N39081

Part: DUCT — BLOWN (NR 1 ENGINE) · airframe 80,088 hrs · 24,786 cycles

THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING TAKEOFF FROM IAH. THE NR 1 NACELLE TEMP WENT TO 300 DEGREES AND THE NR 1 THRUST REVERSER VALVE OPEN LIGHT CAME ON. POWER WAS REDUCED TO JUST ABOVE IDLE AND THE FIRE WARNING LIGHT EXTINGUISHED. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED SAFELY. MAINTENANCE FOUND NR 1 ENGINE PNEUMATIC DUCT BLOWN ON LT SIDE OF ENGINE WITH DAMAGE TO THE NR 1 ENGINE I/B THRUST REVERSER HALF. THE PNEUMATIC DUCT WAS REPLACED. THE NR 1 ENGINE I/B THRUST REVERSER HALF WAS REMOVED AND REPLACED IAW MM 78-32-11. IN ADDITION, THE NR 1 ENGINE OVER PRESSURE S/O VALVE WAS REPLACED IAW MM 78-31-09.

Part: SPAR CAP — CORRODED (CENTER WING) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND CORROSION ON CENTER WING FORWARD LOWER SPAR CAP AT XCW 0.0. THE SPAR CAP WAS REPAIRED IAW ECRA 5311-01104 AND FLS DRAWING 90-53-1071.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND SHEAR CLIPS CORRODED AT FRAME STA 1903 FROM L48R-49R, 50R-51R, AND 50L-52L. THE SHEAR CLIPS WERE REMOVED AND REPLACED IAW SRM 53-30-00.

Part: LONGERON — CORRODED (CARGO BAY) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND LONGERON 48L CORRODED AROUND FASTENERS IN CENTER CARGO BAY AT STA 1521. THE END CAP WAS REMOVED AND A NEW END CAP WAS INSTALLED IAW SRM 51-00-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND STIFFENER ANGLES CORRODED AT FRAME STA 1997 ABOVE L49L TO L49R. THE STIFFENER ANGLES WERE REPLACED IAW SRM 51-00-01.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND SHEAR CLIPS CORRODED AT FRAME STA 1941 L49R - 52L, STA 1959 L50L - L52L, AND STA 1975 L50L - L50R. THE SHEAR CLIPS WERE REPLACED IAW SRM 53-30-00, 53-00-01, AND 51-21-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND G1A -G5 LT SUPPORT BEAM CORRODED AT STA 800. THE SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01.

Part: BEAM — CORRODED (FUSELAGE) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND FLOOR SUPPORT BEAM BENEATH LAV D CORRODED AT STA 836 - 880. THE INNER SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01.

Part: FLOOR SUPPORT — CORRODED (CAIBN) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 392 ADJACENT TO R-1 DOOR. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 53-00-00 AND GMM 10-900-01.

Part: FLOOR SUPPORT — CORRODED (GALLEY) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND FLOOR SUPPORT ADJACENT TO GALLEY G-1 CORRODED. REPAIRED IAW SRM 53-00-00 AND GMM 10-900-01.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND O/B FLOORBEAM CORRODED AT GALLEY 2. THE FLOORBEAM WAS REPLACED IAW SRM 53-00-00 AND GMM 10-900-01.

Part: BEAM — CORRODED (FUSELAGE) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND RT SUPPORT BEAM CORRODED AT STA 840. THE BEAM WAS REPLACED IAW SRM 53-70-00 AND GMM 10-900-01.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 79,573 hrs · 24,709 cycles

INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT STA 836 AND 804, X42 TO X-42. THE CORRODED SECTIONS OF FLOOR SUPPORT BEAM WERE REPLACED IAW GMM 10-900-01.

Part: ENGINE — FAILED (NUMBER ONE) · airframe 78,881 hrs · 24,602 cycles

NUMBER ONE ENGINE FAILED (UNCONTAINED) AT TAKEOFF. ENGINE BEING REMOVED AND FORWARDED TO SHOP FOR FAILURE ANALYSIS. THIS SDR TO REMAIN OPEN PENDING TEARDOWN AND ANALYSIS.

Part: WIRE — DAMAGED (LAVATORY)

THE EXIT IDENTIFIER AT LAV C FAILED TO ILLUMINATE. INSPECTION FOUND CABLES DAMAGED. THE CABLES WERE REPAIRED AND OPERATION CHECKED IAW MM 33-50-00.

Part: WIRE — CHAFED (L-3 DOOR)

INSPECTION FOUND THE EMERGENCY PATH LIGHTING SYSTEM BATTERY POWER SUPPLY BLOWING FUSES AT L-3 DOOR. MAINTENANCE FOUND CHAFED WIRE AT SIDEWALL FORWARD OF LT OVERWING EXIT. REPAIRED IAW MM 20-00-00 AND OPERATION CHECKED GOOD IAW MM 33-50-00.

Part: CHARGER — INOP (L-2 DOOR)

INSPECTION FOUND L-2 DOOR EMERGENCY LIGHTS BATTERY CHARGER UNIT BATTERY DISCONNECT PLUG CABLE BROKEN AT PLUG. THE CHARGER UNIT WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.

Part: SKIN — CORRODED (LT LE SLAT)

INSPECTION FOUND LT WING NR 8 SLAT CORRODED ON LEADING EDGE AT TRACK. THE NR 8 SLAT WAS REMOVED AND REPLACED IAW MM 27-80-01.

Part: END CAP — CORRODED (BS 889)

INSPECTION FOUND FORWARD CARGO BAY STRINGER 44R END CAP CORRODED AT STA 889. THE END CAP WAS REPAIRED IAW SRM 53-30-00.

Part: FLOOR — DELAMINATED (CABIN)

INSPECTION FOUND FLOOR PANEL 283KF DELAMINATED WITH CORRODED FERRULES. A NEW FLOOR PANEL WAS INSTALLED IAW GMM 10-100-01.

Part: SUPPORT — CORRODED (BS 1838-1873)

INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED AT STA Y= 1838-1873, X= 3R. THE CORRODED SECTION OF SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-100-01.

Part: SUPPORT — CORRODED (BS 1990-1996)

INSPECTION FOUND THE LONGITUDINAL FLOOR SUPPORT BEAM CORRODED AT STA Y= 1990-1996, X= 22R. REPAIRED IAW SRM 53-70-00, FIGURE 13 AND 14.

Part: SUPPORT — CORRODED (BS 1887)

INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT Y= 1887, X= 3R TO 70R AND AT Y= 1887, X= 3L TO 70L, J CAPPING STRIP. THE CORRODED SECTIONS OF CAPPING STRIP WERE REMOVED. NEW SECTIONS OF CAPPING STRIP WERE INSTALLED IAW GMM 10-100-01.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION FOUND EMERGENCY FLASHLIGHT IN CABIN INOPERATIVE. THE FLASHLIGHT WAS REMOVED AND REPLACED.

Part: FILTER CASE — BROKEN (NR 3 HYD SYST)

THE NR 3 HYDRAULIC SYSTEM LOST FLUID ACCOMPANIED BY ILLUMINATION OF THE HYDRAULIC SYSTEM ELEVATOR OFF LIGHT WHILE EN ROUTE FROM FCO TO EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS DIVERTED TO CDG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE FILTER CASE ASSEMBLY BROKEN. THE FILTER CASE ASSEMBLY WAS REMOVED AND REPLACED. THE NR 3 HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD.

Part: ACTUATOR — INOPERATIVE (LT MLG)

THE LT MLG WOULD NOT RETRACT AFTER TAKEOFF FROM LGW. APPROPRIATE CHECKLISTS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT GEAR DOOR ACTUATOR SLOW TO OPERATE AND THE GEAR CONTACTED THE OUTER DOOR. THE LT MLG ACTUATOR WAS REPLACED. THE OUTER GEAR DOOR WAS ALSO REPLACED. A GEAR SWING WAS PERFORMED AND OPERATION CHECKED GOOD.

Part: BULKHEAD — BUCKLED (BS 2163)

INSPECTION FOUND TAIL CONE BULKHEAD AT FS 2163, STRINGER 51L BUCKLED. THE BUCKLED AREA WAS REMOVED AND A REPAIR WAS INSTALLED USING DOUBLER AND FILLER IAW SRM 53-00-1 FIGURE 4 SHEET 2.

Part: FLOOR PANEL — CORRODED (CABIN)

INSPECTION FOUND FLOOR PANELS 291AF, 291EF, 292BF, 292DF, 292EF, 293BF, 293CF, AND 293DF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-21-00, AND 53-60-00.

Part: FLOOR PANEL — CORRODED (CABIN)

INSPECTION FOUND FLOOR PANELS 241EF, 241FF, 242BF, 242FF, AND 261BF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-60-00, AND 53-21-00.

Part: FLOORBOARD — CORRODED (PNL 227AF)

INSPECTION FOUND FLOORBOARD PANEL 227AF CORRODED. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-60-00.

Part: SUPPORT — CORRODED (BS 459-501)

INSPECTION FOUND FLOOR SUPPORT AND MOUNT FITTING CORRODED AT STA 459 TO 501, RBL 14. THE MOUNT FITTING WAS REMOVED AND REPLACED IAW SRM 51-31-01. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01 AND 53-00-01.

Part: SKIN — CORRODED (LT TE FLAP)

INSPECTION FOUND LT WING INBOARD FLAP CORRODED. THE LT INBOARD TRAILING EDGE FLAP SKIN WAS REMOVED AND NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 57-52-01.

Part: SUPPORT — CORRODED (BS 475)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 475, RBL 38. THE UPPER FLANGE OF FLOOR SUPPORT WAS TRIMMED OFF AND REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 5310-03505.

Part: SKIN — DENTED (BS 1841)

INSPECTION FOUND A DENT AND CREASE IN LT AFT FUSELAGE SKIN AT STA 1841 BETWEEN LONGERON 40L AND 41L. THE DENT AND CREASE WERE REWORKED IAW SRM 53-20-00, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-20-00 AND ECRA 5330-02532.

Part: SKIN — CORRODED (BS 1501)

INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1501, BL 0. THE CORROSION WAS REMOVED IAW SRM 51-21-01, A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02524.

Part: WEB — ELONGATED HOLES (NR 3 PYLON)

INSPECTION FOUND SEVERAL ELONGATED FASTENER HOLES IN NR 3 PYLON FRONT SPAR WEB. THE WEB WAS REMOVED, A NEW WEB WAS FABRICATED AND INSTALLED IAW EA 5410-01109 AND SRM 51-30-00.

Part: ANGLE — CORRODED (BS 595)

INSPECTION ATTACH CHANNEL CORRODED AT STA 595, LONGERON 45L. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 53-12-01.

Part: FLOOR — CRACKED (COCKPIT)

INSPECTION FOUND AN 8 INCH CRACK AT LIGHTENING HOLE OF FLOOR UNDER FLIGHT ENGINEER'S SEAT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-11-01 AND 51-31-01.

Part: SUPPORT — CORRODED (BS 1901-2007)

INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1901 TO 2007, LBL 57. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-31-01, AND 51-21-01.

Part: ANGLE — CORRODED (BS 1781)

INSPECTION FOUND CENTER CARGO AFT BILGE FORWARD FRAME WEB SUMP PANEL ATTACH ANGLE CORRODED AT STA 1781, RBL 1 TO RBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-31-01, AND 53-15-01.

Part: FLOOR PANEL — CORRODED (CABIN)

INSPECTION FOUND CABIN FLOOR PANELS 231CF, 232AF, 232CF, 233AF, AND 233CF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-60-00, AND 53-21-00.

Part: SKIN — GOUGED (BS 735)

INSPECTION FOUND RT FUSELAGE SKIN GOUGED AT STA 735, LONGERON 28R. THE GOUGED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 53-20-00.

Part: FLOOR PANEL — CORRODED (BS 840-899)

INSPECTION FOUND FLOOR PANEL CORRODED AT STA 840-899, RBL 72. THE PANEL WAS REMOVED AND REPLACED IAW SRM 53-00-01.

Part: WEB — CRACKED (BS 1256)

INSPECTION FOUND A 1.125 INCH CRACK AT CORNER ACCESS HOLE WEB FRAME STA 1256, LONGERON 27R. A 1 INCH CRACK WAS FOUND ON LT SIDE AS WELL, AT LONGERON 27L. THE CRACKS WERE STOP DRILLED, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 4, 53-14-01, AND 51-31-01.

Part: SUPPORT — CORRODED (BS 1884)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1884, LBL 5 TO 21. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-31-01, A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01 AND 51-31-01.

Part: FRAME — CRACKED (BS 1305)

INSPECTION FOUND A .075 INCH CRACK IN FRAME AT FORWARD LOWER CORNER OF ACCESS HOLE WEB, STA 1305, LONGERON 27L. A .5 INCH CRACK WAS FOUND ON THE RT SIDE AT LONGERON 27R. THE CRACKS WERE STOP DRILLED, DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 4, 53-14-01, AND 51-31-01.

Part: SUPPORT — CORRODED (BS 1884)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1884, RBL 4 TO 21. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 53-16-01.

Part: SUPPORT — CORRODED (BS 1884)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1884, LBL 28 TO 33. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01, AND 51-31-01.

Part: SUPPORT — CORRODED (BS 1986)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1986, LBL 30. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-31-01. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01, AND 51-31-01.

Part: SUPPORT — CORRODED (BS 840-899)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 840 TO 899. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-13-01, 51-21-01, AND 51-30-01.

Part: SUPPORT — CORRODED (BS 340-445)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 340 TO 445, RBL 6 TO 19. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-21-01 AND 51-31-01.

Part: SUPPORT — CORRODED (BS 495)

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 495, LBL 30 TO 53 AND RBL 30 TO 54. NEW FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-31-01, ECRA 5310-03475 AND ECRA 5310-03489.

Part: SHEAR TIE — CORRODED (BS 1139)

INSPECTION FOUND SHEAR TIE CORRODED AT STA 1139 BETWEEN L51R AND L52R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 51-10-00.

Part: SUPPORT — CORRODED (BS 1884)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1884, RBL 26 TO 32. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-01, A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01, AND 51-31-01.

Part: ANGLE — CRACKED (WS 373)

INSPECTION FOUND A 2 INCH CRACK IN AFT SIDE INBOARD UPPER CORNER ANGLE AT RT WING STA XW 373. A REPLACEMENT SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-10-00, AND 57-22-01.

Part: SUPPORT — CORRODED (BS 879)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 879 RBL 44. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-31-01.

Part: BRACKET — CRACKED (RUDDER)

INSPECTION FOUND A 5 INCH CRACK IN FORWARD HORIZONTAL BRACKET AT TOP OF RUDDER UNDER PANEL NR 376 WL. THE BRACKET WAS REMOVED IAW SRM 51-30-01. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-38-01, 51-21-01, 51-40-00, AND 51-31-01.

Part: SUPPORT — CORRODED (BS 459-501)

INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT FS 459 TO 501, RBL 14. THE FLOOR SUPPORT BEAM WAS REMOVED, A NEW FLOOR SUPPORT BEAM WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 53-12-01, FIGURE 26.

Part: FRAME — CRACKED (BS 2197)

INSPECTION FOUND FRAME CRACKED AT FS 2197 STIFFENER 2R. THE CRACK LENGTH WAS NOT IDENTIFIED. THE CRACKED SECTION OF FRAME WAS REMOVED, FILLER AND DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-31-01, AND 51-21-01.

Part: SUPPORT — CORRODED (BS 1841)

INSPECTION FOUND UPPER FLOORBOARD SUPPORTS CORRODED IN CARGO AFT BILGE AREA AT FS 1841 FROM LONGERON 43L TO 43R. THE FLOORBOARD SUPPORTS WERE REMOVED, NEW FLOORBOARD SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 53-16-01, FIGURE 14.

Part: CHANNEL — CORRODED (BS 2165-2168)

INSPECTION FOUND WEB CHANNEL CORRODED AND LOOSE FASTENERS ON LONGERON 1L BETWEEN FS 2165 AND 2168. THE CHANNEL WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-52-01 AND 51-21-01.

Part: TRIPLER — CORRODED (FUSELAGE)

INSPECTION FOUND TRIPLER PANEL FOR ADF CORRODED. REPAIRED IAW SRM 53-20-00 AND 51-21-01.

Part: SUPPORT — CORRODED (BS 1911)

INSPECTION FOUND UPPER FLANGE OF FLOOR SUPPORT CORRODED AT STA 1911, LBL 70. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-31-01. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01, AND 51-31-01.

Part: SUPPORT — CORRODED (AFT WASTE TANKK)

INSPECTION FOUND AFT WASTE TANK FORWARD SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01, AND 51-31-01.

Part: SUPPORT — CORRODED (BS 460)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 460, RBL 30 TO 50. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 53-11-01, AND 51-21-01.

Part: SUPPORT — CORRODED (BS 495)

INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT FS 495, LBL 22. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 1914)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1914, LBL 19 TO RBL 19. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01, AND 51-31-01.

Part: SKIN — CORRODED (WING)

INSPECTION FOUND UPPER WING PANEL #641AB OUTBOARD OF TRAPEZOIDAL PANEL CORRODED. THE SKIN WAS REMOVED AND REPLACED IAW SRM 57-32-01 AND 51-70.

Part: SUPPORT — CORRODED (BS 1874)

INSPECTION FOUND CORROSION ON FLOOR SUPPORT AT FS 1874, LBL 4 TO 34. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-31-01, A FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-24-15, 51-21-01, AND 51-31-01.

Part: SKIN — DENTED (LT TE FLAP)

INSPECTION FOUND LT WING OUTBOARD FLAP DENTED ON LOWER SURFACE AT XOF 651, TWELVE INCHES AFT OF THE REAR SPAR PLANE. THE DENTED SECTION WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01, FIGURE 4.

Part: SUPPORT — CORRODED (BS 1874)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1874, RBL 3 TO RBL 34. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-31-01, AND 51-21-01.

Part: SUPPORT — CORRODED (BS 1821-1884)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1821 TO 1884, RBL 36. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-16-01, 51-10-02, AND 51-30-02.

Part: FRAME — CORRODED (BS 1902)

INSPECTION FRAME TOP CAP CORRODED IN AFT CARGO COMPARTMENT AT FS 1902, L49L TO 49R. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 2, 53-16-01, FIGURE 14, 51-21-01, AND 51-31-01.

Part: SUPPORT — CORRODED (BS 495-515)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 495 TO 515, LBL 57. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-01 AND 51-31-01.

Part: SKIN — CORRODED (LT WING)

INSPECTION FOUND CORROSION AROUND FASTENERS OF LT WING PANEL 561EB. THE CORROSION WAS REMOVED IAW SRM 51-21-01, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-31-01 AND 57-00-01.

Part: ANGLE — CORRODED (BS 824)

INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED UNDER PANEL 242BF AT STA 824, RBL 63. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-01 AND 51-31-01.

Part: SKIN — DENTED (BS 310)

INSPECTION FOUND RT FUSELAGE SKIN DENTED FORWARD OF FORWARD E AND E COMPARTMENT AT STA 310, LONGERON 50R. THE DENTED AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 13.

Part: SKIN — DENTED (BS 635)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 635, LONGERON 38L. THE DENTED AREA WAS REMOVED, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW 53-20-00, FIGURE 6 AND 51-31-01.

Part: SKIN — CORRODED (WS 948)

INSPECTION FOUND LT WING UPPER SURFACE WITH TWO FASTENER HEADS PULLING THROUGH SKIN AND CORROSION WAS AROUND FASTENERS AND SEAMS AT XW 948, OUTBOARD FORWARD CORNER OF OUTBOARD ISLAND. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-30-01. THE CORROSION WAS REMOVED AND A SPLICE AND DOUBLER WERE INSTALLED IAW SRM 57-10-01 AND 51-30-01.

Part: ANGLE — CORRODED (BS 824)

INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED UNDER PANEL 242BF AT STA 824, RBL 63. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-01 AND 51-31-01.

Part: SUPPORT — CORRODED (BS 824)

INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT FS 824, LBL 46 TO LBL 70. THE FLOORBOARD SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, FIGURE 10A AND 51-10-00.

Part: ANGLE — CORRODED (BS 1099)

INSPECTION FOUND FRAME TO SKIN ATTACH ANGLE CORRODED IN FORWARD CARGO COMPARTMENT AT STA 1099, STRINGER 35 TO 36L. THE ANGLE WAS REMOVED IAW SRM 51-31-01, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-13-01, 51-31-01, AND 51-21-01.

Part: SUPPORT — CORRODED (BS 462)

INSPECTION FOUND UPPER FLANGE AREA OF FLOOR SUPPORT CORRODED AT STA 462, RBL 1. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-01, A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-11-01 AND 51-21-01.

Part: BRACKET — CORRODED (BS 1561-1581)

INSPECTION FOUND INTERCOSTAL BRACKET CRACKED AND CORRODED AT LONGERON 7R, STA 1561 TO 1581. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 53-15-01, 51-21-01, AND 51-31-01.

Part: INTERCOSTAL — CORRODED (BS 899-919)

INSPECTION FOUND INTERCOSTAL CORRODED IN FORWARD CARGO COMPARTMENT AT STA 899 TO 919, LONGERON 34L. THE CORRODED AREA OF INTERCOSTAL WAS REMOVED IAW SRM 53-00-01, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-13-1 AND 51-31-01.