N606FE

Part: TRANSDUCER — FAILED (ZONE 100) · airframe 88,832 hrs · 21,681 cycles

RECEIVED TIRE FAIL ANNUNCIATION ON TAKEOFF ROLL. COMPLIED WITH QRH. ***EMERGENCY DECLARED*** REMOVED AND REPLACED MAIN WHEEL #5 TIRE PRESSURE TRANSMISSION AMM 32-46-08-4 AND AIR PRESSURE TRANSDUCER AMM32-46-03-4 OPERATIONAL CHECK OK. REQUIRES CATIIIB RTS

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-T0322665 G PART 2 STEP 3A AND STEP 3B, TITLE: WING- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500573 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-07 AND E.A.# 1-5750-T0322664 E PART 2 STEP 3A AND STEP 3B, TITLE: WING- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500562 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-T0322664 E PART 2 STEP 3A AND STEP 3B, TITLE: WING- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500562 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-07 AND E.A.# 1-5750-T0322665 G PART 2 STEP 3A AND STEP 3B, TITLE: WING- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500573 FOR DETAILS)

Part: SKIN — CRACKED (N/A) · airframe 87,764 hrs · 21,424 cycles

RIGHT HAND WING # 11 SLAT TRACK LOWER CUTOUT FOUND CRACKED AT INBOARD SIDE XORS 623 AREA. RIGHT HAND WING # 11 SLAT TRACK LOWER CUTOUT AT INBOARD SIDE XORS 623 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (N/A) · airframe 87,764 hrs · 21,424 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NO. SN10550000 REVISION C ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM 2 ND FASTENER FROM BELOW TO LOWEST FASTENER AND UNABLE TO PROCEED FURTHER INSPECTION DUE TO WEB BLOCKAGE. RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE UPPER REAR SPAR CAP STATION 2164 EXISTING CRACK REPAIRED AS PER EA #1 Ï¿½ 5530 Ï¿½ T0366175 PART 1 TITLE: STABILIZERS Ï¿½ VERTICAL STABILIZER Ï¿½ CRACK REPAIRS ON VERTICAL STABILIZER REAR SPAR LHS & RHS FORWARD FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1841) · airframe 87,764 hrs · 21,424 cycles

LOWER CENTER CARGO COMPARTMENT FLOOR PANEL SUPPORT FOUND CORROSION AT STATION = 1841 X= 45. LOWER CENTER CARGO COMPARTMENT FLOOR SUPPORT AT STATION 1841 X=45 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORRODED SUPPORT REMOVED AND REPLACED WITH FABRICATED SUPPORT AS PER SRM 51- 31-01-0G. SUPPORT REWORKED AS PER DRAWING AGA 7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: PANEL — DELAMINATED (N/A) · airframe 87,764 hrs · 21,424 cycles

CABIN Ï¿½ FLOOR PANEL #232DF AT STATION 495 TO STATION 505 FOUND DELAM. DELAM FLOOR PANEL #232DF AT CABIN STATION 495 TO STATION 505 REMOVED AS PER AMM 53- 21-04-4. FLOOR PANEL #232DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #232DF INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: PANEL — DELAMINATED (N/A) · airframe 87,764 hrs · 21,424 cycles

CABIN Ï¿½ FLOOR PANEL #271GF AT STATION 1437 FOUND DELAM. DELAM FLOOR PANEL #271GF AT CABIN STATION 1437 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL #271GF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #271GF INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1841) · airframe 87,764 hrs · 21,424 cycles

UPON REMOVAL OF AFT FLOOR PANEL SUPPORT AT STATION 1841 FOR REPAIR, LOWER CENTER CARGO COMPARTMENT FLOOR BULKHEAD WEB AT STATION 1841 X=-32 FOUND CORROSION. LOWER CENTER CARGO COMPARTMENT FLOOR BULKHEAD AT STATION 1841 X=-32 WEB CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORRODED WEB REMOVED AND REPLACED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED AS PER DOUGLAS DRAWING AGA 7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: PANEL — DELAMINATED (N/A) · airframe 87,764 hrs · 21,424 cycles

CABIN Ï¿½ FLOOR PANEL 271EF AT STATION 1361 TO STATION 1421 FOUND DELAM. DELAM FLOOR PANEL 271EF AT CABIN STATION 1361 TO STATION 1421 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL 271EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL 271EF INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (N/A) · airframe 87,764 hrs · 21,424 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550012 PER DRAWING NO. SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM 2 ND FASTENER FROM BELOW TO LOWEST FASTENER AND UNABLE TO PROCEED FURTHER INSPECTION DUE TO WEB BLOCKAGE. LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE UPPER REAR SPAR CAP STATION 2164 EXISTING CRACK REPAIRED AS PER EA #1 Ï¿½ 5530 Ï¿½ T0366175 PART 1 TITLE: STABILIZERS Ï¿½ VERTICAL STABILIZER Ï¿½ CRACK REPAIRS ON VERTICAL STABILIZER REAR SPAR LHS & RHS FORWARD FLANGES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (N/A) · airframe 87,764 hrs · 21,424 cycles

LOWER CENTER CARGO COMPARTMENT FLOOR BULKHEAD WEB AT STATION 1841 X= 12 FOUND CRACKED. LOWER CENTER CARGO COMPARTMENT FLOOR BULKHEAD CRACKED WEB AT STATION 1841 X=0 TO X=60 REMOVED AND REPLACED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED AS PER DOUGLAS DRAWING AGA 7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 52-03 AND E.A.# 1-5750-157194 G PART 3 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD AFT HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500594 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND E.A.# 1-5750-157194 G PART 3 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD AFT HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500594 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-T0322665 G PART 2 STEP 3A AND STEP 3B, TITLE: WING- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500573 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND E.A.# 1-5750-157181 G PART 3 STEP 3 AND STEP 4, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500593 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1- 5750-T0322664 E PART 2 STEP 3A AND STEP 3B, TITLE: WING- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500562 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 87,764 hrs · 21,424 cycles

RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 52-03 AND E.A.# 1-5750-157181 G PART 3 STEP 3 AND STEP 4, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500593 FOR DETAILS)

Part: SKIN — CRACKED (ZONE 500) · airframe 87,764 hrs · 21,424 cycles

LEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 FOUND CRACK BETWEEN TRACK # 17 AND # 18. LEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 CRACKED BETWEEN TRACK # 17 AND # 18 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 3 AND EA 1-5750-T0366213 P1 TITLE : WINGS - FLIGHT SURFACES - LH WING - # 8 SLAT ASSY - INNER SKIN SRM SPLICE REPAIR BETWEEN STA XOS 1089 AND STA 1100 - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,764 hrs · 21,424 cycles

LEFT HAND WING, FOUND BEADED DOUBLER CRACKED AT STATION XOS = 662. LEFT HAND WING STATION XOS = 662 CRACKED BEADED DOUBLER REPAIRED AND REPAIR PARTS INSTALLED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT INNER BETWEEN XOS 661 AND XOS 667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,764 hrs · 21,424 cycles

LEFT HAND WING, FOUND BEADED DOUBLER CRACKED AT STATION XOS = 615. LEFT HAND WING STATION XOS = 615 CRACKED BEADED DOUBLER REPAIRED AND REPAIR PARTS INSTALLED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT INNER BETWEEN XOS 610 AND XOS 616. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,764 hrs · 21,424 cycles

LEFT HAND WING, FOUND BEADED DOUBLER CRACKED AT STATION XOS = 755. LEFT HAND WING STATION XOS = 755 CRACKED BEADED DOUBLER REPAIRED AND REPAIR PARTS INSTALLED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT INNER BETWEEN XOS 754 AND XOS 759. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 595-601 RBL47) · corrosion level 2 · airframe 87,764 hrs · 21,424 cycles

CABIN - FLOOR SEAT TRACK AT STATION 595 TO STATION 601 X = - 47.5 FOUND CORROSION. CABIN - FLOOR SEAT TRACK AT STATION 595 TO STATION 601 , X = - 47.5 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 565 TO EXISTING SPLIE STATION 645 , X = - 47.5 AS PER SRM 53- 00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 595-655) · airframe 87,764 hrs · 21,424 cycles

CABIN FLOOR SEAT TRACK AT STATION 595 TO STATION 655 X = - 75.25 FOUND CORROSION. CABIN FLOOR AT SEAT TRACK STATION 595 TO STATION 655 , X = - 75.25 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 585 TO STATION 685 , X = - 75.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (N/A) · airframe 87,764 hrs · 21,424 cycles

LEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 FOUND CRACK BETWEEN TRACK # 17 AND # 18. LEFT HAND WING # 8 SLAT LOWER SURFACE ( COVE PANEL ) ZONE 624 STATION XOS 1097 CRACKED BETWEEN TRACK # 17 AND # 18 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 3 AND EA 1-5750-T0366213 P1 TITLE : WINGS - FLIGHT SURFACES - LH WING - # 8 SLAT ASSY - INNER SKIN SRM SPLICE REPAIR BETWEEN STA XOS 1089 AND STA 1100 - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAL — DAMAGED (BLEED AIR SYS) · airframe 83,253 hrs · 20,249 cycles

ON CLIMB OUT OF KIND R'CVD LEVEL ONE ALERT"AIR SYS 1 OFF". FOLLOWED QRH PROCEDURES. INSTALLED NEW SEAL ON I/B SIDE OF ARROW COUPLING REPOSITIONED COUPLING LEAK CHECKED GOOD, REF AMM 36-14-05-2. ACCOMPLISHED PNEU SYS #1 DECAY CHECK REF AMM 36-00-04-5 DECAY FOUND TO WITHIN LIMITS.OK TO CONTINUE.

Part: WIRE — PULLED (TAT HEAT) · airframe 83,253 hrs · 20,249 cycles

SHORTLY AFTER T.O KIND RCVD LEVEL 1 ALERT "TAT PROB HEAT" FOLLWED QRH PROCEDURES AND DISCOVERED THE ASSOCIATED CIRCUIT BREAKER "POPPED". FOUND RED WIRE B608-3-20 PULLED OUT OF CONTACT #3 ON CONNECTOR P1-1032. REPLACED CONNECTOR SOCKET PER SMP. TAT PROBE HEAT TESTS GOOD PER AMM 30-30-00-5.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 82,797 hrs · 20,139 cycles

AFTER LANDING ROLLOUT RCVD LVL2 ALERT "HYD 2 FAIL" OBSERVED HYD QTY DRAIN TO ZERO. CONSULTED QRH. SHUT DOWN NO. 2 ENGINE. REPLACED DAMAGED PART OF #2 HYDRO SYSTEM RESERVOIR PRESSURE LINE IN AFT COMPT REF MD 11 AMM 20-10-01-2 NO LEAKS NOTED

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM57-44-08 AND FOUND EXCEED LIMIT BASE THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAXIMUM REWORK LIMIT FOR BARREL NUT HOLE. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# : 1- 5750-157177 A PART 2 STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# : 1-5750-T0350808 PART 1 STEP 1 A, TITLE: WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- #2 TO #4 TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-4. LEFT HAND WING OUTBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27- 50-32-5 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# : 1-5750-T0350808 PART 1 STEP 1 A, TITLE: WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- #2 TO #4 TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-4. LEFT HAND WING OUTBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27- 50-32-5 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# : 1-5750-T0350808 PART 1 STEP 1 A, TITLE: WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- #2 TO #4 TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-4. LEFT HAND WING OUTBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27- 50-32-5 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT RIGHT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# : 1-5750-T0350776 PART 1 STEP 1 A, TITLE: WINGS- FLIGHT SURFACES- RH WING- OUTBD FLAP VANE ASSY- #1 TRACK SUPPORT FITTING SLOT HOLE CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-4. RIGHT HAND WING OUTBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27- 50-32-5 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM57-52-04. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-04 AND EA 1-5750-T0350626 PART 1 STEP 1 A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP INBD HINGE (FLAP SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT XORS 254. LEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER STATION XORS 254 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101. REPAIR CARRIED OUT AS PER EA 1-5730-T0350595 PART 1 TITLE: WINGS - PLATES AND SKINS -LT WING-CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER AT INNER REAR SPAR AREA . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM57-52-04. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-04 AND EA 1-5750-T0350624 PART 1 STEP 1 A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- LT WING- OUTBD FLAP INBD HINGE (FLAP SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1441 X= 8.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1441 X= 8.5 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERIAL REMOVED: 0.031 MATERIAL REMAINING: 0.049. SEAT TRACK REPAIR CARRIED OUT AT STATION 1411 TO STATION 1491 X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT 755 X=-47.5 FOUND CROWN DAMAGED. DAMAGED AREA EVALUATED AND FOUND EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1571 TO STATION 1621 X=-107.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1571 TO STATION 1621 X= -107.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080Ï¿½ MATERIAL REMOVED: 0.036 MATERIAL REMAINING: 0.044. SEAT TRACK REPAIR CARRIED OUT AT STATION 1571 TO STATION 1631 X=-107.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1475 X= 75.25 FOUND FLANGE CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1475 X= 75.25 FLANGE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERIAL REMOVED: 0.035 MATERIAL REMAINING: 0.045. SEAT TRACK REPAIR CARRIED OUT AT STATION 1451 TO STATION 5-0 X= 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1190 X=-75.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1190 X= -75.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERIAL REMOVED: 0.046 MATERIAL REMAINING: 0.034. SEAT TRACK REPAIR CARRIED OUT AT STATION 1169 - STATION 1267 X=-75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1256 X=-75.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1256 X= -75.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERIAL REMOVED: 0.032 MATERIAL REMAINING: 0.048. SEAT TRACK REPAIR CARRIED OUT AT STATION 1169 - STATION 1267 X=-75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIEDAS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 755 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT BS 755 X= 47.5, DAMAGED AREA EVALUATED AND FOUND EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (RT WING) · airframe 82,266 hrs · 19,966 cycles

RIGHT WING TRAILING EDGE INBOARD ISLAND FORWARD EDGE UPPER SKIN LOWER SURFACE FINGER DOUBLER AT XW 392 FOUND DETACHED. REPAIR CARRIED OUT AT RIGHT WING TRAILING EDGE INBOARD ISLAND FORWARD EDGE UPPER SKIN LOWER SURFACE AT XW 392 IAW SRM 57-50-01-2R, FIGURE 203, REPAIR 6. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 475) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 475 X=-27.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 475 X= -27.5 FOUND EXFOLIATION CORROSION EXCEED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATION 475 TO STATION 525 X=-27.5 AS PER MD11 SRM 53- 00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 755 X=-27.5 FOUND CROWN DAMAGED. AREA EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,266 hrs · 19,966 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K.INSTALLED FABRICATED DOUBLER AT RIGHT WING FIXED LEADING EDGE AT XOS 667 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 82,266 hrs · 19,966 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE FORMER AT XOS 584 FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB2931 REVISION H. INSTALLED FEBRICATED FORMER AT LEFT WING FIXED LEADING EDGE AT XOS 584 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# : 1-5750-T0350674 PART 1 STEP 1 B AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,266 hrs · 19,966 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FEBRICATED DOUBLER AT LEFT WING FIXED LEADING EDGE AT XOS 906 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT STATION 1282 X= 47.5, CROWN DAMAGED AREA EVALUATED AND FOUND EXCEED LIMIT AS PER MD-11, SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATION 1265 Ï¿½ STATION 1313 X= 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,266 hrs · 19,966 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FEBRICATED DOUBLER AT LEFT WING FIXED LEADING EDGE AT XOS 789 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT WING) · airframe 82,266 hrs · 19,966 cycles

LEFT WING Ï¿½ TRAILING EDGE LOWER SURFACE SILL AT XORS 420 FOUND CRACK. CRACKED SILL REMOVED AS PER SRM 51-34-01-0G AND FABRICATED SILL PER DOUGLAS DRAWING ARC7008 REVISION C. INSTALLED FEBRICATED SILL AT LEFT WING TRAILING EDGE LOWER SURFACE AT XORS 420 AS PER SRM 51-34-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

UPON REMOVED MAIN DECK DELAMINATED FLOOR PANEL #282JF FOR REPLACEMENT FOUND MAIN DECK FLOOR SEAT TRACK AT STATION 1791 X=-75.25 FLANGE CORRODED. MAIN DECK FLOOR SEAT TRACK AT STATION 1791 X=-75.25 FLANGE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1, ORIGINAL MATERIAL THICKNESS: 0.080" MATERIAL REMOVED: 0.052" MATERIAL REMAINING: 0.028". SEAT TRACK REPAIR CARRIED OUT AT STATION 1751 TO STATION 1811, X=-75.25 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,266 hrs · 19,966 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 694 FOUND CRACK. REPAIR CARRIED OUT AT LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 694 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

UPON REMOVAL MAIN DECK DELAMINATED FLOOR PANEL #282JF FOR REPLACEMENT FOUND MAIN DECK FLOOR SEAT TRACK AT STATION 1803 X=-107.25 FLANGE CORRODED. MAIN DECK FLOOR SEAT TRACK FLANGE AT STATION 1803 X=-107.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD 11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AS PER EA 1-5310-T0350631 P1 TITEL: FUSELAGE Ï¿½ MAINFRAME - CORROSION MAIN CARGO COMPARTMENT RIGHT HAND OUTBOARD SEAT TRACK AT X=-107.25 @ STATION 1778 & STATION 1803. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 82,266 hrs · 19,966 cycles

RIGHT WING Ï¿½ NO. 14 LEADING EDGE SLAT TRACK CUTOUT LOWER SKIN AT XOS 891 FOUND CRACK. REPAIR CARRIED OUT AT RIGHT WING NO. 14 LEADING EDGE SLAT TRACK CUT OUT LOWER SKIN AT XOS 891 AS PER SRM 57-40-02-2R FIGURE 201REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1391 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT STATION 1391 X= 47.5.CROWN DAMAGED AREA EVALUATED AND FOUND EXCEED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATION 1371 - STATION 1411 X= 47.5 AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# : 1-5750-T0350674 PART 1 STEP 1 A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,266 hrs · 19,966 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT WING FIXED LEADING EDGE AT XOS 667 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

UPON REMOVAL MAIN DECK DELAMINATED FLOOR PANEL #282JF FOR REPLACEMENT FOUND MAIN DECK FLOOR SEAT TRACK AT STATION 1778 X=-107.25 FLANGE CORRODED. MAIN DECK FLOOR SEAT TRACK FLANGE AT STATION 1778 X=-107.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD 11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AS PER EA 1-5310-T0350631 P1 TITEL: FUSELAGE Ï¿½ MAINFRAME - CORROSION MAIN CARGO COMPARTMENT RIGHT HAND OUTBOARD SEAT TRACK AT X=-107.25 @ STATION 1778 & STATION 1803. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 5-53 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT STATION 5-53 X= 47.5.CROWN DAMAGED AREA EVALUATED AND FOUND EXCEED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATION 5-0 TO STATION 5-63 X= 47.5 AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# : 1-5750-T0350674 PART 1 STEP 1 B AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,266 hrs · 19,966 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X=-47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AREA EVALUATED AND FOUND EXCEED LIMIT AS PER MD-11, SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1 AT STATION 1282 X=-47.5. SEAT TRACK REPAIR CARRIED OUT AT STATION 1249 Ï¿½ STATION 1313 X=-47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1-5750-T0350673 PART 1 STEP 2 B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-08 AND E.A.# : 1-5750-157177 A PART 2 STEP 2 A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# : 1-5750-157177 A PART 2 STEP 2 B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44- 09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 09 AND E.A.# : 1-5750-T0350593 PART 1 STEP 1 C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1-5750-T0350673 PART 1 STEP 2 A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1-5750-T0350593 PART 1 STEP 1 D AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1-5750-T0350673 PART 1 STEP 2 B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1-5750-T0350673 PART 1 STEP 2 B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# : 1-5750-157177 A PART 2 STEP 2 A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1-5750-T0350593 PART 1 STEP 1 A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1- 5750-T0350593 PART 1 STEP 1 B AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44- 09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 09 AND E.A.# : 1-5750-T0350593 PART 1 STEP 1 C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE(#8 HOLE) SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. REPAIR EVALUATED AND FOUND LH OUTBOARD FLAP FORWARD OUTBOARD HINGE ACTUATOR INBOARD LUG SURFACE REMAINING THICKNESS: 0.316" CORRECT AS PER E.A.# : 1-5750-T0350593 PART 1 STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1-5750-T0350593 PART 1 STEP 1 D AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.# : 1-5750-T0350673 PART 1 STEP 2 B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 82,266 hrs · 19,966 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.# : 1-5750-157177 A PART 2 STEP 2 B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BOTTLE — DEPLETED (EVAC SLIDE) · airframe 81,581 hrs · 19,757 cycles

SLIDE PRESSURE BOTTLE AIR DEPLETED DOOR L1 RESET L1 DOOR HANDLE & SERVICED PNEUMATIC RESERVOIR REF MM 52-11-04-5 & MM 12-25-04. A/C OK FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 1372) · airframe 81,424 hrs · 19,704 cycles

CRACK FOUND ON L/H WHEEL WELL FWD BULKHEAD AT TANK PANEL 275AZ AT O/B END OF HORIZONTAL STIFFENER (APB7253-501 LWR STIFFENER) COMPLIED WITH E.A. 1-5310-T0346570. INSTALLED DOUBLER REPAIR.

Part: BULKHEAD — CRACKED (BS 1372) · airframe 81,424 hrs · 19,704 cycles

CRACK FOUND ON R/H WHEEL WELL FWD BULKHEAD AT TANK PANEL 274AZ AT O/B END OF HORIZONTAL STIFFENER (APB7253-501 LWR STIFFENER) COMPLIED WITH E.A. 1-5310-T0346558. INSTALLED REPAIR DOUBLER

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 80,848 hrs · 19,530 cycles

APPROX 2.5 HOURS ENROUTE RECEIVED A LEVEL ONE ALERT "HYDRO 2 OFF". HYD QTY WAS 2.7 GALLONS AND CONTINUED TO LEAK FOR REMAINDER OF FLIGHT. HYD FLUID QTY DROPPED TO 0.0, GOT HYDRO 2 FAIL LEVEL 2 ALERT. DISCOVERED DURING DRY MOTORING ENGINE, LOWER (RIGHT) PUMP WAS LEAKING FLUID FROM LARGE PLUG (SQUARE) ON TOP OF PUMP. REMOVED AND REPLACED NR 2 ENG RT AND LT ENGINE DRIVEN PUMPS. OPS AND LEAK CHECK OK.

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 80,848 hrs · 19,530 cycles

APPROX 2.5 HOURS ENROUTE RECEIVED A LEVEL ONE ALERT "HYDRO 2 OFF". HYD QTY WAS 2.7 GALLONS AND CONTINUED TO LEAK FOR REMAINDER OF FLIGHT. HYD FLUID QTY DROPPED TO 0.0, GOT HYDRO 2 FAIL LEVEL 2 ALERT. REMOVED AND REPLACED NR 2 ENG RT AND LT ENGINE DRIVEN PUMPS PER AMM 29-11-20-4-1. OPS AND LEAK CHECK OK.

Part: SLEEVE — DAMAGED (NR 9 BRAKE) · airframe 79,702 hrs · 19,166 cycles

DURING A POSTFLIGHT INSPECTION, FOUND THE NR 9 BRAKE WAS COMING APART. THE AXLE SLEEVE WAS CRACKED AT THE LOCKING TAB AND THE BRAKE WAS COMING APART AT THE OUTER DISC, DAMAGED THE WHEEL ASSY. THE AXLE SLEEVE WAW REMOVED IAW AMM 32-15-00-4. THE BRAKE AND TIRE IS REMOVED IAW AMM 32-41-01-4, AND 32-43-20-4.

Part: BRAKE — DELAMINATED (MLG) · airframe 79,465 hrs · 19,092 cycles

NORMAL LANDING USING MEDIUM AUTOBRAKES. AFTER FIVE MINUTES BRAKE DIFF TEMP ILLUMINATED. BRAKE NR 1, 158 DEGREES. BRAKE NR 2, 342 DEGREES. R&R NR 1 MAIN BRAKE PER MM 32-43-20-4. REMOVED AND REPLACED DEFECTIVE BRAKE.

Part: GCU — INOPERATIVE (NR 2) · airframe 78,408 hrs · 18,789 cycles

ABOUT 30 MIN INTO FLIGHT, GEN 1 OFF FLASHED ON MOMENTARTLY. ABOUT 20 MIN LATER THE GEN 1 OFF & GEN 2 OFF & GEN 3 OFF FLASHED ON AND OFF CONTINUOUSLY FOR REMAINDER OF FLIGHT. ALL TIE BUSSES OPENED WHEN THE GEN OFF LIGHTS CAME ON. ACCESSED EPCU THRU CFDS AND FOUND FAULTS PRESENT LAST 2 FLIGHT LEGS. LEG -1 FAULT WAS GCU-2 WIRE INTACT GCU/TR-2B, FAULT ALSO LISTED IN-AIR FLT 0440, FAULT LEG 2 WAS GCU-2. REMOVED AND REPLACED THE EPCU IAW MM 24-08-01-4. PERFORMED ELECTRICAL POWER CONTROL ADJ/TEST IAW MM 24-08-01-5, ALL INDICATIONS NORMAL. RAN ALL ENGINES AND APPLIED MAX LOAD WITH EXTERIOR LIGHTS AUX HYD PUMPS AND FUEL PUMPS ON. VERIFIED THAT EACH ENGINE GENERATOR WOULD POWER THE ACFT INDIVIDUALLY. ENGINES RAN IAW JRH CHAPTER 5. ALL INDICATIONS NORMAL. AFTER REPLACEMENT OF THE EPCU, PERFORMED REQUIRED FCC-1 AND FCC-2 AFS TESTS TO MAINTAIN ACFT LLM CAPABILITY. ALL AFS TESTS PASSED ACFT REMAINS LLM CAPABLE.

Part: SLIDE — MALFUNCTIONED (R1 DOOR) · airframe 78,152 hrs · 18,716 cycles

FOUND R1 DOOR EVACUATION SLIDE REMOTE PTT SWITCH ILLUMINATED. REMOVED AND REPLACED THE SLIDE, OPS CHECKED GOOD IAW AMM 25-61-15-4.

Part: SLIDE — INOPERATIVE (R1 DOOR) · airframe 78,152 hrs · 18,716 cycles

FOUND THE R1 DOOR EVACUATION SLIDE REMOTE PTT SWITCH ILLUMINATED. REMOVED AND REPLACED SLIDE OPS CHECK IS GOOD PER AMM 25-61-15-4.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 77,606 hrs · 18,550 cycles

ADVANCING THE THROTTLES FOR TAKEOFF, RECEIVED A LEVEL ONE EMERGENY POWER ON, WITH SWITCH IN ARMED POSITION. REJECTED TAKE OFF. EXITED RUNWAY TURNED OFF THEN BACK TO ARM AND WARNINGS EXTINGUISHED. IAW AMM 24-24-00-5, PERFORMED A SAT EMERGENCY POWER ADJUSTMENT AND TEST. PERFORMED SAT EPCU IAW MM 24-08-1-5. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: WEB — CRACKED (TE FLAP) · airframe 77,412 hrs · 18,500 cycles

UPON REMOVING RT I/B FLAP EXISTING REPAIR, CRACK FOUND ON WEB AT STA XIFH 171.30 AS MARKED. RT INBD FLAP STA XIFH 171.30 WEB CARRIED OUT REPLACEMENT AS PER EA 1-5750-T0336221 PT 1. RT WING INBD FLAP ASSY CENTER BOX UPPER SKIN AND LOWER SEGMENT LOWER SKIN REPAIRS-RSC TRACKING. EO 1-5100-7-5001 B6 P1. REPAIR CLASSIFIEDAS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (TE FLAP) · airframe 77,412 hrs · 18,500 cycles

AGING A/C-EXISTING DOUBLER REPAIR AT RT WING INBD FLAP TO SURFACE CENTER SKIN AT XIFH 165.3 AND XIFH 177.3. EXISTING DOUBLER REPAIR AT RT WING INBD FLAP TOP SURFACE CENTER SKIN XIFH 165.3- XIFH 177.3 EVALUATED AND FOUND DAMAGED. RT WING INBD FLAP TOP SURFACE CENTER SKIN AT XIFH 165.3-XIFH 177.3 EVALUATED AND REPAIRED AS PER EA 1-5750-T0336221 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (NLG) · airframe 77,412 hrs · 18,500 cycles

DURING HFEC INSPECTION ON NOSE LANDING GEAR RT TRUNNION FTG SLOT OUT AREA, CRACK FOUND ON THE RADIUS PARALLEL TO THE SLOT OUT AREA APPROX 3/4 INCH LENGTH AS MARKED. CRACK AT NOSE LANDING GEAR RT TRUNNION FTG EXISTING SLOT OUT REPAIR AREA, REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-10-14-2R REPAIR 2 FIG 202 (LENGTH = 1.500" WITH=0.280") NEW REPAIR FILLER FABRICATED AND INSTALLED AT NOSE LANDING GEAR RT TRUNNION FTG STA 595 AS PER SRM 53-10-14-2R REPAIR 2 FIG 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — CRACKED (RT WING) · airframe 77,412 hrs · 18,500 cycles

RT WING L/E AT STA XOS 584 FOUND FORMER ANGLE CRACK AS MARKED. FORMER ANGLE REMOVED AND REPLACED AS PER SRM 51-35-01-0G FORMER FABRICATED AS PER DWG ARB 2931 REV H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,412 hrs · 18,500 cycles

RT WING L/E AT STA XOS 789 FOUND DOUBLER CRACK AS MARKED. DOUBLER REMOVED AND REPLACED AS PER SRM 51-35-01-0G. DOUBLER FABRICATED AS PER DWG ARB 3954 REV K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,412 hrs · 18,500 cycles

LEFT WING L/E BEADED DOUBLER AT XOS 639 FOUND CRACKED. REPAIRED THE BEADED 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 1541) · corrosion level 2 · airframe 77,412 hrs · 18,500 cycles

MAIN DECK SEAT TRACK AT BS 1541, LBL 8.5, FOUND CORRODED. REPLACED THE SEAT TRACK FROM BS 5-123 TO 1571, 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 77,412 hrs · 18,500 cycles

RT WING L/E BEADED DOUBLER AT REFUELING ACCESS DOOR STA XOS 627 FOUND CRACK. REPAIR CARRIED OUT ON RT WING L/E BEADED DOUBLER AT REFUELING ACCES DOOR STA XOS 627 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 800) · airframe 77,412 hrs · 18,500 cycles

MAIN DECK SEAT TRACK AT BS 800, LBL 8.5 FOUND DAMAGED. REPLACED THE SEAT TRACK FROM BS 783 TO 832, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 800) · airframe 77,412 hrs · 18,500 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 800, LBL 47.5 FOUND DAMAGED. REPLACED THE SEAT TRACK FROM BS 783 TO 869, 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 77,412 hrs · 18,500 cycles

RIGHT WING L/E BEADED DOUBLER AT XOS 586 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,412 hrs · 18,500 cycles

RIGHT WING L/E BEADED DOUBLER AT XOS 667 FOUND CRACKED. REPAIRED THE BEADED 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 635-735) · airframe 77,412 hrs · 18,500 cycles

MAIN DECK SEAT TRACK AT BS 635 TO 735, LBL 8.5 FOUND CORRODED. REPLACED THE SEAT TRACK FROM BS 625 TO 745, 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 77,412 hrs · 18,500 cycles

RIGHT WING L/E BEADED DOUBLER AT XOS 736 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,412 hrs · 18,500 cycles

LEFT WING L/E BEADED DOUBLER AT XOS 766 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 77,412 hrs · 18,500 cycles

RIGHT WING FIXED L/E STRINGER AT XOS 789 FOUND CRACKED. REPAIRED THE STRINGER IAW SRM 57-40-03-2R, FIG 201, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,412 hrs · 18,500 cycles

LEFT WING L/E BEADED DOUBLER AT XOS 699 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,412 hrs · 18,500 cycles

LEFT WING L/E BEADED DOUBLER AT XOS 755 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,412 hrs · 18,500 cycles

LEFT WING L/E BEADED DOUBLER AT XOS 646 FOUND CRACKED. REPAIRED THE BEADED 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 — DAMAGED (BS 1800) · airframe 77,412 hrs · 18,500 cycles

MAIN DECK SEAT TRACK AT BS 1800, RBL 27.5 FOUND DAMAGED. REPLACED THE SEAT TRACK FROM BS 1741 TO 1821 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 77,412 hrs · 18,500 cycles

LEFT WING L/E BEADED DOUBLER AT XOS 732 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 74,838 hrs · 17,694 cycles

UPON DISARMING L1 DOOR AT CRK THE DISARM LIGHT DID NOT COME ON. USED R1 FOR ENTRY. FOUND SLIDE WAS NOT DISARMED. FOUND "DISARM" BULBS BURNED OUT. RELAMP AND CHECKED NML. OPERATION CHECK ARM/DISARM SEVERAL TIMES NML PER AMM 52-11-02-6.

Part: SLIDE RAFT — DEFECTIVE (R1 DOOR) · airframe 73,571 hrs · 17,332 cycles

REPEAT WRITE UP. R1 ESCAPE SLIDE BOTTLE PRESS LIGHT ILLUMINATED DURING CRUISE FLIGHT. FOUND INTERMITTENT CONTINUITY ON ELEC JACK COMING FROM SLIDE RAFT. R & R R1 DOOR SLIDE RAFT. BOTTLE PRESS PTT LIGHT OPERATIONS CHECKED NORMAL.

Part: SKIN — CORRODED (BS 2140-2163) · corrosion level 2 · airframe 73,148 hrs · 17,216 cycles

BS 2140 - 2163, FAIRING 347DF, MATING SURFACE TO FUSELAGE LOWER FOUND SURFACE CORROSION. REPAIRED IAW EA 1-5330-T0322643 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1310) · airframe 73,148 hrs · 17,216 cycles

CABIN MDCC CORROSION FOUND ON SEAT TRACK FLANGE, AT BS 1310, LBL 75.25. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: PAN — CORRODED (BS 401) · corrosion level 2 · airframe 73,148 hrs · 17,216 cycles

LOWER FUSELAGE, TOILET SERVICING DRAIN VALVES, CUT OUT SHROUD PAN, FOUND CORRODED. R & R IAW SRM 51-35-01-0G & SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 73,148 hrs · 17,216 cycles

LEFT WING LE FORMER AT WS XOS 1025 FOUND CRACKED. FORMER REMOVED IAW SRM 51-31-01-0G. FABRICATED NEW FORMER IAW DWG ARB2920 REV BB. INSTALLED NEW FORMER AT LT WING LE IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BEAM — CRACKED (L3 DOOR) · airframe 73,148 hrs · 17,216 cycles

CABIN MAIN DECK CARGO BAY, L3 DOOR, NR 1 BEAM, FOUND CRACKED. R & R IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CORRODED (BS 1310) · airframe 73,148 hrs · 17,216 cycles

CABIN MAIN DECK CARGO L3 DOOR AFT LOWER FUSELAGE FRAME WEB CRACKED AT BS 1310, BETWEEN LONGERONS 26 - 27L. REPAIRED IAW SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1255) · airframe 73,148 hrs · 17,216 cycles

CABIN MAIN DECK CARGO DOOR FWD LOWER FUSELAGE FRAME WEB CRACKED AT BS 1255, BETWEEN LONGERONS 26 - 27R. REPAIRED IAW SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,148 hrs · 17,216 cycles

CABIN MAIN DECK CARGO DOOR AFT LOWER FUSELAGE FRAME WEB CRACKED AT BS 1310, BETWEEN LONGERONS 26 - 27R. REPAIRED IAW SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CORRODED (BS 1255) · airframe 73,148 hrs · 17,216 cycles

CABIN MAIN DECK CARGO L3 DOOR FWD LOWER FUSELAGE FRAME WEB CRACKED AT BS 1255, BETWEEN LONGERONS 26 - 27L. REPAIRED IAW SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1358) · airframe 73,148 hrs · 17,216 cycles

CABIN MAIN DECK CARGO BAY, CORROSION FOUND ON CARGO TRACK RT, BS 1358, RBL 27.5. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BATTERY — MISINSTALLED (L1 DOOR) · airframe 72,769 hrs · 17,100 cycles

L1 DOOR ESCAPE SLIDE, TEST LIGHT INOPERATIVE. INSTALLED BATTERIES CORRECTLY IN HOLDER FOR L1 DOOR SLIDE BOTTLE PRESS REMOTE TEST SWITCH IAW MM CHAPT 25-61-04-4. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PUMP — LEAKING (NR 3 ENGINE) · airframe 723 hrs · 16,975 cycles

ON DESCENT RECEIVED HYD 3 PRESS HI ALERT, IT WENT BACK TO NORMAL, THEN HYD 3 SYS FAILED. TOTAL LOSS OF SYS 3 QTY. RAN QRH & MANUALLY EXTENDED GEAR. FOUND NR 3 ENG RT PUMP BROKEN. REPLACED NR 3 ENG RT HYD PUMP. OPERATIONS & LEAK CHECK GOOD.

Part: TRANSMITTER — MALFUNCTIONED (WARNING SYSTEM) · airframe 69,390 hrs · 16,048 cycles

ON CLIMB OUT STARTED RECEIVING AURAL WARNING LG CONTINUOUSLY. ALSO ON CONFIG PAGE, LT OTBD FLAP HAD INTERMITTENT YELLOW X. NO ALERTS SHOWING. RETURN & AURAL WARNING WENT AWAY DESCENDING BELOW FL290. DID NOT RETURN.

Part: BOLT — MISSING (ARMING LEVER) · airframe 68,952 hrs · 15,909 cycles

THE AFT ARMING LEVER ON THE R1 MAIN ENTRY DOOR DOES NOT DISARM WHEN LEVER IS DISARMED. 1R MAIN ENTRY SLIDE & RAFT REMOVED. COMPLIED WITH EA 1-2560-T0307738 PART 1 & 2.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 68,641 hrs · 15,823 cycles

FORWARD FLOOR PANEL IN COURIER FLIGHT COMPARTMENT IS SPONGY WHEN WEIGHT IS APPLIED ON THE AFFECTED AREA. FLOOR PANEL REPAIRED IAW SRM 53-00-50 FIGURE 206 REPAIR 2 REVISION 53. FLOOR PANEL REMOVED AND INSTALLED IAW AMM 53-21-04-4 REVISION 78.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: SKIN — CRACKED (RT WING) · airframe 68,641 hrs · 15,823 cycles

RIGHT WING SKIN AROUND ACCESS PANEL FOUND CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION BETWEEN XORS = 683.4 & 713.6. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: SKIN — CRACKED (LT WING) · airframe 68,641 hrs · 15,823 cycles

LT WING SKIN AROUND ACCESS PANEL, FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: FLOOR SUPPORT — CORRODED (BS 1941) · corrosion level 2 · airframe 68,641 hrs · 15,823 cycles

MAIN DECK CARGO FLOOR SUPPORT AT BS 1941, RBL 56 FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 53. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: FLOOR SUPPORT — CORRODED (BS 1941) · corrosion level 2 · airframe 68,641 hrs · 15,823 cycles

MAIN DECK CARGO FLOOR SUPPORT AT BS 1941, LBL 56 FOUND CORRODED. REMOVED AND REPLACED FROM BS 1887 TO 2007 IAW SRM 51-31-01 REVISION 53. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: FLOOR SUPPORT — CORRODED (BS 1981) · corrosion level 2 · airframe 68,641 hrs · 15,823 cycles

MAIN DECK CARGO FLOOR SUPPORT AT BS 1981, RBL 24 FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 53. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7087 REVISION M. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: SEAT TRACK — CORRODED (BS 1861) · corrosion level 2 · airframe 68,641 hrs · 15,823 cycles

MAIN DECK CARGO FLOOR SEAT TRACK AT BS 1861, LBL 75.25 FOUND CORRODED AT FLANGE AREA. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 6 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: FIRE LOOP — FALSE ACTIVATION (FIRE DETECTION) · airframe 66,908 hrs · 15,242 cycles

LEVEL 1, FIRE DETECTION 1 FAIL APPROX 5 MINUTES AFTER TAKEOFF FOLLOWED BY INTERMITTENT ENGINE 1 FIRE WARNING (ENGINE OPERATING INDICATIONS WERE NORMAL). ALL INDICATIONS STOPPED UNTIL FINAL APPROACH, AT WHICH TIME HAD INTERMITTENT LEVEL 1, FIRE DETECT 1, FAIL. R & R FIRE DETECTOR HARNESS, LOOP A, ON ENG 1 REF AMM 71-50-04-4-1. BITE TESTED GOOD. GEARBOX LOOP A(DH6) AND UPPER TURB R LOOP A (DH4)REF ESM 71-00-02. RAN ENG IAW JRH TO 83 PERCENT. NO FAULTS NOTED. OK FOR SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 65,747 hrs · 14,899 cycles

CAPTAIN'S WINDSHIELD OUTSIDE PANEL SHATTERED AT FL390. REPLACED WINSHIELD. TORQUED ALL SCREWS PER TIGHTENING SEQUENCE. OPS. CHECK WINDOW HEAT IAW AMM 56-11-01-4-1

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,638 hrs · 14,574 cycles

L1 DOOR REMOTE SLIDE PRESSURE TEST LIGHT DOESN'T TEST. REPLACED BATTERIES LOCATED ON THE UPPER LINING ASSY IN L1 DOOR, IAW AMM: 25-61-04-4. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (L1 DOOR SLIDE) · airframe 64,635 hrs · 14,573 cycles

L1 DOOR REMOTE SLIDE PRESSURE TEST LIGHT DOESN'T TEST. REPLACED BATTERIES LOCATED ON THE UPPER LINING ASSY IN L1 DOOR, IAW AMM 25-61-04-4. OP CHECKED GOOD.

Part: BUSHING — WORN (TE FLAP HINGE) · airframe 64,249 hrs · 14,465 cycles

LEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE ATTACH UPPER BOLT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 0.405" AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72 MAXIMUM ALLOWABLE DIAMETER 0.391". REPAIR CARRIED OUT IAW EA 1-5750-157176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (TE FLAP HINGE) · airframe 64,249 hrs · 14,465 cycles

WORN BUSHING OF PIVOT HOLE AT RT FORWARD (WING) OTBD FLAP, OTBD HINGE FOR NDT INSPECTION ON PIVOT HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 2.3295" AND MAXIMUM ALLOWABLE DIAMETER 2.3135" FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. REPAIR ACCOMPLISHED EA 1-5750-157179, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (LT TE FLAP HINGE) · airframe 64,249 hrs · 14,465 cycles

LEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE ATTACH LOWER BOLT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 0.395" AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72 MAXIMUM ALLOWABLE DIAMETER 0.391". REPAIR CARRIED OUT IAW EA 1-5750-157176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE — WORN (CARGO DOOR) · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO DOOR SIDE NR 1 FIRST 9TH LOBE HOLE FOUND WORN OUT OF LIMITS. REWORKED AND FOUND EXCEED LIMIT IAW CMM 52-34-04, REPAIR 2, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5230-157188. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: TEE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

RIGHT WING OTBD FLAP VANE TEE FITTING NR 4 FROM INBD FOUND TRACK ATTACH HOLE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02 FIG 201, REV 49. EXISTING SLOT SIZE: 0.885" X 0.613", FINAL SLOT SIZE: 0.978" X 0.743", MAXIMUM ALLOWABLE LIMIT: 0.940"X0.670". REPAIR CARRIED OUT IAW EA 1-5750-157189, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 64,249 hrs · 14,465 cycles

LEFT WING ANTI-ICE DUCT CUTOUT SKIN MISREPAIRED. CARRIED OUT REPAIR IAW SRM 57-40-01, FIG 201, REPAIR 10, REV 49. & EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 64,249 hrs · 14,465 cycles

RT WING TELESCOPIC DUCT CUTOUT SKIN XOS 464, MISREPAIRED. CARRIED OUT REPAIR IAW SRM 57-40-01, FIG 201, REPAIR 10, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 64,249 hrs · 14,465 cycles

DURING FLOURESCENT PARTICLE INSPECTION, FOUND CORROSION ON LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG HOLE. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157194 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

SKIN AT FWD OF DOOR FOUND MISREPAIRED. CARRIED OUT REPAIR IAW SRM 53-00-15, FIG 202, REPAIR 8 REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 64,249 hrs · 14,465 cycles

LEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07 REV 72. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. BUSHING FABRICATED AND INSTALLED REF EA 1-5750-157194. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 64,249 hrs · 14,465 cycles

LT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 72. EXISITING THICKNESS 0.321", REMAINING THICKNESS 0.318", MATERIAL REMOVED 0.003", MINIMUM ALLOWABLE THICKNESS 0.320". REPAIR CARRIED OUT IAW EA 1-5750-157176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 64,249 hrs · 14,465 cycles

LEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BUSHING FOUND WORN. BUSHING REMOVED CMM 20-20-07, REV 72, EXISTING HOLE DIAMETER 1.328" , MAX ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 51-52-03, REV 72. BUSHING FABRICATED AND INSTALLED REFER TO EA 1-5750-157194. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

LEFT WING OTBD FLAP, INBD AFT HINGE BRACKET PIVOT INBD LUG BORE, FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 72. EXISTING BORE DIAMETER: 1.147", FINAL BORE DIAMETER: 1.1605", MAXIMUM ALLOWABLE DIAMETER: 1.150". REPAIR ACCOMPLISHED IAW EA 1-5750-157178. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 64,249 hrs · 14,465 cycles

DURING FLOURESCENT PARTICLE INSPECTION, FOUND CORROSION ON LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG HOLE. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157194. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 282FF SEAT TRACK BS 1801 X= -49 RT FOUND CORRODED ALONG FLANGE AREA. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 282GF SEAT TRACK BS 1581 X= -76 RT FOUND CORRODED ALONG FLANGE AREA. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 282JF SEAT TRACK BETWEEN BS 1781 AND 1801 X= -70 RT FOUND CORRODED ALONG FLANGE AREA. REPAIRED IAW SRM 53-00-52, FIG 201, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 283BF, SEAT TRACK AT STA 1569 X= -8.5 RT FOUND CORRODED ALONG FLANGE AREA. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 49. SEAT TRACK REWORKED IAW DWG AFA7795, REV F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100, REV 114.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 64,249 hrs · 14,465 cycles

AGING AIRCRAFT INSPECTION - CENTER CARGO DOOR FWD LOWER CORNER EDGE FOUND MISREPAIRED. CARRIED OUT REPAIR IAW SRM 52-30-16, FIG 201 REPAIR 3, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: RIB — CRACKED (NR 3 SLAT) · airframe 64,249 hrs · 14,465 cycles

UPON REMOVAL OF LT NR 3 L/E SLAT FOUND INBD RIB CRACKED. RIB REMOVED IAW SRM 51-31-01, REV 49 AND REPLACED WITH FABRICATED RIB IAW SRM 51-31-01, REV 49. RIB FABRICATED IAW DWG ARB1680, REV H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

RT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE ATTACH SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72 UPPER: EXISTING THICKNESS 0.451", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.446". LOWER: EXISTING THICKNESS 0.453", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.449". REPAIR ACCOMPLISHED IAW EA 1-5750-157179, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 64,249 hrs · 14,465 cycles

LEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH, INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 72. EXISTING DIAMETER 1.248", FINAL DIAMETER 1.257", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED OUT IAW EA 1-5750-157176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 64,249 hrs · 14,465 cycles

LEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET, ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57- 44-09 REV 72. EXISTING DIAMETER 1.223", FINAL DIAMETER 1.228", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED OUT IAW EA 1-5750-157176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 600) · airframe 64,249 hrs · 14,465 cycles

RIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. HINGE BRACKET ACTUATOR ATTACH REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.223" AND MAXIMUM ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157177, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 64,249 hrs · 14,465 cycles

LEFT WING OTBD FLAP OTBD FORWARD HINGE BRACKET SIDE ATTACH SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72. EXISTING THICKNESS UPPER: 0.468", LOWER: 0.479". MATERIAL REMOVED UPPER: 0.003", LOWER 0.003". REPAIR CARRIED OUT IAW EA 1-5750-157176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-93 AND STA 5-113 LONGERON, 47LT SPLICE CRACK. R & R IAW SRM 51-33-01, REV 49. SPLICE FABRICATED IAW DWG A5A7114, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 600) · airframe 64,249 hrs · 14,465 cycles

RIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BUSHING, FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72 . HOLE MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA 1.253" MAX ALLOWABLE DIA 1.220" . REPAIR ACCOMPLISHED IAW EA 1-5750-157181, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 600) · airframe 64,249 hrs · 14,465 cycles

RIGHT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BUSHING, FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA 1.221" MAX ALLOWABLE DIA. 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-157181, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-93 AND STA 5-113, LONGERON 44 RT SPLICE CRACK. R & R IAW SRM 51-33-01, REV 49. SPLICE FABRICATED IAW DWG A5A7114, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-93 AND STA 5-113, LONGERON 37LT SPLICE CRACK. R & R IAW SRM 51-33-01, REV 49. SPLICE FABRICATED IAW DWG A5A7114, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-93 AND STA 5-113, LONGERON 45 RT SPLICE CRACK. R & R IAW SRM 51-31-01, REV 49. SPLICE FABRICATED IAW DWG A5A7116, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 600) · airframe 64,249 hrs · 14,465 cycles

RIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.222" AND MAXIMUM ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157179, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 64,249 hrs · 14,465 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. HOLE MEASURED FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING HOLE DIAMETER 1.222" AND MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-157180 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON — CRACKED (ZONE 200) · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO, ON REMOVAL OF CRACK SPLICE 6L AT STA 5-123 FOUND LONGERON CRACKED. REPAIRED IAW SRM 53-00-05 REPAIR 1, FIG 202, REV 49 AND SRM 51-31-01, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 600) · airframe 64,249 hrs · 14,465 cycles

RIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH, OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.225" AND MAXIMUM ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157177, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: BUSHING — WORN (ZONE 500) · airframe 64,249 hrs · 14,465 cycles

LEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. HOLE MEASURED FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72 EXISTING HOLE DIAMETER 1.221" AND MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-157180, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 600) · airframe 64,249 hrs · 14,465 cycles

RIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.221" AND MAXIMUM ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157179 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 600) · airframe 64,249 hrs · 14,465 cycles

RIGHT WING L/E NR 10 SLAT TRACK CUT-OUT LOWER OTBD CORNER WITH CRACK AT STA XOS 661. TRIMMED AND REPAIR CARRIED OUT IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REV 49. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 64,249 hrs · 14,465 cycles

FRAME AT STA 535, LONGERON 24 RT MISREPAIRED. CARRIED OUT REPAIR IAW SRM 53-20-07, FIG 201. REPAIR 1, REV 49 EO 1-5100-7-5001B PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 64,249 hrs · 14,465 cycles

DURING X-RAY INSPECTION, FOUND CRACK AT STATION 5-123 LONGERON SPLICE 6L AT CENTER ROW OF CENTER SECTION FASTENER. R & R IAW SRM 51-31-01, REV 49. SPLICE FABRICATED IAW DWG A5A7112, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

SKIN MISREPAIRED. CARRIED OUT REPAIR IAW SRM 53-00-15, FIG 202, REPAIR 8 REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

FWD CARGO COMPARTMENT CEILING AREA APPROX BS 635, X= 47.5. FOUND SEAT TRACK CRACKED. R & R IAW SRM 51-31-01, REV 49. SEAT TRACK REWORKED IAW DWG ACA7399, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

SKIN FOUND MISREPAIRED. CARRIED OUT IAW SRM 53-00-15, FIG 202, REPAIR 8, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

FORWARD CARGO COMPARTMENT CEILING AREA APPROX STA 939, X= 47.5 FOUND SEAT TRACK CRACKED. REPAIRED IAW SRM 53-00-52, FIG 201 REVISION 49. SEAT TRACK REWORKED IAW DWG ACA7399, REV T. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

FWD CARGO COMPARTMENT CEILING AREA APPROX BS 635, X= 27.5 FOUND SEAT TRACK CRACKED. R & R IAW SRM 53-00-52, FIG 201, REV 49. SEAT TRACK REWORKED IAW DWG REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 64,249 hrs · 14,465 cycles

DURING X-RAY INSPECTION, FOUND CRACK AT STATION 5-123 LONGERON SPLICE 4R AT CENTER ROW NR 4 TOWARD NR 5 FASTENER COUNT FROM AFT. R & R IAW SRM 51-31-01, REV 49. SPLICE FABRICATED IAW DWG A5A7111, REV C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: FRAME — MISREPAIRED (BS 535) · airframe 64,249 hrs · 14,465 cycles

FRAME AT STA 535, LONGERON 24 LEFT MISREPAIRED. CARRIED OUT REPAIR IAW EA 1-5310-157190 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (LT WING) · airframe 64,249 hrs · 14,465 cycles

LT WING L/E NR 11 SLAT TRACK CUT-OUT LOWER OTBD CORNER CRACK AT STATION XOS 721. TRIMMED AND CARRIED OUT REPAIR IAW SRM 57-40-02, FIG 201, REV 49. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 114.

Part: ANGLE — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

LEFT WING T/E ACCESS PANEL 541JB FORWARD SUPPORT TEE ANGLE FOUND WITH CORROSION. R & R IAW SRM 51-31-01, REV 49 AND SRM 51-33-01, REV 49. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: STRINGER SPLICE — CRACKED (ZONE 200) · airframe 64,249 hrs · 14,465 cycles

DURING X-RAY INSPECTION, FOUND CRACK APPROX 0.9 INCH LONG AT STA 5-123, LONGERON 6R, STRINGER SPLICE AT CENTER ROW NR 4 TOWARD NR 5 FASTENER COUNT FROM AFT. REMOVED AND REPLACED IAW SRM 51-31-01, REV 49. SPLICE FABICATED IAW DWG A5A7112, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

FWD CARGO COMPARTMENT CEILING AREA APPROX BS 755, X= -30 FOUND SEAT TRACK CRACKED. R & R IAW SRM 51-31-01, REV 49, SEAT TRACK REWORKED IAW DWG ACA7102 REV R. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

FWD CARGO COMPARTMENT CEILING AREA APPROX BS 635, X= -8.5 FOUND SEAT TRACK CRACKED. R & R IAW SRM 51-31-01, REV 49. SEAT TRACK REWORKED IAW DWG ACA7104, REV T. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 64,249 hrs · 14,465 cycles

DURING X-RAY INSPECTION, FOUND A CRACK APPROXIMATELY 0.9" LONG AT STA 5-0. LONGERON 4R, LONGERON SPLICE AT CENTER ROW NR 7 TOWARD NR 8 FASTENER COUNT FROM AFT. R & R IAW SRM 51-33-01, REV 49. SPLICE FABRICATED IAW DWG EA 7634, REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO SEAT TRACK AT BS 1545, X= 8.5 LT FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REV 49. SEAT TRACK REWORKED IAW DWG AFA7795, REVISION F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: KEELBEAM — DAMAGED (BS 1436) · airframe 64,249 hrs · 14,465 cycles

CENTER LANDING GEAR WW, RT SIDE KEEL BEAM WEB STATION Y= 1436, X= 31.50 25" ABOVE DOOR HINGE LINE FOUND OIL CANNING EXCEED LIMIT (MAXIMUM ALLOWABLE IS 0.190", MEASURED 0.35".0). CARRIED OUT REPAIR IAW EA 1-5310-157187. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO SEAT TRACK AT BS 492, X= -27.5 RT FOUND CORRODED. R & R WITH NEW REWORKED SEAT TRACK IAW SRM 51-31-01, REV 49. NEW SEAT TRACK REWORK CARRIED OUT IAW DWG ACA7102, REV R. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BEAM — CRACKED (ZONE 100) · airframe 64,249 hrs · 14,465 cycles

LOWER FUSELAGE CENTER CARGO DOOR JAMB UPPER BEAM APPROX STA 1721, DOOR ACTUATOR LOCATION FOUND 0.75" CRACKED. CARRIED OUT REPAIR IAW EA 1-5310-157182, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 64,249 hrs · 14,465 cycles

MAIN DECK CARGO SEAT TRACK AT BS 1851, X= 8.5 LT, FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REV 49. SEAT TRACK REWORKED IAW DWG AFA7795, REV F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 64,249 hrs · 14,465 cycles

CENTER LANDING GEAR WHEEL WELL FWD BULKHEAD FOUND CRACK ON RT TEE FITTING UPPER AREA. R & R IAW SRM 51-31-01, REV 49. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 114.

Part: INDICATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 63,694 hrs · 14,292 cycles

L1 DOOR SLIDE TEST LAMP RETAINER FOUND INOPERATIVE, DURING SERVICE CHECK. SWAPED WITH R1, SLIDE LIGHT WORKS NORMALLY. R & R L1 REMOTE PRESSURE INDICATOR ASSY IAW AMM 25-61-04-4. OPS CHECKED GOOD.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 63,646 hrs · 14,274 cycles

LEFT INBD FLAP UPPER SKIN CRACKED. REPAIRED IAW EA 1-5750-157587, PART 1.

Part: BEZEL — MISSING (EMERGENCY LIGHT) · airframe 63,471 hrs · 14,224 cycles

EMERGENCY LIGHT ON RT SIDE OF ACFT IN ENTRY AREA ABOVE LAV IS MISSING BEZEL ASSY. INSTALLED EMERGENCY LIGHT BEZEL IAW SMP. PERFORMED EMERGENCY LIGHT TEST IAW 33-50-00-5. OP'S CHECKED GOOD.

Part: SWITCH — FAULTED (ESCAPE SLIDE) · airframe 62,813 hrs · 14,052 cycles

EVACUATION SLIDE REMOTE PTT SWITCH REMAINS ILLUMINATED. FOUND PRESSURE SWITCH ON SLIDE BOTTLE AT FAULT. REMOVED AND REPLACED THE DOOR SLIDE ASSEMBLY

Part: INDICATOR — FALSE INDICATION (R1 SLIDE PRESS) · airframe 62,758 hrs · 14,034 cycles

1R DOOR SLIDE LIGHT ILLUMINATED DURING CRUISE. ON FOR REMAINDER FLIGHT. CHECKED BOTTLE PRESSURE FOUND GREEN BAND AND CONTINUITY CHECK OF THE PRESURE SWITCH FOUND OK. THEN R & R 1R PRESSURE REMOTE INDICATOR ASSY IAW MM 25-61-04-4. INDICATION TEST FOUND OK IAW MM 25.

Part: INDICATOR — INOPERATIVE (ESCAPE SLIDE) · airframe 62,579 hrs · 14,001 cycles

R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR INOPERATIVE. R & R 2 BATTERIES IAW MM:25-61-04-4-0. OPS CHECK OK. ACFT OK TO CONTINUE.

Part: IDG — CRACKED (NR 2) · airframe 60,021 hrs · 13,387 cycles

ON TAXI OUT MEM LEVEL NR 2 "GEN DRIVE 2 FAULT " WARNING DISCONNECT IDG NR 2 CDG U IN WORK. REMOVED AND REPLACED ENGINE NR 2 IDG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,049 hrs · 13,180 cycles

MAIN DECK CARGO SEAT TRACK CROWN STA 755 X=-47 FOUND W/ SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 725 TO STA 765 X=-47 IAW SRM 53-00-52, FIG 201. REPAIR REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — BULGED (FUSELAGE) · airframe 59,049 hrs · 13,180 cycles

SKIN BULGE ALONG FR STA 5-70 BETWEEN LONG 51R - 52R APPROX 4" LENGTH. BULGE SKIN AT FR STA 5-70 BETWEEN LONG 51R - 52R APROX 4" LENGTH TRIMMED OUT AND CARRIED REPAIR IAW SRM 53-00-01, FIG 201, REV 43. HFEC INSP CARRIED OUT IAW NDT SPM REV 13, 06-10-01.001 ON TRIMMED OUT AREA AND FOUND NO CRACK EVIDENT. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,049 hrs · 13,180 cycles

MAIN DECK CARGO SEAT TRACK INBD FLANGE STA 1501-1521 X=-8 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK AT STA 1501 TO STA 1521 X=-8, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1491 TO STA 1531 X=-8 IAW SRM 53-00-52, FIG 201. REPAIR 1 REV 43. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100 REV 110.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 59,049 hrs · 13,180 cycles

SKIN DEFORMATION AT FR STA 5-70, BETWEEN LONG 49R - 50R. SKIN DEFORMED AT FR STA 5-70 BETWEEN LONG 49R -50R TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-00-01 FIG 201 REV 43. HFEC INSP CARRIED OUT IAW DAC NDT SPM REV 13, 06-10-01.001 ON TRIMMED OUT AREA AND FOUND NO CRACK EVIDENT. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,049 hrs · 13,180 cycles

MAIN DECK CARGO SEAT TRACK INBD FLANGE FROM STA 1501 TO 5-0 X= 107 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK INBD FLANGE FROM STA 1501 TO 5-0 X= 107. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO 1531 / 5-0 X= 107 IAW SRM 53-00-52 FIG 201 REPAIR 1 REV 43. REFER TO SNRM N00591 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,049 hrs · 13,180 cycles

MAIN DECK CARGO SEAT TRACK INBD FLANGE AT STA 1481 X= 107 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK INBD FLANGE AT STA 1481 X= 107, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO STA 1531/5-0 X= 107 IAW SRM 53-00-52, FIG 201. REPAIR 1 REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 59,049 hrs · 13,180 cycles

HFEC OPEN HOLE INSP. CARRIED OUT AND FOUND 02EA HOLES W/ CRACK INDICATION RT WING LWR SKIN PANEL OUTER WING ACCESS CUTOUT BTW XORS=683.4 AND XORS=713.6 AS MARKED. QTY 02 EA CRACK FASTENER HOLES ON RT WING LWR SKIN PNL FUEL TANK ACCESS DOOR CUTOUT 636AB BTW STA XORS 683.4 AND XORS 713.6 CARRIED OUT REPAIR IAW EA 1-5710-140329. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 59,049 hrs · 13,180 cycles

HPEC OPEN HOLE INSP. CARRIED OUT AND FOUND 01 HOLE WITH CRACK INDICATION ON LT WING LWR SKIN PANELS, OUTER WING ACCESS DOOR BTW XORS=683.4 AND XORS=713.6 AS MARKED. QTY 01 EA CRACK FASTENER HOLE ON LT WING LOWER PNL FUEL TANK ACCESS DOOR CUTOUT 536AB BTW STA XORS 683.4 AND XORS 713.6 CARRIED OUT REPAIR IAW EA 1-5710-140328, TITLE (AD 2007-07-04 WINGS - LT LOWER SKIN PLANK CUTOUT AT 536AB - REPAIR TO ACCESS DOOR ATTACHMENT BORES WITH CRACK INDICATIONS PSE 57.23.01 AL1) REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.

Part: SUPPORT FITTING — CRACKED (LE SLAT) · airframe 59,049 hrs · 13,180 cycles

LT WING - NR 1 L/E SLAT INBD EDGE FWD LOWER FASTENER SUPPORT FITTING FOUND CRACKED AFTER REMOVAL. LW NR1 L/E SLAT INBD EDGE FWD FASTENER SUPPORT FITTING R & R IAW SRM 51-33-01, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 59,049 hrs · 13,180 cycles

RT WING - OTBD FLAP T/E WEDGE INBD EDGE FOUND DELAMINATION. COMPLIED WITH EA 1-5750-140479.

Part: RIB — CRACKED (LE SLAT) · airframe 59,049 hrs · 13,180 cycles

LT WING - NR 1 L/E SLAT INBD EDGE RIB FOUND CRACKED. LT WING NR1 L/E SLAT INBD EDGE RIB FABRICATED IAW DWG ARB 7128 REV L. RIB R & R IAW SRM 51-53-01, REV 43, LT NR1 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-20-5, REV 66. FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CRACKED (ZONE 500) · airframe 59,049 hrs · 13,180 cycles

LT WING - L/E LOWER ACCESS PANEL 519CB CUT-OUT FWN INBD CORNER FOUND CRACK. LT WING L/E LOWER ACCESS PNL 519CB CUTOUT FWD INBD CRACK CORNER TRIMMED OFF AND REPAIR CARRIED OUT IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — DENTED (RT WING) · airframe 59,049 hrs · 13,180 cycles

RT WING - NR 4 SLAT L/E SURFACE FOUND DENT. RT WING NR 4 SLAT L/E SURFACE DENT EVALUATED AND FOUND WITHIN LIMIT IAW SRM 57-40-02, FIG 201. REPAIR G REV. 43. DEPTH OF DENT 0.032" DIA. OF DENT 1" AFFIXED A CLEAR DOT ADJACENT TO THE DENT AREA IAW GMM 6-3-101, REV 110.

Part: SKIN — CRACKED (ZONE 600) · airframe 59,049 hrs · 13,180 cycles

RT WING - NR 6 L/E SLAT INBD TRACK CUT-OUT OTBD CORNER FOUND CRACKED. RT WING L/E SLAT NR6 INBD TRACK CUTOUT OTBD CRACK CORNER TRIMMED OFF AND REPAIR CARRIED OUT IAW ARM 57-40-02, FIG 201, REPAIR 7, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: VANE — DELAMINATED (TE FLAP) · airframe 59,049 hrs · 13,180 cycles

RT WING - INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. RT WING INBD FLAP VANE R & R IAW AMM 27-50-22-4, REV 66. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5, REV 66 FOUND SATISFACTORY.

Part: VALVE — FAILED (THRUST REVERSER) · airframe 58,091 hrs · 12,938 cycles

REV 3 PRESS FAULT ON T/O REJECTED T/O AT 60KT. PERFORMED HI-POWER RUN IAW JRH, REV 3 PRESS FAULT APPEARED BEFORE 80 PERCENT. SUSPECT NR 3 PRESS REG SHUTOFF VALVE AT FAULT. SWAPPED NR1 AND NR3 PRESS REG SHUTOFF VALVE FOR T/S PURPOSE AND PERFORMED HI-POWER RUN IAW JRH. PROBLEM TRANSFERRED TO NR1. SWAPPED BACK TO ORIGINAL POSITION IAW MM78-31-07-4. NR1 AND NR3 TR OPS CHECK REQUIRE AFTER REPLACE NR3 PRESS REG SHUTOFF VALVE. ENGINES RAN BY 562898. REMOVED AND REPLACED NR 3 T/R PRESS REG S/O VALVE AND PERFORMED NR 1 & NR 3 T/R OPS C'K BY APU AIR IAW MM78-31-07-4. ALL TEST PASSED. RAN NR1 & NR 3 HI PWR ENG RUN IAW JRH. ALL INDICATION NML. CLOSE AND SECURED BOTH ENG COWL IAW MM 71-10-00-2. ACFT OK FOR SVC.

Part: TIRE — FAILED (MLG) · airframe 55,646 hrs · 12,423 cycles

JUST PRIOR TO ROTATION NR 1 TIRE FAILURE. REMOVED AND REPLACED NR 1 AND 2 MAIN WHEEL ASSY AS PER MM 32-41-01-4. VISUAL INSP NR 1 BRAKE ASSY CONDITION GOOD AS PER 32-43-00. ANTI-SKID SYSTEM RTS AS PER MM 32-45-00-5, SPIN CHECK ON EACH BRAKE SYSTEM ALL RELEASED NORMALLY WHILE TRANDUCER TURNED. FOR PRECAUTION DEACTIVED NR 1 BRAKE ASSY AS REF WRI 32-43/4269. VISUAL INSP NR 2 ENGINE, VERIFIED NO FOD DAMAGE COWLING AND FAN. EMPANAGE SECTION, ELEVATORS & RUDDER AREA CHECK CONDITION GOOD. TRAILING EAGE FLAPS INSPECTION WITH FULLY EXTEND, ALL CONDIONS GOOD. LT MLG AREA, MLG DOOR & STRUCT DOOR CHECK ALL GOOD. ACFT OK FOR CONTINUE SERVICE.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 53,973 hrs · 12,076 cycles

HFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK ON LEFT SIDE RADIUS OF LOWER FORWARD SPAR CAP AT LOWER VERTICAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

CRACK INDICATION FOUND ON STA 6-100 AFT SIDE LONGERON 1R OUTBOARD FLANGE APPROXIMATELY 2 INCHES LONG IMAGE ON X-RAY FILM. REPAIRED AS PER SRM 53-10-00. LONGERON REWORKED AS PER DRAWING AEA7476. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

MAIN DECK SEAT TRACK BETWEEN STA 1119 TO 6-10 LBL 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 53,973 hrs · 12,076 cycles

DURING HFEC INSPECTION CARRIED OUT AT LEFT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM-OUT, FOUND LONGERON CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01. FABRICATED LONGERON AS PER EA 1-5310-123111, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

MAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE AT APPROXIMATELY STA 5-75 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

MAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE FOUND CORRODED AT APPROXIMATELY STA 5-87. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

MAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE FOUND CORRODED BETWEEN STA 5-11 AND STA 5-53. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 53,973 hrs · 12,076 cycles

RIGHT WING, INBOARD FLAP VANE LOWER OUTBOARD HALF FOUND DELAMINATION, APPROXIMATELY 7 INCH BY 37 INCH. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 FOUND 'SATISFACTORY'. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 53,973 hrs · 12,076 cycles

HFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK INDICATION ON RIGHT SIDE RADIUS OF LOWER SPAR CAP AT LOWER VERTICAL STABILIZER. REPAIRED AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 53,973 hrs · 12,076 cycles

HFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK INDICATION ON ONE FASTENER TO EDGE OF LEFT LOWER FORWARD SPAR CAP FORWARD FLANGE AT LOWER VERTICAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 53,973 hrs · 12,076 cycles

DURING HFEC INSPECTION CARRIED OUT AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM-OUT FOUND LONGERON CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01. LONGERON FABRICATED AS PER EA 1-5310-123112, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

MAIN DECK SEAT TRACK BETWEEN STA 5-73 TO 5-93 RBL 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENTAS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES A, B AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 53,973 hrs · 12,076 cycles

DURING HFEC INSPECTION, FOUND 14 FASTENER HOLES WITH CRACK INDICATIONS AT RIGHT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT BETWEEN XORS 683.400 AND 713.600. REPAIRED AS PER EA 1-5710-122560, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 53,973 hrs · 12,076 cycles

DURING HFEC INSPECTION, FOUND 11 FASTENER HOLES WITH CRACK INDICATIONS AT LEFT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIRED AS PER EA 1-5710-122559, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATIONS AT HOLES A AND D. CARRIED OUT REPAIR AS PER SRM 53-50-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

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

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

DURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT ON FITTING HOLES A, B, C AND D AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

MAIN DECK, SEAT TRACK BETWEEN STA 1521 - 5-73 LBL, 65 FOUND CORRODED. MAIN DECK CORRODED SEAT TRACK BETWEEN STA 5-0 TO 5-73 LBL 65 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

DURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR ON FITTING CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,973 hrs · 12,076 cycles

DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK DOOR LOWER JAMB NR 4 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. FITTING HOLES CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 100) · airframe 53,973 hrs · 12,076 cycles

NOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. NOSE LANDING GEAR RT TRUNNION FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS.

Part: TRUNNION — CRACKED (ZONE 100) · airframe 53,973 hrs · 12,076 cycles

NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. NOSE LANDING GEAR LT TRUNNION FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS.

Part: WEB — CORRODED (ZONE 200) · airframe 49,192 hrs · 11,066 cycles

FOUND UPPER CARGO DOOR CUTOUT, LOWER SILL'S WEB CORRODED AT STA 660. [SUP 05-22-07] REPAIR CARRIED OUT AT UPPER CARGO DOOR CUTOUT, LOWER SILL'S WEB, STA 660 AS PER FEDEX EA 1-5310-111100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,192 hrs · 11,066 cycles

FOUND UPPER CARGO COMPARTMENT, SEAT TRACK AT LBL 8.5 CORRODED AT STA 1299. [SUP 05-21-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SPAR CAP — CORRODED (RT WING) · airframe 49,192 hrs · 11,066 cycles

RIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1042. [SUP 05-22-07] REPAIRED AS PER FEDEX EA 1-5710-111099.

Part: SKIN — CRACKED (RT WING) · airframe 49,192 hrs · 11,066 cycles

RIGHT WING, LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER FOUND 5/8 INCH CRACK AT XOS 607. [SUP 05-22-07] REPAIR CARRIED OUT AT RIGHT WING - LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER, XOS 607 AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: DUCT — DISCONNECTED (A/C BAY) · airframe 48,529 hrs · 10,898 cycles

INTERMITTENT LEVEL 3 APU FIRE ALERT AFTER 150 EN ROUTE-SUSPECTED BLEED/DUCT LEAK-COMPLIED W/QRH, BOTTLE BLOWN. FOUND FLEX DUCT AT EXHAUST DISCONNECTED AND CLAMP MISSING, DUCT COMES FROM THE GEN COOLING SHROUD. RAN APU FOUND AIR LEAKING AT PRESS REG VALVE CLAMP, TIGHTENED CLAMP. RAN NR 2 ENG AND COULD HEAR A MASSIVE AIR LEAK RUMBLE, WITH ENG RUNNING SHUT DOWN APU AND FOUND AT THE FORWARD FIREWALL THE NR 2/APU MANIFOLD LEAKING AT THE CLAMP. TIGHTENED CLAMP AND AIR LEAK STOPPED. CLAMP WAS EXTREMELY LOOSE. ALL OTHER CLAMPS AND CONNECTIONS LEAK CHECK GOOD. SAFETIED THE FIRE BOTTLES ELE CONNECTIONS AND SQUIBS. SYSTEM OK FOR SERVICE.

Part: DUCT — DISCONNECTED (A/C BAY) · airframe 48,529 hrs · 10,898 cycles

INTMT LVL 3 APU FIRE ALERT AFTER 1 50, EN ROUTE-SUSPECTED BLEED/DUCT LEAK COMPLIED W/QRH, BOTTLE BLOWN INSTALLED SERVICEABLE FIREX CONTAINER AND CARTRIDGE IN THE NR 1 POSITION AND REINSTALLED FIREX CONTAINER IN THE NR 2 POSITION IN REF FOUND FLEX DUCT AT EXHAUST DISCONNECTED AND CLAMP MISSING. RAN APU FOUND AIR LEAKING AT PRESS REG VALVE CLAMP, TIGHTENED CLAMP. RAN NR 2 ENG AND COULD HEAR A MASSIVE AIR LEAK RUMBLE, WITH ENG RUNNING SHUT DOWN APU AND FOUND AT THE FORWARD FIREWALL THE NR 2/APU MANIFOLD LEAKING AT THE CLAMP. TIGHTENED CLAMP AND AIR LEAK STOPPED. CLAMP WAS EXTREMELY LOOSE. ALL OTHER CLAMPS AND CONNECTIONS LEAK CHECK GOOD.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 44,356 hrs · 9,977 cycles

SNRM N0596: RH WING OUTBD FLAP AFT INBD HINGE BRACKET FWD OUTBD AFT ATTACH HOLE FOUND WITH CORROSION. CORRECTIVE ACTION: SNRM N0596: RIGHT HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS.

Part: FLAP — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,356 hrs · 9,977 cycles

SNRM N0963: LH OUTBD FLAP AFT INBD HINGE BRACKET ATTACH FITTING INBD CENTER BORE FOUND CORRODED. CORRECTIVE ACTION: SNRM N0963: LEFT HAND WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS.

Part: SKIN — CORRODED (TE FLAP) · airframe 44,356 hrs · 9,977 cycles

SNRM N1008: CRACK FOUND AT RH WING OUTBD FLAP LOWER FASTENER HOLE COMMON TO ARC 4009 SUPPORT FITTING LOCATED AT THE #2 HOLE FROM INBD DURING HFEC INSPECTION. CORRECTIVE ACTION: SNRM N1008: RIGH HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS.

Part: SUPPORT FITTING — CORRODED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

CRACK FOUND AT LT WING OUTBD FLAP LOWER FASTENER HOLE COMMON TO ARC 4009 SUPPORT FITTING LOCATED AT THE MOST OUTBD HOLE DURING HFEC INSPECTION. LT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 44,356 hrs · 9,977 cycles

LT WING OUTBD FLAP INBOARD HINGE BRACKET OUTBD CENTER ATTACH HOLE FOUND CORRODED. LT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS.

Part: HINGE — WORN (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL DOOR AFT HINGE FOUND WORN. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: HINGE — WORN (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

LEFT MAIN LANDING GEAR WHEEL WELL DOOR AFT HINGE FOUND WORN. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

FOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90057.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

FOUND LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING MOST AFT BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90059.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

FOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING MOST AFT BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90058.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

FOUND LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90056.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

RIGHT FIXED LEADING EDGE INTERIOR BEADED DOUBLER FOUND CRACKED AT XORS663. REPAIRED AS PER FEDEX EA 1-5730-90044

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,356 hrs · 9,977 cycles

FOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STA 5/0 - 5/73, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,356 hrs · 9,977 cycles

FOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STA 1521, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG. 3 VOL. I AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,356 hrs · 9,977 cycles

FOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND EDGE DAMAGED AT STA 5/23, X= -47.5. REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT HAND WING, END OF STRINGER 41. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,356 hrs · 9,977 cycles

MAIN DECK COMPARTMENT, SEAT TRACK EDGE FOUND WORN AT STATION 755, X=-8.5. CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I AND SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 12. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,356 hrs · 9,977 cycles

MAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STATION 5/0- 5/73, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 9.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 10.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK AT RIGHT WING, END OF STRINGER 44 APPROXIMATELY 2 INCHES.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 11. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90051.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 9.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION FOUND CRACK AT RIGHT WING, END OF STRINGER 14 APPROXIMATELY 14 INCHES. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90053

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 43. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 10. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 44 APPROXIMATELY 1/2 INCH. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 11.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK AT RIGHT WING, END OF STRINGER 12 APPROXIMATELY 13.25 INCHES. REPAIR CARRIED OUT IAW SRM 57-20-00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90052.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,356 hrs · 9,977 cycles

DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 14 APPROXIMATELY 13 INCHES. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. CLIP FABRICATION CARRIED OUT AS PER FEDEX E.A. 1-5720-90050 (TITLE: WINGS - STRINGER 14L REPAIR PER SRM VOL. I 57-20-00 FIG. 10 -FX ARB2689-502 CLIP FABRICATION). REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 43,448 hrs · 9,800 cycles

ON FINAL APPROACH GOT FLAP DISAG ALERT WHILE EXTENDING FLAPS FROM 35 TO 50. RETURNED FLAPS TO 35 AND ALERT CLEARED MOMENTARILY THEN CAME BACK ON, MISSED APPROACH ACCOMPLISHED AND RAN QRH PROCEDURES. ABLE TO RETURN FLAPS TO 35/EXT WITH NO ALERTS. NORMAL APPROACH AND LANDING ACCOMPLISHED. REMOVED AND REPLACED XMTR INBOARD FLAP RT POS. AS PER MD11 MM 27-54-04, OPS CHECK SATIS.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RIGHT OUTBOARD FLAP, OUTBOARD HINGE (FLAP SIDE) AFT MOUNTING AREA FORWARD HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.610. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

FORWARD CABIN SEAT TRACK AT STA 495 APRROXIMATELY 27.5 CORRODED. REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I. NEW SET TRACK TRIMMED, REWORKED AND REPAIR PARTS INSTALLED PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 39,607 hrs · 8,945 cycles

CENTER CARGO BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R CRACKED. LONGERON SPLICE 48R REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DWG: A5A7124, INSTALLED PER SRM 51-33-01 VOLUME II AND PART MARKED FX A5A7124-1 PER GMM 7-0-1001.

Part: PRESSURE PANEL — CANNING (ZONE 100) · airframe 39,607 hrs · 8,945 cycles

FUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1. FEDEX EA NR 1-5330-76794 WAS ISSUED FOR TRACKING AND REPETITIVE INSPECTION

Part: FITTING — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORRODED. RT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2 - 4. ORIGINAL DIAMETER = 0.8755 INCH, FINAL DIAMETER = 0.882 INCH, MAXIMUM ALLOWABLE DIAMETER = 0.8755 INCH. EXCEEDED LIMITS PER EO NR 1-5750-7-5005A PART 2, INSPECT/ MODIFY INBOARD FLAP VANE ATTACHING FITTINGS SB MD11-57-034 AND MD 11-57-065 (RT WING) COMPLIED WITH FEDEX EA NR 1-5750-76788, WINGS, RIGHT INBOARD FLAP VANE, TEE FITTING CORRODED.

Part: FITTING — CRACKED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, OUTBOARD FLAP ATTACHING RIB STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II.

Part: PRESSURE PANEL — CANNING (ZONE 100) · airframe 39,607 hrs · 8,945 cycles

FUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1. FEDEX EA NR 1-5330-76794 WAS ISSUED FOR TRACKING AND REPETITIVE INSPECTION.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 1059 - 1065, LBL 47.5 FOUND DAMAGED. MAIN DECK, SEAT TRACK FROM STA 1049 TO STA 1129 LBL 47.5 REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. REPAIR PARTS AND FABRICATED SEAT TRACK INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND 51-31-01 VOLUME II.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LT WING OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER:1.093; FINAL DIAMETER: 1.096 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.504; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.502 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.406; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

FWD CABIN - SEAT TRACK AT STA 635, LBL 47.5 FOUND CRACKED AT THE BOTTOM SIDE. FWD CABIN - SEAT TRACK AT STA 635, LBL 47.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN CABIN, SEAT TRACK AT STA 775, APPROXIMATELY LBL 8.5 CROWN WORN. MAIN CABIN, SEAT TRACK AT STA 745 TO STA 785, LBL 8.5. REMOVED PER SRM 51-33-01 VOLUME I. NEW SEAT TRACK SPLICE FABRICATED AND INSTALLED PER SRM 53- 70-00 FIGURE 1 VOLUME I AND SRM 51-33-01 VOLUME II.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.020; REMAINING THICKNESS: 0.486 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

FWD CABIN, SEAT TRACK AT STA 465 - 495, APPROXIMATELY LBL 58 CORRODED. FWD CABIN, SEAT TRACK AT STA 465 TO STA 495, LBL 58 CUT AND REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-33-01 VOLUME II.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.408; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062"; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.222 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.217 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 1119, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 1049 TO 1129, LBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 51-21-01 VOLUME II. REPAIR PARTS INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.415 INCH; MATERIAL REMOVED 0.011 INCH; REMAINING THICKNESS: 0.404 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SEAT TRACK CROWN AT STA 1129, RBL 28 FOUND WITH GOUGED MARK. MAIN DECK - SEAT TRACK FROM STA 1129 TO 7 - 0, RBL 28 REMOVED AS PER SRM 51-31-01 VOLUME 2. SEAT TRACK REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REWORKED TRACK INSTALLED AS PER 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME 2.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SEAT TRACK CROWN AT STA 6-80, RBL 47.5 FOUND DAMAGED. MAIN DECK - DAMAGED SEAT TRACK AT STA 6-80, RBL 47.5 REMOVED FROM STA 1129 TO STA 7-0 RBL 4.75 AND REPLACED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME 2.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SEAT TRACK CROWN AT STA 6-20, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 6-20, RBL 47.5 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME 2.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.414 INCH; MATERIAL REMOVED 0.005 INCH; REMAINING THICKNESS: 0.409 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.399; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.395 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.222 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 6-80, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 6-40 TO STA 7-0, LBL 47.5 CUT AND REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS INSTALLED AS PER SRM 51-31-01 VOLUME II AND 53-70-00 FIGURE 1 VOLUME I.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.514 INCH; MATERIAL REMOVED 0.004 INCH; REMAINING THICKNESS: 0.510" AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093", FINAL DIAMETER = 1.127. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 870 - STA 890, RBL 47.5 FOUND DAMAGED. MAIN DECK, SEAT TRACK FROM STA 850 TO STA 950, RBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SEAT TRACK CROWN AT STA 1090, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 999 TO STA 1129, RBL 47.5 REPLACED PER SRM 53-70-00 FIGURE 1 VOLUME I AND PER 51-31-01 VOLUME 2.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.495; MATERIAL REMOVED 0.032"; REMAINING THICKNESS: 0.463 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.410 INCH, MATERIAL REMOVED=0.005 INCH, REMAINING THICKNESS=0.405 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

SEAT TRACK CROWN AT STA 1171, LBL 47.5 FOUND WORN. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.470 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.468 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.495 INCH, MATERIAL REMOVED=0.003 INCH, REMAINING THICKNESS=0.492 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.254 INCH, AND REPAIRED AS PER EA NR 1-5750-76787, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.248 INCH, AND REPAIRED AS PER EA NR 1-5750-76787, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 0.323 INCH, FINAL DIAMETER= 0.409 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.130 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.195. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.093 INCH; FINAL DIAMETER: 1.147 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.217 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCH. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SEAT TRACK CROWN AT STA 1795 - 1815, RBL 27.5 FOUND DAMAGED. MAIN DECK AT STA 1795 - 1815, RBL 27.5, SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SEAT TRACK CROWN AT STA 1251, LBL 47.5 FOUND WITH GOUGED MARK. MAIN DECK - DAMAGED SEAT TRACK CROWN AT STA 1251, LBL 47.5 REMOVED FROM STA 1268 TO 7 - 0 LBL 47.5 PER SRM 53-70-00 FIGURE 1 VOLUME I AND 51-31-01 VOLUME 2. REPAIR PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-30-00 VOLUME 2.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.460 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.458 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0503.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.126 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.217 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: SPLICE — CRACKED (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SPLICE FITTING AT RT STA 1531 LONGERON 14 CRACKED. MAIN DECK - SPLICE FITTING AT RT STA 1531 LONGERON 14 REMOVED AS PER SRM 51-31-01 VOLUME 2. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7112 AND INSTALLED AS PER SRM 51-31-01 VOLUME 2.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SEAT TRACK CROWN AT STA 1020, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 999 TO STA 1129, RBL 47.5 REPLACED PER SRM 53-70-00 FIGURE 1 VOLUME I AND PER 51-31-01 VOLUME 2.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 INCH, FINAL DIAMETER = 1.127 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK - SEAT TRACK CROWN AT STA 1801, RBL 27.5 FOUND DAMAGED. MAIN DECK AT STA 1801, RBL 27.5 SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.404 INCH, MATERIAL REMOVED = 0.002 INCH, REMAINING THICKNESS = 0.402 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.405 INCH, MATERIAL REMOVED = 0.003 INCH, REMAINING THICKNESS = 0.402 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.196. COMPLIED WITH FEDEX EA# 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. LEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.326 INCH, AND REPAIRED AS PER EA 1-5750-76787, TITLE: WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RIGHT WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.504 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.407; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.405 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.224 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

MAIN DECK, SEAT TRACK CROWN AT STA 1090, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 1049 TO 1129, LBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 51-21-01 VOLUME II. REPAIR PARTS INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.470 INCH, MATERIAL REMOVED=0.016 INCH, REMAINING THICKNESS=0.454 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.380 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.378 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 2.256 INCH, FINAL DIAMETER=2.329 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 0.516 INCH, FINAL DIAMETER= 0.596 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.218 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.219 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.248 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 39,607 hrs · 8,945 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.343 INCH, MATERIAL REMOVED=0.038 INCH, REMAINING THICKNESS=0.305 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: SPLICE — CRACKED (ZONE 200) · airframe 39,607 hrs · 8,945 cycles

CTR CARGO, BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R CRACKED. CTR CARGO, BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R. REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DWG: A5A7124, INSTALLED PER SRM 51-33-01 VOLUME II AND PART MARKED FX A5A7124-1 PER GMM 7-0-1001.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.497 INCH, MATERIAL REMOVED = 0.010 INCH, REMAINING THICKNESS = 0.487 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.505 INCH, MATERIAL REMOVED = 0.003 INCH, REMAINING THICKNESS = 0.502 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.482 INCH; MATERIAL REMOVED 0.006 INCH; REMAINING THICKNESS: 0.476 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: SUPPORT FITTING — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE REPAIRED PER FEDEX EA NR 1-5750-76755, WINGS, RIGHT OUTBOARD FLAP, SUPPORTS CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.443, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED

Part: HINGE — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.628. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED.

Part: FITTING — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING, THREE (3) HOLES FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING CORROSION REMOVED AS PER SRM 51-21-00 VOLUME II. (1) OUTBOARD MIDDLE HOLE: ORIGINAL DIAMETER = 0.583 INCH, FINAL DIAMETER = 0.653 INCH, (2) INBOARD FORWARD HOLE: ORIGINAL DIAMETER = 0.567 INCH, FINAL DIAMETER = 0.630 INCH (3) OUTBOARD FORWARD HOLE: ORIGINAL DIAMETER = 0.630 INCH, FINAL DIAMETER = 0.699 INCH COMPLIED WITH FEDEX EA NR 1-5750-76755, WINGS, RIGHT OUTBOARD FLAP, SUPPORTS CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.458, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED

Part: HINGE — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.620. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RT OUTBOARD FLAP - SUPPORTS CORRODED

Part: HINGE — CORRODED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.656. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED.

Part: RIB — CRACKED (ZONE 600) · airframe 39,607 hrs · 8,945 cycles

RIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING CRACKED. RIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: COALESCER BAG — DAMAGED (AIR DISTRIBUTION) · airframe 37,450 hrs · 8,481 cycles

DEPARTED CDG, ENGINE ANTI-ICE ON MAX PWR AT 3000 AGL SMOKE ODOR DETECTED THEN SMOKE ENTERED THE COCKPIT TURNED ON THE LIGHTS AND THE COCKPIT HAUL FILLED WITH SMOKE. WENT ON OXYGEN, RAN APPROPIATE CHECKLISTS. RAN NR 1 ENG FOR 20 MIN AND HAD A VERY LITE ODOR. PRECAUTIONARY DEFERRED NR 1 PNEU SUPPLY. ALSO CHANGED ALL 3 COALESCER BAGS PER MM 21-54-05-2. ALL 3 FOUND BLACK.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,645 hrs · 7,672 cycles

MAIN CABIN, SEAT TRACK DAMAGED AT FS 1350.5 X=-47.50. TRIMMED OUT DAMAGED SEAT TRACK IAW SRM. FABRICATED SEAT TRACK AND SPLICE HAT IAW SRM. INSTALLED SEAT TRACK AND SPLICE HAT IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,645 hrs · 7,672 cycles

MAIN DECK CARGO COMPARTMENT, RIGHT FUSELAGE FRAME, BS Y 1139-1159, STRINGER 17, CRACKED. R/R MDCC RT FUSELAGE FRAME BS Y 1139-1159 STRINGER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,645 hrs · 7,672 cycles

MDCC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 585, 685 X -75.25. TRIMMED OUT DAMAGED AREA ON SEAT TRACK FLANGE IAW SRM, FABRICATED FILLER AND STRAP IAW SRM. INSTALLED FILLER AND STRAP IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,645 hrs · 7,672 cycles

MDCC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 585 - 685, X=-107.25. TRIMMED DAMAGED AREA ON FLANGE AT STA 653 RBL 107.25 IAW SRM. FABRICATED FILLER AND STRAP IAW SRM. INSTALLED FILLER AND STRAP IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,645 hrs · 7,672 cycles

MDCC FUSELAGE FRAME STA 1139-1159, STRINGER 17R, FOUND WITH CRACK.

Part: STRAP — CORRODED (FUSELAGE) · airframe 33,645 hrs · 7,672 cycles

MDCC LT FUSELAGE FRAME STA Y 1199 STR 16 FOUND TIE STRAP WITH CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,645 hrs · 7,672 cycles

MDCC FLOOR SEAT TRACK FLANGE FOUND WITH CORROSION AT STA 1521, LBL 8. TRIMMED CORRODED FLANGE AT STA 1521, LBL 8 IAW SRM. NON DESTRUCTIVE TESTING CARRIED OUT AT TRIMMED AREA IAW DAC NDT SPM. FAB FILLER AND STRAP IAW SRM. INSTALLED IAW SRM.

Part: RIB — CRACKED (L/E SLAT) · airframe 33,645 hrs · 7,672 cycles

LT WING L/E SLAT TRACK NR 16 I/B STRUCTURAL RIB FOUND CRACKED APPROX 0.125 INCH.

Part: RIB — CRACKED (RT WING SLAT) · airframe 33,645 hrs · 7,672 cycles

RIGHT WING LEADING EDGE SLAT TRACK NR 16 INBOARD STRUCTURAL RIB FOUND CRACKED APPROXIMATELY (0.125).

Part: BOLT — LOOSE (LANDING GEAR)

DURING PFM NR 61 B-CK FOUND BOTH LT & RT AFT MOUNTING BOLT OF CTR LANDING GEAR TRUNNION PIN PILLOW BLOCK LOOSE.

Part: SEAT TRACK — CRACKED (UPPER CARGO BAY) · airframe 25,020 hrs · 5,789 cycles

CABIN MAIN DECK CARGO SEAT TRACK FLANGE FOUND CRACKED ALONG BS 755, RBL 9. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III & 53-70-00 VOL I.

Part: SEAT TRACK — CRACKED (UPPER CARGO BAY) · airframe 25,020 hrs · 5,789 cycles

CABIN MAIN DECK CARGO SEAT TRACK FLANGE FOUND CRACKED ALONG BS 7552 LBL 28. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III & 53-70-00 VOL I.

Part: SEAT TRACK — CRACKED (UPPER CARGO BAY) · airframe 25,020 hrs · 5,789 cycles

CABIN MAIN DECK CARGO SEAT TRACK FLANGE AREA FOUND CRACKED ALONG LBL 47, BETWEEN BS 925 & 935. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III & 53-70-00 VOL I.

Part: SEAT TRACK — CRACKED (UPPER CARGO BAY) · airframe 25,020 hrs · 5,789 cycles

CABIN MAIN DECK CARGO SEAT TRACK FLANGE AREA FOUND CRACKED ALONG BS 755, LBL 9. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III & SRM 53-70-00 VOL I.

Part: SEAT TRACK — CRACKED (UPPER CARGO BAY) · airframe 25,020 hrs · 5,789 cycles

CABIN MAIN DECK CARGO SEAT TRACK FLANGE FOUND CRACKED ALONG BS 755, LBL 47. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III.

Part: SEAT TRACK — CRACKED (UPPER CARGO BAY) · airframe 25,020 hrs · 5,789 cycles

CABIN MAIN DECK CARGO SEAT TRACK FLANGE FOUND CRACKED AT 2 PLACES, ALONG RBL 45, BETWEEN BS 969 & 999. *S/D* REMOVED AND REPLACED PER 53-42-01 VOL III & 53-70-00 VOL I.

Part: RELAY — FAILED (AILERONS)

LEVEL 2 ALERT IN-FLT AILERON DEFLECT DISAGREE. *S/D* REMOVED AND REPLACED RELAY R2-5060 PER SMP. REMOVED AND REPLACED FLAP HANDLE POS TRANSMITTER PER MD-11 MM 27-54-03. OPS CK OK.

Part: WIRE — DAMAGED (EXTERNAL POWER)

SNRM 322,444,321 - FWD CARGO EXTERNAL PWR CABLE NR C507-3-OC (AL), FOUND INSULATION BREAKDOWN AND OH SIGN (ARCING) AT BS 899, LBL 20 BELOW FLOORBOARD. INSULATION BLANKET AT BILGE AREA BURNT. REMOVED AND REPLACED EXT PWR SYS OPER CK FOUND SATISFACTORY PER 24-40-00-2. SERVICEABLE ITEM ROBBED FROM N590FE. FWD CARGO COMPT AT BILGE REPLACED PER MM 25-85-01-4 AND SUMP PANEL AFT EDGE REPAIRED SRM 53-00-01 VOL 1.

Part: SEAT TRACK — CRACKED (CARGO COMPT)

FOUND CRACK ON SEAT TRACK. SEAT TRACK SPLICE CUT AND REWORKED PER SRM 53-42-01.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

AIL DEFLECT DISAG LVL 2 ALERT ON FLAP RETRACTION, STAYED ON SLAT RETRACTION, GOES AWAY WHEN FLAPS EXT FOR LANDING. A/C RELEASED FOR SERV PER MEL/CDL 27-2 CATEGORY C EXP 4APR99 FCC1-FCC2 REPT NO FAULTS LAST LEG. PERF'D FCC1/FCC2 AIL SYS TEST PER MM 22-00-00-840-801. ALL TESTS PASSED. CONFIRMED CORRECT AIL IND ON CONFIG PG ON FLAP EXT/RET AND INBD AIL FAIRED AND OUTBD DROOP NEUTRAL PER THE AIL NEUTRAL POS PLACARD (MM 27-10-00-5) C/W MSP 27-2 METHOD A PULLED AND TAGGED C/B A-07. A/C OK FOR SERVICE.

Part: BULKHEAD DOUBLER — CRACKED (CENTER MLG WW)

CENTER L/G, RT BULKHEAD DRAG LINK SUPPORT WEB DOUBLER IS CRACKED AFT RT DRAG LINK ATTACH POINT, VERIFIED BY NDT. REMOVED AND REPLACED SUPPORT WEB DOUBLER PER SRM 51-00-01 VOL II.

Part: BULKHEAD DOUBLER — CRACKED (CENTER MLG)

N 00081, CENTER L/G, RT BULKHEAD DRAG LINK SUPPORT WEB DOUBLER IS CRACKED AFT RT DRAG LINK ATTACH POINT. VERIFIED BY NDT. *S/D* REMOVED AND REPLACED SUPPORT WEB DOUBLER PER SRM 51-00-01 VOL II. REPAIR COMPLIED WITH ON 03-06-1997.

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO COMPT)

APPROACHING NRT, CARGO FIRE LOWER AFT ALERT DISPLAYED, AGENT DISCHARGED IAW PROCEDURE. AFTER LANDING NO INDICATION OF FIRE OBSERVED. ALERT OCCURRED AT 3,000 FEET, CARGO TEMPERTURE NORMAL. FOUND NO FAULTS ON CURRENT AND FAULT REVIEW IN MSC AND DEU 1, 2, 3. CHECKED ALL SMOKE DETECTOR AND OVERHEAT DETECTOR, FOUND NORMAL. REMOVED AND REPLACED NR 1 CARGO FIRE CONTAINER PER MM 26-22-01. PRECAUTIONARY REMOVED AND REPLACED MSC PER M/M 31-42-01, RTS PASSED. REMOVED AND REPLACED NR 3 AFT CARGO SMOKE DETECTOR PER MM 26-14-01, FUNCTION TEST GOOD.

Part: HARNESS — CHAFED (NR 1 ENGINE)

NR 1 ENG ELECTRICAL HARNESS, BLACK AT THE SIX O'CLOCK POSITION IS CHAFING HARD AGAINST TRAIN LINES THROUGH THE COATING AND WIRE MESH. REMOVED AND REPLACED CABLE (P/N 7161M60G04) INSTALLED PER MM 71-50-04-4-1. PERFORMED POWER ASSURANCE RUN REQUIRED PER MM 71-50-04-4-1 AND INSTALLED PER MM 70-10-00-2-1.

Part: HARNESS — CHAFED (NR 1 ENGINE)

NR 1 ENG ELECTRICAL HARNESS, BROWN AT THE SIX O'CLOCK POSITION IS CHAFING HARD AGAINST DRAW LINES THROUGH COATING AND WIRE MESH. REMOVED AND REPLACED ELECTRICAL HARNESS (P/N 7161M661G03), COMPLIED WITH EO 1-7520-7-3304 ON NEW HARNESS (P/N 1821M62G03). PERFORMED POWER ASSURANCE ENG RUN PER MM 71-50-04-4-1, ELECTRICAL HARNESS REPLACEMENT PER MM 71-50-04-1-1 AND MM 70-10-00-2-1.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 2 ENGINE)

NRT - CLIMBING THROUGH FL 200, NR 2 FIRE WARNING ILLUMINATED WITH THE THROTTLE PULLED TO IDLE FIRE WARNING LIGHT IN HANDLE AND START SW WENT AWAY, RETURNED RJAA. NR 2 FDCU FAULT REVIEW, UP RIGHT FIRE DET ASSY-A AND LOOP-A FAULT REMOVED WIRE TERMINALS FROM RESPONDER AND CLEAN AND REMOVED DIRTY FOD CLAMPS. NR 2 FDCU R-T-S TEST PASSED PER MM 26-11-02, TOTAL RESISTANCE READS 1,465K OHMS.

Part: DUCT — LEAKING (NR 2 ENGINE)

NR 2 ENG FIRE WARNING ON CLIMBOUT FROM EWR, ALL ENG EGT'S OK, NO OTHER ABNORMAL INDICATIONS ON NR 2 EXCEPT AUDIO/VISUAL FIRE WARNING, PERFORMED ENG FIRE SHUTDOWN CKLIST, DID NOT HAVE TO USE FIRE BOTTLE. REMOVED AND REPLACED NR 2 ENG FCDU, FOUND 11TH STAGE DUCT LEAKING AT CLAMP IN AREA OF RT UPPER LOOP JUNCTION, REPLACED SEALS AND RE-INSTALLED DUCT SECTION. METERED FIRE DETECTION RESPONDERS. ALL SHOW GOOD, A/C OK FOR SERVICE.