N859FT

Part: B-NUT — LEAKING (HYD QTY IND) · airframe 76,567 hrs · 18,051 cycles

ABNORMALITY FOUND ON NR 4 HYD QTY DROPPED 6 GAL AFTER LANDING GEAR RETRACTION CONTINUED FLIGHT WITH AOP OFF AND EDP IN DEPR. FOUND HYD LEAK FORM PRESS LINE B-NUT ABOVE PYLON LWR BLHD THEN RETIGHTED B-NUT SO LEAK CKED OK WITH MOTORING.

Part: PLUG — DAMAGED (THRUST REVERSER) · airframe 75,992 hrs · 17,928 cycles

ON PRE-DEPARTURE, NR 1 EXHAUST PLUG SUSTAINED DAMAGE. REMOVED EXHAUST PLUG ASSY, INSPECTED AREA, NO CRACKS NOTED ON FLANGE OR ANY DEFECTS. EXHAUST PLUG ASSY INSTALLED IAW MM 78-11-01-01.

Part: FAIRING — ERRODED (NR 4 PYLON)

NR 4 ENGINE PYLON STRUT TO WING FAIRING EROSION. REPAIRED PER SRM 51-40-09.

Part: SKIN — DELAMINATED (SPOILER)

WING UPPER SURFACE TRAILING EDGE PANEL BETWEEN 4/5 SPOILER VARIOUS AREAS LIGHT DELAMINATION. REPAIRED PER SRM 51-40-15.

Part: SKIN — DAMAGED (AILERON)

OUTBOARD AILERON UPPER SURFACE ONE OFF LOCATION DAMAGED. REPAIRED PER SRM 51-40-15.

Part: SKIN — DELAMINATED (TE FLAP)

RT WING INBD TE MID FLAP 1 AFT FLAP UPPER SURFACE HAS AREAS OF DELAMINATION. REPAIRED PER SRM 51-40-15.

Part: SKIN — DELAMINATED (TE FLAP)

RT OUTBOARD T/E MID FLAP LWR OUTBOARD END DAMAGE/DELAMINATION MARKED. REPAIRED PER SRM 51-40-09.

Part: SKIN — DELAMINATED (TE FLAP)

RT WING INBD TRAILING EDGE FORE FLAP BETWEEN 5/6 CANOE ASSY DELAMINATED/MARKED. REPAIRED PER SRM 51-40-15.

Part: SKIN — DELAMINATED (TE FLAP)

RT WING OUTBOARD FORE FLAP ASSY AFT OUTBOARD CORNER LS DELAMINATED. REPAIRED PER SRM 51-40-15.

Part: PANEL — DELAMINATED (WING)

UPPER LEADING EDGE FWD SURFACE OF FIBERGLASS PANEL DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: ACTUATOR — FAILED (NLG DOOR)

ON APPROACH NOSE GEAR DOOR WARNING BOTH PRIMARY AND ALTERNATE. REPLACED NOSE LANDING GEAR DOOR ACTUATOR PER MAINTENANCE MANUAL 32-34-14 PAGE 201.

Part: SKIN — CRACKED (BS 2650)

CRACK IN FUSELAGE SKIN JUST ABOVE LEFT ELEVATOR BS 2650. REPAIRED PER BOEING SRM 53-30-03.

Part: ACTUATOR — INOPERATIVE (RT MLG)

INOPERATIVE RIGHT WING LANDING GEAR ALTERNATE EXTENSION MOTOR. REPLACED PER BOEING MAINTENANCE MANUAL 32-35-01.

Part: ACTUATOR — INTERMITTENT (LT MLG)

INTERMITTENT OPERATION OF THE LEFT WING GEAR ALTERNATE EXTENTION ACTUATOR (DURING SCHEDULED OPERATIONAL CHECK). REPLACED ACTUATOR PER BOEING MAINTENANCE MANUAL 32-35-01.

Part: MUFFLER — CRACKED (APU)

CRACKED APU EXHAUST MUFFLER AT 8 AND 12 O'CLOCK POSITIONS. REPAIRED PER BOEING MAINTENANCE MANUAL 49-21-03.

Part: DOOR — DAMAGED (LT MLG)

DAMAGED LEFT BODY LANDING GEAR WHEEL WELL DOOR FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-03.

Part: SKIN — DELAMINATED (TE FLAP)

DELAMINATION RIGHT INBOARD TRAILING EDGE AFT FLAP INBOARD OF NR 6 CANOE AREA. REPAIRED PER BOEING SRM 51-40-15.

Part: PANEL — DAMAGED (RIGHT WING)

DAMAGED RIGHT WING TIP HF PANEL COVER. REPAIRED PER BOEING SRM 51-40-15.

Part: SKIN — DELAMINATION (LT TE FLAP)

LEFT OUTBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED DELAMINATION PER SRM 51-40-06.

Part: KEEL BEAM — CORRODED (BS 1290-1280)

LEVEL 1 CORROSION FOUND ON RT WING GEAR WHEEL WELL INBOARD KEEL BEAM UPPER SURFACE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.

Part: BRACKET — CORRODED (BS 1380R)

LEVEL 1 CORROSION FOUND ON RT BODY GEAR WW VALVE SUPPORT BRACKET. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.

Part: ANGLE — CORRODED (BS 1373)

LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL OUTBOARD CHORD ANGLE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORRODED (WS 586)

LEVEL 1 CORROSION FOUND ON LEFT WING UPPER SKIN AT REAR SPAR AREA. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.

Part: BEAM — CRACKED (BS 280)

LEFT WING TRAILING EDGE BEAM UPPER CHORD INBOARD END CRACKED. REPAIRED PER SRM 51-40-14 FIG 2.

Part: STRINGER — CORRODED (BS 1368-1371)

LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL WELL OUTBOARD STRINGER BS 1368 TO 1371 STR R33. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02.

Part: BRACKET — CORRODED (BS 1352)

LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL WELL BRACKET AT BS 2352L WL 160. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.

Part: BEAM — CORRODED (BS 1352)

LEVEL 1 CORROSION ON RT BODY GEAR WW OUTBOARD BEAM BS 1352 TO 1353 BL R70-R80. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02.

Part: BUMPER PAD — CRACKED (LT MLG)

LT WING GEAR BOGIE BEAM TILT BUMPER CRACKED AND DAMAGED. REMOVED AND REPLACED BUMPER PAD PER SRM 51-10-01.

Part: STANCHION — DAMAGED (BS 480)

FWD CARGO COMPARTMENT STA 480 PLUG SUPPORT CHANNEL DAMAGED. REMOVED AND REPLACED BOTH RT SIDE STANCHIONS AT STA 480 PER SRM 51-30-02 AND 51-10-01.

Part: FASTENER — MISSING (HORIZ STAB)

RT HORIZ STAB NAV LIGHT FIXED WITH SEALANT FASTENERS MISSING. INSTALLED FASTENERS PER SRM 51-30-02.

Part: PANEL — DAMAGED (RT WING)

RT WING TOP L/E FIXED PANEL INBD OF PYLON PREVIOUS REPAIR PEELING OFF. REMOVED PREVIOUS REPAIR, REPAIRED PER SRM 51-40-15.

Part: SILL — CORROSION (CARGO DOORWAY)

LEVEL 1 CORROSION FOUND ON FWD LOWER CARGO SERRATED PLATE ON DOOR SILL NR 5, 6 AND7 BOTTOM AFT HOLE NR 8 HAS CORROSION. REMOVED CORROSION FROM PLATE PER SRM 51-10-01.

Part: PANEL — CRACKED (NR 1 ENG COWL)

NR 1 ENGINE INLET 3 INCH CRACK AT 3 O'CLOCK POSITION ON ACCOUSTIC PANEL. REPAIRED CRACK BY CUTTING IT OUT AND APPLYING POTTING COMPOUND PER SRM 54-31-03.

Part: SKIN — TORN (CARGO DOOR)

FWD CARGO DOOR TORN IN UPPER RT CORNER AT PREVIOUS REPAIR. INSTALLED DOUBLER ON FWD RT CORNER OF DOOR PER SRM 51-30-02.

Part: SKIN — DELAMINATED (RT MLG DOOR)

RT WING MLG LOWER FLYING DOOR IS DELAMINATED. REMOVED DAMAGE, APPLIED FIBERGLASS AND BONDING PER SRM 51-40-06.

Part: OVERHEAT LIGHT — ILLUMINATED (RT WING)

ON CLIMBOUT, RT WING OVERHEAT LIGHT CAME ON. APPLIED CHECKLIST AND RETURNED TO JFK. INSPECTED LEADING EDGE DUCT AREA FOR LEAKS AND FAULTY WIRE CONNECTIONS. FOUND LEADING EDGE DUCT BLANKET TORN AND SHORTING WIRES. REPAIRED WIRE AND REPLACED BLANKET, OPERATIONAL CHECK GOOD PER MM 71-00-00.

Part: SEQUENCE VALVE — CRACKED (NLG)

ON MAINTENANCE WALK AROUND, FOUND NOSE LANDING GEAR OPEN DOOR SEQUENCE VALVE ASSEMBLY LEAKING. VALVE FOUND TO BE CRACKED. REMOVED AND REPLACED NOSE GEAR, OPERATED DOOR SEQUENCE VALVE IAW BOEING M/M 32-34-07, LEAK AND OPERATIONAL CHECK OK.

Part: SKIN — TORN (LT ELEVATOR)

TEAR AND DELAMINATION AT INBOARD AFT CORNER LEFT OUTBOARD ELEVATOR. REPAIRED PER BOEING SRM 51-40-15.

Part: CLAMP — BROKEN (COCKPIT)

UPPER ATTACH CLAMP ON PORTABLE OXYGEN BOTTLE IN COCKPIT BROKEN. REPLACED BRACKET ASSEMBLY PER BOEING MAINTENANCE MANUAL 35-31-00.

Part: PANEL — DELAMINATED (RT WING)

FIBERGLASS SURFACE RIPPING AWAY FROM RIGHT WING UPPER SURFACE LEADING EDGE PANEL. REPAIRED PER BOEING SRM 51-40-12.

Part: LINE — BROKEN (NR 1 PYLON)

ON GEAR EXTENSION AND FLAP EXTENSION LOST ALL HYDRAULIC SYSTEM 1 PRESSURE. FOUND AIR DRIVEN HYDRAULIC PUMP PRESSURE FLEX LINE BROKEN. REPLACED LINE PER BOEING M/M 29-11-17.

Part: PARK BRAKE VALVE — STICKING (RT MLG)

ANTI-SKID LIGHT ON AT START OF TAKEOFF ROLL, LIGHT REMAINED ON STEADY. PARKING BRAKE VALVE OPERATION CHECKED AT MODULE, RIGHT BODY GEAR BAY OPERATIONAL CHECK SATISFACTORY. ELECTRICAL PLUG REMOVED AND CLEANED, 10 CYCLES OF PARKING BRAKE CARRIED OUT, ALL SATISFACTORY. REFERENCE M/M 32-44-00 AND 32-42-00 (FOLLOW-UP REPLACEMENT OF VALVE CARRIED OUT).

Part: WIRE — CHAFED (RT WING)

CHAFED WIRE CAUSED RIGHT WING OVERHEAT WARNING LIGHT TO ILLUMINATE AFTER TAKEOFF. FOLLOWED PROCEDURES PER CHECKLIST AND LIGHT REMAINED ON. RETURNED TO DEPARTURE STATION. WIRE CHAFED DUE TO RUBBING ON CLAMP, REPAIRED PER BAC WDM 26-18-11 AND TESTED OK PER BAC MM 26-18-00.

Part: COMPRESSOR — STALLED (NR 3 ENGINE)

ENGINE COMPRESSOR STALL OCCURED DURING TAKEOFF WITH MOMENTARY DIRECTIONAL INSTABILITY, NO UNUSUAL ENGINE INDICATIONS OBSERVED. ABORTED TAKEOFF AND RETURNED TO BLOCKS. PERFORMED VISUAL INSPECTION PER BAC MM 71-00-43 AND BORESCOPE INSPECTION OF ENGINE COMPRESSOR STAGES 8 AND 9 PER MM 72-00-00, NO FAULT OR DAMAGE FOUND. PERFORMED HIGH POWER ENGINE RUN AND ALL PARAMETERS NORMAL PER MM 71-00-00.

Part: FAN BLADES — FOD DAMAGE (NR 3 ENGINE)

ON MAINTENANCE WALKAROUND, FOUND DAMAGE TO FAN BLADES, INLET CASE AND NOSE COWL. SUSPECT THE DAMAGE OCCURRED ON LANDING SINCE THAT WAS THE LAST TIME THE ENGINE WAS OPERATED AND DAMAGE WOULD HAVE RESULTED IN OPERATIONAL PROBLEMS. ENGINE REMOVED AND REPLACED PER POLAR WORK CARDS M 7100-002 ENGINE RUN PER M/M 71-00-00.

Part: PANEL — DELAMINATED (NR 6 SPOILER)

LEFT WING, NR 6 SPOILER PANEL LOWER OUTBD SURFACE DELAMINATED. REPLACED NR 6 SPOILER IAW MM 27-61-01.

Part: DOOR — LOOSE (PNEU SERVICE)

PNEUMATIC GROUND SERVICE DOOR LOOSE. REPAIRED PER BOEING SRM 51-30-02.

Part: DOOR — DELAMINATED (RT WING)

RIGHT WING UPPER OUTBD HF DOOR LOOSE. REPLACED HINGE PER MM 57-21-09.

Part: R-RAIL — CRACKED (NR 3 ENGINE)

NR 3 ENGINE 'R' RAIL CRACKED AT 9 O'CLOCK BEHIND LWR PRECOOLER EXHAUST PORT SKIRT. WELDED AND STRESS RELIEVED IAW PWA 72-53-01.

Part: BRACE — CHAFED (NR 1 PYLON)

NR 1 PYLON DIAGONAL BRACE CHAFED BY AFT FUSELAGE PIN FAIL-SAFE BRACKET. BLENDED OUT PER BOEING SRM 51-10-06.

Part: FUEL PANEL — CRACKED (LT WING)

LEFT WING OUT HINGE FUEL PANEL CRACKED. REPAIRED PER BOEING SRM 51-10-02.

Part: SKIN — PUNCTURED (LT AILERON)

LEFT OUTBD AILERON PUNCTURE INBD END. REPAIRED PER BOEING SRM 51-40-15.

Part: BRACE — CHAFED (NR 4 PYLON)

NR 4 ENGINE DIAGONAL BRACE CHAFED BY AFT FUSELAGE PIN FAIL-SAFE BRACKET. BLENDED OUT CHAFED AREA IAW BOEING SRM 51-10-01.

Part: FAIRING — DELAMINATED (RT TE FLAP)

RIGHT WING NR 8 FLAP TRACK FAIRING DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — DELAMINATION (LT WING)

DELAMINATION ON UPPER OUTBOARD WING TIP LEADING EDGE PANEL ON LEFT WING. REPAIRED PER BAC SRM 51-40-12 AND 51-10-06.

Part: BRACKET — WORN (NR 4 PYLON)

NR 4 PYLON (DOGHOUSE) ASSY FWD MOUNT BRACKET WORN. REMOVED AND REPLACED BRACKET PER BOEING SRM 51-10-01.

Part: ROLLER TRAY — DAMAGED (CARGO)

AFT LOWER CARGO LT AFT ROLLER TRAY PREVIOUS REPAIR DAMAGED. REMOVED AND INSTALLED NEW TRAY IAW BOEING SRM 51-10-01.

Part: PANEL — ERODED (LT WING)

LEFT WING UPPER SURFACE LEADING EDGE PANELS ERODED. REPAIRED PER BOEING SRM 51-40-09.

Part: CARGO TRACK — BROKEN (BS 1700)

CARGO TRACK STATION 1700 BROKEN. REPAIRED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (RT TE FOREFLAP)

LEVEL 1 CORROSION RIGHT WING INBD FOREFLAP ON LOWER INBD SKIN. CORROSION REMOVED PER BOEING 51-40-06, INSTALLED FOREFLAP IAW MM 27-51-02.

Part: STIFFENER — WORN (NR 4 PYLON)

NR 4 ENGINE PYLON FUEL FAIRING (DOGHOUSE) INBD HORIZONTAL STIFFENER IS WORN THROUGH AT 1ST RIB. REMOVED AND REPLACED ANGLE PER BOEING SRM 51-10-01, TREATED AND PRIMED PER SRM 51-10-06.

Part: FASTENERS — BROKEN (RT WING)

RIGHT WING PANEL UPPER FASTENERS DAMAGED. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02.

Part: ELEVATOR — DAMAGED (RT HORIZ STAB)

RIGHT HAND HORIZONTAL STABILIZER OUTBD OF OUTBD ELEVATOR BROKEN OUT AND LOOSE. REPAIRED PER BOEING SRM 51-40-09.

Part: BRACE — CHAFED (NR 4 PYLON)

NR 4 PYLON DIAGONAL BRACE FWD END CHAFED. BLENDED OUT PER BOEING SRM 51-10-01.

Part: ROD END — ABNORMAL (NLG DOOR)

NOSE LANDING GEAR RIGHTHAND STRUT DOOR ROD END LWR BEARING WORN. REMOVED AND REPLACED PER MM 32-22-04.

Part: FASTENERS — DAMAGED (RT WING)

RIGHT WING UPPER LEADING EDGE DAMAGED FASTENERS. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02.

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN GOUGED BELOW L-1 DOOR. BLENDED AND CHECKED IAW BOEING SRM 53-30-01, TREATED AND PRIMED PER SRM 51-10-02, AND MM 51-24-11.

Part: SKIN — CORRODED (FUSELAGE)

SKIN AREA FORWARD OF RIGHT WING GEAR I/B DOOR BULGED. REMOVED AND REPLACED RIVETS PER BOEING SRM 51-30-02.

Part: BRACE — CHAFED (NR 2 PYLON)

NR 2 PYLON DIAGONAL BRACE FWD END CHAFED. BLENDED OUT PER BOEING SRM 51-10-06.

Part: RADOME BOOT — ERODED (FWD FUSELAGE)

RADOME BOOT ERODED/PAINT REQUIRES UPGRADE. REPAIRED AND REPLACED UPGRADE PAINT AS REQUIRED PER BOEING SRM 51-24-11, MM 53-52-01.

Part: SKIN — CRACKED (RT MLG DOOR)

RIGHT WING GEAR FLYING DOOR AFT CUTOUT EDGE CRACKED. APPLIED FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09, PAINTED AND REPAIRED AREA PER MM 51-24-11.

Part: ELEVATOR — CRACKED (LT HORIZ STAB)

LEFT HAND HORIZONTAL STAB TRAILING EDGE O/B OF O/B ELEVATOR CRACKED AND LOOSE. REPAIRED PER BOEING SRM 51-40-09.

Part: BRACKET — MISSING (LT WING)

LEFT FUELING BAY PANEL BRACKET MISSING. REPAIRED PER BOEING SRM 51-10-01.

Part: SKIN — GOUGE (LT ELEVATOR TE)

GOUGE IN TRAILING EDGE OF LEFT INBOARD ELEVATOR. REPAIRED PER BAC SRM 51-40-09 AND 51-24-11.

Part: SKIN — DAMAGED (PAX DOOR)

L-1 DOOR LOWER SKIN GOUGED. REPAIRED PER BOEING SRM 52-00-02 AND SRM 51-10-02.

Part: SKIN — DAMAGED (RT TE FLAP)

RIGHT WING OUTBD AFT FLAP SEGMENT HAS CREASE IN LOWER SKIN APPX 5 FT FROM INBD END. REMOVED DAMAGED AREA PER BOEING SRM 51-40-06, PAINTED AND REPAIRED AREA PER MM 51-24-11.

Part: DOOR — CRACKED (APU COMPT)

APU INLET DOOR CRACKED. REPAIRED PER BOEING SRM 51-40-09.

Part: FASTENERS — LOOSE (NR 2 PYLON)

NR 2 PYLON DOUBLER ABOVE AFT MOUNT ASSY LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02.

Part: GEAR DOOR — GOUGED (RT MLG)

RIGHT WING GEAR DOOR 2 GOUGES. REPAIRED PER BOEING SRM 51-40-09.

Part: BEARING — MIGRATED (NR 1 ENGINE)

NR 1 ENGINE, TANGENTIAL LINK LOWER BEARING MIGRATED. REMOVED AND REPLACED PER MM 71-21-04.

Part: PANEL — CORRODED (NR 7 SPOILER)

LEVEL 1 CORROSION NR 7 SPOILER PANEL SURFACE. CORROSION REMOVED PER BOEING SRM 51-10-06.

Part: FRAME — CRACKED (BS 1820)

AFT CARGO DOORWAY FUSELAGE FRAME OUTER LEG CRACKED AT BS 1820. REPAIRED PER BOEING SRM 51-30-02, 53-10-04 AND 51-30-02.

Part: HINGE — CRACKED (LT WING)

LEFT WING INBD FUEL PANEL HINGE CRACKED. REMOVED AND REPLACED HINGE PER MM 52-49-09.

Part: FASTENERS — MISSING (NR 4 PYLON)

NR 4 PYLON FAIRING MISSING FASTENERS. REPLACED PER BOEING SRM 51-30-02, MM 78-11-03.

Part: FUEL PANEL — CRACKED (LT WING)

LEFT WING FUEL PANEL CRACKED. REPAIRED PER BOEING SRM 51-40-09.

Part: DUCT — CRACKED (NR 1 ENGINE)

NR 1 PYLON PANEL NR 452 FOUND MISSING ON WALK-AROUND INSPECTION. FOUND NR 1 NACELLE ANTI-ICE DUCT HAS OPEN CRACK. REMOVED AND REPLACED NOSE COWL ANTI-ICE DUCT PER M/M 30-21-00, OPERATIONAL AND LEAK CHECK PER M/M 30-21-00. PANEL DEFERRED PER CDL 54-32-2.

Part: BRACE — DAMAGED (NR 1 PYLON)

DAMAGE ON NR 1 PYLON DIAGONAL BRACE DUE TO RUBBING SAILBOAT DOOR LATCH. FOUND DAMAGE IN LIMITS, INSPECTED PER BAC NDT MANUAL PART 6 54-40-03, FOUND OK, AND BLENDED DAMAGED AREA TREATED PER BAC SRM 51-40-01 AND 51-10-01.

Part: BRACE — DAMAGED (NR 2 PYLON)

DAMAGE ON NR 2 PYLON DIAGONAL BRACE DUE TO RUBBING SAILBOAT DOOR LATCH. FOUND DAMAGE IN LIMITS, INSPECTED PER BAC NDT MANUAL PART 6 54-40-03, FOUND OK, AND BLENDED DAMAGED AREA TREATED PER BAC SRM 51-40-01 AND 51-10-01.

Part: COWL — DAMAGED (LT ENGINE)

NR 2 NOSE COWL STA 72 CREASED AT 3:00 POSITION. REPAIRED PER BOEING SRM 51-40-06.

Part: SKIN — DELAMINATION (WING)

DELAMINATION ON PANEL NR 191XL. REPLACED PANEL NR 191XL IAW BOEING SRM 51-30-02.

Part: SKIN — CORRODED (WS 660-700)

LEVEL 1 - CORRODED AT TRAILING EDGE PANEL FRAME W/S 660-700. REMOVED CORROSION FROM ANGLES IAW BOEING SRM 51-10-01 AND TREATED IAW BOEING SRM 51-10-02.

Part: FUEL LINE — CORRODED (RT WING)

LEVEL 1 CORROSION, FUEL LINE NR 3 INBD TANK FOR ENGINE FEED. CLEANED CORROSION IAW BOEING SRM 51-10-01.

Part: ACCESS PANEL — DELAMINATION (LT AC PACK)

LT A/C PACK ACCESS PANEL NR 191N DELAMINATED SEVERAL AREAS. REPAIRED PANEL IAW BOEING SRM 51-40-12.

Part: NOSE COWL — DAMAGED (LT ENGINE)

LARGE DENT IN NR 1 ENG NOSE COWL APPROX 8 O'CLOCK POSITION. REMOVED DAMAGED SKIN AND POTTED CORE FAB FILLER/DOUBLER AND BONDED PARS ON NOSE COWL IAW BOEING SRM 51-40-06, 54-32-03 AND 51-24-11.

Part: FLANGE — CRACKED (NR 3 ENGINE)

CRACK IN 'R' FLANGE AT 9 O'CLOCK POSITION NR 3 ENG. WELDED IAW P/W 72-53-01 USING GREEK ASCOLOY TIG ROD AND DYE CHECK WELD PER SOPM 20-20-02, NO CRACK. ALSO, STRESS RELIEVED IAW 72-53-01.

Part: COWL — DAMAGED (NR 3 ENGINE)

NR 3 INBD FAN COWL HAS CORNERS BENT AND SEPARATED. CUT OUT DAMAGED SKINS, FAB, REPAIRED PARTS AND HOT BONDED AREA IAW BOEING SRM 51-40-06.

Part: CARGO COVER — CRACKED (RT FUSELAGE)

BULK CARGO CORNER COVER IS CRACKED. REPAIRED MADE ON MAE TRAVELER NR 70393 PER BAC 5975.

Part: STRUCTURE — CORRODED (L3 DOOR)

LEVEL 2, CORROSION ON FWD AND AFT LOWER CORNERS OF L-3 DOOR. ALSO, UPPER EDGE DETERIORATED AT HINGE AREA. REPLACED GATE ASSY IAW MM 52-11-01.

Part: SKIN — DAMAGED (RT TE MID FLAP)

RT I/B MIDFLAP T/E HAS SMALL HOLE OUTER SURFACE. SANDED AND CLEANED APPLIED FIBERGLASS OVERLAYS IAW BOEING SRM 51-40-09.

Part: ANTENNA — CRACKED (FUSELAGE)

SMALL ANTENNA BL O BETWEEN ANTI COLLISION LIGHT AND VHF ANTENNA BENT AND CRACKED. REMOVED AND REPLACED MODE S, ANTENNA IAW MM 34-53-01.

Part: SKIN — DAMAGE (RT AILERON)

RIGHT I/B AILERON T/E IS DAMAGED. CUT OUT DAMAGED AREA, FAB. REPLACED CORE AND BONDED PRE-PREG FIBERGLASS OVER-LAYS W/ELEVATED TEMPERATURE CURE, PER IAW 747 AND BOEING SRM 51-40-12.

Part: FIREWALL SKIRT — DAMAGED (LT ENGINE)

LOWER LT AFT SIDE FIREWALL INNER SKIRT TORN, INNER AFT SIDE. REMOVED DAMAGED STRUCTURE AND REPAIRED IAW BOEING SRM 51-40-03.

Part: PANEL — DAMAGED (RT WING)

2 HOLES ON UPPER RT INBD LEADING EDGE PANEL. CLEANED DAMAGED AREA, POTTED HOLE, SANDED SMOOTH, AND APPLIED FIBERGLASS OVERLAYS IAW BOEING SRM 51-40-09.

Part: FAIRING — DELAMINATION (LT TE FLAP)

LEFT WING NR 1 FLAP TRACK FAIRING UPPER SURFACE OF TRAILING EDGE AREA IS DELAMINATED. SANDED AND CLEANED APPLIED FIBERGLASS OVERLAYS IAW BOEING SRM 51-40-09 AND TREATED IAW BOEING SRM 51-24-11.

Part: FITTING — CORRODED (NR 1 TE FLAP)

LEVEL 1, NR 1 FLAP SPINDLE BEARING SUPPORT FITTING HAS CORROSION. REPAIRED IAW 747 OHM 57-52-55.

Part: STIFFENER — CRACKED (RT PYLON)

NR 1 PYLON RIGHT SIDE AFT SKIRT LOWER (INNER SIDE) STIFFENER BENT AND BRACKET CRACKED. REMOVED STIFFENER AND FABRICATED STIFFENER IAW BOEING SRM 51-40-01.

Part: FITTING — CORRODED (NR 4 TE FLAP)

LEVEL 1, NR 4 FLAP SPINDLE BEARING SUPPORT FITTING HAS CORROSION. REPAIRED IAW TRAVELER NR 70347 IAW 747 OHM 57-52-35.

Part: SKIN — DELAMINATION (RT TE FLAP)

RIGHT WING I/B FLAP T/E FLAP LOWER SIDE DELAMINATED NEAR O/B CONTROL ROD. REMOVED DELAMINATED AREA FAB FILLER AND DOUBLER AND BONDED AREA IAW BOEING SRM 51-40-06.

Part: CANOE FAIRING — DELAMINATED (NR 6 TE FLAP)

NR 6 CANOE DELAMINATED LOWER AFT END. REMOVED DELAMINATED SKIN BONDED FIBERGLASS AND DOUBLERS IAW BOEING SRM 51-40-09 AND PAINTED IAW BOEING SRM 51-24-11.

Part: PANEL — CRACKED (LT WING)

L/E PANEL CRACKED LOCATED ON PANEL RACK BY NR 2 PYLON. SANDED AREA CLEANED AND POTTED AREA, APPLIED FIBERGLASS OVERLAYS IAW 747 BOEING SRM 51-40-09.

Part: WIRE HARNESS — CHAFED (LT WING)

NR 1 RESERVE TANK HAS BARE WIRE AND HAS SIGN OF ARCKING RIB NR 1196. REPAIRED PER WPM 20-10-13.

Part: PANEL — CRACKED (RT WING)

RIGHT WING - INBOARD T.E. FLAP WELL OUTBOARD - END UNDERSIDE OF FIBERGLASS PANEL CRACKED AT AFT INBOARD CORNER. REPAIRED PER BOEING SRM 51-40-09.

Part: HEATSHIELD — CRACKED (NR 1 PYLON)

NR 1 PYLON - STRUT HEATSHIELD CRACKS AND ELONGATED HOLES. REMOVED HEATSHIELD AND FABRICATED PER BOEING SRM 51-30-02.

Part: PANEL — DELAMINATED (FUSELAGE)

PANEL - NR 291AL DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — DELAMINATED (LT WING)

LEFT WING - PANEL NR 571 DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — DAMAGED (LT TE FOREFLAP)

GOUGE IN L/E OF LT SIDE OUTBOARD FOREFLAP. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CORRODED (WS 1530-1548)

LEVEL 1, WS 1530, WS 1548 DRY BAY AREA L/W LOWER FASTENERS CORRODED. CORROSION REMOVED PER BOEING 51-10-02 MATERIAL LOSS WITHIN LIMITS PER BOEING 57-30-01, PG 17, 18 AND 27.

Part: SKIRT — CRACKED (NR 1 PYLON)

NR 1 PYLON SKIRT CRACKED NUTPLATE STRIP. REPAIRED PER BOEING SRM 51-10-01.

Part: SKIN — DAMAGED (NR 4 PYLON)

NR 4 PYLON NAC STA 160 LEFT SIDE HAD ELONGATED HOLE. REPAIRED PER BOEING SRM 51-40-02.

Part: PANEL — DELAMINATED (WING)

DELAMINATED PANEL 671 BB. REPAIRED PER BOEING SRM 51-40-09.

Part: PYLON — CRACKED (PYLON)

NR 4 PYLON FIXED AFT FAIRING CRACKED AT FWD ATTACH SUPPORT. REPAIRED, REWORKED PER BOEING SRM 51-10-02.

Part: FAIRING — DAMAGE (NR 1 FLAP TRACK)

NR 1 FIXED FLAP TRACK FAIRING HAD NUMEROUS GOUGES. REPAIRED PER BOEING SRM 51-40-15.

Part: FAIRING — DELAMINATION (NR 2 TE FLAP)

NR 2 FLAP TRACK FAIRING DELAMINATED. REPAIRED PER BOEING SRM 51-40-15.

Part: PANEL — DAMAGED (WS 862)

RIGHT WING LOWER PANEL BY AILERON AT WING STA 862 DAMAGED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — DELAMINATION (RT TE FOREFLAP)

RIGHT WING I/B FOREFLAP STRESS PANEL UPPER SURFACE DELAMINATED ALONG TRAILING EDGE. REPAIRED PER BOEING SRM 51-40-06.

Part: PANEL — CRACKED (NR 1 PYLON)

NR 1 PYLON O/B SPINDLE ACCESS PANEL CRACKED AT EXISTING REPAIR ON PANEL RACK AFT OF LEFT WING. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — WORN (NR 3 FLAP TRACK)

NR 3 FWD FLAP TRACK FIXED FAIRING WORN INSIDE. REPAIRED PER BOEING SRM 51-40-15.

Part: PANEL — DAMAGED (FUSELAGE)

DAMAGED PANEL NR 293 BL. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — DAMAGED (NR 8 SPOILER)

NR 8 SPOILER O/B CORNER TRAILING EDGE DAMAGED. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — DELAMINATED (FUSELAGE)

DELAMINATED PANEL 194 DR. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — CRACKED (NR 294HR)

FAIRING NR 294HR CRACKED ON EDGE. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 7 TE FLAP)

NR 7 FLAP TRACK CANOE DELAMINATED FWD RIGHT SIDE. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — DELAMINATED (WING)

DELAMINATED PANEL 577ET. REPAIRED PER BOEING SRM 51-40-06.

Part: FAIRING — DELAMINATION (NR 5 TE FLAP)

NR 5 FLAP TRACK CANOE DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — DELAMINATED (RT TE MIDFLAP)

RIGHT WING, I/B FLAP MID-FLAP LOWER SURFACE DELAMINATED AT TRAILING EDGE O/B OF I/B FLAP. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CRACKED (NR 1 PYLON)

NR 1 PYLON O/B ACCESS PLATE 452BL INNER LIP SKIN CRACKED. REPAIRED PER BOEING SRM 54-30-03.

Part: RIVETS — BROKEN (NR 1 FLAP FARING)

LEFT WING NR 1 FLAP TRACK FAIRING I/B SIDE RIVET HEADS BROKEN OFF. REPAIRED PER BOEING SRM 51-40-09.

Part: RETAINING STRIP — CRACKED (NR 3 PYLON)

NR 3 PYLON O/B FWD BTM CORNER NUTPLATE RETAINING STRIP CRACKED AT NAC STA 180. REPAIRED PER BOEING SRM 51-10-01.

Part: SKIN — DELAMINATION (RT TE FLAP)

RIGHT WING, OUTBOARD FOREFLAP, DELAMINATED IN SEVERAL AREAS ALONG TRAILING EDGE. REPAIRED AND REPLACED RUB STRIP PER MM 51-51-11.

Part: FITTING — CRACKED (LT TE FOREFLAP)

LEFT WING I/B FOREFLAP ARM AT ATTACH BASE CRACKED 2ND FROM O/B END. REPAIRED PER BOEING SRM 51-10-01 AND OHM 57-52-31.

Part: HINGE — CRACKED (RT MLG WW DOOR)

RIGHT BODY GEAR O/B LWR WELL DOOR 3RD HINGE FROM FRONT CRACKED. REPLACED PER MM 32-14-02.

Part: STIFFENER — CRACKED (WS 270)

CRACKED STIFFENER INSIDE LEADING EDGE OF LEFT WING AT INBOARD END OF INTERCOASTAL AT WS 270. FABRICATED AND INSTALLED STIFFENER PER BAC SRM 51-40-03.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

DELAMINATION ON INBOARD AFT FLAP LEADING EDGE INBOARD SIDE. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.

Part: SKIN — CRACKED (NR 2 ENGINE)

CRACK ON EXTERNAL SKIN OF THE NR 2 ENGINE EXHAUST SLEEVE AT 9 O'CLOCK POSITION. FABRICATED AND INSTALLED A DOUBLER PER BAC SRM 51-10-04.

Part: CARRIAGE PIN — CRACKED (NR 6 FLAP TRACK)

CRACKED OUTBOARD SUPPORT PIN ON NR 6 FLAP TRACK CARRIAGE AFT BOGIE. REPLACED PIN PER BAC OVERHAUL MANUAL 27-51-81.

Part: BRACKET — CRACKED (NR 1 PYLON)

CRACKED ATTACH BRACKET ON TOP AFT INBOARD SIDE OF NR 1 PYLON. FABRICATED AND INSTALLED BRACKET PER BAC SRM 51-10-01.

Part: FASTENERS — SHEARED (BS 2454)

SEVEN SHEARED FASTENERS AT BS 2454 FORWARD OF RIGHT APU DOOR. REPLACED FASTENERS PER BAC SRM 51-30-02.

Part: SKIN — DELAMINATED (RT TE FLAP)

DELAMINATION ON INBOARD TRAILING EDGE FLAP LOWER OUTBOARD END. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-24-11.

Part: SKIN — DELAMINATED (RT TE FORE FLAP)

DELAMINATION ON RIGHT INBOARD FORE FLAP ON THE BOTTOM OF THE OUTBOARD EDGE. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.

Part: FAIRING RIB — CRACKED (NR 3 PYLON)

CRACKED RIB ON AFT FAIRING FORWARD SUPPORT OF NR 3 PYLON. FABRICATED AND INSTALLED REPLACEMENT RIB PER BAC SRM 51-30-02.

Part: PANEL — CRACKED (LT WING)

CRACKED AND DELAMINATED LEFT WING TRAILING EDGE FIXED PANEL FORWARD OF NR 5 SPOILER. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.

Part: MOUNTING FRAME — CORRODED (HORIZ STAB)

LEVEL 1 CORROSION ON A PANEL MOUNTING FRAME STAB STA 231 ON THE RIGHT SIDE OF THE HORIZONAL STABLIZER. REMOVED CORROSION AND TREATED FRAME PER BAC SRM 51-10-01 AND 51-10-02.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

DELAMINATED OUTBOARD TRAILING EDGE OF OUTBOARD AFT FLAP. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-24-11.

Part: COWL — CRACKED (NR 3 ENGINE)

CRACKED GUIDE PIN HOLE ON NR 3 INBOARD CORE COWL. FABRICATED AND REPLACED COWL LONGERON PER BAC SRM 51-10-01.

Part: BRACKET — CRACKED (NR 4 PYLON)

CRACKED NR 4 PYLON SKIRT AFT SUPPORT BRACKET. FABRICATED AND INSTALLED BRACKET PER BAC SRM 51-10-01.

Part: SKIN — CRACKED (NR 2 ENG COWL)

CRACKED SKIN AND FLANGE FOR ALIGNMENT PIN ON NR 2 ENGINE OUTBOARD CORE COWL. FABRICATED AND INSTALLED FLANGE PER BAC SRM 51-30-02.

Part: BRACKET — CRACKED (NR 4 PYLON)

CRACKED RETAINING BRACKET AT NAC STA 209 OF NR 4 PYLON INTERIOR. FABRICATED AND INSTALLED BRACKET PER BAC SRM 51-10-01.

Part: SKIN — CORROSION (WS 1140)

LEVEL 1 CORROSION ON SEVERAL SPOTS ON TOP RIGHT WING FROM WING STATION 1140 TO WING TIP. REMOVED CORROSION AND RETREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORROSION (WS 740-1140)

LEVEL 1 CORROSION AT SEVERAL SPOTS ON UPPER RIGHT WING FROM WS 740 TO 1140. REMOVED CORROSION AND RETREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: SKIN — DAMAGED (NR 4 ENG PYLON)

DAMAGED AND TORN SKIN ON INBOARD INNER VERTICAL SKIN OF NR 4 ENGINE PYLON HORIZONTAL FIREWALL FROM FORWARD END TO AFT ENGINE MOUNT. FABRICATED AND INSTALLED REPLACEMENT SKIN PER BAC SRM 51-30-02.

Part: SPAR SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION (EXFOLIATION) ON LOWER LEFT WING LEADING EDGE SPAR SKIN OUTBOARD OF FUEL SERVICE DOOR. REMOVED CORROSION (EXFOLIATION) PER BAC SRM 53-30-01 AND REPAIR WITHIN LIMITS PER BAC SRM 57-30-01, RETREATED AREA PER BAC SRM 51-10-02.

Part: DOOR — DETERIORATED (RT MLG)

DETERIORATED FORWARD EDGE AND WEDGE ON RIGHT WING GEAR STRUT DOOR. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.

Part: HOUSING — CRACKED (TAXI LIGHT)

CRACKED LEFT TAXI LIGHT HOUSING ON NOSE LANDING GEAR STRUT. REPAIRED WITH FIBERGLASS OVERLAYS AND PAINTED PER BAC SRM 51-40-15 AND 51-24-11.

Part: SKIN — TORN (NR 2 ENG PYLON)

LOOSE AND TORN EXTERIOR SKIN ON INBOARD NR 2 ENGINE PYLON. FABRICATED AND INSTALLED REPLACEMENT SKIN PER BAC SRM 51-30-02.

Part: SILL — CORROSION (CARGO COMPT)

LEVEL 1 CORROSION ON BULK CARGO DOOR SILL. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: SPAR — CORRODED (LT WING)

LEVEL 1 CORROSION (EXFOLIATION) ON LEFT WING FRONT SPAR INBOARD OF THE FUEL SERVICE DOOR. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: JAMB — CORRODED (CARGO COMPT)

LEVEL 1 CORROSION ON AFT EDGE OF THE BULK CARGO DOOR CUTOUT. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: WING TIP — SEPARATED (RT WING)

SEPARATED SKIN ON RIGHT WING TIP ADJACENT TO ANTENNA. REPAIRED PER BAC SRM 51-40-09 AND PAINTED PER BAC SRM 51-24-11.

Part: FILLER — CORROSION (BS 1264)

LEVEL 2 CORROSION (EXFOILIATED) FILLER ON FRAME AT BS 1264, AT FORWARD OUTBOARD CORNER OF RIGHT WING GEAR WHEEL WELL. FABRICATED AND INSTALLED FILLER PER BAC SRM 51-10-01.

Part: FILLER — MISSING (NR4 ENGINE COWL)

FILLER MISSING ON NR 4 ENGINE FAN COWL UPPER EDGE. REPAIRED WITH FABRICATED FILLER AND DOUBLER PER BAC SRM 51-30-02.

Part: PANEL — DELAMINATED (WS 300)

DELAMINATION ON RIGHT WING LOWER LEADING EDGE FIXED PANEL, AT WS 300. REPAIRED PANEL PER BAC SRM 51-40-09 AND TREATED PER BAC SRM 51-24-11.

Part: DOOR — CORROSION (R3 DOOR)

LEVEL 1 CORROSION ON TOP AFT CORNER OF R3 DOOR. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: SKIN — PUNCTURED (NR 4 ENGINE COWL)

PUNCTURE ON NR 4 ENGINE INBOARD COWL, 36 INCHES FROM AFT EDGE. REPAIRED WITH A FABRICATED DOUBLER AND FILLER PER BAC SRM 54-10-03 AND TREATED PER BAC SRM 51-30-02.

Part: DOUBLER — GOUGED (BS 1780)

GOUGES ON EXTERNAL DOUBLER BELOW MAIN CARGO DOOR CUTOUT, AT STA 1780. BLENDED OUT GOUGES, TREATED AND PRIMED PER BAC SRM 51-10-01, 51-10-02 AND 51-24-11.

Part: SKIN — CORROSION (LE FLAP)

LEVEL 1CORROSION AND BUBBLING OF SKIN ON NR 24 LEADING EDGE DEVICE PANEL. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: SKIN — DAMAGED (NR 4 PYLON)

SKIN DAMAGED AND TORN ON NR 4 ENGINE PYLON HORIZONAL FIREWALL OUTBOARD AND FORWARD OF THE AFT ENGINE MOUNT. FABRICATED AND INSTALLED REPAIR PER BAC SRM 51-30-02.

Part: FLANGE — CORRODED (LT WING)

LEVEL 1 CORROSION AND EXFOLIATION AT PANEL MOUNTING FLANGE ON LEFT WING UPPER LEADING EDGE OUTBOARD OF NR 2 PYLON. REMOVED CORROSION, BLENDED, AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: SKIN — DELAMINATED (NR 1 ENGINE COWL)

DELAMINATION OF NR 1 ENGINE OUTBOARD FAN COWL CORNER. BLENDED OUT DELAMINATION PER BAC SRM 51-40-06.

Part: STIFFENER — CHAFFED (NR 3 ENGINE COWL)

CHAFED STIFFENER ON NR 3 ENGINE COWL BETWEEN NR 6 AND NR 7 RIBS. REPAIRED STIFFENER WITH FABRICATED FILLER AND ANGLE PER BAC SRM 51-40-03 AND TREATED PER BAC SRM 51-10-02.

Part: MOUNT FITTING — GOUGED (CARGO DOOR)

GOUGED AFT MOUNT FITTING ON FORWARD CARGO DOOR. PERFORMED HFEC CHECK PER BAC NDTM PART 6 51-00-00 FIG 4, FITTING OK BLENDED OUT GOUGES AND TREATED PER BAC SRM 53-30-01 AND 51-10-01.

Part: COWL — DELAMINATED (NR 3 ENGINE)

DELAMINATION ON NR 2 ENGINE INBOARD FAN COWL INNER SURFACE. REPAIRED WITH FABRICATED FILLER AND DOUBLER PER BAC SRM 54-34-02 AND 51-40-06.

Part: SKIN — CORROSION (BS 1620-1660)

LEVEL 1 CORROSION AT BS 1620 TO 1660 BETWEEN STR 52R AND 52L AT BL 0. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, PAINTED PER BAC SRM 51-24-11.

Part: SKIN — TORN (NR 3 ENGINE COWL)

TORN SKIN ON NR 3 ENGINE OUTBOARD FAN COWL FORWARD EDGE. REPAIRED DAMAGED AREA PER BAC SRM 51-40-06.

Part: DOOR — DAMAGED (RT MLG)

DAMAGED TRAILING EDGE ON THE RIGHT BODY OUTBOARD FORWARD GEAR DOOR. REPAIRED AREA PER BAC SRM 51-40-01.

Part: STIFFENER — CORRODED (RT REAR SPAR)

LEVEL 1 CORROSION ON RIGHT WING REAR SPAR VERTICAL STIFFENER OUTBOARD OF NR 3 ENGINE. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.

Part: PANEL — CORRODED (LT WING)

LEVEL 1 CORROSION AND EROSION ON UPPER LEFT WING LEADING EDGE PANEL OUTBOARD OF NR 2 PYLON. REPAIRED PANEL PER BAC SRM 51-40-09.

Part: FILLER — LOOSE (NR 3 ENGINE COWL)

LOOSE FILLER ON NR 2 ENGINE INBOARD FAN COWL EXTERNAL SKIN. REPAIRED WITH FABRICATED FILLER AND DOUBLER PER BAC SRM 54-34-02 AND 51-40-02.

Part: BRACKET — BROKEN (LT TE FLAP)

ON ARRIVAL AND WALK AROUND, FOUND NR 1 FLAP INBOARD CANOE LOOSE AND HANGING DOWN. REMOVED CANOE AND DISPATCHED AIRCRAFT PER CDL 27-51. REPLACED FITTING AT JFK PER BOEING MAINTENANCE MANUAL 27-52-06 ANF 27-51-31.

Part: OXY TRANSDUCER — FAILED (COCKPIT)

GATE TURNBACK DUE TO CREW O2 PRESSURE READS 0. FOUND INOPERATIVE CREW O2 INDICATION. PLACARDED O2 INDICATION PER MEL 35-3. LATER TRANSDUCER REPLACED PER MAINTENANCE MANUAL 35-11-03.

Part: SKIN — DAMAGED (FUSELAGE)

GROUND DAMAGE CAUSED BY TAIL POST JUST FORWARD OF TAIL JACK PAD. REPAIRED PER BOEING SRM 53-30-03 DETAIL 1.

Part: ROLLER AND TRAY — BROKEN (FWD CARGO)

BROKEN ROLLER AND TRAY FWD CARGO COMPARTMENT BS 660 RBL 25. REPLACED ROLLER AND TRAY PER BOEING SRM 51-10-01.

Part: SKIN — BENT (FUSELAGE)

BENT EXTERNAL SKIN AT NR 1 MAIN ENTRY DOOR HINGE CUT OUT. REPAIRED PER BOEING SRM 52-00-02.

Part: ROLLER TRACK — DAMAGED (BS 1800)

DAMAGED ROLLER TRACK AFT CARGO COMPARTMENT BS 1800 RBL 36. REMOVED FABRICATED REPLACEMENT TRACK AND INSTALLED PER BOEING SRM 51-10-01.

Part: FAN COWL — DISBONDING (NR 3 ENGINE)

DISBONDING REPAIR ON NR 3 ENGINE LEFT FAN COWL AT 10 O'CLOCK POSITION. REPAIRED PER BOEING SRM 51-40-06.

Part: NOSE COWL — DELAMINATED (NR 2 ENGINE)

DELAMINATED OUTER SKIN ON NR 2 ENGINE NOSE COWL AT 5 AND 7 O'CLOCK POSITIONS. REPAIRED PER BOEING SRM 51-40-06.

Part: KEEL BEAM — CRACKED (BS 1350)

CRACKED LEFT BODY GEAR INBOARD DOOR AT KEEL BEAM PANEL BS 1350 LBL 09 WL 90. REPAIRED PER BOEING SRM 51-40-09.

Part: FAN REV SLEEVE — CRACKED (NR 4 ENGINE)

CRACKED REPAIR PATCH ON NR 4 ENGINE FAN REVERSER SLEEVE AT 8 AND 9 O'CLOCK. REPAIRED PER BOEING SRM 51-40-06.

Part: TURBINE CASE — CRACKED (NR 1 ENGINE)

CRACKS IN R AND S RAILS AT 2 O'CLOCK POSITION. WELD REPAIRED AND STRESS RELIEVED PER PRATT AND WHITTNEY MAINTENANCE MANUAL 73-53-01, FLAP PEENED PER BOEING OVERHAUL MANUAL 20-10-03.

Part: SLEEVE SKIN — DELAMINATED (NR1 ENG TR)

DELAMINATED PREVIOUS REPAIR ON NR 1 ENGINE FAN THRUST REVERSE SLEEVE. REPAIRED PER BAC SRM 51-40-06.

Part: RIVETS — MISSING (NR 4 ENG FAIRING)

SEVERAL MISSING RIVETS ON NR 4 ENGINE LEFT AND RIGHT SKIRT FAIRINGS. REPLACED RIVETS PER BAC SRM 51-30-02.

Part: EXHAUST SLEEVE — DELAMINATED (NR 4 ENGINE)

DELAMINATED AND CURLED LEADING EDGE SKIN ON NR 4 ENGINE EXHAUST SLEEVE. REPAIRED PER BAC SRM 51-40-02.

Part: EXHAUST STRUT — CRACKED (NR 1 ENGINE)

CRACK OF MORE THEN 50 PERCENT OF CHORD WIDTH TO NR 1 ENGINE 7 O'CLOCK EXHAUST STRUT. NO CORRECTIVE ACTION, TO BE INSPECTED EVERY 100 HOURS PER BAC MM 72-53-02.

Part: CONNECTOR — BROKEN (NR 4 PYLON)

BROKEN CANNON PLUG (D0048P) BACK SHELL NR 4 PYLON. REPAIRED PER BOEING STANDARD PRACTICE 20-31-00.

Part: FAIRING — CRACKED (LT WING/PYLON)

CRACKED WING TO PYLON FAIRING ON LEFT WING NR 1 PYLON INBOARD OF NR 5 LEADING EDGE FLAP. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — TORN (NR 2 PYLON)

SKIN TORN ON NR 2 PYLON ABOVE STINGER FAIRING. REPAIRED PER BAC SRM 51-40-01.

Part: SKIN — CRACKED (NR 4 PYLON)

CRACK AT LOWER FORWARD ACCESS HOLE NR 4 PYLON, NR 483CL. REPAIRED PER BOEING SRM 54-30-03, TIME LIMITED REPAIR.

Part: RIBS — DAMAGED (APU DOOR)

DAMAGED RIBS ON THE APU DOOR. REPAIRED PER BOEING SRM 51-10-01.

Part: PANEL — DAMAGED (FUSELAGE)

DAMAGED ACCESS PANEL NR 191CL. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — CRACKED (FUSELAGE)

TWO CRACKS AT FORWARD LAVATORY SERVICE PANEL AT CUTOUT FOR PANEL 194R. REPAIRED PER BOEING SRM 51-30-03.

Part: ACTUATOR — LEAKING (RT MLG TILT)

NR 4 HYDRAULIC SYSTEM FLUID LOSS, EXTENDED WING GEAR AND WING FLAPS BY ALTERNATE METHOD. FOUND RIGHT WING LANDING GEAR POSITIONING ACTUATOR LEAKING AND NR 4 ENGINE HYDRAULIC PUMP LEAKING. REPLACED ACTUATOR AND BLED PER BOEING MAINTENANCE MANUAL 32-11-20. REPLACED NR 4 ENGINE DRIVEN PUMP PER BOEING MAINTENANCE MANUAL 29-11-05.

Part: LIGHT — INOPERATIVE (UPPER DECK)

UPPER DECK CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY PER BOEING MAINTENANCE MANUAL 33-51-00.

Part: PANEL — DELAMINATED (NR 3 PYLON)

DELAMINATED NR 3 ENGINE SLOT SEAL STRUT CLOSURE PANEL, SKIN PEELED OFF. REPLACED PANEL PER BOEING MAINTENANCE MANUAL 71-10-10.

Part: NOSE COWL — DELAMINATED (NR 2 ENGINE)

NR 2 ENGINE NOSE COWL TOP PANEL DELAMINATING. REPLACED NOSE COWL PER BOEING MAINT MANUAL 71-11-02.

Part: TIRE — RUPTURED (NR 9 WHEEL)

NUMBER 9 MAIN TIRE RUPTURED DURING TAXI INTO GATE. REMOVED AND REPLACED NR 9 TIRE IAW MM 32-45-01, REPLACED NR 10 AS PRECAUTIONARY IAW MM 32-45-01. FUSELAGE, WHEEL WELLS AND GEAR DOORS INSPECTED PER BURST TIRE INSPECTION, MM 05-51-34, SATISFACTORY. NO EVIDENCE OF FLAT SPOTTING OR LOCKED BRAKES.

Part: S RAIL — CRACKED (NR 2 ENGINE)

FOUND NR 2 ENGINE AFT S-RAIL CRACKED AT 2 O'CLOCK POSITION. STRESS RELIEVED IAW MM 72-53-01, WELDED IAW P AND W 72-53-01.

Part: PANEL — CRACKED (LT WING)

FOUND LEFT WING AILERON LOCKOUT ACCESS PANEL CRACKED AT FORWARD INBOARD CORNER. REPAIRED AREA IAW SRM 51-40-09.

Part: EXH SLEEVE SKIN — PEELED BACK (NR 2 ENGINE)

FOUND NR 2 ENGINE AFT EXHAUST SLEEVE LEADING EDGE SKIN PEELED BACK AND DAMAGED FROM 2 O'CLOCK TO 7 O'CLOCK POSITION. REPAIRED AREA IAW SRM 54-30-03.

Part: PANEL — WORN (LT TE FOREFLAP)

FOUND HOLE IN LEFT HAND OUTBOARD FOREFLAP LEADING EDGE, OUTBOARD END. REPAIRED DAMAGE IAW SRM 51-40-09.

Part: PANEL — DISBONDING (LT TE FOREFLAP)

FOUND LEFT HAND OUTBOARD FOREFLAP UPPER SURFACE REPAIR DISBONDING ABOVE NR 1 FLAP TRACK. REPAIRED DAMAGED AREA IAW SRM 51-40-06.

Part: PANEL — PUNCTURED (LEFT WING LE)

FOUND HOLE IN LEFT WING LEADING EDGE, LOWER SURFACE AT OUTBOARD HINGE OF VARIABLE CAMBER FLAP. REPAIRED IAW SRM 51-24-11.

Part: ATTACH BRACKET — CRACKED (NR 4 PRECOOLER)

FOUND NR 4 ENGINE LEFT HAND PRECOOLER TOP ATTACH BRACKET CRACKED. REMOVED BROKEN BRACKET AND BUSHINGS IAW MM 36-12-04. INSTALLED NEW BRACKET AND BUSHINGS IAW MM 36-12-04.

Part: PANEL — DAMAGED (RT TE FOREFLAP)

FOUND HOLE IN RIGHT HAND OUTBOARD FOREFLAP LEADING EDGE, OUTBOARD END. REPAIRED IAW SRM 51-40-09.

Part: PANEL — PUNCTURED (LT WING)

FOUND HOLE IN LEFT WING PANEL, FORWARD OF INBOARD AILERON, OUTBOARD OF NR 2 PYLON. REPAIRED IAW SRM 51-40-09.

Part: LEFT SQUIB — NO TEST (NR 2 ENGINE)

NR 2 ENGINE LEFT HAND SQUIB WOULD NOT TEST. REPAIRED BROKEN WIRE, OPS CHECK GOOD IAW MM 26-10-00.

Part: SERVICE PANEL — CRACKED (NLG)

FOUND NOSE LANDING GEAR SERVICE PANEL CRACKED ALONG LOWER EDGE. SANDED DAMAGED AREA, APPLIED FIBERGLASS REPAIR IAW SRM 51-40-08.

Part: SKIN — CRACKED (NR 4 CORE COWL)

NR 4 OUTBOARD CORE COWL TOP AFT INSIDE SKIN CRACKED DUE TO EXCESSIVE HEAT. INSTALLED REPAIR DOUBLER IAW SRM 54-30-02.

Part: PANEL — WORN (LT TE MIDFLAP)

FOUND HOLE WORN IN LEFT HAND OUTBOARD MIDFLAP LEADING EDGE, OUTBOARD END. REPAIRED DAMAGE IAW SRM 51-40-09.

Part: FLOOR PANEL — DAMAGED (BS 1720-1740)

FOUND FLOOR DAMAGED ON MAIN CARGO DECK STA 1720-1740 LT. REMOVED AND REPLACED FLOOR PANELS IAW SRM 51-32-01.

Part: TE PANEL — DELAMINATED (LT WING)

FOUND LEFT WING TRAILING EDGE PANEL DELAMINATED AT OUTBOARD END OF INBOARD FLAP WELL. APPLIED FIBERGLASS REPAIR IAW SRM 51-40-15.

Part: EXH SLEEVE SKIN — CRACKED (NR 4 ENGINE)

FOUND NR 4 ENGINE EXHAUST SLEEVE EXTERNAL LEADING EDGE SKIN PULLED BACK, CRACKED AND PARTLY MISSING, RIGHT SIDE. REMOVED DAMAGED SKIN IAW SRM 54-30-03. INSTALLED REPAIR PLATE IAW SRM 51-30-02. ENGINE TOTAL CYCLES, 16,359.

Part: ACCESS DOOR — PUNCTURED (FUELING PANEL)

FOUND HOLE IN FUELING PANEL ACCESS DOOR, RIGHT WING. SANDED DAMAGED AREA, REPAIRED IAW SRM 51-40-08.

Part: PANEL — DAMAGED (LT ELEVATOR)

FOUND LEFT HAND INBOARD ELEVATOR DAMAGED AT TRAILING EDGE. REMOVED DAMAGED AREA, REPAIRED IAW SRM 51-10-09.

Part: DUCT — CRACKED (LT WING)

ON PUSHBACK, NOTED WING LEADING EDGE OVERHEAT ON LEFT WING. WHEN ADP NR 1 WAS SELECTED, LIGHT WENT OUT. RETURNED TO BLOCKS. FOUND DUCT CRACKED AT BOSS FOR NR 2 PYLON BLEED AIR SENSE LINE, BOSS BLOWN OUT. REMOVED AND REPLACED DUCT ASSY, LEAK CHECK NORMAL PER MM 36-11-01. DUCT VERIFIED BY P/N TO BE IN COMPLIANCE WITH AD 91-06-08.

Part: REGULATOR — INOPERATIVE (COCKPIT)

SECOND OBSERVER'S O2 REGULATOR HAD NO FLOW. REMOVED AND REPLACED REGULATOR AS PER MM 35-11-07.

Part: CONTROL CABLE — WORN (RT AILERON)

DURING PRE-DEPARTURE CHECK, FOUND RIGHT WING GEAR SHELF AREA AILERON CONTROL CABLE FORWARD OF HYDRAULIC RETURN FILTER WORN BEYOND LIMITS. REMOVED AND REPLACED AB-10 CABLE PER MM 20-11-03. SWAGED NEW TERMINALS, INSTALLED, SAFETIED AND TENSIONED IAW MM 27-11-00.

Part: ACTUATOR — INOPERATIVE (RT AILERON)

ON TAXI OUT DURING CONTROL CHECK, RIGHT OUTBOARD AILERON WOULD NOT UNLOCK WITH FLAPS IN TAKEOFF RANGE. REMOVED AND REPLACED LOCK-OUT ACTUATOR IAW MM 27-11-16. OPS CHECK NORMAL.

Part: FLOW DIVIDER — MALFUNCTIONED (NR 2 ENGINE)

NUMBER 2 ENGINE SURGE BLEED VALVE STUCK OPEN AT FLIGHT LEVEL 39, EGT 100 DEGREES CELSIUS HOTTER THAN OTHER ENGINES AND FUEL FLOW 500 LBS HIGHER. REMOVED AND REPLACED ENGINE FLOW DIVIDER IAW MM 75-32-05. REMOVED AND REPLACED TT2 SENSOR IAW MM 73-21-04 AS PRECAUTIONARY. ENGINE RUNUP NORMAL IAW MM 71-00-00.

Part: POSITION IND — INOPERATIVE (TE FLAP)

TRAILING EDGE FLAPS SELECTED TO 30 DEGREES, THEY WOULD ONLY EXTEND TO 25 DEGREES. EXERCISED FLAP DOWN SWITCH FOR INBOARD FLAPS. REPLACED INBOARD FLAP POSITION INDICATOR AND SWITCH S938 ON FLAP POSITION LEVER. OPS CHECKS NORMAL IAW MM 27-51.

Part: TR UNIT — MALFUNCTIONED (NR 3 ENGINE)

NR 3 ENGINE OVERTEMPED IN REVERSE, EGT REACHED 920 DEGREES. VISUALLY INSPECTED ENGINE INTAKE AND TAILPIPE, NO DAMAGE FOUND. REVERSER DEACTIVATED, PENDING RABS SYSTEM CHECK AT JFK.

Part: CIRCUIT BREAKER — FAILED (COCKPIT)

AIRCRAFT RETURNED TO BLOCKS DUE TO FAILURE OF ALL RADIO/AIR DATA INSTRUMENTS ON CAPTAIN'S SIDE. FOUND ESSENTIAL RADIO BUS C/B OPEN, DUE TO HISTORY OF C/B OPENING REPLACED C/B. CHECKED SYSTEM PER MM 34-13-00 AND 24-50-02.

Part: PANEL — DELAMINATED (LT WING)

FOUND UPPER LEFT WING COMPOSITE PANEL AT ROOT DELAMINATED AT LEADING EDGE. REMOVED AND REPLACED PANEL IAW SRM 51-30-02.

Part: SKIN — DELAMINATED (RT ELEVATOR)

FOUND TEMPORARY COMPOSITE REPAIR DELAMINATED AT RIGHT OUTBOARD ELEVATOR INBOARD TRAILING EDGE. REMOVED AND REPLACED SKIN FROM RIGHT OUTBOARD ELEVATOR IAW SRM 51-40-12.

Part: NOSE COWL — DELAMINATED (NR 1 ENGINE)

FOUND NR 1 ENGINE NOSE COWL INLET ACOUSTICAL PANEL AT THE 8 O'CLOCK POSITION IS DELAMINATING AT THE CORNER OF OUTER PANEL. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 54-30-03 AND 51-10-01.

Part: SKIN — CORRODED (WS 300)

FOUND LOWER LEFT HAND WING SKIN WITH LEVEL ONE CORROSION AT APPROX STATION 300. REMOVED CORROSION IAW SRM 51-10-01.

Part: SKIN — CORRODED (WS 300)

FOUND LEVEL ONE CORROSION ON LOWER LEFT WING SKIN AT APPROX STATION 300. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS.

Part: CONTROL BOX — FAILED (ANTI SKID SYST)

DEPARTING KHV, TOWER ADVISED RUBBER LEFT ON RUNWAY. ON ARRIVAL ANC, DISCOVERED NR 11 TIRE BLOWN, HOLE IN WING-BODY FAIRING, 18 OF CONDUIT MISSING FROM RT BG STRUT. REPLACED ANTI-SKID BOX DUE TO FAILED BITE CHECK IAW MM 32-42-00, 3 TIRES IAW MM 32-45-01. PERFORMED INTERIM REPAIR ON PANEL IAW MA5350-02:01.

Part: ENGINE — BIRD STRIKE (NR 3)

AT 7500 FEET WHILE BEING VECTORED FOR APPROACH AT NIGHT ENCOUNTERED BIRD FLOCK, HAD MULTIPLE BIRD STRIKES. WEATHER CONDITIONS, SCATTERED BROKEN LAYERS. NO ABNORMAL ENGINE OR FLIGHT INSTRUMENT INDICATIONS NOTED, NORMAL APPROACH AND LANDING FOLLOWING BIRD STRIKE. ON INSPECTION, FOUND NR 3 ENGINE DAMAGED BEYOND LIMITS, REPLACED SAME IAW PAC WORKCARDS M7100-002, M7100-002A. FOUND NR 4 NOSE COWL DAMAGED, REPLACED IAW 71-11-01. REPAIRED DAMAGE TO SECTION 41 RIBS IAW 53-12, REPAIRED DAMAGE TO WING L/E IAW 57-31.

Part: RETRACT MECH — MALFUNCTIONED (RT NLG DOOR)

ON DEPARTURE FROM ANC AFTER GEAR RETRACTION, RIGHT WING GEAR DOOR REMAINED OPEN AND GEAR REMAINED EXTENDED AS CONFIRMED BY BOTH PRIMARY/ALTERNATE INDICATION SYSTEMS. DUMPED FUEL TO MAX LANDING WEIGHT, RETURNED TO DEPARTURE AIRPORT. CHECKED RIG OF DOOR SEQUENCE VALVE, OPS CHECK GOOD. LUBED GEAR AND C/W GEAR SWING, ALL CHECKED NORMAL. COULD NOT DUPLICATE ON GROUND.

Part: CHIP DETECTOR — CRACKED (NR 2 ENGINE)

NR 2 ENGINE OIL QUANTITY DROPPED TO ZERO FOLLOWED BY A PRESSURE FLUCTUATION. PRECAUTIONARY ENGINE SHUTDOWN COMPLIED WITH, 35 PSI AFTER SHUTDOWN. PERFORMED WINDMILLING INSP PER MM 72-00-00, PERFORMED LEAK CHECK PER MM 71-00-44. FOUND CHIP DETECTOR CRACKED, REPLACED SAME. CHECKED PER 72-61-00, INSPECTED CHIP DETECTORS PER MM 72-61-00, VISUAL INSPECTION FOUND ACCEPTABLE.

Part: OIL SYST — FAILED (ENGINE)

AT TOP OF CLIMB, OIL QTY INDICATION WAS 3.9 GALS, TIME 2359Z AND AT 0025Z QTY WAS 3.5 GALS. RAN THE ENGINE OIL QTY LOW CHECKLIST, AT 0100 OIL QTY WAS 2.8 GALS. RETURNED TO ANC, LANDED WITH .2 GAL INDICATING, HAD GOOD TEMP AND PRESSURE AT ALL TIMES. REPLACED ENGINE.

Part: FUEL GAUGE — MALFUNCTIONED (NR 2)

MAO-GRU - DURING CLIMBOUT, NR 2 FUEL QUANTITY GAUGE DECREASED FROM 26,000 LBS TO 8,800 LBS IN A 10 MINUTE PERIOD. THE NR 2 BOOST PUMPS WERE TURNED OFF AND NR 2 ENGINE CROSSFED FROM OTHER TANKS AND QUANTITY CONTINUED TO DECREASE TO 4,800 LBS. SUSPECTED FUEL LEAK AND RETURNED TO MAO. COMPARED ARRIVAL FUEL TO STICK READINGS, NO ERROR. CHECKED FOR FUEL LEAKS, NO SIGN OF FUEL LEAK DURING PRESS CHECK OF FUEL SYSTEMS. REFUELED AIRCRAFT, RECHECKED STICK READINGS, DISPATCHED AIRCRAFT.

Part: STARTER — FAILED (NR 4 ENGINE)

ORD - ON TAXI, NR 4 ENGINE STARTER LIGHT CAME ON. SHUTDOWN ENGINE AND CLOSED BLEED VALVE. FOUND STARTER FAILED, SHEARED COUPLER AND BLOWN DUCT. REPLACED DAMAGED UNITS AND STARTER SHUTOFF VALVE.

Part: BRACKET — CRACKED (LEFT WING)

FOUND NR 4 LEADING EDGE DRIVE FWD SUPPORT BRACKET HAS TWO CRACKS IN RADIUS NEAR INBOARD ATTACH BRACKET, STA 1400 LEFT WING. REPAIRED AS PER SRM 51-40-03.