N13ZV

ATA 7314

Part: PUMP — LEAKING (FUEL SYSTEM)

AFTER ARRIVAL, CREW FOUND FUEL LEAK IN THE LT NACELLE AREA. REMOVED AND REPLACED LOW PRESSURE FUEL PUMP (PUMP, FUEL BOOST-LOW PRESS ENGINE D) P/N 143890425, S/N B-314.

ATA 3442

Part: CONNECTOR — DIRTY (WX RADAR SYS) · airframe 23,114 hrs · 35,742 cycles

UPON TAKEOFF ON FLIGHT 5576 THE WEATHER RADAR FAILED. THE CREW RETURNED TO THE FIELD WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND RESEATED THE ANTENNA CONNECTOR. NO PARTS WERE USED THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED.

ATA 5411

Part: SPAR CAP — CHAFED (NACELLE) · airframe 22,666 hrs · 35,125 cycles

UPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT LOWER SPAR CAP WAS CHAFFING. BLENDED OUT THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.

ATA 2910

Part: MOTOR — FAILED (HYD POWER PACK) · airframe 21,762 hrs · 33,993 cycles

ON AN ATTEMPT TO LAND, THE CREW TRIED TO EXTEND LANDING GEAR, BUT THE CIRCUIT BREAKER POPPED. THEY RESET CIRCUIT BEAKER ND LANDING GEAR STILL WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY EXTENSION. RECEIVED 3 GREEN GEAR DOWN INDICATORS. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED A HYDRAULIC POWER PACK MOTOR ASSEMBLY. THE TEARDOWN REPORT THAT WAS RECEIVED FROM THE VENDOR REPORTED THAT THE BRUSHES AND BEARINGS WERE WORN AND THE COMMUTATOR SCORED. THE VENDOR REPLACED THE BRUSHES AND BEARINGS.THEN THE COMMUTATOR WAS FIXED. THIS PART WAS OVERHAULED AND TESTED.

ATA 5210

Part: CABLE — BROKEN (PAX DOOR)

UPON ARRIVAL, A RAMPER PROCEEDED TO OPEN PASSENGER DOOR. THE RAMPER BACKED AWAY FROM THE DOOR AND THE DOOR PROCEEDED TO FREE FALL BREAKING THE SUPPORT ANCHOR BRACKETS. THE DOOR SNUBBER CABLE WAS DEFERRED. THE CORRECTIVE ACTION WAS THAT THE CABLE ASSEMBLY WAS REPLACED.

ATA 2910

Part: POWERPACK — FAILED (HYD SYSTEM)

LANDING GEAR FAILED TO EXTEND ON APPROACH, AND LANDING INTO PIT. THE CREW EXTENDED THE GEAR THROUGH EMERGENCY MEANS, AND LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC POWER PACK, AND HYDRAULIC POWER ELECTRICAL RELAY, JACKED AND CYCLED GEAR WITH NO PROBLEMS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

ATA 7110

Part: COWLING — LOOSE (RT NACELLE)

FLT 5425 - ACY-BWI - AFTER DEPARTURE, CREW OBSERVED THE RIGHT UPPER COWLING WAS LOOSE. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. THE COWLING WAS RESECURED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

ATA 7920

Part: OIL LINE — CHAFED (NR 1 ENGINE)

FLT 5596 - AVP-BOS - NR 1 ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. CREW SHUT DOWN ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED IN BOS WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL COOLER LINE. AIRCRAFT AS RETURNED TO SERVICE. (M)

ATA 5520

Part: BRACKETS — CORRODED (ELEVATOR)

DURING A FLEET CAMPAIGN DIRECTIVE INSPECTION, BOTH LEFT AND RIGHT OUTBOARD ELEVATOR ATTACH BRACKETS WERE FOUND TO HAVE INTERGRANULAR CORROSION. MAINTENANCE REMOVED AND REPLACED BOTH ATTACH BRACKETS, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

ATA 5753

Part: ATTACH BRACKET — EXCESS WEAR (RT FLAP)

FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. AFFECTED COMPONENTS P/NS ARE BRACKET, LT INBD AND RT INBD, INBD HINGE, PN 35-165050-31. BRACKET, LT LTBD AND RT INBD, INBD HINGE, PN 35-165050-30. BRACKET, LT INBD AND RT OTBD, OTBD HINGE, PN 35-165050-35. BRACKET, LT OTBD AND RT INBD, OTBD HINGE, PN 35-165050-34. AFT BEARING ASSY, PN 114-521039-1. REF: CONTROL NR MASA97045. PART CYCLES, 5,707. ACFT TC, 19,058.

ATA 5753

Part: ATTACH BRACKET — EXCESS WEAR (LT FLAP)

FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. AFFECTED COMPONENTS P/NS ARE BRACKET, LT INBD AND RT INBD, INBD HINGE, PN 35-165050-31. BRACKET, LT LTBD AND RT INBD, INBD HINGE, PN 35-165050-30. BRACKET, LT INBD AND RT OTBD, OTBD HINGE, PN 35-165050-35. BRACKET, LT OTBD AND RT INBD, OTBD HINGE, PN 35-165050-34. AFT BEARING ASSY, PN 114-521039-1. REF: CONTROL NR MASA97045. PART CYCLES, 2,253. ACFT TC, 19,058.