N42YV
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
7 reports on file, 1995-08-02 – 1997-07-11.
Part: BEARING — 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, 11,548. ACFT TC, 16,591.
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, 11,674. ACFT TC, 16,591.
Part: ACTUATOR — LEAKING (RT MLG)
TEX/DEN - FLT 7601 - AFTER DEPARTURE FROM TEX UPON GEAR RETRACTION, THE GEAR UNSAFE LIGHT ILLUMINATED AND THE 3 GREEN EXTINGUISHED. THE CREW CYCLED THE GEAR AND THE NOSE INDICATION REMAINED ILLUMINATED. THE CREW PUMPED THE GEAR DOWN AND THE 3 GREEN ILLUMINATED SHOWING THE GEAR DOWN AND LOCKED. THE CREW IN COORDINATION WITH MAINTENANCE CONTROL DIVERTED TO FMN FOR MAINTENANCE. MAINTENANCE FOUND THE RT SIDE ACTUATOR LEAKING HEAVILY AND REPLACED THE ACTUATOR, OPS CHK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (X)
Part: ACTUATOR — LEAKING (LT MLG)
AIR SHUTTLE 7709 - DEN-COD, ON APPROACH INTO COD, LT MAIN GEAR EXTENDED UNCOMMANDED. THE CIRCUIT BREAKER POPPED AND THE GEAR WAS THEN MANUALLY EXTENDED UNTIL THREE GREEN DOWNLOCK INDICATORS WERE ACHIEVED. FOUND ACTUATOR TO BE LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED ACTUATOR. PERFORMED GEAR EXTENSION/RETRACTION ON JACKS SUCCESSFULLY. AIRCRAFT RETURNED TO SERVICE. (M)
Part: P3 LINE — BROKEN (RT ENGINE)
CVN/ABQ - FLT 107 - DURING FLIGHT, THE N1 AND FUEL FLOW DROPPED TO NEAR ZERO. THE FLIGHT CREW SHUT DOWN THE NR 2 ENGINE AS A PRECAUTIONARY MEASURE. THE CREW PROCEEDED TO ABQ WHERE THEY DECLARED AN EMERGENCY LANDING. AIRCRAFT LANDED IN ABQ WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED BROKEN P3 LINE AT FCU. ENGINE RUN-UP PERFORMED SATISFACTORILY AND AIRCRAFT RETURNED TO SERVICE. (X)
Part: POWER LEVER SW — OUT OF ADJUST (QUADRANT)
FLT 7587 - MTJ - LEFT ENGINE AUTOFEATHERED BRIEFLY ON DESCENT, LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED POWER LEVER SWITCHES. (M)
Part: AIR SENSE LINE — FAILED (RT ENGINE)
LAX/SMX - AIRCRAFT DEPARTED. APPROXIMATELY 10 MINUTES INTO FLIGHT AT 10,000 FEET, RT ENGINE STARTED TO SURGE IN POWER AND TORQUE DROPPED TO ZERO WITHIN 10 SECONDS. ALL OTHER PARAMETERS NORMAL. FLIGHT CREW SECURED RIGHT ENGINE AND DIVERTED TO BFL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED RT ENGINE AND FOUND P4 LINE TO P3 FILTER BROKEN. INSTALLED NEW P4 LINE. PERFORMED GROUND RUN AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)