N524FE

Part: LINE — BROKEN (HYD SYSTEM) · airframe 65,118 hrs · 11,257 cycles

HYD 3 OFF ALERT AFTER GEAR DOWN & LOCKED, RECEIVED HYD 3 FAIL ALERT 58 DEG C MAX PUMP TEMP HYD QTY 2.0 AT BLOCK IN. LEAK APPEARES TO BE AT LT INBD AILERON AREA. FOUND LEAK AT LT INBD AILERON, NR 3 SYS PRESSURE LINE UNION-CHECK VALVE FOUND LOOSE(JUST SNUG) AND 1 OF THE BACKUP RINGS BAD. RESEARCHING PARTS, REF IPC 27-13-07-01, REPLACED 2EA BACKUP RINGS, PN S4929668-115 & 1EA O-RING, PN NAS1611-115 ON LT INBD AILERON ACTUATOR. SERVICED HYD SYS3 IAW MM 12-13-02-3 & AILERONS LEAK CK OPS CK NORMAL IAW MM 27-10-00-2.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 64,440 hrs · 11,029 cycles

RT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE AT FLAP STATION XIFH 147.300 MISREPAIRED. REPAIRED IAW EA 1-5750-163586. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 64,440 hrs · 11,029 cycles

RT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE AT FLAP STATION XIFH 225.140 MISREPAIRED. REPAIRED IAW EA 1-5750-163586. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 64,440 hrs · 11,029 cycles

LT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE AT FLAP STATION XIFH 219.55 MISREPAIRED. REPAIRED IAW EA 1-5750-163585. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 64,440 hrs · 11,029 cycles

RT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE AT FLAP STATION XIFH 165.300 MISREPAIRED. REPAIRED IAW EA 1-5750-163586. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 64,440 hrs · 11,029 cycles

RT WING INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE MISREPAIRED. REPAIRED IAW EA 1-5750-163586. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 64,440 hrs · 11,029 cycles

LOWER VERTICAL STABILIZER, NR 2 ENGINE INTAKE DUCT, REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED IAW SRM 55-30-02 REPAIR 2 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 64,440 hrs · 11,029 cycles

LT INBD T/E FLAP INBD LOWER SEGMENT UPPER SURFACE FOUND MISREPAIRED. REPAIRED IAW EA 1-5750-163585. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: WEB — CRACKED (BS 2015) · airframe 64,440 hrs · 11,029 cycles

AFT FUSELAGE BS 2015, X= -15 UPPER STABILIZER CUT-OUT PANEL LINE WEB FOUND CRACKED.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 64,440 hrs · 11,029 cycles

RT WING INBD FLAP UPPER SKIN AT XIFH 140 MISREPAIRED. REPAIRED IAW SRM 57-00-01 FIGURE 201 REPAIR 2 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 64,440 hrs · 11,029 cycles

RT WING OTBD T/E FLAP VANE, OTBD LOWER EDGE FOUND CHAFED. REPAIRED AS PER EA 1-5750-165191. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: SKIN — MISREPAIRED (BS 1021 L40R) · airframe 64,440 hrs · 11,029 cycles

FUSELAGE LOWER SKIN BS 1021, LONGERON 40 RT MISREPAIRED. REPAIRED PER SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 51. FUSELAGE LOWER SKIN STATION 1021 LONGERON 40 RIGHT CARRIED OUT REPAIR PER SRM 53-00-01 FIGURE 201, CLASS 1, REPAIR 1 & REVISION 51. EO 1-5100-7-5001B2 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: SKIN — CRACKED (ZONE 500) · airframe 64,440 hrs · 11,029 cycles

LEFT WING DROOP L/E SLAT UPPER SKIN FOUND CRACKED. REPAIRED IAW EA 1-5740-165189. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: FILLET — ERODED (ZONE 600) · airframe 64,440 hrs · 11,029 cycles

RT WING NR 1 SLAT PERFORMANCE FILLET EXTERIOR COMPOSITE ERODED. REPAIRED IAW EA 1-5740-163000. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: FILLET — ERODED (NR 1 SLAT) · airframe 64,440 hrs · 11,029 cycles

LT WING NR 1 SLAT PERFORMANCE FILLET EXTERIOR COMPOSITE ERODED. REPAIRED IAW EA 1-5740-162999. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 64,440 hrs · 11,029 cycles

11 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS =690 AND STA=700. REPAIRED AS PER SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. INITIAL REPEAT INSPECTION REQUIRED 2,000 CYCLES AFTER COMPLETION OF THIS REPAIR AND REPETITIVE INSPECTION EVERY 2,000 CYCLES AS PER SRM 57-20-02 TABLE 201 REPAIR 5 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100 REVISION 116.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 64,440 hrs · 11,029 cycles

12 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STA=700. REPAIRED AS PER SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. INITIAL REPEAT INSPECTION REQUIRED 2,000 CYCLES AFTER COMPLETION OF THIS REPAIR AND REPETITIVE INSPECTION EVERY 2,000 CYCLES AS PER SRM 57-20-02 TABLE 201 REPAIR 5 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100 REVISION 116.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 64,440 hrs · 11,029 cycles

FRAME MISREPAIRED BS 535, LONGERON 24L. REPAIRED IAW SRM 53-20-07 FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.

Part: FRAME — MISREPAIRED (BS 535) · airframe 64,440 hrs · 11,029 cycles

FRAME MISREPAIRED BS 535, LONGERON 18L, REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 64,440 hrs · 11,029 cycles

LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 43 LT FOUND CRACKED. R & R WITH FABRICATED SPLICE IAW SRM 51-33-01, REV 51. SPLICE FABRICATED IAW DWG A5A7116, REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: LONGERON SPLICE — CRACKED (BS 1541) · airframe 64,440 hrs · 11,029 cycles

LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 51 RT FOUND CRACKED. REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 51. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 64,440 hrs · 11,029 cycles

LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 37 LT FOUND CRACKED. REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 51. SPLICE FABRICATED AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 64,440 hrs · 11,029 cycles

LOWER CENTER CARGO LONGERON SPLICE BETWEEN STA 5-113 AND 1541, LONGERON 43 RT FOUND CRACKED. R & R WITH FABRICATED SPLICE IAW SRM 51-33-01, REV 51. SPLICE FABRICATED IAW DWG A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 64,440 hrs · 11,029 cycles

LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 34 LT FOUND CRACKED. REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 51. SPLICE FABRICATED AS PER DWG A5A7112 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: LONGERON SPLICE — CRACKED (52 LEFT) · airframe 64,440 hrs · 11,029 cycles

LOWER CENTER CARGO LONGERON SPLICE BETWEEN STATION 5-113 AND 1541, LONGERON 52 FOUND CRACKED. R & R WITH FABRICATED SPLICE IAW SRM 51-33-01, REV 51. SPLICE FABRICATED IAW DWG A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — CRACKED (ZONE 500) · airframe 64,440 hrs · 11,029 cycles

LEFT WING NR 8 SLAT INNER SKIN FOUND CRACKED BETWEEN NR 17 AND NR 18 SLAT TRACK AREA. REPAIRED IAW SRM 57-40-01 FIGURE 201 REPAIR 3 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: SEAT TRACK — DAMAGED (BS 1125) · airframe 64,440 hrs · 11,029 cycles

MAIN DECK CARGO TRACK AT BS 1125, "X" = -8.5 FOUND DAMAGED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 64,440 hrs · 11,029 cycles

NOSE LANDING GEAR LT TRUNNION ATTACHMENT FITTING FOUND CRACKED. REPAIRED IAW SRM 53-10-14, FIG 202, REPAIR 2, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.

Part: CARGO TRACK — DAMAGED (BS 1125) · airframe 64,440 hrs · 11,029 cycles

MAIN DECK CARGO TRACK AT BS 1125, "X" = 27.5 FOUND DAMAGED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 64,440 hrs · 11,029 cycles

LOWER CENTER CARGO DOOR UPPER FRAME AT DOOR ACTUATOR ARM AREA FOUND CRACKED. REPAIRED IAW EA 1-5310-163577 TITLE: FUSELAGE - MAINFRAME- CENTER CARGO DOOR UPPER JAMB BEAM - CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 60,953 hrs · 10,108 cycles

R1 DOOR DISARM LIGHT INOPERATIVE. REMOVED & REPLACED DOOR 1 R DOOR DISARMED LIGHT ASSY (L2-1117) IAW WDM 52-11-01. OP'S CHECKED NORMAL.

Part: RIB — CRACKED (NR 1 SLAT LT) · airframe 58,773 hrs · 9,609 cycles

LT WING NR 1 SLAT, ADJACENT TO T/E, INBD RIB FOUND CRACKED. CRACKED RIB REMOVED AND REPLACED WITH A NEW RIB AS PER SRM 51-31-01 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: RIB — CRACKED (LT WING) · airframe 58,773 hrs · 9,609 cycles

LT WING - CRUISE PERFORMANCE FILLET, ADJACENT TO T/E, OTBD RIB FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-71 FIG 201 REPAIR 1 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: BEAM — CRACKED (ZONE 200) · airframe 58,773 hrs · 9,609 cycles

MAIN DECK CABIN, RT 3 DOOR NR 2 BEAM FWD STOP SUPPORT FOUND CRACKED. BEAM REMOVED AS PER SRM 51-31-01 REVISION 45. NEW BEAM FABRICATED AND INSTALLED AS PER EA 1-5210-143528. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 58,773 hrs · 9,609 cycles

RT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 69.0. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 69.0.

Part: SEAT TRACK — CORRODED (BS 1359) · corrosion level 2 · airframe 58,773 hrs · 9,609 cycles

MAIN DECK CABIN, LT STA 1359, "X" = 8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1331 TO STA 1371 X=8.5 AS PER SRM 53-00-52 FIG 201 REPAIR I REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 53,607 hrs · 8,350 cycles

MAIN DECK CARGO AT STA 5-70 TO STA 5-120 X= -8.5 SEAT TRACK FOUND CORRODED ON SEVERAL LOCATIONS. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-70-00 FIGURE 1 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 107.

Part: RIB — CRACKED (RT WING LE) · airframe 53,607 hrs · 8,350 cycles

RIGHT HAND WING LEADING EDGE LOWER ACCESS AT STATION XOS 1003 INBOARD RIB FOUND CRACKED. REMOVED IAW SRM 51-31-01. VOLUME II REVISION 40 AND REPLACED WITH A NEW RIB IAW SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 107.

Part: CABLE — FAILED (MLG) · airframe 51,088 hrs · 7,784 cycles

ON TAKEOFF RT MAIN GEAR INDICATED UNSAFE AFTER RAISING HANDLE. ALSO, CONFIRMED ON SD. QRH HAD US CYCLE. SAME INDICATION, ON GEAR DOWN, ALL INDICATED SAFE. INSTALLED NEW TARGET RT MLG GEAR WELL DOOR 32-61-15-4. ADJ CLEARANCE BET PROX SENSOR AND THE TARGET ASSEMBLY 32-61-15-4. REMOVED AND REPLACED RT MLG FOLLOW UP CTL CABLE 20-20-06-2. CARRIED LANDING GEAR POSITION FOLLOW UP CABLE ADJ 32-31-00-010-021. PERFORMED LANDING GEAR EXT/RET IAW AMM 32-30-00-00 FOUND SATIS.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 48,792 hrs · 7,263 cycles

FORWARD CARGO COMPARTMENT: STA 979 TO STA 1019 X = -35 CHANNEL FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5340-117084, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 48,792 hrs · 7,263 cycles

FORWARD CARGO COMPARTMENT: STA 6-70 X = 40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING AREA FOUND HOLE ELONGATED. COMPLIED WITH FEDEX E.A.1-5340-117081. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 48,792 hrs · 7,263 cycles

FORWARD CARGO COMPARTMENT: STA 959 TO STA 979 X = -40 CHANNEL DOLLY ASSEMBLY RETRACTOR, MOUNTING HOLE FOUND DAMAGED. COMPLIED WITH FEDEX EA. 1-5340-117082. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 48,792 hrs · 7,263 cycles

FORWARD CARGO COMPARTMENT: STA 6-70 X = -40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING AREA FOUND DAMAGED. DAMAGED. COMPLIED WITH FEDEX E.A.1-5340-117081. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 48,792 hrs · 7,263 cycles

FORWARD CARGO COMPARTMENT: STA 615 X = -40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING ANCHOR NUT MOUNTING AREA FOUND DAMAGED. COMPLIED WITH FEDEX E.A.1-5340-117080. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 48,792 hrs · 7,263 cycles

FORWARD CARGO COMPARTMENT: STA 615 X = 40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING AREA FOUND DAMAGED. COMPLIED WITH FEDEX E.A.# 1-5340-117080. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CHANNEL — CHAFED (ZONE 100) · airframe 48,792 hrs · 7,263 cycles

FORWARD CARGO COMPARTMENT: STA 859 TO STA 899 X = -35 CHANNEL FOUND CHAFED. COMPLIED WITH FEDEX E.A. 1-5340-117085, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CHANNEL — DAMAGED (ZONE 100) · airframe 48,792 hrs · 7,263 cycles

FORWARD CARGO COMPARTMENT: STA 899 TO STA 919 X = -40 CHANNEL DOLLY ASSEMBLY RETRACTOR MOUNTING HOLE FOUND ELONGATED. COMPLIED WITH FEDEX E.A. 1-5340-117082, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (BS 1741 L12L) · airframe 48,792 hrs · 7,263 cycles

MAIN DECK CARGO, LEFT SIDEWALL STRUCTURE FRAME AT STA 1741 LONGERON 12L FOUND CRACKED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTIONS EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT WING LE) · airframe 48,792 hrs · 7,263 cycles

LEFT WING LEADING EDGE AT STA XOS 774 CAVITY EDGE FOUND CRACKED. REPAIRED AS PER SRM 57-10 -00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DUCT — CRACKED (RT WING) · airframe 48,792 hrs · 7,263 cycles

RT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT OUTBOARD CORNER FOUND CRACKED. FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5710-117087. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — GOUGED (RT WING LE) · airframe 48,792 hrs · 7,263 cycles

RIGHT WING, LEADING EDGE UPPER SURFACE FOUND DEEP GOUGE AT XIS 247. REPAIRED AS PER SRM 57-10-00 FIGURE 24 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 48,792 hrs · 7,263 cycles

LEFT WING INBOARD FLAP SURFACE FOUND DENTS (3 EACH). REPAIRED AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: THRUST REVERSER — DENTED (NR 1 ENGINE) · airframe 45,052 hrs · 6,355 cycles

DURING PASSENGER TO FREIGHT CONVERSION ON THRUST REVERSE ENGINE NR 1 PRATT & WHITNEY, FOUND DENT LONG 15 INCHES AND MAX DEPTH 0.120 INCH, LARGE .800 INCH. REPAIRED FOR SRM MD11 54-30-00 REPAIR N14.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 45,052 hrs · 6,355 cycles

DURING PASSENGER TO FREIGHT CONVERSION: FOUND CORROSION ON LT WING UPPER REAR SPAR CAP AT STA XORS 653.100, XORS 737,550, XORS 826.500. REMOVED CORROSION FOR SRM 57-20-00 FIG 16. MEASURED THK AND IN LIMITS FOR SRM 57-20-00 FIG 16. PERFORMED DYE PENETRANT INSPECTION AND PROTECTED AREA FOR SRM 51-21-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK - CORROSION FOUND ON SEAT TRACK UPPER FLANGE BETWEEN STA 859 TO 879 AT X= 25.7. REPAIR CARRIED OUT AS PER SRM 53-70-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,039 hrs · 6,353 cycles

CABIN - LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 APPROXIMATELY X=21 UPPER SURFACE SEVERAL LOCATION FOUND WITH CORROSION. CABIN - LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 X=21 CORRODED SUPPORT. REMOVED PER SRM 51-31-01 VOLUME II. NEW SUPPORT REWORKED PER DRAWING AGA7497. NEW SUPPORT PAINTED AND PART MARKED AS PER SRM 51-21-01 VOLUME II AND GMM 7-0-1001. NEW SUPPORT INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

LOWER FUSELAGE: FORWARD CARGO DOOR CUTOUT AFT LOWER AREA FOUND WITH DENTS. DENT MARK ON LOWER FUSELAGE: FORWARD CARGO DOOR CUTOUT AFT LOWER AREA REPAIRED AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REFER TO SNRM N0654 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CABIN - FLOOR PANEL 271EF MOUNTING SUPPORT TEE ANGLE BRACKET FOUND CRACKED AT FS STA 1521.00. NEW -T- ANGLE REWORKED AS PER DRAWING ACA3762. CRACKED -T- ANGLE ON CABIN FLOOR PANEL 271EF MOUNTING AREA REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT HAND WING - OUTBOARD FLAP SECONDARY UP STOP FITTING CRACKED. RIGHT HAND WING - OUTBOARD FLAP SECONDARY UP STOP CRACKED FITTING. REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 5-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR, AS PER GMM 6-2-100.

Part: REPAIR — NONE (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

UPPER FUSELAGE AT APPROXIMATELY STA 1781 - 1821 TOP CROWN FORWARD OF NR 2 INLET LIP FOUND DOUBLER REPAIR. PREVIOUS DOUBLER REPAIR AT UPPER FUSELAGE APPROXIMATELY AT STA 1781- 1821 TOP CROWN FORWARD OF NR 2 INLET LIP EVALUATED AND FOUND REPAIR CARRIED OUT IAW DELTA AIRLINES ENGINEERING REPAIR/AUTHORIZATION NO.377652-14, TITLE: "FUSELAGE/CROWN SKIN / FS 1801-1821, STR 3L-4L / SRM REPAIR DEVIATION. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: REPAIR — NONE (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CABIN - ATTIC AREA FS STA 1781 - 1821 BETWEEN STRINGER 2L - 4L FOUND WITH EXISTING SKIN DOUBLER REPAIR TAG ER/A 377652-14 REVISION 03/22/00. PREVIOUS DOUBLER REPAIR AT CABIN ATTIC FS STA 1781-1821 BETWEEN STRINGER 2L-4L EVALUATED AND FOUND REPAIR CARRIED OUT IAW DELTA AIRLINES ENGINEERING REPAIR/AUTHORIZATION NR 377652-14.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK - FLOOR AREA INTERCOSTAL BETWEEN STA 575 TO 595 RIGHT HAND ADJACENT TO LONGERON 27 FOUND CRACKED. MAIN DECK - FLOOR AREA INTERCOSTAL CRACKED AREA BETWEEN STA 575 TO 595 RIGHT HAND LONGERON 27 CARRIED OUT REPAIR AS PER SRM 53-00-01 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CABIN LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 APPROXIMATELY AT X = -75 UPPER SURFACE SEVERAL LOCATION FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: REPAIR — MISMANUFACTURED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

LOWER FUSELAGE CENTER CARGO DOOR CUTOUT AFT LOWER AREA FOUND WITH EXISTING REPAIR (ER/A 361508-14). EXISTING REPAIR ON LOWER FUSELAGE CENTER CARGO DOOR CUTOUT AFT LOWER AREA EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM 53-50-00 FIGURE 16 VOLUME I. EXISTING REPAIR REMOVED AS PER SRM 51-31-01 VOLUME II AND NEW REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 53-50-00 FIGURE 16 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

FS STA 430 LBL 27, FLOOR SUPPORT STRUCTURE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01.

Part: REPAIR — NONE (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

SEAT TRACK MISMATCH RIGHT OUTBOARD CURVED TRACK FS1879. SNRM N2649: PREVIOUS REPAIR AT RIGHT HAND OUTBOARD CURVED SEAT TRACK AT FUSELAGE STATION 1879 MISMATCH EVALUATED AND FOUND REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH DELTA AIRLINES ENGINEERING REPAIR/AUTHORIZATION 333185-14, TITLE: FUSELAGE/CABIN/SEAT TRACK MISMATCH/RT OUTBOARD CURVED TRACK/FS1879. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: MOUNT — CORRODED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

LEFT WING WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE LOWER MOUNT SURFACE CORRODED. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94564.

Part: MOUNT — CORRODED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

FOUND RIGHT WING, REFWERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER MOUNT BORE CORRODED. REPAIRED AS PER FEDEX EA 1-5750-94562.

Part: BUSHING — MIGRATED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT HAND WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE UPPER INBOARD MOUNT BUSHING MIGRATED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94562.

Part: MOUNT — CORRODED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564.

Part: MOUNT — CORRODED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

LEFT HAND WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE LOWER INBOARD MOUNT BORE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564.

Part: HINGE — CORRODED (TE FLAPS) · airframe 45,039 hrs · 6,353 cycles

LEFT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE OUTBOARD SIDE FOUND CORROSION. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94560.

Part: MOUNT — CORRODED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

FOUND RIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94562.

Part: MOUNT — CORRODED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG BORE CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 15750-94562.

Part: BUSHING — MIGRATED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

FOUND RIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE UPPER OUTBOARD MOUNT BUSHING MIGRATED.

Part: MOUNT — CORRODED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD LUG BORE CORRODED.

Part: MOUNT — CORRODED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94563.

Part: MOUNT — CORRODED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR OUTBOARD LUG BORE CORROSION. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564.

Part: MOUNT — CORRODED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND LEFT WING: WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER INBOARD MOUNT BORE CORRODED. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94563.

Part: UNKNOWN — UNKNOWN (ZONE 300) · airframe 45,039 hrs · 6,353 cycles

TO CARRY OUT TRIMMING OF LEFT HAND AFT CHORD TO FACILITATE LEFT HAND NR 35 BORE CLEANING ACCESS. REPAIRED AS PER FEDEX EA 1-5510-94569.

Part: STRUCTURE — TOOL DAMAGE (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

LEFT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE INBOARD SIDE FOUND TOOL MARK. TOOL MARK REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94560.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE INBOARD SIDE FOUND CORROSION. CORROSION REMOVED AS PER FEDEX EA 1-5750-94561.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE OUTBOARD SIDE FOUND CORROSION. CORROSION REMOVED AS PER FEDEX EA 1-5750-94561.

Part: SKIN — CRACKED (ZONE 700) · airframe 45,039 hrs · 6,353 cycles

FOUND LEFT MAIN LANDING GEAR DOOR INTERIOR SKIN ON TOP NEAR THE HINGE AREA FOUND CRACKED. FILLER AND REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 VOLUME I. NEW FILLER AND REPAIR DOUBLER INSTALLED AS PER SRM 51-35-01 VOLUME II. LEFT HAND MAIN LANDING GEAR DOOR REMOVED AND REINSTALLED AS PER MM 32-14-20-4. CARRIED OUT LEFT HAND MAIN LANDING GEAR DOOR OPERATION TEST AS PER AMM 32-34-00-860-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: NONE — NONE (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CONFORMITY INSPECTION RECORD FOR N524FE ITEM 8, 2007 AFT PRESSURE BULKHEAD INTERNAL HAD A SPLICE REPAIR AT 6 O'CLOCK POSITION. REPAIR IS PAINTED GRAY. FOUND REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-40-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. NARI, NO M OR D.

Part: REPAIR — UNKNOWN (BS 775-795) · airframe 45,039 hrs · 6,353 cycles

SNRM N1608: REFERENCE TO EO 1-5100-7-5001 PT1 - FORWARD CARGO - STA 775 TO 795 LONGERON 27R FOUND WITH EXISTING REPAIR. FOUND REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. THIS IS NOT A REPORTABLE ISSUE, NO MALFUNCTION OR DEFECT.

Part: SKIN — DENTED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

FOUND CABIN, R4 DOOR EXTERIOR SKIN LOWER EDGE FOUND WITH DENT. CARRIED OUT REPAIR AS PER SRM 52-10-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

STA 859 LBL 8 SEAT TRACK FOUND CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK, CORROSION FOUND SEAT TRACK UPPER FLANGE BETWEEN STA 899 TO 919 AT X = 8.5. REPAIR CARRIED OUT AS PER SRM 53-70-00.

Part: REPAIR — NONE (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

SNRM N1460: FORWARD CARGO - STA 1079 LONGERON 27R FOUND WITH EXISTING REPAIR. REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. THIS IS NOT A REPORTABLE ISSUE. NO DEFECT OR MALFUNCTION.

Part: REPAIR — UNKNOWN (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

SNRM N1609: REFERENCE TO E1-5100-7-5001 PT1 - FORWARD CARGO - STA 839 TO 859 LONGERON 27R FOUND WITH EXISTING REPAIR. REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. NARI, NO M OR D.

Part: SKIN — DENTED (SERVICE DOOR) · airframe 45,039 hrs · 6,353 cycles

SNRM N2641: CABIN - R4 DOOR EXTERIOR SKIN UPPER EDGE FOUND WITH DENT. CARRIED OUT REPAIR AS PER SRM 52-10-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

FS 5-0 TO 1501 LBL 21 FOUND SEAT TRACK WITH CORROSION. REMOVED AS PER SRM 51-21-01. FOUND EXCEEDED LIMIT AS PER SRM 53-70-00. REMOVED AT EXISTING SPLICE AND TRIMMED AS PER SRM 53-70-00. NEW SEAT TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT ANGLE — CHAFED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE CENTER SUPPORT ANGLE STRUCTURE FOUND CHAFED. REMOVED AS PER CMM 20-11-02 AND FOUND WITHIN DRAWING ARC2126 DESIGN LIMIT. ORIGINAL THICKNESS = 0.180", REMAINING THICKNESS = 0.175", MATERIAL REMOVED = 0.005". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: REPAIR — UNKNOWN (R4 DOOR) · airframe 45,039 hrs · 6,353 cycles

CABIN, R4 DOOR EXTERIOR SKIN LOWER EDGE FOUND WITH EXISTING REPAIR TAG NR ERA382372-14. EVALUATED AND FOUND NOT IAW SRM 52-10-00. REPAIR AREA TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 52-10-00, FIGURE 10, VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: REPAIR — MISINSTALLED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 219 TO 225, YIFH 46 TO 52 FOUND WITH EXISTING REPAIR. EVALUATED AND FOUND NOT CARRIED OUT IN ACCORDANCE WITH SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. RIGHT HAND WING - INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 219 TO 225, YIFH 46 TO 52 WITH EXISTING REPAIR REMOVED AND REPAIR IS CARRIED OUT AS PER SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: REPAIR — MISINSTALLED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 165 TO 171, YIFH 54 TO 60 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 165 TO 171, YIFH 54 TO 60 EVALUATED AND FOUND CARRIED OUT NOT IN ACCORDANCE WITH SRM 57- 10-00 FIGURE 34 SHEET 1 VOLUME I. RIGHT HAND WING - INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 165 TO 171, YIFH 54 TO 60 WITH EXISTING REPAIR REMOVED AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100.

Part: REPAIR — MISINSTALLED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 147 TO 153, YIFH 60 TO 63 FOUND WITH EXISTING DENT REPAIR. EVALUATED AND FOUND REPAIR NOT IN ACCORDANCE WITH SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 147 TO 153, YIFH 60 TO 63 WITH EXISTING DENT REMOVED AND REPAIR IS CARRIED OUT AS PER SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CORROSION FOUND ON SEAT TRACK CROWN AREA FROM STA 810 TO STA 859 AT X = -75. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1. REPAIR IS CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT WING - NR 5 SLAT LEADING EDGE FOUND DENTED. TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK - CORROSION FOUND ON SEAT TRACK BASE FROM STA 839 TO 859 ADJACENT TO X = 75. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

RIGHT WING, NR 3 SLAT LEADING EDGE FOUND DENTED. TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK, SEAT TRACK BASE FOUND CORROSION ADJACENT TO STA 430 APPROXIMATELY X = 27.5. REMOVED AS PER SRM 51-21-01 VOLUME II FOUND EXCEEDED LIMIT AS PER SRM 53-00- 01 VOLUME I. DAMAGED SEAT TRACK REMOVED AS PER SRM 51-31-01 VOLUME II. NEW TRACK PART NUMBER ABA7684-509 MACHINED AS PER DRAWING ABA7684 AT STA 430 APPROXIMATELY X = 27.5 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 45,039 hrs · 6,353 cycles

HORIZONTAL STABILIZER RIGHT NR 36 BORE FOUND CORROSION EXCEED LIMITS. REPAIR CARRIED OUT IAW FEDEX EA 1-5510-94568.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CABIN, LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 APPROX X=-21 LAVATORY TIE DOWN UPPER SURFACE FOUND WITH MINOR 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 6-100-1149) · airframe 45,039 hrs · 6,353 cycles

FOUND MAIN DECK CABIN, STA 6-100 TO 1149 LBL 8 SEAT TRACK FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 830) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK CABIN, STA 830 LBL 26 SEAT TRACK FOUND CORRODED. REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00. TRIMMED AS PER SRM 53-70-00. SPLICE FABRICATED AND INSTALLED AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 899-999) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK CABIN, STA 899, 939, 959 AND 999 RBL 8 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-70-00.

Part: FLOOR SUPPORT — CORRODED (BS 1911) · airframe 45,039 hrs · 6,353 cycles

CABIN, LATERAL FLOOR SUPPORT ADJ TO STA 1911 FROM X=21 TO X= 75 FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1821-1901) · airframe 45,039 hrs · 6,353 cycles

CABIN, LONGITUDINAL FLOOR SUPPORT FROM STA 1821 TO 1901 APRROX X=30 UPPER SURFACE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FLOOR SUPPORT — BROKEN (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CABIN, LONGITUDINAL FLOOR SUPPORT '' U '' CHANNEL ADJ TO X=0 STA 1942 FOUND FASTENER ATTACHMENT HOLE BROKEN. REMOVED AND REPLACED AS PER SRM 51-31-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CABIN, SEAT TRACK BASE ADJ TO STA 1825 APPROX X = -21 FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70- 00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: REPAIR — MISMANUFACTURED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

LOWER FUSELAGE FWD CARGO DOOR CUTOUT AFT LOWER AREA FOUND WITH EXISTING REPAIR. EXISTING REPAIR ON LOWER FUSELAGE FORWARD CARGO DOOR CUTOUT AFT LOWER AREA EVALUATED AND FOUND NOT IAW SRM 53-50-00, FIGURE 16, VOLUME I. EXISTING REPAIR REMOVED AS PER SRM 51-33-01 VOLUME II, AND NEW REPAIR CARRIED OUT AS PER SRM 53-50-00, FIGURE 16, VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2- 100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 APPROX X=18 FOUND UPPER SURFACE CORROSION AT SEVERAL LOCATION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 899) · airframe 45,039 hrs · 6,353 cycles

FOUND MAIN DECK CABIN STA 899 LBL 26 SEAT TRACK CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,039 hrs · 6,353 cycles

CABIN LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 APPROX AT X= 75 UPPER AND LOWER SURFACE SEVERAL LOCATION FOUND 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 859-879) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK CORROSION FOUND ON SEAT TRACK UPPER FLANGE BETWEEN STA 859 TO 879 AT X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00.

Part: SEAT TRACK — CORRODED (BS 6-100-1149) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK CABIN, STA 6-100 TO 1149 RBL 8 SEAT TRACK FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-70-00.

Part: SEAT TRACK — CORRODED (BS 919-979) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK CORROSION FOUND ON SEAT TRACK FROM STA 919 TO 979 ADJ TO X=-8.5. REPAIRED AS PER SRM 53-70-00.

Part: SEAT TRACK — CORRODED (BS 879-899) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK, CORROSION FOUND ON SEAT TRACK UPPER FLANGE BETWEEN STA 879 TO 899 AT X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00.

Part: SEAT TRACK — UNDAMAGED (BS 1136) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK CABIN, STA 1136 LBL 8 SEAT TRACK FOUND WITH CORROSION. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-70-00

Part: SEAT TRACK — CORRODED (BS 839) · airframe 45,039 hrs · 6,353 cycles

MAIN DECK, CORROSION FOUND ON SEAT TRACK CROWN AREA ADJ TO STA 839 AT X=27.5. REPAIR CARRIED OUT AS PER SRM 53-70-00.

Part: REPAIR — CORRODED (ZONE 300) · airframe 45,039 hrs · 6,353 cycles

PT1 HORIZONTAL STABILIZER RT NR 25 BORE FOUND WITH EXISTING BUSHING REPAIR WITH CORROSION. CORROSION AND EXISTING REPAIR BUSHING ON HORIZONTAL STABILIZER RT NR 25 BORE REMOVED BY REAMING BORE TO 1.067 DIAMETER AND FOUND WITHIN LIMIT AS PER FEDEX EO 1-5510-7-5000 D1 PT1. NEW REPAIR BUSHING FABRICATED AND INSTALLED AS PER FEDEX EO 1-5510-7-5000 D1 PT1

Part: RIB — CRACKED (LT WING) · airframe 45,039 hrs · 6,353 cycles

FOUND LEFT WING FIXED LEADING EDGE NR 16 TRACK INBOARD RIB CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 45,039 hrs · 6,353 cycles

FOUND CENTER CARGO, STA 5-113 TO 1541 LONGERON 30 RT SPLICE CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DRAWING A5A7112 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

FOUND CENTER CARGO, STA 5-113 TO 1541 LONGERON 38L SPLICE CRACKED. CRACKED LONGERON SPLICE AT CENTER CARGO STA 5-113 TO 1541 LONGERON 38L REMOVED AND REPLACED WITH NEW FABRICATED SPLICE AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

FOUND CENTER CARGO STA 5-113 TO 1541 LONGERON 44L SPLICE CRACKED. NEW LONGERON 44L SPLICE FABRICATED AS PER DRAWING A5A7116. CRACKED LONGERON 44L SPLICE ON CENTER CARGO STA 5-113 TO 1541 REMOVED AND REPLACED AS PER SRM 51- 33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

FOUND CENTER CARGO, STA 5-113 TO 1541 LONGERON 44R SPLICE CRACKED. CRACKED SPLICE AT CENTER CARGO STA 5-113 TO 1541 LONGERON 44R REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

FOUND CENTER CARGO, STA 1641 TO 1661 LONGERON 44R SPLICE CRACKED. REMOVED AND INSTALLED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

FOUND CENTER CARGO STA 5-113 TO 1541 LONGERON 38R SPLICE CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

FOUND CENTER CARGO STA 1806 TO 1821 LONGERON 46R CORROSION. REPAIR CARRIED OUT AT CENTER CARGO - STA 1806 TO 1821 LONGERON 46R AS PER SRM 53-10-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 45,039 hrs · 6,353 cycles

FOUND CORROSION, LEFT NR 35 BORE. FOUND CORROSION EXCEEDED LIMITS. REPAIR CARRIED OUT IAW FEDEX EA 1-5510-94568.

Part: SPLICE — CRACKED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

FOUND CENTER CARGO, STA 1701 TO 1721 LONGERON 51R SPLICE CRACKED. CRACKED LONGERON SPLICE AT CENTER CARGO STA 1701 TO 1721 LONGERON 51R REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 100) · airframe 45,039 hrs · 6,353 cycles

FOUND LOWER FUSELAGE, CENTER CARGO DOOR CUTOUT FORWARD LOWER AREA FOUND WITH DENTS. TRIMMED OUT AS PER SRM 53-50-00 FIGURE 16 VOLUME I. HFEC INSPECTION CARRIED OUT AS PER NDTSPM PART 06-10-01-001 REV 12 ON THE PERIPHERY OF TRIMMED EDGE AND FOUND NO CRACK EVIDENT. FILLER AND REPAIR DOUBLER FABRICATED AS PER SRM 53-50-00 FIGURE 16 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -7 (UPPER STRINGER). DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 45,039 hrs · 6,353 cycles

BARREL NUT LT NR 7 BORE CORROSION EXCEED LIMIT. COMPLIED WITH FEDEX EA 1-5510-94568

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

CRACK INDICATION FOUND AT END OF STRINGER -13 (UPPER STRINGER). DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -10 (UPPER STRINGER), DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -40 (UPPER STRINGER). DURING HFEC INSPECTION AT LT WING TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -9 (UPPER STRINGER), DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. CLIP FABRICATED AND REPLACED AS PER FEDEX EA 1-5720-94574.

Part: NONE — NONE (ZONE 300) · airframe 45,039 hrs · 6,353 cycles

EMPENNAGE: BARREL NUT RT NR 26 BORE, FOUND WITH EXISTING 2-STEP. BORE EVALUATED AND FOUND WITHIN LIMIT AS PER FEDEX EO 1-5510-7-5000 D1 PT1. BUSHING FABRICATED AND INSTALLED AS PER FEDEX EO 1-5510-7-5000 D1 PT1. N/R, NO M OR D.

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

CRACK INDICATION FOUND AT END OF STRINGER -42 (LOWER STRINGER). DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -12 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT LT WING TANK. CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -9 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT LT WING TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

CRACK INDICATION AT END OF STRINGER -11 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT RIGHT WING TANK. REPAIRED AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -10 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT LT WING TANK. CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION FOUND AT END OF STRINGER -12 (UPPER STRINGER) DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,039 hrs · 6,353 cycles

CRACK INDICATION FOUND AT END OF STRINGER -14 (UPPER STRINGER). DURING HFEC INSPECTION AT RIGHT WING TANK. REPAIRED AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -13 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT LHS WING TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,039 hrs · 6,353 cycles

FOUND CRACK INDICATION AT END OF STRINGER -50 (LOWER STRINGER). DURING HFEC INSPECTION AT LHS WING TANK. CRACK AT END OF STRINGER 50 TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.