-30-4. FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. TEST OF THE FLAP OPERATION/RANGE OF MOVEMENT CARRIED OUT AS PER AMM 27-50-00-710-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ELEMENT — FAILED (CABIN AIR) · airframe 41,227 hrs · 9,366 cycles

AT SFS DURING PRE-FLIGHT, GOT AIR SYSTEM TEST FAIL. TRIED SECOND TIME WITH SAME ALERT. CALLED MX, THEY TEST AIR SYSTEM AND GAVE OK TO GO. UPON DEPARTURE DURING CLIMB, GOT AVIONICS FAN OVRD PASSING FL230 FOLLOWED SHORTLY BY LEVEL 2 AIR MANF 1 FAIL. FOLLOWED QRH AND RETURNED TO SFS. REMOVED AND REPLACED MANIFOLD FAILURE SENSING ELEMENT D1-44C, P/N 35663-2-255, PER MM 36-23-07-4. SYSTEM TEST PASSED AS PER MM 36-23-07-5, A/C OK FOR SERVICE.

Part: BRAKE — SEPARATED (NR 1) · airframe 40,017 hrs · 9,077 cycles

DURING TIRE CHANGE, FOUND THAT NR 1 BRAKE COMING APART REMOVED AND REPLACE NR 1 BRAKE PER AMM 32-43-01-4. OPS AND LEAK CHECK GOOD.

Part: DOUBLER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

RIGHT HAND WING - STA XOS 641 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 38,405 hrs · 8,697 cycles

SNRM N00670: RT WING - STA XOS 641 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED. SNRM N00670: COMPLIED WITH NR 1-5730-100726, TITLE: WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

LEFT HAND WING - STA XOS 639 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

RIGHT HAND WING - STA XOS 647 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

RIGHT HAND WING - STA XOS 761 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

LEFT HAND WING - STA XOS 761 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

LEFT HAND WING - STA XOS 701 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: SKIN — CRACKED (ZONE 600) · airframe 38,405 hrs · 8,697 cycles

SNRM N00669: RT WING - STA XOS 647 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED. SNRM N00669: COMPLIED WITH FEDEX EA NR1-5730-100726, TITLE: WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

RIGHT HAND WING - STA XOS 758 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

LEFT HAND WING - STA XOS 646 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

RIGHT HAND WING - STA XOS 701 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

RT WING - STA XOS 701 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED. COMPLIED WITH NR1-5730-103472, TITLE: WINGS, LEADING EDGE BEADED DOUBLER, PERMANENT REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 38,405 hrs · 8,697 cycles

SNRM N00639: LT WING - STA XOS 639 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED. SNRM N00639: COMPLIED WITH FEDEX EA NR1-5730-100725, TITLE: WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

LEFT HAND WING - STA XOS 628 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

LEFT HAND WING - STA XOS 671 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

RIGHT HAND WING - STA XOS 731 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

LEFT HAND WING - STA XOS 758 FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACKED.

Part: SPAR CAP — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

UPON REMOVAL OF LEFT HAND WING OUTBOARD ISLAND FOUND LOWER REAR SPAR CAP AFT FLANGE FROM STA XORS 1042 TO XORS 1045 WITH CRACKS AT FASTENERS HOLES.

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 38,405 hrs · 8,697 cycles

SNRM N00400: UPON REMOVAL OF LT WING OB ISLAND FOUND LOWER REAR SPAR CAP AFT FLANGE FROM STA XORS 1042 TO XORS 1045 WITH CRACKS AT FASTENERS HOLES. SNRM N00400: COMPLIED WITH FEDEX EA NR1-5710-103474, TITLE: WINGS - LT WING LOWER SPAR CAP AFT FLANGE CRACKING BETWEEN XORS = 1042 AND XORS=1045 REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

CRACK FOUND ON RT WING OUTBOARD END OF STRINGER S-16R LOCATED AT XORS 386 WITH CRACK LENGTH APPROX 13.5". SNRM N00239: CRACK AT RIGHT WING OUTBOARD END OF STRINGER S-16R LOCATED AT XORS 386. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. STRINGER 16 CLIP FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5720-102141, TITLE: WINGS, OUTER WING, STRINGER REPAIR/CLIP FABRICATION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00239: CRACK FOUND ON RT WING OB END OF STRINGER S-16R LOCATED AT XORS 386 WITH CRACK LENGTH APPROX. 13.5 INCHES.

Part: STRINGER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00257: CRACK FOUND ON LT WING OB END OF STRINGER S-43L LOCATED AT XORS 565 WITH CRACK LENGTH APPROX 1 INCH.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00245: CRACK FOUND ON RT WING OUTBOARD END OF STRINGER S-10R LOCATED AT XORS 760 WITH CRACK LENGTH APPROX 12". SNRM N00245: CRACK AT RIGHT WING OUTBOARD END OF STRINGER S-10R LOCATED AT XORS 760. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00245: CRACK FOUND ON RT WING OB END OF STRINGER S-10R LOCATED AT XORS 760 WITH CRACK LENGTH APPROX 12 INCHES.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

CRACK FOUND ON RT WING OUTBOARD END OF STRINGER S-13R LOCATED AT XORS 577 WITH CRACK LENGTH APPROX 6 INCHES.

Part: STRINGER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00259: CRACK FOUND ON LT WING OB END OF STRINGER S-9L LOCATED AT XORS 819 WITH CRACK LENGTH APPROX. 10.5 INCHES.

Part: STRINGER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

CRACK FOUND ON LT WING OUTBOARD END OF STRINGER S-43L LOCATED AT XORS 565 WITH CRACK LENGTH APPROX 1". SNRM N00257: CRACK AT LEFT WING OUTBOARD END OF STRINGER S-43L AT XORS 565. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00240: CRACK FOUND ON RT WING OUTBOARD END OF STRINGER S-9R LOCATED AT XORS 819 WITH CRACK LENGTH APPROX 12". SNRM N00240: CRACK AT RIGHT WING OUTBOARD END OF STRINGER S-9R LOCATED AT XORS 819. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00240: CRACK FOUND ON RT WING OB END OF STRINGER S-9R LOCATED AT XORS 819 WITH CRACK LENGTH APPROX 12 INCHES.

Part: STRINGER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

CRACK FOUND ON LT WING OUTBOARD END OF STRINGER S-14L LOCATED AT XORS 521 WITH CRACK LENGTH APPROX 14.5", SNRM N00254: CRACK AT LEFT WING OUTBOARD END OF STRINGER S-14L LOCATED AT XORS 521. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00190: RT WING: TELESCOPIC DUCT ACCESS DOOR CUTOUT OF FIXED LEADING EDGE SKIN (IB AND OB) FOUND CRACKED.

Part: STRINGER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00259: CRACK FOUND ON LT WING OUTBOARD END OF STRINGER S-9L LOCATED AT XORS 819 WITH CRACK LENGTH APPROX 10.5". SNRM N00259: CRACK AT LEFT WING OUTBOARD END OF STRINGER S-9L AT XORS 819. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00188: LT WING: TELESCOPIC DUCT ACCESS DOOR CUTOUT OF FIXED LEADING EDGE SKIN (IB AND OB) FOUND CRACKED.

Part: STRINGER — CRACKED (LT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00254: CRACK FOUND ON LT WING OB END OF STRINGER S-14L LOCATED AT XORS 521 WITH CRACK LENGTH APPROX. 14.5 INCHES.

Part: STRINGER — CRACKED (ZONE 600) · airframe 38,405 hrs · 8,697 cycles

SNRM N00248: CRACK FOUND ON RT WING OB END OF STRINGER S-11R LOCATED AT XORS 704 WITH CRACK LENGTH APPROX. 12 INCH. SNRM N00248: CRACK AT RT WING OB END OF STRINGER S-11R LOCATED AT XORS 704 REPAIRED IAW SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

CRACK FOUND ON RT WING OUTBOARD END OF STRINGER S-11R LOCATED AT XORS 704 WITH CRACK LENGTH APPROX 12 INCHES.

Part: STRINGER — CRACKED (RT WING) · airframe 38,405 hrs · 8,697 cycles

SNRM N00238: CRACK FOUND ON RT WING OUTBOARD END OF STRINGER S-13R LOCATED AT XORS 577 WITH CRACK LENGTH APPROX 6". SNRM N00238: CRACK AT RIGHT WING OUTBOARD END OF STRINGER S-13R LOCATED AT XORS 577. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SWITCH — OUT OF POSITION (MLG) · airframe 38,057 hrs · 8,625 cycles

AFTER TOUCHDOWN DECELERATING THROUGH ABOUT 110 KTS, GOT AN UNSAFE NOSE GEAR INDICATION (PRIMARY) WITH A "LANDING GEAR" AURAL ALERT. SECONDARY INDICATIONS WERE ALL GREEN. HORN COULD NOT BE SILENCED UNTIL FLAPS WERE RETRACTED. ACN RELEASED FOR SERVICE PER MEL/CDL: 32-61-01-01-A "MEL 32-61-01-01-A: NOSE GEAR POSITION INDICATION SENSOR, INOP. OBSERVE CARGO CONTAINER LOADING RESTRICTIONS AND VERIFY AFFECTED POSITIONS ARE VOIDED ON WEIGHT AND BALANCE". REMOVED GEAR PINS AFTER TOW. TROUBLESHOT AND FOUND THE PSEU IN THE ALT POSITION FOR GEAR INDICATION RE-POSITIONED GEAR INDICATION SWITCH ON THE PSEU TO THE "NORMAL" POSITION. PRIMARY INDICATION OPERATES "GOOD". SYNOPTIC DISPLAY IS "INOP".

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENGINE) · airframe 33,818 hrs · 7,646 cycles

FL290 GOT A LEVEL 1 ALERT "ENG 2 ANTI-ICE OFF". A FEW MINUTES LATER GOT A LEVEL 3 "ENG 2 ANTI-ICE DUCT" ALERT WHICH REQUIRED THE NR 2 ENG BE SHUT DOWN. DIVERTED TO RJBB. CHECKED INDIVIDUAL RESISTANCE AND FOUND OVERHEAT SENSOR D1-90 IS 4.8K OHM. REPLACED D1-90 PER MM 30-22-11-4 AND ALSO VISUAL INSPECTED DUCT FROM PANEL NR 364PR AND 364HR, FOUND NORMAL.

Part: RIB — CRACKED (ZONE 600) · airframe 33,757 hrs · 7,627 cycles

RT WING LEADING EDGE CAVITY RIB BETWEEN SLAT TRACK NR 16 AND NR 17 FOUND CRACKED AT EDGE. FABRICATED IAW DRAWING NR: ARB2920. RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II.

Part: RIB — CRACKED (ZONE 500) · airframe 33,757 hrs · 7,627 cycles

LT WING LEADING EDGE CAVITY BETWEEN SLAT TRACK NR 16 AND 17, FOUND RIB FLANGE CRACKED. FABRICATED AS PER DRAWING NR ARB2920. RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II.

Part: RIB — CRACKED (ZONE 500) · airframe 33,757 hrs · 7,627 cycles

LT WING LEADING EDGE CAVITY BETWEEN SLAT TRACK NR 17 AND NR 18 FOUND WITH RIB FLANGE CRACKED. FABRICATED AS PER DRAWING NR: ARB2920. RIBS PN ARB2920-41 AND ARB2920-47. REMOVED AND REPLACED IAW SRM 51-35-01 VOLUME II.

Part: SKIN — CHAFED (ZONE 500) · airframe 33,757 hrs · 7,627 cycles

LEFT WING: LEADING EDGE SLAT NR 1 INBOARD AREA LOWER SURFACE FOUND WITH CHAFFING MARK ABOVE SLAT TRACK NR 1. (OPEN)

Part: STRINGER — CHAFED (ZONE 400) · airframe 33,757 hrs · 7,627 cycles

NR 2 ENGINE RT THRUST REVERSER INTERIOR NR 3 STRINGER CHAFED. REMOVED AND REPLACED IAW SRM 51-35-02 VOLUME II.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 21 LT BARREL NUT BORE, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 34L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 3L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 31L, BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 35L. BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA#1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 23L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT BR 29L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 27L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 33L. BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR25L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR 34R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82994.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 32R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82994

Part: FITTING — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER CENTER SKIN PLANK NR 26 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 14L BARREL NUT BORE FOUND EXCEEDED LIMITS.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 28R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82994.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 19R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-83001.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RT UPPER AFT SKIN PANEL NR 35R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82994.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON RIGHT HORIZ STAB UPPER FRONT SPAR SKIN PLANK NR 1R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82997.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RT UPPER CENTER SKIN PANEL NR 23R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83001.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON LEFT HORIZ STAB UPPER AFT SKIN PLANK NR 28L, BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON RIGHT HORIZ STAB UPPER FORWARD SKIN PLANK NR 9R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON LEFT HORIZ STAB BORE NR 24L, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON LEFT HORIZ STAB UPPER AFT SKIN PANEL NR30L, BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82993.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RT UPPER CENTER SKIN PANEL NR 25R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83001.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON LT HORIZ STAB UPPER REAR SPAR NR 36L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82995.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 17R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-83001.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZ STAB RIGHT HORIZ STAB BORE NR 5R FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 13R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 21R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA1-5510-83001.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON RIGHT HORIZ STAB BORE NR 11R FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000.

Part: PANEL — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STAB LEFT BORE NR 24L FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82952.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND BORE NR 22L FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82952.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 16L, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 10L, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER CENTER SKIN PLANK NR 36R BARREL NUT BORE FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82996.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND BORE NR 6L FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82991.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER CENTER SKIN PLANK NR 1L BARREL NUT BORE FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82998.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 18L, FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82952.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 8L FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,757 hrs · 7,627 cycles

AFT FUSELAGE COMPARTMENT STATION 2007 RIGHT HAND BEAM APPROX X=20 FOUND VERTICAL L-ANGLE BRACKET SUSPECT CRACK AT THE TOP MOST EDGE. REPAIRED AS PER FEDEX EA 1-5310-83088.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 4R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-83000.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 8R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 2R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-83000.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 5L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82991.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 11L BARREL NUT FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82991.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 9L BARREL NUT BORE, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA1-5510-82991.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 13L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,757 hrs · 7,627 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 7L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 33,757 hrs · 7,627 cycles

MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT STA 1581 LBL 8. CUT AND REMOVED IAW SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-70-00 FIG 1 VOL I.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 33,757 hrs · 7,627 cycles

MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT STA 1686 RBL 28. CUT AND REMOVED IAW SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-70-00 FIG 1 VOL I.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 33,757 hrs · 7,627 cycles

MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT STA 1581 RBL 8. CUT AND REMOVED IAW SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-70-00 FIG 1 VOL I.

Part: BEAM — CRACKED (ZONE 200) · airframe 33,757 hrs · 7,627 cycles

AFT FUSELAGE COMPT STA 2007 RT BEAM APPROX X=20 FOUND VERTICAL L-ANGLE BRACKET SUSPECT CRACK AT THE TOP MOST EDGE AS MARKED. REPAIRED AS PER FEDEX EA 1-5310-83088.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 33,757 hrs · 7,627 cycles

FOUND WELL INTERIOR FWD RT SIDE WEB WITH DOUBLER CUT OUT. CRACKED AT LOWER FASTENERS HOLE LOCATION AS MARKED. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II.

Part: SKIN — DEFORMED (ZONE 200) · airframe 33,757 hrs · 7,627 cycles

FWD CABIN, L1 DOOR SKIN UPPER EDGE FOUND DEFORMED. REPAIRED IAW EA 1-5210-83093.

Part: BRACKET — BROKEN (ZONE 700) · airframe 29,728 hrs · 6,751 cycles

UNSAFE GEAR INDICATION LEFT MLG DURING GEAR RETRACTION AT 230 KTS. UPON LANDING FOUND LEFT MLG ELECTRICAL HARNESS AND BRAKE HYD HOSES SUPPORT BRACKET ATTACHMENT TO TORSION LINK DAMAGED. SUPPORT BRACKET AND WIRE HARNESS REPLACEMENT CARRIED OUT REFER TO WRI 32-10/9350 AND 32-60/9357, 32-60/9358 FOR WORK DETAILS LANDING GEAR EXTENSION AND RETRACTION CARRIED OUT AS PER MM 32-31-00, FOUND SATISFACTORY.

Part: STRINGER — CRACKED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING STRINGER 11 CRACKED. LEFT WING STRINGER 11 REPAIRED AS PER SRM 51-33-01 VOL 2.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B AFT MOUNT HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B AFT MOUNT HOLE CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75282 TITLE: WINGS - RIGHT O/B FLAP, O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75298 - WINGS - OUTBOARD TRAILING EDGE FLAPS, INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, - REPAIR.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER AFT MOUNT AFT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR.

Part: STRINGER — CRACKED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING STRINGER 12 SUSPECT CRACKED. LEFT WING STRINGER 12 REPAIRED AS PER SRM 51-33-01 VOL 2.

Part: FRAME — DENTED (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1601 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TITLE : FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAILED IN THE WORK STEPS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B FWD BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B FWD MOUNT HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B FWD MOUNT HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75282 TITLE WINGS - RIGHT O/B FLAP, O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B CTR BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER I/B SURFACE FWD SURFACE FOUND CORROSION. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-75296 TITLE: WINGS - O/B TRAILING EDGE FLAPS - I/B HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP AFT MOUNT AFT BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR.

Part: FRAME — DENTED (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

MAIN DECK LEFT FRAME INNER EDGE FOUND DENTED AT STA 1581 STRINGER 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL I AND FEDEX EA 1-5330-75320. FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAME BETWEEN STATIONS 5- 113 AND 1721 LEFT AND RIGHT AS DETAILED IN THE WORKSTEPS.

Part: FRAME — DENTED (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1581 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TITLE : FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAILED IN THE WORK STEPS.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

MAIN DECK FLOOR SUPPORT BEAM AT STA 635/ X = 8.5 FOUND CRACK AT THE EXISTING REPAIR SECTION. MAIN DECK FLOOR SUPPORT BEAM AT STA 635/ X = 8.5 FOUND CRACK AT THE EXISTING REPAIR SECTION REMOVED & REPAIR CARRIED OUT SECTIONAL REPLACED SEAT TRACK FROM STA 525 - STA 545 -X=8.5 AS PER MD11 SRM 53-70-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON EXISTING TRIMMED AREA AT STA 525 & STA 545 CRACK FREE CONDITION.

Part: FRAME — DENTED (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1681 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TITLE: FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAILED IN THE WORK STEPS.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING I/B FLAP O/B HINGE BRACKET (FLAP SIDE) LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75300 - WINGS - INBOARD TRAILING EDGE FLAP, LEFT HAND OUTBOARD BRACKET (FLAP SIDE), PIVOT BORE CORROSION - REPAIR.

Part: STRINGER — CRACKED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING STRINGER 10 END SUSPECT CRACKED. LEFT WING STRINGER 10 REPAIRED AS PER SRM 51-33-01 VOL 2.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B AFT BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER AFT MOUNT FWD HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER AFT MOUNT FWD HOLE CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75282 TITLE: WINGS - RIGHT O/B FLAP, O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING I/B FLAP O/B HINGE BRACKET MOST AFT UPPER BRACKET FOUND CRACKED. REPAIRED CARRIED OUT AT RIGHT WING I/B FLAP O/B HINGE AS PER EA 1-5750-75299, TITLE: WINGS - I/B T/E FLAP, O/B HINGE FAIRING (FLAP SIDE) UPPER AFT RIB - REPAIR.

Part: RIB — CRACKED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING I/B FLAP O/B HINGE BRACKET (FLAP SIDE) MOST UPPER AFT FAIRING SUPPORT BRACKET FOUND CRACKED. REPAIRED AS PER EA 1-5750-75304, TITLE: WINGS - T/E FLAPS - LEFT I/B FLAP - O/B HINGE BRACKET FAIRING - CRACK REPAIR.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,726 hrs · 6,750 cycles

LEFT MLG - W/W HYD SERVICING CONTAINER SUPPORT INBOARD ANGLE BRACKET CRACKED. REPAIRED AS PER EA 1-5310-75313, TITLE: FUSELAGE - LEFT WHEEL WELL - HYDRAULIC RESERVOIR SUPPORTING STRUCTURE - BRACKET REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (WING SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75297 - WINGS - OUTBD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER O/B FWD SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER I/B SURFACE FWD SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER O/B NUT SIDE SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (WING SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75297 - WINGS - OUTBD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR

Part: SEAT TRACK — CHIPPED (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

MAIN DECK SEAT TRACK AT STA 1239 RBL 27.5 WITH CROWN AREA EDGE CHIPPED. MAIN DECK STA 1239/ RBL 47.5 DAMAGED SEAT TRACK CARRIED OUT SECTIONAL REPAIR AS PER SRM 53-70-00 VOL 1.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: FRAME — WORN (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

AFT TAIL CONE FWD RT FRAME FOUND 2 EA STOP PLATE WORN. AFT TAIL CONE FWD RT FRAME 2 EA STOP PLATE REMOVED, FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER EA 1-5390-75285. FUSELAGE AERODYNAMIC FAIRING AFT TAILCONE ASSY PLATE.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING I/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HOLE FOUND CORROSION. CORROSION REMOVED AS PER EA 1-5750-75312, TITLE : WINGS - I/B TE FLAP - RT O/B BRACKET (FLAP SIDE) - PIVOT BORE CORROSION - REPAIR.

Part: PLATE — WORN (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

AFT TAIL CONE FWD RT FRAME FOUND 2 EA STOP PLATE WORN. AFT TAIL CONE FWD RH FRAME 2 EA STOP PLATE REMOVED, FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER (TITLE : FUSELAGE AERODYNAMIC FAIRING AFT TAIL CONE ASSY PLATE FABRICATION) EA 1-5390-75285.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LEFT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL & REPAIR.

Part: FITTING — CRACKED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP STOP FITTING FOUND CRACKED. LT WING O/B FLAP CRACKED STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II.

Part: CLIP — DAMAGED (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

FWD TAIL CONE LT AFT FRAME FOUND L-ANGLE BRACKET DAMAGED. FWD TAIL CONE LT AFT FRAME ANGLE BRACKET REMOVED AND REPLACED AS PER FEDEX EA 1-5340-75283 - FUSELAGE - AERODYNAMIC FAIRINGS - FORWARD TAILCONE ASSEMBLY - CLIP FABRICATION

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: CLIP — CRACKED (ZONE 200) · airframe 29,726 hrs · 6,750 cycles

AFT TAIL CONE RT UPPER SUPPORT STRUCTURE BRACKET FOUND CRACKED. AFT TAIL CONE RH UPPER SUPPORT STRUCTURE BRACKET REMOVED, FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER (TITLE: FUSELAGE AERODYNAMIC FAIRING AFT TAIL CONE ASSY CLIP FABRICATION) EA 1-5390-75284.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING I/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HOLE FOUND CORROSION. CORROSION REMOVED & REPLACED AS PER EA 1-5750-75312, TITLE : WINGS - I/B TE FLAP - RT O/B BRACKET (FLAP SIDE) - PIVOT BORE CORROSION - REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288. WINGS - LT O/B FLAP O/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LEFT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE CORROSION R & R AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281. RT OUTBD FLAP INBD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75281 TITLE WINGS - RT O/B FLAP I/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75281 TITLE WINGS - RT O/B FLAP I/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR.

Part: BRACKET — CORRODED (TE FLAP) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75282 TITLE WINGS - RT O/B FLAP - O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281. RT OUTBD FLAP INBD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR.

Part: SUPPORT — CRACKED (T/E FLAP) · airframe 29,726 hrs · 6,750 cycles

RT WING OUTBOARD FLAP INBOARD HINGE BRACKET SUPPORT RIB (INTERIOR) FOUND CRACKED. RT WING O/B FLAP ASSY REMOVED & REPLACED AS PER AMM 27-50-30, OPERATION TEST & ADJUSTMENT CARRIED OUT FOUND SATIS AS PER AMM 27-50-00. COMPLIED WITH EA 1-5750-7529.1 TE FLAPS O/B RT FLAP - BUILDUP OF THE NRC6753-506 ASSY FOR USE IN PLACE OF THE NRC6753-502 ASSY.

Part: WEB — CRACKED (TAILCONE) · airframe 29,726 hrs · 6,750 cycles

TAIL CONE CENTER FWD WEB FOUND CRACKED. AFT TAILCONE CENTER FWD WEB REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II.

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 29,726 hrs · 6,750 cycles

LT WING SLAT TRACK 16 I/B SUPPORT RIB FOUND CRACKED. LT WING SLAT TRACK NR 16 I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II.

Part: RIB — CRACKED (ZONE 600) · airframe 29,726 hrs · 6,750 cycles

RIGHT WING SLAT TRACK NR 16 I/B SUPPORT RIB FOUND CRACKED. RIGHT WING SLAT TRACK NR 16 I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,975 hrs · 5,616 cycles

FUSELAGE TRANSVERSE FRAME AT STA Y-1701 RT SIDE DENTED & CRACKED APPROX 2 INCHES LONG. R&R FRAME PER SRM 53-30-00 VOL I.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,975 hrs · 5,616 cycles

FUSELAGE TRANSVERSE FRAME LT CRACKED AT 2 PLACES STA Y= 535, LONGERON 19L-20L WAS 1.531 INCHES AND AT LONGERON 23L-24L WAS 2.781 INCHES. R&R FRAME PER DWG SRZ-53-503, SRM 51-21-01 VOL II.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,975 hrs · 5,616 cycles

FWD CABIN BOTTOM OF PORTABLE FIRE EXTINGUISHER MOUNTING BRACKET, FOUND SEAT TRACK CORRODED AT BS 475-495. R&R SEAT TRACK PER SRM 51-33-01 VOL II.

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 22,370 hrs · 5,027 cycles

2-2 ALERT BELL NR 2 THROTTLE TO IDLE AND LIGHT WENT OUT. ENGINE IND NORMAL. SHUTDOWN NR 2.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 22,311 hrs · 5,009 cycles

ON FINAL FLAPS GOT DISAGREE ALERT. CHECKED CFDS, NO FAULT FOUND PERFORMED TEST ON PSEU PER FIM 31-71-07-00.

Part: STALL WARNING — FAULTY (COCKPIT)

ON SHORT FINAL GOT STICK SHAKER. AMBER SLATS WERE ILLUM ON PFD. PREF RTS ON FCC NR 1 AND 2 AOA TESTS AND AUTOLAND TESTS ALL PASSED OK TO CONTINUE.

Part: PUMP — OVERTEMP (NR 2 ENGINE) · airframe 19,834 hrs · 4,460 cycles

AFT T/O HYD NR 2 LEFT PUMP OFF FOR HIGH TEMP. SWITCH TO AUTO PUMPS TURNED OFF, TEMP WENT BACK UP AGAIN.

Part: SENSING ELEMENT — FAULTY (NR 3 ENGINE) · airframe 19,665 hrs · 4,419 cycles

LEVEL 3 ENG 2 A-ICE DUCT ALERT IND. SHUTDOWN ENG 3. *S/D* REMOVED AND REPLACED SENSING ELEMENT D190 (LOWER SIDE) PER MD11 MM 30-22-11-4.

Part: MANIFOLD — BROKEN (NR 2 ENGINE)

LEVEL 1 ALERT HYDRO 2 QTY LOW. FOUND HYD LEAK FROM NR 2 EDP MANIFOLD ASSY. REMOVED AND REPLACED PER MM 29-12-30-21, 29-11-20. NO LEAK FOUND.

Part: ENGINE — OVERHEATED (NR 1)

ON T/O, NR 1 ENGINE OVERHEATED (MASTER CAUTION, LEVEL 3 ALERT). REMAIN HIGH UNTIL THROTTLE RETURN TO IDLE, ENGINE SHUTDOWN. NO LEAK AND CRACK NOTED. EGT WITHIN LIMIT PER JRH ENGINE TEST AND CKS PG 608 FIG 3. CLOSED NR 1 ENGINE PER MM 71-1-00. AC OK FOR SERVICE.

Part: ENGINE — OVERHEATED (NACELLE)

ON T/O MSL ENGINE OVERHEATED (MASTER CAUTION & EGT ALERT) REACH 966C. REMAIN HIGH, ENG SHUTDOWN.

Part: SEAT TRACK — CRACKED (BS 635)

SNRM 431, 430, 355, 354 CRACK ON SEAT TRACK BS 635, X=8.5 RT, X=47.5 RT, X=27.5 LT, X=47.5 LT. REPAIRED SEAT TRACK IN ACCORD WITH SRM 53-70-00.

Part: FILTERS — CONTAMINATED (1, 2 & 3 ENGINE)

LEVEL 1 ENG 3 FUEL FILTER ALERT AND LEVEL 1 FUEL CONTAMINATION ALERT DISPLAY. CREW DUMP FUEL TO REDUCE DOWN TO MAX WT. REMOVED AND REPLACED ALL THREE ENG FILTERS PER 73-11-04-04-1.

Part: FIRE LOOP — FAILED (NR 2)

98-219 - FIRE DET 2 FAIL ILLUM ON T/O B LOOP WAS PLACARD INOP FOR DISPATCH. REMOVED AND REPLACED A LOOP HARNESS 224W9726-517. REMOVED AND REPLACED UPPER LT DET ASSY P/N 224-9743-509, SYS, OPS CHECK GOOD.

Part: RETRACT MECH — SLOW (LANDING GEAR)

ARRIVAL, GEAR HANDLE DOWN AND IN-GEAR DID NOT EXTEND ALL RED LIGHT, CONFIRMED GEAR WAS STILL UP ON CONFIG PAGE. CYCLE GEAR, GEAR CAME DOWN MUCH SLOWER THAN NORMAL, NOSE FIRST, CENTER, THEN MAIN. HYDRO PRESS NORMAL.

Part: NOSE COWL — SEPARATED (NR 2 ENGINE)

EN ROUTE FROM VANCOUVER TO MEMPHIS, THE TOP OF THE NR 2 ENGINE INTAKE COWLING SEPARTED FROM THE AIRCRAFT, RESULTING IN DAMAGE TO NOSE COWL AND THE LEADING EDGE OF THE VERTICAL STABILIZER. NOSE COWL REMOVED AND REPLACED. BULKHEAD BLANKETS REPLACED AND REPAIRED, RESEALED BY DOUGLAS SUPPORT TEAM PER FAA FORM 337 DATED 14 DEC 1995 DOCUMENTS ON FILE. SECONDARY DAMAGE TO VERTICAL STAB LEADING EDGE REPAIRED AND REPLACED PER DOCUMENTATION NOTED ABOVE.

Part: INTAKE COWL — SEPARATED (NR 2 ENGINE)

EN ROUTE FROM VANCOUVER TO MEM, THE TOP OF THE NR 2 ENGINE INTAKE COWLING SEPARATED FROM THE A/C RESULTING IN DAMAGE TO THE NOSE COWL AND THE LEADING EDGE OF THE VERTICAL STABILIZER.