N907UP

Part: MODULE — FAILED (MLG)

UPON GEAR RETRACTION RED LNDG GEAR LIGHTS & TAIL SKID LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE EITHER UP OR OFF. ***SUPPLEMENTAL*** TROUBLESHOT SYSTEM PER MM 32-61-01. UNABLE TO RE PRODUCE LOGBOOK CONDITION. REPLACED LANDING GEAR ELECTRICAL MODULE. ADJ TEST OK.

Part: WEB — CRACKED (FUEL CELL) · airframe 58,392 hrs · 50,725 cycles

INSPECTION TYPE:C, WHILE WORKING CUSTOMER CARD 134185, FOUND CRACK IN VERTICAL WEB IN CENTER FUEL CELL BS 825, LBL 27, WL 193 FWD SIDE OF WEB. REMOVED VERTICAL WEB FROM LBL 25 FOR ACCESS, REMOVED DAMAGED AREA 3 X 3, FABRICATED REPAIR DOUBLER FOR WEB. INSTALLED DOUBLER AND STIFFENER FITTING WET WITH SEALANT ALL WORK PERFORMED PER SRM 51-20-1 SRM 51-30-2, SRM 51-40-2.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 58,392 hrs · 50,725 cycles

INSPECTION TYPE:C, WHILE WORKING CUSTOMER NR 134500 FUSELAGE 88 DISCOVERED MAIN WHEEL WELL RT FWD BULKHEAD CORRODED BS 870 RBL 45 - 54. REMOVED CORROSION 5.5 X 8 AREA RBL 45 TO 54 PER SRM 51-10-6. FABRICATED FILLER AND REPAIR PLATE AND SHIMS AND INSTALLED ALL REPAIR PARTS PER 727 SRM 51-40-2, 51-30-2 AND 51-20-151

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,392 hrs · 50,725 cycles

INSPECTION TYPE: C, FOUND CORROSION ON LOWER SIDE OF THE UPPER SKIN AT STA 870, RBL 50. REPAIRED IAW ER 00-662.

Part: STRAP — CORRODED (SKIN) · airframe 58,392 hrs · 50,725 cycles

INSPECTION TYPE: C, CORROSION BETWEEN BARE STRAP AND FUSELAGE SKIN AFT UPPER MCD BS 632 WL 300 RBL 22-30 REPAIRED IAW ER 00-0665

Part: HINGE FITTING — CORRODED (KRUGER FLAP) · airframe 58,392 hrs · 50,725 cycles

INSPECTION TYPE: C, NR 6 KRUGER FLAP FIXED CENTER LE HINGE FITTING CORRODED AT LE ATTACH POINT. REPLACED FIXED CENTER LE FITTING

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,392 hrs · 50,725 cycles

INSPECTION TYPE:C, BULGING SKIN AT BS 360 BETWEEN STR 26 LT TO 27 LT ON EXTERNAL SKIN. ACCOMPLISHED REPAIR PER EO B727-5310-1371 APP 8.5 AND DRAWING NR 69-62161.

Part: SPAR — CORRODED (CENTER WING) · airframe 58,392 hrs · 50,725 cycles

INSPECTION TYPE: C, CORROSION ON CENTER WING BS 870 REAR SPAR WEB BL 0 - BL 6, WL 160 REPAIRED IAW ER 00-0662

Part: TAB — DAMAGED (LT AILERON)

LEFT OUTBOARD AILERON IE WEDGE OUTBOARD OF TAB HAS CORNER MISSING. REPAIRED PER SRM 57-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS LEFT ON FROM LAST FLIGHT. RELAMPED AND REPLACED BATTERY, OPS CHECK GOOD.

Part: LIGHT — INOP (CABIN)

INSPECTION TYPE-N/A, EMER EXIT LIGHT (ENTRANCE) ASSY ROBBED FOR A/C 820 (S/N 20896 A 450467). REPLACED ROBBED EMER EXIT LIGHT (P/N ON 10-0067-9) (S/N 22574), OPS CK PER MM 33-50-00. NO DEFECTS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERG EXIT LIGHTS AT COCKPIT DOOR AND FWD ENTRY DEAD. REPLACED BATTERIES IN BOTH PACKS, OPS CHECKED NORMAL MANUAL AND IN ARMED.

Part: YAW DAMPER — INOPERATIVE (E/E COMPT)

INSPECTION TYPE-N/A, UNCOMMANDED UPPER FULL RT DEFLECTION. A/C STARTED ROLL LOWER RUDDER INPUT OF YAW DAMP CORRECT. UPPER RUD HYD SHUT OFF, RUDDER SLOWLY DRIFTED BACK TO CENTER. LANDED WITH LOWER RUDDER ONLY. *S/D* REMOVED AND REPLACED UPPER YAW IAW MM 22-11-13 OPS CHK GOOD. (P/N 2585800-1) (S/N 0550647) ON, (0661015) OFF.

Part: ENGINE — DAMAGED (NR 3)

INSPECTION TYPE-N/A, ATB-NR 3 ENG FOD DAMAGE (INC NR RS97-274) POST FLIGHT INSPECTION (VISUAL) OF NR 3 ENGINE INDICATES FOD DAMAGE. REPLACED NR 3 ENGINE PER T/C.

Part: BATTERIES — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, DURING PREFLIGHT INSPECTION INDOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERG EXIT LIGHT BATTERIES, EMERG EXIT LIGHTS OP CK NORMAL IAW M/M 33-50-00.

Part: BATTERY PACK — MISSING (CABIN)

INSPECTION TYPE-N/A, ROBBED BOTH EMERGENCY LIGHT AND BATTERY PACK ASSY FOR A/C 906. INSTALLED NEW EMERGENCY LIGHT AND BATTERY PACK ASSY, OPS CKS OK.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, CRACKS ON BS 740 FITTING RT FITTING. REPLACED IAW UPS EO B727-5310-7477-C AN SRS EO 97-23-005R1.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, CRACKS ON BS 740 FITTING LT FITTING. REPLACED IAW UPS EO B727-5310-7477 AND SRS EO 97-23-006.

Part: WEB — CRACKED (BS 1284)

INSPECTION TYPE-C, CRACK IN LT VENTRAL STAIRWELL BS 1284. REPAIRED IAW SRM 51-40-2.

Part: TORQUE BOX — CRACKED (BS 1237)

INSPECTION TYPE-C, CRACK IN LIGHTENING HOLE OF LT VENTRAL STAIRWELL AT BS 1237. REPAIRED IAW 51-40-2.

Part: BRACKET — CRACKED (WING)

INSPECTION TYPE-C, T-BRACKET FWD OF NR 7 SPOILER PANEL UPPER SKIN ON T/E OF WING BROKEN. REPLACED BRACKET IAW SRM 51-30-2.

Part: TORQUE BOX — CRACKED (STAIRWELL)

INSPECTION TYPE-C, CRACK IN LIGHTENING HOLE OF LT VENTRAL STAIRWELL TORQUE BOX. REPAIRED IAW SRM 51-40-2.

Part: SKIN — CRACKED (BS 251)

INSPECTION TYPE-C, CRACK FOUND AT BS 251.6 WL 220 APPROX LT SKIN. REPAIRED IAW SRM 53-30-3 FIG 3.

Part: WEB — CRACKED (RT VENTRAL)

INSPECTION TYPE-C, CRACK ON WEB OF RT VENTRAL TORQUE BOX. REPAIRED IAW SRM 51-40-2.

Part: STRINGER — CRACKED (BS 856)

INSPECTION TYPE-C, CRACK ON EXTERNAL FUSELAGE STIFFENER S18R BS 856. REPAIR OF STR 18R CARRIED OUT IAW SRS EO 97-23-002 AND UPS EO B727- 5310-9709-A.

Part: PRESSURE WEB — CRACKED (NLG WW)

INSPECTION TYPE-C, RT NOSE WHEEL WELL PRESSURE WEB AT BS 284 FOUND TO BE CRACKED AND DUE TO THE LARGE NUMBER OF PREVIOUS REPAIRS REPLACEMENT OF WEB IS NECESSARY. NLG WHEEL WELL PRESSURE WEB RT REPLACED IAW BOEING DRG NR 65-18414.

Part: FRAME — CRACKED (BS 303.9)

INSPECTION TYPE-C, CRACK FOUND AT BS 303.9 FRAME STR 14 LT AT FWD ENTRY DOOR. REPAIRED IAW B727-5310-0149.

Part: SKIN — DENTED (WS 373)

INSPECTION TYPE-C, RT WING L/E DAMAGE TO L/E SKIN FS 373 APPROX. REPAIR CARRIED OUT IAW SRM 57-50-3.

Part: HINGE — CRACKED (NR 7 SPOILER)

INSPECTION TYPE-C, NR 7 SPOILER HINGE FITTING CRACKED. HINGE REPLACED IAW BOEING DWG 65-16216 AND SRM 51-30-2.

Part: CASTING — BROKEN (RT TE MIDFLAP)

INSPECTION TYPE-C, RT I/B FLAP I/B MIDFLAP ACTUATING PULLEY SUPPORT CASTING BROKEN. CASTING REPLACED IAW OHM 57-52-01.

Part: SEAT TRACK — CORRODED (BS 360)

INSPECTION TYPE-C, EVIDENCE OF SURFACE CORROSION ON SEAT TRACK AT STA 360 RBL 45.75. SEAT TRACK REPAIRED IAW SRM 53-10-5 FIG 1.

Part: RIBS — CRACKED (NR 1 LE SLAT)

INSPECTION TYPE-C, NR 1 L/E SLAT ROD END CRACKED. ROD END AND RIBS REPLACED PER OHM 20-50-03 AND MM 27-81-32.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE N/A, EMERGENCY EXIT ILLUMINATED AND POPPED OUT OF SOCKET ON LANDING, LIGHT IN COCKPIT. REPLACED LIGHT OVER CABIN DOOR AND OPS CHECK NORMAL.

Part: SEAT TRACK — CORRODED (BS 960-1180)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED SEAT TRACK STA 960-1180, BL ZERO CORRODED. REPLACED IAW SRM EWO 96-2170 SRM 51-30-2.

Part: BLKHD SHEARTIE — CORRODED (BS 351)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER END OF SHEARTIE AT BS 351, RBL 45, WL 168, FORWARD SIDE OF BS 351 BULKHEAD. CORROSION OUT OF LIMITS, REPAIRED WEB AND SHEARTIE IAW SRM 51-30-2, 53-10-3, 53-10-4, 51-10-2, 51-40-2, AND 51-40-3.

Part: BLKHD ANGLE — CORRODED (BS 480)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING AC/CG, DISCOVERED CORROSION AT BS 480 29 ON BULKHEAD Z-ANGLE. REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-10-1, REMOVED AND REPLACED Z-ANGLE 51-20-1 AND IAW SRM 51-10-1 AND 51-30-2.

Part: FITTING — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOORWAY UPPER FORWARD STOP PAD FITTING CRACKED. REMOVED OUTSIDE DIAMETER STOP PAD FITTING, RECEIVED AND INSTALLED ON AIRCRAFT, WORK DONE IAW SRM 51-30-2, AND 52-31-01.

Part: FLOOR BEAM — CORRODED (BS 1110)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON LOWER FLANGE OF FLOORBEAM STA 1110, WL 200, AND LBL 9-19. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT LOWER FLANGE AND REPAIRED PER E.O. 727-53-1745.

Part: CHORD — CRACKED (BS 1152)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING NRC, FOUND BL ZERO CHORD, STA 1152, WL 200, TO BE CRACKED ON VERTICAL LEG. REPAIRED BL ZERO CHORD AT STA 1152 IAW UPS E.O. 727-53-1748.

Part: WEB — CORROSION (BS 1131)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON SHEAR WEB BS 1131, RBL 62, WL 208. REMOVED AND REPLACED SHEAR WEB RT IAW SRM 51-30-2, 51-10-1, AND M/M 51-20-151.

Part: FITTING — CRACKED (CARGO D00R)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED TRANSFERRED FROM DMI LOG CONTROL NR M-106749 1 PRESSURE STOP FITTING CRACKED ON LOWER FWD CARGO DOOR. REMOVED AND REPLACED FITTING IAW EO B727-5230-0032 APP C.

Part: FLOOR BEAM — CORRODED (BS 1130)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM UPPER CHORD STA 1130 LBL 65 WL 207. REMOVED CORROSION PER SRM 53010-1 AND REPAIRED FLOOR BEAM IAW UPS EO 727-53-1744.

Part: SKIN — CORRODED (BS 856-864)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING NRC 437442 FOUND CORROSION ON FUSELAGE SKIN AT STA 856 TO 864 WL 191 LBL 70.5. REMOVED CORROSION PER UPS EO 96-2154.

Part: SKIN — CORRODED (BS 740-870)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON TOP OF FUEL CELL SKIN AT STA 740 TO 870 LBL 25 TO 45 WL 180 TO 202. REMOVED CORROSION, OUT OF LIMITS IAW SRM 57-30-1. REPAIRED SKIN IAW UPS EO 727-57-1689.

Part: SPAR — CORRODED (PNL 7340)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FRONT SPAR CUTOUT 7340 HAS CORROSION ON THE INSIDE. REPAIRED FRONT SPAR CUTOUT ON INSIDE OF TANK AT PNL 7340, IAW UPS EO 727-57-1687.

Part: FLOOR BEAM — CORRODED (BS 1130)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM UPPER CHORD STA 1130 RBL 65 WL 207. REMOVED AND REPLACED CHORD PER SRM 51-30-2.

Part: SEAL RETAINER — CORRODED (BS 870)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STA 870 SEAL RETAINER LBL 60 RBL 60. REMOVED CORRODED SEAL RETAINER IAW 53-10-1, FABRICATED REPAIR PARTS AND INSTALLED EO 727-57-1690 AND SRM 51-30-2, 51-10-1.

Part: ANGLE — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOOR NR 4 TRAVERSE BEAM AND OUTBOARD L-ANGLE CRACKED IN RADIUS AT OUTER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED NR 4 TRAVERSE BEAM AND OUTBOARD L-ANGLE IAW SRM 51-10-1, 51-30-2, 51-30-5, 51-10-2 AND M/M 51-20-151.

Part: BEAM — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CARGO DOOR NR 2 TRAVERSE BEAM CRACKED IN OUTBOARD RADIUS AT NR 1 OUTER SKIN VERTICAL STIFFENERS. REMOVED AND REPLACED NR 2 TRAVERSE BEAM IAW SRM 51-10-1, 51-10-2, 51-20-4, 51-30-2 AND M/M 51-20-151.

Part: CHORD — CORROSION (BS 1176)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING THE 1176 CHORD CORRODED OUT OF LIMITS FROM RBL 65 TO LBL 65, WL 208, IAW SRM 53-10-1. REMOVED AND REPLACED CHORD IAW SRM 51-10-1, 51-10-2, 51-30-2, 51-30-5, 51-20-4, AND M/M 51-20-151.

Part: SEAT TRACK — CORRODED (BS 1100-1300)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED SEAT TRACK CORRODED OUT OF LIMITS AT STA 1100-1300, RBL 25, WL 208. REPLACED IAW SRM 53-10-5, 51-10-6MM, 51-20-151, 51-30-2.

Part: BEAM — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 5 TRAVERSE BEAM CRACKED IN OUTBOARD RADIUS AT NR 1, NR 2, AND NR 3 OUTER SKIN VERTICAL STIFFENERS. REMOVED AND REPLACED BEAM IAW SRM 51-30-2, 51-10-1, 51-20-21, 51-40-2.

Part: ANGLE — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOOR NR 2 OUTBOARD TRAVERSE BEAM L-ANGLE CRACKED IN RADIUS AT NR 2 OUTER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED NR 2 OUTBOARD TRAVERSE BEAM L-ANGLE IAW SRM 51-10-1, 51-10-2, 51-20-4, 51-30-2 AND M/M 51-20-151.

Part: BULKHEAD — CORRODED (BS 294.5)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON AFT SIDE OF BS 294.5 BULKHEAD ALONG TOP OF HORIZONTAL CHORD BETWEEN RBL 4 + 25 WL 182. OUT OF LIMITS. REPAIRED 294.5 FROM LBL 26-RBL26 IAW SRM 51-10-1, 51-10-2, 51-20-4, 51-30-2, 51-30-5, 51-40-2, AND M/M 51-20-151.

Part: WING RIB — CRACKED (WS 601.5)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING WING RIB REPAIR AT WS 601.5 LT STR 7 LOWER HAS 1 INCH CRACK. REMOVED CRACK IAW B727-5710-1325 APP A, REPLACED RIB, AND INSTALLED IAW B727-5710-1325 APP C.

Part: DOOR FRAME — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR FORWARD LOWER FRAME CRACKED AT FORWARD CENTERING GUIDE ROLLER FITTING. REMOVED AND REPLACED AFT CARGO DOOR FORWARD LOWER FRAME PER SRM 51-30-2.

Part: HAT CHANNEL — CORRODED (BS 304-344)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON HAT CHANNEL STA 304 - 344, RBL 14, WL 208. OUT OF LIMITS. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-30-5, 51-30-8.

Part: FRAME — CORRODED (BS 294.5)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON BS 294.5 FRAME WEB AT RBL 37, WL 168. REPAIRED FRAME WEB IAW SRM 51-20-1. UPPER WEB AT BS 290 WAS ALSO REPLACED IAW SRM 51-20-1, 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 314)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON FLOOR SUPPORT STA 314, RBL 15-40, WL 208 AROUND NUTPLATE HOLES. OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-20-1, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 344)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING SEAT TRACK CRACKED ON FLANGE, STA 344, WL 208. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-20-151, 51-30-2.

Part: SEAL — CRACKED (BS 673-674)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED MOY SEAL HAS CRACKS AT BS 673-674.5 AND 135.702.5 - 704, WL 208, LBL 65 CONTAINED CRACKS AND FABRICATED REPAIR PARTS IAW SRM 51-40-3, AND INSTALLED PARTS IAW 51-30-2.

Part: CHORD — CORRODED (BS 294.5)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING ON CUSTOMER CARD NR 437378, FOUND HORIZONTAL CHORD AT STA 294.5, WL 181, LBL 17, AND RBL 4-25, TO HAVE CORROSION. OUT OF LIMITS. REMOVED AND REPLACED FUSELAGE CHORD AND HORIZONTAL CHORD IAW SRM 51-30-2, 51-20-4, 51-30-5.

Part: SEAT TRACK — CORRODED (BS 660-740)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON SEAT TRACK LBL 62, STA 660-740, WL 208 OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-1, 51-30-2.

Part: HAT CHANNEL — CORROSION (BS 1137)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL BS 1137 LBL 25 TO 65 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND FABRICATED HAT CHANNEL AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 51-30-8.

Part: EXPANSION LINK — CORROSION (BS 850-870)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON EXPANSION LINK STA 850 TO 870 LBL 45, WL 208. CORROSION REMOVAL WAS OUT OF LIMITS. FABRICATED NEW LINK AND INSTALLED IAW SRM 53-10-1, 51-10-2, OHM 20-50-3 AND MM 51-20-31.

Part: STRINGER — CORROSION (BS 480)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION STA 480 STR 21 RT LOWER FLANGE. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 21R IAW SRM 53-10-3.

Part: STRINGER — CORROSION (BS 488)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION STA 488 STR 22 RT UPPER FLANGE WL 170 RBL 50. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 22R FROM STA 470 TO 490 IAW SRM 53-10-3.

Part: STRINGER — CORROSION (BS 360-410)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STR 21R AT BS 400 WL 177. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-10-1. REMOVED SECTION OF STR FROM STA 360 TO 410 AND REPLACED SECTION IAW SRM 53-10-1 AND 51-40-3.

Part: HAT CHANNEL — CORROSION (BS 1130-1180)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED. CORROSION ON HAT CHANNEL BS 1130 TO 1180 RBL 25 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND FABRICATED HAT CHANNEL AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 51-30-8.

Part: HAT CHANNEL — CORROSION (BS 1130-1175)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL BS 1130 TO 1175 LBL 25 TO 65 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED HAT CHANNEL AND INSTALLED PER SRM 51-30-2, 51-30-5, 51-30-8 AND 51-20-1.

Part: INTERCOSTAL — CORROSION (BS 316)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER AND LOWER SURFACE OF INTERCOSTAL AROUND NUT CLIP HOLES STA 316 RBL 51 WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2.

Part: HAT CHANNEL — CORROSION (BS 1137)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL BS 1137 RBL 62 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND FABRICATED HAT CHANNEL AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 51-30-8.

Part: FLOOR BEAM — CORROSION (BS 328)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM STA 328 LBL 4, 19 AND 46, WL 208. REMOVED CORROSION, CUT FLOOR BEAM UPPER FLANGE AT RBL 18 TO LT END, FABRICATED NEW CHORD AND INSTALLED PER SRM 53-10-8.

Part: TAB FITTING — CORROSION (LT AILERON)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING I/B AILERON SIDE TAB HINGE FITTINGS ARE CORRODED. REMOVED AND REPLACED TAB FITTINGS UPS SRM 51-30-2.

Part: INTERCOSTAL — CORROSION (BS 312-328)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER AND LOWER SURFACE OF INTERCOSTAL AROUND NUT CLIP HOLES STA 312 TO 328 RBL 40 WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2 AND 51-30-8.

Part: SEAT TRACK — CORROSION (BS 344-480)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED SEAT TRACK AT LBL 45 STA 344 TO 480 WL 208 HAS CORROSION. REMOVED CORROSION AND FOUND TO OUT OF LIMITS. FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.

Part: INTERCOSTAL — CORROSION (BS 312-328)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER AND LOWER SURFACE OF INTERCOSTAL AROUND NUT CLIP HOLES STA 312 TO 328, LBL 31 WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2 AND 51-30-8.

Part: SEAT TRACK — CORROSION (BS 480-650)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED SEAT TRACK AT LBL 25 STA 480 TO 650 WL 208 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK. ALSO, FOUND INTERCOSTAL AND ANGLE DAMAGED, ALL WORK DONE IAW 51-10-2, 53-10-2, MM 51-20-151, SRM 51-30-5 AND 51-30-8.

Part: THRESHOLD — CORROSION (BS 304)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON COCKPIT THRESHOLD SUPPORT CHANNEL STA 304 WL 208 LBL 11 TO RBL11. REMOVED AND REPLACED C/P THRESHOLD CHANNEL IAW SRM 51-20-1, 51-20-31, 51-30-8, 53-10-1 AND 51-30-2.

Part: L-ANGLE — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 2 O/B TRANSVERSE BEAM L-ANGLE CRACKED IN RADIUS AT NR 2 OUTER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED DOOR L-ANGLE IAW SRM 51-10-1, 51-30-2, 51-30-2, 51-30-5, 51-30-1 AND MM 51-20-151 AND 51-20-21.

Part: BEARING — CORRODED (NR 6 TE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 6 K-FLAP BULLNOSE I/B BEARING HAS CORROSION ON O/B SIDE. REPLACED K-FLAP NR 6 IAW MM 27-81-01.

Part: SEAT TRACK — CORROSION (BS 1000-1050)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK STA 1000 TO 1050 RBL 45. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT OUT AND REPLACED SEAT TRACK IAW SRM 53-10-1, 53-10-5, AND 51-20-4.

Part: ANGLE — CORRODED (BS 305)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON SUPPORT ANGLE STA 305 RT STR 20. REMOVED AND REPLACED ANGLE IAW SRM 51-20-1, 51-30-2, 51-10-2, 51-20-4 AND MM 51-20-151.

Part: STRINGER — CORRODED (BS 356)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STRINGERS 4 AND 5 RT AT BS 356. CORROSION REMOVAL ON STR 4R WITHIN LIMITS, CORROSION REMOVAL ON STR 5R OUT OF LIMITS. REMOVED DAMAGED SECTION OF STR BETWEEN BS 338 AND 356, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-3.

Part: L ANGLE — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 3 O/B TRANSVERSE BEAM L-ANGLE CRACKED IN RADIUS AT NR 1 OUTER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED DOOR L-ANGLE IAW SRM 51-10-1, 51-30-2, 51-40-2, 51-20-21, 51-30-1 AND MM 51-20-151 AND 51-20-21.

Part: ANGLE — CORRODED (BS 304)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON L-ANGLE AT STA 304 RBL 33 TO 57 WL 208. REMOVED CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1, REPAIRED ANGLE IAW SRM 51-20-1 AND 51-20-4.

Part: SHEAR TIE — CRACKED (BS 277)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CRACKED SHEAR TIE AT STA 277 STR 16 RT. REPAIRED SHEAR TIE IAW SRM 51-30-00, 51-40-2, 51-30-2 AND MM 51-20-151.

Part: WEB — CORRODED (BS 342)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON WEB AT STA 342, RBL 63, WL 208. REMOVED AND REPLACED WEB IAW 53-10-6, 53-10-1, 51-20-1, AND 51-30-2.

Part: FLOOR BEAM — CORRODED (STA 344)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON TOP OF FLOOR BEAM AT STA 344 WL 208 LBL 65 TO RBL 65. REMOVED CORROSION FROM FLOOR BEAM FOUND TO BE OUT OF LIMITS IAW 53-10-1, REPAIRED FLOOR BEAM IAW SRM 53-10-8, 51-30-2 AND MM 51-30-00 AND 51-20-151.

Part: STRINGER TIE — CRACKED (BS 950)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED STR 7 LEFT TIE AT STA 950 CRACKED. REMOVED AND REPLACED STA IAW SRM 53-10-1, 51-30-6, 51-30-5, AND 51-30-2.

Part: FRAME — CORRODED (BS 312)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FRAME AT STA 312, RBL 43, WL 170. REMOVED DAMAGED SECTION OF FRAME AND FAB REPAIR PARTS AND INSTALLED. ALL WORK IAW SRM 51-10-2, 51-40-2, 53-10-1, 51-10-6, 51-30-2, AND MM 51-20-151.

Part: CARRIAGE — CORRODED (NR 1 TE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON NR 1 CARRIAGE INSIDE SPINDAL BOLT. REMOVED AND REPLACED NR 1 FLAP CARRIAGE ON NRC 438048.

Part: INTERCOSTAL — CORRODED (BS 215)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL AT BS 215, RBL 26, WL 176. REMOVED CORROSION AT BS 215, RBL 26, WL 176 PER SRM 51-20-4, 53-10-1, AND 51-30-5.

Part: TAB ASSY — CORRODED (LT AILERON)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON TAB SIDE HINGE FITTINGS ARE CORRODED. REPLACED TAB ASSY.

Part: BONDING JUMPER — CRACKED (NR 2 LE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 2 K-FLAP OUTBOARD BULLNOSE BONDING JUMPER UPPER HAS PITTING ON OUTBOARD SIDE OF RIB. REMOVED DAMAGED AREA FAB REPAIR PARTS AND INSTALLED IAW SRM 57-50-3.

Part: CARRIAGE — CORRODED (NR 8 TE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON NR 8 CARRIAGE INSIDE SPINDAL BOLT. REMOVED AND REPLACED NR 8 FLAP CARRIAGE ON NRC 437965.

Part: FORK ASSY — CORRODED (BS 742)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORK ASSY CORRODED BEYOND REPAIR. REMOVED AND REPLACED FORK ASSY IAW OHM 20-50-01 AND SRM 51-20-4.

Part: FITTING — CORRODED (LT AILERON)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON CENTER HINGE FITTING IS CORRODED, WING SIDE. REPLACED FITTING IAW MM 27-10-1.

Part: FITTING — CORRODED (LT AILERON)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON CENTER HINGE FITTING IS CORRODED, AILERON SIDE. REPLACED FITTING IAW SRM 51-30-2, AND OHM 57-50-1.

Part: CLIP — CORRODED (BS 734)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STRINGER CLIP BS 734, STR 6 RT. REMOVED AND REPLACED STR TIE PER SRM 51-30-2, AND MM 53-11-00.

Part: INTERCOSTAL — CORRODED (BS 740-760)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 740-760, RBL 65, WL 208, AROUND FASTENER HOLES. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2.

Part: WEB — CRACKED (BS 292)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CRACK ON NLG W/W WEB AT BS 292, RBL 23, WL 191. REMOVED AND REPLACED WEB IAW UPS SRM 51-40-02, 51-10-2, 51-30-2, AND 51-20-4.

Part: SILL — CORRODED (BS 304-335)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON MOP SILL AT STA 304-309, RBL 58, WL 208. REMOVED CORROSION IAW 53-10-1. CORROSION EXTENDED TO STA 335, STA 320, AND STA 334 OUT OF LIMITS. REPAIRED MOP SILL PER SRM 51-40-3 AT STA 320, 334.

Part: TIE — CORRODED (BS 363-380)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STR 22R AT BS 363 TO BS 380 RBL 50, WL 165. REMOVED CORROSION IAW SRM 53-10-1. REPLACED STRINGER FRAME TIE IAW 51-30-2.

Part: STRINGER — CORRODED (BS 680-700)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STR 9R FROM BS 680 - BS 700. REPAIRED STRINGER IAW 53-10-1 AND 53-10-3.

Part: FRAME — CORRODED (BS 212)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON LOWER END OF FRAME AT BS 212 LBL 16 WL 168. REMOVED CORROSION, FABRICATED NEW WEB AND INSTALLED PER SRM 51-30-2.

Part: STRINGER — CRACKED (BS 993)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED STR AT STA 993 CRACKED. STOP DRILLED AND SPLICED IN REPAIR IAW MM 51-20-31 SRM 53-10-3, 51-30-2, AND 51-20-4.

Part: SKIN — DELAMINATED (RT AILERON TAB)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED RT WING O/B AILERON TAB I/B AND SKIN IS DELAMINATED UPPER SURFACE. REPAIRED RIGHT WING OUTBOARD AILERON TAB IAW SRM 51-40-6 AND 51-80-6.

Part: RIB — CRACKED (NR 6 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 6 SLAT HAS CRACK ON FIRST RIB I/B FROM O/B END. REMOVED AND REPLACED RIB IAW SRM 57-50-3.

Part: BUSHING — CORRODED (LT WING/FUS)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION LEFT FRONT BOTTLE PIN BUSHING, ON FWD FACE. REMOVED AND REPLACED BUSHING IAW MM 57-41-11 AND 57-10-7.

Part: FLOOR SUPPORT — CORRODED (BS 328-344)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON FLOOR SUPPORT STA 328-344, RBL 41, WL 208 OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-1, 51-30-2.

Part: BEAM — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOOR NR 5 TRANSVERSE BEAM CRACKED IN OUTBOARD RADIUS AT NR 1 AND NR 2 SKIN VERTICAL STIFFENERS. REMOVED INNER SKIN, REMOVED NR 5 TRANSVERSE BEAM, FABRICATED NEW TRANSVERSE BEAM, AND INSTALLED IN DOOR. ALSO, REPLACED INBOARD AND OUTBOARD L-ANGLES. INSTALLED INNER SKIN. ALL WORK DONE IAW SRM 51-30-2.

Part: TRANSVERSE BEAM — CRACKED (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FWD CARGO DOOR TRANSVERSE BEAM AND O/B L-ANGLE ARE CRACKED IN O/B RADIUS AT OUTER SKIN VERT STIFFENERS. REMOVED AND REPLACED TRANVERSE BEAM IAW SRM 51-10-1, 51-10-2, 51-30-5, 51-30-2, 51-20-4 AND MM 51-20-151.

Part: GATE — CRACKED (GALLEY DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION AND CRACKING MID GALLEY DOOR UPPER GATE UPPER EDGE. REMOVED AND REPLACED UPPER GATE IAW UPS OHM 52-46-01.

Part: GATE — CRACKED (GALLEY DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION AND CRACKING MID GALLEY DOOR LOWER GATE LOWER FWD CORNER. REMOVED AND REPLACED LOWER GATE IAW UPS OHM 52-46-01.

Part: BATTERY — DISCHARGED (CABIN)

MAINTENANCE REPORTED, CREW ENTRY DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED CREW ENTRY EMERGENCY EXIT LIGHT BATTERIES AND LIGHT OPERATES NORMALLY.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED EMER EXIT LIGHT WOULD NOT ILLUMINATE AT CREW ENTRY DOOR WHEN TESTED DURING PREDEPARTURE CHECK. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: WARNING LIGHT — MALFUNCTIONED (TAIL SKID)

(SUPPLEMENTAL MRR) PILOT REPORTED THAT AFTER TAKEOFF, RED GEAR LIGHTS REMAINED ON WITH GEAR HANDLE UP, TAIL SKID LIGHT REMAINED ON. RECYCLED HANDLE, ALL GREEN POS LIGHTS WORKED NORMALLY AND DOOR LIGHTS WORKED NORMALLY. RED LIGHTS REMAINED ON AFTER RECYCLE ON TAIL SKID LIGHT. PULLED ACTUATOR CIRCUIT BREAKER. TESTED TAIL SKID PER MM 32-71-01 WITH NO FAULTS FOUND. DMI CLEARED.

Part: FITTING — CRACKED (LT/RT MLG)

DURING 'C' CHECK, MAINTENANCE REPORTED FORWARD SUPPORT ATTACH FITTING (WING ATTACH) IS CRACKED. REPLACED FITTING PER SRM 51-10-1, 51-30-2.

Part: FITTING — CRACKED (LT/RT MLG)

DURING 'C' CHECK, MAINTENANCE REPORTED FORWARD SUPPORT ATTACH FITTING (WING ATTACH) CRACKED AND CORRODED, LEFT AND RIGHT MLG. REPLACED FITTING PER SRM 51-30-2, 51-10-1.

Part: CHANNEL — CORRODED (BS 600)

DURING 'C' CHECK, MAINTENANCE REPORTED LEFT MAIN ENTRY DOOR UPPER SIDE OF LOWER 'U' CHANNEL CORRODED. FABRICATED REPAIR PER SRM 51-40-1, 51-10-2, 51-20-4.

Part: SEAT TRACK — CORRODED (BS 740-820)

DURING 'C' CHECK, MAINTENANCE REPORTED SEAT TRACK CORRODED AT FS 740-820. FABRICATED AND INSTALLED SEAT TRACK PER SRM 53-10-5, 51-30-2, 53-10-2.

Part: ANGLE — CRACKED (BS 744)

DURING 'C' CHECK, MAINTENANCE REPORTED ATTACH ANGLES CRACKED AT WING CENTER SECTION LEFT SIDE AT STA 744. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-2.

Part: SKIN — CRACKED (BS 259.7-277)

DURING 'C' CHECK, MAINTENANCE REPORTED FASTENER HOLES CRACKED AT BS 259.7-277, RT SIDE AT STR 9. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-3, 51-30-2.