N603FE

Part: SKIN — CORRODED (ZONE 600 AILERON) · corrosion level 2 · airframe 92,454 hrs · 22,377 cycles

RIGHT INBD AILERON UPPER SURFACE OUTBOARD SIDE TRAILING EDGE AREA FOUND CORRODED. RIGHT HAND INBOARD AILERON ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-10-20-4. NEUTRAL POSITION ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-10-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

FLOOR PANEL #231HF AT LEFT BS 595 TO 675 SURFACE FOUND DAMAGED. DAMAGED FLOOR PANEL #231HF AT CABIN LEFT HAND STATION 595 TO STATION 675 REMOVED AND REPLACED IAW AMM 53-25-04-4. FLOOR PANEL #231HF FABRICATED AS PER DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (ZONE 800) · airframe 92,454 hrs · 22,377 cycles

CABIN L2 DOOR NR 6 BEAM FORWARD STOP FOUND CRACKED AT BS 794 CRACK LENGTH 1.0". AT L2 DOOR CRACKED NR 6 STOP BEAM. R & R IAW SRM 51-31-01-0G & DRAWING ADA3462, REVISION AC. L2 DOOR NR 6 STOP BEAM FABRICATED BY MACHINING IAW EA 1-5210-T0385415 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 92,454 hrs · 22,377 cycles

RIGHT WING: WING SIDE RIGHT INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA FOUND CORROSION. CORROSION AT RIGHT HAND WING : WING SIDE RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHIING FABRIATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-07 AND EA # 1-5750-T0329456 E PART 4 STEP 2.A AND STEP 2.C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 92,454 hrs · 22,377 cycles

LEFT WING :(FLAP SIDE) LEFT INBOARD FLAP OUTBOARD AFTER HINGE OUTBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT LEFT HAND WING : ( FLAP SIDE ) LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE AREA 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 EA # 1-5750-72646 E PART 6 STEP 2.A AND 2.B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 92,454 hrs · 22,377 cycles

LEFT WING: WING SIDE LEFT INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA FOUND CORRODED. ORROSION AT LEFT HAND WING : WING SIDE LEFT HAND INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR CARRIED OUT AS PER EA # 1-5750-72644 G PART 5 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 92,454 hrs · 22,377 cycles

RIGHT WING :(FLAP SIDE) RIGHT INBOARD FLAP OUTBOARD AFTER HINGE INBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT RIGHT HAND WING : ( FLAP SIDE ) RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE AREA 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 EA # 1-5750-72651 F PART 6 STEP 2.A AND 2.B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 92,454 hrs · 22,377 cycles

LEFT WING:(FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFTER HINGE INBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT LEFT HAND WING ( FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHIING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND EA # 1-5750-72646 E PART 6 STEP 2.A AND 2.B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 92,454 hrs · 22,377 cycles

RIGHT WING :(FLAP SIDE) RIGHT INBOARD FLAP OUTBOARD AFTER HINGE OUTBOARD PIVOT HOLE AREA FOUND CORROSION. CORRROSION AT RIGHR HAND WING: (FLAP SIDE) RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE AREA 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 EA # 1-5750-72651 F PART 6 STEP 2.A AND 2.B. REPAIR CLASIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 92,454 hrs · 22,377 cycles

LEFT WING: (ON WING SIDE), LEFT INBOARD FLAP OUTBOARD FORWARD HINGE PIVOT HOLE SPOTFACE AREA FOUND CORRODED. CORRODED AT LEFT HAND WING : (ON WING SIDE) , LEFT HAND INBOARD FLAP OUTBOARD FORWARD HINGE PIVOT HOLE SPOT FACE AREA REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07.REPAIR WASHER FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-17 AND EA# 1-5750-72644 G PART 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 92,454 hrs · 22,377 cycles

FUSELAGE: #1 AIRCONDITION RAM AIR EXHAUST ASSY CUT OUT PRODUCTION DOUBLER SUSPECT CRACKED. CRACKED DOUBLER AT FUSELAGE #1 AIRCONDITION RAM AIR EXHAUST ASSEMBLY AT LEFT HAND STATION 561.667 REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER MD-11 SRM 51- 35-01-OG. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ACA3850 REVISION AA. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 92,454 hrs · 22,377 cycles

FUSELAGE: #1 AIRCONDITION RAM AIR EXHAUST ASSY CUT OUT PRODUCTION DOUBLER SUSPECT CRACKED. CRACKED DOUBLER AT FUSELAGE #1 AIRCONDITION RAM AIR EXHAUST ASSEMBLY AT LEFT HAND STATION 561.667 REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER MD-11 SRM 51- 35-01-OG. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ACA3850 REVISION AA. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (ZONE 100) · airframe 92,454 hrs · 22,377 cycles

LOWER CENTER CARGO DOOR UPPER DOOR JAMB CENTER BEAM FOUND CRACKED AT BS 1746.925. LOWER CENTER CARGO DOOR UPPER DOOR JAMB CENTER BEAM CRACKED AT STATION 1746.925 REPAIRED AS PER MD-11 SRM 53-50-15-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1401 X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1401, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN FROM STATION 1371 TO STATION 1411 X= -8.5 EXISTING SPLICE AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 879 X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 879 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN STATION 869 TO EXISTING SPLICE STATION 929 X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 879 X= 47.5 FOUND CROWN WORN. SEAT TRACK STATION 879, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN STATION 869 TO EXISTING SPLICE STATION 909 X= 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1661 X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1661 X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM STATION 1651 TO STATION 1691 X= 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 879 X= -27.5 FOUND CROWN WORN. SEAT TRACK STATION 879 X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN STATION 909 TO EXISTING SPLICE STATION 869 X= -27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT BS 1801 X= -8.5 FOUND CROWN WORN. SEAT TRACK BS 1801, X= -8.5 WORN CROWN EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM EXISTING SPLICE BS 1791 TO 1811 X= -8.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK BS 1275 X= 8.5, FOUND THE CROWN WORN. THE SEAT TRACK CROWN WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

CABIN-SEAT TRACK AT STAION 1275 X= -8.5 FOUND CROWN WORN. SEAT TRACK BS 1275 X= -8.5 CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM BS 1264 TO BS 1313 X= -8.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT BS 1275 X= 27.5, FOUND THE CROWN WORN. THE SEAT TRACK CROWN WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1247 TO BS 1331IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

CABIN LEFT HAND FLOOR PANEL 231CF AT BS 495 TO 595 BETWEEN X=27.5 TO X=47.25 ACCESS CUT OUT FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 53-25-04-4. FLOOR PANEL 231CF FABRICATED IAW DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1541 X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 1541 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM EXISTING SPLICES STATION 1531/5-123 TO STATION 1651 X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIRCLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1661 X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1661 X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN BS 1691 TO EXISTING SPLICE STATION 1631 X= 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STAION 1275 X= -27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1275 X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN FROM STATION 1264 TO STATION 1313 X= -27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 5-10 X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 5-10 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN FROM EXISTING SPLICE STATION 1531/5-0 TO STATION 1531/5-63 X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT BS 1421 X= -47.5 FOUND CROWN WORN. SEAT TRACK CROWN EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1661 X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 1661 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM STATION 1651 TO STATION 1691 X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

CABIN-SEAT TRACK AT STAION 1421 X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1421, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN FROM STATION 1391 TO STATION 1431 X= 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1541 X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1541 X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN STATION 1631 TO EXISTING SPLICE STATION 1531/5-123 X= 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIRCLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT BS 1169 X= 47.5 FOUND CROWN WORN. THE SEAT TRACK CROWN WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

LEFT 3 AFT DOOR JAME LOWER WEB AT STATION 1310 FOUND CRACKED. CANIN-LEFT 3 AFT DOOR JAME LOWER WEB AT STATION 1310 CRACKED REPAIR CARRIED OUT AS PER MD-11 SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 919 X= 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 919 X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN FROM EISTING SPLICES STATION 909 TO STATION 989 X= 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIRCLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1169 X= 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1169, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN FROM EXISTING SPLICE STATION 1129/6-100 TO STATION 1229 X= 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 685 X= 27.5 FOUND CRACKED. CRACKED SEAT TRACK AT STATION 695 X= 27.5 REMOVED FROM EXISTING SPLIES STATION 665 TO STATION 745 X=27.5 AS PER MD-11 SRM 51-31-01-0G. CRACKED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM EXISTING SPLICES STATION 665 TO STATION 745 X= 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1169 X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1169 X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN BS 1189 TO 1129/6-100 X= 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK BS 1249 X= 75.25 FOUND THE CROWN WORN. THE SEAT TRACK CROWN WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 1169 - BS 1264, X= 75.25 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

CABIN-SEAT TRACK AT STATION 635 X= -47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 635, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT ON CABIN FROM EXISTING SPLICES STATION 605 TO STATION 645 X= -47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT BS 1169 X= -27.5 FOUND THE CROWN WORN. THE SEAT TRACK CROWN WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE BS 1129 TO BS 1189 IAW SRM 53-00-52-2R, FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 755 X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 755 X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN EXISTING SPLICES STATION 745 TO STATION 825 X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT STATION 1169 X= -8.5 FOUND CROWN WORN. SEAT TRACK CROWN WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT BS 999 X= 47.5, FOUND CROWN WORN. SEAT TRACK CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE BS 989 TO BS 1049, X=47.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON — WORN (ZONE 100) · airframe 92,454 hrs · 22,377 cycles

FUSELAGE: FUSELAGE APPROXIMATEL STATION 583 X= 24 LONGERON SUSPECTED CRACKED. FUSELAGE STATION 583 X= 24 CRACKED LONGERON REMOVED AND REPLACED AS PER MD-11 SRM 51-35-01-0G AND FABRICATED LONGERON PER DOUGLAS DRAWING ACA 3796 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: SPAR CAP — CORRODED (ZONE 600) · airframe 92,454 hrs · 22,377 cycles

RIGHT WING LOCATED BETWEEN OUTBOARD TRAILING EDGE ISLAND AND RIGHT HAND OUTBOARD AILERON, OUTBOARD TRAILING EDGE LOWER CAP XORS 1048 FOUND CORRODED. CORROSION REMOVED & FOUND EXCEEDED LIMIT IAW SRM 57-00-01-1A ALLOWABLE DAMAGE 1. REAR SPAR LOWER CAP CARRIED OUT SECTIONAL REPAIR AS IAW SRM 57-20-10-2R, REPAIR 1, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

CABIN-SEAT TRACK AT STATION 999 X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 999, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT ON CABIN STATION 1049 TO EXISTING SPLICE STATION 989 X= 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

CABIN-SEAT TRACK AT STATION 939 X= 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 939, X= 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT ON CABIN FROM STATION 909 TO EXISTING SPLICE STATION 949 X= 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

FORWARD CARGO COMPARTMENT CEILING CABIN FLOOR SEAT TRACK FOUND CRACKED AT STATION 635 X= -8.5 AS MARKED. FORWARD CARGO COMPARTMENT CEILING CABIN AT STATION 635 X= -8.5 CRACKED SEAT TRACK REMOVED AS PER MD-11 SRM 51-31-01-0G, FROM EXISTING SPLICES STATION 625 TO STATION 665 X= -8.5. CARCKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT CABIN FROM EXISTING SPLICES STATION 625 TO STATION 665 X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

CABIN SEAT TRACK AT STATION 1019 X= -47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1019, X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT ON CABIN FROM EXISTING SPLICES STATION 949 TO STATION 1067 X= -47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

CABIN SEAT TRACK AT STAATION 1005 X= -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1005, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT ON CABIN FROM STATION 929 TO STATION 1029 X= -8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT BS 1073 X= -47.5 FOUND CROWN WORN. WORN CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. CROWN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICES BS 1069 TO BS 1129/6-0, X= -47.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 600 AILERON) · airframe 92,454 hrs · 22,377 cycles

RIGHT INBOARD AILERON UPPER SURFACE OUTBOARD SIDE TRAILING EDGE AREA FOUND CORRODED. RIGHT HAND INBOARD AILERON ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-10-20-4. NEUTRAL POSITION ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-10-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SDR TRACKING NUMBER # 25-2117 FOR DETAILS.

Part: TRUNNION — CRACKED (ZONE 100) · airframe 92,454 hrs · 22,377 cycles

DURING HFEC INSTPECTION ON EXISTING SLOT OUT AREA ON THE LEFT NOSE LANDING GEAR TRUNION FITTING AT APPROIMATELY STATION 580 AND FOUND 01EA CRACK PROPAGATED WITH OF APPROIMATELY 1/4". LEFT NOSE LANDING GEAR TRUNNION FITTING AT APPROMIATELY STATION 580 CRACKED AREA REPAIRED AS PER EA # 1-5310-T0385347 PART 1 TITLE: FUSELAGE - MAINFRAME - CRACK REPAIR ON LH NOSE LANDING GEAR TRUNNION FITTING, STA 595. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT AT STATION 1019 X= -27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1019, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT CABIN FROM BS 969 TO BS 1029 X= -27.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 92,454 hrs · 22,377 cycles

SEAT TRACK AT BS 1301 X= -47.5 FOUND CROWN WORN. SEAT TRACK STATION 1301 X= -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1229 - 1313 X= -47.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 89,815 hrs · 21,840 cycles

DURING PREFLIGHT EMER LT BAT 1 LO DISPLAYED WHEN TESTING THE EMERGENCY LIGHTS REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY AND OPS CHECKS GOOD.

Part: PANEL — DELAMINATED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

LH WING UPPER SURFACE - APPROX BETWEEN XORS 683-713 AT REAR SPAR - PANEL DAMAGED/BULGING REPAIRED L/H WING UPPER SURFACE PNL PER SRM 51-62-01-OG. INSTALLED PANEL ARC7163-1 ON LH WING UPPER SURFACE. REF MD-11 SRM 51-33-01-0G.

Part: WEB — CRACKED (ZONE 300) · airframe 87,671 hrs · 21,266 cycles

TAILCONE - LH PATIO DOOR AFT EDGE ABOUT 15" UP FROM PATIO DOOR HING SIDE IS BENT AND CRACKED. REPAIRED LH PATIO DOOR AFT EDGE REF SRM 52-00-00-2R FIG 204

Part: BEAM — CORRODED (ZONE 100) · airframe 87,671 hrs · 21,266 cycles

CENTER CARGO, DOOR ENTRY CEILING BEAM PN AFA7594-432 SHOWS EXFOLIATION AROUND NUTPLATE INSTALLED AFA7594-37 WITH REPAIR STRAP, INSTALLED REPAIR STRAP REF SRM 51-33-01-0G, AND E.A 1-5300-T0372850

Part: SKIN — WORN (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

LH WING OUTBOARD SKIN AT WING FIXED L/E P/N ARB2363-1 NEEDS TO BE REPAIRED TO ACCOMMODATE REPAIR OF FWD SECTION REF N1461 & N1462. REMOVED DAMAGED SECTION AND SPLICED A NEW SECTION OF SKIN ARB2363-1, REF E.A.# 1- 5730-T0373009, TITLE: WING - PLATES AND SKINS - LH WING FIXED LEADING EDGE LOWER SKIN XDLE 330.2745 TO XW 344.250- REPAIR. MAJOR REPAIR

Part: SKIN — CRACKED (N/A) · airframe 87,671 hrs · 21,266 cycles

"REWORK: REWORK ITEM. REPAIR FASTENERS DO NOT MAINTAIN SPACE DISTANCE PER SRM 57- 40-02-2R FIG 2A" N/R N01277 HAS WRONG SDR NUMBER 23-0296 IS ASSIGNED TO N/R N01464. N/R N01277 REQUIRES NEW SDR AND UPDATED INFORMATION ON RDR. <DEL> 0000675378 : DUONG, KEVIN - 18-FEB-2023 22:05 GENERATEDNEW SDR IN REF N1277. PERFORMED MAJOR REPAIR PER SRM 57-40-02-2R FIG.201, SHT01 & E.A.1-5780-T0372718 P1 MD11 N603-WING-OUTBOARDING-RH OUTER WING TRACK#12 PERMANENT REPAIR. MAJOR REPAIR. 0000675378 : DUONG, KEVIN - 19-FEB-2023 03:31 RESET AMT</DEL> 0000675378 : DUONG, KEVIN - 19-FEB-2023 03:32 GENERATEDNEW SDR IN REF N1277. NEW SDR NUMBER IS 23-0298 AND RDR UPDATED. PERFORMED MAJOR REPAIR PER SRM 57-40-02

Part: NONE — CORRODED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

LEFT WING UPPER TRAILING EDGE SILL ARC0839-1 WAS FOUND CORRODED A VARIOUS LOCATIONS DURING PROCCESS OF GETTING OK TO INSTALL BY W.C. 000589 STEP 7. REMOVED DAMAGED SILL, INSTALLED NEW FABRICATED SILLS AND SPLICED/REPAIRED AT XOSP 623 PER SRM 57-50-02-2R FIG 201 REPAIR 10 DWG ARC0839

Part: SKIN — CHAFED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

#1 ENGINE PYLON: BOTTOM SURFACE OF FIXED L/E HAS DEEP WEAR/GROOVE/GOUGE INTO SKIN. (MARKED AND DOT 64). REPAIRED WING LEADING EDGE SKIN, REF MD11 SRM 57-40-01-2R, FIG 201, WING LEADING EDGE SKIN, SHEET 1 TO 5. MAJOR REPAIR.

Part: NONE — CRACKED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

LEFT WING, SPOILER SILL P/N ARC0839-1 IS CRACKED. FABRICATED REPAIR SILL ARC0839-1 PER SRM 57-50-02-2R AND PER DAC. DWG. ARC0839. RESET. FABRICATED REPAIR SILL PER MD11 SRM 57-50-02-2R FIG 201, REPAIR 10, PAGES 201-204 AND IN REFERENCE TO DAC. DWG. ARC0839. INSP C/W

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOORBOARD 231BF DAMAGED/WORN FABRICATED FLOORBOARD REF FEDEX SRZ-25-005 MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOORBOARD 231BF DAMAGED/WORN FABRICATED FLOORBOARD REF FEDEX SRZ-25-005 MAJOR REPAIR

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK, SEAT TRACK CORRODED AT APPR. STATION 1800, RBL -72. REMOVED AND REPLACED SEAT TRACK AFA7789-539 AT STATION 1800-1887 RBL72 IAW DWG AFA7433

Part: STRUT — MISALIGNED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

PER EA 1-5710-T-372370 P3 WORK INSTRUCTIONS STRUT P/N ARC0639-7 REQUIRES FABRICATION FABRICATED STRUT ARC0639-7 PER EA 1-5710-T0372370 P3 & DWG ARC 0639. (NOTE: WILL BE INSTALLED ON N939) REF EA T 1-5710-T0372370P3; WINGS - BASIC WING STRUCTURE - LH WING REAR SPAR UPPER CAP AFT LEG MAJOR REPAIR

Part: SUPPORT — CORRODED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

MAIN CABIN, R/H SIDE APPROX. STA.1741 RBL 72 FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED AFA3853-10 FLOOR SUPPORT, REF DRAWING AFA3853. "MAJOR REPAIR".

Part: STRUT — MISALIGNED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

PER EA 1-5710-T-372370 P3 WORK INSTRUCTIONS STRUT P/N ARC0639-9 REQUIRES FABRICATION FABRICATED STRUT P/N ARC0639-9 REF DWG ARC0636 AND EA 1-5710-T-372370 P3.

Part: FLOOR SUPPORT — NOT ENTERED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

REPAIR ASSESSMENT: UPPER FUSELAGE, MAIN DECK STA 1661 LBL 75 - 104 EXISTING FLOORBOARD SUPPORT FX AFA3853-5. DOT 140. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER DWG AFA3853. REF E.A. #1-5100-T0372004 Ï¿½REPAIR CATALOGÏ¿½ ATTACHMENT A-1 #140.

Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 87,671 hrs · 21,266 cycles

REPAIR ASSESSMENT: R/H FIXED WING L/E, STA APROX. XOS 672 - 678 EXINTING BEADED DOUBLER. DOT 78. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 Ï¿½ 4. REF E.A. #1-5100-T0372004 Ï¿½REPAIR CATALOGÏ¿½ ATTACHMENT A-1 #78.

Part: NONE — NONE (N/A) · airframe 87,671 hrs · 21,266 cycles

REPAIR ASSESSMENT: UPPER FUSELAGE L1 DOOR STA 436 ? 446, L15L EXISTING REPAIR DOUBLER ON DOOR SKIN TOP FWD CORNER. DOT 15.5. REPAIRED PER SRM 52-10-01, REPAIR 3. RSC REPAIR TRACKING EA 1-5210-T0372870 A.

Part: FLOOR SUPPORT — NOT ENTERED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

REPAIR ASSESSMENT: UPPER FUSELAGE, MAIN DECK STA 1741 LBL 75 - 104 EXISTING FLOORBOARD SUPPORT FX AFA3853-9. DOT 141. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER DWG AFA3853. REF E.A. #1-5100-T0372004 Ï¿½REPAIR CATALOGÏ¿½ ATTACHMENT A-1 #141.

Part: DOUBLER — NONE (ZONE 300) · airframe 87,671 hrs · 21,266 cycles

TAILCONE LH INNER SKIN - APPROX STA.2163 UPPER AREA - SKIN CHAFED. REPAIRED CHAFED AREA REF E.A.# 1-5352-T0372823 '' TAILCONE & PLATFORM - LH INNER DOUBLER WORN - REPAIR''.

Part: SKIN — CHAFED (TAIL CONE) · airframe 87,671 hrs · 21,266 cycles

TAILCONE RH INNER SKIN - APPROX STA.2163 UPPER AREA - WORN/CHAFED. TAILCONE RH INNER SKIN STA Y=2163 - Y=2165, Z=45 - Z=61 STRUCTUAL REPAIR PERFORMED IAW EA#1-5253-TO372704 PART 1 "FUSELAGE -TAILCONE AND PLATFORM- RH INNER DOUBLER WORN- REPAIR"

Part: SKIN — CHAFED (TAIL CONE) · airframe 87,671 hrs · 21,266 cycles

TAILCONE RH INNER SKIN - APPROX STA.2163 UPPER AREA - WORN/CHAFED.

Part: NONE — MISALIGNED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

PER EA WORK INSTRUCTIONS SILL P/N ARC0639-3 REQUIRES FABRICATION FABRICATED SILL ARC0639-3 PER DAC DRAWING ARC0639 AND SAMPLE PER EA 1-5710-T0372370 P3; WINGS - BASIC WING STRUCTURE - LH WING REAR SPAR UPPER CAP AFT LEG. (NOTE: INSTALLATION IN EA) MAJOR REPAIR.

Part: NONE — MISALIGNED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

PER EA WORK INSTRUCTIONS CLIP P/N ARB0005-207 REQUIRES FABRICATION CLIP P/N ARB0005-207 FABRICATED PER DAC DWG. #ARB0005. REF EA T 1-5710-T0372370 P3; WINGS - BASIC WING STRUCTURE - LH WING REAR SPAR UPPER CAP AFT LEG MAJOR REPAIR

Part: FLOOR SUPPORT — CORRODED (BS 1821) · airframe 87,671 hrs · 21,266 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL SUPPORT AT BS 1821, RBL 8 HAS EXFOLIATION CORROSION. REMOVED FABERCATED AND INSTALLED NEW AGA3814-29 FLOOR SUPPORT IAW DWG AGA7554 AND AGA3814

Part: ANGLE — CORRODED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

UPPER CARGO, CENER WING TANK, R/H TUNNEL, ANGLE PN ANB7392-2 EXFOLIATION CORROSION AT STA 1372 X110 INSTALLED ANGLE PN ANB7392-2 REF MD11 SRM 51-31-01-0G. AND EA 1-5710-T0372599 AND TORQUED BOLTS REF MD-11 AMM 20-50-02-2. WING - BASIC WING STRUCTURE - CENTER WING UPPER SKIN - OVERSIZED FASTENER HOLE. MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR PANEL 263KF AT STA 1256-1281 HAS DAMAGED/MISING INSERTS. FABRICATE MAIN DECK FLOOR PANEL (263KF) AEA0179-17 REF SRZ-25-005.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR PANEL 262NF HAS DAMAGED INSERTS. FABRICATED NEW MAIN DECK CARGO COMPT- FLOORBOARD PANEL 262NF PER FEDEX DRWG SRZ-25-005 , AEAO181 " MAJOR REPAIR" ORIG SUBMISSION DATE: 1/16/2023

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR PANEL 261FF HAS DAMAGED INSERTS. FABRICATED NEW MAIN DECK CARGO COMPT -FLOOR PANEL261FF PER FEDEX DRWG SRZ-25- 005 AEA7435 "MAJOR REPAIR"

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOORBOARD PANEL 261BF HAS DAMAGED INSERTS. FABRICATED NEW NAIN DECK CARGO COMPT-FLOORBOARD PANEL 261BF PER FEDEX DRWG SRZ- 25-005 ACA3209 "MAJOR REAIR"

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR PANEL 262KF AT STA.1219-1256 HAS DAMAGE/MISSING INSERTS. FABRICATED FLOOR PANEL (262KF) AEA7435-10 REF FEDEX DWG SRZ-25-005

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR PANEL 262FF AT STA.1256-1321 HAS DAMAGED INSERTS. FABRICATED FLOOR PANEL 262FF PER FEDEX DWG SRZ-25-005. REMOVED AND REPLACED INSERTS REF FEDEX DWG SRZ-25-005.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR PANEL 252LF HAS DAMAGED INSERTS. FABRICATED NEW FLOOR PANEL 252LF REF FEDEX SRZ-15-005. ORIG SUB DATE: 1/16/2023

Part: FLOORBOARD — DAMAGED (N/A) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK CTR PANEL AT STA 770 HAS IMPACT DAMAGE FABRICATED NEW FLOORBOARD REF FEDEX DWG SRZ-25-005 MAJOR REPAIR

Part: INSERT — MISSING (FLOORBOARD) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOORBOARD 281HF AT STA 1700, MISSING INSERTS FABRICATED NEW FLOORBOARD REF FEDEX SRZ-25-005 MAJOR REPAIR

Part: INSERT — MISSING (FLOOR PANEL) · airframe 87,671 hrs · 21,266 cycles

MISSING INSERTS ON AFA3204-513 FLOOR PANEL INSTALLED INSERTS ON AFA3204-513 FLOOR PANEL PER SRZ-25-005. ORIG SUBMISSION DATE: 1/2/2023

Part: INSERT — MISSING (FLOOR PANEL) · airframe 87,671 hrs · 21,266 cycles

MISSING INSERTS ON AFA3200-501 FLOOR PANEL INSTALLED INSERTS PER SRZ-25-005. ORIG SUBMISSION DATE: 1/2/2023

Part: GUSSET — MISALIGNED (ZONE 100) · airframe 87,671 hrs · 21,266 cycles

FWD CARGO COMPT. REQUIRES (2) L/H AND R/H REPAIR GUSSET TO BE MADE NCA6044-157/-158 REMOVED AND REPLACED (2) REPAIR GUSSETS NCA 6044-157/-158 AT FWD CARGO COMPT. STA 595 Z=80 REF SRM 53-20-08-2R FIG 201 "MAJOR REPAIR"

Part: SUPPORT — OUT OF ALIGNMENT (BS 595) · airframe 87,671 hrs · 21,266 cycles

FWD CARGO COMPT AT STA 595 LBL 8 AND RBL 8 Z=80 (2) SUPPORT BRACKETS ACA 3834-501 REQUIRES FABICATION REMOVED AND REPLACED 2 SUPPORTS ACA3834-501 AT FWD CARGO BULKHEAD STA 595 REF SRM 51-31-01-0G AND SRM 53-20-08-2R FIG 201 SH 4 "MAJOR REPAIR"

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR PANEL 291DF HAS DAMAGED/CORRODED INSERTS AFTER CLEANING FOUND PANEL DELAMINATED. FABRICATED NEW PANEL REF FEDEX DWG SRZ- 25-005

Part: SEAT TRACK — CORRODED (MAIN CARGO) · airframe 87,671 hrs · 21,266 cycles

MAIN CARGO SEAT TRACK STA.6-70 RBL75 - CORROSION ON INBD FLANGE. FOUND CORROSION OUT OF LIMIT PER SRM 53-00-52-1A, SEAT TRACK WAS REPLACED FROM STA 1130 TO 1180 THAT INCLUDED STA 6-00 TO 6-100 ON NON-ROUTING N00431 W/O 84094 IAW SRM 53- 00-52-2R FIG. 201, SHT 1-2.

Part: FITTING — CORRODED (ZONE 100) · airframe 87,671 hrs · 21,266 cycles

MAIN CARGO RH AFT OF STA.1179 AT STR.27 - CORROSION ON STR/FITTING. REMOVED AND REPLACED LONGERON (P/N: AEA0427-506) LOCATED AT STR 27R BETWEEN STA 1179-1199 IAW DAC DWG # AEA0427 AND MD-11 SRM 51-33-01-0G. **MAJOR REPAIR**

Part: FLOOR SUPPORT — DAMAGED (BS 890) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK: SUB-FLOOR SUPPORT BRACKET IS BROKEN AT APPROX. STA. 890 LBL 70. "BROKEN" WRITTEN IN RED GREASE PENCIL REMOVE AND REPLACE PER. DOUGLAS DRAWING NCA6018

Part: NONE — CORRODED (ZONE 500) · corrosion level 3 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 292.0 INCHES O/B FROM XW372.94 AREA HAS MINOR SURFACE EXFOLIATION NEAR FASTENER HOLE (MARKED) REPAIR PER E.A: 1-5710-T0372370 TITLED WINGS- BASIC WING STRUCTURE- LH WING REAR SPAR UPPER CAP AFT LEG- REWORK

Part: NONE — CORRODED (ZONE 500) · corrosion level 3 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 5.5 INCHES O/B FROM XW372.94 AREA HAS MINOR SURFACE EXFOLIATION NEAR FASTENERS HOLES (MARKED) REPAIR PER E.A: 1-5710-T0372370 TITLED WINGS- BASIC WING STRUCTURE- LH WING REAR SPAR UPPER CAP AFT LEG- REWORK

Part: NONE — CORRODED (ZONE 500) · corrosion level 3 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 552.0 INCHES O/B FROM XW372.94 AREA HAS SURFACE EXFOLIATION NEAR FASTENERS HOLES (MARKED) REPAIR PER E.A: 1-5710-T0372370 TITLED WINGS- BASIC WING STRUCTURE- LH WING REAR SPAR UPPER CAP AFT LEG- REWORK

Part: NONE — CORRODED (ZONE 500) · corrosion level 3 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 82.0 INCHES O/B FROM XW372.94 AREA HAS MINOR SURFACE EXFOLIATION NEAR FASTENERS HOLES (MARKED) REPAIR PER E.A: 1-5710-T0372370 TITLED WINGS- BASIC WING STRUCTURE- LH WING REAR SPAR UPPER CAP AFT LEG- REWORK

Part: NONE — CORRODED (ZONE 500) · corrosion level 3 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 2 INCHES TO 4.0 INCHES O/B FROM XW372.94 AREA EXFOLIATED NEAR FASTENERS HOLES. REPAIRED PER E.A.#:1-5710-T0372370 TITLED WINGS - BASIC WING STRUCTURE - LH WING REAR SPAR UPPER CAP AFT LEG - REWORK

Part: NONE — CORRODED (ZONE 500) · corrosion level 3 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 15.0 INCHES O/B FROM XW372.94 AREA HAS SURFACE EXFOLIATION NEAR FASTENERS HOLES (MARKED) REPAIR PER E.A: 1-5710-T0372370 TITLED WINGS- BASIC WING STRUCTURE- LH WING REAR SPAR UPPER CAP AFT LEG- REWORK

Part: SPAR CAP — CORRODED (LT WING TE) · corrosion level 2 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 500.0 INCHES TO 501.0 INCHES O/B FROM XW372.94 AREA HAS MINOR SURFACE EXFOLIATION NEAR FASTENERS HOLES (MARKED)

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STA.1887 - STA.2007 RBL54 - RBL59 P/N AGA7551-504. REMOVED AND FABRICATED FLOOR PANEL SUPPORT P/N AGA7551-504 AND INSTALLED NEW FLOOR SUPPORT PER DAC DWG AGA7544, AJC7382 AND SRM 51-38-01-0G. "MAJOR REPAIR".

Part: NONE — CORRODED (ZONE 500) · corrosion level 3 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 555.0 INCHES O/B FROM XW372.94 AREA HAS SURFACE EXFOLIATION NEAR FASTENER HOLE (MARKED) REPAIR PER E.A: 1-5710-T0372370 TITLED WINGS- BASIC WING STRUCTURE- LH WING REAR SPAR UPPER CAP AFT LEG- REWORK

Part: SPAR — CORRODED (ZONE 500) · corrosion level 2 · airframe 87,671 hrs · 21,266 cycles

LH WING TRAILING EDGE UPPER REAR SPAR CAP, 500.0 INCHES TO 501.0 INCHES O/B FROM XW372.94 AREA HAS MINOR SURFACE EXFOLIATION NEAR FASTENERS HOLES (MARKED) AREA BLENDED AT XORS 980 - 985 ON LH WING TRAILING EDGE UPPER REAR SPAR CAP AND FOUND TO BE OUT OF LIMITS PER SRM 57-00-10-1A FIG 201 SH 2. REPAIRED AREA PER EA 1-5710- T0372370 P3; WINGS - BASIC WING STRUCTURE - LH WING REAR SPAR UPPER CAP AFT LEG - REWORK MAJOR REPAIR

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STA.1887 RBL4 - RBL7. REMOVED AND REPLACED FLOOR SUPPORT IAW DWG AGA7559 & SRM 51-38-01-0G

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STA.1887 - STA.2007 RBL23 - RBL26 P/N AGA7087-512. REMOVED AND REPLACED FLOOR SUPPORT CORRODED AT STA.1887 - STA.2007 RBL23 - RBL26 P/N AGA7087-512. IN REFERENCE PER DWG AGA7544. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 1914-2007) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STA.1914 - STA.2007 RBL20 - RBL23 P/N AGA7088-2. REMOVED AND REPLACED FLOOR SUPPORT AT STA.1914 - STA.2007 RBL20 - RBL23 P/N AGA7088-2 PER DWG AGA7127 AND SRM 51-31-01-0G

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STA.1887 - STA. 2007 LBL0 TO LBL5 P/N AGA7081-509. REMOVED, FABERCITED AND INSTALLED NEW AGA7081-509 FLOOR SUPPORT IAW AGA7544, AJC7382, AGA7081 SRM 51-38-01-0G AND SRM 51-21-01-0G

Part: FLOOR SUPPORT — CORRODED (BS 1914-2007) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STA.1914 - STA.2007 LBL20 - LBL23 P/N AGA7088-1. REMOVED AND REPLACED FLOOR SUPPORT P/N AGA7088-1 IAW DWG AGA7544, AJC7382 AND SRM 51-38-01-0G

Part: FITTING — DAMAGED (CENTER MLG) · airframe 87,671 hrs · 21,266 cycles

CENTER LANDING GEAR LT PILLOW BLOCK SHEAR PIN HOLE CORRODED. REPAIRED SUPPORT FITTING SHEAR PIN HOLE IAW SRM 53-40-14-2R, AND EA 1-5340-T0372310.

Part: FITTING — CORRODED (CENTER MLG) · airframe 87,671 hrs · 21,266 cycles

CTR LANDING GEAR L/H PILLOW BLOCK AFT BOLT HOLE COUNTER BORE CORRODED REPAIRED PER E.A. 1-5340-T0372310. ORIG SUBMISSION DATE: 1/4/2023

Part: FITTING — CORRODED (CENTER MLG) · airframe 87,671 hrs · 21,266 cycles

CENTER LANDING GEAR LT PILLOW BLOCK FWD BOLT HOLE COUNTER BORE CORRODED. BLENDED THE SUPPORT FITTING FWD BOLT HOLE COUNTER BORE TO REMOVE CORROSION IAW SRM 53-40-14-2R, 23, AND EA 1-5340-T0372310.

Part: SKIN — GOUGED (FUSELAGE) · airframe 87,671 hrs · 21,266 cycles

UPPER FUSELAGE - UPPER CARGO DOOR AREA - LOWER FORWARD EXTERNAL SKIN IS DAMAGED, ADJACENT TO THE DOOR SEAL RETAINER (MARKED). REPAIRED DAMAGED SKIN AT LOWER FORWARD AREA OF UPPER CARGO DOOR, REF SRM 53-00- 15-2R, REPAIR 8 FIGURE 203, SHEET 3.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 87,671 hrs · 21,266 cycles

MULTIPLE INSERTS DAMAGE ON FLOOR PANEL 293HF FABRICATED NEW FLOOR PANEL 293HF PER SRZ25-005 REV.R

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK CARGO HOLD STATION 6-70 TO 1159 RBL 48-75 FLOOR PANEL ADA7557 CRACKED AT MISSING INSERTS. FABRICATED PANEL ADA7557 PER SRZ-25-005 REV R

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOOR PANEL 241GF HAD MISSING INSERTS. REPLACED THE INSERTS IAW SRM 53-00-50-2R, FIG 202.

Part: FITTING — DAMAGED (CENTER MLG) · airframe 87,671 hrs · 21,266 cycles

CENTER LANDING GEAR L/H PILLOW BLOCK SHEAR PIN BUSHING DAMAGED DURING REMOVAL FOR HFEC INSP. L/H CENTER L/G SUPPORT FITTING SHEAR PIN BUSHING REPAIR COMPLETED ON N/R 841 AND E.A. 1-5340-T0372310. ORIG SUBMISSION DATE: 1/4/2023

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

UPPER FUSELAGE, MAIN CABIN: FIRE SUPPRESSION TANK ALIGNMENT INTERCOSTAL IS CRACKED AT FWD END. STA. 1401, LONG. 2R. REMOVED FABRICATED AND INSTALL NEW VA-FSS-6040-1 INTERCOSTAL IAW DWG VA-FSS-6040

Part: ANGLE — CRACKED (BS 1401 L2R) · airframe 87,671 hrs · 21,266 cycles

UPPER FUSELAGE, MAIN CABIN: FIRE SUPPRESSION TANK ALIGNMENT INTERCOSTAL, FWD CLIP IS CRACKED. STA. 1401, LONG. 2R (MARKED). REMOVED FABRICATED AND INSTALLED NEW VA-FSS-6045-1 CLIP

Part: BEAM — CRACKED (BS 595 BULKHEAD) · airframe 87,671 hrs · 21,266 cycles

FWD CARGO COMPT AT STA. 595 AFT PRESSURE BULKHEAD BEAM AT X= -6 AND Z= -80 HAS A 1.5 IN. CRACK AT THE LOWER RADIUS. REPAIRED FWD CARGO COMPT. STA 595 AFT PRESSURE BULKHEAD BEAM AT X= -6 AND Z= -80 REF SRM 53-20-08-2R FIG. 201. "MAJOR REPAIR"

Part: FLOOR SUPPORT — CORRODED (BS 1741 LBL 80) · airframe 87,671 hrs · 21,266 cycles

BS 1741 LBL 80 FLOOR SUPPORT CORRODED REMOVED CORRODED FLOOR SUPPORT AT STA 1741 LBL 80 AND INSTALLED SERVICEABLE FLOOR SUPPORT AFA 3853-9 PER DWG AFA 3853 AND SRM 51-33-01-0G.

Part: FRAME — CORRODED (BS 1821 L50L-R) · airframe 87,671 hrs · 21,266 cycles

CTR CARGO COMPT BILGE AREA, CORROSION ON FRAME AT HAT SECTION STA 1821 L-50 L/H - L-50 R/H (MARKED #11) REPAIRED J CHANNEL ON FRAME AT HAT SECTION STATION 1821 BETWEEN L-50 LH AND L50-RH IAW MD11 SRM 53-00-07-2R FIG 202 REPAIR 5 SHEET 1&2

Part: FRAME ANGLE — CORRODED (ZONE 100) · airframe 87,671 hrs · 21,266 cycles

CTR CARGO COMPT BILGE AREA, CORROSION ON FRAME AT HAT SECTION STA 5-113 L-52 (MARKED #14) REMOVED CORRODED SECTION OF FRAME CAP AND REPAIRED FRAME CAP REF SRM 53-00- 00-2R, FIGURE 209 SHEETS 2,5,6 AND 7. MAJOR REPAIR.

Part: SPLICE STRAP — CORRODED (CENTER CARGO) · airframe 87,671 hrs · 21,266 cycles

CTR CARGO COMPT BILGE AREA, EXFOLIATED CORROSION ON LONGERON SPLICE STA 5-55 L-48 RT. REMOVED AND REPLACED SPLICE STRAP REF DWG AEA7653. ORIG SUBMISSION DATE: 1/13/2023

Part: FRAME — CORRODED (BS 1841 L43L-R) · airframe 87,671 hrs · 21,266 cycles

AFT CARGO COMPT STA 1841 FRAME WEB TOP CAP HAS CORROSION L43L/H - L43R/H. REMOVED AND REPLACED TOP CAP SUPPORT IAW SRM 51-33-01-0G & DWG AGA7170. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (N/A) · airframe 87,671 hrs · 21,266 cycles

MAIN CARGO COMPT, STA 1710, LBL 81 ,SEAT TRACK ALONG SIDEWALL, UNDER SIDE HAS CORROSION/EXFOLIATION BY FASTENER HOLE (MARKED). REPAIRED SEAT TRACK LOBE AT STA 1710 LBL 107 PER SRM 53-00-52-2R FIG 201 SH 2

Part: FLOOR SUPPORT — CORRODED (BS 1661 LBL 80) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK -- BS 1661 LBL 80 FLOOR SUPPORT CORRODED REMOVED CORRODED FLOOR SUPPORT AT STA 1661 LBL 80 AND INSTALLED SERVICEABLE FLOOR SUPPORT AFA 3853-5 PER DWG AFA 3853 AND SRM 51-33-01-0G.

Part: SEAT TRACK — CORRODED (BS 1841-1967) · airframe 87,671 hrs · 21,266 cycles

AFT CARGO COMPT STA 1841-1967 SEAT TRACK/FLOORBOARD SUPPORT HAS SEVERAL AREAS OF SURFACE CORROSION. MRKD RBL 20. REMOVED AND REPLACED SEAT TRACK AS REQUIRED. REF MD 11 SRM 51-31-01-0G, DAC DWG AGA3855. MAJOR REPAIR. ORIG SUBMISSION DATE: 1/13/2023

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 87,671 hrs · 21,266 cycles

AFT CARGO COMPT STA 1844-1854 FLOORBOARD SUPPORT CORRODED. MRKD RBL60 REMOVED AND REPLACED FLOOR SUPPORT AGA3857-2 REF. DWG. AGA3857.

Part: FRAME — CRACKED (BS 465) · airframe 87,671 hrs · 21,266 cycles

FORWARD AVIONICS COMPT: LEFT SIDE, APPROX STA 465 (UNDER RAM AIR DUCT FOR ACM #1) AT BOOT. A BOOT ATTACHMENT BOLT HAS CHAFED/WORN INTO THE FRAME. MARKED

Part: ANGLE — CORRODED (VERTICAL STAB) · airframe 87,671 hrs · 21,266 cycles

VERTICAL STABILIZER; RIGHT PANEL 374FR ATTACH POINT STRUCTURE EXFOLIATED AT NUTPLATE. REMOVED CORRODED ANGLE AMC 7202-49 AND INSTALLED NEW SERVICEABLE ANGLE AMC7202-49 FOR PANEL 374FR IAW SRM 51-33-01-0G.

Part: FRAME — CRACKED (ZONE 100) · airframe 87,671 hrs · 21,266 cycles

FORWARD AVIONICS COMPT: LEFT SIDE, APPROX STA 465 (UNDER RAM AIR DUCT FOR ACM #1) AT BOOT. A BOOT ATTACHMENT BOLT HAS CHAFED/WORN INTO THE FRAME. MARKED R & R BOLT PER SRM 51-31-01-OG,CHECK FOR DAMAGE ON FRAME, REPAIR AS NECESSARY.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 87,671 hrs · 21,266 cycles

RT LOWER VERTICAL STABILIZER SKIN PANEL UPPER AFT FASTENER HOLE HAS A .600 IN CRACK PROPAGATING TO THE EDGE OF THE SKIN PANEL (AT PYLON CARRY THOUGH CAP AND REAR SPAR STA. 2164. REPAIRED IAW EA 1-5530-T0372226 P1. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1887) · airframe 87,671 hrs · 21,266 cycles

MAIN CABIN. FLOOR SUPPORT CORRODED UNDER PANEL 293BF AT STA. 1902 RBL 9 TO RBL 27. REMOVED AND FABRICATED FLOOR PANEL SUPPORTS P/N AGA7559-5, AGA3814-14 PER DAC DWG A7559, INSTALLED NEW FLOOR SUPPORT PER DAC DWG AGA7559 AND SRM 51-38-01-0G. "MAJOR REPAIR".

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 87,671 hrs · 21,266 cycles

MAIN CABIN, CENTER FLOOR SUPPORT IS CORRODED AT STA. 1902 TO 2007, P/N AGA 7544-503/509. REMOVED AND REPLACED FLOOR SUPPORT P/N AGA7544-503/509 IAW DWG AGA7544, AJC7382 AND SRM 51-38-01-0G. MAJOR REPAIR

Part: FLOOR SUPPORT — CORRODED (BS 1914-2005) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK CENTER FLOOR SUPPORT CORRODED FROM STA. 1914 TO STA. 2005, RBL 4. REMOVED FABERCATED AND INSTALLED AGA7080-509 FLOOR IAW DWG AGA7544, AGA7382 ,AGA7080 AND SRM51-38-01-0G

Part: FLOORBEAM — CORRODED (BS 1914 R-LBL 20) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK FLOORBEAM CORRODED BS 1914, RBL 20 TO LBL 20. REMOVED AND FABRICATED FLOOR SUPPORT P/N AGA7085-501 PER DAC DWG AGA7085 - INSTALLED NEW FLOOR SUPPORT P/N AGA7085-501 PER DAC DWG AGA7544, AJC7382 AND SRM 51-38-01-0G 'MAJOR REPAIR'

Part: SEAT TRACK — CORRODED (BS 1130-1180) · airframe 87,671 hrs · 21,266 cycles

MAIN CARGO DECK, STA 6-70 TO 6-90, RBL 75, SEAT TRACK FLOOR SUPPORT LOBES, CORROSION EVIDENT. REMOVED AND REPLACED CORRODED SEAT TRACK FROM STA 1130 - 1180 PER SRM 53-00-52-2R FIG. 201, AND DWG. A6A7083. SEE JPF "MAJOR REPAIR" ORIG SUBMISSION DATE: 1/13/2023

Part: SKIN — WORN (RT WING LE) · airframe 87,671 hrs · 21,266 cycles

RT WING: DROOP L/E - DEEP GROOVE WORN THROUGH SKIN ON UPPER, OUTBD SURFACE OF DLE (MARKED AND DOT 58) REPAIRED DAMAGED DLE SKIN IN REFERENCE TO MD11 SRM 57-40-01 FIG 202 REPAIR 15

Part: SKIN — CRACKED (N/A) · airframe 87,671 hrs · 21,266 cycles

R/H WING LEADING EDGE SKIN AT SLAT TRACK #12 CUT OUT AFT OUTBOARD CORNER HAS A .400 IN. CRACK. (MARKED) INSTALLED DOUBLER AND FILLER REF SRM 57-40-02-2R FIGURE 201 REPAIR 7.

Part: SKIN — WORN (RT WING LE) · airframe 87,671 hrs · 21,266 cycles

RT WING: DROOP L/E - DEEP GROOVE WORN THROUGH SKIN ON UPPER, OUTBD SURFACE OF DLE. REPAIRED DAMAGED DLE SKIN IN REFERENCE TO MD11 SRM 57-40-01 FIG 202 REPAIR 15. MAJOR REPAIR. REPAIRED DAMAGED DLE SKIN IAW SRM 57-40-01 FIG 202 REPAIR 15. MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING) · airframe 87,671 hrs · 21,266 cycles

RIGHT WING LEADING EDGE SKIN AT FUEL ACCESS PANEL FWD INBOARD CORNER HAS A .600 INCH CRACK. INSTALLED REPAIR DOUBLER IAW DWG ARB1232 AND IAW SRM 57-40-02-2R AND SRM 51-31- 01-OG. ORIG SUBMISSION DATE: 1/4/2023

Part: SKIN — CRACKED (LT FAN COWL) · airframe 87,671 hrs · 21,266 cycles

NR 2 ENG INLET DUCT, L/H LWR FAN COWL DOOR LAND WORN AND CRACKED. (MARK) 0003749939 : EGASHIRA, JUN - 18-JAN-2023 14:20 REMOVED SKIN PANEL AJC7415-157 FROM ASSEMBLY AJC7415-159 IAW MD11 SRM 51-31-01-0G/ MD11 SRM 51-35-01-0G. FABRICATED SKIN PANEL AJC7415-157 IAW DRAWING AJC7415. INSTALLED FABRICATED SKIN PANEL AJC7415-157 TO ASSEMBLY AJC7415-159 IAW MD11 SRM 51-31-01- 0G/MD11 SRM 51-35-01-0G/ DRAWING AJC7415.

Part: SKIN — CRACKED (LT WING LE) · airframe 87,671 hrs · 21,266 cycles

L/H WING LEADING EDGE SKIN AT SLAT TRACK #15 CUT OUT AFT INBOARD CORNER HAS A .500 IN. CRACK. (MARKED) 0004311346 : SCHRADER SR., STEPHEN D - 15-JAN-2023 01:23 REPAIRED L/H WING LEADING EDGE SKIN AT SLAT TRACK # 15 PER SRM 57-40-02-2R. "MAJOR REPAIR"

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 87,671 hrs · 21,266 cycles

FLOOR PANEL 272DF DAMAGED. FABRICATED NEW PANEL PER SRZ -25-005.

Part: SEAT TRACK — CORRODED (BS 1109-1189) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK: SEAT TRACK AT APPROX. STA.1100 RBL6 HAS LIGHT CORROSION. DOT 7 REPAIRED SEAT TRACK FROM RBL6 STA 1109 TO STA 1189 (80") REF SRM 53-00-52-2R, REPAIR 1 FIG 201 AND SRM 51-31-01-OG. "MAJOR REPAIR"

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 87,671 hrs · 21,266 cycles

RH WING, INBD FLAP UPPER SURFACE AT XIFH 171, UPPER SECTION - APPROX .400" CRACK IN SKIN AT FASTENER. CRACK CONFIRMED USING NDT HFEC. R/H INBD FLAP TOP SKIN AT XIFH 171.300 ON ARC2369-4 AND ARC2369-21, DOUBLER AND FILLER REPAIR PERFORMED IAW SRM 57-00-01-2R REPAIR 1. EA COMPLIED WITH FOR TRACKING IAW EA # 1-5750-T0372585 PART 1. MAJOR REPAIR.

Part: SKIN — CRACKED (ZONE 500 LE) · airframe 87,671 hrs · 21,266 cycles

LEFT WING, CRACK ON WING LEADING EDGE AT FWD I/B CORNER OF FUELING PANEL. REMOVED DAMAGED AND INSTALLED NEW DOUBLER AND FILLER AT L/H WING LEADING EDGE SKIN AT SLAT TRACK #11 IAW SRM 57-40-02-2R, REPAIR 7, FIG 201, SHEET 1.

Part: SEAT TRACK — CORRODED (BS 1470 RBL 6) · airframe 87,671 hrs · 21,266 cycles

MAIN DECK: SEAT TRACK AT APPROX. STA.1470 RBL6 HAS CORROSION. REPAIRED NEW SEAT TRACK SECTION AND SPLICE CHANNEL REF SRM 53-00-52-2R FIG 201 SHEET 1,2. MAJOR REPAIR

Part: SKIN — CRACKED (LT WING LE) · airframe 87,671 hrs · 21,266 cycles

LEFT WING, CRACK ON WING LEADING EDGE AT FWD I/B CORNER OF FUELING PANEL. REPAIRED LEFT WING, LEADING EDGE CUT OUT CORNER AT FWD I/B OF FUELING PANEL REF MD11 SRM 57-40-01-2R REPAIR 18 FIGURE. 201 MAJOR REPAIR.

Part: SKIN — CORRODED (RT WING) · airframe 87,671 hrs · 21,266 cycles

RH WING UPPER SURFACE - APPROX XORS 417 AT REAR SPAR - FILLER BULGING. BLENDED AND REMOVED CORROSION IAW SRM 51-21-01-0G, APPLIED REPAIR IAW EA# 1-5710-T0372292 "WING - BASIC WING STRUCTURE - RT WING REAR SPAR UPPER CAP AFT LEG STA. XORS 412 TO XORS 420 - REWORK"

Part: SKIN — CRACKED (LT WING) · airframe 87,671 hrs · 21,266 cycles

L/H WING L/E ACCESS PANEL FOR SLAT DRIVE MECHANISM, I/B CORNER CUT OUT, LOWER WING SKIN IS CRACKED. VERIFIED BY NDT. REPAIRED LOWER WING SKIN I/B CORNER CUT OUT OF L/H WING L/E ACCESS PANEL FOR SLAT DRIVE MECHANISM REF MD11 SRM 57-40-01-2R REPAIR 17 FIG. 201, MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

LH WING UPPER SURFACE - APPROX XORS 122 STR 19 - CORROSION AROUND ONE (1) FASTENER. COMPLIED WITH EA 1-5730-T0372330 (P2) SEQ 812; WING - PLATES AND SKINS - LH WING UPPER SKIN - REWORK. MAJOR REPAIR

Part: SKIN — CORRODED (N/A) · airframe 87,671 hrs · 21,266 cycles

LH WING UPPER SURFACE - APPROX XORS 213 STR 16 - CORROSION AROUND ONE (1) FASTENER. COMPLIED WITH EA 1-5730-T0372330 (P2) SEQ 812; WING - PLATES AND SKINS - LH WING UPPER SKIN - REWORK. MAJOR REPAIR

Part: SKIN — CORRODED (LT WING) · airframe 87,671 hrs · 21,266 cycles

LH WING UPPER SURFACE - APPROX XORS 97 STR 15 - CORROSION AROUND THIRTEEN (13) FASTENERS. REPAIRED CORROSION ON L/H UPPER WING SURFACE AT XORS 97 STR. 15 PER E. A. 1-5730- T0372330- LH WING UPPER SKIN- "MAJOR REPAIR".

Part: HINGE PIN — CORRODED (AFT CARGO DOOR) · airframe 87,671 hrs · 21,266 cycles

HINGE PIN AND LOBES ARE RUSTED ON AFT LWR CARGO DOOR. REMOVED RUST ON HINGE PINS AND LOBES ON AFT CARGO DOOR. REMAINING THICKNESS AT SPOTFACE .490 WITHIN LIMITS IAW 52-30-16-1A, FIG 101, SHEET#2, MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 500) · airframe 87,671 hrs · 21,266 cycles

LH WING UPPER SURFACE - APPROX XORS 213 STR 16 - CORROSION AROUND ONE (1) FASTENER. COMPLIED WITH EA 1-5730-T0372330 (P2) SEQ 812; WING - PLATES AND SKINS - LH WING UPPER SKIN - REWORK. MAJOR REPAIR

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 87,600 hrs · 21,245 cycles

EMER LT BAT 1 LO DISPLAYS ON TEST. REMOVED AND REPLACED EMERGENCY LT POWER SUPPLY REF 33-51-01-4. OPS NORMAL. OK FOR SVC.

Part: DOUBLER — NOT REPORTED (CARGO DOOR) · airframe 87,471 hrs · 21,195 cycles

REMOVE REPAIR DOUBLER AND FILLER ON LWR CENTER CARGO DOOR TO BE REPLACED USING SRM 52-30-16-2R. REPAIRED IAW SRM 52-30-16-2R, REPAIR 3 FIGURE 201.

Part: BRACKET — BROKEN (VSV) · airframe 86,226 hrs · 20,834 cycles

ENG 3 FADEC MAINT LEVEL 1 ALERT, FOLLOWED BY ENG 3 RPM LOW LEVEL 2 ALERT, FOLLOWED BY GEN 3 OFF ALERT. ATTEMPT RE START, NO JOY. EGT 585. PERFORMED ENGINE SHUTDOWN, FOUND BRACKET ABOVE VSV ACTUATION LEVER BROKEN ON INBOARD SIDE. PERFORMED ENGINE POST-WINDMILLING INSPECTION IAW AMM 72-00-05-6-1 REF WRI 75-31 9736 FOR VSV ACTUATOR GUIDE REPLACEMENT. INTERRORGATED #3 ECU, NO CURRENT FAULTS OR NEW FAULTS ON FAULT REVIEW. REPLACED SUPPORT BRACKET IAW SMP AND IPC 71-40-20-01. C/W POWER ASSURANCE TEST PER MM 71-00-00-5-1, AND JRH, ENGINE RUN TESTS PASSED, OK FOR SERVICE.

Part: NONE — FAILED (N/A) · airframe 85,819 hrs · 20,739 cycles

PDIS 603 36-22 9517 28DEC21 KIX FACT U IN CRUISE AT FL310, 1:40 INTO FLIGHT, RECEIVED AIR SYS 3 OFF ALERT, SYSTEM 3 PRESSURE INDICATED 0. BLEED AIR 3 PRESS AND OFF LIGHTS ALONG WITH MANF LIGHT WHICH REMAINED ON FOR APPROXIMATELY 1 MINUTE BEFORE EXTINGUISHING (MANF ONLY.) AT MOC RECOMMENDATION, CYCLED AIR SYSTEM TO MANUAL AND BACK TO AUTO WITH NO CHANGE IN SYSTEM STATUS. WAS TOLD A/C WAS REPORTING A TEMP SENSOR OVER TEMP CONDITION, SO THE CONSENSUS WAS TO NOT ATTEMPT ANY FURTHER TROUBLESHOOTING. SHGN 28DEC21 04:50 KIX U FACT 28DEC21 09:15 KIX U CONTINUITY CHK WAS GOOD WITH NO SHORT TO GND ON D1-153 SENSING ELEMENT PER WDM36-23-01. REMOVED AND REPLACED D1-153 SENSING ELEMENT PRECAUTIONALLY PER AMM36-23-07-4. FOLLOWED FIM36-23-06(MFC PNEU 3 OUT), REMOVED AND REPLACED MFC PER AMM36-23-01-4. PERFORMED HIGH PWR ENG RUN-UP(10 MIN) AND NO DEFECT FOUND PER AMM71-00-00-5-1. PERFORMED MFC R-T-S TEST PASSED 36-23-01-5. A/C OK FOR SERVICE.

Part: NONE — FAILED (N/A) · airframe 85,347 hrs · 20,591 cycles

PDIS 603 32-60 9311 26OCT21 MEM FACT U ON FINAL TO RUNWAY 9 WE GOT FOUR GREEN GEAR INDICATION ABOVE GEAR HANDLE, AND AN UNSAFE WHITE LANDING GEAR BOX ON THE EAD, ALSO NO GREEN ON CONFIG PAGE. PART 26OCT21 07:26 MEM U IDENTIFIED PARTS ELEC SWITCH PROX (CAT2/3) MPN: 8-598-03 CPN: 3110141 QTY: 1 PART 26OCT21 07:26 MEM U ORDER PART MPN: 8-598-03 CPN: 3110141 QTY: 1 ICT: 361906 R/I 26OCT21 08:07 MEM U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 8-598-03 POS: ONL SRL: 216 TAG NBR: 66G126 ON MPN: 8-598-03 CPN: 3110141 SRL: 112 TAG NBR: G20304 FACT 26OCT21 08:07 MEM U T/S REF MD11 SSM 32-62-0 AND FOUND SD MISSING GREEN/RED INDICATION ON LANDING GEAR PAGE. INTERRROGATED PSEU AND FOUND FAULT CODE 42, BOX INTERNAL CARD FAULT. REMOVED AND REPLACED PSEU REF MD11 AMM 31-71-01-2. FUNCTIONAL CHECK GOOD AND ALL INDICATIONS ARE NOW AS NORMAL. ELDEC PSEU P/N 8-598-03 S/N 112

Part: FUEL SYS — MALFUNCTIONED · airframe 83,559 hrs · 20,107 cycles

ENG #3 SHUTDOWN IN FLT. FUEL INDICATOR MALFUNCTION MEL. APPARENT FLAMEOUT. COMPLETED FUEL IMBALANCE INSPECTION PER AMM 05-51-08-6 AND ENGINE 3 WINDMILL INSPECTION PER AMM 72- 00-05-6-1, TRANSFERRED FUEL TO #3 TANK AND PERFORMED AND RUNS, OPERATED ENGINE AT PARTIAL POWER AND NO FAULTS FOUND.

Part: DOUBLER — CORRODED (RT MLG WW) · airframe 82,662 hrs · 19,855 cycles

RIGHT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION. FOUND CORROSION YW 467 RIGHT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER YW 467. CORROSION REMOVED AND FOUND EXCEED LIMIT AS 0.100" MAXIMUM MATERIAL. REMOVAL FOR GENERAL CORROSION REMOVAL, PER SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1 AND CARRIED OUT REPAIR, AS PER EA: 1-5730-T0356755 PART 1. TITLE: WINGS-PLATES AND SKINS-RT WING-CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN AUX SPAR AND YW 467. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CORRODED (LT MLG WW) · airframe 82,662 hrs · 19,855 cycles

LEFT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEED LIMIT AS 0.100" MAXIMUM MATERIAL REMOVAL. REMOVAL FOR GENERAL CORROSION REMOVAL, PER SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1 AND CARRIED OUT REPAIR, AS PER EA: 1-5730-T0356842 PART 1. TITLE: WINGS-PLATES AND SKINS-LT WING-CORROSION ON MLG SUPPORT UPPER DOUBLER BETWEEN AUX SPAR AND YW 467. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FLOORBEAM — CRACKED (CENTER CARGO) · airframe 82,662 hrs · 19,855 cycles

CENTER CARGO COMPARTMENT, STATION 1741, X=0 FLOOR BEAM FOUND CRACK. CENTER CARGO COMPARTMENT, STATION 1741, X=0 CRACK FLOOR BEAM REMOVED, PER SRM 51-31-01-0G. FLOOR BEAM FABRICATED, PER DOUGLAS DRAWING AFA0040 REVISION V AND INSTALLED PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 82,662 hrs · 19,855 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NUMBER 252EF AT STATION 1099 TO STATION 6-70 FOUND EDGE DELAMINATED. DELAMINATED FLOOR PANEL 252EF AT CABIN STATION 1099 TO STATION 6-70 REMOVED, AS PER PER AMM 53-21-04. FLOOR PANEL 252EF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 252EF INSTALLED, AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 82,662 hrs · 19,855 cycles

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

Part: SKIN — CRACKED (ZONE 200) · airframe 82,662 hrs · 19,855 cycles

CABIN-MAIN DECK CARGO COMPARTMENT R3 DOOR AFT LOWER FUSELAGE JAMB, SKIN FOUND CRACKED AT RIGHT HAND STATION 1310 BETWEEN LONGERON 26 RIGHT 27 RIGHT. CABIN-MAIN DECK CARGO COMPARTMENT R3 DOOR AFT LOWER FUSELAGE JAMB AT RIGHT HAND STATION 1310 BETWEEN LONGERON 26 RIGHT TO 27 RIGHT, CRACKED SKIN REPAIRED, AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 82,662 hrs · 19,855 cycles

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

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 82,662 hrs · 19,855 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NUMBER 252UF AT STATION 6-70 TO STATION 1159 FOUND EDGE DELAMINATED. DELAMINATED FLOOR PANEL 252UF AT CABIN STATION 6-70 TO STATION 1159 REMOVED, AS PER AMM 53-21-04. FLOOR PANEL 252UF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 252UF INSTALLED, AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.

Part: FRAME — DENTED (MAIN DECK CARGO) · airframe 82,662 hrs · 19,855 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FRAME FOUND DENTED AT STATION 1601, LONGERON 12 LEFT. CABIN, MAIN DECK CARGO COMPARTMENT AT STATION 1601, LONGERON 12 LEFT, DENTED LEFT HAND FRAME. REPAIRED, AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT EVERY 9,500 CYCLES TO BE CARRIED OUT, AS PER SRM 53-00-07-2R TABLE 201 REPAIR 2. METHOD HIGH FREQUENCY EDDY CURRENT. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (MAIN DECK CARGO) · airframe 82,662 hrs · 19,855 cycles

CABIN, MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE FOUND CRACKED AT STATION 1220, X= -75.25. CABIN, MAIN DECK CARGO COMPARTMENT, CRACKED SEAT TRACK AT STATION 1220, X= -75.25. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO EXISTING SPLICE STATION 1269, X= -75.25, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FRAME — DENTED (MAIN DECK CARGO) · airframe 82,662 hrs · 19,855 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FRAME FOUND DENTED AT STATION 1721, LONGERON 12 RIGHT. CABIN, MAIN DECK CARGO COMPARTMENT DENTED FRAME AT STATION 1721 LONGERON 12. RIGHT REPAIRED, AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT EVERY 9,500 CYCLES TO BE CARRIED OUT, AS PER SRM 53-00-07-2R TABLE 201 REPAIR 2. METHOD HIGH FREQUENCY EDDY CURRENT. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100 .

Part: DOUBLER — DELAMINATED (RT WING) · airframe 82,662 hrs · 19,855 cycles

RIGHT WING TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE FINGER DOUBLER FOUND DETACHED AT XW 388. RIGHT WING TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE XW 388 DETACHED. FINGER DOUBLER REPAIR CARRIED OUT, AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,662 hrs · 19,855 cycles

RIGHT HAND WING, LEADING EDGE CAVITY AT STATION XOS=639 BEADED DOUBLER FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY XOS=639 CRACK BEADED DOUBLER. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,662 hrs · 19,855 cycles

RIGHT HAND WING, LEADING EDGE CAVITY AT STATION XOS=666 BEADED DOUBLER FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY STATION XOS=666 CRACK BEADED DOUBLER. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,662 hrs · 19,855 cycles

RIGHT HAND WING, LEADING EDGE CAVITY AT STATION XOS=705 BEADED DOUBLER FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY AT STATION XOS=705 CRACK BEADED DOUBLER. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — DELAMINATED (LT WING) · airframe 82,662 hrs · 19,855 cycles

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

Part: DOUBLER — CRACKED (LT WING) · airframe 82,662 hrs · 19,855 cycles

LEFT HAND WING, LEADING EDGE CAVITY AT STATION XOS=657 BEADED DOUBLER FOUND CRACK. LEFT WING LEADING EDGE CAVITY AT XOS=657 CRACK BEADED DOUBLER REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,662 hrs · 19,855 cycles

RIGHT HAND WING, LEADING EDGE CAVITY AT STATION XOS=693 BEADED DOUBLER FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY STATION XOS=693 CRACK BEADED DOUBLER. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,662 hrs · 19,855 cycles

LEFT HAND WING LEADING EDGE CAVITY AT STATION XOS=693 BEADED DOUBLER FOUND CRACK. LEFT WING LEADING EDGE CAVITY AT XOS=693 CRACK BEADED DOUBLER REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203. REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,662 hrs · 19,855 cycles

RIGHT HAND WING, LEADING EDGE CAVITY AT STATION XOS=730 BEADED DOUBLER FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY STATION XOS=730 CRACK BEADED DOUBLER. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ACCESSORY BAY) · corrosion level 2 · airframe 82,662 hrs · 19,855 cycles

LOWER FUSELAGE CENTER ACCESSORY COMPARTMENT FLOOR LONGERON NR 51 RIGHT FOUND WITH CORROSION STATION 1139. LOWER FUSELAGE CENTER ACCESSORY COMPARTMENT FLOOR STATION 1139 LONGERON NR 51 RIGHT CORROSION. REMOVED AND FOUND EXCEED LIMIT, AS PER SRM 53-00-00-2R FIGURE 205. REPAIR GENERAL AND LONGERON 51 RIGHT REMOVED AND REPLACED, AS PER SRM 51-33-01-0G. FABRICATED LONGERON 51 RIGHT, AS PER DOUGLAS DRAWING AAA7086 REVISION: NEW. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: LONGERON — CORRODED (ACCESSORY BAY) · corrosion level 2 · airframe 82,662 hrs · 19,855 cycles

LOWER FUSELAGE CENTER ACCESSORY COMPARTMENT FLOOR LONGERON NR 51 LEFT FOUND WITH CORROSION STATION 1139. LOWER FUSELAGE CENTER ACCESSORY COMPARTMENT FLOOR LONGERON NR 51 LEFT STATION 1139 AREA CORROSION. REMOVED FOUND EXCEED LIMIT, AS PER SRM 53-00-00-2R FIGURE 205. REPAIR GENERAL AND LONGERON 51 LEFT REMOVED AND REPLACED, AS PER SRM 51-33-01- 0G. FABRICATED LONGERON 51 LEFT, AS PER DOUGLAS DRAWING AAA7086 REVISION NEW. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 82,662 hrs · 19,855 cycles

CABIN, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NUMBER 271EF AT STATION 1361 TO STATION 1481 FOUND ACCESS DOOR HOLE EDGE DELAMINATED. DELAMINATED FLOOR PANEL 271EF AT CABIN STATION 1361 TO STATION 1481 REMOVED, AS PER AMM 53-21-04. FLOOR PANEL 271EF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 271EF INSTALLED, AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 80,450 hrs · 19,249 cycles

DURING CLIMBOUT RECIEVED LEVEL ONE ALERT FOR REV 2 PRESS FAULT, AND RED U/L ALERT. ON ARRIVAL A VISUAL CHECK OF REVERSER SHOWED FULLY STOWED, IAW CREW DEBRIEF WHEN THE THROTTLE WAS REDUCED TO FLIGHT IDLE, ALL INDICATIONS EXTINGUISHED. CHECKED FCC 1 AND FCC 2 SENSOR READOUTS, THRUST REVERSER POSITION LEFT AND RIGHT CHANNELS A AND B ALL INDICATE 0.00%.

Part: ACTUATOR — DAMAGED (THRUST REVERSER) · airframe 80,450 hrs · 19,249 cycles

PDIS 603 78-30 6952 09OCT19 PHX OPEN U LOGPAGES:3159490 ON CLIMBOUT RECIEVED LEVEL ONE ALERT "REV 2 PRESS FAULT" AND RED U/L ALERT. SHGN 09OCT19 15:20 PHX U ON ARRIVAL VISUAL CHECK OF REVERSER SHOWS FULLY STOWED, PER CREW DEBRIEF WHEN THE THROTTLE WAS REDUCED TO FLIGHT IDLE ALL INDICATIONS EXTINGUISHED. CHECKED FCC 1 AND FCC 2 SENSOR READOUT, THRUST REVERSER POSITION LEFT AND RIGHT CHANNELS A AND B ALL INDICATE 0.00%. COMPLIED WITH FIM 78-30-00-2 UP TO STEP 3, NO REV 2 PRESS FAULT AT THIS TIME. CYCLED #2 T/R AND GOT AMBER REV U/L INDICATION, LEFT SLEEVE DEPLOYS,RIGHT SLEEVE REMAINS STOWED. UPON INSPECTION OF R/H CDU FOUND CDU SEPERATING FROM DRIVESHAFT AT PARTING SURFACE AND FLEXIBLE PNEUMATIC LINE AT CDU BIRDCAGED AT LOWER CONNECTION.REMOVED AND RELACED THRUST REVERSER CENTER DRIVE UNIT UP TO STEP E (1) (Z) IN AMM 78- 31-01-4-1. ADJUSTED REVERSER PER AMM 78-30-00-5-1.OPS CHECKS GOOD PART CHANGED. RH FDBK ACTUATOR ASSY, HONEYWELL ACTUATOR OFF P/N 3269086-28, S/N GRTC0674C. ACTUATOR ON P/N 3269086-28, S/N GRTC0054C

Part: ADC — FAILED (NR 2) · airframe 80,423 hrs · 19,241 cycles

DURING CLIMBOUT, NOTICED FIRST OFFICER'S AIRSPEED AND CAPTAIN AIRSPEED DID NOT MATCH, DETERMINED F/O INDICATOR WAS UNRELIABLE. STANDBY AIRSPEED AND ALTIMETER MATCHED THE CAPTAIN'S, NR 2 ADC FAILED A FUNCTIONAL TEST, R & R THE NR 2 ADC IAW MM 34-16-01-4. OPS CHECKED NORMAL.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 79,562 hrs · 18,971 cycles

IN FLIGHT GOT LEVEL 1 "HYDRA. 2 OFF" ALERT. COMPLIED WITH QRH PROCEDURE AND ALSO REVIEWED THE REFERENCED "HYD. 2 FAIL" QRH PROCEDURE. THE "HYDR. 2 FAIL" ALERT APPEARED DURING CONFIG ON APPROACH. SINCE WE ALREADY REVIEWD THE PROCEDURE, AND WE HAD NO DEGRATION TO ANY CONTROLS, WE CONTINUED & LANDED UNEVENTFUL. REMOVED AND REPLACED #2 ENG DRIVEN HYD PUMP 2R (LOWER) REF MD11 29-11-20-4-1.

Part: TRANSDUCER — FAILED (ZONE 700) · airframe 78,987 hrs · 18,804 cycles

ON CLIMB OF APPROXIMATELY FL220 LEVEL 1 TIRE PRESSORE LOW, WARNING ILLUMINATED. CONSULTED QRH AT APPROXIMATELY 290 RECEIVED LEVEL 2 TIRE FAIL ALERT. CONSULTED QRH AND CONTINUED TO TPE. NORMAL APPROACH AND LANDING WITH ASSITANCE FROM RUNWAY AND LOCAL EMERGENCY EQUIPMENT. VISUAL INSPECTION ALL TIRE CONDITION NORMAL, BTMTP FAULT REVIEW- IN FLT TPI PRESS XDUCR - 02 SENSOR FAIL, TIRE 02 LOW INTMT. TIRE 01 & 02 DIFF PRESS INTMT, TIRE 02 FAILED INTMT. REMOVED NR 2 TIRE HUBCAP FOUND TRANSDCR DAMAGED, R/I TRANSDCR AND BTMTP RTS TEST ALL TEST PASSED, ALL TIRE PRESS CK'D OK FOR SERVICE. PER MM 32-46-03-4 .

Part: SKIN — CRACKED (RT WING) · airframe 77,968 hrs · 18,534 cycles

DURING HIGHFREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON RIGHT HAND WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUT OUT FOUND HOLE #7, #33, #34 AND #36 WITH CRACK INDICATION. (AT BETWEEN STA XORS 690 AND STA XORS 700 ). RIGHT HAND WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT AT STA XORS 690 AND STA XORS 700, 04 EACH HOLES #7, #33, #34 AND #36 BUSHING REPAIR CARRIED OUT AS PER MD11 SRM 57-20-02-2R, REPAIR 5 FIGURE 201. INITAL INSPECTION TO BE CARRIED OUT AT 2,000 FLIGHT CYCLE AFTER BUSHING REPAIR COMPLETION AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2,000 FLIGHT CYCLE BY HIGH FREQUENCY EDDY CURRENT INSPECTION METHOD PER MD11 SRM 57-20-02-2R REPAIR 5 TABLE 201, FIGURE 202 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (FUSELAGE) · airframe 77,968 hrs · 18,534 cycles

EMPENNAGE - AFT ACCESSORY COMPARTMENT, RIGHT HAND SURFACE AREA FOUND SKIN CORROSION AROUND ANCHOR NUT AT STA Y = 2159 TO Y = 2149. LONGERON 33 RIGHT TO LONGERON 35 RIGHT. AFT ACCESSORY COMPARTMENT, RIGHT HAND SURFACE AREA SKIN CORROSION AROUND ANCHOR NUT AT STA Y = 2159 TO Y = 2149 BETWEEN LONGERON 33 RIGHT TO LONGERON 35 RIGHT REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. CORRODED AREA CARRIED OUT REPAIR AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,968 hrs · 18,534 cycles

MAIN DECK CARGO FLOOR SUPPORT FOUND WITH CORROSION AT STA 1902 X = 57. FLOOR SUPPORT CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. ORIGINAL THICKNESS: 0.188 INCH MATERIAL REMOVED: 0.100 INCH, REMAINING THICKNESS: 0.088 INCH. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-OG, FABRICATED FLOOR SUPPORT AS PER DRAWING 7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 77,968 hrs · 18,534 cycles

LEFT HAND WING LEADING EDGE CAVITY FORMER AT STA XOS 1025 FOUND CRACKED. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG AND 51-33-01-OG. FORMER PART NUMBER ARB2920-13 FABRICATED AS PER DRAWING ARB2920 REVISION BB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,968 hrs · 18,534 cycles

RIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 543. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,968 hrs · 18,534 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 655. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,968 hrs · 18,534 cycles

RIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 626. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,968 hrs · 18,534 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 612. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CHAFED (FUSELAGE) · airframe 77,968 hrs · 18,534 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RIGHT HAND STA 535 LONGERON 19 RIGHT. FRAME REPAIR AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,968 hrs · 18,534 cycles

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

Part: DOUBLER — CRACKED (LT WING) · airframe 77,968 hrs · 18,534 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 763. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CHAFED (FUSELAGE) · airframe 77,968 hrs · 18,534 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RIGHT HAND STA 535, LONGERON 24 RIGHT. FRAME REPAIR AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,968 hrs · 18,534 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED AT STA XOS 626. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 77,938 hrs · 18,521 cycles

R1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO TEST INDICATION SYSTEM IS INOP ON PREFLIGHT CHECK. R1 EVAC SLIDE REMOTE PRESS INDICATOR INOP. TRIED TO REPLACE IND KIT (26C17528-2) BUT NO HELP. FOUND R1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO TEST INDICATION SYSTEM BATTERY LOW. REPLACE NEW BATTERY AND TEST NORMAL PER AMM 25-61-04-5.

Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY LIGHTS) · airframe 77,757 hrs · 18,456 cycles

EMERGENCY LIGHT BATTERY 1 LOW ALERT DURING TEST.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 77,724 hrs · 18,438 cycles

SLIDE BOTTLE TEST LIGHT INOP ON L1 DOOR. R&R BULBS ON SLIDE BOTTLE TEST LIGHT ON L1 DOOR & OPS CHECKED GOOD REF AMM 25-61-04-4.

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 77,135 hrs · 18,282 cycles

HYD 1 FAIL, QTY 0.0. REMOVED AND REPLACED NR 1 ENGINE LEFT PUMP (UPPER) PRESSURE HOSE ASSY REF AMM 20-40-01-2.

Part: HINGE — WORN (NOT REPORTED) · airframe 76,337 hrs · 18,057 cycles

FOUND TWO LOBES ON HINGE BEYOND SRM LIMITS EA T1-5310-T0337841 PT1 WAS ISSUED AND COMPLIED WITH.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED · airframe 73,415 hrs · 17,293 cycles

LEVEL 1 ALERT "A-ICE SENSOR FAIL" AT FL350. STAYED ON FOR REMAINDER OF FLIGHT. IDENTIFIED PARTS, (W/KIT) PNEUMATIC PRESSURE. UPGRADED PNEU SYSTEM. CFDS SENSOR READOUT, PSC 1 SHOWED PE1 XXXX AND PSC 2 SHOWED PE1B XXXX. READINGS RETURN TO NORMAL AFTER PSC 1 AND PSC 2 RTS. SENSORS AND PSC NIS. ON ARRIVAL FOUND PSC 1 FAULT REVIEW AND CURRENT FAULT REPORTED "PE1 XXXX" AND PSC #2 FAULT REVIEW AND CURRENT FAULT REPORTED "PE1B XXXX" SENSOR READ OUTS PSC 1&2 SAME. PERFORMED CONTINUITY CHECKS WITH SHAKING OF HARNESSES FROM PSC'S TO PE1 & PE1B IAW SWPM 20-00-09 WITH NO FAULTS NOTED. R & R THE PSC NR 1, & 2 IAW MM 36-10-02-4 AND PE1, PE1B SENSORS IAW MM 36-11-05-4, ALL TESTED NORMAL.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329456A P1, STEP 1F.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A WASREPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-72644C PART 2 STEP 1.F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-7-TO329708 PART 1 STEP 1A AND STEP 1.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1A AND DTEP 1.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OTBD, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09, A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1C.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1STEP 1B AND STEP 1.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1B.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1C.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE SURFACE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT HAND WING - OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750- T0329763 PART 1 STEP 1A AND STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING, OUTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750- T0329763 PART 1 STEP 1A AND STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND WITH SURFACE CORROSION. REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1 STEP 1A AND STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING OUTBD FLAP, INBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO329708 PART 1STEP 1A AND STEP 1.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1A.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE FOUND WITH CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0329763. PART 1 STEP 1B.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING - OUTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE FOUND WITH CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-70329763 PART 1 STEP 1B.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND CORRODED.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1C.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE SURFACE CORROSION. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE FOUND WITH CORROSION. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329760 PART 1 STEP 1C.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1B.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING, OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1C.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND WITH CORROSION. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0329761 PART 1 STEP 1A AND 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING OTBD FLAP OUTBD FWD HINGE (WING SIDE) BARREL NUTS HOLE BORE CORROSION. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0329763 PART 1 STEP 1D.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. A NEW BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72646B PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72651C PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OUTBOARD FLAP VANE FITTING, BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72646B PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100.

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

RIGHT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-72651C PART 5 STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. A NEW BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

LEFT WING OUTBOARD FLAP VANE FITTING BUSHING HOLE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIG 201. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-100680A PART 2 STEP 1E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 73,168 hrs · 17,228 cycles

HFEC INSPECTION CARRIED OUT ON SLOT OUT AREA ON THE LT NOSE LANDING GEAR TRUNNION FITTING AND FOUND ONE CRACK PROPAGATED BS 580. REPAIRED IAW SRM 53-10-14-2R, REPAIR 2, FIG 202. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 755) · airframe 73,168 hrs · 17,228 cycles

MAIN DECK SEAT TRACK FOUND CRACKED AT BS 755, LBL 8. REPAIRED IAW SRM 53- 00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1761-1781) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

MAIN DECK SEAT TRACK FLANGE FOUND CORRODED AT BS 1761 - 1781, RBL 8. REPAIRED IAW SRM 53-00- 52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1541) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

MAIN DECK SEAT TRACK FLANGE CORRODED AT BS 1541, X -47.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

SEAT TRACK FLANGE CORRODED AT STA. 5-73- 5-113, X-27.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 809) · airframe 73,168 hrs · 17,228 cycles

MAIN DECK SEAT TRACK FLANGE DAMAGED AT BS 809, LBL 8.5. REPAIRED IAW SRM 53-00-52- 2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,168 hrs · 17,228 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER CRACKED XOS 734. REPAIRED IAW SRM 57-40- 02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 73,168 hrs · 17,228 cycles

CENTER CARGO BILGE LONGITUDINAL SPLICE FITTING FOUND CRACKED AT LONGERON 52 BS 5-123. REMOVED AND REPLACED WITH NEW SPLICE FITTING IAW SRM 51-33-01-0G. SPLICE FITTING FABRICATED IAW DWG A5A 7114 REV 'J'. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

MAIN DECK SEAT TRACK FLANGE CORRODED AT BS 5-73 - 5-113, X-47.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 755) · airframe 73,168 hrs · 17,228 cycles

MAIN DECK FLOOR SEAT TRACK FOUND CRACKED AT BS 755, RBL 8. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1771) · corrosion level 2 · airframe 73,168 hrs · 17,228 cycles

MAIN DECK SEAT TRACK FLANGE CORRODED AT BS 1771, RBL 47.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,168 hrs · 17,228 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER CRACKED AT XOS 589. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: BEAM — CRACKED (R3 DOOR) · airframe 73,168 hrs · 17,228 cycles

MAIN DECK CARGO COMPARTMENT, R3 DOOR PLUG DOOR AFT STOP CRACKED AT NUMBER 2 DOOR BEAM. REMOVED AND REPLACED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1255) · airframe 73,168 hrs · 17,228 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 73,168 hrs · 17,228 cycles

MAIN DECK FLOOR SEAT TRACK FOUND CRACKED AT STA 695, X=-8.5. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES FROM STA 745 TO STA 665 X=-8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,168 hrs · 17,228 cycles

LEFT WING LEADING EDGE CAVITY WITH BEADED DOUBLER CRACKED AT XOS 734. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,168 hrs · 17,228 cycles

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

Part: SEAT TRACK — CRACKED (BS 735) · airframe 73,168 hrs · 17,228 cycles

MAIN DECK SEAT TRACK FOUND CRACKED AT BS 735, X -8. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1255) · airframe 73,168 hrs · 17,228 cycles

MAIN DECK CARGO COMPARTMENT, R3 DOOR FORWARD LOWER FRAME WEB CRACKED AT BS 1255, BETWEEN LONGERONS 26 - 27R. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (RT WING) · airframe 73,168 hrs · 17,228 cycles

RIGHT WING LEADING EDGE RIB 16 FOUND CRACKED AT XOS 1003. RIB REMOVED AND REPLACED IAW SRM 51-31-01-0G AND, SRM 51-33-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LE SLAT) · airframe 73,111 hrs · 17,210 cycles

LEFT WING LE DROOP EXTERIOR SKIN FOUND CRACKED. LE DROOP ASSEMBLY REMOVED AND REPLACED WITH SERVICEABLE ASSEMBLY AS PER AMM 27-80-10-4 REVISION 79.1 LEADING EDGE DROOP ASSEMBLY ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-10-5 REVISION 79.1. FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 122.

Part: FRAME — DENTED (FUSELAGE) · airframe 73,111 hrs · 17,210 cycles

CABIN LT STATION 1661 L12 FRAME FOUND DENT. DENTED AREA REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 56 REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 FLIGHT CYCLES, REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES TO BE CARRIED OUT AS PER SRM 53-00-07 TABLE 201 REPAIR 2 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.

Part: VANE — DELAMINATED (TE FLAP) · airframe 73,111 hrs · 17,210 cycles

LEFT WING INBD FLAP VANE FOUND DELAMINATED AT LOWER SURFACE AS MARKED. AREA REPAIRED AS PER SRM 57-50-80 FIGURE 201 REPAIR 2 PARAGRAPH 2A(2)A(2) REV 56 AND EA 1-5750-T0310448 PART 1 TITLE: "WINGS - FLIGHT SURFACES - LT WING - INBD FLAP VANE ASSY - LOWER SURFACE - SRM REPAIR - RSC TRACKING" REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.

Part: SKIN — CRACKED (ZONE 200) · airframe 73,037 hrs · 17,185 cycles

NR 1 PACK BAY DOOR CUT OUT HAS TWO POTENTIAL CRACKS IN PREVIOUS REPAIR DOUBLER & TRIPLER. BOTH APPROX 1.5 INCHES LONG REQUESTED NDT TO DETERMINE IF CRACKED. PERFORMED HFEC IAW NTM PT6 TO VERIFY TWO POTENTIAL CRACKS, CRACKS VERIFIED & ADDITIONAL CRACK NOTED & VERIFIED IN SAME AREA. REPAIR INSTALLED IAW SRM-53-20-15 REPAIR 3.

Part: LAMP — INOPERATIVE (R1 DOOR) · airframe 71,153 hrs · 16,584 cycles

FOUND R1 DOOR PRESS TO TEST LAMP INOPERATIVE DURING SERVICE CHECK. R & R R1 DOOR PRESS TO TEST LAMP IAW REF TO AMM CHAPTER 25-61-04-4, SYS TESTS GOOD.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,168 hrs · 15,651 cycles

MAIN DECK AUXILLIARY TANK UPPER SURFACE AT STA 1229, X=-85 TO -95 FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REV.50 ORIGINAL THICKNESS : 0.160 INCH, MATERIAL REMAINED: 0.106 INCH, MATERIAL REMOVED: 0.054 INCH FOUND EXCEEDED LIMIT AS PER SRM 57-10-01 FIGURE 101 REV. 50 REPAIRED AS PER EA 1-5730-160997. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 300) · airframe 68,168 hrs · 15,651 cycles

RT INTAKE DUCT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-30-02 REPAIR 2 FIGURE 201 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER FEDEX GMM 6-2-100 REVISION 115

Part: CARGO TRACK — CRACKED (BS 635) · airframe 68,168 hrs · 15,651 cycles

MAIN DECK CARGO TRACK AT BS 635, X=-8.5, FOUND CRACKED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — WORN (BS 755) · airframe 68,168 hrs · 15,651 cycles

MAIN DECK CARGO TRACK AT BS 755, X= 47 , FOUND CROWN WORN. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: SEAT TRACK — WORN (ZONE 200) · airframe 68,168 hrs · 15,651 cycles

MAIN DECK CARGO TRACK AT BS 755, X= 27 , FOUND CROWN WORN. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 68,168 hrs · 15,651 cycles

LEFT WING INBD FLAP UPPER SKIN FOUND CRACKED. REPAIR CARRIED OUT AS PER EA 1-5750-162576 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — DAMAGED (ZONE 200) · airframe 68,168 hrs · 15,651 cycles

MAIN DECK CARGO TRACK AT BS 635, X= 27" HAS A CROWN HOLE ELONGATED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — DELAMINATED (NR 1 SPOILER) · airframe 68,168 hrs · 15,651 cycles

RT WING NR 1 SPOILER UPPER SURFACE FOUND DELAMINATED. SPOILER REMOVED AS PER AMM 27-60-02-4 REV.72.1 AND REPLACED AS PER E.A.#15750-162577 PART 1. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 115

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 68,168 hrs · 15,651 cycles

MAIN DECK CARGO TRACK AT STATION 635, X=-27 FOUND CROWN HOLE ELONGATED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 68,168 hrs · 15,651 cycles

MAIN DECK CARGO TRACK AT STATION 755, X=-47 HAS A CROWN HOLE ELONGATED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115

Part: CARGO TRACK — DAMAGED (ZONE 200) · airframe 68,168 hrs · 15,651 cycles

MAIN DECK CARGO TRACK AT STATION 635, X= 47" HAS A CROWN HOLE ELONGATED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115

Part: SKIN — CRACKED (RT WING) · airframe 68,168 hrs · 15,651 cycles

RT WING FIXED L/E AT STATION XOS =717 SLAT TRACK CUTOUT OTBD CORNER CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02 REPAIR 7 FIGURE 201 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SLIDE — NO TEST (R1 DOOR) · airframe 66,772 hrs · 15,244 cycles

R1 DOOR SLIDE DOES NOT PRESS TO TEST DURING TROUBLESHOOTING, SWAPPED LIGHT MODULES AND REPLACED BATTERIES WITH NO HELP. R & R BUILDS IAW SMP, OPS CHECKED NORMAL.

Part: FUEL TANK — CONTAMINATED · airframe 65,124 hrs · 14,797 cycles

ENG 1, FUEL FILTER, LEVEL 1 ALERT INFLIGHT, FL 340, RECEIVED FUEL CONTAMINATION LEVEL 1 ALERT. THEN FUEL FILTER ENG 2 LEVEL 1. CHECKED AND REPLACED ALL 3 ENG FUEL FILTERS AND APU FILTER, FOUND CONTAMINATION. MILKY AND TOILET PAPER LIKE SUBSTANCE. SUMPED 1 AND 3 TANKS AND FOUND SIMILAR CONTAMINATION. UNABLE TO SUMP FUEL OUT OF NR 2 TANK. CONTACTED MOCC WITH UPDATE. CONTACTED LOCAL VENDORS FOR DEFUELING AND WAS TOLD THAT THEY WOULD NOT. ALL CONTAMINATION CLEANED IN ALL TANKS BY FCC VENDOR IAW WO 5110376. ACFT OK FOR SERVICE. FINAL CLOSED.

Part: SEAT TRACK — CORRODED (BS 1598) · corrosion level 2 · airframe 62,996 hrs · 14,331 cycles

MAIN DECK CARGO, AFTER REMOVAL OF FLOOR PANEL (282GF) WITH CORRODED FERRULES FOUND SEAT TRACK FLANGE CORRODED AT STA 1598 X= 107.25. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. FOUND EXCEEDED LIMIT AS PER SRM 53-00-52 FIGURE 101 REVISION 44. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 53-00-52 FIGURE 201 REVISION 44. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111

Part: SEAT TRACK — CORRODED (BS 1701-1785) · corrosion level 2 · airframe 62,996 hrs · 14,331 cycles

MAIN DECK CARGO SEAT TRACK RBL 106 CORRODED AT STATION 1701 TO STATION 1785. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. ORIGINAL THICKNESS= 0.080"; MATERIAL REMOVED= 0.050"; MATERIAL REMAINED= 0.030" FOUND EXCEEDED LIMIT AS PER SRM 53-00-52 FIGURE 101 REVISION 44. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 53-00-52 FIGURE 201 REVISION 44 FROM STA 1701 TO STA 1785 AND E.A. 1-5310-143426. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CRACKED (BS 1541) · airframe 62,996 hrs · 14,331 cycles

MAIN DECK CARGO COMPARTMENT - SEAT TRACK CRACKED AT STATION 1541 LBL 47. MAIN DECK CARGO COMPARTMENT - SEAT TRACK REMOVED AND REPLACED AS PER SRM 53-00-52 FIGURE 201 REVISION 44 FROM STA 1531 TO STA 1571 , X= 47.25. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (BS 1610-1750) · corrosion level 2 · airframe 62,996 hrs · 14,331 cycles

MAIN DECK CARGO - AFTER REMOVAL OF FLOOR PANEL (282GF) WITH CORRODED FERRULES FOUND SEAT TRACK FLANGE CORRODED AT STATION 1610 TO STATION 1750 X= -75. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. FOUND EXCEEDED LIMIT AS PER SRM 53-00-52 FIGURE 101 REVISION 44. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 53-00-52 FIGURE 201 REVISION 44 FROM STA 1610 TO STA 1750. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111

Part: SKIN — CRACKED (ZONE 500) · airframe 62,996 hrs · 14,331 cycles

HFEC OPEN HOLE CARRIED OUT AND FOUND 04 EA HOLES WITH CRACK INDICATION AT LT WING OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STA XORS= 683.4 AND XORS= 713.6. REPAIRED HOLES AS PER SRM 57-20-02 REVISION 44 REPAIR 4 AND DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 62,996 hrs · 14,331 cycles

HFEC OPEN HOLE CARRIED OUT AND FOUND 02 EA HOLES WITH CRACK INDICATION AT RT WING OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STATION XORS= 683.4 AND XORS= 713.6. REPAIRED HOLES AS PER SRM 57-20-02 REVISION 44 REPAIR 4 AND DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (BS 1281) · corrosion level 2 · airframe 62,996 hrs · 14,331 cycles

MAIN DECK CARGO - SEAT TRACK AT STA 1281 X= 47.5 FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. ORIGINAL THICKNESS= 0.100"; MATERIAL REMOVED= 0.050"; MATERIAL REMAINED= 0.050" FOUND EXCEEDED LIMIT AS PER SRM 53-00-52 FIGURE 101 REVISION 44. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 53-00-52 FIGURE 201 REVISION 44 FROM STA 1250 TO STA 1370 X=47.5. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,996 hrs · 14,331 cycles

MAIN DECK CARGO - SEAT TRACK AT STA 1717 X= -27 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK CROWN AREA CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. ORIGINAL THICKNESS= 0.100"; MATERIAL REMOVED= 0.050"; MATERIAL REMAINED= 0.050" FOUND EXCEEDED LIMITS AS PER SRM 53-00-52 FIGURE 101 REVISION 44. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 53-00-52 FIGURE 201 REVISION 44 FROM STA 1670 TO STA 1730 X= 27. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,715 hrs · 14,269 cycles

FLT 5034/06, FLIGHT CREW STATED THE ACFT ENCOUTERED SEVERE TURBULENCE AT 10,000 FT MSL. THE CAPTAIN REPORTS LOOSING 700 FT AND EXPERIENCING MOMENTARY STICK SHAKER. COMPLY WITH MM 05-51-01-6 EXCESSIVE MANEUVER OR TURBULENCE - OVERLOAD CONDITON. COMPLY WITH ALL CHECKS IN AREA A-CHECK INSPECTED AREA B-CHECK INSP IS REQUIRED ONLY IF DAMAGE IS FOUND DURING THE A INSP. REMOVE OR DOWN LOAD FLIGHT DATA RECORDER FOR FLIGHT SAFETY. DOWNLOAD & TRANSFER DATA MM 31-31-00-2. COMPLETED ALL ITEMS PERFORMED INSP IAW MM 05-51-01-6. NO FAULTS FOUND, ACFT OK FOR SERVICE.

Part: SWITCH — FAILED (DETECTOR) · airframe 61,177 hrs · 13,933 cycles

ON CLIMBOUT, WINDSHEAR DETECT FAIL AND ALT COMPARATOR ALERTS ILLUMINATED, CONSISTENT WITH POTENTIAL CADC FAILURE. SHORTLY THEREAFTER WE LOST ALL FCP FUNCTIONS. A/P UNABLE TO HOLD ALTITUDE, CONSIDERING HISTORY OF ACFT WITH CADC PROBLEMS AND LOSS OF UNRELIABLE AIRSPEED INDICATION, DECISION MADE TO DIVERT IAW GOC. LANDED CDG WITHOUT INCIDENT. MX REMOVED AND REPLACED AIR DATA SWITCHING UNIT AS PER AMM 34-16-13-5 OPS CK GOOD.

Part: BRAKE — DAMAGED (MLG) · airframe 61,004 hrs · 13,894 cycles

BRAKE DIFF TEMP ALERT CLIMBOUT. TEMPS ON LT MAIN TRUCK WERE : NR1-72, NR 2-387, NR 3-95, NR 4-127 DEGREES. NR 2 BRAKE TEMP WAS CONTINUING TO INCREASE. GEAR EXTENDED TO EXPEDITE COOLING. WHEN TEMP DECREASED TO 225, GEAR WAS RETRACTED. INSPECTED NR 2 BRAKE, FOUND BRAKE DISK BROKEN AND VERY HARD TO SPIN WITH AXLE ON JACK. R & R NR 2 BRAKE ASSY IAW AMM 32-43-20-4. OPS CHECK SATISFACTORY. ACFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION OFF MFG 2609472-4, POS 2 SRL B2857, TAG 3758C4 ON MFG 2609472-4 SRL B0591, TAG 44218B INSPECTED NR 2 BRAKE, FOUND BRAKE DISK BROKEN AND VERY HARD TO SPIN WITH AXLE ON JACK. R & R NR2 BRAKE ASSY IAW AMM 32-43-20-4. OPS CHECK SATISFACTORY. ACFT OK FOR SERVICE.

Part: CANISTER — FIRE (CARGO BAY) · airframe 59,606 hrs · 13,605 cycles

LEVEL 3 LOWER FWD CARGO FIRE INDICATION DURING LANDING ROLLOUT. FIRE BOTTLE DISCHARGED. BOTTLES WERE BLOWN DUE TO CARGO FIRE IN ONE LD3 CAN. THE CAN WAS REMOVED FROM ACFT AND FIRE WAS EXTIGUISHED BY FIRE DEPARTMENT. INSPECTED FWD CARGO COMPARTMENT AND NO DAMAGE FOUND.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 58,344 hrs · 13,268 cycles

EXISTING DOUBLER REPAIR ON RT FUSELAGE STA 1093, LONGERON 38-39. EXISTING DOUBLER REPAIR ON THE RT FUSELAGE STA 1093, LONGERON 38-39 EVALUATED AND FOUND NOT CARRIED OUT IN ACCORDANCE WITH ANY REPAIR SCHEME. EXISTING DOUBLER REPAIR ON THE RT FUSELAGE STA 1093, LONGERON 38-39 RE-EVALUATED AND REPAIR FOUND CARRIED OUT IN ACCORDANCE WITH SRM 53-20-00 FIG 6 VOL I AND EA 1-5330-127893, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: ANGLE — CRACKED (ZONE 300) · airframe 58,344 hrs · 13,268 cycles

EMPENNAGE, AFT FUSELAGE UPPER AFT DOG HOUSE AFT BULKHEAD LOWER ANGLE STIFFENER SUSPECT CRACKS AT 3 LOCATIONS. CRACKS AT 03 LOCATIONS ON EMPENNAGE AFT FUSELAGE UPPER AFT DOG HOUSE AFT BULKHEAD LOWER ANGLE STIFFENER TRIMMED OUT AND CARRIED OUT REPAIR AS PER EA 1-5310- 127765, THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STOP FITTING — CRACKED (L4 DOOR) · airframe 58,344 hrs · 13,268 cycles

CABIN, L4 DOOR FWD 3RD FROM BOTTOM STOP FITTING CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 58,344 hrs · 13,268 cycles

LT WING OTBD FLAP FWD OTBD HINGE ACTUATOR INBD BORE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-127737, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · airframe 58,344 hrs · 13,268 cycles

RT WING, OTBD FLAP OTBD FWD HINGE ACTUATOR ATTACH INBD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-127738. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · airframe 58,344 hrs · 13,268 cycles

RT WING, OTBD FLAP OTBD FWD HINGE ACTUATOR ATTACH OTBD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-127738, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 58,344 hrs · 13,268 cycles

FIVE FASTENER HOLES, FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS=690 AND STA XORS-700.

Part: FORGING — CORRODED (L3 DOOR WINDOW) · airframe 58,344 hrs · 13,268 cycles

CABIN, L3 DOOR EXTERIOR WINDOW FORGING, FOUND CORROSION.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,344 hrs · 13,268 cycles

RT WING, OTBD FLAP OTBD FWD HINGE AFT LOWER ATTACH HOLES FWD AND AFT FACE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-127739, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND ON HOLE NR C ON FIRST SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 1 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND ON HOLE NR D ON FIRST SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 6 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND ON HOLE NR A ON FIRST SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 3 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 58,344 hrs · 13,268 cycles

LOWER CENTER CARGO COMPARTMENT BILGE AREA AT STATION 5-123, LONGERON 49 LEFT SPLICE FITTING FOUND 1 INCH CRACKED.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON HOLE NR A ON SECOND SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 3 FITTING.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON HOLE NR D ON SECOND SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 6 FITTING.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON HOLE NR A ON SECOND SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 1 FITTING. REPAIR CARRIED OUT AS PER E.A. 1-5310-127741, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND ON HOLE NR D ON FIRST SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 1 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIR CARRIED OUT AS PER EA 1-5310-127741, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · airframe 58,344 hrs · 13,268 cycles

LOWER CENTER CARGO COMPARTMENT BILGE AREA AT STATION 1701, LONGERON 48 RIGHT FOUND WITH CORROSION.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 58,344 hrs · 13,268 cycles

LEFT INBOARD FLAP UPPER SURFACE FOUND WITH EXISTING DOUBLER REPAIR AT OUTBOARD SEGMENT. EXISTING DOUBLER REPAIR AT LT INBOARD FLAP UPPER SURFACE OUTBOARD SEGMENT EVALUATED AND FOUND NOT CARRIED OUT IN ACCORDANCE WITH SRM 57-10-00 FIG 38 VOL I. EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-35-01 VOL II AND NEW REPAIR INSTALLED AS PER SRM 57-10-00 FIG 38 VOL I EO 1-5100-7-5001, REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATIONS FOUND ON HOLE NR A ON FIRST SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 1 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

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

Part: FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CABIN, RIGHT STATION 1781 LONGERON 13 RIGHT FRAME SPLICE FOUND CRACKED. FABRICATED AS PER DRAWING AFA0030. SPLICE REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND ON HOLE NR C ON FIRST SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 2 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION.

Part: STRUCTURE — DELAMINATED (RT WING TE FLAP) · airframe 58,344 hrs · 13,268 cycles

RIGHT WING INBOARD FLAP VANE LOWER SURFACE FOUND WITH DELAMINATION.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLE NR A, NR C AND NR D. CRACKED NR 3 SUPPORT FITTING AT MAIN CARGO DOOR LOWER JAMB AREA REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II AND REPAIR BUSHING INSTALLED AS PER 53-50-00 FIG.10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLE NR A, NR B, NR C AND NR D. CRACKED NR 2 SUPPORT FITTING AT MAIN CARGO DOOR LOWER JAMB AREA REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II AND REPAIR BUSHINGS INSTALLED AS PER SRM 53-50-00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND ON HOLE NR A ON SECOND SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 7 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLE NR A, NR. B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. AND REPAIR BUSHINGS INSTALLED AS PER SRM 53-50-00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLE NR A AND NR B.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND ON HOLE NR B ON FIRST SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 2 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND ON HOLE NR D ON FIRST SKIN LAYER IN MAIN CARGO DOOR LOWER JAMB NR 2 FITTING DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE NR A, NR B, NR C AND NR D.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,344 hrs · 13,268 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE NR A.

Part: ACTUATOR — BROKEN (THRUST REVERSER) · airframe 57,343 hrs · 13,058 cycles

FOUND NR 1 LT T/R DAMAGED. FOUND LT LWR SCREWJACK BROKE OFF AND DAMAGED THE TRANSLATING COWL, DAMAGED PARTS FOUND AT RUNWAY TOUCH DOWN AREA. VISUALLY INSPECTED LT WING, FLAP, AFT FUSELAGE, STAB SURFACE AND NO DAMAGE FOUND. MANUAL DEPLOY AND STOW NR 1 RT REVERSER HALF AND FOUND OK. REVERSER P/N MUST BE 683L216G04 FOR NR1 LT CONFIG PER IPC. REMOVED AND REPLACED NR 1 ENGINE LT T/R COWL AS PER MM 78-33-01-4 AND CARRIED OUT ADJUSTMENT TEST PER MM 78-30-00-5. ALL CHECKED NORMAL. ACFT OK FOR SERVICE. CLOSED ALL NR 1 ENGINE COWLS PER MM 71-10-00.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 54,375 hrs · 12,425 cycles

AFTER SELECTING GEAR DOWN RECEIVED ANTI-SKID R FAIL AND RT MAIN GEAR RED UNSAFE LIGHT. EXECUTED GO-AROUND. RECYCLED MAIN GEAR ONLY TO HAVE BOTH ALERTS APPEAR AGAIN. COMPLIED WITH QRH PROCEDURES AND LANDED ON LONGEST RWY FLAPS 50 WITHOUT INCIDENT. REMOVED AND REPLACED FWD RT MLG DOWN AND LOCKED SENSOR (D1-43).

Part: PRESSURE SWITCH — MALFUNCTIONED (OIL SYSTEM) · airframe 54,359 hrs · 12,420 cycles

DURING CRUISE FLIGHT, GOT A LEVEL 2 ALERT "ENG 2 OIL FILTER". THIS ALERT DID NOT GO AWAY, EVEN WITH THROTTLE IDLE. ENGINE SHUT DOWN IAW QRH NO OTHER ABNORMAL INDICATIONS. REPLACED OIL FILTER DIFFERENTIAL PRESSURE SWITCH PER MM 79-35-01-4. REFLUSH NR 2 ENG OIL SYS PER MM 12-12-01-3 AND INSPECTION MASTER CHIP DETECTOR PER MM 79-36-01-6. REPLACED NR 2 ENG OIL SCAVENGE FILTER PER MM 79-22-04-4. ALL NO DSIC FOUND PER MM 79-22-04-6. RAN NR 2 ENG PER MD-11 JRH ALL PARAMETER NORMALLY.

Part: STRUCTURE — CRACKED (ZONE 600) · airframe 53,277 hrs · 12,190 cycles

RIGHT WING, NR 1 LEADING EDGE SLAT INBOARD EDGE FILLET ASSEMBLY ALIGNMENT PIN HOLE FOUND CRACK. [08-17-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-114770, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: TRUNNION — CHAFED (ZONE 700) · airframe 53,277 hrs · 12,190 cycles

CENTER LANDING GEAR LEFT MOUNTING TRUNNION FITTING BOTTOM SURFACE FOUND WITH CHAFED MARK. [08-03-07] REPAIR CARRIED OUT AT CENTER LANDING GEAR LEFT HAND MOUNTING TRUNNION FITTING BOTTOM SURFACE AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 53,277 hrs · 12,190 cycles

CENTER LANDING GEAR RIGHT TRUNNION FITTING FOUND WITH CORROSION. [08-03-07] REPAIR CARRIED OUT AT CENTER LANDING GEAR RIGHT HAND TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 53,277 hrs · 12,190 cycles

CENTER LANDING GEAR MOUNTING LEFT TRUNNION FITTING FOUND WITH CORROSION. [08-03-07] REPAIR CARRIED OUT AT CENTER LANDING GEAR MOUNTING LEFT HAND TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 53,277 hrs · 12,190 cycles

CRACK INDICATIONS REVEALED IN FASTENER HOLE TOWARDS EDGE OF ACCESS CUTOUT IN RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT (PANEL 636AB). [08-09-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112366, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 53,277 hrs · 12,190 cycles

CRACK INDICATIONS REVEALED IN FASTENER HOLE TOWARDS EDGE OF ACCESS CUTOUT IN LEFT WING LOWER SKIN ACCESS DOOR CUTOUT (PANEL 536AB). [08-09-07] REPAIR CARRIED OUT IN FASTENER HOLE TOWADS EDGE OF ACCESS CUTOUT IN LT WING LOWER SKIN ACCESS DOOR CUTOUT (PANEL 536AB) AS PER FEDEX EA 1-5710-112365, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 53,277 hrs · 12,190 cycles

CENTER LANDING GEAR LEFT MOUNTING TRUNNION FITTING CENTER GUIDE HOLE FOUND WITH CORROSION. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-112364, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: REDUCER — BROKEN (HYD SYSTEM) · airframe 50,174 hrs · 11,474 cycles

HYD 3 FAIL LEVEL 2 ALERT AT ALTITUDE. QUANTITY .2, PUMPS OFF WHEN SD CHECKED. DIVERTED TO KIX. FOUND NR 3 HYD RESERVOIR DRAIN VALVE REDUCER IS BROKEN. REMOVED REMAINING PART OF REDUCER THREAD & CAPPED TO RELEASE A/C WITH EA REMOVED AND INSPECTED. SYS AND ENG HYD MANIFOLD FILTERS, FOUND NORMAL. INSTALLED NEW FILTERS IAW MM. C/W E.A.1-2910-102928 PT-1. SERVICED HYD FLUID AND LEAK CKD OK. RETURNED TO SERVICE.

Part: FITTING — CORRODED (ZONE 600) · airframe 49,908 hrs · 11,426 cycles

RIGHT HAND WING FLAP VANE SUPPORT NR 4 TO TRACK FOUND WITH CORROSION. RIGHT HAND WING FLAP VANE SUPPORT NR 4 TO TRACK CORROSION REPAIRED AS PER FEDEX EA 1-5750-100683, WINGS - RIGHT HAND NR 4 FLAP VANE TO TRACK SUPPORT CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 600) · airframe 49,908 hrs · 11,426 cycles

RIGHT HAND WING FLAP VANE SUPPORT NR 2 TO TRACK FOUND WITH CORROSION. RIGHT HAND WING FLAP VANE SUPPORT NR 2 TO TRACK CORROSION REPAIRED AS PER FEDEX EA 1-5750-100681, WINGS - RIGHT HAND NR 2 FLAP VANE TO TRACK SUPPORT CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CORRODED (T/E FLAP) · airframe 49,908 hrs · 11,426 cycles

LEFT HAND WING OUTBOARD FLAP VANE FITTING ON NR 2 TRACK FOUND WITH CORROSION. LEFT HAND WING OUTBOARD FLAP VANE FITTING ON NR 2 TRACK CORROSION REPAIRED AS PER FEDEX EA 1-5750-100680. LEFT HAND NR 2 FLAP VANE TO TRACK SUPPORT CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 600) · airframe 49,908 hrs · 11,426 cycles

RIGHT HAND WING FLAP VANE SUPPORT NR 3 TO TRACK FOUND WITH CORROSION. RIGHT WING FLAP VANE SUPPORT NR 3 TO TRACK CORROSION REPAIRED AS PER FEDEX EA 1-5750-100682, WINGS - RIGHT HAND NR 3 FLAP VANE TO TRACK SUPPORT CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 49,908 hrs · 11,426 cycles

WASTE TANK COMPARTMENT CEILING AREA, MAIN DECK FLOOR STRUCTURE HAT SECTION CORRODED AT STA 1967 TO STA 2007, LBL 20. WASTE TANK COMPARTMENT CEILING AREA, MAIN DECK FLOOR STRUCTURE HAT SECTION CORRODED AT STA 1967 TO STA 2007, LBL 20. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7088. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1902-2007) · airframe 49,908 hrs · 11,426 cycles

MAIN DECK UPPER CARGO FLOOR SUPPORT AT STA 1902 TO STA 2007 RBL 27, FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 660) · airframe 49,908 hrs · 11,426 cycles

MAIN DECK UPPER CARGO AT STA 660 RBL 101.2 SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53-70-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 49,908 hrs · 11,426 cycles

AFT CARGO COMPARTMENT, FLOORBEAM UPPER CHORD CORRODED AT STA 1902, LONGERON 49R TO LONGERON 49L. CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5310- 100700, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 670) · airframe 49,908 hrs · 11,426 cycles

MAIN DECK UPPER CARGO AT STA 670 RBL 75.2 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-70-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER 6-2-100.

Part: FAIRING — CORRODED (ZONE 500) · airframe 49,908 hrs · 11,426 cycles

FOUND LEFT WING OUTBOARD FLAP INBOARD AFT HINGE FAIRING, FORWARD MATING SURFACE OUTBOARD MIDDLE HOLE FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX E.A. #1-5750-100669, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FAIRING — CORRODED (ZONE 500) · airframe 49,908 hrs · 11,426 cycles

FOUND LEFT WING OUTBOARD AFT HINGE FAIRING, AFT MATING SURFACE AFT HOLE FOUND WITH CORROSION. CORROSION REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-100670.

Part: SUPPORT FITTING — DAMAGED (ZONE 800) · airframe 49,908 hrs · 11,426 cycles

FOUND MAIN DECK COMPARTMENT, L4 DOOR LOWER SUPPORT FITTING ASSEMBLY DAMAGED NR 2 FROM LOWER. CARRIED OUT REPAIR AS PER FEDEX E.A. #1-5210-100679, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 49,908 hrs · 11,426 cycles

FOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING FOUND AFT MATING SURFACE AFT HOLE WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX E.A. #1-5750-100671

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 49,908 hrs · 11,426 cycles

FOUND RIGHT WING OUTBOARD FLAP OUTBOARD HINGE FITTING FORWARD OUTBOARD MATING SURFACE MIDDLE HOLE WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX E.A. #1- 5750-100672,

Part: TRUNNION — CRACKED (NLG) · airframe 49,908 hrs · 11,426 cycles

SNRM N00531: NOSE LANDING GEAR, GEAR AT TRUNNION WEB LEFT HAND SIDE SUSPECT CRACK. STOP DRILL DEVIATION FROM SRM. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SKIN — DENTED (T/E FLAP) · airframe 49,908 hrs · 11,426 cycles

SNRM N00367: LEFT HAND WING INBOARD FLAPS OUTBOARD SEGMENT LOWER SURFACE FOUND WITH 3EA DENTS. REPAIRED AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: TRUNNION — CRACKED (NLG) · airframe 49,908 hrs · 11,426 cycles

SNRM N00533: NOSE LANDING GEAR - GEAR AT TRUNNION WEB RIGHT HAND SIDE SUSPECT CRACK. REPAIR CARRIED OUT AS PER SRM 53-40-00 FIG.22 VOL.I CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 49,908 hrs · 11,426 cycles

RIGHT HAND WING - 3EA FASTENER HOLES FOUND CRACKED ON ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713.6, STRINGER 36, LOWER SKIN PANEL. COMPLIED WITH FEDEX E.A. #1-5710-100665, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 49,908 hrs · 11,426 cycles

SNRM N00955: LEFT HAND WING - 3EA FASTENER HOLES FOUND CRACKED ON ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713-6, STRINGER 36, LOWER SKIN PANEL. COMPLIED WITH FEDEX E.A. #1-5710-100663

Part: SKIN — DENTED (T/E FLAP) · airframe 49,908 hrs · 11,426 cycles

SNRM N00143: LEFT HAND WING INBOARD FLAPS LOWER SURFACE FOUND WITH SEVERAL DENTS. DENTS FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I. DENT AREAS TRIMMED OFF AND REPAIR IS CARRIED OUT ON TRIMMED OFF AREAS AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STOP FITTING — CRACKED (R3 DOOR) · airframe 49,908 hrs · 11,426 cycles

SNRM N00892: MAIN DECK CABIN DOOR R3 FORWARD EDGE, NR 3 STOPPER FITTING AS FROM BOTTOM, FOUND CRACKED. REMOVED AS PER SRM 51-31-01 VOLUME II. FASTENER HOLES TRANSFERED AS PER SRM 51-31-01 VOLUME II. NEW FITTING INSTALLED AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,908 hrs · 11,426 cycles

FAC AT APPROX STA 390 TO 401 LBL 36 CEILING FOUND CABIN FLOOR SUPPORT CRACKED. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · airframe 49,908 hrs · 11,426 cycles

SNRM N00579: LEFT HAND WING REAR SPAR UPPER CAP AT STA XORS 1042 FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710-100689.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,908 hrs · 11,426 cycles

CENTER CARGO COMPARTMENT BILGE AREA, LONGERON 50L FOUND CRACKED AT STA 1705. TRIMMED OUT AS PER SRM 53-10-00 FIGURE 1 VOLUME I. NEW REPAIR LONGERON MACHINED AS PER DRAWING AFA7772. NEW SPLICE MACHINED AS PER FEDEX E.A. #1-5310-100675

Part: STRUCTURE — DENTED (T/E FLAP) · airframe 49,908 hrs · 11,426 cycles

RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT FOUND WITH SEVERAL DENTS. DENTS ON RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT REPAIRED AS PER SRM 57 -10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 49,908 hrs · 11,426 cycles

SNRM N00734: MAIN DECK CABIN SEAT TRACK AT STA 635 RBL 47 FOUND WITH CHAFFING MARK. REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · airframe 49,908 hrs · 11,426 cycles

SNRM N00385: LEFT HAND WING REAR SPAR UPPER SURFACE OF THE SPAR CAP AT STA 970 TO 980 FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710-100688.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,908 hrs · 11,426 cycles

CENTER CARGO COMPARTMENT BILGE AREA, LONGERON 49L FOUND CRACKED AT STA 1705. TRIMMED OUT AS PER SRM 53-10-00 FIGURE 1 VOLUME I. NEW REPAIR LONGERON MACHINED AS PER DRAWING AFA7772. NEW SPLICE MACHINED AS PER FEDEX E.A. 1-5310-100666.

Part: SPAR CAP — CORRODED (RT WING) · airframe 49,908 hrs · 11,426 cycles

SNRM N00394: RIGHT HAND WING REAR SPAR UPPER CAP BENEATH THE UPPER CLOSE OUT PANEL BETWEEN STA XORS 1042 TO XORS 981 FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710-100690.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 49,908 hrs · 11,426 cycles

SNRM N00493: MAIN DECK CABIN STA 815 LBL 47 SEAT TRACK EDGES FOUND DEEP CHAFED MARK. AREA REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 49,908 hrs · 11,426 cycles

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

Part: STRINGER — CRACKED (LT WING) · airframe 49,908 hrs · 11,426 cycles

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

Part: STRINGER — CRACKED (RT WING) · airframe 49,908 hrs · 11,426 cycles

CRACK FOUND ON RIGHT HAND WING TANK AT THE END OF STRINGER 40 AT XORS 747. REPAIR CARRIED OUT ON SLOTTED OUT AREA AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (T/E FLAP) · airframe 49,908 hrs · 11,426 cycles

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

Part: STRINGER — CRACKED (RT WING) · airframe 49,908 hrs · 11,426 cycles

CRACK FOUND ON RIGHT HAND WING TANK AT THE END OF STRINGER 10 AT XORS 760. SLOTTED OUT AND REPAIR CARRIED OUT AT SLOTTED OUT AREA AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 49,908 hrs · 11,426 cycles

CRACK FOUND ON RIGHT HAND WING TANK AT THE END OF STRINGER 13 AT XORS 577. REPAIR CARRIED OUT AS SPLICE OUT AREA AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 49,908 hrs · 11,426 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT HAND WING TANK AT THE END OF STRINGER 16 AT APPROX XORS 386. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I AND CLIP FABRICATED AS PER FEDEX E.A. 1- 5720-100664, TREPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — DAMAGED (L4 DOOR) · airframe 49,908 hrs · 11,426 cycles

MAIN DECK COMPARTMENT - L4 DOOR LOWER SURFACE FITTING ASSEMBLY FOUND DAMAGED NR 2 FROM LOWER. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II AND CARRIED OUT REPAIR AS PER FEDEX EA 1-5210-100679.

Part: STRINGER — CRACKED (LT WING) · airframe 49,908 hrs · 11,426 cycles

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

Part: STRINGER — CRACKED (RT WING) · airframe 49,908 hrs · 11,426 cycles

CRACK FOUND ON RIGHT HAND WING TANK AT THE END OF STRINGER 11 AT XORS 704. REPAIR CARRIED OUT ON SPLICE OUT AREA AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 45,979 hrs · 10,565 cycles

ABOUT 2.5 HRS FROM TOUCHDOWN, GOT LEVEL 1 HYD 3 OFF, FOLLOWED BY LEVEL 2 HYD 3 FAIL. LOST ALL HYD 3 QTY FOLLOWED QRH PROCEDURES AND DID ALT GEAR EXTENSION. A/C TOWED TO GATE FROM RUNWAY. FLEX LINE INSTALLED IN HYD SYSTEM NR 3 LOCATED AT TRIM MOTOR VALVE BLOCK, HORZ STAB REMOVED AND REPLACED NR 3 ENGINE DRIVEN PUMP PER AMM 29-11-20-4 AND CASE DRAIN MANIFOLD FILTERS FOR LT (UPPER) EDP PER AMM29-12-41-2. BLED EDP AND SUPPLY LINES PER AMM 29-03-00-2. DRY MOTOR THE ENG PER AMM 71-00-00-51 AND PERFORMED LEAK CHECK SATISFACTORY.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 1029, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 805, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: WEB — CORRODED (ZONE 700) · airframe 44,846 hrs · 10,327 cycles

CENTER WHEEL WELL FORWARD LEFT HAND VERTICAL WEB FOUND CRACK APPROXIMATELY 4 INCHES LONG FROM BOTTOM. CRACKED DOUBLER REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 910, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 910, X = -48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 805, X = -28. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 1059, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 1421, X = -8. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 1090, X = -48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 6-80, X = -48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 1126, X = -48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 6-70 TO Y = 6-90, X = -8. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,846 hrs · 10,327 cycles

CABIN SEAT TRACK DAMAGED AT STA Y = 1372, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I.

Part: DCU — MALFUNCTIONED (ZONE 200) · airframe 41,888 hrs · 9,645 cycles

AS PER MEL 28-01-02-02-A MEL HAS MAINTENANCE DEACTIVATE ALL AUX AND TAIL FUEL BOOST PUMP. TOP OF CLIMB NOTICED AUX UPPER RIGHT PUMP LOW ALERT. ALL INDICATION'S OF PUMP ON OVERHEAD AND SYNOPTIC DISPLAY INDICATE PUMP IS RUNNING, WHEN DEACTIVATED. R AND I DCU PER MM 28-41-91-4. REACTIVATE ALL C/B'S, CONNECTORS AND PERFORMED FSC RTS PER MM 28-08-01-5, ALL TEST PASSED.

Part: PUMP — BURNED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

HYD AUXILIARY PUMP NR 2 ELECTRICAL CONNECTOR FOUND ELECTRICALLY SHORTED AND ARCING DAMAGED. AUX ELEC PUMP REMOVED AND REPLACED AS PER AMM 29-21-01. ELECTRICAL: REMOVED AND REPLACED B1-624 RCCB AS PER STANDARD WIRING PRACTICE. REMOVED AND REPLACED NR 2 HYD PUMP ELECT CONNECTOR AS PER STANDARD WIRING PRACTICE. NR 2 PUMP ELECT WIRING INSULATION CHECKED, FOUND SATISFACTORY. PUMP OPS CHECK CARRIED OUT AS PER MM 29-21-01-5, FOUND SATISFACTORY.

Part: HINGE — CRACKED (TAIL CONE) · airframe 40,211 hrs · 9,258 cycles

FWD EXTENDED TAILCONE LT HINGE UPPER ATTACHED FITTING MOUNTED AT FWD FACE OF AFT BULKHEAD STA Y2164 (AFT ACCESSORY COMPT) FOUND WITH 02 EA HAIR LINE CRACKS AS MARKED. FWD EXT TAILCONE LT HINGE UPPER ATTACHED CRACKED FITTING WHICH MOUNTED AT FWD FACE OF AFT BULKHEAD STA Y2164 (AFT ACCESSORY COMPT) REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-33-01 VOL2 & SRM 51-35-01 VOL2 IAW EA 1-5310-73319. NEW FITTING FABRICATED AS PER DWG AJC7346 IAW EA 1-5310-73319 WITH TITLE FUSELAGE - MAIN FRAME - TAILCONE HINGE SUPPORT FABRICATION.

Part: SPLICE — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

POSSIBLE CRACK AT LONGERON SPLICE AT TRANSVERSE SPLICE STA 1540 RT TUNNEL. CTR CARGO STA 1540 LONG 37R CRACK LONGERON SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG N5A6774 AND SRM 51-33-01 VOL 2.

Part: SPLICE — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

CTR CARGO PIT - POSSIBLE CRACK AT STA 5-115 STRINGER SPLICE 46L FLOOR AREA. CTR CARGO STA 5-115 S46L STRINGER CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG N5A6774 AND SRM 51-33-01 VOL 2.

Part: SPLICE — CORRODED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

UPON REMOVAL OF TRANSVERSE SPLICE. FOUND CORROSION ON AFT STRINGER UNDER REMOVED SPLICE. CTR CARGO STA 1541 S48R STRINGER CORROSION REPAIRED AS PER SRM 53-00-01 FIG 3 VOL 1.

Part: SPLICE — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

CENTER CARGO PIT HAS A POSSIBLE CRACK AT STR 47R STA 1540 UNDER PANEL 183CF JUST AFT OF TRANSVERSE SPLICE.

Part: FITTING — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

POSSIBLE CRACKS AT STRINGER SPLICE 39R STA 1540 AT TRANSVERSE SPLICE RT TUNNEL. CTR CARGO STA 1540 STR 39R STRINGER CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG N5A6774 AND SRM 51-33-01 VOL 2.

Part: SPLICE — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

CTR CARGO COMPT - POSSIBLE CRACK AT STA 1541 STRINGER SPLICE 45R. CTR CARGO STA 1541 STR 45R STRINGER CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG NSA6774 & SRM 51-33-01 VOL 2.

Part: SPLICE — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

POSSIBLE CRACK AT STA 1541 STR SPLICE 44R. CTR CARGO STA 1541 STRINGER 44R CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL 2.

Part: SPLICE — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

POSSIBLE CRACK AT STR 51R STA 1540 UNDER PANEL 183CF JUST AFT OF TRANSVERSE SPLICE. CTR CARGO STA 1540 S51R CRACK SPLICE FITTING REMOVED AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-33-01 VOL 2.

Part: SPLICE — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

CENTER CARGO BAY, UPON REMOVAL OF STRINGER SPLICE 48R STA 1541 REF CARD NUMBER N0697 FOUND SUPPORTING BRACKET CRACKED.

Part: SPLICE — CRACKED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

CENTER CARGO PIT HAS A POSSIBLE CRACK AT STA 5-115 STRINGER SPLICE 45L FLOOR AREA.

Part: SPAR CAP — CORRODED (ZONE 300) · airframe 40,211 hrs · 9,258 cycles

REFERENCE EO 1-5510-7-5000: HORIZONTAL STABILIZER LT UPPER END CAP NR 36L BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION AFTER REWORK. HORIZONTAL STAB LT UPPER END CAP 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-73294 STABLIZERS - HORIZONTAL STABILIZER - CORROSION REMOVAL AND REPAIR OF BARREL NUT BORE 36 LEFT HAND SIDE.

Part: SUPPORT BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) INBOARD PIVOT ATTACHMENT BORE BUSHING FOUND LOOSE.

Part: SUPPORT BRACKET — LOOSE (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT ATTACHMENT BORE BUSHING FOUND LOOSE.

Part: BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBD PIVOT LUG INBD AND OUTBD SURFACE FOUND CORRODED.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RIGHT WING I/B FLAP VANE O/B TEE FITTING FWD BORE FOUND CORRODED. CORROSION ON RT WING I/B FLAP VANE O/B TEE FTG FWD BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING I/B FLAP VANE I/B TEE FITTING MID BORE FOUND WITH CORROSION. CORROSION ON RT WING, I/B FLAP VANE, I/B TEE FITTING, MID BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL 2 AND FOUND WITHIN LIMITS.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING I/B FLAP VANE I/B TEE FITTING I/B FACE AND O/B FACE FOUND WITH SURFACE CORROSION. SURFACE CORROSION ON RT WING, I/B FLAP VANE, I/B TEE FITTING, I/B & O/B FACE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL 2 AND FOUND WITHIN LIMITS.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RIGHT WING I/B FLAP VANE I/B TEE FITTING FWD BORE FOUND CORRODED. CORROSION ON RT WING, I/B FLAP VANE I/B TEE FTG FWD BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL 2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RIGHT WING I/B FLAP VANE O/B TEE FITTING AFT BORE FOUND CORRODED. CORROSION ON RT WING I/B FLAP VANE O/B TEE FTG AFT BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING I/B FLAP VANE I/B TEE FITTING AFT BORE FOUND CORRODED. CORROSION ON RT WING I/B FLAP VANE I/B TEE FTG AFT BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RIGHT WING I/B FLAP VANE O/B TEE FITTING I/B AND O/B FACE FOUND WITH SURFACE CORROSION. SURFACE CORROSION ON RT WING I/B FLAP VANE O/B TEE FTG I/B AND O/B FACE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING I/B FLAP VANE O/B TEE FITTING MID BORE FOUND CORRODED. CORROSION ON RT WING I/B FLAP VANE O/B TEE FTG MID BORE REMOVED BY HAND CLEAN AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER DWG ARC7490.

Part: SPLICE — CORRODED (ZONE 100) · airframe 40,211 hrs · 9,258 cycles

CENTER CARGO PIT HAS A DAMAGED STRINGER SPLICE AT STA 1541, 48R AT TRANSVERSE AND LONGITUDINAL SPLICE. DAMAGED STRINGER SPLICE AT STA 1541 48R AT TRANSVERSE AND LONGITUDINAL SPLICE REPAIRED AS PER SRM 53-10-00 FIG 2 SHT 5 IAW EA 1-5310-72657

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING O/B FLAP O/B HINGE (A/C SIDE) I/B ACTUATOR ATTACH BORE FOUND CORRODED.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING O/B FLAP O/B HINGE (A/C SIDE) O/B ACTUATOR ATTACH BORE FOUND CORRODED.

Part: BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (A/C SIDE) ACTUATOR OUTBD ATTACH BORE, FOUND CORRODED.

Part: BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (A/C SIDE) INBOARD ACTUATOR ATTACH BORE FOUND CORRODED.

Part: STRAP — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING INBOARD FLAP OUTBOARD HINGE PIVOT LUG FACE (FLAP SIDE) FOUND CORRODED. LT WING I/B FLAP O/B HINGE PIVOT (O/B LUG O/B FACE) STRAP P/N ARC2518-501. REMOVED AND REPLACED WITH NEW STRAP IAW EA 1-5750-72646, TITLE : WINGS - TRAILING EDGE DEVICES - LT INBOARD FLAP OUTBOARD AFT HINGE PIVOT BORE CORROSION AND EA EA 1-5750-72650

Part: BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (A/C SIDE) OUTBOARD ACTUATOR ATTACH BORE FOUND CORRODED.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LEFT WING O/B FLAP I/B HINGE (A/C SIDE) LOWER ATTACHMENT BORE MATING SURFACE FOUND WITH CORROSION.

Part: SKIN — CORRODED (ZONE 200) · airframe 40,211 hrs · 9,258 cycles

MAIN DECK- CTR AUX TANK UPPER SKIN EXTERIOR SURFACE FOUND CORRODED AT STA 1239, LBL 24. MAIN DECK STA 1239 LBL 24 CTR AUX TANK UPPER SKIN CORROSION REPAIRED AS PER SRM 57-00-01 VOL 1 AND EA 1-5720-72606 FUSELAGE. MAINFRAME - UPPER CTR WING SKIN CORROSION REPAIR.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING O/B FLAP VANE NR 2 FROM I/B TEE FITTING FWD BORE FOUND CORRODED.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING I/B FLAP O/B HINGE (FLAP SIDE) LOWER I/B BORE FOUND CORRODED.

Part: BARREL NUT — CORRODED (ZONE 300) · airframe 40,211 hrs · 9,258 cycles

HOR STAB RT UPPER CENTER PLANK NR 26 RT BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. HORIZONTAL STAB RT UPPER CENTRE PLANK NR 26 RT FITTING REMOVED AND REPLACED AS PER EA 1-5510-72642 STABILIZERS - HORIZONTAL STABILIZER - FITTING ALC 8107-2 FABRICATION.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING O/B FLAP I/B HINGE (A/C SIDE) I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING O/B FLAP VANE NR 4 FROM I/B, TEE FITTING FWD BORE FOUND CORRODED.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING O/B FLAP VANE NR 3 FROM I/B TEE FITTING FWD BORE FOUND CORRODED. RT WING O/B FLAP VANE NR 3 FROM I/B TEE FITTING FWD CORRODED BORE REPAIRED AS PER EA 1-5750-73297.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING O/B FLAP VANE MOST I/B TEE FITTING NR 1 FOUND FORWARD BORE CORRODED. RT WING O/B FLAP VANE MOST I/B TEE FITTING (NR 1) FWD CORRODED BORE REPAIRED AS PER EA 1-5750-73297 WITH TITLE : WINGS - TRAILING EDGE DEVICES - RH O/B FLAP VANE TO TRACK SUPPORT REWORK.

Part: BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RTWING OUTBOARD FLAP INBOARD HINGE (A/C SIDE) INBD ACTUATOR ATTACH BORE FOUND CORRODED.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 40,211 hrs · 9,258 cycles

LT WING- O/B FLAP VANE SUPPORT FITTING NR 5 FROM I/B ATTACH HOLE FOUND CORRODED. CORROSION ON LT WING, O/B FLAP VANE SUPPORT FITTING NR 5 FROM I/B ATTACH HOLE REMOVED AND REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-73298.

Part: SUPPORT FITTING — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING- O/B FLAP VANE SUPPORT FITTING NR 2 FROM I/B ATTACH HOLE FOUND CORRODED. CORROSION ON LT WING, O/B FLAP VANE SUPPORT FITTING #2 FROM I/B ATTACH HOLE REMOVED AND REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-73298.

Part: TEE FITTING — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING O/B FLAP VANE NR 3 FROM I/B TEE FITTING FWD BORE FOUND CORRODED. RHW O/B FLAP VANE NR 3 FROM I/B TEE FITTING FWD CORRODED BORE REPAIRED AS PER EA 1-5750-73297.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING I/B FLAP O/B HINGE (FLAP SIDE) LOWER O/B BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE) LOWER O/B BORE (PIVOT HOLE) CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-72651 TITLE : WINGS - TRAILING EDGE DEVICES - RT I/B FLAP O/B AFT HINGE PIVOT BORE CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING I/B FLAP O/B HINGE (AIRCRAFT SIDE) I/B FACE OF I/B PIVOT BEARING BORE FOUND CORRODED. LT WING I/B FLAP O/B HINGE (A/C SIDE) I/B FACE OF I/B PIVOT BEARING BORE (LUG SURFACE) CORROSION REMOVED AND REPLACED AS PER EA 1-5750-72644.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,211 hrs · 9,258 cycles

LT WING - UPPER SURFACE, STA 118 TO 162, FWD AREA BETWEEN FRONT AND REAR AREA, NUMEROUS PLACES FOUND CORRODED. LT WING UPPER SURFACE, NUMEROUS CORRODED PLACES AT FORWARD AREA BETWEEN FRONT AND REAR AREA STA 118 TO 162 BLENDED OUT AS PER SRM 51-21-01 VOL 2 WITH MATERIAL REMOVED : 0.035" FROM ORIGINAL THICKNESS = 0.170" AND FOUND WITHIN LIMIT AS PER EA 1-5750-73296 WITH TITLE : WINGS - WING STRUCTURE - LT UPPER WING SKIN CORROSION REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING- O/B FLAP I/B HINGE (FLAP SIDE) UPPER ATTACHMENT BORE FOUND CORRODED. LT WING- O/B FLAP I/B HINGE (FLAP SIDE) UPPER ATTACHMENT BORE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71894. WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: SUPPORT BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING OUTBOARD FLAP INBD HINGE (FLAP SIDE) LOWER OUTBOARD ATTACHMENT BORE FOUND CORRODED.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING O/B FLAP O/B HINGE (FLAP SIDE) LOWER ATTACHMENT BORE FOUND CORRODED.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

O/B FLAP I/B HINGE (FLAP SIDE) LOWER ATTACHMENT BORE FOUND CORRODED. O/B FLAP I/B HINGE (FLAP SIDE) LOWER ATTACHMENT I/B & O/B BORES. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71894. WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: SUPPORT BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) LOWER INBOARD ATTACHMENT BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING- I/B FLAP O/B HINGE LOWER BORE FOUND CORRODED. (FLAP SIDE).

Part: HINGE — CRACKED (LT WING OB FLAP) · airframe 40,211 hrs · 9,258 cycles

LT WING OUTBOARD FLAP HINGE (A/C) SIDE FWD SEAL ATTACHMENT STRIP FOUND CRACKED.

Part: RIB — CRACKED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING L/E CAVITY, NR 16 RIB CRACKED. LT WING- L/E CAVITY, NR 16 RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 40,211 hrs · 9,258 cycles

LT WING O/B FLAP I/B HINGE (A/C SIDE) PIVOT BEARING ATTACHMENT BORE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (A/C SIDE) PIVOT BEARING ATTACHMENT BORE CORROSION REMOVED AND REPLACED AS PER EA 1-5750-72654 .

Part: BRACKET — CORRODED (ZONE 600) · airframe 40,211 hrs · 9,258 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (A/C SIDE) SIDE ATTACHMENT BORE FOUND CORRODED.

Part: MFC — MALFUNCTIONED (NR 1) · airframe 37,653 hrs · 8,655 cycles

AFTER TAKEOFF, RECEIVED A LEVEL 2 AIR MANF 1 FAIL ALERT. DUMPED 62000 LBS FUEL AND MFC FAULT REVIEW LAST LEG SHOWS IN FLIGHT FAULTED MFC PNEU 1 OUT AND ON GROUND FAULTED ALARM (PNEU 1 Z4 OVHT). INSPECT Z4 FOR AIR LEAK NOT FOUND. TROUBLESHOT FIM 36-23-06 R AND I MFC PER MM AND RTS ALL TEST PASSED. A/C OK FOR SERVICE.

Part: FITTING — CORRODED (LT MLG)

LT MLG RETRACT ACTUATOR FITTING FOUND PITTING CORROSION ON UPPER FWD BOLT HOLE. REMOVED AND REPLACED ACTUATOR FITTING PER SRM 51-31-01 VOL 11.

Part: FITTING — CORRODED (RT MLG)

RT MLG RETRACT ACTUATOR FITTING FOUND CORRODED ON LOWER BOLT HOLES. REMOVED AND REPLACED ACTUATOR FITTING PER SRM 51-31-01 VOL 11.

Part: FITTING — CORRODED (LT MLG) · airframe 35,870 hrs · 8,228 cycles

LT MLG RETRACT ACTUATOR FITTING FOUND BOTH LOWER MOUNTING BOLT HOLES CORRODED (PITTING CORROSION). REMOVED AND REPLACED ACTUATOR FITTING PER SRM 51-31-01 VOL 11.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 35,870 hrs · 8,228 cycles

INTERGRANULAR CORROSION ON FWD CARGO COMPT AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X=+ 29 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 35,870 hrs · 8,228 cycles

EXFOLIATION CORROSION ON FWD CARGO COMPT AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X=+ 8 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 35,870 hrs · 8,228 cycles

EXFOLIATION CORROSION ON FWD CARGO COMPT VERTICAL BEAM SUPPORT (U-CHANNEL) AT X=-8 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 35,870 hrs · 8,228 cycles

EXFOLIATION CORROSION ON FWD CARGO COMP AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X =+ 56 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094.

Part: AILERON — MALFUNCTIONED (RT WING)

AILERON DEFLECT DISAGREE LIGHT ILLUM'D LEVEL 2 ALERT ON FLAP RETRACTION. COMPLETED QRH PROCEDURES, LIGHT REMAINED ILLUM'D. CONFIG PAGE SHOWED RIGHT OUTBOARD AILERON EXTENDED. HARD RIGHT AILERON CONTROL REQ'D THIS INPUT ALL THE WAY TO TOUCHDOWN.

Part: SUPPORT FITTING — CRACKED (SLAT) · airframe 32,118 hrs · 7,392 cycles

RT WING L/E STA XFS 1004, NR 16 SLAT TRACK SUPPORT FITTING CRACKED. *S/D* REMOVED AND REPLACED PER DWG ARB2850.

Part: STOP FITTING — CRACKED (R3 DOOR) · airframe 32,118 hrs · 7,392 cycles

CABIN R3 DOOR PLUG AFT LWR STOP FITTING FOUND CRACKED. *S/D* REMOVED AND REPLACED PER SRM 51-31-01, VOL II, IAW DWG NO ADA 3462. HOLES TRANSFERRED TO NEW STOP FITTING AS PER SRM 51-35-01, VOL II.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS)

DURING CLIMBOUT RECEIVED ALERT FLAP DISAGREE. REMOVED AND REPLACED LEFT INBD FLAP POSITION TRANSMITTER PER MM 27-54-04. BOTH FCC FLAP SYS RTS PASSED, WORKS NORMAL.

Part: CONTROL CABLE — TWISTED (AILERON)

AILERON LOCKOUT SLAT INPUT CABLE 85B. REMOVED AND REPLACED AS PER MM 20-20-06. ADJ AND OPER CK CARRIED OUT PER MM 27-10-00, FOUND SATISFACTORY.

Part: SEAT TRACK — CRACKED (CABIN)

MAIN DECK SEAT TRACK CRACKED AT 635 X= 47.5 LEFT 557. MAIN DECK SEAT TRACK CRACK AT 755 X= 8.5 RIGHT 640. REMOVED AND REPLACED PER SRM 51-31-01 VOL II, SRM 53-70-00 FIG I VOL I.

Part: SEAT TRACK — CRACKED (BS 635)

MAIN DECK SEAT TRACK CRACKED AT BS 635 X PLUS 27.5 RT. REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL 1.

Part: SILL — DAMAGED (CARGO DOOR)

UPPER CARGO DOOR JAMB FORWARD LWR SILL SKIN DAMAGED. REPAIR, FABRICATED PER SRM 53-50-00 FIG 4 VOL 1.

Part: CARGO TRACK — CORRODED (BS 1361 - 1481)

UPPER CARGO COMP FLOOR TRACK HOLE FROM BS 1361 TO BS 1481 AT RBL 106 CORRODED. REMOVED AND REPLACED PER SRM 53-70-00 FIG 3 VOL 1.

Part: BLEED VALVE — MALFUNCTIONED (APU)

00-24 - AC AIR TURN BACK DUE TO NR 1 BLD LOW ALERT. NR 2 BLD WAS ALREADY DEFERRED. NO LEAKS NOTED, FOR T/S MANUALLY CLOSED AND LOCKED APU LOAD BLD VALVE. REMOVED AND INSTALLED APU LOAD BLEED VALVE REF WRI 49-50/5443. PRESSURE DECAY TEST ALL PASSED. A/C OK FOR SERVICE.

Part: MFDU — FAILED (COCKPIT)

99-260 - AT FLT LEVEL 330, ON CLIMB-OUT RECEIVED AIR MANIFOLD 2 FAIL GOT ALERT AIR SYS 1/2 FAIL, NOTE THE NR 2 ENGINE BLD VALVE DID NOT CLOSE. REMOVED AND REPLACED THE MANIFOLD FAILURE CONTROLLER PER MM 36-23-00-5. SYSTEM TEST NORMAL.

Part: STRUT — DEFORMED (CTR MLG)

CENTERLINE LAND GEAR CARRIER AYG 7216-503 CRACK AND RING AYG7217-1 DEFORMED. 1.5 INCH CRACK AT SHOCK STRUT PISTON TOP CHROME AREA. REMOVED AND REPLACED CTR LAND GEAR RING IAW MM 32-15-01-8. REMOVED AND REPLACED LAND GEAR PISTON WITH CLG CARRIER SERVICEABLE FROM AC N583FE. REFER SNRM 0589 AND 0590.

Part: TAIL CONE — CRACKED (AFT FUSELAGE)

SNRM 413 TAIL CONE STRUCTURE OF RT HINGE FAIL DURING OPER: AREA DAMAGED DURING EXTEND OPER. REMOVED AND REPLACED TAIL CONE RT HINGE STRUCTURE DAMAGE LWR SKIN, INTERCOSTAL, RIBS, FRAME, PNL AND DOUBLERS PER DWG AKC 7504 AND OPER CK MM 53-52-01-2 FND SAT.

Part: SENSOR — DIRTY (NLG)

SIN - PASSING FL260 IN CLIMB, AIRCRAFT EXPERIENCED BUFFET AND VIBRATION. CHECKED CONFIGURATION PAGE AND IT SHOWED THE NOSE GEAR UNSAFE. RETURNED TO SINGAPORE AT 260KTS .REVIEWED CFDS LRU FAULT - NO FAULT. PER CREW INFO ALERT SHOWN ON PILOT DISPLAY VISUAL INSPECTION ON NOSE GEAR, NO ABNORMALITIES OR DAMAGES. PERFORMED BITE TEST ON PSEU PER FIM 31-71-00 AND OK. CLEAN ALT SENSORS. AIRCRAFT OK FOR SERVICE.

Part: TRIM CYLINDER — MALFUNCTIONED (LANDING GEAR)

AFTER TAKEOFF, GEAR HANDLE WOULD NOT RAISE TO RETRACT THE GEAR. REMOVED AND REPLACED THE BOGIE TRIM CYCLINDER, OPS CHECK GOOD.

Part: FAN AIR VALVE — MALFUNCTIONED (NR 2 ENGINE)

NR 2 ENG BLEED AIR HIGH TEMP, POWER REDUCED, ALERT WENT OUT. REMOVED AND REPLACED NR 2 ENG FAN AIR VALVE SYS OPS CHECK GOOD WITH ENG RUN.

Part: SPAR CHORD — CORROSION (WS 670-830)

NR 5050 AND 505. LEFT WING REAR SPAR UPPER CHORD ANGLE AFT TANG BETWEEN STA XORS 670 TO 830 HAS NUMEROUS AREAS OF EXFOLIATION CORROSION. REMOVED CORROSION PER SRM 51-21-01.

Part: SPAR CHORD — CORRODED (WS 782-827)

NR 6047. RIGHT WING TOP TE PANEL OUTBOARD OF NR 5 SPOILER BULGING AT AFT SPAR STA XORS 782 - 827. SUBJECT CORROSION HAS BEEN REMOVED, AREA TREATED AND PAINTED PER 51-21-01.