N311FE

Part: NONE — NONE · airframe 106,170 hrs · 32,102 cycles

HYD 3 ELEV OFF LEVEL ONE ALERT APPROXIMATELY:30 MINUTES INTO FLIGHT, APPROXIMATELY 15 MINUTES LATER HYD 3 OFF LEVEL ONE ALERT, ON FINAL AFTER SELECTING LANDING GEAR DOWN HYD 3 FAIL LEVEL 2 ALERT. REMOVED AND REPLACED PRESSURE PORT UNION O-RING ON 1/3 RMP. REF AMM 29-22-01-2. LEAK CHECKED OK/ NO DEFECTS NOTED.

Part: CAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

LOWER BLADDER CELL AFT BULKHEAD LOWER CAP CUTOUT AREA FOUND CORROSION AT STATION 1368.650 X=-4.95 TO X=-13.95. LOWER BLADDER CELL AFT BULKHEAD LOWER CAP CUTOUT AREA CORROSION REMOVED AS PER SRM 51-21-01 VOLUME 2 AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIGURE 1B VOLUME 1 AT STATION 1368.650 BETWEEN X=-4.95 TO X=-13.95. REPAIR CARRIED OUT AS PER E.A : # 8-5310-T0362946 PART 1, TITLE: FUSELAGE - MAINFRAME - EXFOLIATION CORROSION FOUND ON THE AFT PRESSURE BULKHEAD LOWER CAP P/N: AYB7080-7 HORIZONTAL FLANGE UPPER SURFACE AT STA 1368.650. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1256) · airframe 106,048 hrs · 32,047 cycles

CABIN - STATION 1256 L3 DOOR CUTOUT FORWARD UPPER JAMB INNER SKIN FOUND CRACKED. CABIN - AT STATION 1256 L3 D00R CUT OUT FORWARD UPPER JAMB , CRACKED INNER SKIN REPAIRED AS PER E.A.#: 8-5300-T0363092 PART 1 , TITLE: FUSELAGE - GENERAL - REPAIR FOR L3 AND R3 CENTER FUS PAX DOOR JAMB FWD AND AFT INNER SKIN. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1256) · airframe 106,048 hrs · 32,047 cycles

CABIN - STATION 1256 R3 DOOR CUTOUT FORWARD UPPER JAMB INNER SKIN FOUND CRACKED. CABIN - AT STATION 1256 R3 DOOR CUT OUT FORWARD UPPER JAMB , CRACKED INNER SKIN REPAIRED AS PER E.A.#: 8-5300-T0363092 PART 1 , TITLE: FUSELAGE - GENERAL - REPAIR FOR L3 AND R3 CENTER FUS PAX DOOR JAMB FWD AND AFT INNER SKIN. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CENTER LOWER CARGO COMPARTMENT - WHILE REMOVAL OF ADDITIONAL ACCESS (REFERENCE NRSM 01768) FOUND DOOR JAMB STATION 1708 AREA FOUND CORROSION LONGERON 42 RIGHT TO LONGERON 43 RIGHT CENTER LOWER CARGO COMPARTMENT DOOR CUTOUT FORWARD INNER LOWER FRAME ANGLE STATION 1708 BETWEEN LONGERON 42 RIGHT TO LONGERON 43 RIGHT CORROSION REMOVED AS PER SRM 51-21-01 VOLUME 2 AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIGURE 1A VOLUME 1. REPAIR CARRIED OUT AS PER EA: 8-5310-T0363271 PART 1 TITLE: FUSELAGE - MAINFRAME - CENTER CARGO DOOR FWD JAMB - STA 1708 FRAME LOWER ANGLE REPAIR AND DOOR CUTOUT FWD LOWER CORNER REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1305) · airframe 106,048 hrs · 32,047 cycles

CABIN - STATION 1305 L3 DOOR CUTOUT AFT UPPER JAMB INNER SKIN FOUND CRACKED. CABIN - AT STATION 1305 L3 DOOR CUT OUT AFT UPPER JAMB , CRACKED INNER SKIN REPAIRED AS PER E.A.#: 8-5300-T0363092 PART 1 , TITLE: FUSELAGE - GENERAL - REPAIR FOR L3 AND R3 CENTER FUS PAX DOOR JAMB FORWARD AND AFT INNER SKIN. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CORRODED (BS 1841) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

AFT LOWER CARGO COMPARTMENT - WHILE REPAIR OF FLOOR WEB ( REFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM : N01471), FOUND FLOOR SUPPORT STATION 1841 X=32 FOUND CORROSION. AFT LOWER CARGO COMPARTMENT DAMAGED FLOOR SUPPORT CHORD AT STATION 1841 X=32 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME 2 . REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FILLER — DAMAGED (LT WING LE) · airframe 106,048 hrs · 32,047 cycles

RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT STATION XIS 160.500 FILLER FASTENERS HOLES FOUND DAMAGED AFTER EXISTING REPAIR DOUBLER REMOVED (REF : SNRM N00253) RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT STATION XIS 160.500 FILLER WITH DAMAGED FASTENERS HOLES REMOVED AND REPLACED WITH FABRICATED FILLER AS PER EA : 8-5730-T0363091 PART 1 TITLE : WINGS - PLATES AND SKINS - RH WING FIXED LEADING EDGE SKIN CUTOUT REPAIR BETWEEN XIS 163.407 AND XIS 164.972. FILLER FABRICATED AS PER EA 8- 5730-T0363091 PART 1 AND SERVICE REWORK DRAWING WZZ7589 REV E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — DAMAGED (RT WING) · airframe 106,048 hrs · 32,047 cycles

RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT STATION XIS 160.500 FORMER FASTENER HOLES FOUND ELONGATED AFTER EXISTING REPAIR DOUBLER REMOVED (REF : SNRM N00253) RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT STATION XIS 160.500 FORMER WITH ELONGATED FASTENER HOLES REMOVED AND REPLACED WITH FABRICATED FORMER AS PER SRM 51-35-01 VOLUME 2. FORMER FABRICATED AS PER DOUGLAS DRAWING : ARB7127 REV : AL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LUG HOLE SURFACE FOUND WITH CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LUG HOLE SURFACE REWORKED AS PER MD-10 CMM 57-44-08 AND FOUND UPPER AND LOWER BARREL NUT WALL THICKNESS EXCEED LIMIT BASED THE DIFFERENCE BETWEEN DRAWING AND CMM MAXIMUM REWORK LIMITS FOR BARREL NUT HOLE. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-10 CMM 57-44-08 AND E.A. # 8-5750-T0362705 PART 1 STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BEAM — CRACKED (L3 DOOR AREA) · airframe 106,048 hrs · 32,047 cycles

CABIN - L3 DOOR PLUG #7 BEAM FORWARD STOP FITTING FOUND CRACKED. CABIN - AT L3 PLUG DOOR CRACKED #7 BEAM REMOVED AND REPLACED WITH NEW BEAM AS PER SRM 51-31-01 VOLUME 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BEAM — CRACKED (L3 DOOR AREA) · airframe 106,048 hrs · 32,047 cycles

CABIN - L3 DOOR PLUG #6 BEAM FORWARD STOP FITTING FOUND CRACKED AT STATION 1260. CABIN - AT L3 PLUG DOOR CRACKED #6 STOP BEAM AT STATION 1260 REMOVED AND REPLACED AS PER E.A. #: 8-5210-T0363122 PART 1, TITLE : DOORS - PASSENGER / CREW - L3 DOOR - STOP BEAM #6 FOUND CRACKED AND SEVERED AT FWD EDGE - FABRICATION USING ALTERNATE MATERIAL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

RIGHT HAND WING INBOARD AILERON LOWER SURFACE AT STATION XIA 316 FOUND WITH CORROSION RIGHT HAND WING INBOARD AILERON LOWER SURFACE AT STATION XIA 316 REPAIR CARRIED OUT AS PER EA 8-5730-T0362995 PART 1 TITLE : WINGS - FLIGHT SURFACES - NEW LOWER SKIN SPLICE REPAIR FOR RH INBD AILERON. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CRACKED (BS 495 L32-33L) · airframe 106,048 hrs · 32,047 cycles

LEFT HAND AIRCON PACK #2 COMPARTMENT FUSELAGE FRAME AT STATION 495 LONGERON 32 LEFT TO LONGERON 33 LEFT FOUND CRACKED. LEFT HAND AIRCON PACK #2 COMPARTMENT FUSELAGE FRAME CRACKED AT STATION 495 LONGERON 32 LEFT TO LONGERON 33 LEFT REPAIR CARRIED OUT AS PER E.A #: 8-5310- T0362915 PART 1, TITLE: FUSELAGE - MAINFRAME - REPAIR FOR 1.75-INCH LONG CRACK FOUND COMMON TO ACA0053-3 FRAME Y=495.000 AT AIR CONDITIONING COMPARTMENT DOOR CUTOUT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CHAFED (BS 535 L19R) · airframe 106,048 hrs · 32,047 cycles

CABIN - RIGHT HAND STATION 535 LONGERON 19 RIGHT FRAME FOUND CHAFFED. CABIN AT RIGHT HAND FRAME STATION 535 LONGERON 19 RIGHT CHAFFED MARKS REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-01 FIGURE 1B VOLUME 1. REPAIR CARRIED OUT AT RIGHT HAND FRAME STATION 535 LONGERON 19 RIGHT AS PER SRM 53-30-00 FIGURE 14 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 106,048 hrs · 32,047 cycles

AFT LOWER CARGO FLOOR PANEL #183KF SUPPORT FOUND CORROSION AT STATION 1841, X = 47" AFT LOWER CARGO FLOOR PANEL #183KF CORRODED SUPPORT AT STATION 1841 X=47" REMOVED AND REPLACED WITH REWORKED SUPPORT AS PER SRM 51-31-01 VOLUME 2. SUPPORT REWORKED AS PER DOUGLAS DRAWING :AGA7170 REVISION:T. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. THE SUPPORT CORROSION EVALUATED FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-01 FIGURE 1A VOLUME 1.

Part: WEB — CRACKED (AFT CARGO) · airframe 106,048 hrs · 32,047 cycles

AFT LOWER CARGO COMPARTMENT FLOOR WEB FOUND CRACKED AT STATION 1841 X = 5". WEB REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME 2. WEB FABRICATED AS PER DOUGLAS DRAWING AGA 7170 REVISION: T. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TEE FITTING — CRACKED (BS 1368) · airframe 106,048 hrs · 32,047 cycles

CENTER WHEEL WELL FORWARD BULKHEAD LEFT HAND T-CHORD FITTING FOUND CRACKED AT STATION 1368.650, X= 31.5. CENTER WHEEL WELL FORWARD BULKHEAD LEFT HAND CRACKED T-CHORD FITTING. REMOVED AND REPLACED WITH FABRICATED T-CHORD FITTING IAW SRM 51-31-01 VOLUME 2 AT STATION 1368.650, X= 31.5. T-CHORD FITTING FABRICATED IAW DRAWING: APB7158 REVISION:C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CAP — CORRODED (BS 1368 BULKHEAD) · airframe 106,048 hrs · 32,047 cycles

LOWER BLADDER CELL AFT BULKHEAD LOWER CUTOUT AREA FOUND CORROSION AT STATION 1368.650. LOWER BLADDER CELL AFT BULKHEAD LOWER CAP CUTOUT AREA CORROSION REMOVED IAW SRM 51-21-01 VOLUME 2 AND FOUND EXCEED LIMIT IAW SRM 53-00-01 FIGURE 1B VOLUME 1 AT STATION 1368.650 BETWEEN X= 13.6 TO X= 6.6 AND X= -4.95 TO X= -13.95. REPAIR CARRIED OUT AS PER E.A # 8-5310-T0362946 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 09 AND E.A.#8-5750-T0362750 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 10 CMM 57-44-09 AND E.A.#8-5750-T0362750 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00401 ATTACHED E.A. # 8-5750-T0362750 PART 1 FOR WORK DETAILS.

Part: BARREL NUT — CORRODED (RT TE FLAP HINGE) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER LUG HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 10 CMM 57-44-09 AND E.A.#8-5750-T0362750 PART 1 STEP 2C AND STEP 2, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00401 ATTACHED E.A. # 8-5750-T0362750 PART 1 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT BORE LUG HOLE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-52-02. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-52- 02 AND E.A.#8-5750-T0362751 PART 1 STEP 1A AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BARREL NUT — CORRODED (RT TE FLAP HINGE) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 09 AND E.A.#8-5750-T0362750 PART 1 STEP 2D AND STEP 2, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00401 ATTACHED E.A. # 8-5750-T0362750 PART 1 FOR WORK DETAILS.

Part: BARREL NUT — CORRODED (RT TE FLAP HINGE) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER LUG HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44-09 AND E.A.#8-5750-T0362750 PART 1 STEP 2C AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00401 ATTACHED E.A. # 8-5750-T0362750 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 10 CMM 57-44-09 AND E.A.#8-5750-T0362750 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00401 ATTACHED E.A. # 8-5750-T0362750 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 10 CMM 57-44-08 AND E.A. # 8-5750-T0362749 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00449 ATTACHED E.A. # 8-5750-T0362749 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44-08 AND E.A. # 8-5750-T0362749 PART 1 STEP 2D AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00449 ATTACHED E.A. # 8-5750-T0362749 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD LUG HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 10 CMM 57-44-08 AND E.A. # 8-5750-T0362749 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00449 ATTACHED E.A. # 8-5750-T0362749 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 10 CMM 57-44-08 AND E.A. # 8-5750-T0362749 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00449 ATTACHED E.A. # 8-5750-T0362749 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LOWER LUG HOLE BORE FOUND WITH CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LOWER LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 08 AND E.A. # 8-5750-T0362749 PART 1 STEP 2E AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00449 ATTACHED E.A. # 8-5750-T0362749 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44-08 AND E.A. # 8-5750-T0362749 PART 1 STEP 2D AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00449 ATTACHED E.A. # 8-5750-T0362749 PART 1 FOR WORK DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CABIN - LEFT HAND STATION 1761 - 1781 , X = 27.5 SEAT TRACK FOUND WITH CORROSION. CABIN AT LEFT HAND STATION 1761 TO STATION 1781 , X = 27.5 CORROSION AT SEAT TRACK EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1.CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1731 TO EXISTING SPLICE STATION 1811 , X = 27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 106,048 hrs · 32,047 cycles

LEFT HAND WING - LEADING EDGE COMPARTMENT STATION XOS 667 RIB DOUBLER CRACKED CRACKED RIB DOUBLER REMOVED AS PER SRM 51-31-01 VOLUME 2 AND FABRICATED RIB DOUBLER AS PER DOUGLAS DRAWING ARB3954 REV K. INSTALLED FABRICATED RIB DOUBLER AT LEFT HAND WING COMPARTMENT STATION XOS 667 AS PER SRM 51-31-01 VOL 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 09 AND E.A.#8-5750-T0362741 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000I- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE SURFACE FOUND WITH CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. REPAIR EVALUATED AND FOUND FORWARD MOUNT OUTBOARD LUG THICKNESS ACCEPTED AS PER E.A.#8-5750-T0362741 PART 1 STEP 1 FIGURE 1, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000I- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00249 ATTACHED E.A.#8-5750-T0362741 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND WITH CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 09 AND E.A.#8-5750-T0362741 PART 1 STEP 1C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000I- LH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00249 ATTACHED E.A.#8-5750-T0362741 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT UPPER LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT UPPER LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 08 AND E.A. # 8-5750-T0362749 PART 1 STEP 2E AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00449 ATTACHED E.A. # 8-5750-T0362749 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 106,048 hrs · 32,047 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 08 AND E.A. # 8-5750-T0362749 PART 1 STEP 2C AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 8-5750-7-5000- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1561 L12L) · airframe 106,048 hrs · 32,047 cycles

CABIN - LEFT HAND STATION 1561 LONGERON 12 LEFT FRAME FOUND DENT. CABIN AT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT , DENT AREA REPAIRED AS PER SRM 53-30-00 FIGURE 4 VOLUME 1. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53 - DAMAGE TOLERANCE ASSESSMENT TABLE 1 VOLUME 1 , 53-30-00 PARAGRAPH 5 FIGURE 4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CABIN - RIGHT HAND STATION 1401 - 1421 X = - 75.25 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND STATION 1401 TO STATION1421 , X = - 75.25 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1391 TO EXISTING SPLICE STATION 1451 , X = - 75.25 AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1541 L12L) · airframe 106,048 hrs · 32,047 cycles

CABIN - LEFT HAND STATION 1541 LONGERON 12 LEFT FRAME FOUND DENT. CABIN AT LEFT HAND FRAME STATION 1541 LONGERON 12 LEFT DENT AREA REPAIRED AS PER SRM 53-30-00 FIGURE 4 VOLUME 1. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53 - DAMAGE TOLERANCE ASSESSMENT TABLE 1 VOLUME 1 , 53-30-00 PARAGRAPH 5 , FIGURE 4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1236-1256) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CABIN - LEFT HAND STATION 1236 - 1256 X = 47.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND STATION 1236 TO STATION 1256 , X = 47.5 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1286 TO EXISTING SPLICE STATION 1189 , X = 47.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CABIN - RIGHT HAND STATION 1821 - 1861 X = - 8.5 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND STATION 1821 TO STATION 1861 , X = - 8.5 CORROSION AT SEAT TRACK EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1771 TO END OF PART STATION 1887 , X = - 8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CABIN - LEFT HAND STATION 1819 X = 27.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND STATION 1819 , X = 27.5 CORROSION AT SEAT TRACK EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1811 TO END OF PART STATION 1887 , X = 27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1215) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CABIN - RIGHT HAND STATION 1215 X = - 75.25 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND STATION 1215 , X = - 75.25 CORROSION AT SEAT TRACK EVALUATED ,FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1129 TO STATION 1269 , X = - 75.25 AS PER SRM 53-70-00 FIGURE 1 VOLUME 1.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CABIN - LEFT HAND STATION 1841 X = 8.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND STATION 1841 , X = 8.5 CORROSION AT SEAT TRACK EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1811 TO END OF PART STATION 1887 , X = 8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1305-1339) · corrosion level 2 · airframe 106,048 hrs · 32,047 cycles

CABIN - RIGHT HAND STATION 1305 - 1339 X = - 75.25 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND STATION 1305 TO STA 1339 , X = - 75.25 CORROSION AT SEAT TRACK EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-70-00 FIGURE 5 VOLUME1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1269 TO STATION 1391 , X = - 75.25 AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1601 L12L) · airframe 106,048 hrs · 32,047 cycles

CABIN - LEFT HAND STATION 1601 LONGERON 12 LEFT FRAME FOUND DENT. CABIN AT LEFT HAND FRAME STATION 1601 LONGERON 12 LEFT DENT AREA REPAIRED AS PER SRM 53-30-00 FIGURE 4 VOLUME 1. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53 - DAMAGE TOLERANCE ASSESSMENT TABLE 1 VOLUME 1 , 53-30-00 PARAGRAPH 5 , FIGURE 4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 106,048 hrs · 32,047 cycles

LEFT HAND WING - LEADING EDGE COMPARTMENT STATION XOS 585 BEADED DOUBLER CRACKED LEFT HAND WING LEADING EDGE COMPARTMENT STATION XOS 585 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 71 VOL 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 106,048 hrs · 32,047 cycles

LEFT HAND WING - LEADING EDGE COMPARTMENT STATION XOS 627 BEADED DOUBLER CRACKED LEFT HAND WING LEADING EDGE COMPARTMENT STATION XOS 627 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 71 VOL 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 106,048 hrs · 32,047 cycles

LEFT HAND WING - LEADING EDGE COMPARTMENT STATION XOS 666 BEADED DOUBLER CRACKED LEFT HAND WING LEADING EDGE COMPARTMENT STATION XOS 666 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 71 VOL 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 106,048 hrs · 32,047 cycles

LEFT HAND WING - LEADING EDGE COMPARTMENT STATION XOS 668 BEADED DOUBLER CRACKED LEFT HAND WING LEADING EDGE COMPARTMENT STATION XOS 668 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 71 VOL 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR — FAILED (LT MLG) · airframe 105,911 hrs · 31,981 cycles

AFTER T/O, HEARD A LOUD SOUND AS THE GEAR WAS RAISED. DURING THE AFTER T/O FLOW, FO(P.M.) POINTED OUT THE LEFT MAIN GEAR LT WAS SHOWING RED. THE CONFIG SYNOPTIC ALSO SHOWED RED FOR THE LEFT GEAR. FOLLOWED THE QRH AND BROUGHT THE GEAR DOWN - ALL GREEN. RAISING THE GEAR AGAIN PER QRH LEAD BACK TO ALL RED LTS FOR THE LEFT MAIN. CONSULTED MX OVER SATCOM AND ELECTED TO RETURN KIND ON APPROACH, AS A/C SLOWED TO 200K, GEAR UNSAFE LT EXTINGUISHED. CONTINUED APPROACH TO UNEVENTFUL LANDING. SHGN 01MAY21 13:59 IND U AFTER A/C RETURNED TO GATE, THE LEFT MAIN GEAR DOOR DROPPED, ONCE HYD PRESSURE WAS REMOVED. UPON PERFORMING THE GVI OF THE LEFT GEAR AREA, FOUND DOOR CRACKED AROUND THE ENTIRE PERIMETER OF WHERE THE DOOR FITTING (IPC 52-82-01-01, FIG 1, SHT 1, ITEM 456) ATTACHES TO THE DOOR. NEW LEFT MAIN LANDING GEAR DOOR IS NEEDED. L/H MLG DOOR, CPN 5213662, SHOWS IN STOCK AT IND BASE. FACT 02MAY21 16:18 IND CONTINUED INSTALLATION OF LEFT MAIN GEAR DOOR FROM 3. D. (4) THROUGH COMPLETION REF AMM 32-14-01-2. LEFT MAIN GEAR DOOR AND INDICATION CHECKS NORMAL, NO FAULTS NOTED.

Part: A/C PACK — ODOR (NR 1) · airframe 105,272 hrs · 31,656 cycles

HEAVY OIL SMELL COMING FROM NR 1 PACK. 1 PACK INOPERABLE.TROUBLE SHOT TO THE PACK NR1 TURBINE INLET TEMP SENSOR WAS CAUSING THE OVER HEAT CONDITION. REMOVED AND REPLACED NR 1 PACK TURBINE INLET TEMP SENSOR, REF MD-10-30 AMM 21-53-32-4. LEAK AND OPERATIONS CHECKED GOOD. PERFORM THE DISTRUBUTION DUCT ODOR CLEANING/BURNOUT PROCEDURE FOR THE NR 1 PACK, REF AMM 21-53-00-7. NO DEFECTS NOTED AND NO OIL SMELL NOTED.

Part: B-NUT — LOOSE (HYD LINE) · airframe 105,097 hrs · 31,560 cycles

AFTER LANDING RECIEVED LEVEL 1 "HYD 3 ELEV OFF" AT BLOCK IN RECEIVED LEVEL 1 "HYD 3 QTY LO" BRAKE CONTROL VALVE LEAKING IN RT WHEEL WELL. TIGHTENED BRAKE VALVE SUPPLY LINE B NUT. SERVICED NR 3 HYDRAULICS. LEAK AND OPS CHECK GOOD.

Part: SKIN PANEL — CRACKED (DROOP LE) · airframe 103,345 hrs · 30,667 cycles

RT DROOPED LEADING EDGE FLEX SKIN PANEL HAS A CRACK ON THE F/W ATTACH POINT. MARKED IN RED. REPAIRED PER SRM 57-10-00 FIG 58 SHEET 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 103,345 hrs · 30,667 cycles

MAIN CABIN, APPROX. STA. 1481 BETWEEN LBL 70 TO 107 FOUND DAMAGED FLOOR SUPPORT. 13-JUL-2019 16:30 INSTALLED NEW FLOOR SUPPORT AT STA 1481 LBL70 TO 107 IAW AFA3853.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 103,345 hrs · 30,667 cycles

MAIN CABIN, SEAT-TRACK IS CORRODED FROM STA. 1481 TO 1521 AT LBL 70. REMOVED AND REPLACED SECTION OF SEAT-TRACK PER SRM 53-70-00 FIG 1.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 103,345 hrs · 30,667 cycles

LOWER FWD CARGO HAS A BROKEN FLOOR SUPPORT ASSY (P/N# ADA0235-3) AT STA. 791.00 LBL 16.00 (MRK) INSTALLED SUPPORT AT STA.791.00 LBL 16.00 LOWER FWD CARGO REF. SRM 51-35-01 VOLII. "MAJOR REPAIR' SEE JPF---->

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 103,345 hrs · 30,667 cycles

SEAT TRACK CORROSION ON MAIN DECK, STA. 1661-1761, RBL 107.25 REMOVED AND REPLACED DAMAGED SEAT TRACK PER SRM 53-70-00 FIG. 1, VOL. 1.

Part: RIB — CRACKED (LT WING) · airframe 103,345 hrs · 30,667 cycles

LT WING #2 SLAT CLOSE OUT RIB XDLES 328.106 ARB 1647-3 AND -5 RIB IS CRACKED. REMOVED AND REPLACED ARB1647-3 AND -5 PN LT WING #2 SLAT REF ARB1647 DWG AND NRB6025. (MAJOR REPAIR) JPF--->

Part: SKIN — CRACKED (LT WING) · airframe 103,345 hrs · 30,667 cycles

LEFT LOWER WING SKIN AT THE FWD INBOARD CORNER OF THE SLAT ACTUATOR DOOR CUT OUT HAD A .300 INCH CRACK. REPAIRED THE SKIN IAW SRM.57-10-00, PG 502, FIG.105.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 103,345 hrs · 30,667 cycles

COCKPIT RT OBSERVER`S SEAT FLOOR PANEL DOUBLER WAS CRACKED. REMOVED CRACKED FLOOR PANEL DOUBLER, AND REPAIRED WITH INSTALLATION OF A REPAIR WEB AND DOUBLER IAW SRM 53-60-01, VOL I, FIG 4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 103,345 hrs · 30,667 cycles

AFT CARGO STA.1931 RBL 38 RT SLANT PANEL LOWER FLOOR SUPPORT EXFOLIATED. - 25-JUN-2019 02:37 REPLACED FLOOR SUPPORT PER DWG AGA 3857 JPF OPEN WORK ITEM: MATERIAL CHECK REQUIRED FOR NEW AGA3857-506 CORRECTIVE ACTION: MATERIAL 7075-0 .050 MP0314675. OPEN WORK ITEM: FABRICATED FOOR SUPPORT PER DWG AGA 3857 CORRECTIVE ACTION: FABRICATED FLOOR SUPPORT PER DWG AG A3857I CORRECTIVE ACTION: FABRICATED HEAT TREATED IAW DPS 7.00-1. OPEN WORK ITEM: DRILL UP ON PROCESS PART CORRECTIVE ACTION: PROCESSED PART PER DWG AGA3857OPEN WORK ITEM: TREAT PRIME AND PAINT CORRECTIVE ACTION: TREATED PRIMED AND PAINTED PER SRM 51-21-01 VOL II. OPEN WORK ITEM: INSTALL PART CORRECTIVE ACTION: INSTALLED PART PER SRM 51-35-01 VOL II AND DWG AGA3857.

Part: STRUCTURE — BENT (AFT CARGO DOOR) · airframe 103,345 hrs · 30,667 cycles

AFT CARGO DOOR WAS BENT IN TWO PLACES ON THE LOWER EDGE OF THE DOOR. REPAIRED THE LOWER EDGE AFT CARGO DOOR IAW SRM 52-10-00, VOL I, FIG 17. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 1741) · airframe 103,345 hrs · 30,667 cycles

[MAIN DECK SEAT TRACK SUPPORT UNDERSIDE:(VIEWED FROM LWR. CTR CARGO COMPT) - STA.1741 LBL 27.50-47.50 SUPPORT UNDERSIDE CORRODED/EXFOLIATED. (MRKD), 2019-06-13] REMOVED AND REPLACED REPLACEMENT SUPPORT IAW AFA3853

Part: FLOORBEAM — CORRODED (BS 1561) · airframe 103,345 hrs · 30,667 cycles

MAIN DECK SEAT TRACK SUPPORT UNDERSIDE:(VIEWED FROM LWR. CTR CARGO COMPT) - STA.1561 RBL 47.50-75.25 SUPPORT UNDERSIDE CORRODED/EXFOLIATED. (MRKD) 0003748737 : KOTSOGLOU, CHRISTOPHER - 16-JUN-2019 14:40 REMOVED AND REPLACED SUPPORT PER DWG AFA3853

Part: SEAT TRACK — CORRODED (BS 1721-1821) · airframe 103,345 hrs · 30,667 cycles

MAIN DECK SEAT TRACK UNDERSIDE:(VIEWED FROM LWR. CTR CARGO COMPT) - STA.1721- 1821 RBL 75.25 SEAT TRACK UNDERSIDE CORRODED/EXFOLIATED IN NUMEROUS AREAS. (MRKD) REMOVED AND REPLACED SECTION OF SEAT TRACK IN REF TO SRM 53-70-00 FIG1 AND DWG # SR10-53-002

Part: SEAT TRACK — WORN (BS 879) · airframe 103,345 hrs · 30,667 cycles

MAIN CABIN, STA. 879 APPROX. LBL 48 SEAT-TRACK HAS LOBE ENLONGATED WORN. REMOVED AND REPAIRED SECTION OF SEAT-TRACK PER SRM 53-70-00 FIG 1

Part: SEAT TRACK — WORN (BS 879) · airframe 103,345 hrs · 30,667 cycles

MAIN CABIN, STA. 879 APPROX. LBL7 SEAT TRACK LOBE ENLONGATED WORN. REMOVED AND REPLACED SECTION OF SEAT-TRACK PER SRM 53-70-00 FIG 1

Part: SEAT TRACK — CORRODED (BS 1701-1741) · airframe 103,345 hrs · 30,667 cycles

[MAIN DECK SEAT TRACK UNDERSIDE:(VIEWED FROM LWR. CTR CARGO COMPT) - STA.1701- 1741 RBL 107.25 SEAT TRACK UNDERSIDE CORRODED/EXFOLIATED. (MRKD), 2019-06-13] REMOVED AND REPLACED SECTION OF SEAT TRACK AT STA 1701-1741 @ RBL 107.25 IN REF TO SRM 53-70-00 FIG 1

Part: SEAT TRACK — WORN (BS 1521) · airframe 103,345 hrs · 30,667 cycles

MAIN CABIN, STA. 1521 APPROX. LBL 48 SEAT-TRACK HAS LOBE ENLONGATED WORN. REMOVED AND REPAIRED SECTION OF SEAT-TRACK PER SRM 53-70-00 FIG. 1 VOL 1

Part: SEAT TRACK — CORRODED (BS 1661) · airframe 103,345 hrs · 30,667 cycles

[MAIN DECK SEAT TRACK SUPPORT UNDERSIDE:(VIEWED FROM LWR. CTR CARGO COMPT) - STA.1661 LBL 27.50-47.50 SUPPORT UNDERSIDE CORRODED/EXFOLIATED. (MRKD), 2019-06-13] REMOVED AND REPLACED THE FLOOR SUPPORT AT STA 1661 @ LBL 27.50-47.50 IN REF TO DWG # AFA 3853

Part: SUPPORT ANGLE — BENT (BS 1701) · airframe 103,345 hrs · 30,667 cycles

CENTER CARGO BAY, BS 1701, LONGERONS 46L-48L, THE WEB SUPPORT ANGLE REPAIR WAS DAMAGED. REMOVED AND REPLACED THE WEB SUPORT ANGLE IAW SRM 53-00-01, VOL I, PAGES 23-28. MAJOR REPAIR,

Part: SEAT TRACK — CORRODED (1661-1761) · airframe 103,345 hrs · 30,667 cycles

MAIN DECK SEAT TRACK: STA. 1661-1761 RBL 107.25 - SEAT TRACK CORRODED/EXFOLIATED IN NUMEROUS AREA ON UPPER AND LOWER SURFACE. (AREAS MARKED & CAN BE WORKED IN CONJUNCTION WITH N/R #364) REPAIRED PER SRM 53-70-00 F.18, SHT. 1-3 VOL. I

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 103,345 hrs · 30,667 cycles

L/H LWR WING FUEL ACCESS PANEL CUT OUT AT XORS 686 (5 O'CLOCK POSITION) HAS 1 EA. ATTACH HOLE WITH A CRACK INDICATION. (MARKED) REAMED ATTACH HOLE TO .317 DIA. CLEAR OF ANY INDICATIONS, FABRIACTED AND INSTALLED REPAIR BUSHING TO ORIGINAL HOLE DIA. OF .260 DIA.PER SRM VOL. 1 57-10-00 PG. 218A. FIG. 69A

Part: DOOR — CORRODED (E&E BAY) · airframe 103,345 hrs · 30,667 cycles

AFT AVIONICS COMPARTMENT DOOR(115AZ) HAS EXFOLIATED CORROSION AT LOWER HINGE. (DOOR SIDE, MARKED IN RED) REMOVED AND REPLACED DOOR IN REF. TO AMM 52-41-01-2.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 103,345 hrs · 30,667 cycles

MAIN DECK SEAT TRACK SUPPORT UNDERSIDE:(VIEWED FROM LWR. CTR CARGO COMPT) - STA.1661 LBL 27.50-47.50 SUPPORT UNDERSIDE CORRODED/EXFOLIATED. (MRKD) REMOVED AND REPLACED THE FLOOR SUPPORT AT STA 1661 @ LBL 27.50-47.50 IN REF TO DWG # AFA3853

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 103,345 hrs · 30,667 cycles

FWD CARGO COMPT: APPROX STA 1100, RBL X=-54. LOWER BULKHEAD "L" FLOORBOARD SUPPORT ANGLE IS CORRORED. MARKED. 26-JUN-2019 03:45 REMOVED AND REPLACED AS REQUIRED FLOORBOARD SUPPORT ASSY. AT FWD CARGO COMPT: APPROX STA 1100, RBL X=-54, LOWER BULKHEAD FRAME. REF. DWG:ADA7667 AND SRM 51-31-01, VOL II.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 103,345 hrs · 30,667 cycles

FWD CARGO COMPT: APPROX STA 1100, RBL X =-6. LOWER BULKHEAD FRAME "L" FLOORBOARD SUPPORT ANGLE IS CORRORED ON UNDERSIDE OF ANGLE. MARKED. 0000883983 : JIMENEZ, ISAAC - 26-JUN-2019 03:04 REMOVED AND REPLACED AS REQUIRED FLOORBOARD SUPPORT ASSY. AT FWD CARGO COMPT: APPROX STA 1100, CENTER OF LOWER BULKHEAD FRAME. REF. DWG:ADA7667 AND SRM: 51-31-01, VOL II.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 103,345 hrs · 30,667 cycles

AFT CARGO COMPARTMENT, APPROX 5" LBL, STA 1902, CORROSION UNDERNEATH SIDE OF FLOORBOARD BEAM. MARKED WITH DOT AND RED GREASE PENCIL - 13-JUN-2019 03:57. REMOVED AND REPLACED AGA3850-7 ANGLE PER DWG AGA3850.

Part: RUB STRIP — CRACKED (LE SLAT) · airframe 103,345 hrs · 30,667 cycles

LEFT WING, CRACK ON UPPER O/B RUB STRIP OF LT #2 SLAT. (MARKED) REMOVED AND REPLACED THE UPPER O/B RUB STRIP ON THE LT #2 SLAT REF. SRM 57-10-00 VOLI FIG.32. "MAJOR REPAIR" JPF---->

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 103,345 hrs · 30,667 cycles

LT WHEELWELL AFT BULKHEAD STA1521 BELOW SYS 2 HYD ACCUMULATOR, OUTER CAP ANGLE HAS CORROSION/EXFOILATION (MARKED). REINSTALLED FASTENERS AND NEW INTERCOSTALS REF EA 8-5310-T03417758 "CORROSION @ PRESSURE BULKHEAD STA 1521 T-CAP & DAC DWG AEA7163 "MAJOR REPAIR" SEE JPF.

Part: SKIN — GOUGED (RT WING) · airframe 103,345 hrs · 30,667 cycles

RT WING: DROOP L/E, OUTBD SKIN EDGE HAS DEEP WEAR (MARKED AND DOT 93) REMOVED AND REPLACED DAMAGED REPAIR FILLER IN REFERENCE TO SRM 57-00-01 FIG. 4, SHEET 2

Part: COALESCER BAG — ODOR (AC BAY) · airframe 103,053 hrs · 30,527 cycles

PACKS SMELL OF FUEL FUMES WHEN FIRST TURNED ON. REMOVED AND REPLACED THE PACK 3 WATER SEPERATOR COALESCER BAG IAW AMM 21-54-03-2. AC OK FOR SERVICE.

Part: CABLE — MISROUTED (SLATS) · airframe 101,658 hrs · 29,770 cycles

WHILE PERFORMING A RIGHT WING SLAT LUBE IAW WC 27B2114. NOTICED ALUMINUM MATERIAL ON THE SLAT CABLES. ON FURTHER INVESTIGATION, THE SLAT CABLE RUN NR 80 FOUND MISROUTED AND WORN INTO THE RIGHT WING RIB AND TWO SLAT DRUM BRACKETS. THE RIB WAS BLENDED IAW EA 8-2780-70338881 AND BOTH BRACKETS SLAT CABLE RUN NR 80 WERE CHANGED.

Part: STIFFENER — CRACKED (NR 3 NACELLE) · airframe 100,552 hrs · 29,200 cycles

NR 3 PYLON WEB STIFFENER CRACKED. REPLACED THE STIFFENER.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 100,552 hrs · 29,200 cycles

HORIZONTAL STAB LEFT SIDE THIRD L/E EDGE FROM INBD, DAMAGED ON TOP. REPAIRED IAW EA 8-5510-T0333730.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 100,552 hrs · 29,200 cycles

NR 3 PYLON, VERTICAL STIFFENER HAS A 1 X 6 INCH AREA OF MATERIAL SHEARED OFF AT VSS 360.

Part: ANGLE — CRACKED (BS 2163 BULKHEAD) · airframe 100,552 hrs · 29,200 cycles

FUSELAGE BULKHEAD, BS 2163, THIRD STIFFENER DOWN FROM THE TOP. LT AND RT SIDE OF TAILCONE, PERIMETER OUTER FLANGE ANGLE IS CRACKED. REMOVED AND REPLACED FLANGE ANGLE IAW DWG AJC 7001-83.

Part: STIFFENER — CRACKED (RT WING) · airframe 100,552 hrs · 29,200 cycles

RIGHT WING L/E XFS 397 OTBD STIFFENER IS CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-33-01, VOL 2, AND EA. 8-5710-T0333527.

Part: SUPPORT — CORRODED (BS 636-664) · airframe 100,552 hrs · 29,200 cycles

FOUND CORROSION ON THE NR 2 MCD HINGE ON ANGLE ACA7292 BEYOND LIMITS. FABRICATED A NEW HINGE SUPPORT IAW DWG ACA7292. REMOVED AND REPLACED THE SUPPORT IAW DRAWING ACA7303.

Part: FITTING — CRACKED (RT MLG DOOR) · airframe 100,552 hrs · 29,200 cycles

RIGHT MAIN LANDING GEAR DOOR IS CRACKED AT FWD SIDE BY RUB STRIP. REMOVED AND REPLACED PAN FITTING AS REQUIRED SRM 51-35-01.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 100,552 hrs · 29,200 cycles

MAIN CARGO DOOR HINGE CORRODED ON LOWER LEG. REMOVED HINGE SECTIONS AND REPLACED IAW DRAWINGS NCA6080, ACA7303, AND ACA7223.

Part: GUIDE — CORRODED (BS 1841) · airframe 100,552 hrs · 29,200 cycles

CENTER CARGO BAY, BS 1841, METAL RAIL GUIDE IS BULGING AT AFT END CORNER. REMOVED AND REPLACED THE RAIL GUIDE AND SPLICE ANGLE IAW DWG AFJ7013, AND SRM 51-31-01 VOL 2

Part: HINGE — CORRODED (CARGO DOOR) · airframe 100,552 hrs · 29,200 cycles

AFT CARGO DOOR HINGE, DOOR SIDE SEGMENT IS PITTING OUT OF LIMITS. REMOVED AND REPLACED THE HINGE SEGMENT IAW SRM 52-10-00.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 100,552 hrs · 29,200 cycles

VERTICAL STAB RT, HAD CORROSION BELOW UPPER RUDDER ACTUATOR. REMOVED CORROSION AND BLEND OUT IAW EA 8-5530-T0333328 P1, SRM 51-21-01, VOL II, SRM 51-21-02, VOL II, PGS 2-9, SOPM 20:10.10, PG 25, AND DPS 2.50.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 100,552 hrs · 29,200 cycles

VERTICAL STAB HAD SURFACE CORROSION JUST BELOW ACCESS PANEL NR 373GL. BLENDED OUT AND REMOVED CORROSION IAW EA 8-5530-T0333328 P1, SRM 51-21-01, VOL II, SRM 51-21-02, VOL II, PGS 2-9, SOPM 20:10.10, PG 25, AND DPS 2.50

Part: CARGO TRACK — GOUGED (BS 1265) · airframe 100,552 hrs · 29,200 cycles

MAIN CARGO BAY, BS 1265 LBL 8.50, CARGO TRACK GOUGED. REPLACED THE CARGO TRACK IAW SRM 53-70-00, VOL.1, & 53-31-01, VOL 2.

Part: CARGO TRACK — GOUGED (BS 1059) · airframe 100,552 hrs · 29,200 cycles

MAIN CARGO BAY, BS 1059 RBL 47.5, CARGO TRACK GOUGED. REPAIRED THE CARGO TRACK IAW SRM 53-70-00, PG 3, FIG 3, VOL 1.

Part: DOUBLER — CRACKED (LT WING) · airframe 100,552 hrs · 29,200 cycles

LEFT WING LE, DOUBLER HAS A 2 INCH CRACK AFT AND INBD OF SLAT TRACK NR 8. REMOVED AND REPLACED THE DOUBLER IAW DWG ARB2933.

Part: CARGO TRACK — GOUGED (BS 1250) · airframe 100,552 hrs · 29,200 cycles

MAIN CARGO BAY, BS 1250 LBL 8.50, CARGO TRACK GOUGED. REPLACED THE CARGO TRACK IAW SRM 53-70-00, VOL 1, & 53-31-01, VOL 2.

Part: CARGO TRACK — GOUGED (BS 1065-1079) · airframe 100,552 hrs · 29,200 cycles

MAIN CARGO BAY, BS 1065 - 1079, RBL 47.5, CARGO TRACK GOUGED AT MULTIPLE LOCATIONS, BEYOND LIMITS. REPLACED THE CARGO TRACK IAW SRM 53-70-00, VOL 1, FIG 1, PG 3.

Part: CARGO TRACK — GOUGED (BS 1491) · airframe 100,552 hrs · 29,200 cycles

MAIN CARGO BAY, BS 1491, RBL 27.50, CARGO TRACK GOUGED. REPLACED THE CARGO TRACK IAW SRM 53-70-00, FIG 1, VOL 1, 51-41-01, VOL 2, & SRM 10-53-002.

Part: CARGO TRACK — GOUGED (BS 1256) · airframe 100,552 hrs · 29,200 cycles

MAIN CARGO BAY, BS 1256 LBL 8.50, CARGO TRACK GOUGED. REPLACED THE CARGO TRACK I SRM 53-70-00 VOL.1 & 53-31- 01 VOL 2.

Part: SEAT TRACK — CORRODED (BS 1670) · airframe 100,552 hrs · 29,200 cycles

MAIN DECK SEAT TRACK DAMAGED AND EXFOILATED AT BS 1670, RBL 78. REPLACED THE SEAT TRACK FROM BS 1631-1671. SPLICE INSTALLED IAW SRM 53-70-00, FIG 1, VOL 1, 51-41-01, VOL 2, 51-31-01, VOL 2, AND SR10-53-002.

Part: UNKNOWN — ODOR · airframe 99,914 hrs · 28,923 cycles

WHEN BRINGING THE PACKS ONLINE AFTER INITIAL PREFLIGHT THE AIR OUTPUT SMELLS VERY STRONG OF OIL OR OTHER ENVIRONMENTAL CHEMICALS. RUNNING ALL 3 PACKS REQUESTING HOT TEMPS IN ALL 3 ZONES APPEARED TO HELP THE ODOR TO DISSIPATE. RAN APU AS PER JRH. RAN ALL 3 PACKS AS PER MM 21-53-00-7 -AIR CONDITIONING PACK AND DISTRIBUTION DUCT ODOR CLEANING. ALL CHECKS PASSED WITH NO ODOR. NO HISTORY FOUND FOR 90 DAYS. A/C OK FOR SERVICE.

Part: SENSOR — FAILED (BRAKES TEMP) · airframe 99,732 hrs · 28,830 cycles

AFTER TAKE OFF AT FL 340, RECEIVED A BRAKE DIFF TEMP. QUICKLY TURNED TO LEVEL 2 BRAKE OVERHEAT. COMPLIED WITH QRH AND TEMP DROPPED FROM HIGH OF 708 TO 80. TEMP IMMEDIATELY LOWERED UPON LOWERING LANDING GEAR. R & R NR 2 BRAKE TEMPERATURE SENSOR IAW AMM 32-46-01-2. TEMP INDICATED NORMAL AND EVENLY WITH THE OTHER BRAKES OK TO CONTINUE SERVICE.

Part: RIB — CRACKED (NR 2 NACELLE) · airframe 972 hrs · 27,783 cycles

NR 2 ENGINE, LEFT CORE COWL FWD NR 4 RIB IS CRACKED. REPLACED THE NR 2 ENG LT CORE COWL WITH A SERVICEABLE UNIT IAW AMM 71-13-01-2.

Part: SPAR CAP — CRACKED (LT HORIZ STAB) · airframe 972 hrs · 27,783 cycles

LEFT HORIZONTAL STAB UPPER OUTER REAR SPAR CAP AFT BARREL NUT HOLE HAS .600" CRACK. REPAIRED IAW EA 5510-T0317220 P1.

Part: SPAR — CRACKED (RT HORIZ STAB) · airframe 972 hrs · 27,783 cycles

RIGHT HORIZONTAL STAB, UPPER SURFACE OF OUTER REAR SPAR IS CRACKED FROM BARREL NUT HOLE. REPAIRED IAW EA 8-5510-T0317221.

Part: INTERCOSTAL — CORRODED (RT MLG WW) · airframe 972 hrs · 27,783 cycles

RIGHT MAIN GEAR WELL AT STATION 1521, THE UPPER INTERCOSTAL HAS HEAVY CORROSION AT TWO AREAS. R & R INTERCOSTAL IAW SRM 51-33-01 & AEA0026-18.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 972 hrs · 27,783 cycles

CENTER CARGO COMPARTMENT STATION 1741, CTR LINE FLOOR FRAME HAS 10" CRACK BELOW CARGO LOCK. REPAIRED IAW SRM 53-20.

Part: SKIN — CORRODED (LT WING) · airframe 972 hrs · 27,783 cycles

LEFT WING UPPER SURFACE, BETWEEN STATION XORS 264 & OXRS 299, AFT SPAR SKIN NEAR MLG UPPER DOUBLE AREAS HAS CORROSION IN 1 PLACE. REMOVED SURFACE CORROSION IAW SRM 51-21-01 VOL II & ACCOMPLISHED REPAIR OF LT WING UPPER SURFACE CORROSION IAW EA 8-5730-T0317219.

Part: SKIN — GOUGED (FUSELAGE) · airframe 972 hrs · 27,783 cycles

AFT CARGO COMPARTMENT 1975 INTERNAL BETWEEN LONGERON 49L - 50L SKIN GOUGED IN NUMEROUS PLACES. INSTALLED DOUBLER IAW EA 8-5330-T0317549 P1.

Part: SKIN PANEL — DELAMINATED (LT WING) · airframe 972 hrs · 27,783 cycles

LEFT WING, LOWER SURFACE, PANEL 541HB IS DELAMINATED. REPAIRED PANEL 541HB IAW SRM 51-71-00 VOL II, SEE JPF ON BACK.

Part: SKIN PANEL — PUNCTURED (RT HORIZ STAB) · airframe 972 hrs · 27,783 cycles

RIGHT STABILIZER-HINGED PANEL 344DB, OTBD OF INBD ELEVATOR ACTUATOR HAS PUNCTURE IN OUTER SURFACE. REPAIRED PANEL 344DB AS REQUIRED IAW SRM 51-71-00 VOL II. .

Part: PANEL — DELAMINATED (NR 2 NACELLE) · airframe 972 hrs · 27,783 cycles

NUMBER 2 ENG INLET, RT SIDE, PANEL 364JR IS DELAMINATED. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL II.

Part: LONGERON — CRACKED (NR 1 COWLING) · airframe 972 hrs · 27,783 cycles

NUMBER 1 ENG CORE COWL LONGERON CRACKED AFT OF CTR HINGE BRACKET. #1 ENGINE CORE COWL REPLACED.

Part: FAIRING — DELAMINATED (LT TE FLAP) · airframe 972 hrs · 27,783 cycles

LEFT OTBD FLAP, INBD HINGE FAIRING PANEL 535AR DISBONDED AT FWD EDGE. REPAIRED LT OTBD FLAP, INBD HINGE FAIRING PANEL 535AR AT FWD EDGE IAW SRM 51-71-00 VOL 2.

Part: WIRE — DAMAGED (FUSELAGE) · airframe 972 hrs · 27,783 cycles

FOUND DAMAGED WIRE G201-217-22 AT STATION Y=1305.200. REPLACED WIRE G201-217-22 FROM D10-544A, 16, TO STATION 1437 LT SIDE WHERE WIRE WAS SPLICED IAW SWP 20-10-01.

Part: SKIN — DAMAGED (TE FLAP VANE) · airframe 972 hrs · 27,783 cycles

LEFT INBD FLAP VANE LE EDGE SKIN MISSING, HONEYCOMB MATERIAL EXPOSED. INSTALLED NEW LT INBD FLAP VANE IAW 27-50-03-2.

Part: INDICATOR — FAILED (L1 DOOR) · airframe 968 hrs · 27,597 cycles

PREFLIGHT CHECK L1 DOOR SLIDE LIGHT IS ILLUMINATED. MEL 04 JAN 15 13:25 RELEASED FOR SERVICE PER MEL 52-10-03 CATEGORY C EXPIRATION 14 JAN 15. L1 MAIN ENTRY SLIDE RAFT INOPERATIVE. R & R REMOTE SLIDE PACK PRESS INDICATOR IAW MM 25-61-03-2 & MM 25-61-03-5. OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 95,444 hrs · 27,030 cycles

ON WALK AROUND FOUND SUSPECTED CRACK ON RIGHT WING INBD CORNER OF FUEL PANEL ON LOWER WING. COMPLIED WITH HFEC INSPECTION OF ABOVE NOTED AREA IAW SPM 06-10-01.001 CRACK NOTED. RUNNING FROM CORNER OUT PAST FIRST RIVET TO SECOND RIVET APPROXIMATELY 2 1/2 INCHES LONG. RIGHT WING REFULEING DOOR & LOWER SKIN PANEL REMOVED IAW SMP TO FOM ACCESS & REPAIR OF CRACK. DISPLACED TERMINAL STRIPS STRINGER 3 - 688 & STRINGER 3 - 690 FROM RT WING AT WS 610.840 TO FOM SHEETMETAL REPAIR. DISPLACED TERM STRIP ZIPTIED TO ADJACENT STRUCTURE. REMOVED DAMAGED AREA IAW SRM 57-10-00 VOLUME 1 FIGURE 68. RECEIVED FINAL FORM 8100-9 & ACCOMPLISHED REPAIRS IAW EA 8-5710-T0308360.

Part: TRUNNION — CORRODED (ZONE 100) · airframe 94,244 hrs · 26,531 cycles

RT TRUNNION PILLOW BLOCK AFT BOLT HOLE HAS CORROSION. REMOVED CORROSION IAW EA T8-5310-T0302228 P1.

Part: TRUNNION — CORRODED (ZONE 100) · airframe 94,244 hrs · 26,531 cycles

LT TRUNNION PILLOW BLOCK AFT BOLT HOLE HAS CORROSION. REMOVED CORROSION IAW EA T8-5310-T032228 P1.

Part: TRUNNION — CORRODED (MLG) · airframe 94,244 hrs · 26,531 cycles

RT TRUNNION PILLOW BLOCK FWD BOLT HOLE HAS CORROSION ON UPPER SPOT FACE AND EDGE. REMOVED CORROSION IAW EA T8-5310-T0302228.

Part: STRINGER — CRACKED (ZONE 600) · airframe 94,244 hrs · 26,531 cycles

RIGHT WING INNER FIXED L/E UPPER SKIN STRINGER IS CRACKED, OTBD OF L/E SLAT TRACK NR 16. CUT AND REMOVED CRACKED SECTION OF STRINGER, IAW SRM 57-20-00, FIG. 41, VOL. 1 AND REPAIRED IAW EA T8-5710-T0302171 P1.

Part: FINGER DOUBLER — CORRODED (BS 1501-1521) · airframe 94,244 hrs · 26,531 cycles

MAIN CABIN RT SIDE RBL 27, BS 1501-1521, RIVETS MISSING AND LIGHT CORROSION ON FINGER DOUBLER. REMOVED FINGER DOUBLER, REMOVED CORROSION IAW SRM 51-21-01 VOL 2, FABRICATED NEW FINGER DOUBLER AND INSTALLED IAW DWG SG1053000.

Part: HORN — CRACKED (RT WING) · airframe 94,244 hrs · 26,531 cycles

RT OTBD FWD BEARING HORN IS CRACKED. CRACK PROPAGATES FROM LOWER INBD CORNER TO INBD SIDE. R & R IAW WC E-8-5750-5000, F5, PT2 SEQ 259.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 93,515 hrs · 26,242 cycles

EMERGENCY LIGHTS WOULD NOT COME ON WHEN SWITCH ON OR DURING TEST, EMERGENCY TEST PASSES INDICATING BATTERY GOOD. R & R EMERGENCY LIGHTS BATTERY POWER SUPPLY IAW 33-51-01-4 ALL EMERGENCY LIGHTS OPS CHECKED NORMAL. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,498 hrs · 25,845 cycles

ON PREDEPARTURE CHECK, FOUND THE EMERGENCY LIGHT INOPERATIVE, RELAMPED LIGHT AND PERFORMED SUCCESSFUL EMERGENCY LIGHT TEST IAW AMM 33-52-04-2.

Part: SKIN — GOUGED (ZONE 100) · airframe 90,307 hrs · 25,028 cycles

RT FUSELAGE SKIN IS GOUGED AT APPROX STA. 348, APPROX. LONGERON R-36. REMOVED DAMAGE, NDT AS REQUIRED, FAB REPAIR PARTS INSTALLED IAW SRM 53-20-00. NO FUTHER ACTION REQUIRED.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,305 hrs · 25,023 cycles

CTR CARGO BILGE AREA BETWEEN BS1701-1721 AND STRINGER 48R. STRINGER HAS EXFOLIATION CORROSION. R & R STRINGER SPLICE IAW SRM 51-31-01. STRINGER SPLICE FABRICATED ON TRAVELER T10/825356. CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CRACKED (ZONE 600) · airframe 90,305 hrs · 25,023 cycles

DROOP L/E HAS CHAFED AT LEADING INBD AND OTBD SIDES AND CRACK ON THE UPPER SKIN AT RT WING. REPAIR CRACK UPPER SKIN WITH A 0.100" 301-50 STAINLESS STEEL DOUBLER IAW SRM 57-10-00 FIG 55, MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 90,305 hrs · 25,023 cycles

RADOME AREA JUST AFT OF RT SIDE HAS DENT ON EXTERNAL FUSELAGE SKIN. REPAIRED DENT AREA AFT OF RADOME OF RT SIDE OF EXTERNAL FUSELAGE SKIN FROM FS 275 TO FS 295 BETWEEN STR 37R TO STR 39R IAW SRM 53-20-00, MAJOR REPAIR.

Part: FAIRING — CHAFED (RT WING LE) · airframe 90,305 hrs · 25,023 cycles

RT WING FIXED L/E FAIRING LOWER SURFACE HAS CHAFED MARK AT INBD FAIRING TO NR 3 PYLON. REPAIRED RT WING FIXED L/E FAIRING LOWER SURFACE IAW SRM 57-10-00 AND SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 392-450) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN FLOOR RT SIDE AT RBL 26, GALLEY FLOOR BOARD SUPPORT CORRODED. R & R MAIN CABIN FLOORBOARD SUPPORT IAW SRM 51-31-01 AND SRM 53-11-01-19, MAJOR REPAIR.

Part: SEAT TRACK — WORN (BS 1681-1781) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN SEAT TRACK FROM STA 1681 TO STA 1781 AT RBL 76 HAS SEVERAL AREAS "MARKED" ON AND OR INSIDE TRACK THAT ARE WORN. R & R SEAT TRACK FROM STA 1681 TO STA 1781 AT RBL 76 IAW SRM 53-70- 00 FIG 1, REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (RT WING AILERON) · corrosion level 2 · airframe 90,305 hrs · 25,023 cycles

RT WING OTBD AILERON SKIN LOWER SURFACE HAS CORROSION. R & R RT OTBD AILERON IAW AMM 27-10-02-4. OP CHECKED AILERON IAW AMM 27-10-02-4. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 490) · airframe 90,305 hrs · 25,023 cycles

UPPER CARGO SEAT TRACK AT FS 490 AT LBL 8 HAS CORROSION FORMING FROM UNDER FASTENER TO LOWER TRACK AREA. R & R SEAT TRACK SECTION FROM STA 485 TO STA. 505 AT LBL 8 IAW SRM 53-70-00 FIG 1, MAJOR REPAIR.

Part: SKIN — CORRODED (RT WING AILERON) · corrosion level 2 · airframe 90,305 hrs · 25,023 cycles

LT WING OTBD AILERON LOWER SURFACE HAS FASTENERS UNDER PAINT PULLING THROUGH SKIN AND CORROSION FORMING UNDER PAINT. R & R LT OTBD AILERON IAW AMM 27-10-02-4. OPS CHECKED AILERON IAW AMM 27-10-02-4. OPS CHECK GOOD.

Part: SEAT TRACK — DAMAGED (BS 1511-1521) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN SEAT TRACK, RBL 48 STA. 1521-1511 HAS DAMAGED (2 EA) LOBES. R & R SEAT TRACK RBL 48, STA. 1521-1511 IAW SRM 53-70-00. FABRICATED AND RECEIVED NEW SEAT TRACK ON TRAVELER T10/822764.

Part: SEAT TRACK — DAMAGED (BS 1321-1361) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN SEAT TRACK, RBL 48 STA. 1321-1361 HAS 3 DAMAGED LOBES. FOUND SEAT TRACK OUT OF LIMITS IAW SRM 53-70-00 FIG 5. REMOVED DAMAGED SEAT TRACK AT STA 1321-1391 RBL 48 IAW SRM 51-31-01. RECEIVED NEW SEAT TRACK ON TRAVELER NR T10-822763. DRILLED, LOCATED, DEBURRED AND COUNTERSUNK IAW SRM 53-70-00 FIG 1 AT STA 1321-1391 RBL 48. TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED NEW SEAT TRACK AT STA 1321-1391 RBL 48 IAW SRM 53-70-00 FIG 1 AND SRM 51-31-01.

Part: SEAT TRACK — DAMAGED (BS 1441) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN SEAT TRACK, RBL 28 STA 1441 HAS A DAMAGE LOBE. EVALUATED DAMAGE AND DETERMINED TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5. REMOVED DAMAGED SEAT TRACK FROM BS 1391-1451 RBL 28 IAW SRM 51-31-01. FABBED NEW SEAT TRACK ON TRAVELER T10/822387 BATCH NR 0001366488 AND (PLATE) 0001375870 IAW SRM 51-10-01. FABBED NEW SPLICE HAT AND PLATE ON TRAVELER T10/822389 BATCH NR SPLICE HAT AND PLATE IAW SRM 53-70-00. LOCATED AND DRILLED NEW SEAT TRACK AND SPLICE IAW SRM 51-31-01 VOL 2. TREATED AND PRIMED NEW SEAT TRACK AND SPLICE IAW SRM 51-31-01 VOL 2. INSTALLED NEW SEAT TRACK IAW SRM 51-31-01, VOL.2.

Part: SEAT TRACK — DAMAGED (BS 808-908) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN SEAT TRACK, LBL 48 UPPER SURFACE HAS MIN OF 7EA LOBES WORN BETWEEN STA 808-908. R & R SEAT TRACK SEGMENT IAW SRM 53-70-00, STA 785-815 LBL 48. RECEIVED NEW SEAT TRACK ON TRAVELER NR T10/822388. BLENDED OUT GOUGES FROM STA 824-908. AFTER BLEND OUT MINIMUM LIP WIDTH=0.300" MAXIMUM GAP=0.427'. WITHIN LIMITS IAW SRM 53-70-00 FIG. 5.

Part: SEAT TRACK — DAMAGED (BS 1009-1049) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN SEAT TRACK, RBL 48 STA 1009-1049 HAS 4 DAMAGED LOBES. R & R SEAT TRACK RBL 48 STA 1009-1049 IAW SRM 53-70-00 FIG 1. NEW SEAT TRACK FABRICATED ON MAE TRAVELER T10/822479.

Part: SEAT TRACK — DAMAGED (BS 1381-1390) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN, SEAT TRACK AT LBL 8 BETWEEN FS 1381 TO FS 1390 HAS 2 EA DAMAGED TRACK LOBES. FOUND DAMAGE OUT OF LIMIT, R & R SEAT TRACK SECTION IAW SRM 53-70-00 FIG 1 AND SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — WORN (BS 655) · airframe 90,305 hrs · 25,023 cycles

MAIN CABIN SEAT TRACK AT LBL76, F.S. 655 WORN LOBE FOUND OUT OF LIMIT AFTER BLENDING. MAIN CABIN SEAT TRACK FROM STA 635 TO STA 695 AT LBL 76 HAS MIN OF 3 EA WORN LOBES (MARKED). AFTER BLENDING, FOUND LOBES BETWEEN STA 635 TO STA 695 AT LBL 76 WITHIN LIMIT PER SRM 57-70-00 FIG 5, EXCEPT STA 655 FOUND OUT OF LIMIT. R & R SEAT TRACK SECTION FROM STA 625 TO STA 665 AT LBL 76 IAW SRM 57-70-00 FIG 1 AND SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 89,717 hrs · 24,816 cycles

DUE TO FWD CARGO FIRE INDICATION CREW DISCHARGED NR1 CARGO EXTINGUISHER. RELEASED FOR SERVICE IAW MEL: 26-22-01-02-A. ACFT OK FOR SERVICE. REMOVED AND REPLACED NR1 LWR CARGO COMPARTMENT FIRE EXTINGUISHER CONTAINER REF MM 26-22-01-4. PERFORMED LOW PRESSURE TEST OF THE LWR CARGO FIRE EXTINGUISHER CONTAINER REF MM 26-22-02. OPS CHECK GOOD. PERFORMED LOW PRESSURE TEST OF FIRE EXTINGUISHER CONTAINER REF MM 26-22-02. OPS CHECK GOOD. PERFORMED FIRE DISCHARGE CIRUITRY TEST FOR NR 1 SYS. ALL CHECKS GOOD. REF: AMM 26-22-01-5.

Part: SMOKE DETECTOR — INOPERATIVE (CABIN) · airframe 89,348 hrs · 24,690 cycles

AFTER TAXI IN, FOR ABOUT 6 MINUTES, GOT AN INTERMITTENT CABIN SMOKE LEVEL 3 ALERT. IT DID NOT REAPPEAR FOR ABOUT 3 MORE MINUTES. THEN IT WENT ON/OFF MULTIPLE TIMES. RETURN TO GATE. RELEASED FOR SERVICE IAW MEL: 26-17-01-03-A.

Part: SMOKE DETECTOR — MALFUNCTIONED (CABIN) · airframe 86,065 hrs · 23,582 cycles

CABIN SMOKE WARNING, TWO TIMES. FIRST TIME IN CLIMB PASSING FL310. BRIEF FLASH OF MASTER WARNING THEN WENT AWAY. 4-5 MIN LATER LEVEL AT FL330 GOT 2ND MASTER WARNING AND CABIN SMOKE FOR ABOUT 10 SECS. LANDED AT KPDX. FIRE DEPARTMENT INSPECTION NO INDICATION OF HEAT. PER MX TURNOVER CREW REPORTED AREA 2 OF UPPER DECK WAS AREA CAUSING INPUT DURING FLIGHT. REMOVED AND REPLACED ALL NR 2 AREA DETECTOR UNITS PER MM 26-15-00. REMOVED AND REPLACED MSC PER MM 26-15-00. ALL OPS CKS C/W SYSTEM CKS NORMAL. ALSO CHECKED EACH VIA IN COMMAND MODE PER MM 26-15-01, OPS CK NORMAL.

Part: SMOKE DETECTOR — FAILED · airframe 86,065 hrs · 23,582 cycles

CABIN SMOKE WARNING, TWO TIMES. FIRST TIME IN CLIMB PASSING FL310. BRIEF FLASH OF MASTER WARNING THEN WENT AWAY, 4-5 MIN LATER LEVEL AT FL330 GOT 2ND MASTER WARNING AND CABIN SMOKE FOR ABOUT 10 SECS. LANDED AT KPDX. FIRE DEPARTMENT INSPECTION NO INDICATION OF HEAT. PER MX TURNOVER CREW REPORTED AREA 2 OF UPPER DECK WAS AREA CAUSING INPUT DURING FLIGHT. REMOVED AND REPLACED ALL NR 2 AREA DETECTOR UNITS PER MM 26-15-00. REMOVED AND REPLACED MSC PER MM 26-15-00. ALL OPS CKS C/W SYSTEM CKS NORMAL. ALSO CHECKED EACH VIA IN COMMAND MODE PER MM 26-15-01. OPS CK NORMAL.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 86,038 hrs · 23,565 cycles

MCD SEAT TRACK STA 1321 LBL 27 FOUND PITTING CORROSION REMOVED DAMAGED TRACK SECTION IAW 53-70-00. FABBED NEW SECTION ON TRAVELER T8/732807, T8/732808 AND T8/732809. LOCATED AND DRILLED AND INSTALLED NEW TRACK AND SPLICES IAW SRM 53-70-00 AND SRM 53-21-01.

Part: SKIN — DENTED (ZONE 100) · airframe 86,038 hrs · 23,565 cycles

FWD CARGO CUT OUT DOOR AFT LOWER EDGE HAS TWO DENTS, MEASURED DENTS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REPAIRED IAW SRM 53-50-00 FIGURE 8 SHEET 1 AND 2 MAJOR REPAIR.

Part: FRAME — CHAFED (FUSELAGE) · airframe 86,038 hrs · 23,565 cycles

MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGE FROM LINER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/29475, LOCATED AND DRILLED HOLES AND INSTALLED NEW SPLICE AT STA 715 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 86,038 hrs · 23,565 cycles

FWD CARGO DOOR CUT-OUT AFT JAMB CORRODED AT LWR AFT SIDE UNDER GUIDE ROLLER FITTING. REMOVED CORROSION, REMOVED AND REPLACED INTERCOSTAL,STRAP, CORNER FITTING, SEAL RETAINER AND FORMER IAW SRM 51-31-01 AND 53-50-00 FIG 1.

Part: FRAME — CHAFED (FUSELAGE) · airframe 86,038 hrs · 23,565 cycles

MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LINER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729477, LOCATED AND DRILLED HOLES AND INSTALLED NEW SPLICE AT STA 735 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES.

Part: FRAME — CHAFED (FUSELAGE) · airframe 86,038 hrs · 23,565 cycles

MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LINER MOUNT FASTENER. EVALUATED FRAME BLENDED ROUGH EDGES DRILLED HOLE REMOVING ALL DAMAGE FILLED HOLE WITH RIVET IAW SRM 530001 FIG 1A. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES.

Part: FRAME — CHAFED (FUSELAGE) · airframe 86,038 hrs · 23,565 cycles

MCD-FUSELAGE UPPER LOBE AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LINER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729478, LOCATED AND DRILLED HOLES AND INSTALLED NEW SPLICE AT STA 675 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES.

Part: FRAME — CHAFED (FUSELAGE) · airframe 86,038 hrs · 23,565 cycles

MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LINER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/29478, LOCATED AND DRILLED HOLES AND INSTALLED NEW SPLICE AT STA 695 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES.

Part: FRAME — CHAFED (FUSELAGE) · airframe 86,038 hrs · 23,565 cycles

MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LINER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729478, LOCATED AND DRILLED HOLES AND INSTALLED NEW SPLICE AT STA 655 IAW SRM 51-31-01, 53-30-00 FIG 4 REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES.

Part: FRAME — CHAFED (FUSELAGE) · airframe 86,038 hrs · 23,565 cycles

MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED AND DAMAGED FROM LINER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729476, LOCATED AND DRILLED HOLES AND INSTALLED NEW SPLICE AT STA 635 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES.

Part: FRAME — CHAFED (FUSELAGE) · airframe 86,038 hrs · 23,565 cycles

MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LINER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729477, LOCATED AND DRILLED HOLES AND INSTALLED NEW SPLICE AT STA 755 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES.

Part: ENGINE — FAILED (APU) · airframe 84,721 hrs · 23,072 cycles

RETURN TO RAMP DUE TO INABILITY TO SHUT DOWN APU. FOUND PORTIONS OF N1 HAD EXITED DOWN PASSED APU AIR INLET BOOT AT CLAMPS, SLICED THRU APU PRESSURE OIL LINE AND THEN BECAME LODGED INTO APU COMPARTMENT ACCESS DOOR. APU REF WRI 52-40 2307 FOR THE APU ACCESS DOOR REPAIR. REMOVED AND REPLACED APU REF AMM 49-00-00-4.

Part: WIRE HARNESS — BURNED (EXTERNAL POWER) · airframe 83,282 hrs · 22,621 cycles

GROUND POWER IS INTERMITTENT. POWER SHUTS DOWN WHEN A LOAD IS APPLIED. FOUND BURNT "C" PHASE OUTPUT CABLE (C501-21-00C) OF GROUND SERVICE RELAY. REPLACED DAMAGED C501-21-00C CABLE BETWEEN EXTERNAL POWER CONTACTOR R2-218 AND 53-517 REF W/D 24-41-01 PG 703 SHT 2 OF 2. OPS CHECK NORMAL.

Part: SUPPORT — CORRODED (AILERON ACTUATOR) · airframe 82,820 hrs · 22,475 cycles

THE RT INBD AILERON SUPPORT ASSY ACTUATOR FRAME, O/B BARREL NUT BOLT HOLE IS CORRODED. REAMED BARREL NUT BOLT HOLE TO 0.925 DIA" TO REMOVE CORROSION. REQUESTED EA AILERON SUPPORT SUPPORT ASSY ACTUATOR "A" FRAME BOLT HOLE REPAIRED PER EA 8-5740-102045.

Part: SUPPORT — CORRODED (RT AILERON) · airframe 82,820 hrs · 22,475 cycles

THE RIGHT INBOARD AILERON SUPPORT ASSY ACTUATOR A FRAME, O/B BARREL NUT BOLT HOLE IS CORRODED.

Part: DOOR FRAME — CHAFED (ZONE 100) · airframe 79,453 hrs · 21,331 cycles

C/W EA8-5310-55459 FUSELAGE-MAIN FRAME-AFT ENTRY DOOR JAMB REPAIR (P/N AJC7207- 181). CLOSING ACTION 03/10/05 C/W EA8-5310-55459. ON NO. S00017.

Part: PANEL — DAMAGED (ZONE 100) · airframe 79,453 hrs · 21,331 cycles

COMPLY WITH EA 8-5310-55460 MAIN FRAME-AFT BODY PLANK BLEND REPAIR FS 2051, L45L (P/N AJC7164-503). COMPLIED WITH EA 8-5310-55460 MAIN FRAME-AFT BODY PLANK BLEND REPAIR FS 2051, L45L (P/N AJC7164-503).

Part: HINGE — CORRODED (ZONE 600) · airframe 76,175 hrs · 20,069 cycles

COMPLY WITH EA8-5750-60625. WINGS- RT WING I2FB FLAP 2FB FLAP HINGE SUPPORT LOWER 2FB SUPPORT - CORROSION INSPECTION AND REPAIR. CLOSING ACTION ON 82 F11 2F3 ON 2FR JOB ACCOMPLISHED ON N2FR S00033 2C REWORK LOWER 2FB HOLE ON EA 8-5740-70995A 2C S00043 LOWER I2FB HOLE ON EA 8-5740-70995A 28 LOWER I2 FB BUSHING REPLACED PER CMM 57-44-07 ON EA 8-5750-60625. REINSTALLATION ON EA 8-5740-70995A IAW.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 76,175 hrs · 20,069 cycles

REMOVED AND REPLACED 3EA ANGLES IAW 2F SRM 51-31-01 STA 1361. CLOSED 08 2F122 2003 ON FEDEX N 2FR N00327 AND N0112 10 UNDER MAE 2FO NR 3423.

Part: HINGE — CORRODED (RT FLAP) · airframe 76,175 hrs · 20,069 cycles

MDIS 311 57-10 0008867 06AUG03 BFM CLOSE R COMPLLY WITH EA 8-5750-72247 WINGS- RT OUTBOARD FLAP -INBD HINGE CORROSION REPAIR (P/N ARCO502). FACT 08AUG03 19:35 BFM R COMPLIED WITH EA 8-5750-72247 WINGS-RT OUTBOARD FLAP -INB'D HINGE CORROSION REPAIR (P/N ARC0502).

Part: BRACKET — CRACKED (NR 3 ENGINE) · airframe 76,175 hrs · 20,069 cycles

233 ENG HP TURBINE COOLING PNEUMATIC DUCT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW AMM 70-00-00-2.

Part: STATIC PORT — SEPARATED (PITOT/STATIC SYS) · airframe 76,175 hrs · 20,069 cycles

NAVIGATION - ENLARGED GAP BETWEEN ALT STATIC PORT AND FUSE SKIN BY 3A 39017C RPT BY3A 39017 FACT 09AUG03 6 3A20 BFM RD COMPLIED WITH EA 8-3411-72250 NAVIGATION - ENLARGED GAP BETWEEN ALT STATIC PORT AND FUSE SKIN 40 MAE 0D 0 ARII.

Part: HINGE — CORRODED (RT FLAP) · airframe 76,175 hrs · 20,069 cycles

MDIS 311 57-10 0008862 01AUG03 BFM CLOSE RD COMPLY WITH E.A. 8-5750-70999 WINGS-RT OB 27D FLAP-IB HINGE-ACTUATOR ATTACH LUG FACE CORROSION REPAIR ENT BY 3A 39014C RPT BY 3A 39014C. FACT08AUG03 04 3A29 BFM R COMPLIED WITH E.A. 8-5750-70999 WINGS-RH OB FLAP IB HINGE-ACTUATOR ATTACH LUG FACE CORROSION REPAIR MAE ENT BY 3A 39014C RPT BY 3A 39014C.

Part: BRACKET — CRACKED (LT FLAP) · airframe 76,175 hrs · 20,069 cycles

LT WING O/B FLAP IB FWD HINGE PANEL BRACKET CRACKED. REMOVED 2C FABRICATED AND INSTALLED BRACKET IAW SRM 51-31-01.

Part: RIB — DAMAGED (T/E FLAP) · airframe 76,175 hrs · 20,069 cycles

WINGS- RT OUTBD FLAP- INBD CLOSURE RIB DAMAGED HOLE REPAIR 2C P 2FN ARCV 2179 ENT BY 3A 39014C RPT BY 3A 39014C0D. FACT 08AUG03 04 3A34 BFM COMPLIED WITH EA 8-5750-72242 WINGS- RT 2FB FLAP-INBD CLOSURE RIB DAMAGED HOLE REPAIR 2C P 2FN AARC 2179 40 MAE ENT BY3 A 39014C RPT BY 3A 39014C.

Part: CARGO TRACK — GOUGED (CARGO DECK) · airframe 76,175 hrs · 20,069 cycles

MAIN CARGO DECK CARGO TRACK GOUGED STA 575-675 2C RBL 47.50. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 26+51-33-01.

Part: HINGE BRACKET — CORRODED (T/E FLAP) · airframe 76,175 hrs · 20,069 cycles

FLAP HINGE BRACKET LOWER O5 CB BOLT HOLE BORE PITTED ENT BY 3A 484466 RPT BY 3A 484466. FACT 04AUG03 05 3A45 BFM COMPLIED WITH EA 8-5740-70995 WINGS - LT INBOARD FLAP 2C HINGE ASSY ATTACH LUG REWORK 40 MAE NT BY 3A 39014C RPT BY3A 39014C.

Part: BUSHING — CORRODED (T/E FLAP) · airframe 76,175 hrs · 20,069 cycles

LEFT INBOARD FLAP - FLAP MOUNTED HINGE BUSHINGS CORRODED. REMOVED AND REPLACED 4EA BUSHINGS IAW CMM 57-52-01 N 2FR.

Part: SPAR CAP — CORRODED (VERTICAL STAB) · airframe 76,175 hrs · 20,069 cycles

MDIS 311 55-30 0008866 05AUG03 BFM CLOSE COMPLY WITH E.A.8-5530-72245. STABILIZER-VERT-REWORK OF CORROSION ON SPARS AMC7107 AND AMC7185 ENT BY3A 60601C RPT BY 3A 60601C. FACT 08AUG03 19 PERCENT 3A29 BFM COMPLIED WITH EA 8-5530-72245 STABILIZER-VERT-REWORK OF CORROSION ON SPAR CAPS AMC7107 AND AMC7185 ENT BY 3A 39017C RPT BY 3A 39017C.

Part: HINGE — CORRODED (T/E FLAP) · airframe 76,175 hrs · 20,069 cycles

WINGS-R 2FH INBOARD FLAP 2C HINGE ASSY ATTACH LUG REWORKED ENT BY 3A 39017C RPT BY 3A39017. FACT 10AUG03 21 3A10 BFM COMPLIED WITH EA 8-5740-70995A WINGS-R 2FH INBOARD FLAP 2C HINGE ASSY ATTACH LUG REWORK MAE BY 3A DC40999V RPT BY 3A 40999V.

Part: HINGE BRACKET — CORRODED (T/E FLAP) · airframe 76,175 hrs · 20,069 cycles

RIGHT I\B FLAP HINGE BRACKET LOWER O\B BOLT HOLE BORE PITTED. FACT 04AUG03 05:45 BFM R COMPLIED WITH EA 8-5740-70995 WINGS- LEFT I/B FLAP, HINGE ASSY ATTACH LUG REWORK AT MAE.

Part: RING — CRACKED (THRUST REVERSER) · airframe 76,175 hrs · 20,069 cycles

EXHAUST- THRUST REVERSER-REPAIR OF TR OUTER RING P/N 3113M59P001A. FACT 02AUG03 01:10 BFM R COMPLIED WITH EA 8-7832-70994 EXHAUST- THRUST REVERSER- REPAIR OF T/R OUTER ENG P/N 3113M59P001A AT MAE.

Part: HEAT SHIELD — CRACKED (NR 3 ENG) · airframe 76,175 hrs · 20,069 cycles

NR 473 NR 3 ENG AFT ELECTRICAL JUNCTION BOX HEAT SHIELD IS CRACKED. REMOVED AND REPLACED HEAT SHIELD IAW SRM 51-31-01 @ MAE ON N/R N00473.

Part: RING — CORRODED (RT WING) · airframe 76,175 hrs · 20,069 cycles

R/H WING FUEL TANK ACCESS PANEL CHAFE RING HAS PITTED CORR. REMOVED AND REPLACED CHAFE RING AND GANG CHANNEL IAW SRM 51-42-04 AND SRM 51-31-01 AT MAE ON N/R N00926

Part: TRACK — CRACKED (FUSELAGE) · airframe 76,175 hrs · 20,069 cycles

N 462 CROSSTRACK ASSY CRACKED AT STA 969 LBL 27-47 MCD. REPLACED CROSSTRACK ASSY AND INSTALLED IAW W/C 25C5510-01 @ MAE.

Part: ANGLE — CRACKED (ZONE 600) · airframe 76,175 hrs · 20,069 cycles

N 651 RT WING L/E, CRACKED ANGLE AT XORS 317 CLOSING ACTION ON 07/30-03. REMOVED ANGLE IAW SRM 51-31-01.FAB NEW ANGLE IAW DPS 3.69. TREATED AND PRIMED IAW SRM 51-21-01, WITH 2024-T3 BATCH 545293, SERVICE ORDER 6016327.INSTALLED ANGLE IAW SRM 51-31-01.

Part: SPLICE — CRACKED (FRAME) · airframe 76,175 hrs · 20,069 cycles

LEFT MLG WHEEL, AFT END, OUTBOARD WALL, FRAME REPAIR IS CRACKED. CLOSING ACTION ON 07/19/03. FOUND CRACK IN FRAME REPAIR. REMOVED IAW SRM 53-33-01 FAB NEW SPLICE IAW GMM 7-0-1-001 SECTION 3C FROM 7070-T6 .125C. INSTALLED NEW SPLICE IAW SRM 31-33-01.

Part: BOLT — CORRODED (FLAP) · airframe 73,554 hrs · 18,984 cycles

RIGHT I/B FLAP O/B HINGE FWD BRACKET O/B H-11 BOLT CORRODED. R&R BOLTS PER EA 8-5750-60625.

Part: TIRE — BLOWN (MLG) · airframe 73,097 hrs · 18,785 cycles

DURING FLIGHT TEST ALL MAIN LANDING GEAR TIRES BLEW (10) EA.

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS) · airframe 73,097 hrs · 18,785 cycles

DURING FLIGHT TEST BRAKE LAND ALL MAIN LANDING GEAR TIRES BLEW (10) EACH. REMOVED AND REPLACED ALL MLG WHEEL AND TIRE ASSY. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER AMM 32-45-01-2.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 625 TO 765 UPPER CARGO DOOR FWD AND AFT DOOR JAMB STRUCTURAL DAMAGE. REMOVED AND REPLACED DOOR PER EA 8-5330-56188.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

SEAT TRACK AT BS 630 X = 27.50 HAS CRACK IN LWR INBOARD AND OUTBOARD FLANGES.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,097 hrs · 18,785 cycles

FWD LOWER CARGO BS 775 RT FLOOR SUPPORT SIDE STRUT CORRODED. REMOVED AND REPLACED SIDE STRUT PER SRM 53-13-01.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

VERTICAL SUPPORT AT BS 495, X=73 HAS CRACK.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

VERTICAL SUPPORT AT BS 555, X=71 HAS CRACK. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-31-01, 51-00-00, 51-21-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

VERTICAL SUPPORT AT BS 575, X=73 HAS A CRACK. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-31-01, 51-00-00, 51-21-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

VERTICAL SUPPORT AT BS 495 X=73 Z=16 CRACKED BELOW FLOOR. REMOVED AND REPLACED SUPPORT PER SRM 51-10-00 & 51-21-01.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

FWD CARGO BS 939 X=-99 Z=30 CEILING SUPPORT CHANNEL CRACKED. REMOVED AND REPLACED CHANNEL AND BRACKETS PER SRM 51-10-01 & 51-35-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,097 hrs · 18,785 cycles

CORRODED SEAT TRACK AT X=108.00 Z=-19.00 BS 1539-1553. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1841, LBL 22 TO RBL -52, WL -93 ANGLE FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED ANGLE PER SRM 51-35-01 & 51-33-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,097 hrs · 18,785 cycles

BS 1841, LBL 54 TO RBL 54 BELOW AFT FLOOR ROLLER TRAY SUPPORT IS CORRODED. REMOVED AND REPLACED SUPPORT PER SRM 51-35-01 & 51-33-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

FRAME AT BS 1841 ABOVE LONGERON 43R CORRODED. REMOVED AND REPLACED FRAME PER SRM 51-35-01 & 51-33-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1841, RBL 56R, WL -96 CORROSION ON FRAME ABOVE LONGERON 43R. REMOVED AND REPLACED CAP PER SRM 51-35-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1879, X=-59, Z=-19 SEAT TRACK LOBE HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1936, LBL 27, WL 80 SEAT TRACK CORRODED SEAT TRACK CHANNEL. REMOVED AND REPLACED SEAT TRACK PER SRM.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1175, X=-48 SEAT TRACK IN MAIN CABIN GOUGE. REMOVED AND REPLACED SEAT TRACK PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1028-1068 LONG 52 OML DEEP PITTED CORROSION TO EXTERIOR SKIN BOTTOM. REMOVED AND REPLACED SKIN PER SRM & EA.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,097 hrs · 18,785 cycles

BS 1841, LBL 53-58, WL 97 AFT SIDE FRAME CORRODED. REMOVED AND REPLACED CAP PER SRM.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 615 AND 635 X=-27 SEAT TRACK IN MAIN CABIN GOUGED AND OBLONG. REMOVED AND REPLACED SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1079-1099 LONG 27R EXFOLIATING CORROSION ON FLOORBOARD SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 450 TO 460 X=-21 LOWER AVIONICS SKIN BENT INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1028-1068 LONG 52 OML DEEP PITTED CORROSION TO EXTERIOR SKIN BOTTOM. REMOVED AND REPLACED SKIN PER SRM & EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

BS 1877 TO 1887 X=10.Z=-19 SEAT TRACK HAS CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,091 hrs · 18,785 cycles

SEAT TRACK AT BS 1865 TO BS 1871 X=49Z=19 CORRODED. REMOVED AND REPLACED SEAT TRACK PER IAW SRM 53-10-00 FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,097 hrs · 18,785 cycles

BS 1741, X=71.5 TO X=103 FLOOR SUPPORT CORRODED. R&R FLOOR SUPPORT PER SRM 51-00-01 & 51-30-00.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 73,097 hrs · 18,785 cycles

NR 491 AFT PIN RBL 22 AT BS 1967 VERTICAL CORROSION LVL 2 UNDER SEALANT AROUND ACCESS PNL. ** S/D ** COMING

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,097 hrs · 18,785 cycles

HEAVY CORROSION ON FRAME AFT SIDE X=60, Z=-96, BS 1841 LT. REMOVED AND REPLACED FRAME PER SRM 51-35-01 & 51-33-01.

Part: WEB — CRACKED (L/E SLAT) · airframe 73,097 hrs · 18,785 cycles

CRACK NR 3 SLAT RT WING BS XO8 464 & CRACK IN WEB. REMOVED AND REPLACED WEB PER SRM 51-41-01 EA 8-5510-56177.

Part: FIRE WARNING — ACTIVATED (COCKPIT)

ON START APU FIRE LIGHT ILLUM RED TAB, AND FIRED CYLINDER NR 1 BOTTLE. Removed and replaced ENG 2/APU NR 1 FIRE EXT CONTAINER PER DC-10 AMM 26-21-02-2. Removed and replaced APU CARTRIDGE, STARTER PER MM 49-44-01. LEAK CHECK GOOD.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 72,747 hrs · 18,675 cycles

NR 1 ENG SHUTDOWN IN FLT DUE TO COMPRESSOR STALLS DURING PWR REDUCTIONS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,141 hrs · 17,907 cycles

SEAT TRACK CROWN AND FLANGE AREA CORRODED BS 1917 TO BS 1987, RBL 88. SEAT TRACK CROWN AND FLANGE AREA CORRODED BS 415 TO BS 465, RBL 28. *S/D* REMOVED AND REPLACED PER SRM 51-35-01 & 51-32-02 VOL II & 53-70-00 FIG 1 VOL I. REMOVED AND REPLACED PER SRM 53-40-00 VOL 1, 51-31-01 VOL II & DWG NBA 6018.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 70,141 hrs · 17,907 cycles

RIGHT HORIZONTAL STABILIZER CTR LEAD EDGE TEE ANGLE CRACKED. LEFT HORIZONTAL STAB CTR LEAD EDGE TEE ANGLE CRACKED. *S/D* REMOVED AND REPLACED PER 51-31-01 VOL II.

Part: BULKHEAD — CORRODED (MLG WW) · airframe 70,141 hrs · 17,907 cycles

CENTER LAND GEAR WHEEL WELL FWD BULKHEAD AFT FACE CORRODED ON 1 STIFFENER LT & RT O/B. CENTER LANDING GEAR WHEEL WELL FOUND CORRODED ON L-ANGLE FWD BULKHEAD AFT FACE LWR EDGE. *S/D* REMOVED AND REPLACED PER 51-21-01 VOL LLL & 53-00-01 FIG IA VOL I. SNRM 156- REMOVED AND REPLACED PER SRM 51-33-01 VOL II.

Part: SKIN — CRACKED (LE FLAP)

A/C ARRIVED TO EWR WITH DAMAGE TO LH WING OUTBD FORE FLAP. ** S/D ** R&R LT OTBD VANE ASSY PER MM 27-50-03-2. PER OPS CK NO DEFECT NOTED.

Part: FILLET — MISSING (LT WING/FUS)

PIECE OF AC LOST ON T/O ROTATION. LEFT SLAT TO FUSELAGE FILLET DEPARTED A/C. INSP FUSELAGE AFT OF MISSING PERFORMANCE FAIRING NO DAMAGE NOTED. ALSO INSPECTED NR 2 ENG INTAKE WITH NO DAMAGE NOTED. REMOVED AND REPLACED CLOSE-OUT STRIP OF I/B 1L SLAT UPON INSPECTION. REPLACED LOWER FAIR MT FITTING IAW DC10 SRM 51-33-01.

Part: FLEX DUCT — TORN (NR 1 PACK)

STA-ORD - UNABLE TO CONTROL CABIN PRESS IN ANY MODE. CABIN ALT CLIMB AT RATE EXCEED AUTO-SCHEDULE AND AT LEVEL OFF CONTINUE TO CLIMB AT 300 TO 400 FPM. UNABLE TO GAIN CONTROL USING STBY PRESS OR MANUAL PRESS PER RED TABS. CABIN ALT EXCEED 10000 AND EMERGENCY PROC ACCOMPLISHED AND DESCENT AND DIVERT TO ORD. FOUND NR 1 PACK OUTPUT DUCT APART AT FLEX DUCT. ALSO, FOUND FLEX DUCT TORN. REPLACED FLEX DUCT, LEAK CHECKED GOOD. PRESSURIZED A/C. HELD PRESS UP TO 2.0 PSID. IPC REF 21-54-01-01 SHEET 4 ITEM 563 P/N DUO1006-28-20.

Part: ANGLE — CRACKED (VERTICAL STAB)

UPPER VERTICAL FIN BASE ANGLE HAS CRACK INDICATION BETWEEN THE NR 4, 5 FASTENER HOLES FROM THE RT SIDE REF WC 8-553074303B1 - P1 EA 8-5530-3855 DATED 6/8/98 WRITTEN BASE ANGLE WILL BE REPETITIVE INSPECTED AT INTERVALS NOT TO EXCEED 1800 HRS. BASE ANGLE TO BE REPLACED AT NEXT C-CHECK OR APPROXIMATELY 3,600 FLIGHT HOURS.