N644FE

Part: PUMP — LEAKING (NR 3 HYD) · airframe 78,961 hrs · 14,177 cycles

LEVEL 2 NR 3 HYD FAIL ON SHORT FINAL, 3.9 GAL LEFT BOTH PUMPS WERE OFF. FOUND NR 3 FWD EDP LEAKING AT PUMP HSG ON ENGINE. R & R NR 3 ENGINE FWD EDP IAW AMM 29-11-20-4-2, SERVICE NR 3 HYD SYS TO PROPER LEVEL IAW AMM 12-13-02-3, DRY MOTORED NR 3 ENGINE IAW JRH, NO LEAK NOTE. NR 3 ENG RAN IAW AND OBSERVED HYD QTY IN GAUGE, NO DROP. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (ZONE 600) · airframe 77,869 hrs · 13,805 cycles

RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6. THREE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SKIN — CRACKED (ZONE 500) · airframe 77,869 hrs · 13,805 cycles

LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6, SIX FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION

Part: FRAME — DENTED (ZONE 200) · airframe 77,869 hrs · 13,805 cycles

MAIN DECK BS 1661, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: FRAME — DENTED (ZONE 200) · airframe 77,869 hrs · 13,805 cycles

MAIN DECK BS 1701, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: FRAME — DENTED (ZONE 200) · airframe 77,869 hrs · 13,805 cycles

MAIN DECK BS 1741, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: FRAME — DENTED (ZONE 200) · airframe 77,869 hrs · 13,805 cycles

MAIN DECK BS 1661, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: FRAME — DENTED (ZONE 200) · airframe 77,869 hrs · 13,805 cycles

MAIN DECK BS 1701, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 77,869 hrs · 13,805 cycles

RT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R RT WING INBD FLAP VANE IAW AMM 27-50-22-4, REV 76.1 CARRIED OUT FLAP VANE ADJUSTMENT TEST IAW AMM 27-50-22-5, REV 76.1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 116.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 77,869 hrs · 13,805 cycles

CABIN - RT BS 1019 X= -8.5 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 1009 TO 1049 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REV 52 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: PITOT LINE — BLOCKED · airframe 77,516 hrs · 13,711 cycles

RTO DUE TO IAS ALERT AT 90 KTS ON CAPTAIN`S SIDE. REPLACED CAPTAINS PITOT TUBE, FOUND BLOCKAGE.

Part: BUSS — MALFUNCTIONED (AC SYS) · airframe 77,358 hrs · 13,665 cycles

ON FINAL, RECEIVED "EMER PWR ON" ALERT. AFTER LANDING, RECYCLED EMERGENCY POWER SWITCH AND CPT DISPLAY UNITS 1,2,3 WENT BLANK/DARK WITH NR 2 DISPLAY RED "X". TRIED TO RECYCLE AGAIN WITH NO CHANGE. DUPICATED SYMPTOMS AT BLOCK-IN. ON ELECTRICAL PAGE, FOUND LT EMERGENCY AC BUSS IN AMBER. PULLED AND RESET LT EMERGENCY AC BUSS CIRCUIT BREAKER, ALL SYMPTOMS WENT AWAY, EPCU R-T-S OK. OK TO CONTINUE.

Part: COMPUTER — FAILED (INSTUMENTS) · airframe 73,260 hrs · 12,448 cycles

ON TAKEOFF F/O AND STBY FLT INSTRUMENTS WERE ERRATIC. FOUND BOTH FCC'S AND ALL 3 IRU'S WITH NUMEROUS FAULTS ON NR2 ADC, REPLACED NR2 ADC IAW AMM 34-16-01-4 CK'S GOOD. WHILE INSPECTING PITOT PROBES FOUND DEBRIS IN THE F/O'S PROBE AND SOME IN THE STANBY PROBE. REPLACED ALL 3 PITOT PROBES AS A PRECAUTION IAW AMM 34-11-01-2, AND PERFORMED A PITOT STATIC SYS LEAK CK ON ALL 3 SYS (CAPT, F/O, AND STANDBY) IAW AMM 34-11-00-2.

Part: DOUBLER — CRACKED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

WHEEL COMPARTMENT LT FWD SIDE SPOILER MIXER ROD CUT-OUT DOUBLER FOUND CRACK. R & R AS SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CHAFED (RT WING) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E LOWER SKIN FOUND WITH CHAFE MARKS WHERE PYLON NR1- TO -WING FAIRING CONTACTS. CHAFED SKIN REMOVED AS PER SRM 51-33-01 AND SRM 51-35-01 REV 46. FABRICATED SKIN AS PER DWG ARB2363 AND INSTALLED AS PER SRM 51-33-01 AND MD-11 SRM51-35-01 REV 46. REWORK AREA PROTECTED & PAINTED AS PER SRM 51-21-01 REV 46. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SKIN — CHAFED (LT WING) · airframe 73,182 hrs · 12,414 cycles

LEFT WING FIXED L/E LOWER SKIN FOUND WITH CHAFE MARKS WHERE PYLON-TO-WING CONTACTS. REFER TO SNRM N01217: LT WING FIXED L/E SKIN CHAFED. R & R SRM 51-33-01, REV 46 AND SRM 51-35-01, REV 46 AND DAC DWG ARB2363. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: RIB — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT NR 16 SLAT TRACK INBOARD SUPPORT BRACKET FOUND CRACKED RIB REMOVED AS PER SRM 51-33-01 & 51- 35-01 REV 46. FABRICATED RIB AS PER DWG ARB2850 REV G & INSTALLED AS PER SRM 51-33-01 & 51-35-01 REV 46. REPAIR AREA PROTECTED AS PER SRM 51-21-01 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112

Part: LONGERON — CORRODED (FUSELAGE) · airframe 73,182 hrs · 12,414 cycles

CENTER ACCESSORY COMPARTMENT - STA 6-70 TO STA 6-90, LONGERON NR 49R CORRODED CENTER ACCESSORY COMPARTMENT - CORRODED LONGERON NR 49R CUT-OUT AT STA 6-90 IAW SRM 53-00-05, REV 46, REPAIR 1. HFEC INSP CARRIED OUT IAW NDT SPM, REV 13, PART 6-10-01-001 FOUND NO CRACK EVIDENT. SECTIONAL LONGERON AND SPLICE FABRICATED IAW SRM 53-00-05, REV 46. REPAIR PARTS FASTENER HOLES TRANSFERRED, TREATED AND PAINTED. REPAIR PARTS INSTALLED IAW SRM 53-00-05, REV 46, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (BS 1651) · corrosion level 2 · airframe 73,182 hrs · 12,414 cycles

CENTER CARGO COMPARTMENT BILGE AREA STA 1651, LONGERON 47R, FOUND CORROSION ACCOMPLISHED EA ED E.A. 1-5310-149713 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 73,182 hrs · 12,414 cycles

CRACK INDICATION FOUND ON THE LOWER VERTICAL STABILIZER LEFT HAND UPPER FORWARD FLANGES OF THE REAR SPAR CAP. ACCOMPLISHED E.A.1-5530-149805, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: LONGERON — CORRODED (BS 1853-1863) · airframe 73,182 hrs · 12,414 cycles

LOWER AFT CARGO STA 1853 TO STA 1863, LONGERON 48R FOUND CORRODED. CORROSION REMOVED IAW SRM 51-31-01, REV 46. FOUND EXCEEDED LIMITS IAW SRM 53-00-00, REV 46, FIG 205. NEW SPLICE CHANNEL FABRICATED IAW DWG AGA7438 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SUPPORT BRACKET — CRACKED (NR 16 SLAT TRACK) · airframe 73,182 hrs · 12,414 cycles

RIGHT WING FIXED L/E COMPARTMENT NR 16 SLAT TRACK INBD SUPPORT BRACKET FOUND CRACKED. RT WING L/E COMPT NR 16 SLAT TRACK INBD SUPPORT RIB REMOVED IAW SRM 51-33-01 & 51-35-01, REV 46. FABRICATED RIB IAW DWG ARB2850, REV G AND INSTALLED IAW SRM 51-33-01 & 51-35-01, REV 46. REPAIR AREA REPROTECTED IAW SRM 51-21-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-113 TO 1541, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF CORROSION IAW SRM 52-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1581 TO 1601, X = 76.5 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201, NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46 , FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-93 TO 5-113, X =7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112

Part: SEAT TRACK — CORRODED (BS 1541-1561) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1541 TO 1561, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK TRIMMED- OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIGURE 201, AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-113 TO 1541, X =10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-53 TO 5-73, X = 10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. DAMAGED SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-113 TO 1541, X =7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF IAW SRM 52-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1561 TO 1661, X = 7.0 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. TRIMMED OFF AS PER SRM 53-00-52 REV 46, FIGURE 201. NEW SET TRACK REPAIR SECTION AND SPLICE FABRICATED AS SRM PER 53-00-52 REV 46, FIGURE 201 AND INSTALLED AS PER SRM 51-31-01 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: FLOOR PANEL — WORN (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-32 TO 5-53, X =-74 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND ELONGATED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1561 TO 1661, X = -7.0 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. ACCOMPLISHED "EA 1-5310-142539, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1561 TO 1581, X = 76.5 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201 NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46 , FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: ACCESS PANEL — WORN (NR 2 PYLON) · airframe 73,182 hrs · 12,414 cycles

NR 2 PYLON ACCESS PANEL 475GR FOUND ONE (1) EACH WORN MOUNTING HOLE. ACCOMPLISHED EA 1-5480-142549, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: STOP FITTING — CRACKED (LT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

LT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED, R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2 FOUND SATISFACTORY.

Part: STOP FITTING — CRACKED (RT TE FLAP) · airframe 73,182 hrs · 12,414 cycles

RT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED. R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: BULKHEAD — CRACKED (BS 2033 BULKHEAD) · airframe 73,182 hrs · 12,414 cycles

AFT FUSELAGE COMPARTMENT - STA 2033 BULKHEAD, LT SIDE FORGING FOUND CRACK LINE NEAR TO UPPER CEILING CUT-OUT. ACCOMPLISHED EA 1-5310-149742, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 73,182 hrs · 12,414 cycles

CRACK INDICATION FOUND ON THE LWR VERTICAL STAB ON THE RT UPPER FWD FLANGE OF THE REAR SPAR CAP FITTING. ACCOMPLISHED EA 1-5530-149805, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: CHANNEL — DAMAGED (BS 1711-1831) · airframe 73,182 hrs · 12,414 cycles

LOWER CTR CARGO COMPARTMENT BOTH AFT STA 1711 AND STA 1831, X= 38 AND X= -38 SHUTTLE BEAM LT AND RT CHAIN PROTECTIVE HATS BROKEN LOWER CTR CARGO COMPARTMENT AT STA 1711-STA 1831, X=38 AND X= -38, BOTH AFT SHUTTLE BEAM LT AND RT CHAIN PROTECTIVE HATS REMOVED, FABRICATED AND INSTALLED IAW EA 1-2550-179739, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CHAFED (RT WING) · airframe 73,182 hrs · 12,414 cycles

RT WING FIXED L/E OTBD EXTERIOR SURFACE ABOVE PYLON FOUND CHAFED SKIN. REMOVED IAW SRM 51-33-01 AND SRM 51-35-01, REV 46. NEW SKIN FABRICATED IAW DWG ARB236 AND INSTALLED IAW SRM 51-33-01 AND SRM 51-35-01, REV 46. REWORK AREA REPROTECTED & PAINTED IAW SRM 51-21-01, REV 46. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CHAFED (LT WING) · airframe 73,182 hrs · 12,414 cycles

LT WING FIXED L/E OTBD EXTERIOR SURFACE ABOVE PYLON FOUND CHAFED SKIN. REMOVED AS PER SRM 51-33-01 REV 46 AND SRM 51-35-01 REV 46. FABRICATED AS PER DWG ARB2363 AND INSTALLED AS PER SRM 51-33-01 REV 46 AND SRM 51-35-01 REV 46. REPAIR AREA PAINTED AS PER SRM 51-21-01 REV 46. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100 REV 112.

Part: STRINGER — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RT WING UPPER AUX TANK AT STA XCW 17 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: STRINGER — CRACKED (ZONE 500) · airframe 73,182 hrs · 12,414 cycles

LT WING UPPER AUX TANK AT STA XCW 46.500 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 457 AND 495, X = -29 SEAT TRACK UPPER AND LOWER FLANGE FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SUPPORT BRACKET — CRACKED (SLAT TRACK) · airframe 73,182 hrs · 12,414 cycles

LT WING L/E COMPARTMENT NR 16 SLAT TRACK INBD SUPPORT BRACKET FOUND CRACKED. SUPPORT REMOVED IAW SRM 51-33-01 & 51-35-01, REV 46. FABRICATED IAW DWG ARB2850, REV G, AND INSTALLED IAW SRM 51-33-01, REV 46 AND SRM 51-35-01, REV 46. REPAIR AREA REPROTECTED IAW SRM 51-21-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: STRINGER — CRACKED (ZONE 500) · airframe 73,182 hrs · 12,414 cycles

RT WING UPPER AUX TANK AT STA XCW 46.500 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 1.75 INCH CRACKED. STOP DRILLED IAW SRM 57-40-01 REV 46, REPAIR 5, FIG 201. REPAIR DOUBLER FABRICATED IAW SRM 57-40-01, REV 46, REPAIR 5, FIG 201 AND INSTALLED IAW SRM 51-33-01, REV 46. REPAIR AREA REPROTECTED IAW SRM 51-21-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (ZONE 500) · airframe 73,182 hrs · 12,414 cycles

LT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 0.375 INCH AND 0.3125 INCH CRACK. STOP DRILLED IAW SRM 57-40-01, REV 46, REPAIR 5 FIG 201. REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 57-40-01, REV 46, REPAIR 5, FIG 201 AND SRM 51-35-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 1661-1669) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1661 TO STA 1669, X = 73 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. FABRICATED REPAIR SECTION AND SPLICE IAW SRM 53-00-52 REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 73,182 hrs · 12,414 cycles

LOWER CARGO DOOR JAMB STA 160 - STA 1741, X = -147 UPPER SIDE FOUND WITH CORROSION. ACCOMPLISHED EA 1-5310-149741, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

LOWER CTR CARGO DOOR JAMB, STA 1601 - STA 1741, X = -147 LOWER SIDE FOUND WITH CORROSION. ACCOMPLISHED EA 1-5310-149741. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN ATV STA 1561 - 1576, X = 27.5 SEAT TRACK UPPER FLANGE FOUND CORRODED. DAMAGED SEAT TRACK TRIMMED OFF IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION AND SPLICES FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1675 TO STA 1686, X = 107 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK SECTION AND SPLICES FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,182 hrs · 12,414 cycles

LT WING INBD FLAP OTBD HINGE (FLAP SIDE), PIVOT INBD HOLE FOUND CORRODED FLAP HINGE. REWORKED AND FOUND EXCEEDED LIMIT PER CMM 57-52-03 REV 69. ACCOMPLISHED E.A 1-5750-149737, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112

Part: SKIN — CORRODED (BS 2163) · airframe 73,182 hrs · 12,414 cycles

RT ACCESSORY COMPARTMENT EXTERNAL SURFACE AFT OF HORIZONTAL STABILIZER CUT-OUT AT STA 2163 FOUND WITH CORROSION. ACCOMPLISHED EA 1-5330-149813, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 73,182 hrs · 12,414 cycles

LT WING INBD FLAP OTBD HINGE (FLAP SIDE), PIVOT OTBD HOLE FOUND CORRODED FLAP HINGE. REWORKED AND FOUND EXCEEDED LIMIT PER CMM 57-52-03 REV 69. ACCOMPLISHED E.A. 1-5750-149737, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: PIVOT ASSY — CORRODED (RT WING TE FLAPS) · airframe 73,182 hrs · 12,414 cycles

RT WING OTBD FLAP INBD HINGE (FLAP SIDE) XW486.403, PIVOT BOARD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-04, REV 69. ACCOMPLISHED EA 1-5750-149728. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

RT WING INBD FLAP OTBD HINGE (FLAP SIDE) XW254.000, PIVOT INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 69. ACCOMPLISHED EA 1-5750-149736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

RT WING OTBD FLAP INBD HINGE (FLAP SIDE) STA XW486.403, PIVOT INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-04, REV 69. ACCOMPLISHED EA 1-5750-149728. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 1871) · airframe 73,182 hrs · 12,414 cycles

CABIN STA 1871 X = 8.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLE FOUND CORRODED. DAMAGED SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED WITH THE EXISTING SPLICE IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN SEAT TRACK BETWEEN STA 1853 TO 1887 X =47.5 FOUND CORRODED. TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-73 TO 5-93, X = -10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-53 TO 5-73, X =107 SEAT TRACK FLOOR PANEL ATTACHMENT FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-11 TO 5-32, X = -74 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND ELONGATED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 1541-1561) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1541 TO STA 1561, X =75, SEAT TRACK FLOOR PANEL ATTACHMENT HOLE FOUND CORRODED. SEAT TRACK SECTION TRIMMED OFF IAW SRM 53-00-52, FIG 201, REV 46. FABRICATED REPAIR SECTION AND SPLICE IAW SRM 53-00-52, FIG 201, REV 46 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 1541-1651) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1541 TO 1561 X = -46 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. FABRICATED REPAIR SECTION AND SPLICE IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 1761) · airframe 73,182 hrs · 12,414 cycles

CABIN SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE AT STA 1761, X = 85 FOUND CORRODED. TRIMMED-OFF IAW SRM 51-31-01, REV 46. SEAT TRACK REPAIR SECTION FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 112

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-53 TO 5-73, X =75 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

RT WING INBD FLAP UPPER SKIN AFT SEGMENT INBD UPPER CHORD FOUND WITH APPROX 8.5 INCH CRACK AFTER REMOVING THE SEGMENT FOR ACCESS TEE-FITTING. COMPLIED WITH "EO1-5100-7-5001 A5 PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 1541-1561) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1541 TO STA 1561, X = -7, SEAT TRACK FLOOR PANEL ATTACHMENT HOLES LOWER SURFACE FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. FABRICATED REPAIR SECTION IAW SRM 53-00-52, FIG 201, REV 46 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 5-73 TO STA 5-93, X =7.5 , SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. FABRICATED REPAIR SECTION IAW SRM 53-00-52, FIG 201, REV 46 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 1541) · airframe 73,182 hrs · 12,414 cycles

CABIN BETWEEN STA 1541 TO STA 156, X = 10, SEAT TRACK FLOOR PANEL ATTACHMENT HOLE FOUND CORRODED. TRIMMED-OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SET TRACK REPAIR SECTION AND SPLICE FABRICATED SRM IAW 53-00-52, REV 46, FIG 201 AND INSTALLED IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

RT WING OTBD FLAP INBD FORWARD HINGE AT STA XW 486.403 BARREL NUT FITTING SURFACE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149729 WINGS-FLT SURFACES-RT WING FWD OTBD FLAP INBD HINGE-(WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

RT WING, STA XW 486.403 OTBD FLAP INBD FWD HINGE ACTUATOR INBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149729. WINGS- FLIGHT SURFACES- RT WING FWD OTBD FLAP INBD HINGE - (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: STRINGER — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RIGHT WING, LOWER WING TANK S-10 STRINGER END FOUND WITH APPROX 4 INCH CRACK. ACCOMPLISHED EA 1-5720-149715, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

RT WING STA XW 638.3059 OTBD FLAP, OTBD FWD HINGE BARREL NUT FITTING SURFACE FOUND CORRODED. RT WING OTBD FLAP OTBD FWD HINGE BARREL NUT FITTING SURFACE REWORK IAW CMM 20-11-02, REV 69 FOUND WITHIN LIMITS IAW DWG ARC0503, SHT 2, REV BG AND CMM 57-44-09, FIG 601, REV 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

RT WING STA XW 486.403 OTBD FLAP INBD FWD HINGE ACTUATOR OTBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149729. WINGS - FLIGHT SURFACES - RT WING FWD OTBD FLAP INBD HINGE - (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: STRINGER — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RIGHT LOWER WING - XORS 737 TANKS S-40 STRINGER END FOUND WITH APPROX 1.5 INCH CRACKED. ACCOMPLISHED EA 1-5720-149722. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

STA 6-70- TO STA 6-80, LONGERON 49L CORRODED. CUT OUT DAMAGED AREA IAW SRM 53-00-05, REV 46, REPAIR 1. HFEC INSP CARRIED-OUT IAW NDT SPM REV 13, PART 6-10-001 FOUND NO CRACK EVIDENT. SECTIONAL LONGERON AND SPLICES FABRICATED AND INSTALLED IAW SRM 53-00-05, REV 46, REPAIR 1. REWORK AREA REPROTECTED AND PAINTED IAW SRM 51-21-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (BS 1541 L42R) · airframe 73,182 hrs · 12,414 cycles

CTR CARGO COMPARTMENT RT TUNNEL AREA, STA 1541, LONGERON 42R, FOUND WITH CORROSION. ACCOMPLISHED EA 1-5310-149707. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CRACKED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

LWR CTR CARGO UNDERFLOOR AREA STA 5-100 TO STA 5-110, LONGERON 45R FOUND CRACKED. ACCOMPLISHED EA 1-5310-142547, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (ZONE 500) · airframe 73,182 hrs · 12,414 cycles

LT WING L/E COMPARTMENT AT STA XORS 588 FOUND FINGER DOUBLER WITH APPROX (3) INCH CRACKED LT WING L/E COMPT STA XORS 558 FINGER DOUBLER TRIMMED IAW SRM 57-40-02, REV 46, REPAIR 9, FIG 203. HFEC INSP CARRIED OUT ON REPAIR AREA FOUND NO CRACK EVIDENT. DOUBLER, ANGLE AND FILLER FABRICATED, AND INSTALLED IAW SRM 57-40-02, REV 46, REPAIR 9, FIG 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

STA 6-70, LONGERON 47L FOUND CORRODED. CUTOUT DAMAGE IAW SRM 53-00-05, REPAIR 1, REV 46. HFEC C/OUT FOUND NO CRACK EVIDENT. FABRICATED LONGERON SECTION & SPLICE & INSTALLED IAW SRM 53-00-05, REPAIR 1, REV 46. REWORK AREA REPROTECTED & PAINTED IAW SRM 51-21-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

CTR ACCESSORY COMPARTMENT: STA 6-70 TO 6-80, LONGERON 51L CORRODED. TRIMMED OUT IAW SRM 53-00-05, REV 46, REPAIR 1. HFEC INSP CARRIED OUT FOUND NO CRACK EVIDENT. LONGERON SECTION AND SPLICE FABRICATED AND INSTALLED IAW SRM 53-00-05, REV 46, REPAIR 1. REWORK AREA REPROTECTED AND PAINTED IAW SRM 51-21-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

CTR CARGO COMPARTMENT LT TUNNEL AREA STA 1741, LONGERON 36L, LONGITUDINAL SPLICE FOUND WITH CORROSION. ACCOMPLISHED EA 1-5310-149745. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

CTR CARGO COMPARTMENT BILGE AREA STA 1641 TO STA 1661, LONGERON 51L FOUND WITH CORROSION AND SUSPECTED CRACKED. ACCOMPLISHED EA 1-5310-149824, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (ZONE 500) · airframe 73,182 hrs · 12,414 cycles

LT WING L/E COMPT AT STA XORS 530 FOUND FINGER DOUBLER WITH APPROX 2 INCH CRACK. CRACKED AT LT WING L/E COMPT AT APPROX STA XORS 530 REPAIRED IAW SRM 57-40-02, REV 46, REPAIR 9, FIG 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (BS 1954-1964) · airframe 73,182 hrs · 12,414 cycles

AFTER CARGO STA 1954 TO STA 1964, LONGERON 36R FOUND CORRODED. REPAIR ACCOMPLISHED IAW EA 1-5310-142544, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 73,182 hrs · 12,414 cycles

LT WING OTBD FLAP, INBD FWD HINGE BARREL NUT FITTING SURFACE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149730, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

LT WING OTBD FLAP, OTBD FWD HINGE ACTUATOR INBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149725, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: STRUCTURE — CORRODED (LT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

LT WING OTBD FLAP, INBD FWD HINGE ACTUATOR OTBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149730, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,182 hrs · 12,414 cycles

LOWER CTR CARGO UNDER-FLOOR AREA STA 5-118, LONGERON 48L FOUND WITH CORROSION. ACCOMPLISHED EA 1-5310-142547. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

LT WING OTBD FLAP, INBD FWD HINGE ACTUATOR, INBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149730. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (BS 1976 L36R) · airframe 73,182 hrs · 12,414 cycles

LOWER AFT CARGO WASTE TANK COMPARTMENT BS 1976 LONGERON 36R FOUND CORRODED. ACCOMPLISHED E.A. 1-5310-142544, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112

Part: LONGERON — CORRODED (BS 1535-1545) · airframe 73,182 hrs · 12,414 cycles

LOWER CTR CARGO UNDER-FLOOR AREA STA 1535 TO STA 1545, LONGERON 48L FOUND WITH CORROSION. ACCOMPLISHED EA 1-5310-142547, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

LT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT SURFACE FOUND CORRODED FLAP HINGE ARC0503-403. XW638.3059. ACCOMPLISHED EA 1-5750-149725. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

LT WING OTBD FLAP OTBD FWD HINGE ACTUATOR INBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149725. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

LT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT FITTING. SURFACE FOUND CORRODED FLAP HINGE ARC0503-403, XW638.3059. REWORKED AS PER CMM 20-11-02 REV 69. FOUND WITHIN LIMITS PER DWG ARC0503 SHEET 2, REV BG AND CMM 57-44-09 REV 15, FIG 601 REWORK LIMITS. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E COMPT ACCESS PANEL NR 626DB SUPPORT CUT-OUT FOUND WITH APPROX (2) IN CRACK. L/E DOUBLER STRUCTURE ARB7575-2, XOS 906. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-40-03 REPAIR 1 FIGURE 201, SRM 51-33-01 AND SRM SRM 35-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SKIN — CRACKED (ZONE 500) · airframe 73,182 hrs · 12,414 cycles

LT WING L/E LOWER ACCESS PANEL, NR 526DB, SUPPORT CUT-OUT FOUND WITH APPROX (2) IN CRACKED L/E DOUBLER, STRUCTURE, ARB7575-2, XOS 906. REPAIR DOUBLER FABRICATED AND INSTALLED PER SRM 57-40-03 REPAIR 1, FIGURE 201, SRM 51-33-01 AND SRM 51-35-01 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: FINGER DOUBLER — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E COMP AT STA XORS 480 FOUND FINGER DOUBLER WITH APPROX (6) IN CRACK L/E SKIN ARB7574-2, XOS 580. REPAIRED IAW SRM 57-40-02, REPAIR 9, FIG 203 REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: FINGER DOUBLER — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E COMP AT STA XORS 510 FOUND FINGER DOUBLER WITH APPROX (5) INCH CRACK L/E SKIN ARB7574-2, XOS 620. TRIMMED IAW SRM 57-40-02, REPAIR 9, FIG 203, REV 46. HFEC C/OUT ON REPAIR AREA FOUND NO CRACK EVIDENT. FABRICATED DOUBLER, ANGLE AND FILLER; AND INSTALLED IAW SRM 57-40-02, REPAIR 9, FIG 203, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: FINGER DOUBLER — CRACKED (RT WING SKIN) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E COMP AT STA XORS 536 FOUND FINGER DOUBLER WITH APPROX TEN (10) INCH CRACK L/E SKIN ARB7574-2, XOS 640. TRIMMED IAW SRM 57-40-02, REPAIR 9, FIG 203 REV 46. HFEC CARRIED OUT ON REPAIR AREA FOUND NO CRACK EVIDENT. FABRICATED DOUBLER, ANGLE AND FILLER; INSTALLED IAW SRM 57-40-02, REV 46. REPAIR 9, FIG 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: FINGER DOUBLER — CRACKED (RT WING SKIN) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E COMP AT STA XORS 560 FOUND FINGER DOUBLER WITH APPROX TEN (10) IN CRACK L/E SKIN. REPAIRED IAW SRM 57-40-02 REV 46, REPAIR 9 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112

Part: FINGER DOUBLER — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E COMP AT STA XORS 480 FOUND FINGER DOUBLER WITH APPROX (6) IN CRACK L/E SKIN, ARB7574-2, XOS 580. REPAIRED IAW SRM 57-40-02, REPAIR 9, FIG 203 REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 420-457) · airframe 73,182 hrs · 12,414 cycles

CABIN RT NR 1 DOOR STA 420 TO 457, X = -85 SEAT TRACK FOUND CORRODED. R & R IAW SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E NR 14 SLAT TRACK LOWER CUT-OUT FOUND WITH APPROX 1 IN CRACK L/E STRUCTURE. REPAIRED IAW SRM 57-40-02 REV 46, REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 112.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RT WING L/E COMPARTMENT ACCESS PANEL NR 627AB SUPPORT CUT-OUT. FOUND WITH APPROX 2 IN CRACK. SUPPORT CUT-OUT REPAIRED IAW SRM 57-40-01, REV 46, REPAIR 9, FIG 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — CORRODED (BS 1644-1654) · airframe 73,182 hrs · 12,414 cycles

LOWER CENTER CARGO COMPARTMENT STA 1644 TO STA 1654, LONGERON 47R FOUND WITH CORROSION AND SUSPECTED CRACKED. AFA0168-1 ACCOMPLISHED EA 1-5310-149713, FUSELAGE MAINFRAME LOWER CENTER CARGO COMPARTMENT STA 1681 TO STA 1631 LONGERON L-47 RT CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — CORRODED (BS 1321-1341) · airframe 73,182 hrs · 12,414 cycles

CABIN FLOOR LT SEAT TRACK AT STA 1321-1341, X = 8.5 CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 73,182 hrs · 12,414 cycles

RIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR INBOARD HOLE FOUND CORRODED REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 REV 69. ORIGINAL DIAMETER = 1.228 INCH, FINAL DIAMETER = 1.250 INCH, MAX ALLOW DIAMETER = 1.220 INCH. ACCOMPLISHED E.A. 1-5750-149729. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: LONGERON — CORRODED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

LOWER CARGO COMPARTMENT - FWD CARGO BILGE AREA BETWEEN FRAME STA 6.70 TO STA 6.50 RT SIDE LONGERON 49 FOUND WITH CORROSION. CUT- OUT SRM 51-31-01, REV 46 AND SRM 53-0-05, REV 46, REPAIR 1. FABRICATED LONGERON, REPAIR SPLICE AND FASTENERS INSTALLED IAW SRM 53-0-05, REV 46, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 73,182 hrs · 12,414 cycles

LT LOWER FUSELAGE UNDERWING EXTERIOR STRUCTURE AROUND STA 1289 FOUND WITH APPROX 2 INCH CRACK. ACCOMPLISHED EA 1-5310-142536. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 73,182 hrs · 12,414 cycles

REPAIR FOUND AT RT INBD FLAP LOWER SKIN. FOUND NOT IAW APPROVED DATA. REPAIR REMOVED AND NEW REPAIR ACCCOMPLISHED PER SRM 57-50-01 REV 46, REPAIR 1 FIG 201. COMPLIED WITH E.O. 1-5100-7-5001 A5 PART 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SKIN — MISREPAIRED (NR 4 SLAT) · airframe 73,182 hrs · 12,414 cycles

AGING ACFT - EXISTING REPAIR FOUND AT LT NR4 SLAT INNER SKIN EXISTING REPAIR AT LT WING 4 SLAT INBD SKIN EVALUATED AND FOUND NOT IAW ANY APPROVED DATA. NR4 SLAT R & R IAW AMM 27-80-30-4, REV 69.2. COMPLIED WITH "EO 1-5100-7-5001 A5 PART 1, REPAIR CLASSIFIED AS MINOR, IAW GMM 6-2-100, REV 112.

Part: SKIN — MISREPAIRED (MAIN PAX) · airframe 73,182 hrs · 12,414 cycles

REPAIR FOUND AT NR 4 PASSENGER DOOR RT UPPER AFT EDGE. FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY APPROVED DATA. REPAIR REMOVED & NEW REPAIR ACCOMPLISHED IAW SRM 52-10-01, FIG 201, REPAIR 3, REV 46. COMPLIED WITH "EO 1-5100-7-5001 A5 PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.