N79749

Part: POSITION SWITCH — MISRIGGED (L/E FLAP)

DURING TAXI OUT NR 4 LEADING EDGE FLAPS RIGHT DOES NOT HAVE A GREEN LIGHT ON THE F/E PANEL POSITION TEST, RETURNED TO THE GATE. TROUBLESHOT AND FOUND NR 4 LEADING EDGE FLAP POSITION SWITCH LEVER ARM MISALIGNED. ADJUSTED THE POSITION SWITCH LEVER ARM IAW MM REF 27-82-0, NOW OPERATES NORMALLY.

Part: PACKING — PINCHED (OIL TANK CAP)

AFTER ENGINE START ON THE NR 3 NOTICED THE LOW OIL QUANTITY INDICATION. RETURNED TO THE GATE. REPLACED THE DEFECTIVE PACKING ON THE OIL TANK CAP AND TIGHTENED OIL PRESSURE SWITCH LINE B-NUT, IAW MM REF 79-20-11 AND 79-11-0. SERVICED THE NR 3 ENGINE FOUR QUARTS OF OIL AND PERFORMED AN ENGINE GROUND RUN, NO LEAKS NOTED.

Part: LINE — OVERTORQUED (BYPASS FILTER)

DURING CRUISE FLIGHT, ENGINE NR 3 OIL QUANTITY WENT OT ZERO FOLLOWED BY A LOSS OFF OIL PRESSURE AND INCREASE IN OIL TEMP. ACCOMPLISHED PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE AND DIVERTED TO SVMI. LANDED WITH NO INCIDENT, TROUBLESHOOT AND FOUND OVERTIGHTENED FILTER BYPASS PRESSURE PORT ON MAIN ENGINE OIL FILTER HOUSING. ACCOMPLISHED GEARBOX HOUSING BOSS THREAD REPAIR AS PER ENGINE MANUAL PWA 72-61-01, RAN ENGIEN LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: VALVE — DEFECTIVE (NR 2)

NR 2 ENGINE SHUT-DOWN DURING FLIGHT DUE TO HIGH OIL TEMP IN YELLOW ARC. TROUBLESHOT AND FOUND FUEL HEAT VALVE OPEN. CLOSED MANUALLY AND SAFETY WIRED SHUT. RAN ENGINE ALL PARAMETERS NORMAL AND AIRCRAFT RETURNED TO SERVICE WITH FUEL HEAT VALVE ON DMI. NO FURTHER INCIDENTS.

Part: PUMP — FAILED (NR 1 ENGINE FUEL)

DURING INITIAL CLIMB ENGINE NR 1 FAILED, FLAMED OUT, DUMPED FUEL AND RETURNED TO KMIA WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER MM 73-11-01. OPS CHECK GOOD, A/C RETURNED TO SERVICE NO FURTHER INCIDENTS. (M)

Part: STRINGER — CORRODED (FUSELAGE)

DURING A C-CHECK, CORROSION WAS NOTED ON STRINGER 30 AT STA 1148-1166.

Part: FRAME — CORRODED (FUSELAGE)

DURING A C-CHECK CORROSION WAS NOTED ON SUPPORT FRAME AT STA 720-720A, BLO-13 LBL.

Part: SKIN — CORRODED (FUSELAGE)

DURING A (C) CHECK, CORROSION WAS NOTED ON FUSELAGE BILDGE INTERIOR SKIN AND N/PS UNDER SUPPORT FRAME AT STA 660-680, LBL13.5.

Part: FRAME — CORRODED (FUSELAGE)

DURING A C-CHECK CORROSION WAS NOTED ON SUPPORT FRAME STA 920-920A AT BLO-LBL-1.

Part: FRAME — CORRODED (FUSELAGE)

DURING A C-CHECK CORROSION WAS NOTED ON CIRCUMFRENTIAL AND ATTACH FRAME STA 344 RT.

Part: SKIN — CORRODED (FUSELAGE)

DURING A (C) CHECK, CORROSION WAS NOTED ON FUSELAGE SKIN INTERIOR AT STA 600-680, LBL85.

Part: SKIN — CORRODED (FUSELAGE)

DURING C CHECK, CORROSION WAS NOTED ON FUSELAGE INTERIOR SKIN AT STA 660-680 RBL-1.

Part: STRINGER — CORRODED (FUSELAGE)

DURING A (C) CHECK, CORROSION WAS NOTED ON STRINGER 22R AT STATION 1166-1183.

Part: SKIN — CORRODED (FUSELAGE)

DURING (C) CHECK, CORROSION WAS NOTED ON FUSELAGE INTERIOR SKIN AT STA 660-680, LBL-1.

Part: TIRE — FAILED (MLG)

UPON LANDING IN CCS, WHEN EXITING RUNWAY NR 4 TIRE BLEW AFTER REPLACING SAME NR 3 NR 2 AND NR 1 TIRE ALSO HAD TO BE REPLACED PER MM 32-45. AIRCRAFT WAS RETURNED TO SERVICE. NOTE ANTI-SKID WAS ON MEL AT THE TIME. (M)

Part: BEARING — DAMAGED (L1 DOOR)

DURING CLIMB, L1 DOOR HAD LOUD NOISE WHILE PRESSURIZING A/C RETURNED TO CCS MTX REMOVED AND REPLACED BEARING AT L1 DOOR LOWER RAIL PER MM 52-10. AIRCRAFT PRESSURIZED AND CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RELIEF VALVE — FAILED (CABIN PRESSURE)

FLT 523 - MIA-CCS - DURING CLIMB-OUT, CREW UNABLE TO CONTROL CABIN PRESSURE. OUTFLOW VALVE CLOSED DURING ENTIRE TIME. AIRCRAFT RETURNED TO MIAMI WITH NO EMERGENCY LANDING DECLARED. SWAPPED AIRCRAFT, FLIGHT DEPARTED TO ORIGINAL DESTINATION 3:45 MIN DELAY. TROUBLE SHOT PRESSURIZATION PROBLEM TO CABIN SAFETY RELIEF VALVE FAILED IN THE OPEN POSITION. REMOVED AND REPLACED SAFETY RELIEF VALVE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEARING — WORN (SHAFT ASSY)

ON FAE FLT NR 506 - SVMG-KMIA, DURING APPROACH AND 11 MILES FROM LANDING, DURNIG LANDING GEAR EXTENSION, GEAR WAS SLOW TO RESPOND. THERE WAS NO INDICATION OF GEARS DOWN AND LOCKED. GEARS WERE MANUALLY LOWERED. ON GROUND MAINTENANCE, FOUND THE UPPER AND LOWER SHAFT BEARINGS WORN ON THE GEAR HANDLE CONTROL CABLE DRUM AND SHAFT ASSEMBLY. BEARINGS WERE REPLACED IAW MM 20-50-3 AND OPS CHECKED GOOD IAW 32-31-0 PAGE 501-503. AIRCRAFT WAS RELEASED INTO SERVICE. (M)

Part: BATTERY — DISCHARGED (PASSENGER DOOR)

INSPECTION FOUND BOTH FORWARD ENTRY EMERGENCY FLASHLIGHTS WITH CHARGE LIGHTS NOT BLINKING. THE BATTERIES FOR BOTH FLASHLIGHTS WERE REMOVED AND REPLACED IAW MM 25-60-00.

Part: FLOORBEAM — CORRODED (BS 1130)

INSPECTION FOUND MAIN CABIN FLOORBEAM CAP CORRODED AT STA 1130 FROM RBL 25-45. THE FLOORBEAM CAP WAS REMOVED AND REPLACED IAW ECRA 5310-03861.

Part: KEEL BEAM — CRACKED (BS 950)

INSPECTION FOUND A 4 INCH CRACK IN KEEL BEAM CHORD AT STA 950E, STRINGER 29R. A REPAIR WAS INSTALLED IAW ECRA 5310-03862.

Part: SKIN — CORRODED (BS 950)

INSPECTION FOUND FUSELAGE SKIN CORRODED AROUND BELLY DRAIN AT STA 950E BETWEEN STRINGER 29R TO 30. A REPAIR WAS INSTALLED IAW ECRA 5330-02822.

Part: WIRE — BROKEN (ROW 12)

THE EMERGENCY PATH LIGHTING AT SEAT NR 12 WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE FOUND AT LIGHT ASSEMBLY AND OPERATION CHECKED GOOD IAW MM 33-50-02, PAGE 201.

Part: ANGLE — CRACKED (WS 92)

INSPECTION FOUND A .3125 INCH CRACK IN DOUBLER ANGLE AT RT WING FRONT SPAR WBL 92. THE ANGLE AND STIFFENER WERE REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, FIGURE 4.

Part: BATTERY PACK — DISCHARGED (PAX DOORWAY)

INSPECTION FOUND AFT ENTRY OVERHEAD EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW MM 33-50-01, PAGE 501.

Part: SKIN — DELAMINATED (NR 1 SPOILER)

INSPECTION FOUND NR 1 SPOILER PANEL UPPER SKIN DELAMINATED. THE SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-61-81.

Part: BATTERY PACK — DISCHARGED (R2 DOORWAY)

INSPECTION FOUND R-2 DOOR UPPER EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW MM 33-50-01, PAGE 501.

Part: BATTERY PACK — DISCHARGED (EXTERIOR)

INSPECTION FOUND LT AFT EXTERNAL EMERGENCY LIGHT ON AFT WING FAIRING WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW MM 33-50-01, PAGE 501.

Part: BATTERY PACK — DISCHARGED (L1 DOOR)

INSPECTION FOUND L-1 DOOR UPPER EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW MM 33-50-01, PAGE 501.

Part: FLOORBEAM — CORRODED (BS 1110)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1110 FROM RBL 25-45. A REPAIR WAS INSTALLED IAW SRM 51-10-8, PAGE 18.

Part: STRINGER — CORRODED (BS 620)

INSPECTION FOUND STRINGER 27R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 620. THE CORRODED SECTION OF STRINGER WAS CUT OUT. A STRINGER REPAIR WAS INSTALLED IAW SRM 51-30-2, 53-10-3, AND 51-10-6.

Part: FLAP — CRACKED (RT TE MIDFLAP)

INSPECTION FOUND A .125 INCH CRACK WITH DENT IN THE RIGHT I/B MIDFLAP TRAILING EDGE INBOARD MOST END. THE FLAP WAS REPAIRED IAW SRM 51-40-6.

Part: FRAME — CRACKED (BS 620)

INSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO FRAME AT STA 620, RBL 27-28. THE CRACKED AREA WAS CUT OUT, A SPLICE REPAIR WAS INSTALLED IAW SRM 51-40-3, 51-10-6 AND 51-30-2.

Part: SUPPORT — CORRODED (BS 1070)

INSPECTION FOUND FLOOR SUPPORT J-ANGLE CORRODED AROUND SCREW HOLES AT BS 1070 BETWEEN RBL 45 AND 62. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-1, 51-10-2, PAGE 1 AND 51-20-2, PAGE 1.

Part: SKIN — GOUGED (RT TE FOREFLAP)

INSPECTION FOUND RT WING I/B FOREFLAP BULLNOSE LOWER SIDE ABOVE CENTER HINGE POINT GOUGED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-50-00.

Part: SKIN — DEBONDED (LT TE FOREFLAP)

INSPECTION FOUND LEFT I/B FOREFLAP UPPER SKIN DEBONDED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.

Part: SUPPORT — CORRODED (BS 1035)

INSPECTION FOUND CABIN FLOOR PANEL SUPPORT CORRODED AT STA 1035, RBL 15 TO RBL 62. THE CORROSION WAS REMOVED IAW SRM 51-6-1. THE SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 1 AND 51-10-1, PAGE 4.

Part: ANGLE — CORRODED (BS 1178)

INSPECTION FOUND CABIN FLOOR CHORD ANGLE AT STA 1178, RBL 46 CORRODED AROUND LAV TANK AFT I/B MOUNT BOLT. THE CORRODED AREA WAS REMOVED AND A REINFORCEMENT CHORD REPAIR WAS INSTALLED IAW ECRA 5310-01585.

Part: WEB — CHAFED (BS 1283-1342)

AFT AIR STAIR ENTRY WAY LEFT WEB PANEL HAS CHAFE MARKS (6 EA) FROM STA 1283 TO 1342. FABRICATED, TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER PER SRM 52-01 FIG 61, 51-10-2, AND 51-30-2.

Part: SKIN — DEBOND (RT TE AFT FLAP)

RIGHT INBOARD AFT FLAP AFT SEGMENT UPPER SURFACE HAS 3.25 CHAFED SPOT AND 1.25 X .75 DEBOND AREA 27.5 FROM INBOARD END. REMOVED AND REPLACED FLAP.

Part: FLOORBEAM — CORRODED (BS 344)

FLOORBEAM FS 344 HAS CORROSION TOP FLANGE BOTH SIDES RBL 24 TO LBL 60. REPAIRED AREA PER SRM 53-40-8 PAGE 51.

Part: INTERCOSTAL — CORRODED (BS 400-420)

INTERCOSTAL CORROSION FS 400 TO 420 RBL 12. REMOVED INTERCOSTAL, FABRICATED, TREATED, PRIMED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-6, 51-10-1, 51-10-2 AND 51-30-2.

Part: SKIN — GOUGED (RUDDER)

UPPER RUDDER TRAILING EDGE JUST BELOW NR 2 CONTROL TAB ATTACH HINGE (FROM BOTTOM) AREA GOUGED. REMOVED DAMAGED AREA BY ROUTING, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PER SRM 51-10-2 AND 51-40-2.

Part: WEB — CORRODED (BS 1178)

FLOOR LEVEL WEB CORRODED WHERE FS 1178 CHORD ANGLE REMOVED AT RBL 34. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED PER SRM 53-41-2.

Part: SKIN — BULGED (BS 1050-1070)

FUSELAGE LOWER SKIN BETWEEN STATIONS 1050 TO 1070 AND STRINGER 30 AREA BULGED. REMOVED FASTENERS FROM FUSELAGE SKIN, NO CORROSION WAS FOUND. FABRICATED DOUBLER USING 2024 T3 .080 TREATED, PRIMED AND INSTALLED PER SRM 51-30-2 AND 53-30-3.

Part: CHANNEL — CRACKED (RT ELEVATOR)

RIGHT ELEVATOR LOWER SKIN FORWARD OF CONTROL TAB INNER CHANNEL CRACKED (.5). STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 55-20-3, 51-10-1 AND 51-30-2.

Part: CHORD — CRACKED (NR 7 LE SLAT)

APPROX 2.25 INCH CRACK BELOW OUTBOARD UP STOP PAD AT LOWER CHORD RIGHT WING NR 8 SLAT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-4, 51-10-2 AND 51-30-2.

Part: STRINGER — CRACKED (VERT STAB)

VERTICAL STABILIZER INNER COMPARTMENT NR 8 RIB RT STRINGER NR 8 CRACKED AT ATTACH BOLT (2). STOP DRILLED CRACK, FABRICATED ANGLE AND FILLER REPAIR, TREATED AND PRIMED REPAIR PARTS, INSTALLED PER SRM 55-30-4, 55-30-9 AND 51-30-2.

Part: CHORD — CORRODED (BS 306-348)

CHORD CORROSION INBOARD OF LEFT CUTOUT AT FS 306 TO 348. REMOVED OLD ANGLE, FABRICATED, TREATED, PRIMED AND INSTALLED NEW ANGLE PER SRM 51-10-1.

Part: INTERCOSTAL — CORRODED (BS 700-720)

STATION 700 TO 720 STRINGER 28R OUTBOARD INTERCOSTAL FLANGE CORRODED. CUT OUT DAMAGED AREA. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PER SRM 51-40-3, 51-10-6 AND 51-30-2.

Part: MECHANISM — HUNG UP (PASSENGER DOOR)

AFT ENTRY DOOR DOES NOT OPEN SMOOTHLY, HANGS UP AT BOTTOM. ADJUSTED AFT DOOR UPPER LATCH FITTING PER MM 52-13-0 PAGE 405.

Part: SHIELD PLATE — CRACKED (VERT STAB)

VERTICAL STABILIZER INNER COMPARTMENT SHIELD PLATE AT I/B 1 AND LEFT HAND STRINGER NR 7 AREA HAS A SMALL CRACK (.25). REMOVED FASTENERS, FABRICATED ANGLE PER SRM 55-30-6. TREATED, PRIMED AND INSTALLED DOUBLER PER SRM 51-10-2 AND 55-30-6 PG 2A.

Part: INTERCOSTAL — CRACKED (BS 760)

INTERCOSTAL CRACK AT 3 EACH TOP FLANGE HOLES BETWEEN FLOORBEAMS 760 TO 740 0 BL (1). REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED PER SRM 51-10-2 AND 51-30-2.

Part: SKIN — CRACKED (RT ELEVATOR)

RIGHT ELEVATOR LOWER SKIN JUST FORWARD OF CONTROL TAB AREA CRACKED (3). STOP DRILLED CRACK. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 51-10-1, AND 55-20-3.

Part: BEAM — CORRODED (BS 328-344)

CABIN STA 328 TO 344 LBL 30 J BEAM CORRODED. REMOVED J BEAM, RECEIVED EXTRUSION, DRILLED, TREATED, PRIMED AND INSTALLED PER SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 312)

FLOORBEAM FS 312 HAS 2 HOLES WITH CORROSION AT LBL 20 AND 3. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PER SRM 53-10-9 FIG 8.

Part: STRINGER — CORRODED (BS 700-720)

CORROSION AT STA 28R INBOARD BETWEEN STATION 700 AND 720. REMOVED FAIRING RIBS STA 700 TO 710 RIGHT. CUT OUT DAMAGED AREA, REMOVED INTERCOSTAL STA 700 TO 720 STR 28 RIGHT. ACCOMPLISHED HFEC, NO CKACK FOUND. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PER SRM 53-30-3, 51-10-6 AND 51-30-2.

Part: HINGE — CRACKED (LT WING)

APPROX .25 CRACK AT LEFT WING UPPER T/E AT 2ND FROM O/B CUT OUT FOR NR 4 SPOILER HINGE. STOP DRILLED CRACK PER SRM 57-30-4. FABRICATED REPAIR PER SRM 57-30-04 PAGE 29. TREATED PRIMED AND INSTALLED PER SRM 51-10-2 AND 57-30-04 PAGE 27.

Part: INTERCOSTAL — CORRODED (BS 400-420)

CABIN FLOOR INTERCOSTAL CRACKED (10) ON TOP FLANGE 0 BL FS 400 - 420. REMOVED DAMAGED FLANGE AND FABRICATED NEW FLANGE, TREATED, PRIMED, AND INSTALLED PER SRM 51-10-1, 51-30-2, AND 51-10-6.

Part: MOUNT — CRACKED (NR 2 LE SLAT)

APPROX .375 VISIBLE BRANCHING CRACK AT LEFT WING NR 2 SLAT WHERE INBOARD UP STOP PAD MOUNTS. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED EXTRUDED ANGLE REPAIR PER 51-4-4 FIG 3. INSTALLED PANELS PER 51-30-2.

Part: SUPPORT — CRACKED (BS 720)

FORWARD CARGO COMPARTMENT OVERHEAD FLOOR BEAM SUPPORT SIDE BRACE BETWEEN STA 720 - 720A CRACKED IN THREE PLACES. REMOVED AND FABRICATED NEW ANGLE, TREATED PRIMED AND INSTALLED ANGLE PER SRM 51-30-2.

Part: RIB — CRACKED (NR 2 LE SLAT)

APPROX 1.25 CRACK AT 3RD FROM INBOARD END RIB INSIDE LEFT WING NR 2 SLAT. STOP DRILLED CRACK. FABRICATED AND INSTALLED TYPICAL FORM DOUBLER FROM 2024 T3 PER SRM 51-40-3. INSTALLED ACCESS PANEL PER 51-30-2.

Part: SPAR — CRACKED (VERT STAB)

VERTICAL STAB UPPER RIGHT LEADING EDGE SPAR CRACKED (.25) AROUND RIVET AT STIFFENER PLATE JUST BELOW TENSION TIE FORWARD ATTACH BOLT. REMOVED FASTENERS. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR PER SRM 55-30-6 AND 51-1-20.

Part: DOUBLER — CHAFED (LT TE FLAP)

LEFT OUTBOARD FLAP AFT SEGMENT UPPER L/E HAS CHAFED AREA AT DOUBLER 24 FROM OUTBOARD END. REMOVED PREVIOUS REPAIR. FABRICATED, TREATED, PRIMED, AND INSTALLED REPAIR PER SRM 57-50-4, 51-10-2, 57-51-4, AND 51-30-2.

Part: RIB — CRACKED (LT TE MID FLAP)

RIGHT OUTBOARD MID FLAP HAS .5 CRACK AT INBOARD MOST RIB LOWER END. INSTALLED DOUBLER AT RIB LOWER END OF MID FLAP PER SRM 51-40-3.

Part: SKIN — CHAFED (NR 4 LE SLAT)

LEFT WING NR 4 SLAT LOWER TRAILING EDGE UPPER SURFACE CHAFED INBOARD TO OUTBOARD END. BURNISHED AREA. FOUND OUT OF LIMITS. FABRICATED, TREATED, PRIMED, AND INSTALLED DOUBLER PER SRM 57-50-3 PABE 2B.

Part: FLOORBEAM — CORRODED (BS 400)

FLOORBEAM CORRODED AT SCREW HOLE FS 400 RBL 35. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS, PICKED UP HOLES, TREATED, PRIMED, AND INSTALLED REPAIR PER SRM 51-10-6 AND 53-10-8 FIG 8.

Part: MOUNT — CRACKED (NR 6 FLAP)

OUTBOARD BRACKET HAS .25 VISIBLE CRACK AT LOWER CORNER WHERE NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. REPAIRED BRACKET PER SRM 51-30-2 AND 51-20-1.

Part: CLIP — CRACKED (RT MLG WW)

KEEL BEAM RIGHT WHEEL WELL ATTACH CLIP CRACKED. REPLACED VERTICAL STIFFENER RT INBOARD CORNER AS PER ORIGINAL PER SRM 51-30-2.

Part: BRACKET — CRACKED (LE FLAP ACT)

INSPECTION FOUND A 1 INCH CRACK IN NR 5 LEADING EDGE FLAP AFT INBOARD ACTUATOR MOUNT BRACKET BELOW ACTUATOR TRUNNION. THE MOUNT BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: SKIN — CRACKED (RT ELEVATOR)

INSPECTION FOUND A .25 INCH CRACK COMING FROM SCREW HOLE TO ACCESS CUTOUT IN RT ELEVATOR SKIN. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-20-03.

Part: SPAR — CRACKED (WING)

INSPECTION FOUND A 1.5 INCH CRACK ON OUTBOARD SIDE AND A 1.5 INCH CRACK ON INBOARD DOUBLER OF NR 8 SLAT INBOARD ACTUATOR MOUNT AREA OF FRONT SPAR. THE INBOARD DOUBLER WAS REMOVED AND REPLACED AND THE OUTBOARD CRACK WAS STOP DRILLED IAW SRM 51-10-1.

Part: SKIN — DENTED (BS 1145)

INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 1145, STRINGER 24L. A REPAIR WAS FABRICATED AND DOUBLERS WERE INSTALLED IAW SRM 51-30-1 AND 51-10-2.

Part: ACTUATOR — FAILED (NR 2 LE FLAP)

THE NR 2 KRUGER FLAP WOULD NOT RETRACT AFTER TAKEOFF FROM MGA. THE AIRCRAFT WAS RETURNED TO MGA WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 KRUGER FLAP ACTUATOR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.

Part: WINDOW — CRACKED (RT COCKPIT)

COCKPIT R-2 WINDOW OUTER GLASS CRACKED. CRACK OBSTRUCTING F/O VIEW. REPLACED WDW PER MM 56-12-11 PG 403, OPS CHECK NORMAL.

Part: FITTING — CRACKED (RT AILERON)

RIGHT HAND AILERON CASTING AND WEB CRACKED AND CORRODED. A 1 INCH CRACK IN WEB. REMOVED CRACKED WEB PER SRM 51-10-1, 51-30-2 AND 57-10-2. REMOVED CORRODED FITTING PER SRM 51-30-2. FABRICATED WEB AND TREATED PER 51-40-5 AND 51-10-2. INSTALLED WEB AND NEW FITTING ASSEMBLY.

Part: BUSHING — WORN (LT MLG WW)

LEFT MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD DOOR ACTUATOR BEAM LINK UPPER END MOUNT BOLT AND BUSHING WORN. REPAIRED ELONGATED BULKHEAD HOLE, INSTALLED NEW PLATE BUSHING AND BOLT IN ACCORDANCE WITH MM 32-10-1 AND EC/RA 5310-03465.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY PATH LIGHTING INOP AT SEATS ROW 30 AND 23. REMOVED AND REPLACED BATTERY IN ACCORDANCE WITH MAINTENANCE MANUAL 33-51-12.

Part: WIRE — FAILED (CABIN)

RIGHT HAND FORWARD AND AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED WIRE AT SOCKET IN ACCORDANCE WITH MAINTENANCE MANUAL 33-51-0.

Part: FLOORBEAM — CORRODED (BS 380)

FLOOR SUPPORT BEAM UPPER CHORD HAS CORROSION BETWEEN BL 48 RT AND BL 58 RT AT STATION 380. CUT OUT DAMAGED AREA AND FABRICATED REPAIR IN ACCORDANCE WITH SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 380-400)

CORROSION AT CABIN FLOOR TRACK STATION 380 TO 400 LBL 24. INSTALLED NEW SEAT TRACK IN ACCORDANCE WITH SRM 51-10-1.

Part: BRACKET — CRACKED (LT LE FLAP)

LEFT WING KRUEGER FLAP ACTUATOR ATTACH BRACKET LOWER OUTBOARD CORNER HAS CRACK .75 INCH. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPLACEMENT IN ACCORDANCE WITH SRM 51-20-1 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 400)

CORROSION BULGE AT FLOORBEAM NUT PLATE STA 400 LBL 20. CUT OUT CORRODED AREA AND FABRICATED FLOORBEAM REPAIR IN ACCORDANCE WITH SRM 51-10-8.

Part: SKIN — CRACKED (RT WING)

TWO CRACKS AND FASTENER HEAD BROKEN AT RIGHT WING UPPER LEADING EDGE SKIN. ONE CRACK .8125, ONE CRACK 1 - AFT OF NUMBER 5 SLAT OUTBOARD ON W/S 430 APPROX. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IN ACCORDANCE WITH SRM 57-30-4.

Part: ANGLE — CRACKED (BS 1253)

A 2 INCH CRACK ON REINFORCEMENT ANGLE RIGHT HAND AIRSTAIR VENTRAL BOX STATION 1253. INSTALLED REPAIR IN ACCORDANCE WITH DRAWING 65C27136.

Part: SKIN — DISBOND (LT TE FOREFLAP)

A 6 FT LONG AREA OF SKIN DISBOND NOTED ON UPPER SURFACE AT SPAR OF LEFT TRAILING EDGE OUTBOARD FOREFLAP 15 IN FROM OUTBOARD EDGE. REMOVED FOREFLAP, REPAIRED AND REINSTALLED IN ACCORDANCE WITH SRM 57-50-0.

Part: FLOOR TRACK — CORRODED (BS 380-410)

CORROSION AT CABIN FLOOR TRACK STATION 380 TO 410 LBL 36. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH 51-10-8.

Part: FLOOR TRACK — CORRODED (BS 380-410)

CORROSION AT CABIN FLOOR TRACK STATION 380 TO 410 LBL 36. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-10-8.

Part: SKIN — CRACKED (TE MID FLAP)

INSPECTION FOUND A .75 INCH CRACK IN LT INBOARD MID FLAP TRAILING EDGE INBOARD CUTOUT AT AFT FLAP EXTEND/RETRACT ROD. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.

Part: SKIN — CRACKED (RT WING)

RIGHT WING LOWER LEADING EDGE FIXED SKIN CRACKED AND CHAFED 1 AT OUTBOARD SIDE OF CUTOUT FOR NR 6 SLAT OUTBOARD TRACK. INSTALLED REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH SRM 57-2-3.

Part: ANGLE — CRACKED (LT LE SLAT)

INSPECTION FOUND A 2 INCH CRACK AT AFT END OF LT WING LEADING EDGE SLAT STA 0 RIB UPPER ATTACH ANGLE. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.

Part: SKIN — CRACKED (RT ELEVATOR)

RIGHT HAND ELEVATOR LOWER SKIN AT PANEL 9413 AREA CRACKED .75 INCH. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IN ACCORDANCE WITH SRM 55-20-3.

Part: ACCESSORY UNIT — INOPERATIVE (E/E COMPT)

THE LANDING GEAR OVERRIDE TRIGGER HAD TO BE USED TO RETRACT GEAR AFTER TAKEOFF. TROUBLESHOOTING PER MM 32-31-11, FOUND NO FAULTS. THE LANDING GEAR ACCESSORY UNIT WAS REPLACED AS A PRECAUTIONARY MEASURE, OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 1070)

INSPECTION FOUND TRANSVERSE FLOOR SUPPORT CORRODED AT BS 1070, RBL 20 TO RBL 32. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: FLOOR SUPPORT — CORRODED (BS 1130)

INSPECTION FOUND TRANSVERSE FLOOR SUPPORT CORRODED AT BS 1130, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-00.

Part: STRINGER — CORRODED (STA 446)

GSO - INSPECTION FOUND STRINGER 27R CORRODED AT STA 446. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (W)

Part: DOOR SILL — CORRODED (AFT AIRSTAIR)

GSO - INSPECTION FOUND THE AFT AIRSTAIR DOOR SILL CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (W)

Part: STRINGER — CORRODED (STA 1130)

GSO - INSPECTION FOUND STRINGER 23R IN AFT PIT AT STA 1130 CORRODED. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-10-3, AND 51-30-2. (W)

Part: ANGLE — CORRODED (STA 440)

GSO - INSPECTION FOUND DOOR SILL ANGLE AND NUT PLATES CORRODED INSIDE WEB AT STATION 440, STRINGER 25R. THE CORROSION AND ANGLE WERE REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-1-21A. (W)

Part: STRINGER — CRACKED (STA 420-440)

GSO - INSPECTION FOUND A 1 INCH CRACK IN FORWARD PIT STRINGER 28R BETWEEN STATION 420 AND 440. THE CRACKED AREA WAS CUT OUT AND CHANNEL FILLER AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND 51-30-2. (W)

Part: INTERCOSTAL — CRACKED (BS 984)

GSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 984, LBL 37. THE INTERCOSTAL WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-3-0. (W)

Part: SKIN — CRACKED (NR 4 SLAT ACT)

GSO - INSPECTION FOUND A .375 INCH CRACK AND A DENT IN THE LEFT WING NR 4 SLAT ACTUATOR CUT OUT. A REPAIR DOUBLER WAS FORMED AND INSTALLED IAW EC5762-01020 AND SRM 51-30-2. (W)

Part: FLOOR SUPPORT — CORRODED (STA 312)

GSO - INSPECTION FOUND CORROSION UNDER FLOOR SUPPORT AT STA 312. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-4. A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-4. (W)

Part: SUPPORT — CORRODED (L-2 DOOR)

GSO - INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. (W)

Part: EEL WIRING — CUT (CABIN)

EWR - FLT 0397 - EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE IN FIRST CLASS SECTION OF CABIN DURING A PRE-FLIGHT CHECK. MAINTENANCE FOUND WIRING TO BATTERY PACK CUT UNDER LT FIRST CLASS SEATS AND 3 BLOWN FUSES. THE WIRING WAS REPAIRED AND THE THREE FUSES WERE REPLACED. OPERATION OF THE EMERGENCY AISLE PATH LIGHTING IN FIRST CLASS CABIN WAS RESTORED. (X)