N588FE

Part: MODULE — FAILED (UNKNOWN) · airframe 95,265 hrs · 21,583 cycles

ON DOWNWIND FOR APPROACH AT 4000FT, EXTENDED THE SLATS AND RECEIVED A LEVEL 2 SLAT DISAG ALERT. WE DISCONTINUED THE APPROACH AND RAN THE QRH. DECLARED AN EMERGENCY WITH ATC AND PERFORMED A NO SLAT/FLAPS 28 APPROACH. LANDING ON KIND RUNWAY 05L UNEVENTFUL. NO HOT BRAKES NOTED. TERMINATED EMERGENCY AND TAXIED TO OUR SPOT. REMOVED AND REPLACED FLAP/SLAT CONTROL MODULE, REF MD-11 AMM 27-51-01-4-2. OPS TESTS GOOD.

Part: PSEU — FAILED (SLAT SYSTEM) · airframe 95,137 hrs · 21,552 cycles

SLAT DISAG ON EXTENSION DURING APPROACH PHASE. COMPLIED WITH QRH RESULTING IN FLAP 28/SLATS RETRACT LANDING. EMERGENCY DECLARED. REPLACED PSEU PER ABOVE REFERENCE, OPS CHECKS OK. PANELS OPENED FOR ACCESS FOR SLAT LUBE. LUBRICATED INBOARD AND OTBOARD SLAT DRIVES. OPERATED SLATS, SMOOTH AND UNIFORM THROUGH OPERATION

Part: UNKNOWN — UNKNOWN (N/A) · airframe 93,479 hrs · 21,052 cycles

AFT ACCESSORY COMPARTMENT HAS CORROSION ON ROW OF NUT PLATES ON RH SIDE AFT. MWT REPAIRED IAW SRM 53-70-01-2R

Part: DOUBLER — CRACKED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

REFERENCE TO SNRM #N01411 - UPON REMOVAL OF DOUBLER NCA 6244-3 FOUND INNER WEB DOUBLER NCA 6244-85 CRACKED (01 EACH OF APPROXIMATELY 0.5" LENGTH). FUSELAGE - MAIN FRAME AT STATION 595 CRACKED WEB DOUBLER NCA 6244-85 CARRIED OUT REPAIR IN ACCORDANCE WITH EA # 1-5310-T0370285P1AND P2 TITLE : FUSELAGE - MAIIN FRAME - CRACKS ON STA 594-875 AFT PRESSURE BULKHEAD DOUBLER & WEB LAYERS AT X= 42 , Z= -109. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.REFER SPECIAL / NONROUTINE MAINTENANCE FORM # N01411 FOR REPAIR DETAILS. ORIG SUB DATE: 10/11/2022

Part: DOUBLER — CRACKED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

REFERENCE TO SNRM # N01369 HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON ACCESSED FASTENER HOLES WITHIN THE AREA OF THE REMOVED NCA6244-3 DOUBLER FOOTPRINT AREA AT STATION 595 AND FOUND 03 EACH HOLES WITH CRACK INDICATION. FUSELAGE - MAIN FRAME AT STATION 595 CRACKED AT AFT PRESSURE BULKHEAD DOUBLER AND WEB CARRIED OUT REPAIR IN ACCORDANCE WITH EA#1-5310-T0370285 PART 1 AND PART 2. TITLE: FUSELAGE - MAIN FRAME - CRACKSON STA 594.875 AFT PRESSURE BULKHEAD DOUBLER & WEB LAYERS AT X=42, Z=-109. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 10/5/2022

Part: SKIN — DENTED (BS 595-615) · airframe 92,791 hrs · 20,853 cycles

LEFT SKIN BETWEEN STATION 595 TO 615 AND LONGERON 37 AND LONGERON 46 FOUND DENT. REPAIR CARRIED OUT AS PER EA NUMBER: 1-5330-T0370337 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022

Part: LONGERON — CORRODED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

REFERENCE SNRM NUMBER N01369, AFTER ADDITIONAL REMOVAL FOUND LONGERON NUMBER 49 LEFT CORRODED BETWEEN STATION 535 TO STATION 575. STATION 535 TO STATION 575 LONGERON NUMBER 49 LEFT CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202. LONGERON REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-31-01-0G AND SRM 53-35-01-0G . LONGERON FABRICATED IN ACCORDANCE WITH DOUGLAS DRAWING # ACA 3796 REVISION A .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: SUPPORT — CRACKED (ZONE 200) · airframe 92,791 hrs · 20,853 cycles

CABIN - WHILE ACCOMPLISHING FLOOR BEAM REPAIR PER SPECIAL/NONROUTINE MAINTENANCE FORM N01209 FOUND CHANNEL (SUPPORT) AT LEFT HAND STATION 1256 X=116 CRACKED. CRACKED CHANNEL ( SUPPORT) AT LEFT HAND STATION 1256 X=116 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-33-01-0G . CHANNEL (SUPPORT) FABRICATED BY MACHINING IN ACCORDANCE WITH DOUGLAS DRAWING AEA 7601 REV : NEW . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (BS 595 L42) · airframe 92,791 hrs · 20,853 cycles

REFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM N00314, TO INSPECT STATION 595 BULKHEAD FOUND FUSELAGE NO.1 AIRCON BAY AFT BULKHEAD STATION 595 APPROXIMATE LONGERON NO.42 SUSPECTED CRACK. FUSELAGE STATION 595 BULKHEAD NO.1 AIRCON BAY CRACKED AT DOUBLER AND WEB CARRIED OUT REPAIR IN ACCORDANCE WITH EA#1-5310-T0370285 PART 1 AND PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (BS 595-615) · airframe 92,791 hrs · 20,853 cycles

RIGHT SKIN BETWEEN BS 595 AND 615, BETWEEN LONGERON 44R-46R DENTED. CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5330-T0370284 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT HAND WING - OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 757 FORMER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 757 CRACKED FORMER REMOVED AND FABRICATED PER DOUGLAS DRAWIING ARB 2930 REV F. INSTALLED FABRICATED FORMER AS PER SRM 51-33-01-0G .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SPAR — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC INSPECTION CARRIED OUT ON UPPER SPAR ASSEMBLY, TAIL PYLON MANUFACTURING JOINT SPAR BETWEEN STATION YID 408.5 TO 413.2 AND FOUND CRACK INDICATION PROPAGATE IN AFT DIRECTION FROM THE EDGE OF LEFT HAND SIDE UPPER CAP VERTICAL FLANCE AT STATION YID 408.5 APPROXIMATE 3/4 INCHES LENGTH.

Part: SKIN — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT HAND WING - OUTBOARD FIXED LEADING EDGE #16 SLAT TRACK CUTOUT STATION XOS 1003 CRACKED. LEFT HAND WING - OUTBOARD FIXED LEADING EDGE NUMBER 16 SLAT TRACK CUTOUT STATION XOS 1003 CRACKED AREA REPAIR CARRIED OUT AS PER EA: 1-5730-T0370336 PART 1. TITLE: WING - PLATES AND SKIN - CRACKS, LH WING FIXED LEADING EDGE SKIN AND LOWER STRINGER DOUBLER AT SLAT TRACK #16 CUTOUT, STA XOS 993 TO STA XOS 1013. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

FORWARD CARGO COMPARTMENT , FOUND UNDERFLOOR LONGERON SPLICE BETWEEN STATION 755 TO STATION 775 , LONGERON - 44 LEFT SUSPECT CRACKED. REMOVED AND REPLACED PER SRM 51-31- 01-OG. LONGERON SPLICE FABRICATED BY MACHINING PER DOUGLAS DRAWING ACA7150 REVISION C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION CARRIED OUT ON LEFT HAND SIDE OVERWIING FLOOR BEAM AT STATION Y=1256 AND FOUND CRACK INDICATION ON THE OVERWING FLOOR BEAM WEB AND UPPER FLANGES BETWEEN STATION X = 107 AND STATION X = 116 APPROXIMATELY 1 INCHES LENGTH . LEFT HAND OVERWING CRACKED FLOOR BEAM AT STATION Y=1256 CARRIED OUT REPAIR FROM X = 88.00 TO X = 107.250 IN ACCORDANCE WITH EA 1-5310-T0370165 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUBMISSION DATE: 9/16/2022

Part: SKIN — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT HAND WING - OUTBOARD FIXED LEADING EDGE #11 SLAT TRACK CUTOUT STATION XOS 714 CRACKED. REPAIR CARRIED OUT PER SRM 57-40-02-2R REPAIR 7 FIGURE 201 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT HAND WING - OUTBOARD FIXED LEADING EDGE #15 SLAT TRACK CUTOUT STATION XOS 949 CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 92,791 hrs · 20,853 cycles

RIGHT HAND WING - OUTBOARD FIXED LEADING EDGE NUMBER 16 SLAT TRACK CUTOUT STATION XOS 1007 CRACKED. SKIN REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 92,791 hrs · 20,853 cycles

RIGHT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 758 BEADED DOUBLER CRACKED. DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 92,791 hrs · 20,853 cycles

RIGHT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 880 BEADED DOUBLER CRACKED. DOUBLER 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 92,791 hrs · 20,853 cycles

RIGHT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 613 BEADED DOUBLER CRACKED. DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R. REPAIR 15. FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 92,791 hrs · 20,853 cycles

RIGHT HAND WING - OUTBOARD FIXED LEADING EDGE NUMBER 15 SLAT TRACK CUTOUT STATION XOS 950 CRACKED. SKIN REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201 . REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

CENTRE CARGO COMPARTMENT, FOUND UNDERFLOOR LONGERON SPLICE SUSPECT CRACK BETWEEN STATION 1521 TO 1541, LONGERON 49 LEFT. LONGERON REMOVED AND REPLACED PER SRM 51-31-01-OG. LONGERON SPLICE FABRICATED BY MACHINING PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

CENTRE CARGO COMPARTMENT, FOUND UNDERFLOOR LONGERON SPLICE SUSPECT CRACK BETWWEEN ATATION 1521 TO 1541, LONGERON 49 LEFT. REMOVED AND REPLACED PER SRM 51-31-01-OG. LONGERON SPLICE FABRICATED BY MACHINING PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

CENTRE CARGO COMPARTMENT, FOUND UNDERFLOOR LONGERON SPLICE SUSPECT CRACK BETWEEN STATION 1521 TO 1541, LONGERON 52. REMOVED AND REPLACED PER SRM 51-31-01- OG. LONGERON SPLICE FABRICATED BY MACHINING PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CHAFED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

CABIN - LEFT HAND STATION 535 LONGERON 24 LEFT FRAME REPAIR OUTER ANGLE FOUND CHAFFING. BLENDED AND FOUND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-00-2R FIGURE 202 SHEET 1 . FRAME STATION 535 LONGERON 24 LEFT REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-20-07-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 651 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT HAND WING - INBOARD FIXED LEADIING EDGE UPPER SURFACE STATION XIS 247 CHAFFING MARK. AREA SMOOTHED OUT AND FOUND WITHIN LIMIT AS PER SRM 57-40-02-2R REPAIR 8 FIGURE 201 . REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 705 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CHAFED (ZONE 100) · airframe 92,791 hrs · 20,853 cycles

CABIN - LEFT HAND STATION 535 LONGERON 19 LEFT FRAME REPAIR OUTER ANGLE FOUND CHAFFING . BLENDED AND FOUND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-00-2R FIGURE 202 SHEET 1 .FRAME STATION 535 LONGERON 19 LEFT REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-20-07-2R REPAIR 1 FIGURE 202 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 906 RIB DOUBLER CRACKED. DOUBLER REMOVED AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB 3954 REVISION K . FABRICATED DOUBLER INSTALLED AS PER SRM 51-33-01-0G. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 666 STRINGER CRACKED. STRINGER REPAIR CARRIED OUT AT STRINGER AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202 . REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 92,791 hrs · 20,853 cycles

LEFT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 791 STRINGER CRACKED. STRINGER REPAIR CARRIED OUT AT STRINGER AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (ZONE 600) · airframe 92,791 hrs · 20,853 cycles

RIGHT HAND WING - INBOARD FIXED LEADING EDGE UPPER SURFACE STATION XIS 247 CHAFFING MARK . AREA SMOOTHED OUT AND FOUND WITHIIN LIMIT AS PER SRM 57-40-02-2R REPAIR 8 FIGURE 201. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: MOTOR — LEAKING (STAB TRIM) · airframe 92,561 hrs · 20,782 cycles

ON CLIMB OUT. LVL 1 HYD 3 ELEV OFF . HYD 3 QTY INDICATED 4.7 AND DROPPING. FOLLOWED BY A LVL 1 HYD 3 OFF AND THEN A LVL 2 HYD 3 FAIL . QTY AT ZERO. COMPLIED WITH QRH. EMERGENCY DECLARED DIVERT TO INDY AT GOC REQUEST. REMOVED AND REPLACED #1 HORIZONTAL STAB TRIM MOTOR IAW AMM 27-43-30-4. LEAK AND OPS CHECKED GOOD IAW AMM 27-43-30-4. ACFT OK FOR SERVICE.

Part: CYLINDER — FAILED (NLG STEERING) · airframe 92,318 hrs · 20,726 cycles

TAXI OUT WAS FINE. ON TAXI IN, FIRST RIGHT HAND TURN NOTICED ABOUT HALF WAY THROUGH THE RIGHT TURN, TILLER BECAME IN EFFECTIVE AND USED DIFFERENTIAL BRAKING TO STRAITENED UP. TRIED NEXT RIGHT TURN AT GATE VERY SLOW, AGAIN NO AUTHORITY. STOPPED THE AIRPLANE AND CALLED TO BE PULLED IN. REMOVED AND REPLACED RIGHT NOSE LANDING GEAR STEERING CYCLINDER OPS AND LEAK CHECK NORMAL REF MM CHAP 32-52-30-4.

Part: BATTERY PACK — UNKNOWN · airframe 83,067 hrs · 18,204 cycles

EMER LT BAT 1 LO LEVEL ALERT 1 WHEN TESTING EMER LIGHTS. PERFORMED EMER LT TEST IAW AMM 33-50-00-5 OPS CHECKS NORMAL. A/C OK FOR SERVCE

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 87,700 hrs · 19,502 cycles

EMPENNAGE LEFT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE 331FT FOUND WITH EXISTING BLIND RIVET REPAIR AT XFS=322.131 TO XFS 333.764. EMPENNAGE LEFT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE 331FT, WITH EXISTING BLIND RIVET REPAIR BETWEEN XFS=322.131 TO XFS=333.764. REMOVED AND REPAIR CARRIED OUT, AS PER SRM 55-10-02-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-10.

Part: BEAM — CRACKED (L3 DOOR) · airframe 87,700 hrs · 19,502 cycles

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

Part: INTERCOSTAL — CRACKED (ZONE 300) · airframe 87,700 hrs · 19,502 cycles

EMPENNAGE,UPON REMOVAL FOR BANJO FITTING REPAIR ACCESS,RIGHT HAND SIDE LOWER WEB PANEL FOUND WITH A CRACKLINE FROM CORNER EDGE AT STATION Y=2164. RIGHT HAND SIDE LOWER WEB INTERCOSTAL REAR CENTER SPAR TO REAR SPAR CRACK AT STATION Y=2164 REPAIR CARRIED OUT, AS PER EA 1-5530-T0356758 P1. TITLE: STABILIZERS-VERTICAL STABILIZER-REAR CENTER SPAR TO REAR SPAR LOWER PANEL-CRACK FOUND ON RT INTERCOSTAL. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: BULKHEAD WEB — DENTED (CENTER CARGO) · airframe 87,700 hrs · 19,502 cycles

AFT CARGO, STATION 1841 BULKHEAD WEB X=2" TO 18" FOUND DENTS. AFT CARGO STATION 1841 BULKHEAD WEB X=2 TO 18 REMOVED, AS PER SRM 51-33-01-0G AT STATION 1841 X=0 TO X=60. WEB FABRICATED, AS PER DOUGLAS DRAWING AGA 7170 REVISION R. WEB INSTALLED AT STATION 1841, X=0 TO X=60, AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: WEB — CRACKED (AFT CARGO) · airframe 87,700 hrs · 19,502 cycles

AFT CARGO-STATION 1841 X= -44" WEB CRACK ON EXISTING DOUBLER REPAIR. AFT CARGO STATION 1841 BULKHEAD WEB X= -44" REMOVED, AS PER SRM 51-33-01-0G AT STATION 1841, X=0 TO X= -62. WEB FABRICATED, AS PER DOUGLAS DRAWING AGA 7170 REVISION R. WEB INSTALLED, AS PER SRM 51-33-01-0G AT STATION 1841 X=0 TO X= -62. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (ZONE 300) · airframe 87,700 hrs · 19,502 cycles

EMPENNAGE, UPON REMOVAL FOR BANJO FITTING REPAIR ACCESS, LEFT HAND SIDE LOWER WEB PANEL FOUND WITH A CRACKLINE FROM CORNER EDGE AT STATION Y=2164. LEFT HAND SIDE LOWER WEB INTERCOSTAL REAR CENTER SPAR TO REAR SPAR CRACK AT STATION Y=2164 REPAIR CARRIED OUT, AS PER EA 1- 5530-T0356757 P1. TITLE: STABILIZERS-VERTICAL STABILIZER-REAR CENTER SPAR TO REAR SPAR LOWER PANEL-CRACK FOUND ON LT INTERCOSTAL. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FRAME — CRACKED (ZONE 300) · airframe 87,700 hrs · 19,502 cycles

CRACK FOUND APPROXIMATELY 0.4 INCH IN LENGTH AT PYLON CARRY THROUGH STRUCTURE WEBS AT 364QR ACCESS PANEL FRAME CUTOUT AT STATION 2164. CRACKED AT PYLON CARRY THROUGH STRUCTURE WEBS AT 364QR ACCESS PANEL FRAME CUTOUT AT STATION 2164. REMOVED AS PER SRM 51-33-01-0G AND REPLACED WITH FABRICATED FRAME, AS PER EA 1-5500-T0356609 PART 1. TITLE: STABILIZERS-GENERAL-NR 2 RT SIDE UPPER PYLON CARRY-THRU PANEL FRAME AJC7593-52-ALTERNATE SURFACE FINISH. FRAME FABRICATED, AS PER DOUGLAS DRAWING AJC7593 REVISION: Y. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 87,700 hrs · 19,502 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NUMBER 272EF AT STATION 1361 TO STATION 1481, FOUND ACCESS DOOR HOLE EDGE DELAMINATED. DELAMINATED FLOOR PANEL 272EF AT CABIN STATION 1361 TO STATION 1481 REMOVED, AS PER AMM 53-21-04. FLOOR PANEL 272EF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION REVISION R. FABRICATED FLOOR PANEL 272EF INSTALLED, AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 87,700 hrs · 19,502 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 614 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 614 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 87,700 hrs · 19,502 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON RIGHT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FASTENERS TOWARDS THE LOWEST FASTENER. RIGHT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164 CRACK REPAIR CARRIED OUT, AS PER EA 1-5530-T0356595 P1. TITLE: STABILIZERS-VERTICAL STABILIZER-CRACK REPAIRS ON VERTICAL STABILIZER REAR SPAR LT & RT FORWARD FLANGES. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 87,700 hrs · 19,502 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER 5 FOUND CRACK APPROXIMATELY 2.2 INCHES AT XOS 490. RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER 5 AT XOS 490 REPAIR CARRIED OUT, AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 17. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. DUPLICATED SDR NR 20-2208 WAS RAISED FOR SNRM N00816. WORK ORDER 00077030 WITH SDR NR 20-2207 REPORTED.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 87,700 hrs · 19,502 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FASTENERS FROM BELOW TOWARDS SECOND FASTENER. DUPLICATED SDR RAISED. PLEASE REFER TO SDR NR 20-2195 FOR THE DETAILS.

Part: TRUNNION — CRACKED (NLG) · airframe 87,700 hrs · 19,502 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING, STATION 583 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATELY 0.4 INCHES. CRACKED NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AT STATION Y=583 REPAIRED, AS PER SRM 53-10-14-2R FIGURE 202 REPAIR 2. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 1500 FLIGHT CYCLES, AS PER SRM 53-10-14-2R FIGURE 202 REPAIR 2 TABLE 201. REQUIREMENT METHOD BY HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT. REPAIR CLASSIFID AS MAJOR PER, GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 87,700 hrs · 19,502 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER 5 FOUND CRACK APPROXIMATELY 2.2 INCHES AT XOS 490 . RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER 5 AT XOS 490 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 17 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: RIB — CRACKED (RT WING SLAT) · airframe 87,700 hrs · 19,502 cycles

RIGHT HAND WING NUMBER 1 SLAT CRUISE PERFORMANCE FILLET RIB AT XIS 150.7474 ALIGNMENT PIN AREA FOUND CRACK. RIGHT HAND WING NUMBER 1 SLAT ASSEMBLY (INCLUDES SLAT AND CRUISE PERFORMANCE FILLET). REMOVED AND REPLACED, AS PER AMM 27-80-20-4. REFERENCE TO WRI: 57504099, SEQUENCE NUMBER 000737 FOR WORK DETAILS. REPAIR CLASSIFIED MINOR, AS PER GMM 06-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,700 hrs · 19,502 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 700 FOUND CRACK . RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 700 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (LT WING) · airframe 87,700 hrs · 19,502 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 688 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 688 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 87,700 hrs · 19,502 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FASTENERS FROM BELOW TOWARDS SECOND FASTENER. LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164 CRACK REPAIR CARRIED OUT, AS PER EA 1-5530-T0356595. PART1, TITLE: STABILIZERS-VERTICAL STABILIZER-CRACK REPAIRS ON VERTICAL STABILIZER REAR SPAR LT SIDE & RT SIDE FORWARD FLANGES. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 87,700 hrs · 19,502 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 682 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 682 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 87,700 hrs · 19,502 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 618 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 618 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 87,700 hrs · 19,502 cycles

LEFT HAND WING FIXED LEADING EDGE SLAT TRACK OUTBOARD AFT CUT OUT SKIN AT XOS 892 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE SLAT TRACK OUTBOARD AFT CUT OUT SKIN AT XOS 892 REPAIRED, AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER, GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 87,700 hrs · 19,502 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING, STATION 583 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATELY 0.45 INCHES. CRACKED NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AT STATION Y=583 REPAIRED, AS PER SRM 53-10-14-2R FIGURE 202 REPAIR 2. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 1500 FLIGHT CYCLES, AS PER SRM 53-10-14-2R FIGURE 202 REPAIR 2 TABLE 201. REQUIREMENT METHOD BY HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT. REPAIR CLASSIFIED AS MAJOR PER, GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 87,700 hrs · 19,502 cycles

FWD CABIN, FOUND FLOOR PANEL 232FF AT STATION 595 TO STA 675 DELAMINATED. DELAMNATED FLOOR PANEL 232FF AT FOWARD CABIN STATION 595 TO STATION 675 REMOVED, AS PER AMM 53-21-04-4. FLOOR PANEL 232FF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 232FF INSTALLED, AS PER AMM 53-21-04-4. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — WORN (MAIN DECK CARGO) · airframe 87,700 hrs · 19,502 cycles

MAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK CROWN WORN AT STATION 6-10, X= -47.5. MAIN DECK CARGO COMPARTMENT-CABIN AT SEAT TRACK STATION 6-10, 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 6-60 TO EXISTING SPLICE STATION 6-0 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 — WORN (MAIN DECK CARGO) · airframe 87,700 hrs · 19,502 cycles

MAIN DECK CARGO COMPARTMENT-CABIN, FOUND SEAT TRACK CROWN WORN AT STATION 1015, X= -27.5 MAIN DECK CARGO COMPARTMENT-CABIN AT SEAT TRACK STATION 1015, 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 989 TO STATION 1029, 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 — WORN (MAIN DECK CARGO) · airframe 87,700 hrs · 19,502 cycles

MAIN DECK CARGO COMPARTMENT-CABIN, FOUND SEAT TRACK CROWN WORN AT STATION 1015 X=47.5. MAIN DECK CARGO COMPARTMENT-CABIN AT SEAT TRACK STATION 1015 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 989 TO STATION 1029, 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 — WORN (MAIN DECK) · airframe 87,700 hrs · 19,502 cycles

MAIN DECK CARGO COMPARTMENT, FOUND SEAT TRACK CROWN WORN AT STATION 879, X= -47.5. MAIN DECK CARGO COMPARTMENT-CABIN, AT SEAT TRACK STATION 879, 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 869 TO STATION 909, X= -47.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: TIRE — LOW PRESSURE (LT MLG) · airframe 86,923 hrs · 19,324 cycles

TIRE PRESS LO LEVEL ALERT AT LRMSE. PRES WENT DOWN TO 56 PSI NR 5 TIRE. REMOVED AND REPLACED NR 5 AND NR 6 TIRE DUE TO NR 5 TIRE LOW PRESSURE. NO DAMAGE NOTED TO LEFT MAIN LANDING GEAR. TIRES CHANGED IAW AMM 32-41-01-4. OK FOR SERVICE.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE ACTUATOR ATTACHED INBD BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 1.2205", FINAL HOLE DIA 1.224" MAXIMUM ALLOWABLE HOLE DIA 1.220", OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127785 A P2 STEP 1C AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. HINGE UPPER MOUNT O/B BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08, EXISTING HOLE DIA 0.944", FINAL HOLE DIA 0.950" MAXIMUM ALLOWABLE HOLE DIA 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T03421926 P1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. HINGE UPPER MOUNT O/B BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 0.943", FINAL HOLE DIA: 0.9465", MAXIMUM ALLOWABLE DIA: 0.944. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-341992 P1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT OUTBD BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.612" MAXIMUM ALLOWABLE HOLE DIA 0.584", SHOULDER BUSHING FABRICATED AS PER EA 1-5750-127785 A P2 STEP 1A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127785 A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. HINGE PIVOT BORE(NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 2.309", FINAL HOLE DIA: 2.315", MAXIMUM ALLOWABLE DIA: 2.3135. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-341992 P1 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE SURFACE CORROSION. HINGE LOWER MOUNT OUTBD BORE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING THICKNESS 0.408", MATERIAL REMOVED FWD FACE 0.004", AFT FACE 0.011", REMAINING THICKNESS 0.393", MINIMUM ALLOWABLE THICKNESS 0.408". REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5756-127785 A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. HINGE ACTUATOR ATTACHED OUTBD BORE (NR 8 HOLE) 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", OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127785 A P2 STEP 1C AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE SURFACE CORROSION. HINGE LOWER MOUNT INBD BORE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING THICKNESS 0.408", MATERIAL REMOVED FWD FACE 0.004", AFT FACE 0.014", REMAINING THICKNESS 0.390", MINIMUM ALLOWABLE THICKNESS 0.408". REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5756-127785 A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE (WING SIDE) LOWER MOUNT O/B BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.712", MAXIMUM ALLOWABLE DIA: 0.709. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-341992 P1 STEP 1C AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-341992 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE ACTUATOR ATTACH I/B BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 1.2105", FINAL HOLE DIA: 1.222", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1- 5750-341992 P1 STEP 1D AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT O/B BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08, EXISTING HOLE DIA 0.705", FINAL HOLE DIA 0.722" MAXIMUM ALLOWABLE HOLE DIA 0.709". SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T03421926 P1 STEP 1B AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0341926 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE BARREL NUT UPPER BOLT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.327", FINAL HOLE DIA 0.406" MAXIMUM ALLOWABLE HOLE DIA 0.391", OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127785 A P2 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE CORROSION. HINGE BARREL NUT LOWER BOLT (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.390", FINAL HOLE DIA 0.410" MAXIMUM ALLOWABLE HOLE DIA 0.391", OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127792 A P2 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 82,518 hrs · 18,034 cycles

LOWER VERTICAL STABILIZER LT SIDE IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN CRACK. CRACKED SKIN REPAIRED AS PER EA 1-5530-T0341902 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. HINGE LOWER MOUNT INBD BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.599" MAXIMUM ALLOWABLE HOLE DIA 0.584", SHOULDER BUSHING FABRICATED AS PER EA 1-5750-127785 A P2 STEP 1A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127785 A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING OUTBD ISLAND AREA UPPER T/E SURFACE STA XORS 1070 FOUND CORROSION. CORRODED SKIN REPAIRED AS PER EA 1-5730-T0341923 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. HINGE LOWER MOUNT I/B BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.587", FINAL HOLE DIA: 0.611", MAXIMUM ALLOWABLE DIA: 0.584. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-127792 A P2 STEP 1A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127792 A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09. EXISTING THICKNESS UPPER: 0.408"; LOWER: 0.408", MATERIAL REMOVED: UPPER: 0.012"; LOWER: 0.012", REMAINING THICKNESS UPPER: 0.396"; LOWER;0.396". REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127792 A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 1.231", FINAL HOLE DIA: 1.252", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127792 A P2 STEP 1C AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 82,518 hrs · 18,034 cycles

LOWER VERTICAL STABILIZER RT SIDE IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN CRACK. CRACKED SKIN REPAIRED AS PER EA 1-5530-T0341903 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — WORN (LT WING) · airframe 82,518 hrs · 18,034 cycles

LT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) PIVOT BUSHING WORN. WORN BUSHING AT FWD HINGE (WING SIDE) PIVOT BORE, REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0332025 A PART 1 STEP 1F (1) AND STEP 1F (3). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE BARREL NUT UPPER BOLT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.390", FINAL HOLE DIA: 0.410", MAXIMUM ALLOWABLE DIA: 0.391. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127792 A P2 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING OUTBD AILERON AREA UPPER T/E SURFACE STA XORS 1040 FOUND CORROSION. CORRODED SKIN REPAIRED AS PER EA 1-5730-T0341923 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT O/B BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.595", FINAL HOLE DIA: 0.611", MAXIMUM ALLOWABLE DIA: 0.584. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-127792 A P2 STEP 1A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127792 A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-07. EXISTING HOLE DIA: 1.064", FINAL HOLE DIA: 1.1065", MAXIMUM ALLOWABLE DIA: 1.0935. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332025 A PART 1 STEP 1F (1) AND STEP 1F (3). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. HINGE BARREL NUT HOLE (NR 10 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.678", FINAL HOLE DIA: 0.707", MAXIMUM ALLOWABLE DIA: 0.667. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127792 A P2 STEP 1D AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — WORN (RT WING) · airframe 82,518 hrs · 18,034 cycles

RT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) PIVOT BUSHING WORN. WORN BUSHING REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332026 A PART 1 STEP 1F(1) AND STEP 1F(3). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. HINGE PIVOT INBD BORE (HOLE G & F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.282", FINAL HOLE DIA: 1.326", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0324370 C PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT O/B BORE CORROSION. HINGE PIVOT OUTBD BORE (HOLE B & A) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.218", FINAL HOLE DIA: 1.251", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-69374 C PART 5 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

RT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. HINGE PIVOT INBD BORE (HOLE G & F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.2565", FINAL HOLE DIA: 1.281", MAXIMUM ALLOWABLE DIA: 1.220Ï¿½. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-69374 C PART 5 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

LT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT O/B BORE CORROSION. HINGE PIVOT O/B BORE (HOLE A & B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.255", FINAL HOLE DIA: 1.283", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0324370 C PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DELAMINATED (NR 2 SPOILER) · airframe 82,518 hrs · 18,034 cycles

RT WING NR 2 SPOILER PANEL UPPER SURFACE FOUND DELAMINATION, STA XOSP2 523 TO XOSP2 530. UPPER SURFACE REPAIRED AS PER EA 1-5750-T0341848 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1871) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK RIGHT, AFT FLOOR SEAT TRACK AT BS 1871, RBL 75.25, FOUND THE FLANGE CORRODED. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS 1860 TO 1887 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1783) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 1783, RBL 27.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS 1771 TO 1887, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (BS 1887-2007) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK AFT FLOOR SUPPORT AT BS 1887 - 2007, X=-25 WAS FOUND CRACKED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, AND DRAWING AGA7087, REVISION M. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1880) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS1880, X=-47.5 FOUND CORRODED. CORROSION REMOVED AND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1831 TO 1887 IAW SRM 53-00- 52-2R, FIG 201, REPAIR 1. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (BS 1887-2007) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK AFT FLOOR SUPPORT AT BS 1887 - 2007, X= 25 WAS FOUND CRACKED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, AND DRAWING AGA7087, REVISION M. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1800) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 1800, RBL 8.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED, AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1771 TO 1887 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK RT AFT FLOOR CURVE SEAT TRACK AT STA 1901-2007 X=-107 FOUND CORROSION. CORROSION REMOVED AND EXCEEDED LIMIT PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK (CURVED) REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE AT STA 1877 TO STA 2007, X=-107 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1791) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 1791, LBL 8.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS 1771 TO 1887, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (BS 535) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK LT FRAME AT BS 535 LONGERON 19L FOUND WITH AN EXISTING REPAIR DOUBLER DAMAGED. THE DAMAGED OUTER REPAIR ANGLE WAS REMOVED IAW SRM 51-33-01-0G, AND REPAIRED IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 82,518 hrs · 18,034 cycles

RIGHT WING, FIXED LEADING EDGE COMPARTMENT AT XOS 907 HAD A STRINGER CRACKED. REPAIRED THE STRINGER IAW SRM 57-40-03-2R, FIGURE 202, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (BS 1887-2007) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK AFT FLOOR SUPPORT AT BS 1887 - 2007, X=-56 WAS FOUND CRACKED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, AND DRAWING AGA7551, REVISION G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1871) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 1871, LBL 8.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS 1771 TO 1887 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1880) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK, BS 1880 X=-8.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT, FROM BS 1771 TO 1887 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1880) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 1880, X=-27.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS 1771 TO 1887, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 455) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 455, X= 27.5 FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS421 - 467, IAW SRM 53-00- 52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 475) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 475, X=75.25 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPAIRED THE SEAT TRACK FLANGE IAW SRM 53-00-52-2R, FIG 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 82,518 hrs · 18,034 cycles

LOWER VERTICAL STABILIZER FRONT CENTER SPAR FITTING FOUND CRACKED AT AFT FUSELAGE COMPARTMENT LEFT HAND SIDE APPROXIMATE STA 2014. CRACKED LOWER VERTICAL STABILIZER FRONT CENTER SPAR FITTING AT AFT FUSELAGE COMPARTMENT LEFT HAND SIDE APPROXIMATE STA 2014 REPAIRED AS PER EA 1-5530-T0341975 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 82,518 hrs · 18,034 cycles

RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 642 WAS 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: SEAT TRACK — CRACKED (BS 755) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 755, RBL 8.5 FOUND CRACKED. SEAT TRACK REPLACED FROM BS 785 TO 745 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 755) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 755, LBL 47.5 WAS FOUND CRACKED. THE SEAT TRACK WAS REPLACED BETWEEN BS 725 & 765, IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (BS 1641) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK LEFT FRAME AT BS 1641, LONGERON 12L WAS FOUND DAMAGED. THE FRAME WAS REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,518 hrs · 18,034 cycles

RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 626 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1215) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1215, RBL 27.5 WAS FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1199 TO 1229 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1284) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 1284, RBL 47.5 WAS FOUND WITH CROWN DAMAGE. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1269 TO 1311 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (MAIN DECK) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK, BS 5-11 LBL 8.5 WAS FOUND WITH CROWN DAMAGE. BLENDED AND FOUND TO BS OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 5-63 TO EXISTING SPLICE IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (MAIN DECK) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK CROWN AT 5-11, X= 47.5 WAS FOUND DAMAGED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,518 hrs · 18,034 cycles

RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 665 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 775) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 775, RBL 75.25 CROWN WAS DAMAGED. REMOVED THE CORROSION, AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT BETWEEN BS 815 & 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 5-11, RBL 8.5 FOUND CROWN DAMAGED. BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 1421) · airframe 82,518 hrs · 18,034 cycles

MAIN DECK SEAT TRACK AT BS 1421, LBL 47.5, WAS THE CROWN WAS FOUND DAMAGED. THE SEAT TRACK WAS BLENDED AND FOUN OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT, BS 1411 - 1451 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,518 hrs · 18,034 cycles

RIGHT WING LEADING EDGE CAVITY, BEADED DOUBLER AT XOS 652 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (BS 535) · airframe 82,518 hrs · 18,034 cycles

NR 3 AIR CONDITIONING ACCESS DOOR 114AR. UPPER AFT CORNER SKIN CUTOUT WAS FOUND CRACKED AT BS 535. REPAIRED IAW SRM 53-20-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,518 hrs · 18,034 cycles

LEFT WING LEADING EDGE CAVITY BEADED DOUBLER, XOS 553 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1560) · corrosion level 2 · airframe 82,518 hrs · 18,034 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1560, LBL 27.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT, BS 1571 TO EXISTING SPLICE IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,518 hrs · 18,034 cycles

LEFT WING LEADING EDGE CAVITY BEADED DOUBLER, XOS 543, WAS FOUND CRACKED. 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 (RT WING) · airframe 82,518 hrs · 18,034 cycles

RIGHT WING FIXED L/E, XOS 906 RIB DOUBLER CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW DOUBLER IAW DWG ARB3954, REVISION K. INSTALLED THE NEW DOUBLER IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 82,518 hrs · 18,034 cycles

RIGHT WING, DROOP LEADING EDGE ASSY, UPPER SURFACE FASTENER AREA FOUND CRACKED AT XDLE 328. REPAIREDTHE SKIN IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 82,518 hrs · 18,034 cycles

RIGHT WING FIXED L/E COMPARTMENT, XOS 666, STRINGER WAS CRACKED. REPAIR THE STRINGER IAW SRM 57-40-03-2R, FIGURE 202, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 82,518 hrs · 18,034 cycles

LEFT WING LEADING EDGE CAVITY, FORMER AT XOS 1025 WAS FOUND CRACKED. THE FORMER WAS REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW FORMER IAW DRAWING ARB2920, REVISION BB. INSTALLED THE FORMER IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (RT SPOILER) · corrosion level 2 · airframe 77,452 hrs · 16,498 cycles

RIGHT WING, NR 2 SPOILER OTBD TIP FOUND CORRODED AS MARKED AT XOSP2 546.436. REPAIRED AS PER EA 1-5750-T0327284A PART 1. LOWER SKIN SRM REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,452 hrs · 16,498 cycles

CABIN LEFT BS 1471 - 1481, X 75.25 SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1390 TO STA 1531 X=75.25 IAW SRM 53-00-52-2R, FIG 201, REPAIR NR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,452 hrs · 16,498 cycles

LEFT WING FIXED LEADING EDGE CAVITY AT XOS 733 BEADED DOUBLER FOUND CRACKED. AREA REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

R3 DOOR AT BS 1305.25 - 1315.42, LONGERON 26 - 27R AFT DOOR FRAME LOWER WEB BOX FOUND CRACKED. AFT JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R, FIG 201, REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,452 hrs · 16,498 cycles

LEFT WING FIXED LEADING EDGE CAVITY AT XOS 880 BEADED DOUBLER FOUND CRACKED. AREA REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

L3 DOOR AT BS 1305.25 - 1315.42, LONGERON 26 - 27L. AFT DOOR FRAME LOWER WEB BOX FOUND CRACKED. AFT JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R, FIG 201, REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

CABIN RT STA 635, X= -8.5 SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665 X =-8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

CABIN LT STA 635, X=27.5 SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665 X=27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

CABIN LEFT, STA 1410, X=8.5, SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1310 TO STA 1410. X= 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

CABIN LT STA 1541-STA 1551, X=8.5 SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531-STA 1670 X= 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO SNRM NR N00435 FOR WORK DETAIL.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

BS 1341, X -8.5, SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR NR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

CABIN LEFT, STA 1641, X=8.5 SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531 TO STA 1670 X= 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

CABIN RT STA 635, X=-27.5 SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665 X= -27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR NR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 77,452 hrs · 16,498 cycles

CABIN LT STA 635, X=47.5 SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665 X=47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STICK SHAKER — FALSE ACTIVATION (COCKPIT) · airframe 77,189 hrs · 16,420 cycles

STICK SHAKER: AFTER TAKEOFF AND BEFORE FLAP RETRACTION, THE STICK SHAKER ACTIVATED FOR ABOUT 2 SECONDS. THE PDF SHOWED BOXED, SLATS, IN AMBER. ALTITUDE WAS ABOUT 300 FEET. NO CURRENT OR PREVIOUS LEG FAULTS IN FCC'S. PERFORMED OPERATION TEST OF SLAT POSITION, INDICATION REF MM 27-84-00-5, ALL PASS. CHECKED SLAT, FLAP HANDLE POSITION TRANSMITTER REF MM 27-50-00-5, WITHIN LIMITS AS INDICATED IN FCC 1 & 2 SENSOR READOUT. PERFORMED FCC 1 AND 2 RTS REF MM 22-00-00-5, ALL PASS. ACFT OK FOR SERVICE.

Part: PANEL — ABNORMAL (NR 1 PYLON) · airframe 758 hrs · 15,963 cycles

ON ARRIVAL FOUND NR 1 ENG PYLON MISSING PANEL 438EL. INSTALLED REPAIRED ATTACH BRACKET IAW SRM 51-35-01. INSTALLED NEW 438EL PANEL ON NR 1 ENG IAW MM 54-81-01-4-0. ACFT OK FOR SERVICE.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 754 hrs · 15,852 cycles

MINOR CORROSION ON UPPER SURFACE OF RT WING SKIN PANEL JUST INBD OF XRDS345, STRINGER 2, AFT THE NR 3 ENG. REPAIRED IAW SRM 57-00-01-1A, WITHIN LIMITS AS FAR AS MATERIAL REMOVED.

Part: SIGN — UNSECURE (CABIN) · airframe 749 hrs · 15,670 cycles

L1 SLIDING DOOR OVERHEAD EXIT SIGN IS HANGING DOWN. L1 DOOR SLIDING PANEL INOPERATIVE DUE TO EMER EXIT LIGHT REMOVED. REFERENCED & COMPLIED WITH AMM 25-23-23-2. RELEASED TO OPEN ITEM LIST EMER LIGHT WIRES CAPPED & STOWED. R & R L1 DOOR SLIDING CEILING PANEL TENSION SPRING IAW AMM 25-23-23-4. INSTALLING THE PANELS NEXT. TERMINATING ACTION ACCOMPLISHED FOR AMM 25-23-23-2 A. INSTALLED PASSENGER L1 DOOR SLIDING CEILING PANEL USING AMM 25-23-23-4. OPERATIONS CHECKED GOOD.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 73,148 hrs · 15,090 cycles

CRACK INDICATION FOUND DURING X-RAY INSPECTION AT BS 5-0, LONGERON SPLICE 1R FROM TWO EACH FASTENER HOLE. CRACK LENGTH APPROX 0.3 INCHES. AREA REMOVED IAW SRM 51-33- 01. NEW LONGERON SPLICE FABRICATED IAW DRAWING AEA7634 REVISION B. NEW LONGERON SPLICE INSTALLED IAW SRM 51-33-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 73,148 hrs · 15,090 cycles

CENTER ACCESSORY COMPARTMENT BS 6-87 LBL 51 LONGERON SPLICE FOUND CRACKED. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-33-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1581) · corrosion level 2 · airframe 73,148 hrs · 15,090 cycles

CABIN MAIN DECK CARGO TRACK BS 1581 X -8.5 FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 73,148 hrs · 15,090 cycles

LEFT WING FIXED EDGE BEADED DOUBLER CRACKED AT XOS 673 - 679. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 14. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,148 hrs · 15,090 cycles

LEFT WING FIXED LE BEADED DOUBLER CRACKED XOS 608 - 703. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (MAIN CARGO) · airframe 73,148 hrs · 15,090 cycles

CABIN MAIN DECK CARGO TRACK FOUND CRACKED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 73,148 hrs · 15,090 cycles

LEFT WING FIXED LE BEADED DOUBLER CRACKED AT XOS 626 - 629. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 73,148 hrs · 15,090 cycles

RIGHT WING ANTI-ICING TELESCOPIC DUCT DOOR CUT OUT XOS 464 - 470 FOUND CRACKED AT OTBD CORNER. REPAIRED IAW SRM 57-40-01, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 72,142 hrs · 14,747 cycles

GOT INTERMITTENT CABIN SMOKE LEVEL 3 ALERT WITH TRITONE ALERT WAS ON 2 TIMES FOR ABOUT 2 SECONDS. LANDED UNEVENTFULLY & FIRE DEPT SAID NO INDICATION OF FIRE OR HEAT. FOUND NR 9 SMOKE DETECTOR FAILED. R & R NR 9 SMOKE DETECTOR & TESTED GOOD IAW AMM 26-15-01-4. ACFT OK FOR SERVICE.

Part: PANEL — MISSING (NR 3 PYLON) · airframe 71,156 hrs · 14,380 cycles

FOUND A PANEL MISSING ON NR 3 ENG INBD, PANEL MPN AUB7726-501. SS OIL 20NOV13 09:05 SYD U NO RESTRICTION IAW1-5480-T0304174 NR 3 ENG PYLON PANEL 488EL MISSING FROM INBD SIDE. OK TO CONTINUE IAW EA 1-5480-T0304174. COMPLIED WITH PT1 OF EA 1-5480-T0304174 C0575159 OIL 20NOV13 09:05 SYD U NO RESTRICTION. INSTALLED MISSING PANEL. AIRCRAFT OK FOR SERVICE.

Part: BRACKET — TORN (MLG) · airframe 69,976 hrs · 13,989 cycles

AFTER TAKEOFF HAD UNSAFE LT GEAR UP INDICATION. COMPLIED WITH CHECKLIST AND RECYCLED THE GEAR. HAD A SECOND UNSAFE GEAR UP INDICATION ON BOTH INDICATORS. NO FUEL WAS DUMPED. FOUND AFT MLG TRUCK HOSE SUPPORT BRACKET BROKEN. HOSE/HARNESS SUPPORT AND ANTI-SKID HARNESS DAMAGED. REPLACED BROKEN BRACKET ON REAR OF LT MAIN GEAR FOR HYD AND ELECTRICAL ROUTING TO BOGGIE. REPLACED DAMAGED ANTI-SKID HARNESS. ACCOMPLISHED OPS TEST OF ANTI-SKID SYS FOR LT GEAR, ACCOMPLISHED BRAKE TEMP MONITOR, TIRE PRESSURE IND SYS TEST, ACCOMPLISHED MAIN GEAR AND GEARWELL DOOR OPS TEST FOR LT MLG. OPS TEST NORMAL.

Part: RELAY — FAILED · airframe 69,073 hrs · 13,710 cycles

AFTER TAKEOFF RECEIVED ACFT TIE 1 OFF ALERT. WITH NR 1 IDG DISCONNECTED, LOST LT BUSS AND MOST DISPLAYS ON CAPTS SIDE, EMERGENCY POWER CAME ON. ADG WAS DEPLOYED TO CHARGE BATTERY. FOUND BTR-1/INTFC FAULT CODE. PERFORMED TROUBLESHOOTING IAW FIM 24-20-37, FOUND BTR-1 FAIL INTERMITTENT, REPLACED BTR-1 (R2-4) IAW AMM 24-26-05-4. ACTIVATED IDG NR 1, RAN ALL ENGINES IAW JRH, ALL ENGINE PARAMETERS NORMAL. PERFORMED OPS TEST OF AC BUSS TIE RELAY IAW AMM 24-26-05-5, CARRIED OUT OPS TEST OF EPCU IAW AMM 24-08-01-5, ALL TEST SATIS TURN ON/OFF APU. POWER & ETERNAL POWER SEVERAL TIMES, FOUND AC TIE 1 WORK NORMAL. PERFORMED OPS TEST OF ESC IAW AMM 21-08-01-5, ALL TEST PASSED, AND PERFORMED BOTH FCC AUOTFLIGHT TEST PER AMM 22-00-00-5, ALL TEST PASSED, AC REMAINED CATIII. ACFT OK FOR SERVICE.

Part: SUPPORT FITTING — DAMAGED (NR 8 SLAT) · airframe 68,536 hrs · 13,554 cycles

LEFT WING NR 8 L/E SLAT INBD SUPPORT FITTING FWD HOLE OTBD SIDE SURFACE FOUND STEPPED. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GENERAL MM 6-2-100, REV 115.

Part: SUPPORT FITTING — CHAFED (LT WING) · airframe 68,536 hrs · 13,554 cycles

LEFT WING NR 8 L/E SLAT, INBD SUPPORT FITTING, AFT HOLE, BOTH SIDES SURFACES FOUND CHAFED. FOUND DURING LT OTBD SLAT DRIVE CABLES TENSION CHECK. SUPPORT FITTING REMOVED IAW STRUCTURAL REPAIR MANUAL 51-31-01 REV 50. HOLES PICKED UP ON NEW SUPPORT FITTING IAW STRUCTURAL REPAIR MANUAL 51-31-01 REV 50. NEW SUPPORT FITTING INSTALLED IAW STRUCTURAL REPAIR MANUAL 51-31-01 REV 50 AND FEDEX EA 1-5750-163522 TITLE "WINGS-FLIGHT SURFACES-LT WING-NR 8 SLAT ASSY-INBD RIB ASSY REPLACEMENT-REPLACEABLE STRUCTURAL COMPONENT TRACKING" WORK INSTRUCTIONS. REPAIR CLASSIFIED AS MAJOR IAW GENERAL MM 6-2-100, REV 115. LT WING, NR 8 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW ACFT MM 27-80-00-830-805, REV 74.0 AND FOUND SATISFACTORY.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 68,536 hrs · 13,554 cycles

LEFT WING INBD FLAP UPPER SKIN PANEL ASSY CRACKED AT XIFH 171.3. REPAIRED IAW SRM 57-00-01 REPAIR 1 FIGURE 201 REVISION 50 AND EA 1-5750-163526

Part: SEAT TRACK — CORRODED (BS 555) · corrosion level 2 · airframe 68,536 hrs · 13,554 cycles

MAIN DECK SEAT TRACK CLIP NUT HOLE AT BS 5-55, "X" = -107.25 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS FABRICATED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 68,536 hrs · 13,554 cycles

LEFT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 203, REPAIR 15, TYPE A, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM REVISION 115.

Part: SLAT TRACK — CRACKED (RT WING SLAT) · airframe 68,536 hrs · 13,554 cycles

RT WING L/E NR 10 SLAT TRACK CUT OUT INBD CORNER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 201, REPAIR 7, REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,536 hrs · 13,554 cycles

CENTER LANDING GEAR WHEEL WELL RT UPPER FORWARD SPLICE JOINT FOUND CRACKED. SPLICE REMOVED AND REPLACED WITH WITH NEW SPLICE IAW SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — CORRODED (BS 1372) · corrosion level 2 · airframe 68,536 hrs · 13,554 cycles

MAIN DECK SEAT TRACK BS 1372, "X" = -8.5 FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 50. NEW SEAT TRACK SEGMENT REWORKED IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 50. NEW SEAT TRACK SEGMENT INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: FRAME — DENTED (ZONE 200) · airframe 68,536 hrs · 13,554 cycles

DENT FOUND FRAME AT BS 1741, L11R. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — CORRODED (BS 1861) · corrosion level 2 · airframe 68,536 hrs · 13,554 cycles

MAIN DECK SEAT TRACK BS 1861, "X" = -27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201 REPAIR 5, REV 50. REPAIR PARTS FABRICATED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: FRAME — DENTED (BS 1641) · airframe 68,536 hrs · 13,554 cycles

DENT FOUND ON RT SIDE OF CABIN FUSELAGE FRAME AT BS 1641, NEAR L11R. REPAIR CARRIED OUT IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: FRAME — DENTED (BS 1761) · airframe 68,536 hrs · 13,554 cycles

DENT FOUND AT RT SIDE FRAME AT BS 1761, NEAR L11R. REPAIRED IAW SRM 53-00-07 FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,536 hrs · 13,554 cycles

CENTER CARGO BAY BS 5-123, L41L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7115 REVISION D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 500) · airframe 68,536 hrs · 13,554 cycles

DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND CRACK INDICATIONS AT FASTENER HOLES. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: LONGERON FITTING — CRACKED (ZONE 100) · airframe 68,536 hrs · 13,554 cycles

CENTER CARGO COMPARTMENT BS 5-123, LONGERON 44 RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,536 hrs · 13,554 cycles

CENTER CARGO BS BS 5-123, LONGERON 40L LONGEORN SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,536 hrs · 13,554 cycles

CENTER CARGO BAY BS 5-123, L46L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,536 hrs · 13,554 cycles

CENTER CARGO BAY BS 5-123 L45R LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,536 hrs · 13,554 cycles

CENTER CARGO COMPARTMENT BS 5-123, LONGERON 37 RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE REMOVED AS PER SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 50. SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: WEB — CRACKED (ZONE 500) · airframe 68,536 hrs · 13,554 cycles

LEFT WING INBD FLAP OTBD EDGE CENTER WEB FOUND CRACKED. CRACKED WEB REMOVED AS PER SRM 51-35-01 REVISION 50. NEW WEB FABRICATED IAW DRAWING ARC2305 REVISION C. NEW FABRICATED WEB INSTALLED IAW SRM 51-35-01 REVISION 50 AND EA 1-5750-163519. FLAP OPS TEST CARRIED OUT IAW AMM 27-50-00-860-801 REVISION 74 AND FOUND SATISFACTORY. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 68,536 hrs · 13,554 cycles

RT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 74. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 68,536 hrs · 13,554 cycles

UPPER CENTER CARGO DOOR FRAME, BS 1743 BETWEEN LONGERON 28 - 29R, "X" = 106 FOUND CRACKED. APPROX 1.25" IN LENGTH. REPAIRED IAW EA 1-5310-163524. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SPAR CAP — CRACKED (ZONE 600) · airframe 68,536 hrs · 13,554 cycles

RT WING T/E REAR SPAR LOWER CAP XORS 433 FOUND CRACKED. REMOVED AND REPLACED WITH NEW SILL AS PER SRM 51-34-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: BEAM — BROKEN (R3 DOOR) · airframe 68,536 hrs · 13,554 cycles

R3 DOOR NR 7 BEAM FOUND BROKEN. BEAM REMOVED IAW SRM 51-31-01 REVISION 50. HOLES PICKED UP ON NEW BEAM IAW SRM 51-31-01 REVISION 50. NEW BEAM INSTALLED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 600) · airframe 68,536 hrs · 13,554 cycles

DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND 713.6. FOUND CRACKED INDICATION AT FASTENER HOLES. FASTENER HOLES CRACKED AT RIGHT WING LOWER SKIN ACCESS DOOR COUTOUT REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,536 hrs · 13,554 cycles

CENTER CARGO BAY BS 5-123, L44L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.

Part: TIE ROD — BROKEN (NLG DOOR) · airframe 67,455 hrs · 13,230 cycles

ON GEAR RETRACTION AFTER T/O, THE ACFT HAD SEVERE VIBRATION. VIBRATION DIMINISHED AFTER ACFT WAS SLOWED AND GEAR EXTENDED. LANDING WAS NORMAL. NO FUEL DUMP. NO UNSAFE GEAR INDICATIONS. FOUND RT NLG DOOR TIE ROD END BROKE, REMOVED, REPLACED AND ADJUSTED RT NLG DOOR DRIVE LINK ASSY IAW MM 32-23-03-4. OPS CHECKED GOOD IAW MM 32-36-01-4.

Part: CONTROL VALVE — INOPERATIVE (NLG STEERING) · airframe 67,388 hrs · 13,208 cycles

TOUCHDOWN FELT NORMAL, NO HARD PULL, BUT AS LANDING ROLL PROGRESSED IT SEEMED TO TAKE AN INCREASING AMOUNT OF RUDDER IN ORDER TO STAY ON RUNNWAY CENTERLINE W/ WINDS 40 DEG LT OF CENTERLINE AT 12 KNOTS. WHEN I DID GET ON THE BRAKES THEY GRABBED SIGNIFICANTLY AND THEY CHUGGED UNTIL LEAVING THE RUNWAY. R & R STEERING CONTROL VALVE AND STEERING CONTROL CABLE.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 66,128 hrs · 12,885 cycles

CRUISE FLIGHT NR 1 OIL QTY DECREASING, NOTICED AT 8 QTS REMAINING. AT 5 QTS REMAINING PLACED NR1 ENG AT IDLE THIS SIGNIFICANTLY SLOWED THE RATE OF DEPLETION 2 HRS LATER OIL QTY DECREASED TO 0 WITH A CORESPONDING DROP IN PRESSURE TO 15 PSI. SHUTDOWN NR 1 ENG IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PER WORKCARD 71T0901-GE. OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 65,835 hrs · 12,803 cycles

DURING EMERGENCY LIGHT TEST RECEIVED A LEVEL 1, EMERGENCY LIGHT BATTERY 1 LOW ALERT. R & R POWER SUPPLY PER AMM 33-51-01-4-0. TESTED OK.

Part: OVEN — ODOR (GALLEY) · airframe 65,369 hrs · 12,674 cycles

OVEN EMITTED A STRONG BURNING ODOR. LOOSE PARTS (METAL GRATE AND SCREWS) FOUND STACKED ASIDE THE OVEN. CLEANED OVEN IAW SMP, RAN OVEN; OVEN WORKED NORMALLY AND DID NOT SMELL. ACFT OK FOR SERVICE. FINAL CLOSED.

Part: BULB — FAILED (ESCAPE SLIDE) · airframe 64,400 hrs · 12,433 cycles

DURING PREFLIGHT CHECK FOUND LH DOOR EVAC SLIDE REMOTE PRESSURE PRESS TO TEST LIGHT INOP. REPLACED PRESS TO TEST SW BULB AND REMOTE PRESS INDICATION OPS TEST PASSED PER MM25-61-04-4-0

Part: STRUCTURE — DEPARTED (NR 2 NACELLE) · airframe 64,394 hrs · 12,432 cycles

AFTER DEPARTURE, WEST OF THE AIRPORT BY APPROX 20NM OVER THE WATER, FELT A SHARP BUMP THAT FELT LIKE WAKE TURBULENCE CLIMBING THROUGH APPROX 14000 FT AND 320 KTS UPON LANDING, COWLING ON NR 2 ENGINE JUST BEHIND WHERE THE REVERSER SEPARATES IS COMPLETELY MISSING-ALL COCKPIT INDICATIONS NORMAL-ACFT HANDING NORMAL.

Part: SKIN — CRACKED (ZONE 500) · airframe 63,477 hrs · 12,205 cycles

LT WING FIXED L/E SLAT TRACK NR12 CUT OUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 201, REV 45. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 63,477 hrs · 12,205 cycles

MAIN DECK CARGO TRACK AT STATION 1665, 'X' = -27.5 FOUND CORRODED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM STA 1631 TO STA 1671, 'X' = -27.5 IAW SRM 53-00-52, FIG 201 REPAIR 1, REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 63,477 hrs · 12,205 cycles

RT WING FIXED L/E SLAT TRACK NR12 CUT OUT INBD LOWER FOUND CRACKED. REPAIR CARRIED OUT AT RT WING L/E SLAT TRACK NR12 CUT OUT INBD LOWER AREA IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 45. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 111.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 63,477 hrs · 12,205 cycles

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

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 63,477 hrs · 12,205 cycles

MAIN DECK - DURING HFEC INSP, LONGERON 3, RT SPLICE FITTING AT STA 6-100, FOUND 02 EACH CRACKED APPROX 0.5 INCH. CRACKED SPLICE FITTING AT STA 6-100. R & R IAW SRM 51-31-01, REV 45. NEW LONGERON SPLICE FITTING FABRICATED IAW DOUG DWG A6A7112 REV A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: FRAME — DEFORMED (ZONE 200) · airframe 63,477 hrs · 12,205 cycles

MAIN DECK CARGO FRAME AT STA 1661, LONGERON 12 LT FOUND DEFORMED. MAIN DECK CARGO - DEFORMED FRAME AT STA 1661, LONG 12 LT REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2 REV 45. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES, IAW SRM 53-00-07, FIG 201, REPAIR 2, TABLE 201 REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 63,477 hrs · 12,205 cycles

LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND 04 EACH FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 63,477 hrs · 12,205 cycles

LT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R IAW AMM 27-50-22-4 REV 69.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5, REV 69.0 FOUND SATISFACTORY.

Part: SPAR CAP — CORRODED (LT WING) · airframe 63,477 hrs · 12,205 cycles

LEFT WING REAR SPAR LOWER CAP, ACCESS THROUGH PANEL NR541FB, 8 IN OTBD OF JACK POINT FOUND CORROSION. REMOVED IAW SRM 51-31-01, REV 45 AND REPLACED WITH A FABRICATED STRAP IAW SRM 51-34-01, REV 45. STRAP FABRICATED IAW DWG ARB2615 REV D. FUEL LEAK CHECK CARRIED OUT ON REWORK AREA IAW AMM 12-11-04 REV 69.0 FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 111.

Part: CONTROL UNIT — FAILED (FIRE DETECTION) · airframe 62,888 hrs · 12,056 cycles

DURING DESCENT, FSS DISCHARGED LIGHT ILLUMINATED. COMPLIED WITH EA EA 1-2620-141430 AND EA 1-2623-1441 28. OK. REMOVED AND REPLACED FIRE CONTROL UNIT, BOTH SENSOR BARS AND SURROGATE FIRE DETECTION UNIT AND WIRING HARNESS ON PENTRATOR 13.

Part: O-RING — MISSING (NR 2 EDP) · airframe 62,833 hrs · 12,041 cycles

NOTICED NR 2 ENGINE OIL AT 7 QTS. LOSING APPROX 1 QT IN 20 MINUTES. DIVERTED. ENROUTE OIL QTY DECREASED TO 2 QTS & OIL PRESS STARTED TO DECREASE. ENGINE SHUTDOWN. EMERGENCY DECLARED. LANDING UNEVENTFUL. ISOLATED LEAK TO NR 2 ENG LOWER INBD HYD PUMP DRIVE PAD DRAIN. CAPPED DRAIN & PLUGGED DRAIN LINE IAW MM 71-70-00-6 1, PARA 12 (E) REPAIR GOOD FOR 10 ENG CYCLES. ON ARRIVAL, OIL LEVEL CHECKED, NO FURTHER LOSS OF OIL NOTED. REMOVED LT HYD EDP IAW AMM 29-11-20-4 & INSPECTED GARLOK SEAL, FOUND NO O-RING PACKING INSTALLED ON LT HYD EDP. INSPECTED EDP, NO DISCREPANCIES NOTED. INSTALLED O-RING ON EDP SHAFT, REINSTALLED EDP, & RAN NR 2. LEAK CHECKED GOOD ON HYD SYS & EDP. NO FURTHER OIL LEAKS NOTED.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 59,975 hrs · 11,370 cycles

LOST HYD 3 FLUID AT LEVEL OFF ALT. THE LOSS WAS RA PID BEFORE PUMPS COULD BE SECURE. ALT GEAR WAS EXT ENDED. UNABLE TO GET CTR FEAR DOWN. LANDED APPROX 15000 NR OVERWEIGHT. PUMPED 9000 NR OF FUEL. FOUND HYD LINE IN RT W/W BETWEEN NR 3 HYD RES C/L/G CNTL VALVE BROKEN. MFG AND INSTALLED HYD LINE USING PERMASWAGE FITTINGS IAW CH 20. LK CK GOOD. SERVICED HYD JACKED AC AND SWUNG GEAR SEVERAL TIMES MOVED AC TO GATE RAN NR 3 ENG LEAK CHECK OF PUMPS AND FILTERS GOOD HYD QTY STABLE.

Part: LINE — BURST (OXYGEN SYSTEM) · airframe 58,935 hrs · 11,136 cycles

O2 LINE BEHIND 1ST OBSERVERS MASK BURST. ALL 3 OXYGEN SYS DEPLETED. COMPLIED WITH EA 1-3510-132815, DOC PART NR 1. INSTALLED CAP AND LEAKED CHECKED. REINSTALLED NR1 OBSERVER OXY MASK STORAGE BOX. CONNECTOR PLUG UNSECURED. REMOVED AND REPLACED NR 2 AND NR 3 O2 BOTTLES IAW MM 35-11-01-4.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 58,259 hrs · 10,975 cycles

RIGHT WING INBOARD FLAP ASSEMBLY UNDER-SURFACE, EXISTING DOUBLER REPAIR FOUND AT LOWER SEGMENT AFT EDGE, STA XIFH 270. FOUND NOT CONFORM TO SRM REPAIR. RT INBD FLAP ASSY REMOVED AND REPLACED AS PER AMM 27-50-20-4 REV. 62. ADJUSTMENT AND TEST CARRIED OUT FOUND SATIS AS PER AMM 27-50-00-5 REV. 62. EO 1-5100-75001 A4 PT1, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 107.

Part: SKIN — MISREPAIRED (NR 4 SLAT) · airframe 58,259 hrs · 10,975 cycles

AGING INSPECTION, EXISTING REPAIR FOUND ON LT WING NR 4 SLAT LOWER SURFACE STA XOS= 602. EXISTING REPAIR ON LT WING NR 4 SLAT LOWER SURFACE STA XOS=602 EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. NR 4 SLAT ASSEMBLY REMOVED, REPLACED AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-80-30-4 REV 62, EO NR 1-5100-7-5001 A4 PT1.

Part: SKIN — MISREPAIRED (RT WING AILERON) · airframe 58,259 hrs · 10,975 cycles

RIGHT WING, INBOARD AILERON ASSY UPPER SURFACE, EXISTING DOUBLER REPAIR FOUND AT LEADING EDGE STA XIA 328. RIGHT WING, INBOARD AILERON ASSY UPPER SURFACE, EXISTING REPAIR FOUND NOT IN ACCORDANCE WITH SRM REPAIR. RIGHT WING INBOARD AILERON ASSY UPPER SURFACE CARRIED OUT REPAIR AS PER SRM 57-10-00 FIG 38 VOL I REV 40, EO 1-5100-7-5001 A4 PT. 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 107.

Part: SKIN — MISREPAIRED (NR 2 SLAT) · airframe 58,259 hrs · 10,975 cycles

AGING INSPECTION, EXISTING REPAIR FOUND ON LT WING NR 2 SLAT LOWER SURFACE STA XIS= 325. EXISTING REPAIR ON LT WING NR 2 SLAT LOWER SURFACE STA XIS= 325 EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. LT WING NR 2 SLAT LOWER SURFACE STA XIS= 325 SKIN REPAIRED AS PER SRM 57-00-01 FIG 8 VOL I REV 40. EO 1-5100-7-5001 A4 PTI. REPAIR CLASSIFIED AS MAJORS PER GMM 6-2-100 REV 107.

Part: DOOR — MISREPAIRED (ZONE 100) · airframe 58,259 hrs · 10,975 cycles

CENTER CARGO, DOOR FOUND WITH EXISTING REPAIR. CENTER CARGO, DOOR EXISTING REPAIR EVALUATED AND FOUND THAT IT DOES NOT CONFORM TO SRM REPAIR IN CHAPTER 52. COMPLIED WITH EA 1-5230-127808, CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV 107. EO NR 1-5100-7-5001 A4 PT1.

Part: STRUCTURE — MISREPAIRED (CARGO DOOR) · airframe 58,259 hrs · 10,975 cycles

AFT CARGO DOOR INTERNAL STRUCTURE FOUND WITH EXISTING REPAIR. AFT CARGO, DOOR INTERNAL STRUCTURE EXISTING DOUBLER EVALUATED, FOUND NOT IN ACCORDANCE WITH SRM REPAIR. AFT CARGO, DOOR INTERNAL STRUCTURE REPAIR CARRIED OUT AS PER EA 1-5280-127811. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 107.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 58,259 hrs · 10,975 cycles

FUSELAGE, EXISTING REPAIR DOUBLER FOUND AT RT STA 860 TO STA 865 STRINGER 34R TO 35R. FUSELAGE, EXISTING REPAIR DOUBLER AT RT STA 860 TO STA 865 STRINGER 34R TO 35R. EVALUATED AND FOUND TO BE NOT IN ACCORDANCE WITH THE SRM. COMPLIED WITH EA 1-5310-127807. RT SIDE FUSELAGE SKIN EXISTING REPAIR AT STA 860, BETWEEN 34R AND 35R, REPAIR. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV 107. EO NR 1-5100-7-5001 A4 PT1.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 58,259 hrs · 10,975 cycles

FUSELAGE, EXISTING REPAIR DOUBLER AT RT STA 1781 STRINGER 49R TO 50R. FUSELAGE, EXISTING REPAIR DOUBLER AT RT STA 1781 STRINGER 49R TO 50R FOUND REPAIR DOES NOT CONFORM TO SRM. FUSELAGE STA 1781 STRINGER 49R TO 50R CARRIED OUT REPAIR AS PER MD-11 SRM 53-20-00 FIG 6 VOL I REV 40 EO 1-5100-7-5001 A4 PT 1 TITLE, STRUCTURES- REPAIR CATALOG MD-11. REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REV 107.

Part: FRAME — DENTED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

RT STA 1721 LONGERON 12 FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG I VOL. I REV. 40. REPETITIVE INSPECTION REQUIRED INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 58,259 hrs · 10,975 cycles

FUSELAGE, EXISTING REPAIR DOUBLER FOUND AT LT STA 730 TO STA 760 STRINGER 37L TO 39L. FUSELAGE, EXISTING REPAIR DOUBLER FOUND AT LT STA 730 TO STA 760 STRINGER 37L TO 39L. FOUND NOT IN ACCORDANCE TO SRM REPAIR. FUSELAGE LT STA 730 TO STA 760 STRINGER 37L TO 39L SKIN REPAIRED AS PER SRM 53-20- 00 FIG 2 VOL I REV 40. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REV 107.

Part: VANE — CORRODED (LT WING TE FLAP) · airframe 58,259 hrs · 10,975 cycles

LT WING OTBD FLAP VANE T-FITTING NR 1 FROM INBD TRACK ATTACH BORE FOUND CORRODED. COMPLIED WITH EA 1-5750-128666. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.

Part: TEE FITTING — CORRODED (LT WING TE FLAP) · airframe 58,259 hrs · 10,975 cycles

LT WING OTBD FLAP VANE TEE FITTING NR 4 FROM INBD TRACK ATTACH BORE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-128667. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, RT STA 5-43 TO STA 5-83 X= -8.5, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. 1 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1341 TO STA 1361 X= 75, SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1371 TO STA 1381 X= 75, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. 1 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: VERTICAL SUPPORT — CRACKED (ZONE 300) · airframe 58,259 hrs · 10,975 cycles

AFT FUSELAGE LOWER COMPARTMENT RT VERTICAL STIFFENER AT APPROX STA 2007 UPPER EDGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-00-01 FIG. 9 VOL. I REV. 40. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1491 TO STA 1501 X= 8.5, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, RT STA 1381 TO STA 1481 X= -8.5, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1331 X= 75 SEAT TRACK FOUND CORRODED. SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, RT STA 1305 X= -8.5 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (BS 1401) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1401 TO STA 1461, X= 8 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: BRACKET — DAMAGED (LT WING TE FLAP) · airframe 58,259 hrs · 10,975 cycles

LT WING OTBD FLAP OTBD FWD HINGE SIDE LINK BARREL NUT HOLE FOUND CORRODED. COMPLIED WITH EA 1-5750-127792. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1325 TO STA 1381, X= 8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1299 TO STA 1309, X= 75 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, RT STA 1401 TO STA 1426, X= -8 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, RT STA 1279 TO STA 1299, X= -8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: MOUNT — CORRODED (RT WING TE FLAP) · airframe 58,259 hrs · 10,975 cycles

RT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT INBD FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127785. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.

Part: DOUBLER — CRACKED (KEELBEAM) · airframe 58,259 hrs · 10,975 cycles

CENTER LANDING GEAR WHEEL WELL LT KEEL BEAM WEB FWD DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.

Part: DOUBLER — CRACKED (KEELBEAM) · airframe 58,259 hrs · 10,975 cycles

CENTER LANDING GEAR WHEEL WELL RT KEEL BEAM WEB FWD DOUBLER FOUND CRACKED. DOUBLER REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.

Part: MOUNT — CORRODED (RT WING TE FLAP) · airframe 58,259 hrs · 10,975 cycles

RT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT OTBD HOLE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127785. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 58,259 hrs · 10,975 cycles

CRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON THE LT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 55-20-00 FIG. 3 VOL. I REV. 40. CATEGORY 'B' REPAIR INITIAL INSPECTION TO BE CARRIED OUT AT 5400 CYCLES THERE AFTER REPETITIVE INSPECTION AT EVERY 2700 CYCLES. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 107.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 58,259 hrs · 10,975 cycles

CRACK INDICATION APPROXIMATELY 1 1/4 INCH LENGTH FOUND ON THE RT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAP. CARRIED OUT REPAIR AS PER SRM 55-20-00 FIG. 3 VOL. I REV. 40. CATEGORY 'B' REPAIR INITIAL INSPECTION TO BE CARRIED OUT AT 5400 CYCLES THERE AFTER REPETITIVE INSPECTION AT EVERY 2700 CYCLES. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN,LT STA 415 TO STA 475. X= 107 SEAT TRACK FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 695 TO STA 735, X= 8.5 SEAT TRACK FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 665 TO STA 745 X= 8.5 AS PER SRM 53-70-00 FIG. I VOL. I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1521 TO STA 1531 X=8 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1411 TO STA 1531 X= 8 AS PER SRM 53-70-00 FIG. I VOL. I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER REV. 107.

Part: FRAME — DENTED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, RT STA 1741 LONGERON 12 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: FRAME — DENTED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1701 LONGERON FRAME DOUBLER FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I REV. 40. REPETITIVE INSPECTION REQUIRED INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: FRAME — DENTED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, RT STA 1661 LONGERON 12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: FRAME — DENTED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CABIN, LT STA 1721 LONGERON 12 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT EVERY 9,500 CYCLES. TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SKIN — CRACKED (LT WING LE) · airframe 58,259 hrs · 10,975 cycles

LT WING LEADING EDGE LOWER PANEL NR 526GB CUT-OUT AT STA XOS=996 FOUND CRACKED. REPAIR CARRIED-OUT AT LT WING LEADING EDGE LOWER PANEL NR 526GB CUT-OUT AT STA XOS= 996 AS PER SRM 57-10-00 FIG. 41 VOL. I REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCHES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SEAL — CRACKED (LT WING TE) · airframe 58,259 hrs · 10,975 cycles

LT WING TRAILING EDGE PANEL NR 541GB CUT-OUT STRIP FOUND CRACKED. REMOVED AND REPLACED CRACKED SEAL AT LT WING TRAILING EDGE PANEL NR 541GB AS PER SRM 51-34-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.

Part: SKIN — CRACKED (LT WING LE) · airframe 58,259 hrs · 10,975 cycles

LT WING LEADING EDGE SKIN AT STA XOS=997 FOUND WITH CRACK APPROXIMATELY 10 INCHES LONG. REPAIR CARRIED OUT AS PER EA 1-5740-127781, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,259 hrs · 10,975 cycles

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

Part: WEB — CORRODED (ZONE 100) · airframe 53,136 hrs · 9,821 cycles

LEFT AIRCONDITIONING COMPARTMENT CENTER LOWER INBOARD WEB FOUND WITH CORROSION. 10-01-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-115193. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: TRUNNION — CORRODED (FUSELAGE) · airframe 53,136 hrs · 9,821 cycles

CENTER LANDING GEAR LEFT MOUNTING. TRUNNION FITTING FORWARD AND AFT HOLE FOUND WITH CORROSION. 10-01-07 COMPLIED WITH FEDEX E.A. 1-5310-115189. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (FUSELAGE) · airframe 53,136 hrs · 9,821 cycles

CENTER LANDING GEAR RIGHT MOUNTING. TRUNNION FITTING FORWARD AND AFT HOLE FOUND WITH CORROSION. 10-01-07 COMPLIED WITH FEDEX E.A. 1-5310-115190. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CRACKED (FUSELAGE) · airframe 53,136 hrs · 9,821 cycles

FASTENER HOLE FOUND CRACK AT 9 AND 3 O'CLOCK POSITION ON LONGERON AT RIGHT SIDE NOSE LANDING GEAR TRUNNION. 09-28-07 REPAIR CARRIED OUT AT FASTENER HOLE, 9 AND 3 O'CLOCK POSITION ON LONGERON AT RT NLG TRUNNION AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 53,136 hrs · 9,821 cycles

MAIN DECK - STA 1601, LONGERON 10R-11R FRAME FOUND DENTED. 09-26-07 REPAIR CARRIED OUT AS PER SRM 53-30- 00 FIG. 1 VOL.I. DAMAGE TOLERANCE INSPECTION REQUIREMENT REQUIRES INITIAL INSPECTION AT 14500 CYCLES FROM THE CURRENT 9821 CYCLES AND REPETITIVE INSPECTION AT 9500 CYCLES THEREAFTER. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 53,136 hrs · 9,821 cycles

LEFT NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 09-28-07 REPAIR CARRIED OUT AT LT HAND NOSE LANDING GEAR TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: TRUNNION — CRACKED (FUSLEAGE) · airframe 53,136 hrs · 9,821 cycles

RIGHT NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 09-28-07 REPAIR CARRIED OUT AT RT NLG TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 500) · airframe 53,136 hrs · 9,821 cycles

LEFT WING, LEADING EDGE TELESCOPING DUCT CUTOUT I/B AND O/B CORNERS FOUND CRACKS. 10-01-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115191. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: ACTUATOR — BROKEN (RT MLG) · airframe 51,185 hrs · 9,394 cycles

AFTER GEAR RETRACTION ON TAKEOFF (FROM ALA RWY 05) RECEIVED RED UNSAFE GEAR INDICATION ON RT MAINS INDICATED ON GEAR HANDLE INDICATORS AS WERE AS CONF SYNOPTIC. RAN RED TABS. RETURNED TO ALA AFTER DUMPING AP PXLY 100.000 LBS CONFIG SYNOPTIC SHOWED RIGHT GEAR TEMPS COLD VS ALL OTHERS. TEMPS WERE -2 SAME AS OAT. AT WALK AROUND, FOUND RIGHT MAIN LANDING GEAR UNLOCK ACTUATOR BROKEN. THE UNLOCK ACTUATOR FROM RIGHT MLG REMOVED PER MD-11 MM 32-33-02-4. INSTALLED NEW RT MLG UNLOCK ACTUATOR PER AMM 32-33-02-4. CHECK ACCOMPLISHED PER AMM OK. NO LEAKS. AIRCRAFT RETURNED TO SERVICE.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 48,201 hrs · 8,717 cycles

LT WING, AT STA XOS 647 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 647 LEADING EDGE CAVITY CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 48,201 hrs · 8,717 cycles

LT WING, AT STA XOS 670 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 670 LEADING EDGE CAVITY CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 48,201 hrs · 8,717 cycles

LT WING, AT STA XOS 762 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 762 LEADING EDGE CAVITY CRACKED BEADED DOUBLER. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 48,201 hrs · 8,717 cycles

LT WING, AT STA XOS 697 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 697 LEADING EDGE CAVITY CRACKED BEADED DOUBLER. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ACCESS DOOR — CRACKED (ZONE 100) · airframe 48,201 hrs · 8,717 cycles

FUSELAGE - AIRCON NR 2 COMPARTMENT ACCESS DOOR EXTERIOR CRACKED. CRACKED AIRCON NR 2 COMPARTMENT ACCESS DOOR EXTERIOR SKIN. REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. NEW SKIN FABRICATED AS PER DRAWING NR ACA3822. THE ACCESS DOOR REMOVED AND REINSTALLED AS PER AMM 52-42-01. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1531 TO 5-73 RBL 75. MAIN DECK COMPARTMENT, CORRODED SEAT TRACK AT STA 1531 TO STA 5-73 RBL 75. REMOVED AND REPLACED AT STA 1531 TO STA 5-123 RBL 75 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1341 - 1361 RBL 75. CORRODED SEAT TRACK ON MAIN DECK COMPARTMENT AT STA 1279 TO STA 1373 RBL 75. REMOVED AS PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 600) · airframe 48,201 hrs · 8,717 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD LOWER FASTENER HOLES COMMON TO INBOARD HINGE SUPPORT FITTING ARC4009 FOUND OUTBOARD LOWER HOLE REVEALED CRACK INDICATION. OUTBOARD LOWER HOLE AT RIGHT WING OUTBOARD FLAP OUTBOARD LOWER FASTENER HOLES COMMON TO INBOARD HINGE SUPPORT FITTING ARC 4009 ENLARGED AS PER SRM 51-31-01 VOLUME II. ORIGINAL HOLE DIAMETER =0.187", REWORKED HOLE DIAMETER =0.316". HFEC INSPECTION CARRIED OUT AS PER NDT SPM PART 06-10-01.001 ON THE OVERSIZED BOLT HOLE AND FOUND CRACK AT 3 O'CLOCK POSITION VIEW LOOKING AFT. REFER TO SNRM N01198 FOR RIGHT HAND WING OUTBOARD FLAP ASSEMBLY REPLACEMENT WORK DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 5-10 TO 5-93 LBL 08. MAIN DECK COMPARTMENT, CORRODED SEAT TRACK AT STA 5-10 TO STA 5-93 LBL 08. REMOVED AND REPLACED AT STA 5-10 TO STA 5-123 LBL 08 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1501 - 1531 RBL 08. MAIN DECK COMPARTMENT, CORRODED SEAT TRACK AT STA 1491 TO 1531 RBL 08. REMOVED AND REPLACED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

MAIN DECK COMPARTMENT RIGHT FUSELAGE FRAME FOUND WITH DENT AT STA 1681 LONGERON 12R. DENT MARK ON MAIN DECK COMPARTMENT RIGHT FUSELAGE FRAME AT STA 1681 LONGERON 12R EXISTING REPAIR DOUBLER REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. ACCOMPLISH AN INITIAL INSPECTION AT OR BEFORE REACHING 23,217 CYCLES (14,500 CYCLES FROM THE TIME THE REPAIR WAS INSTALLED) AND ACCOMPLISH A REPETITIVE INSPECTION EACH 9,500 CYCLES AFTER REACHING THE INITIAL INSPECTION THRESHOLD AS PER FEDEX EA NR1- 5330-95806, TITLE: FUSELAGE - FRAME - TRACKING SRM FRAME REPAIR AT STATION Y=1681 AT LONGERON 12 LEFT AND 12 RIGHT. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

MAIN DECK COMPARTMENT RIGHT FUSELAGE FRAME FOUND WITH DENT AT STA 1701 LONGERON 12R. DENT ON MAIN DECK COMPARTMENT RIGHT FUSELAGE FRAME AT STA 1701 LONGERON 12R REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. ACCOMPLISH AN INITIAL INSPECTION AT OR BEFORE REACHING 23,217 CYCLES AND ACCOMPLISH A REPETITIVE INSPECTION EACH 9,500 CYCLES AFTER REACHING THE INITIAL INSPECTION THRESHOLD AS PER FEDEX EA NR 1-5330-95807, TITLE: FUSELAGE FRAME TRACKING SRM FRAME REPAIR AT STATION Y=1701 AT LONGERON 12 RIGHT. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

FOUND MAIN DECK COMPARTMENT LT FUSELAGE FRAME FOUND WITH DENT AT STA 535 BETWEEN STRINGER 23-24L. MAIN DECK COMPARTMENT LT FUSELAGE DENTED FRAME AT STA 535 BETWEEN STRINGER 23-24L, REPAIR CARRIED OUT AS PER DWG SRZ-53-503. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6 -2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

FOUND MAIN DECK COMPARTMENT LT FUSELAGE FRAME FOUND WITH DENT AT STA 535 BETWEEN STRINGER 20-21L. MAIN DECK COMPARTMENT LT FUSELAGE DENTED FRAME AT STA 535 BETWEEN STRINGER 20-21L, REPAIR CARRIED OUT AS PER DWG SRZ-53-503. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6 -2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 48,201 hrs · 8,717 cycles

LT WING, AT STA XOS 624 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON LEFT WING STA XOS 624 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA NR 1-5730-95801, TITLE: WINGS, LEADING EDGE BEADED DOUBLER, PERMANENT REPAIR. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 48,201 hrs · 8,717 cycles

LT WING REAR SPAR UPPER END CAP STA XORS 1042 FOUND CORROSION. CORRODED AREA ON LEFT WING REAR SPAR UPPER END CAP STA XORS 1042 REPAIRED AS PER FEDEX EA NR 1-5710-95805, TITLE: WINGS, LEFT REAR SPAR UPPER CAP AFT TANG CORROSION CENTERED AT STATION XORS = 1042, REPAIR. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR — CORRODED (LT WING) · airframe 48,201 hrs · 8,717 cycles

LT WING, REAR SPAR AT STA XORS 590 - 593 UPPER CHORD UPPER SURFACE FOUND CORROSION. CORROSION AT LEFT WING REAR SPAR STA XORS 590-593 UPPER CHORD UPPER SURFACE REPAIRED AS PER FEDEX E.A. NR 1-5710-95800, TITLE: WINGS, LEFT HAND REAR SPAR UPPER CAP CORROSION AT STATIONS XORS = 590 THROUGH XORS = 593, REPAIR. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR — DAMAGED (ZONE 500) · airframe 48,201 hrs · 8,717 cycles

RIGHT WING, REAR SPAR AT STA XORS 564 UPPER CHORD FOUND ELONGATED HOLE. ELONGATED HOLE ON RIGHT WING REAR SPAR STA XORS 564 UPPER CHORD REPAIRED AS PER FEDEX EA NR 1-5710-95804, TITLE: WINGS, RIGHT WING AFT SPAR UPPER CAP AFT TANG AT STATION XORS = 564 (REAR SPAR CAP) ELONGATED FASTENER HOLE, REPAIR. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 600) · airframe 48,201 hrs · 8,717 cycles

RIGHT WING REAR SPAR UPPER END CAP BETWEEN STA XORS 949 TO XORS 981 FOUND CORROSION. CORROSION AT RIGHT WING REAR SPAR UPPER END CAP BETWEEN STA XORS 949 TO XORS 981 REMOVED AS PER SRM 51-21-01 VOLUME II. MINIMUM ORIGINAL THICKNESS =0.182" (0.197"-0.015"), THICKNESS REMOVED =0.023" AND REMAINING THICKNESS =0.159" FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 48,201 hrs · 8,717 cycles

LT WING AT STA XOS 632 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON LEFT WING STA XOS 632 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA NR1-5730-95801, TITLE: WINGS, LEADING EDGE BEADED DOUBLER PERMANENT REPAIR. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,201 hrs · 8,717 cycles

MAIN DECK COMPARTMENT LEFT FUSELAGE FRAME FOUND WITH DENT AT STA 1681 LONGERON 12L. DENTED FRAME ON MAIN DECK COMPARTMENT LEFT FUSELAGE AT STA 1681 LONGERON 12L REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. ACCOMPLISH AN INITIAL INSPECTION AT OR BEFORE REACHING 23,217 CYCLES (14,500 CYCLES FROM THE TIME THE REPAIR WAS INSTALLED) AND ACCOMPLISH A REPETITIVE INSPECTION EACH 9,500 CYCLES AFTER REACHING THE INITIAL INSPECTION THRESHOLD AS PER FEDEX EA NR 1-5330-95806, TITLE: FUSELAGE, FRAME TRACKING SRM FRAME REPAIR AT STATION Y=1681 AT LONGERON 12 LEFT AND 12 RIGHT. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,201 hrs · 8,717 cycles

SNRM N00604 : HFEC INSPECTION FOUND CRACK ON LT UPPER WING OB END OF STRINGER S-13L APPROX. 1 INCH LONG. REPAIRED AS PER SRM 57-20-00.

Part: SKIN — CRACKED (ZONE 600) · airframe 48,201 hrs · 8,717 cycles

SNRM N00719 : RT WING AT STA XOS 908 FIXED LEADING EDGE FOUND CRACKED. CRACK ON RIGHT HAND WING STA XOS 908 FIXED LEADING EDGE REPAIRED AS PER SRM 57-10-00 FIGURE 37 VOLUME I. NR 7 SLAT ASSEMBLY REMOVED AND INSTALLED AS PER AMM 27-80-30-4 AND RANGE OF MOVEMENT TEST CARRIED OUT AS PER AMM 27-80-00. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: REPAIR — CHAFED (ZONE 100) · airframe 48,201 hrs · 8,717 cycles

CENTER CARGO, DOOR CUTOUT FWD LOWER SECTION APPROX CARGO FLOOR LEVEL REPAIR DOUBLER FOUND CHAFED. CHAFED REPAIR DOUBLER ON CENTER CARGO DOOR CUTOUT FORWARD LOWER SECTION APPROX CARGO FLOOR LEVEL REPAIRED AS PER SRM 53-50-00 FIGURE 16 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (WS14L) · airframe 48,201 hrs · 8,717 cycles

SNRM N00606 : HFEC INSPECTION FOUND CRACK ON LT UPPER WING OB END OF STRINGER S-14L APPROX 13 INCHES LONG. REPAIRED AS PER SRM57-20-00.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 48,201 hrs · 8,717 cycles

RT WING AT STA XOS 550 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON RIGHT HAND WING STA XOS 550 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA 1-5730-95802, TITLE: WINGS - LEADING EDGE BEADED DOUBLER -PERMANENT REPAIR. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CHAFED (ZONE 100) · airframe 48,201 hrs · 8,717 cycles

SNRM N00623 : CENTER CARGO - DOOR CUTOUT AFT LOWER SECTION APPROX FLOOR LEVEL FOUND CHAFED. REPAIRED AS PER SRM 53-50-00.

Part: WARNING LIGHT — UNKNOWN (MLG) · airframe 47,591 hrs · 8,576 cycles

AFTER T/O WITH GEAR HANDLE UP, HAD BOTH PRIM AND SEC RT MAIN GEAR DSPL "RED" LIGHT (GEAR NOT UP). RAN QRH, AND 1ST ATTEMPT TO CYCLE GEAR SAME IND. AFTER 2ND ATTEMPT GEAR SHWD PRIM AND SEC "UP AND LOCK" IND. CONT TO DEST. PSEU FAULT RVW GOT FAULT CODE NR 9:R MLG DOWN AND LOCK PRIM, NR 13:R MLG UP AND LATCH PRIM, NR 17:R MLG DOWN AND LOCK SEC AND NR 21:R MLG UP AND LOCK SEC. T/S AS PER FIM 31-71-00 PSEU AND SENSORS PASS TEST. REF TO FIM 32-30-03 INSP R MLG DOOR LATCH, PROX SNSR GAP AND DOOR RETRACT CYL, MLG DOOR CYL AND SEL VALVE FOR LKGE ALL NORM NO DEFECT FOUND. R/I PSEU ASSY AS PER MM31-71-01-2 AND CARRIED OUT R MLG PROX SENSOR TEST AS PER MM 32-61-15-5 FOUND SATIS.

Part: NOSE COWL — VIBRATION (NR 1 ENGINE) · airframe 46,247 hrs · 8,257 cycles

ON TAKEOFF RWY 25L VHHH, AFTER POWER REDUCTION TO CLIMB AT 1500 AFL, GOT A YAW "BUMP" AND NOISE AND VIBRATION "BUZZ" IN AIRFRAME. NO ABNORMAL INDICATIONS INITIALLY, THEN NR 1 COMPRESSOR VIBRATION CLIMBED TO 5.0 AMBER, REDUCED NR 1 THROTTLE AND BUZZ DIMINISHED. NOISE QUIET AND INDICATION NORMAL AT IDLE, LEFT ENGINE RUNNING FOR SYSTEMS AVAILABILITY, DUMPED 147,000 POUNDS FUEL, LANDING VHHH.

Part: FIRE LOOP — SHORTED (NR 2 ENGINE) · airframe 39,625 hrs · 6,689 cycles

AT 1455Z, FL360,M.83.ENG NR 2 FIRE LIGHT CAME ON. INTERMITTENT AT FIRST IT BECAME STEADY AND ENG NR 2 WAS SHUTDOWN IAW CHECKLIST. NO OTHER ADVERSE INDICATIONS OBSERVED EXCEPT FIRE DETECT 2 FAIL LEVEL 1 ALERT. RTB WAS UNEVENTFUL, 1 FIRE BOTTLE WAS DISCHARGED. USING MEGGER FOUND UPPER LT B-LOOP AND LOWER TURBINE A-LOOP SHORTED TO GROUND. R AND I BOTH LOOP DETECTOR PER MM 26-11-03-4 FDCU NR 2 RTS TEST PASSED. R AND I ENG NR 2 SYS 1 FIRE BOTTLE AND TEST PER MM 26-21-01-4 TEST OK. RUN NR 2 ENG PER MD11 JRH ALL PARAMETERS AND INDICATIONS NML. PERFORMED NR 2 ENG DECAY CHK PER MD11 JRH TEST PASSED. OPEN AND CLOSED ENG COWLS AND PLATFORM PER MM 71-10-00.

Part: FIRE WARNING — MALFUNCTIONED (CARGO BAY) · airframe 39,545 hrs · 6,667 cycles

LOWER AFT CARGO FIRE MASTER WARNING AND ALERT CAME ON DURING CRUISE AT FLT 390 DIVERTED IN DEN MEL 12AUG03 DEN ACN RELEASED FOR SERVICE PER MEL CDL 3A 26-22-01- 02 CATEGORY 3A B EXPIRATION 3A 15AUG03 AFTER DOWN LOAD 2 C INSPECTED AREA FOR SMOKE AND 2 FOR FIRE FOUND NONE. NO FREIGHT ON 2F 2C EMPTY CANS UP LOADED. DEFERRED PER MEL 26-22-01-02. PER FAULT ISOLATION MANUAL 26-14-00 2C. PERFORMED RTS OF AMSC 2C, NO FAULTS NOTED. PERFORMED LIGHTS AND MANUAL TEST FUNCTION PER 26-14-03-00 2CSTEP 2. SYSTEM OK. AFTER MAINTENANCE PERFORMED 2C RED FIRE BOTTLE 231 PER MM CHP 26-22-01-4 PERFORMED TESTS PER MM CHP 26-22-01-5. SYSTEM CKS OK USED TESTER DZZ7703-501B 2FN 4831 MEL ISC 2FW 2FC IS OK FOR FLT.

Part: SWITCH — INTERMITTENT (CARGO DOOR) · airframe 39,353 hrs · 6,613 cycles

AT APPROX 500 FEET CARGO DOOR AFT -A- LEVEL TWO ILLUMINATED. DUMPED TO MAX LANDING WEIGHT. COMPLIED WITH QRH AND RETURNED TO SFS. NOTE: DOOR OPEN LIGHT ALSO ILLUMINATED. ENT BY: 317084 RPT BY: 096537 FACT 18JUL03 22:14 SFS R REMOVED AND REPLACED S1 -383 DOOR CLOSE SWITCH DUE FOUND INTERMITTENT OPERATION, AND S1-261 DOOR LOCK SWITCH FOR PRECAUTIONARY PER MD11 AMM 52-33-04. PERFORMED CARGO DOOR CHECK, OPENING AND CLOSING NORMAL. ENT BY: 363743 RPT BY: 363743.

Part: NUT — CORRODED (ZONE 300) · airframe 39,341 hrs · 6,607 cycles

HORIZONTAL STABILIZER, LT UPPER AFT PLANK BARREL NUT BORE NR 34L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LT HOR STAB UPPER AFT PLANK BARREL NUT NR 34L BORE REPAIR CARRIED OUT IAW EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · airframe 39,341 hrs · 6,607 cycles

HORIZONTAL STAB LEFT UPPER FWD PLANK BARREL NUT BORE NR 1L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. HORIZONTAL STAB LEFT UPPER FWD PLANK BARREL NUT BORE NR 1L REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · airframe 39,341 hrs · 6,607 cycles

HORIZONTAL STAB RIGHT UPPER AFT SPAR CAP BARREL NUT BORE NR 36R FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. RIGHT HORIZONTAL STAB UPPER AFT SPAR CAP BARREL NUT BORE NR 36R REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · airframe 39,341 hrs · 6,607 cycles

HORIZONTAL STAB LEFT UPPER CENTER PLANK BARREL NUT BORE NR 21L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LEFT HORIZONTAL STAB UPPER CENTER PLANK BARREL NUT NR 21L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · airframe 39,341 hrs · 6,607 cycles

HORIZONTAL STAB LEFT UPPER AFT PLANK BARREL NUT BORE NR 31L FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LEFT HORIZONTAL STAB UPPER AFT PLANK BARREL NUT NR 31L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: STRUCTURE — CHAFED (LT WING TE FLAP) · airframe 39,341 hrs · 6,607 cycles

LT WING, I/B FLAP CTR (FLAP VANE TRACK) CUTOUT FOUND CHAFED. LT WING, I/B FLAP CTR (FLAP VANE TRACK) CUTOUT, DAMAGED RIB REMOVED AS PER SRM 51-31-01 VOL II, ON SKIN EDGES CHAFE MARKS SMOOTHED OUT AND FOUND WITHIN LIMIT AS PER SRM 57-00-01 VOL I FIG 1A, NEW RIB FABRICATED AS PER DRAWING ARC 2951, RIB INSTALLED AS SRM 51-31-01 VOL II.

Part: VANE — CORRODED (ZONE 500) · airframe 39,341 hrs · 6,607 cycles

LT WING- O/B FLAP VANE NR 4 FITTING FORWARD HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-69380 - WINGS - TRAILING EDGE FLAPS - LEFT HAND OUTBOARD FLAP - VANE SUPPORTS - CORROSION REPAIR AND REFURBISHMENT.

Part: FITTING — CORRODED (O/B FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING- O/B FLAP VANE NR 4 FITTING FWD HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-69380 - WINGS - TRAILING EDGE FLAPS - LEFT HAND OUTBOARD FLAP - VANE SUPPORTS - CORROSION REPAIR AND REFURBISHMENT.

Part: VANE — CORRODED (TE FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING- O/B FLAP VANE MOST I/B FITTING FWD HOLE FOUND CORROSION. LEFT WING- O/B FLAP VANE MOST I/B FITTING FWD HOLE REWORK AS PER DWG ARC 7053. BUSHING FABRICATED AS PER FEDEX EA 1-5750-69380, WINGS- TRAILING EDGE FLAPS- LEFT HAND OUTBOARD FLAP- VANE SUPPORTS- CORROSION REPAIR AND REFURBISHMENT.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 39,341 hrs · 6,607 cycles

LEFT HORIZONTAL STAB UPPER AFT PLANK 28L BORE FOUND CORROSION BEYOND EO 1- 5510-7-5000 LIMITATIONS. LEFT HORIZONTAL STAB UPPER AFT PLANK NR 28L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 39,341 hrs · 6,607 cycles

LEFT HORIZONTAL STAB UPPER CENTER PLANK 24L BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 39,341 hrs · 6,607 cycles

LEFT HORIZONTAL STAB UPPER CENTER PLANK 20L BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. LEFT HORIZONTAL STAB UPPER CENTER PLANK 20L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: SKIN — CORRODED (ZONE 300) · airframe 39,341 hrs · 6,607 cycles

SNRM N0897 - LT HOR STAB UPPER FWD PLANK NR 8L BORE FOUND CORROSION BEYOND EO 1- 5510-7-5000 LIMITATIONS. CORRECTIVE ACTION: SNRM N0897 - LT HOR STAB UPPER FWD PLANK NR 8L BORE REPAIR CARRIED OUT IAW EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 39,341 hrs · 6,607 cycles

LEFT HORIZONTAL STAB UPPER AFT PLANK 30L BORE FOUND CORROSION BEYOND EO 1- 5510-7-5000 LIMITATIONS.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 39,341 hrs · 6,607 cycles

LEFT HORIZONTAL STAB UPPER CENTER PLANK 16L BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. LEFT HORIZONTAL STAB UPPER CENTER PLANK 16L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: SPAR CAP — CORRODED (ZONE 300) · airframe 39,341 hrs · 6,607 cycles

SNRM N0824 - HOR STAB LT UPPER SPAR CAP NR 36L BARREL NUT BORE CORROSION FOUND BEYOND EO 1-5510-7-5000 B PT1 LIMITATION. CORRECTIVE ACTION: SNRM N0824 - HOR STAB LH UPPER SPAR CAP NR 36L BARREL NUT BORE REPAIR CARRIED OUT EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT REWORK/REPAIR- 1-5510-7-5000.

Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · airframe 39,341 hrs · 6,607 cycles

HORIZONTAL STAB LT UPPER SPAR CAP 36L BARREL NUT BORE CORROSION FOUND BEYOND EO 1-5510-7-5000 B PT1 LIMITATION. HORIZONTAL STAB LT UPPER SPAR CAP 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR- 1-5510-7-5000.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 39,341 hrs · 6,607 cycles

HORIZONTAL STAB UPPER FWD PLANK 14L BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 B PT1 LIMITATIONS. HORIZONTAL STAB UPPER FWD PLANK 14L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT REWORK /REPAIR 1-5510-7-5000.

Part: HINGE — CORRODED (TE FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE FOUND CORROSION. LEFT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE REPAIRED AS PER FEDEX EA 1-5750-69372, TITLE: WINGS- TRAILING EDGE FLAP SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE FOUND CORROSION. RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE REPAIRED AS PER FEDEX EA1-5750-69375, RIGHT HAND OUTBOARD FLAP - INBOARD SUPPORT BRACKET - CORROSION REMOVAL AND REPAIR.

Part: HINGE — LOOSE (ZONE 500) · airframe 39,341 hrs · 6,607 cycles

LT-O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT POINT BUSHING FOUND LOOSE. CORRECTIVE ACTION: SNRM N0712 - LHW- O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT POINT BUSHING REPLACED AS PER FEDEX EA 1-5750-69372, TITLE: WINGS- TRAILING EDGE FLAP SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR.

Part: HINGE — LOOSE (ZONE 600) · airframe 39,341 hrs · 6,607 cycles

RT- O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT POINT BUSHING FOUND LOOSE. RT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT POINT BUSHING REPLACED IAW EA 1-5750-69375, TITLE: WINGS- TRAILING EDGE FLAP- RT OUTBOARD FLAP- INBOARD SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,341 hrs · 6,607 cycles

LT WING O/B FLAP O/B HINGE O/B LOWER BORE FOUND CORROSION. LT WING O/B FLAP O/B HINGE O/B LOWER BORE REPAIRED AS PER FEDEX EA 1-5750- 69373, OUTBOARD TRAILING EDGE FLAP - SUPPORT BRACKETS - CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING O/B FLAP O/B HINGE I/B LOWER BORE FOUND CORROSION. LT WING O/B FLAP O/B HINGE I/B LOWER BORE REPAIRED AS PER FEDEX EA 1-5750- 69373 OUTBOARD TRAILING EDGE FLAP - SUPPORT BRACKETS - CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING- O/B FLAP I/B HINGE O/B LOWER STUD (NUT SIDE) FOUND SURFACE CORROSION. RIGHT WING- O/B FLAP I/B HINGE AFT SURFACE OF O/B LOWER STUD (NUT SIDE) AREA REPAIRED AS PER FEDEX EA 1-5750-69386, TITLE: WINGS- TRAILING EDGE FLAPS- OUTBOARD TRAILING EDGE FLAPS- INBOARD FLAP SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: STOP FITTING — CRACKED (T/E FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING O/B FLAP STOP FITTING (NR 2 FLAP VANE TRACK) FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-67554 PT 1 - WINGS OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR.

Part: FITTING — CRACKED (ZONE 600) · airframe 39,341 hrs · 6,607 cycles

RT WING O/B FLAP STOP FITTING (NR 2 FLAP VANE TRACK) FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-67554 PT 1 - WINGS OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR

Part: HINGE — CORRODED (TE FLAP) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING- O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT BORE FOUND CORROSION. RIGHT WING- O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT BORE REPAIRED AS PER FEDEX EA 1-5750-69372, TITLE: WINGS- TRAILING EDGE FLAP SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR.

Part: ACTUATOR — CORRODED (ZONE 600) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING - O/B FLAP O/B HINGE O/B ACTUATOR BORE FOUND CORROSION. - RIGHT WING - O/B FLAP O/B HINGE O/B ACTUATOR BORE REPAIRED AS PER FEDEX EA 1-5750-69373.

Part: HINGE — CORRODED (TE FLAP) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING- O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT BORE FOUND CORROSION. RIGHT WING- O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT BORE REPAIRED AS PER FEDEX EA 1-5750-69372 TITLE: WINGS- TRAILING EDGE FLAP SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR.

Part: ACTUATOR — CORRODED (TE FLAPS) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING- O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR I/B BORE FOUND CORROSION. RIGHT WING- O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR I/B BORE REPAIRED AS PER FEDEX EA 1-5750-69375, TITLE: WINGS- TRAILING EDGE FLAP- RIGHT HAND OUTBOARD FLAP- INBOARD SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR.

Part: STUD — CORRODED (T/E FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING - O/B FLAP I/B HINGE UPPER I/B STUD FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-69379 - WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAPS - INBOARD FLAP SUPPORT, UPPER INBOARD STUD BOLT - REPAIR AND INTERIM USE.

Part: HINGE — CORRODED (TE FLAP) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING- I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE FOUND CORROSION. RIGHT WING- I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE REPAIRED AS PER FEDEX EA 1-5750-69374, TITLE: WINGS- TRAILING EDGE FLAP- INBOARD TRAILING EDGE FLAP- OUTBOARD SUPPORT BRACKET- CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING- O/B FLAP O/B HINGE I/B ACTUATOR BORE FOUND CORROSION. SNRM N0588 - RIGHT WING- O/B FLAP O/B HINGE I/B ACTUATOR BORE REPAIRED AS PER FEDEX EA 1-5750-69373, TITLE: WINGS- TRAILING EDGE FLAP- OUTBOARD TRAILING EDGE FLAP- SUPPORT BRACKETS- CORROSION REMOVAL AND REPAIR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,341 hrs · 6,607 cycles

AFT CARGO COMPT STRINGER SPLICE BRACKET AT STA 1951 STRINGER 51LT FOUND CRACKED. AFT CARGO COMPARTMENT STA 1951 STRINGER 51LT CRACKED CLIP REMOVED AND NEW CLIP FABRICATED PER DRAWING AGA 3092, SRM 51-35-01 VOL II, SRM 51-33-01 VOL II AND REFER TO FEDEX EA 1-5310-71724, FUSELAGE- MAINFRAME- TRACKING OF B TYPE REPAIR ON FRAME.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,341 hrs · 6,607 cycles

LT WING, O/B FLAP I/B HINGE LOWER O/B STUD BORE AFT SURFACE FOUND CORROSION. AFT SURFACE OF O/B STUD BORE REPAIRED AS PER CMM 57-44-08, WITHIN ALLOWABLE LIMIT AS PER CMM 57-44-08 AT LHW O/B FLAP I/B HINGE.

Part: HINGE — CORRODED (TE FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING- O/B FLAP I/B HINGE LOWER O/B STUD BORE AFT SURFACE FOUND CORROSION. AFT SURFACE OF O/B STUD BORE REPAIRED AS PER CMM 57-44-08. WITHIN ALLOWABLE LIMIT AS PER CMM 57-44-08 AT LEFT WING O/B FLAP I/B HINGE.

Part: HINGE — CORRODED (TE FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING O/B FLAP O/B HINGE ACTUATOR O/B BORE FOUND CORROSION. LEFT WING O/B FLAP O/B HINGE O/B ACTUATOR BORE REPAIRED AS PER FEDEX EA 1-5740-71722, TITLE: WINGS- LEFT O/B FLAP- O/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 39,341 hrs · 6,607 cycles

SNRM N0516 - MAIN DECK CABIN: STA Y635, X0 FOUND SEAT TRACK CRACKED. SNRM N0516 - DAMAGED SEAT TRACK AT STA Y635; X0 SPLICED AND REPAIRED BETWEEN STA Y625 AND STA Y665 PER SRM 53-70-00 VOL I.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,341 hrs · 6,607 cycles

LT W O/B FLAP O/B HINGE ACTUATOR I/B BORE FOUND CORROSION. WORK CARRIED OUT IAW EA 1-5740-71722, WINGS- LEFT O/B FLAP- O/B HINGE BRACKET ASSEMBLY FOR ACTUATOR INSTALLATION CORRODED.

Part: HINGE — CORRODED (TE FLAP) · airframe 39,341 hrs · 6,607 cycles

LEFT WING- O/B FLAP I/B HINGE ACTUATOR I/B BORE FOUND CORROSION. LEFT WING- TRAILING EDGE FLAP- OUTBOARD TRAILING EDGE FLAP- SUPPORT BRACKETS- CORROSION REMOVAL AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69373.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 39,341 hrs · 6,607 cycles

HORIZONTAL STAB UPPER CENTER PLANK 26L BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 B PT1 LIMITATIONS. HORIZONTAL STAB CENTER PLANK 26L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/REPAIR- 1-5510-7-5000.

Part: RIB — CRACKED (ZONE 500) · airframe 39,341 hrs · 6,607 cycles

SNRM N0065 - LT WING L/E NR 16 SLAT TRACK I/B RIB FOUND CRACKED. LT WING L/E NR 16 SLAT TRACK I/B CRACKED RIB REMOVED AND NEW RIB INSTALLED IAW SRM 51-31-01 VOL.II.

Part: RIB — CRACKED (ZONE 600) · airframe 39,341 hrs · 6,607 cycles

RIGHT WING L/E NR 16 SLAT TRACK I/B RIB FOUND CRACKED. SNRM N0066 - NEW RIB FABRICATED AS PER DRAWING NR ARB2850. CRACKED RIB ON RIGHT WING L/E NR 16 SLAT TRACK I/B AREA REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.

Part: O-RING — BROKEN (MANIFOLD FILTER) · airframe 30,190 hrs · 4,482 cycles

NR 3 HYD FLUID SYS LEAK. REMOVED AND REPLACED NR 3 HYD MANIFOLD FILTER AND O-RING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,176 hrs · 4,475 cycles

DURING D-CK, 2 INCH CRACK FOUND ON WEB OF RT UPPER FRAME AT Y=1305 WHICH IS AFT OF NR 3 OVERWING DOOR CUTOUT. REMOVED AND REPLACED PER IAW FEDEX EA 1-5310-51454.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,176 hrs · 4,475 cycles

DURING D-CK, A 2 INCH CRACK FOUND INNER FLANGE OF RT UPPER FRAME AT Y=1256 WHICH IS AFT OF NR 3 OVERWING DOOR CUTOUT. REMOVED DAMAGE THEN PERF HFEC TO ENSURE CONTAINMENT. APPLY RESTORATIVE STRENGTH STRAP TO INNER CHORD PER IAW FEDEX EA 1-5310-51452.