N628FE

Part: CONTROL PANEL — CONTAMINATED (APU FIRE WARNING) · airframe 111,622 hrs · 23,127 cycles

APU FIRE LEVEL 3 ALERT, MASTER WARNING ILLUMINATED, APU FIRE AURAL WARNING SOUNDED AND APU FIRE INDICATION IN APU FIRE HANDLE ILLUMINATED NEAR RZC AT FL350 CRUISING AT .85M. CONFIRMED INDICATIONS WITH F/O AND PERFORMED PHASE 1 BY PULLING AND ROTATING APU FIRE HANDLE TO DISCHARGE AGENT. WHEN INDICATIONS DID NOT SUBSIDE, CONFIRMED & ROTATED HANDLE TO DISCHARGE SECOND AGENT REMOVED APU GROUND FIRE CONTROL PANEL IAW MM 26-21-10-4. NO DEFECTS OR CORROSION FOUND. ENTIRE PANEL & WIRES FOUND CONTAMINATED WITH FLUID. CLEANED PANEL IAW SWPM 20-00-09. REINSTALLED PANEL IAW MM 26-21-10-4.

Part: TRUNNION — CRACKED (NLG) · airframe 110,120 hrs · 22,651 cycles

NOSE LANDING GEAR WHEEL WELL - LEFT HAND TRUNNION STATION 584 AREA FOUND WITH CRACK PROPAGATION. NOSE LANDING GEAR WHEEL WELL - LEFT HAND TRUNNION STATION 584 AREA REPAIR CARRIED OUT AS PER EA 1-5340-T0301502 B P3 TITLE : FUSELAGE - ATTACH FITTINGS - LH NLG TRUNNION FITTING SRM REPAIR EXCEPT WITH 2 EXTRA FASTENER HOLES OUTSIDE PITCH AND AND ED LIMITS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT ANGLE — CRACKED (BS 1236) · airframe 110,120 hrs · 22,651 cycles

LEFT HAND FUSELAGE INTERIOR - UPON REMOVAL OF BLADDER CELL FOUND CENTER WING LOWER BARREL STRUCTURE SUPPORT ANGLE AT APPROXIMATE STATION 1236.8 CRACKED. LEFT HAND FUSELAGE INTERIOR BLADDER CELL CENTER WING LOWER BARREL STRUCTURE STATION 1236.8 SUPPORT ANGLE ( FITTING ) REMOVED AND REPLACED AS PER SRM 51-33-01- 0G . FABRICATED SUPPORT ANGLE ( FITTING ) AS PER DOUGLAS DRAWING AYB 7052 REVISION REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 110,120 hrs · 22,651 cycles

LOWER FORWARD CARGO COMPARTMENT BILGE STATION 939 , X = -5 , FLOOR BEAM FOUND CRACK . LOWER FORWARD CARGO COMPARTMENT BILGE STATION 939, X = -5 CRACKED FLOOR BEAM CARRIED OUT REPAIR AS PER SRM 53-00-00-2R REPAIR GENERAL FIGURE 210 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,120 hrs · 22,651 cycles

LOWER AFT CARGO COMPARTMENT STATION 1841, X 8 FRAME FLOOR SUPPORT FOUND WITH SURFACE CORROSION. LOWER AFT CARGO COMPARTMENT STATION 1841 X 8 FRAME FLOOR SUPPORT SURFACE CORROSION REMOVED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202 REPAIR GENERAL AT X = 8. REPAIR CARRIED OUT AS PER EA # 1-5310-T0360997P1 TITLE: " FUSELAGE - MAINFRAME - CENTER CARGO COMPARTMENT - CORROSION FOUND ON STA 1841 BULKHEAD SUPPORT BETWEEN X = 0 AND X = 10.000". REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100. REFER SNRM # N00748 FOR REPAIR DETAILS WO # 00079140.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,120 hrs · 22,651 cycles

LOWER AFT CARGO COMPARTMENT STATION 1841, X=0 FRAME FLOOR SUPPORT FOUND WITH SURFACE CORROSION. LOWER AFT CARGO COMPARTMENT STATION 1841 X = 0 FRAME FLOOR SUPPORT SURFACE CORROSION REMOVED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R, FIGURE 202 REPAIR GENERAL AT X = 0. REPAIR CARRIED OUT AS PER EA # 1-5310 - T0360997P1 TITLE: "FUSELAGE - MAINFRAME - CENTER CARGO COMPARTMENT - CORROSION FOUND ON STA 1841 BULKHEAD SUPPORT BETWEEN X = 0 AND X = 10.000". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 100) · airframe 110,120 hrs · 22,651 cycles

LOWER FORWARD CARGO COMPARTMENT BILGE STATION 6-0 LONGERON 44 LEFT SPLICE FITTING FOUND WITH CRACK.. LOWER FORWARD CARGO COMPARTMENT STATION 6-0 TO STATION 6-10 LONGERON 44 LEFT SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01-0G . FABRICATED SPLICE FITTING AS PER DOUGLAS DRAWING ADA 8424 REVISION A .REPAIR CLASSIFIED AS MAJOR PER PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 110,120 hrs · 22,651 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 655 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2100.

Part: SKIN — CRACKED (RT WING) · airframe 110,120 hrs · 22,651 cycles

CRACK FOUND APPROXIMATELY 1.1 INCH IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE CUTOUT NUMBER 5 AT XOS XOS 490 SLAT DOOR. RIGHT HAND WING FIXED LEADING EDGE CUTOUT NUMBER 5 AT XOS 490 SLAT DOOR REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 17 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 110,120 hrs · 22,651 cycles

RIGHT HAND WING DROOPED LEADING EDGE UPPER SKIN TRAILING EDGE FOUND CRACK AT XDLE 319. RIGHT HAND WING DROOPED LEADING EDGE UPPER SKIN TRAILING EDGE AREA AT XDLE 319 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 110,120 hrs · 22,651 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231LF AT STATION 675 TO STATION 735 FOUND DELAMINATED. DELAMINATED FLOOR PANEL #231LF AT CABIN STATION 675 TO STATION 735 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL #231LF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #231LF INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 110,120 hrs · 22,651 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT STATION XOS 650. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 650 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2100.

Part: DOUBLER — CRACKED (RT WING) · airframe 110,120 hrs · 22,651 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT AT STATION XOS 545 BEADED DOUBLER FOUND CRACKS. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 545 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 110,120 hrs · 22,651 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231HF AT STATION 595 TO STATION 675 FOUND DELAMINATED. DELAMINATED FLOOR PANEL #231HF AT CABIN STATION 595 TO STATION 675 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL #231HF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #231HF INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 110,120 hrs · 22,651 cycles

CABIN - LEFT HAND MAINFRAME AT STATION 5-32 LONGERON 12 LEFT FRAME FOUND DENT. CABIN - AT LEFT HAND MAINFRAME STATION 5-32 LONGERON 12 LEFT , DENTED FRAME 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 OUT AS PER SRM 53-00-07- 2R TABLE 201 REPAIR 2 - METHOD HIGH FREQUENCEDDY CURRENT. CURRENT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1761) · airframe 110,120 hrs · 22,651 cycles

CABIN - LEFT HAND MAIN FRAME AT STATION 1761 LONGERON 12 LEFT EXISTING REPAIR ANGLE ANGLE FOUND DENT. CABIN - AT LEFT HAND MAINFRAME STATION 1761 LONGERON 12 LEFT , DENTED EXISTING REPAIR ANGLE REMOVED AS PER SRM 51-31-01-0G AND 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 TABLE TABLE 201 REPAIR 2 - METHOD HIGH FREQUENCY EDDY CURRENT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: UNKNOWN — ODOR (CABIN) · airframe 105,841 hrs · 21,362 cycles

SMELLED AN ODOR DURING TAKEOFF SIMILAR TO DEICING FLUID OR OIL IN THE AIR SYSTEM . NOT SIGNIFICANT UNTIL WE BEGAN DESCENT INTO IAD. DONNED OXYGEN AND DECLARED AN EMERGENCY FOR PRIORITY.STILL APPARENT WHEN MECHANICS BOARDED THE AIRCRAFT. T/S PERFORMED REMOVED AND REPLACED ALL 3 WATER COALESOR BAGS M/M 21-54-05-2. RAN ENGINES PER J.R.H. ISOLATED BLEED SYSTEM FOUND ODER COMING FROM NR 1 BLEED. OPEN NR 1 ENGINE COWL AND INSPECTED ENGINE FOR OIL LEAK AND CHECKED DUCTS NONE FOUND COWLING SECURED CLOSED. M/M 71-10-00-2-2. FUTHER T/S REQUIRE. PERFORMED AIR CONDITIONING PACK AND DISTRIBUTION DUCT CLEANING M/M 21-53-00-7 OPS CHECKED NORMAL.

Part: ENGINE — DAMAGED (NR 2) · airframe 105,770 hrs · 21,338 cycles

PDIS 628 79-32 7899 02JUL19 BOS OPEN U LOGPAGES:2725454 ENG 2 RPM LO, FOLLOWED BY ENG 2 OIL PRESSURE LO, OIL PRESSURE WAS "0". PRECAUTIONARY MANUAL SHUTDOWN. FL310 @0030Z REMOVED NO 2 ENG IAW W/C 71T0002-PW. INSTALLED NO 2 ENGINE REF W/C 71T0902-PW. A/C IS OK FOR SERVICE

Part: SEAT TRACK — CORRODED (BS 450) · corrosion level 2 · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR CURVE SEAT TRACK AT STATION 450 X=-107.25 FOUND CORROSION. MAIN DECK CORRODED FLOOR CURVE SEAT TRACK AT STATION 450 X= -107.25 CARRIED OUT REPAIR FROM STATION 431 TO STATION 485 X = - 107.25 AS PER EA # 1-5310-T0345982 PART 1 TITLE - "FUSELAGE - MAINFRAME - EXFOLIATION CORROSION FOUND C/T MDC SEAT TRACK @ X = -107.25 , BETWEEN STA 440.344 AND STA 459.227". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X = - 47.5 FOUND CROWN DAMAGED AS MARKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 1531 / 5-0 TO STATION 5-23 X = - 47.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (LT WING) · corrosion level 2 · airframe 105,318 hrs · 21,205 cycles

LEFT WING UPPER WING SKIN AT XORS 252 FOUND CORROSION LEFT WING UPPER WING SKIN AT XORS 252 CORROSION REMOVED AS PER SRM 51-21-01-0G. ORIGINAL THICKNESS 0.237" REMAINED 0.091" MATERIAL REMOVED 0.146". LENGTH 3.7" WIDTH 3.5" FOUND EXCEEDED LIMIT PER SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101. REWORKED AREA REPAIR PERFORMED AS PER EA 1-5730-T0345910 P1 TITLE : WINGS - PLATES AND SKINS - LH WING - CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER JUST AFT OF INNER REAR SPAR REFERENCE LINE. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 105,318 hrs · 21,205 cycles

RIGHT WING UPPER WING SKIN AT XORS 253 FOUND CORROSION RIGHT WING UPPER SKIN AT XORS 253 CORROSION REMOVED AS PER SRM 51-21-01-0G ORIGINAL THICKNESS : 0.131" REMAINED : 0.050" MATERIAL REMOVED : 0.081" LENGTH : 6" WIDTH : 4" FOUND EXCEEDED LIMIT PER SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101. REWORKED AREA REPAIR PERFORMED AS PER EA 1-5730-T0345911 P1 TITLE : WINGS - PLATES AND SKINS - RH WING - CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN STRINGER NO.1 AND INNER REAR SPAR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

01 EACH FASTENER HOLE FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700 REPAIR CARRIED OUT ON 01 EACH FASTENER HOLE AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS 690 AND STATION XORS 700 AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 2,000 FLIGHT CYCLES AFTER COMPLETION OF THIS REPAIR AND REPETITIVE INSPECTION AT EVERY 2,000 FLIGHT CYCLES BY HFEC INSPECTION METHOD PER SRM 57-20-02- 2R TABLE 201 REPAIR 5.

Part: STRINGER — CRACKED (ZONE 100) · airframe 105,318 hrs · 21,205 cycles

CENTER UPPER AUXILIARY TANK STRINGER 47 XCW 46.5 TO XCW 50.5 FOUND CRACK CRACK STRINGER AT CENTER UPPER AUXILIARY TANK STRINGER 47 XCW 46.5 TO XCW 50.5 CARRIED OUT REPAIR AS PER MD-11 SRM 57-10-03-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DAMAGED (BS 535) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 19 LEFT EXISTING REPAIR OUTER ANGLE FOUND DAMAGED. MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 19 LEFT CARRIED OUT REPAIR AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24L EXISTING REPAIR OUTER ANGLE FOUND DAMAGED. MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24L CARRIED OUT REPAIR AS PER EA # 1-5310-T0318700A P2 TITLE : "FUSELAGE - MAINFRAME - FORWARD FUSELAGE - EXISTING REPAIR FOUND AT STA 535 FRAME AT L-24L - DEVIATION TO SRM REPAIR". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 105,318 hrs · 21,205 cycles

RIGHT WING - LEADING EDGE NO 12 SLAT TRACK CUTOUT LOWER OUTBOARD CORNER SKIN FOUND CRACK AT XOS 776.5 . REPAIR CARRIED OUT ON RIGHT WING LEADING EDGE NO 12 SLAT TRACK CUTOUT LOWER OUTBOARD CORNER SKIN AT STATION XOS 776.5 AS PER SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 105,318 hrs · 21,205 cycles

RIGHT WING - FIXED LEADIING EDGE BEADED DOUBLER AT XOS 711 FOUND CRACK . REPAIR CARRIED OUT ON RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 711 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 755 X = -8.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STATION 745 TO STATION 783 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 623 FOUND CRACKED.

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING - FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK . DOUBLER ON LEFT WING - FIXED LEADING EDGE AT STATION XOS 667 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DRAWING ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 613 FOUND CRACK. REPAIR CARRIED OUT ON LEFT WING FIXEDLEADING EDGE BEADED DOUBLER AT XOS 613 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 623 FOUND CRACKED . REPAIR CARRIED OUT ON LEFT WING -FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 623 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 587 FOUND CRACK . REPAIR CARRIED OUT ON LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 587 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 105,318 hrs · 21,205 cycles

RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 694 FOUND CRACK . REPAIR CARRIED OUT ON RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 694 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 105,318 hrs · 21,205 cycles

RIGHT WING - LEADING EDGE NO.14 SLAT TRACK CUTOUT LOWER OUTBOARD CORNER SKIN FOUND CRACKED AT XOS 891 . REPAIR CARRIED OUT ON RIGHT WING - LEADING EDGE NO.14 SLAT TRACK CUTOUT LOWER OUTBOARD CORNER SKIN AT STATION XOS 891 AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1974) · corrosion level 2 · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR CURVE SEAT TRACK AT STATION 1974 X = 107.25 FOUND CORROSION. MAIN DECK FLOOR CURVE SEAT TRACK FROM STATION 1751 TO STATION 2007 X = 107.25 CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AS PER 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 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 745 X = 75.25 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK REPAIR CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. FROM STATION 725 TO STATION 765 X = 75.25. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (NOTE - NON ROUTINE NUMBER ENTERED IN ERROR, TO BE CORRECTED WITH NON ROUTINE NUMBER -N00858)

Part: DOUBLER — CRACKED (RT WING) · airframe 105,318 hrs · 21,205 cycles

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

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACK REPAIR CARRIED OUT ON LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 664 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 694 FOUND CRACK REPAIR CARRIED OUT ON LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 694 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DELAMINATED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING - TRAILING EDGE INBOARD ISLAND FIXED SKIN LOWER SURFACE FORWARD EDGE FINGER DOUBLER FROM XW 375 TO XW 399 FOUND DETACHED. REPAIR CARRIED OUT ON LEFT WING - TRAILING EDGE INBOARD ISLAND FIXED SKIN FROM STA XW 375 TO STATION XW 399 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DELAMINATED (RT WING) · airframe 105,318 hrs · 21,205 cycles

RIGHT WING - TRAILING EDGE INBOARD ISLAND FIXED SKIN LOWER SURFACE FORWARD EDGE FINGER DOUBLER FROM XW 375 TO WX 399 FOUND DETACHED. REPAIR CARRIED OUT ON RIGHT WING TRAILING EDGE INBOARD ISLAND FIXED SKIN FROM STATION XW 375 TO STATION XW 399 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 755 X = 47.5 FOUND CRACKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 725 TO STATION 785 X = 47.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 635 X = 27.5 FOUND CRACKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT FROM STATION 625 TO STATION 645 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 670 FOUND CRACK REPAIR CARRIED OUT ON LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 670 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 105,318 hrs · 21,205 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 650 FOUND CRACK REPAIR CARRIED OUT ON LEFT WING - FIXED LEADINIG EDGE BEADED DOUBLER AT STATION 650 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 755 X = -27.5 FOUND CRACKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT FROM STATION 745 TO STATION 783 X = -27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1351 X = -8.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STATION 1311 TO STATION 1391 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X= -8.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AS PER SRM 53-00-52-2R FIGURE 201 REPAIR1 FROM STATION 1531/5-0 TO STATION 5-23 X= -8.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1491 X = - 47.5 FOUND CORROSION AS MARKED. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT FROM STATION 1471 TO STATION 5-0 X = -47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X = 8.5 FOUND CROWN DAMAGED AS MARKED. MAIN DECK FLOOR SEAT TRACK REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STATION 1531 / 5-0 TO STATION 5-23 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1019) · corrosion level 2 · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1019 X= 8.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT AT STATION 1009 TO STATION 1029 X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 869 X = 8.5 FOUND CORROSION. MAIN DECK FLOOR CARRIED OUT SEAT TRACK REPAIR BY SECTIONAL REPLACEMENT FROM STATION 849 TO STATION 909 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 105,318 hrs · 21,205 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 6-40 X = -8.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK CARRIED OUT REPAIR BY SECTIONAL REPALCEMANT AT STATION 1129 / 6-0 TO STATION 6-60 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT WING) · airframe 105,212 hrs · 21,177 cycles

PDIS 628 30-10 7458 20FEB19 MSP FACT U LOGPAGES:3042522 DURING DESCENT RECIEVED LEVEL 2 WING A-ICE RIGHT DISAG R/I 20FEB19 09:50 MSP U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 3290278-1 CPN: 3000067 POS: NR 2 SRL: 417 TAG NR: 9C8178 ON MPN: 3290278-1 CPN: 3000067 SRL: 822 TAG NBR: 566D90 FACT 20FEB19 09:50 MSP U R&R THE RT WING ANTI ICE VALVE PER MM 30-11-00-2, PERFORMED OPS CK AND LEAK TEST AND OPS ARE GOOD. OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CABIN) · airframe 104,252 hrs · 20,862 cycles

INTERMITTENT CAB SMOKE WARNING THROUGOUT FLIGHT AND TAXI-IN. WARNING STAYED ON FOR ABOUT 1 SECOND. R&R NR 9 SMOKE DETECTOR, NOW TEST GOOD REF MM 26-15-01-4.

Part: TRUNNION — CORRODED (LT MLG) · airframe 103,319 hrs · 20,554 cycles

CORROSION WAS FOUND ON THE LT MLG TRUNION FAYING SURFACE. BORE HOLES ALSO HAD CORROSION. EA 1-3210-T0339350 ISSUED FOR REPAIRS. REPAIRED THE LT MLG A FRAME IAW SRM 57-20-14-2R, AND EA 1-3210-T0339350, PART 2.

Part: DOUBLER — CRACKED (RT WING) · airframe 101,093 hrs · 19,896 cycles

RIGHT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 625 - 627 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15 .THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 101,093 hrs · 19,896 cycles

ONE CRACK FOUND APPRROXIMATELY .250 INCH IN LENGTH ON THE RT WING FIXED LEADING EDGE, FUEL ACCESSS DOOR FORWARD INBD CORNER AT XOS 610. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 18. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1617) · corrosion level 2 · airframe 101,093 hrs · 19,896 cycles

MAIN DECK CARGO TRACK CORRODED AT BS 1617, RBL 75.25. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1591 - 1651 IAW SRM 53-00-52, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1721) · airframe 101,093 hrs · 19,896 cycles

MAIN DECK CARGO, FRAME DENTED AT BS 1721, LONGERON 12L. REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 101,093 hrs · 19,896 cycles

LEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 633 - 636 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON — CORRODED (BS 1954) · corrosion level 2 · airframe 101,093 hrs · 19,896 cycles

AFT CARGO BAY BS 1954, LONGERON 44R FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-00-2R, FIGURE 205. REPLACED THE LONGERON IAW EA1-5310-0333281, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 101,093 hrs · 19,896 cycles

ONE CRACK FOUND APPRROXIMATELY .500 INCH IN LENGTH ON THE LT WING FIXED LEADING EDGE SLAT ACTUATOR ACCESS DOOR FORWARD INBD CORNER AT XOS 490. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 17. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.

Part: LONGERON — CORRODED (BS 1954) · corrosion level 2 · airframe 101,093 hrs · 19,896 cycles

AFT CARGO BAY, BS 1954, LONGERON 45R FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-00-2R, FIGURE 205. REPLACEED THE LONGERON IAW EA 1-5310- T0333344, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1597) · corrosion level 2 · airframe 101,093 hrs · 19,896 cycles

MAIN DECK CARGO TRACK CORRODED BS 1597, RBL 75.25. THE CORROSION FOUND TO EXCEEDED THE LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (BS 1215) · airframe 101,093 hrs · 19,896 cycles

MAIN DECK CARGO TRACK CROWN AREA FOUND DAMAGED BS 1215, RBL 75.25. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 101,093 hrs · 19,896 cycles

RIGHT WING LEADING EDGE CAVITY AT XOS 614, BEADED DOUBLER CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 100,708 hrs · 19,784 cycles

DURING FINAL, SHORTLY AFTER SELECTING FLAPS 15, RECEIVED A LEVEL 2 SLATS DISAGREE & SPEED FOOT WENT UP TO APROXIMATELY 205. PERFORMED MISSED APPROACH AND FOLLOWED QRH. RECONFIGURED FOR SECOND APPROACH WITHOUT INCIDENT. EXTENDED LEADING EDGE SLATS AND PERFORMED VISUAL INSPECTION OF ALL LEADING EDGE SLATS IAW AMM 27-80-00-2. NO DEFECTS NOTED. PERFORMED FUNCTIONAL TEST OF PSEU IAW FIM 31-71-07-00. NO FAULTS FOUND. NO SLAT DISAGREE ALERT SHOWN AT THIS TIME. ACFT OK FOR SERVICE.

Part: BUTTON — DEFECTIVE (EVAC SLIDE) · airframe 99,256 hrs · 19,334 cycles

DURING PREFLIGHT, R1 DOOR ESCAPE SLIDE LIGHT DOES NOT TEST. REPLACED RT DOOR SLIDE PRESSURE LENS BUTTON. OPS CHECKS NORMAL IAW MM 25-61-04.

Part: TIRE — BLOWN (MLG) · airframe 972 hrs · 18,628 cycles

AFTER TOUCHDOWN ON LANDING ROLLOUT BELOW 60 KTS, NR 9 TIRE FAILURE ALERT. FOUND NR 9 TIRE BLOWN. R & R NR 9 & 10 TIRE IAW MM CHP 32-41-01-4. INTERROGATED CFDS NO ANTI-SKID FAULTS FOUND. PERFORMED ANTI-SKID RTS IAW MM CHP 32-45-01-5. PERFORMED AUTO BRAKE RTS IAW MM CHP 32-48-00-700, NO FAULTS FOUND. INSPECTED AIRFRAME, NO DAMAGE NOTED. PERFORMED HIGH ENERGY STOP INSPECTION IAW MM CHP 05-56-00-0, NO DEFECTS NOTED.

Part: SEAT TRACK — CRACKED (BS 755) · airframe 966 hrs · 18,441 cycles

CABIN SEAT TRACK FOUND CRACKED AT BS 755 X -8. REPAIR IAW SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 966 hrs · 18,441 cycles

CABIN SEAT TRACK FOUND CRACKED AT BS 635 X -8. REPAIRED IAW SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

FORWARD CARGO FLOOR SEAT TRACK FOUND CRACKED AT STATION 695 X= -8.0. CRACKED SEAT TRACK AT CABIN BETWEEN STA 624 STA 745 X= -8.5 CARRIED OUT REPAIR IAW SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6.2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

FORWARD CARGO FLOOR SEAT TRACK FOUND CRACKED AT STATION 635 X = 8.0. CRACKED SEAT TRACK AT FORWARD CARGO FLOOR STA 635 X= 8.5 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

FORWARD CARGO FLOOR SEAT TRACK FOUND CRACKED AT STATION 635 X= 47.5. CRACKED SEAT TRACK AT FWD CARGO FLOOR STA 635 X=47.5 REPAIRED AS PER MD11 SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA AT STATION 765, X = 75.25 FOUND DAMAGED. DAMAGED SEAT TRACK CROWN AT MAIN DECK CARGO COMPARTMENT STA 765, X = 75.25 CARRIED OUT REPAIR I.A.W SRM 53-00-52-2R REPAIR 1, FIGURE 201. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100

Part: WIRE — DAMAGED · airframe 966 hrs · 18,441 cycles

FOUND 14 TWISTED WIRES, OUTER PROTECTIVE INSULATION BADLY DETERIORATED AT ABOUT BS 495 - 555 FLOOR AREA. R & R IAW SWPM 20-10-01. CONTINUITY CHECKED IAW WDM 22-16-02, WDM 27-66-01, WDM 28-48-01, WDM 52-71-02, WDM 73-33-01, WDM 29-31-01 & WDM 79-33-01 FOUND SATISFACTORY. OPERATIONAL CHECK CARRIED OUT IAW AMM 52-70-00-05, AMM 22-01-10-5, AMM 28-4100-5, AMM 28-48-01.5 & AMM 71-00-00--5-1, FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CRACKED (TE FLAP) · airframe 966 hrs · 18,441 cycles

RIGHT OTBD FLAP, INBD FWD HINGE, OTBD SIDE LOAD FITTING CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 966 hrs · 18,441 cycles

RIGHT INBD FLAP, OTBD AFT HINGE, OTBD PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIR ACCOMPLISHED IAW EA1-5750-T0318614 PART 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

LEFT OTBD FLAP, OTBD AFT HINGE PIVOT, OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-04. EXISTING 1.141 INCH, FINAL 1.152 INCH & MAXIMUM ALLOWABLE 1.150 INCH. REPAIR ACCOMPLISHED IAW EA 1- 5750-T0318605 PART 1. REFER TO WRI 57502077 FOR WORK DETAILS. REPAIR CLASSIFIED A MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 966 hrs · 18,441 cycles

RIGHT INBD FLAP, OTBD AFT HINGE, INBD PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIR ACCOMPLISHED IAW EA 1-5750-T0318614 PART 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

LEFT INBD FLAP, OTBD AFT HINGE PIVOT, INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HALF HINGE LUG 1.252 INCH, STRAP 1.220 INCH, FINAL HALF HINGE LUG 1.284 INCH, STRAP 1.284 INCH & MAXIMUM ALLOWABLE 1.220 INCH. REPAIR ACCOMPLISHED IAW EA 1-5750-T0318612 PART 1. REFER TO WRI 57502083 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

LEFT INBD FLAP, OTBD AFT HINGE PIVOT, OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER, HALF HINGE LUG 1.281 INCH, STRAP 1.220 INCH, FINAL DIAMETER, HALF HINGE LUG 1.326 INCH, STRAP 1.326 INCH, MAXIMUM ALLOWABLE 1.220 INCH. REPAIR ACCOMPLISHED IAW EA 1-5750-T0318612 PART 1. REFER TO WRI 57502083 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1681) · airframe 966 hrs · 18,441 cycles

MAIN DECK CARGO BS 1681, LONGERON 12L FRAME. REPAIR FOUND DENTED. REPAIR REMOVED IAW SRM 51-31-01-0G & INSTALLED WITH NEW FABRICATED REPAIR DOUBLER IAW SRM 53-00-07-2R. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR INBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (BS 1661) · airframe 966 hrs · 18,441 cycles

MAIN DECK CARGO BS 1661, LONGERON 12L FRAME. REPAIR FOUND CHAFED. REPAIR REMOVED IAW SRM 51-31-01-0G & INSTALLED WITH NEW FABRICATED REPAIR DOUBLER IAW SRM 53-00-07-2R FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

RIGHT WING FLAP OTBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHINGS FABRICATED & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1701) · airframe 966 hrs · 18,441 cycles

MAIN DECK CARGO BS 1701, LONGERON 12L FRAME. REPAIR FOUND DENTED. FRAME TRIMMED OUT & REPAIRED IAW SRM 53-0-07-2R REPAIR 2 FIG 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 966 hrs · 18,441 cycles

RIGHT WING, OTBD FLAP OTBD FWD HINGE LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING 0.387 INCH, FINAL 0.405 INCH, MAXIMUM ALLOWABLE IS 0.391 INCH. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318565 P 1 STEP 1B. REFER TO WRI 57502076 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING) · airframe 966 hrs · 18,441 cycles

RIGHT WING, OTBD FLAP INBD FWD HINGE ACTUATOR INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER = 1.247 INCH, MAXIMUM ALLOWABLE =1.220 INCH. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1C. REFER TO WRI 57502078 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: REPAIR — CHAFED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

CABIN MAIN DECK CARGO COMPARTMENT LT STATION 535, LONGERON 24L FRAME. EXISTING REPAIR FOUND CHAFED. EXISTING REPAIR REMOVED. NEW REPAIR CARRIED OUT IAW EA 1-5310-TO318700 P 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. REFER TO WRI 53102075 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP INBD FWD HINGE PIVOT HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

RIGHT WING, OTBD FLAP OTBD FWD HINGE UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING IS 0.387 INCH, FINAL IS 0.405 INCH, MAXIMUM ALLOWABLE IS 0.391 INCH. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318565 P 1 STEP 1B. REFER TO WRI 57502076 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — GOUGED (RT WING) · airframe 966 hrs · 18,441 cycles

RIGHT WING, FIXED LE ABOVE NR 6 SLAT, FOUND WITH DEEP GOUGE AT XOS 855.964. REPAIRED IAW SRM 57-40-02-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: REPAIR — CHAFED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

CABIN MAIN DECK CARGO COMPARTMENT LT STATION 535, LONGERON 19L FRAME EXISTING REPAIR FOUND CHAFED. EXISTING REPAIR PARTS AT MAIN DECK CARGO COMPARTMENT LT STATION 535, LONGERON 19L ON FRAME REMOVED. NEW REPAIR CARRIED OUT IAW SRM 53-20-07-2R REPAIR 1 FIGURE 202. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 966 hrs · 18,441 cycles

RIGHT WING, OTBD FLAP INBD FWD HINGE PIVOT HOLE BORE CORROSION. CORROSION AT HOLE NR 4 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 2.313 INCH, FINAL DIAMETER = 2.316 INCH & MAXIMUM ALLOWABLE DIAMETER = 2.3135 INCH. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318610 P 1 STEP 1A. REFER TO WRI 57502078 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

RIGHT WING, OTBD LAP OTBD FWD HINGE LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING 0.0711 INCH, FINAL= 0.715 INCH, MAXIMUM ALLOWABLE= 0.709 INCH. SHOULDER BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1B. REFER TO WRI 57502078 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING) · airframe 966 hrs · 18,441 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER = 1.210 INCH, FINAL DIAMETER = 1.247 INCH, MAXIMUM ALLOWABLE= 1.220 INCH. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1C. REFER TO WRI 57502078 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. BRACKET ASSEMBLY PN ARC0502-14.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 966 hrs · 18,441 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE HAS SURFACE CORROSION. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED & INSTALLED IAW EA1-5750-T0318565 P1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP INBD FWD HINGE LOWER OTBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 966 hrs · 18,441 cycles

RIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT INBD HOLE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0318565 P1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

LEFT WING, OTBD FLAP INBD FWD HINGE LOWER INBD HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318531 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 966 hrs · 18,441 cycles

RIGHT WING, OTBD FLAP INBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7, REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING 0.0713 INCH, FINAL= 0.719 INCH & MAXIMUM ALLOWABLE= 0.709 INCH. SHOULDER BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1B. REFER TO WRI 57502078 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 966 hrs · 18,441 cycles

LEFT WING, OTBD FLAP INBD FWD HINGE BARREL NUT HOLE HAS CORROSION. WORKED IAW CMM 57-44-08 AND REPAIRED IAW EA 1-5750-T0318531 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. SHOULDER BUSHING, FABRICATED IAW EA 1-5750-T0318563 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT OTBD HOLE SURFACE CORRODED. FOUND WITHIN LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW CMM 57-44-09. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT UPPER HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318563 PART 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

CABIN MAIN DECK CARGO COMPARTMENT RT BS 1256, LONGERON 26R FWD R3 DOOR LOWER JAMB FOUND WEB CRACKED. REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED MAJOR IAW SMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK BS 1159, X = 8.5 FOUND SURFACE CORRODED. REPAIRED IAW SRM 53-00-52-2R, REPAIR 1 FIG 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT LOWER HOLE BORE CORRODED. WORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0318563 PART 1 STEP 1B.

Part: HINGE — CORRODED (TE FLAP) · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT HOLE SURFACE CORROSION. WORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 966 hrs · 18,441 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT INBD HOLE SURFACE CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0318563 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1256) · airframe 966 hrs · 18,441 cycles

MAIN DECK CARGO BS 1256, LONGERON 26L, FWD L3 DOOR LOWER JAMB WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1310) · airframe 966 hrs · 18,441 cycles

MAIN DECK CARGO BS 1310, LONGERON 26R AFT R3 DOOR LOWER JAMB WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (FUSELAGE) · airframe 966 hrs · 18,441 cycles

CABIN MAIN DECK CARGO COMPARTMENT BS 1310, LONGERON 26L AFT L3 DOOR LOWER JAMB FOUND WEB CRACKED. REPAIRED IAW EA 1-5310-T0318727 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 964 hrs · 18,367 cycles

LEVEL 3 CABIN SMOKE ALERT UPON LANDING, NO SMOKE PRESENT. PERFORMED OPERATIONAL TEST OF THE CARGO SMOKE DETECTOR IAW AMM 26-14-01-5, TEST PASSED. NO FAULT FOUND IN MSC CURRENT FAULT & FAULT REVIEW, NO HISTORY WITHIN 99 DAYS. ITEM CLOSED, ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (GENERATOR) · airframe 961 hrs · 18,288 cycles

GENERATOR LOAD HIGH LEVEL 2 ALERT. RAN CHECKLIST, WHILE WORKING CHECKLIST, WENT AWAY. BATTERY DISCHARGE, WENT AWAY. ACFT TIE FAULT. ADG ELEC SWON. DUMPED FUEL TO LAND WT. ALL THIS OCCURRED AFTER APU STARTED & CREW SHUTDOWN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 958 hrs · 18,223 cycles

EMERGENCY LIGHTS FAILED TEST. R & R BATTERY PACK IAW MM 33-51-01-4-0. OPERATIONS TESTED GOOD.

Part: HYDRAULIC LINE — FAILED (NR 2 ENGINE) · airframe 94,532 hrs · 17,819 cycles

UPON TOUCHDOWN WITH FLAPS 35 & MEDIUM BRAKES SELECTED, EXPERIENCED COMPLETE LOSS OF NR 2 HYD SYS FLUID RESERVOIR WAS ZERO & PUMPS OFF. ALL THESE HAPPENED BETWEEN TOUCHDOWN & TAXI SPEED. NR 2 LT FAN COWL OPENED, FOUND PRESS LINE GOING INTO THE HYD CONTROL UNIT COMPLETELY BROKEN OFF. R&R HYD LINE & LEAK CHKED NML AS PER EA 1-2902-T0301846.

Part: SKIN — CRACKED (LT WING) · airframe 93,925 hrs · 17,623 cycles

DURING COMPLIANCE OF FCD 1-5710-F0308148, FOUND SKIN CRACKED NEAR ZONE 519, LT WING INBD OF NR 1 ENGINE, JUST AFT OF INBD SLATS. PERFORMED HFEC OF THE SUSPECTED CRACK IN THE LT WING. CRACK APPROXIMATELY INCHES INCHES. INSTALLED FILLER AND DOUBLER IAW EA 1-5710-T0308293 P1.

Part: SKIN — CRACKED (RT WING) · airframe 93,925 hrs · 17,623 cycles

FOUND POSSIBLE SMALL CRACK RT WING ROOT LE. COMPLIED WITH HFEC IAW SPM 06-10-01001. CRACK NOTED .750 INCH LONG. REMOVED CRACK AT OTBD CORNER OF FIRE BOTTLE ACCESS DOOR LOWER SKIN. MADE CUT OUT IAW SRM 57-10-00 FIG 68. PERFORMED HFEC INSPECTION IAW NTM CHAP 20-00-00 PART 6. NO DEFECTS NOTED. REPAIR DOUBLER & FILLER INSTALLED ON RT WING NR 16 SLAT TRACK IAW SRM 57-40-02.

Part: LONGERON SPLICE — CRACKED (BS 1651 L11R) · airframe 92,073 hrs · 16,956 cycles

MAIN DECK LONGERON 11R SPLICE AT BS 1651 FOUND CRACKED. R & R SRM 51-31-01, REV 53. SPLICE FABRICATED IAW DWG AFA7181, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: TRUNNION — CRACKED (NLG) · airframe 92,073 hrs · 16,956 cycles

NOSE LANDING GEAR WHEEL WELL RT TRUNNION FITTING LOWER AREA FOUND CRACKED. AREA TRIMMED OUT AND REPAIRED IAW SRM 53-10-14, FIG 202. REPAIR 2, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. INITIAL INSP AT 1500 CYCLES AND REPETITIVE INSP REQUIRED AT 1500 CYCLES USING HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT METHOD IAW SRM 53-10-14, TABLE 201, FIG 202, REPAIR 2, REVISION 53.

Part: SKIN — CRACKED (ZONE 500) · airframe 92,073 hrs · 16,956 cycles

LEFT HAND WING FIXED L/E XOS 715, SLAT TRACK 11 CUTOUT CRACKED. REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: STOP FITTING — CRACKED (ZONE 800) · airframe 92,073 hrs · 16,956 cycles

MAIN DECK L3 PLUG DOOR, ONE DOOR STOP FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 92,073 hrs · 16,956 cycles

RT WING FIXED L/E COMPARTMENT AT XOS 794 BEADED DOUBLER FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 57-40-02, FIG 203, REPAIR 15, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: TRUNNION — CRACKED (NLG) · airframe 92,073 hrs · 16,956 cycles

NOSE LANDING GEAR WHEEL WELL LEFT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED IAW EA 1-5340-T0301502A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SUPPORT FITTING — CRACKED (DOOR FRAME) · airframe 92,073 hrs · 16,956 cycles

DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION, FOUND ONE CRACK INDICATION ON NR 7 MAIN DECK CARGO DOOR LOWER FRAME FITTING AT HOLE "A". SUPPORT FITTING R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — CRACKED (ZONE 500) · airframe 92,073 hrs · 16,956 cycles

LEFT WING FIXED L/E XOS 660, SLAT TRACK NR 10 CUTOUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: LONGERON SPLICE — CRACKED (BS 1631 L12L) · airframe 92,073 hrs · 16,956 cycles

MAIN DECK LONGERON 12L SPLICE AT BS 1631 FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. FABRICATED IAW DWG AFA7181 REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: UNKNOWN — UNKNOWN (YOKE) · airframe 87,940 hrs · 15,757 cycles

F/O YOKE IS APPROXIMATELY 5 LT (DOWN) WHEN IT SHOULD BE FULLY NEUTRAL (LEVEL). NO DIFFERENCE WHEN EITHER AUTOPILOT SELECTED. ACFT IS TRIMMED. PERFORMED OPS TEST OF AILERONS IAW AMM 27-10-00-5-0. FOUND ALL NORMAL. PERFORMED FCC 1 AND FCC 2 CONTROL WHEEL SYS TEST IAW AMM 22-00-06-5. TEST PASSED. PERFORMED FCC-1 AND FCC-2 AILERON SYS TEST IAW AMM 27-13-00-5. TEST PASSED. ACFT CAT STATUS DOWNGRADED. ACFT OK TO CONTINUE SERVICE.

Part: SKIN — DAMAGED (ZONE 100) · airframe 87,288 hrs · 15,608 cycles

FORWARD CARGO DOOR CUTOUT FOUND WITH SCRATCHES AT L39-41R. REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIG.202 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SKIN — DAMAGED (ZONE 100) · airframe 87,288 hrs · 15,608 cycles

FORWARD DOOR CUTOUT AFT FUSLAGE SKIN FOUND WITH SCRATCHES AT L-38-39R. REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIG.202 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV112.

Part: SKIN — DAMAGED (ZONE 100) · airframe 87,288 hrs · 15,608 cycles

AFT CARGO DOOR CUTOUT AFT JAMB FOUND WITH SCRATCHES AT L43-44L. CUTOUT AFT JAMB AREA, REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIG.202 REV47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV112.

Part: BEAM — CRACKED (L3 DOOR) · airframe 87,288 hrs · 15,608 cycles

CABIN L3 DOOR NR 1 BEAM AFT STOP SUPPORT FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 REV 47. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV112.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 87,288 hrs · 15,608 cycles

RT WING INBD FLAP LOWER SKIN AT STA XIFH 245 MISREPAIRED. REPAIR REMOVED AND NEW REPAIR CARRIED OUT AT RTWING I/B FLAP LWR SKIN AS PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. EA 1-5750-143656. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2- 100 REV 112.

Part: SKIN — CORRODED (CENTER WING) · corrosion level 2 · airframe 87,288 hrs · 15,608 cycles

CABIN RT STA 1214 XCW=-100 - XCW=-103 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS 0.162", REMAINING THICKNESS 0.136", MATERIAL REMOVED 0.026" AND FOUND ACCEPTABLE AS PER EA 1-5710-143645. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.

Part: SKIN — CORRODED (CENTER WING) · corrosion level 2 · airframe 87,288 hrs · 15,608 cycles

CABIN RT STA 1229 XCW=-90 - XCW=-100 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS 0.166", REMAINING THICKNESS 0.096", MATERIAL REMOVED 0.070" AND FOUND ACCEPTABLE AS PER EA 1-5710-143645. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.

Part: WEB — CRACKED (BS 1841) · airframe 87,288 hrs · 15,608 cycles

CTR CARGO COMPARTMENT STA 1841 , WEB FOUND CRACKED AT LBL 40. REPAIR CARRIED OUT AS PER SRM 53-00-00 FIG.211 REV.47 AT CTR CARGO COMPT. STA.1841 WEB END CAP AT LBL 40. EO1-5100-7-5001 A5-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112

Part: WEB — CRACKED (BS 1841) · airframe 87,288 hrs · 15,608 cycles

CTR CARGO BAY STA 1841, WEB FOUND CRACKED. AT LBL 13. REMOVED AND NEW WEB FABRICATED AS PER DWG AGA7170 REV T AND INSTALLED AS PER SRM 51-31-01 REV.47 EO1-5100-7-5001 A5-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 87,288 hrs · 15,608 cycles

RT WING INBD FLAP LOWER SKIN XIFH218 MISREPAIRED. REPAIR CARRIED OUT PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.

Part: WEB — CRACKED (BS 1841) · airframe 87,288 hrs · 15,608 cycles

CTR CARGO COMPARTMENT STA 1841, WEB FOUND CRACKED AT RBL 40. REMOVED AND NEW WEB FABRICATED AS PER DOUGLAS DWG AGA7170 REV T AND INSTALLED AT CTR CARGO COMPT. AS PER SRM 51-31-01 REV.47 EO1-5100-7-5001 A5-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112

Part: SKIN — UNKNOWN (BS 990) · airframe 87,288 hrs · 15,608 cycles

REPAIR AT FUSELAGE SKIN STA 990 BETWEEN LONGERON 40 TO 42RT. REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIGURE 202 REV 47. EO 1-5100-7-5001 A5 PT1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.

Part: WEB — CRACKED (BS 1841) · airframe 87,288 hrs · 15,608 cycles

CTR CARGO BAY STA 1841, WEB FOUND CRACKED LBL 8. REMOVED AND NEW WEB FABRICATED AS PER DWG AGA7170 REV T AND INSTALLED AS PER SRM 51-31-01 REV.47 EO1-5100-7-5001 A5-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112

Part: SKIN — UNKNOWN (BS 1960) · airframe 87,288 hrs · 15,608 cycles

REPAIR AT FUSELAGE SKIN STA 1960 BETWEEN LONGERON 40 TO 42L. REMOVED AND REPAIRED AS PER SRM 53-00-15 REPAIR 8 FIGURE 202 REV 47. EO 1-5100-7-5001 A5 PT1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.

Part: SKIN — CRACKED (LT WING) · airframe 87,288 hrs · 15,608 cycles

LT WING L/E LOWER SKIN AT XOS 575, CRACKED. CARRIED OUT REPAIR AS PER EA 1-5740-143647. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV112.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 87,288 hrs · 15,608 cycles

LT WING INBD FLAP LOWER SURFACE XIFH198 MISREPAIRED. REPAIR CARRIED OUT PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 87,288 hrs · 15,608 cycles

RT WING INBD FLAP LOWER SKIN AT XIFH 188 MISREPAIRED. REPAIR CARRIED OUT PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.

Part: WEB — CRACKED (BS 1841) · airframe 87,288 hrs · 15,608 cycles

BS 1841 WEB FOUND CRACKED AT RBL 47. NEW WEB FABRICATED AS PER DWG AGA7170 REV T AND INSTALLED. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 87,288 hrs · 15,608 cycles

LT WING INBD FLAP LOWER SURFACE XIFH245 MISREPAIRED. REPAIR CARRIED OUT PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.

Part: SKIN — MISREPAIRED (LT WING) · airframe 87,288 hrs · 15,608 cycles

REPAIR FOUND ON LT WING INBD L/E UPPER. FOUND NOT IAW SRM 57-40-02 REPAIR 8 FIG.201 REV 47. NEW REPAIR CARRIED OUT IAW SRM 57-40-02 REPAIR 8 FIG.201 REV.47. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.

Part: FRAME — DENTED (BS 1721 L11R) · airframe 87,288 hrs · 15,608 cycles

CABIN RT 1721 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: FRAME — DENTED (BS 1741 L11R) · airframe 87,288 hrs · 15,608 cycles

CABIN RT STA 1741 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: FRAME — MISREPAIRED (BS 535) · airframe 87,288 hrs · 15,608 cycles

REPAIR AT CABIN LT STA 535 9G NET UPPER SUPPORT YOKE, FOUND NOT CARRIED OUT IAW DWG SG10530002. REMOVED AND NEW REPAIR CARRIED OUT PER DWG SG10530002 AND EA 1-5310-143652. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.

Part: FRAME — DENTED (BS 1701 L11R) · airframe 87,288 hrs · 15,608 cycles

CABIN RT STA 1701 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: FRAME — MISREPAIRED (BS 535) · airframe 87,288 hrs · 15,608 cycles

FRAME REPAIR AT CABIN LT STA 535 9G NET LOWER SUPPORT YOKE FOUND NOT CARRIED OUT IAW DWG SG10530002. REPAIR CARRIED OUT PER DWG SG10530002 AND EA1-5310-143652. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.

Part: FITTING — DAMAGED (ZONE 300) · airframe 82,182 hrs · 14,385 cycles

NR4 BANJO FITTING OF VERTICAL STAB FOUND EXISTING REPAIR ON LT SIDE UPPER FASTENER HOLE. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: FITTING — DAMAGED (ZONE 300) · airframe 82,182 hrs · 14,385 cycles

BANJO FITTING STA Y-2169 LT SIDE FWD FLANGE 02EA EXISTING FASTENERS HOLE FOUND OVERSIZED DURING REPAIR JUST ABOVE CARRY THROUGH CAP. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: FITTING — WORN (ZONE 300) · airframe 82,182 hrs · 14,385 cycles

HFEC OPEN HOLE INSP UNABLE TO BE CARRIED OUT ON FASTENER HOLE NR11 (COUNTING FROM LT SIDE) AT NR4 BANJO FITTING AFT STA 2164 DUE TO HOLE DAMAGED. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: FITTING — GOUGED (ZONE 300) · airframe 82,182 hrs · 14,385 cycles

AFTER REMOVAL OF STRAP AT RT SIDE OF BANJO NR4 FOUND GOUGE MARK ON BANJO FITTING SURFACE. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: ANGLE — CRACKED (ZONE 300) · airframe 82,182 hrs · 14,385 cycles

UPON REMOVAL OF CRACKED ANGLE AT BANJO FITTING NR 4 AFT FOUND 8 EA HOLES WITH REPAIR BUSHING. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: STRAP — GOUGED (ZONE 300) · airframe 82,182 hrs · 14,385 cycles

EMPENNAGE- UPON STRAP REMOVAL ON THE RT SIDE FOUND WITH GOUGE MARKS. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 82,182 hrs · 14,385 cycles

WHILE CARRYING OUT BANJO FITTING REPAIR PER MANUFACTURER INSTRUCTION, FOUND RT AFT BANJO FITTING CRACKED. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: FRAME — DENTED (ZONE 200) · airframe 82,182 hrs · 14,385 cycles

CABIN - LT STA 1761, L-11 TO L-12 FOUND DENT. REPAIRED IAW SRM 53-00-07 FIG 201. REPAIR 2 REV 41 INITIAL INSP TO BE CARRIED OUT AT 14,500 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSPECTIONS AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07, TABLE 201, REPAIR 2 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 108.

Part: FRAME — CHAFED (ZONE 200) · airframe 82,182 hrs · 14,385 cycles

CABIN - LT STA 1781, L-11 TO L-12 FOUND CHAFED. REPAIRED IAW SRM 53-00-07 FIG.201. REPAIR 2 REV 41 INITIAL INSP TO BE CARRIED OUT AT 14,500 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSP AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07, TABLE 201. REPAIR 2, REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 108.

Part: FRAME — DENTED (ZONE 200) · airframe 82,182 hrs · 14,385 cycles

CABIN - RT STA 1661, L-11 TO L-12 FOUND DENT. REPAIRED IAW SRM 53-00-07 FIG 201, REV 41. INITIAL INSP TO BE CARRIED OUT AT 14,500 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSPECTIONS AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07 TABLE 201, REPAIR 2 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 108.

Part: FRAME — DENTED (ZONE 200) · airframe 82,182 hrs · 14,385 cycles

CABIN - RT STA 1761, L-11 TO L-12 FOUND DENT. REPAIRED IAW SRM 53-00-07 FIG 201. REPAIR 2, REV 41. INITIAL INSP TO BE CARRIED OUT AT 14,500 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSPECTIONS AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07, TABLE 201, REPAIR 2 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 108.

Part: DOUBLER — CRACKED (LT MLG WW) · airframe 82,182 hrs · 14,385 cycles

CTR LANDING GEAR WW, WWL LT FWD SIDE DOUBLER CRACKED. REMOVED IAW SRM 51-31-01 REV. 41. DOUBLER FABRICATED IAW DWG AEA0526 REV. NC. NEW DOUBLER INSTALLED IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.

Part: FRAME — DENTED (ZONE 200) · airframe 82,182 hrs · 14,385 cycles

CABIN - RT STA 1641, L-11 TO L-12 FRAME FOUND DENT. REPAIRED IAW SRM 53-00-07 FIG 201, REV 41. INITIAL INSP TO BE CARRIED OUT AT 14,500 FLT CYCLES AND SUBSEQUENT REPETITIVE INSPECTIONS AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07, TABLE 201. REPAIR 2, REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 108.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 82,182 hrs · 14,385 cycles

CRACK INDICATION FOUND APPROX 0.50" IN LENGTH DURING HFEC ON LT SIDE OF THE LWR VERTICAL STABILIZER FWD FLANGE OF UPPER REAR SPAR CAP. REPAIR CARRIED OUT IAW EA 1-5530-135612, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 108.

Part: CONTROLLER — FAILED (ANTI SKID SYSTEM) · airframe 82,074 hrs · 14,358 cycles

RECEIVED LEVEL-2 ANTI-SKID FAILURE ALERT WITH MASTER CAUTION ON TAKEOFF ROLL APPROX 70 KNOTS. ALL TEST PASSED IAW MM 32-45-01. INSPECT ALL WHEEL AND BRAKES NO DEFECT FOUND. CONSULT WITH MOCC FOR PRECAUTION REMOVED AND REPLACED ASCU AND RTS TEST PASSED IAW MM 32-45-01-05. PERFORMED ABSCU RTS TEST ALL TEST PASSED IAW MM 32-48-00-05. SYS OK FOR SERVICE.

Part: FRAME — DAMAGED (ZONE 200) · airframe 77,557 hrs · 13,324 cycles

MAIN DECK INTERIOR FUSELAGE AT LEFT STA 535 FRAME, UPPER SUPPORT YOKE FOUND DAMAGED. MAIN DECK INTERIOR FUSELAGE AT LEFT HAND STA 535, UPPER SUPPORT YOKE, DAMAGED FRAME REPAIRED AS PER FEDEX DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100.

Part: FRAME — DAMAGED (ZONE 200) · airframe 77,557 hrs · 13,324 cycles

MAIN DECK INTERIOR FUSELAGE AT LEFT STA 535 FRAME, LOWER SUPPORT YOKE, FOUND DAMAGED. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100.

Part: SKIN — CORRODED (CENTER WING) · airframe 77,557 hrs · 13,324 cycles

MAIN DECK CENTER WING UPPER SKIN SURFACE AT STA 1341 X = 101 FOUND CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-113145, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 77,557 hrs · 13,324 cycles

UPPER FUSELAGE INTERIOR FRAME AT RIGHT STA 1681 LONGERON 11 FOUND DAMAGED. UPPER FUSELAGE INTERIOR, DENT FRAME AT RT BS 1681 LONGERON 11 REPAIRED AS PER SRM 53-30-00. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR) · airframe 77,557 hrs · 13,324 cycles

MAIN DECK CARGO DOOR NR 4 LOWER JAMB SUPPORT FITTING 'B' HOLE FOUND CRACK AT 1 O'CLOCK POSITION. MAIN DECK CARGO DOOR NR 4 LOWER JAMB CRACKED SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 77,557 hrs · 13,324 cycles

14 FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. COMPLIED WITH E.A. 1-5710-113138, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 77,557 hrs · 13,324 cycles

16 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. COMPLIED WITH E.A. 1-5710-113137, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 77,557 hrs · 13,324 cycles

LEFT WING INBOARD FLAP LOWER SURFACE CENTER LOWER SEGMENT FOUND DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 17 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: INDICATION SYS — MALFUNCTIONED (FUEL QTY) · airframe 77,489 hrs · 13,306 cycles

90 MINUTES INTO FLIGHT RECEIVED LATER FUEL IMBALANCE WITH FUEL CONTROLLER IN AUTO. RAN QRH AUTO CONTROLLER RESOLVED IMBALANCE OF TNK 14000 LBS HEAVY. APPROXIMATELY 10 MINUTES LATER FP/R FUEL LOG INDICATED A CHANGE OF 2000 LBS UNACCOUNTED FOR AND INCREASING OVER TIME. THEN RECEIVED LVL 2 ALERT: FUEL OFF SCHEDULE. RAN QRH AND PUT FUEL SYS CONTROLLER IN MANUAL. OVER NEXT 20 MINUTES EFOB AT DESTINATION CONTINUED TO DECREASE AND T/O FUEL MINUS USED CONTINUED TO INCREASE. REMOVED AND REPLACED NR 1 INBOARD AND OUTBOARD MJP IAW MM-28-41-40-4, LEAK CHECK GOOD. OPS TEST CHECKED GOOD IAW MM 28-41-00-5.

Part: SKIN — CRACKED (RT WING) · airframe 73,318 hrs · 12,329 cycles

RIGHT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND XORS = 713.6 FOUND CRACK ON FASTENER HOLE LOCATED AT 3:30 POSITION (LOOKING FORWARD VIEW UP). RIGHT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND XORS 713.6 CRACK ON FASTENER HOLE AT 3:30 POSITION REPAIRED AS PER FEDEX EA NR 1-5710-105559, TITLE: WINGS RIGHT LOWER SKIN PLANK CUT OUT AT 636AB, ONE ACCESS DOOR ATTACHMENT BORE WITH CRACK INDICATIONS CENTERED AT XORS = 696.73 PSE 57.23.01 ALI. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 73,318 hrs · 12,329 cycles

LEFT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND XORS = 713.6 FOUND CRACK ON FASTENER HOLE LOCATED AT 1:30 POSITION (LOOKING FORWARD VIEW UP). LEFT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND XORS 713.6 FOUND CRACK ON FASTENER HOLE LOCATED AT 1:30 POSITION REPAIR. CARRIED OUT AS PER FEDEX EA NR 1-5710-105558, TITLE: WINGS, LEFT LOWER SKIN PLANK CUT OUT AT 536AD, ONE ACCESS DOOR ATTACHMENT BORE WITH CRACK INDICATIONS CENTERED AT XORS = 696.73 PSE 57.23.01 ALI. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DELAMINATED (FLAP VANE) · airframe 73,318 hrs · 12,329 cycles

LT WING INBD FLAP VANE INBD LOWER SURFACE FOUND DELAMINATION. REPAIRED AS PER FEDEX E.A. 1-5750-105562.

Part: HINGE — CORRODED (T/E FLAP) · airframe 73,318 hrs · 12,329 cycles

LEFT WING, INBOARD FLAP OUTBOARD HINGE PIVOT POINT INBOARD LUG BORE HOLE FOUND CORRODED. REPAIRED PER FEDEX E.A. 1-5750-105566.

Part: HINGE — CORRODED (RT WING) · airframe 73,318 hrs · 12,329 cycles

RIGHT WING, (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACHMENT INBOARD LUG HOLE FOUND CORRODED. REPAIRED PER FEDEX E.A. 1-5750-105569.

Part: HINGE — CORRODED (T/E FLAP) · airframe 73,318 hrs · 12,329 cycles

RIGHT WING, INBOARD FLAP OUTBOARD HINGE PIVOT POINT OUTBOARD LUG BORE HOLE FOUND CORRODED. REPAIR AS PER FEDEX E.A. 1-5750-105567.

Part: HINGE — CORRODED (T/E FLAP) · airframe 73,318 hrs · 12,329 cycles

LEFT WING, INBOARD FLAP OUTBOARD HINGE PIVOT POINT OUTBOARD LUG BORE HOLE FOUND CORRODED. CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5750-105566.

Part: HINGE — CORRODED (T/E FLAP) · airframe 73,318 hrs · 12,329 cycles

RIGHT WING, INBOARD FLAP OUTBOARD HINGE PIVOT POINT INBOARD LUG BORE HOLE FOUND CORRODED. REPAIRED PER FEDEX E.A. 1-5750-105567.

Part: TRUNNION — CORRODED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CENTER LANDING GEAR LT TRUNNION MATING SURFACE FOUND CORRODED. CENTER LANDING GEAR LEFT TRUNNION MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. FORWARD SIDE ORIGINAL THICKNESS = 2.485". REMOVED MATERIAL = 0.050" AND REMAINING THICKNESS = 2.435". AFT SIDE ORIGINAL THICKNESS = 2.497". REMOVED MATERIAL = 0.050" AND REMAINING THICKNESS = 2.447". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING CTR BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING CTR BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 200) · airframe 73,318 hrs · 12,329 cycles

CARGO CTR FUEL TANK UPPER PANEL (STA 1239, RH X=100) FOUND LOCK FASENER PERIPHERY CORRODED. MAIN DECK CARGO (STA 1239, RH X = 100) CENTER FUEL TANK UPPER PANEL CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.1848", MATERIAL REMOVED = 0.0048", AND REMAINING MATERIAL = 0.180" AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 VOLUME I FIGURE 12. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING FWD BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — DIRTY (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING FWD BORE HOLE FOUND STAIN. STAIN AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING FWD BORE HOLE CLEANED UP AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING AFT BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING AFT BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CENTER LANDING GEAR RT TRUNNION MATING SURFACE FOUND CORRODED. CENTER LANDING GEAR RIGHT TRUNNION MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. FORWARD SIDE ORIGINAL THICKNESS = 2.477". REMOVED MATERIAL = 0.045" AND REMAINING THICKNESS = 2.432" FT SIDE ORIGINAL THICKNESS = 2.491". REMOVED MATERIAL = 0.045" AND REMAINING THICKNESS = 2.446". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 73,318 hrs · 12,329 cycles

M/D CARGO, INTERIOR FUSELAGE FOUND RT FRAME (STA 1781, L12) DENTED. MAIN DECK CARGO RIGHT FRAME (STA 1781, LONGERON 12) CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CTR CARGO COMPARTMENT, STA 5-11, L52 FOUND CORROSION. CENTER CARGO COMPARTMENT, STA 5-11, LONGERON 52 REPAIRED AS PER FEDEX EA#1-5310-105561, TITLE:"FUSELAGE-LONGERON L-52 LEFT AT STATION 5-21, SRM SPLICE REPAIR CLARIFICATION" AND SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 200) · airframe 73,318 hrs · 12,329 cycles

M/D, STA 6-100 LONGERON 1R ON THE FORWARD SIDE OF THE INNER TRANSVERSE STRAP FOUND CRACK. CRACKED SPLICE AT MAIN DECK CARGO COMPARTMENT AT STA 6-100 LONGERON 1R. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE MACHINED AS PER DRAWING A6A7112 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (ZONE 100) · airframe 73,318 hrs · 12,329 cycles

CTR CARGO COMPARTMENT, STA 5-113 L49L SPLICE FITTING FOUND CRACKED. CRACKED SPLICE FITTING AT CENTER CARGO COMPARTMENT STA 5-113 LONGERON 49L. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE FITTING FABRICATED AS PER DRAWING A5A7114. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 73,318 hrs · 12,329 cycles

CARGO LT FRAME (STA 1661, L12) FOUND DENT. MAIN DECK CARGO LEFT HAND FRAME (STA 1661, LONGERON 12) CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 73,318 hrs · 12,329 cycles

CARGO LT FRAME (STA 1681, L11-13) FOUND DENT. MAIN DECK CARGO LEFT HAND FRAME (STA 1681, LONGERON 11 TO 13) CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 73,318 hrs · 12,329 cycles

CARGO LT FRAME (STA 1641, L12) FOUND DENT. MAIN DECK CARGO LEFT HAND FRAME (STA 1641, LONGERON 12) CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,318 hrs · 12,329 cycles

LT WING, AT XOS 654 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,318 hrs · 12,329 cycles

LT WING, AT XOS 645 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 73,318 hrs · 12,329 cycles

CABIN: SLIDE/RAFT AT L1 DOOR FOUND FIRING LANYAND DISCONNECTED WITH QUICK-DISCONNECT WHEN DOOR INTERIOR LWR COVER REMOVED FOR REPAIR. RECONNECTED L1 DOOR SLIDE/RAFT FIRING LANYAND AS PER AMM 25-61-06-4.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,318 hrs · 12,329 cycles

LT WING, AT XOS 518 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,318 hrs · 12,329 cycles

LT WING, AT XOS 631 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,318 hrs · 12,329 cycles

LT WING, AT XOS 639 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 73,318 hrs · 12,329 cycles

CABIN: SLIDE/RAFT AT R1 DOOR FOUND FIRING LANYAND DISCONNECTED WITH QUICK-DISCONNECT WHEN DOOR INTERIOR LWR COVER REMOVED FOR REPAIR. RECONNECTED R1 DOOR SLIDE/RAFT FIRING LANYAND AS PER AMM 25-61-06-4.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,318 hrs · 12,329 cycles

RT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XOS 669. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 73,318 hrs · 12,329 cycles

HFEC INSPECTION FOUND CRACK ON RT WING TANK AT THE END OF STRINGER 38. CRACK (STARTING FROM STOP DRILL HOLE TO INBOARD) ON EXISTING REPAIR DURING HFEC INSPECTION ON RT WING TANK AT THE END OF STRINGER 38 XORS 877 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,318 hrs · 12,329 cycles

RT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XORS 636-643. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 73,318 hrs · 12,329 cycles

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

Part: DOUBLER — CRACKED (RT WING) · airframe 73,318 hrs · 12,329 cycles

RT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XOS 665. RT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 665 REPAIRED AS PER SRM TR 57-5 57-10-00 FIGURE 25B VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 73,318 hrs · 12,329 cycles

HFEC INSPECTION FOUND CRACK ON LT WING TANK AT THE END OF STRINGER 9. CRACK ON LT WING TANK AT THE END OF STRINGER 9 AT XORS 819 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 600) · airframe 73,318 hrs · 12,329 cycles

RT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACK. REPAIRED AS PER FEDEX E.A. 1-5730-105556.

Part: DUCT — CRACKED (ZONE 500) · airframe 73,318 hrs · 12,329 cycles

LT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACK. CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5730-105557.

Part: FRAME — CRACKED (FUSLEAGE) · airframe 69,172 hrs · 11,377 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F, FOUND CRACK 2.5 INCHES LONG ON FRAME LUG AT STA 1256 B/T L11 AND L12, RT SIDE. CUT OUT DAMAGED AREA AND REPAIR FRAME IAW SRM 53-30-00 FIG 2. CUT OUT DAMAGED AREA AND REPAIR FRAME IAW SRM 53-30-00 FIG 2.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 69,172 hrs · 11,377 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 5-53, STR 50-51 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-20-00 FIG 6, SHEET 7, VOL 1.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 69,172 hrs · 11,377 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: EXISTING REPAIR AT FWD CARGO, FROM STA 775 TO STA 791, Z19, X= -117 LOWER FLOOR. NO ACTION REQUIRED: REPAIR IS IAW SRM 53-00-01, FIG 8, SHEET 5.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 69,172 hrs · 11,377 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 990, STR 40-42 RT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-50-00 FIG 7A.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 69,172 hrs · 11,377 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 1960, STR 40-42 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-50-00 FIG 16.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,172 hrs · 11,377 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: EXISTING REPAIR ON BULKHEAD, AT STA 595, X=56 LT SIDE. NO ACTION REQUIRED. REPAIR IS IAW SRM 53-20-00 FIG 6 SHEET 5.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 69,172 hrs · 11,377 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 635, STR 43-46 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 5320-00 FIG 2 SHEET 3.