N23YV

Part: RIB — CRACKED (VERTICAL STAB) · airframe 20,868 hrs · 29,524 cycles

WHILE PERFORMING AND INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 54.026 WAS FOUND CRACKED IN TWO PLACES ON THE RIGHT SIDE NEAR THE FWD, CENTER STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 20,868 hrs · 29,524 cycles

WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED AT FWD CENTER STRINGER INTERSECTION. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE BMM P/N 114-590021-9, 51-70-03.

Part: PLATE — CHAFED (FUSELAGE) · airframe 21,949 hrs · 30,683 cycles

WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE RIGHT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFE.

Part: RIVET — CHAFED (FUSELAGE) · airframe 21,949 hrs · 30,683 cycles

WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE LEFT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 21,949 hrs · 30,683 cycles

WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, SKIN UNDER STRINGER 10R WAS FOUND CRACKED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 21,949 hrs · 30,683 cycles

WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, STRINGER 13R WAS FOUND TO HAVE A CRACKED CLIP.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 23,544 hrs · 34,476 cycles

WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED IN TWO PLACES ON THE RIGHT SIDE BY THE FOWARD AND AFT STRINGER INTERSECTION. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 21,949 hrs · 30,683 cycles

WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED ON THE LEFT SIDE NEAR THE FWD STRINGER INTERSECTION. REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.

Part: EMERGENCY DOOR — MIS-ALIGNED (FUSELAGE)

FLT 5320 - FLL-TPA - DURIG PRE-FLIGHT WALK AROUND, CREW NOTICED THAT THE RIGHT REAR EMERGENCY EXIT EXTERIOR HANDLE WAS NOT FLUSH WITH THE DOOR. MAINTENANCE REMOVED AND REINSTALLED THE DOOR. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STOP — OUT OF ADJUST (RT EMERG EXIT)

DURING ROUTINE INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR NOT FLUSH WITH EXTERIOR SURFACE. MAINTENANCE RERIGGED DOOR STOPS. PRESSURE CHECKED, OPS CHECK GOOD. (M)

Part: WIRE — BROKEN (CENTER CONSOLE)

AIRSHUTTLE 5308 - GNV-MIA - ON LANDING, THE NR 1 COMM WENT BLAND AND EMITTED SMOKE. THE RADIO WAS SWITCHED TO OFF AND THE SMOKE STOPPED. MAINTENANCE FOUND A SHORTED WIRE BETWEEN THE AUDIO SELECT PANEL AND THE NR 1 COMM. REMOVED AND REPLACED THE NR 1 COMM CONTROL HEAD, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

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, 6,753. ACFT TC, 17,456.

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, 8,353. ACFT TC, 17,456.

Part: SUN GEAR — FAILED (POWER SECTION)

POWER SECTION FAILURE WAS CAUSED BY THE SUN GEAR FAILURE. THE SUN GEAR, CARRIER, CARRIER GEARS, PT SHAFT, AND THE RING GEAR WERE SENT TO PW & C FOR INVESTIGATION.