N142ZV
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.
24 reports on file, 1997-07-11 – 2007-12-06.
Part: BATTERY — DISCHARGED (MAIN) · airframe 23,274 hrs · 34,641 cycles
BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY.
Part: BATTERY — DISCHARGED (MASTER) · airframe 23,167 hrs · 34,486 cycles
DURING FLIGHT, THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY.
Part: BATTERY — WEAK (MASTER) · airframe 22,538 hrs · 33,426 cycles
DURING FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CONTINUED TO DESTINATION WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP UP IS A NUISANCE WRITEUP WITH SEVERE DISTRACTION TO THE AIR CREW.REMOVED AND REPLACED BATTERY AND ADJUSTED VOLTAGE REGULATOR
Part: SKIN — CHAFED (RT NACELLE) · airframe 22,220 hrs · 32,929 cycles
FRICTION CHAFFING OCCURED DURING ENGINE OPERATION RESULTING IN WORN SEGMENTS ON THE RT ENGINE UPPER AFT NACELLE ALONG ENTIRE LENGTH & SHAPE OF NACELLE. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-1 REV 1R.
Part: STIFFENER — CORRODED (LWS 124) · airframe 22,220 hrs · 32,929 cycles
BIO CORROSION DAMAGE IN LT MAIN TANK NACELLE. RIB REPAIR WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-3
Part: SKIN — CHAFED (LT NACLELLE) · airframe 22,220 hrs · 32,929 cycles
FRICTION CHAFFING OCCURED DURING ENGINE OPERATION RESULTING IN WORN SEGMENTS ON THE LT ENGINE UPPER AFT NACELLE ALONG ENTIRE LENGHT & SHAPE OF NACELLE. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-1 REV 1R.
Part: SPAR CAP — CORRODED (WING) · corrosion level 3 · airframe 22,220 hrs · 32,929 cycles
BIO - CORROSION RT LOWER SPAR CAP AT WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-7 REV 1R.
Part: SPAR CAP — CORRODED (ZONE 600) · corrosion level 3 · airframe 22,220 hrs · 32,929 cycles
BIO - CORROSION DAMAGE RT LOWER SPAR CAP AT WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-7 REV 1R.
Part: FRAME — CHAFED (BS 228-378) · airframe 22,220 hrs · 32,929 cycles
AT MULTIPLE FUSELAGE STATIONS FRICTION CHAFING HAS OCCURED, THE DEPTH OF THE CHAFFING RANGES FROM .019 TO .030. REPAIRED IAW ENGINEERING AUTHENTICATION REPAIR DRAWING 1900D142-6 REVA
Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 22,073 hrs · 32,705 cycles
DURING CLIMBOUT, CARGO DOOR ANNUN ILLUM, A/C RETURNED TO FIELD WITH NO FURTHER INCIDENT.ADJUSTED SWITCH.
Earlier reports · 1997–2005 · 14 reports
2005
Part: DISPLAY — FAILED (COCKPIT) · airframe 19,356 hrs · 28,711 cycles
CAPT EHSI WENT BLANK AND CREW SMELLED AN ODOR THEY DETERMINED IT TO BE ELECTRICAL RELATED. AIRCRAFT LANDED WITH NO FUTHER INCIDENT. MAINTENANCE REPAIRED WIRES. NO PARTS WERE USED.
Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 17,964 hrs · 26,659 cycles
IN CRUISE, CARGO DOOR ANNUNCIATOR ILLUMINATED. RAN APPROPRIATE EMERGENCY CHECKLIST. DECLARED EMERGENCY WITH PHX/ABQ CENTER. LANDED AT PHX WITH NO INJURY TO AIRCRAFT OR PASSENGERS. SYSTEM MEL'D. MAINTENANCE ADJUSTED CARGO DOOR JAM SWITCH.
2004
Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 16,897 hrs · 25,008 cycles
CAPT ADVISED FMN OPS THAT THE CAPT SIDE NAV WAS NOT DISPLAYING NAV DATA, CAPT ADVISED BY MX CTL TO RETURN TO FIELD FMN. A/C LANDED FMN WITH NO FURTHER INCIDENT. COULDN'T DUPLICATE DISCREPANCY, OPS CK NORMAL
Part: ANNUNCIATOR — MALFUNCTIONED (INSTRUMENT PANEL) · airframe 16,763 hrs · 24,814 cycles
IN FLIGHT, CREW NOTICED SEVERAL ANNUNC ILLUM AND EXTINGUISHED WITH AN ELECTRICAL SMELL IN COCKPIT. ON LANDING THE RT PROP WENT INTO FEATHER. A/C LANDED WITHOUT FURTHER INCIDENT. NO FUMES NOTED INS CB PANELS, INSTRUMENT PANEL.
Part: WHEEL — DAMAGED (NLG) · airframe 16,716 hrs · 24,737 cycles
UPON APPROACH HII, GEAR WOULD NOT EXTEND ON FIRST ATTEMPT. CREW RESET GEAR RELAY2 AMP C/B AND GEAR EXTENDED. AIRCRAFT LANDED AND TAXIED TO GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE WHEEL ASSY.
Part: WARNING HORN — ACTIVATED (STALL WARNING) · airframe 16,716 hrs · 24,737 cycles
DURING TAKEOFF ROLL STALL WARNING HORN STARTED SOUNDING. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. JACKED AC, CYCLED GEAR 5 TIMES CND ON GND.
Part: VANE — DIRTY (STALL WARNING) · airframe 16,610 hrs · 24,575 cycles
ON TAKEOFF ROLL AT V1,VR STALL WARNING HORN CAME ON AND SOUNDED CONTINUOUSLY AND DID NOT SHUT OFF. CREW ELECTED TO RETURN TO DEPARTURE. AIRCRAFT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. CLEANED STALL VANE, OPS CK NORMAL.
Part: SCREW — LOOSE (AIRSTAIR DOOR) · airframe 16,247 hrs · 24,072 cycles
AT DFW AIRSTAIR DOOR WILL NOT CLOSE SECURE. NO FURTHER INCIDENT. RESECURED LOOSE SCREWS ON COVER PLATES.
2003
Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 14,573 hrs · 21,688 cycles
ON FLIGHT 700 FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO, DURING THE TAKEOFF ROLL STALL WARNING WENT OFF AND WOULD NOT RESET. THE AIRCRAFT WAS RETURNED TO GATE WITH NO FURTHER INCIDENT. THE CREW WAS THEN GIVEN AIRCRAFT 3199Q TO COVER THE LINE. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY EVEN AFTER A TEST FLIGHT. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED.
Part: SPAR CAP — CHAFED (NACELLE) · airframe 13,572 hrs · 20,356 cycles
UPON A DETAILED INSPECTION MAINTENANCE FOUND THAT THE LEFT AND RIGHT LOWER SPAR CAP BEHIND NACELLE INNER WAS CHAFED. BLENDED BOTH OF THE LOWER SPAR CAPS IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JMP/0209-03. NO TEARDOWN REPORT WILL BE REQUIRED.
2002
Part: HANDLE — FAILED (MLG SELECTOR) · airframe 12,964 hrs · 19,517 cycles
AFTER THE DEPARTURE FROM ROSWELL, NEW MEXICO TO ALBUQUERQUE NEW MEXICO ON FLIGHT 415, THE LANDING GEAR FAILED TO RETRACT. THERE WAS NO ABNORMAL INDICATIONS IN THE COCKPIT.THE AIRCRAFT CONTINUED ON ITS FLIGHT TO ALBUQUERQUE AND LANDED WITH NO FURTHER INCIDENT. THE ALBUQUERQUE MAINTENANCE FOUND THE LANDING GEAR HANLDE HAD FAILED. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE LANDING GEAR HANDLE. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. THE TEARDOWN REPORT HAS BEEN RECEIVED ON 11/18/02. THE REPORT STATES THAT THE UNIT REQUIRES THE REPLACEMENT OF TWO SWITCHES.
1998
Part: EHSI — FAILED (RT COCKPIT)
FLT 5337 - LEB-PHL - AFTER DEPARTURE, CAPTAIN REPORTED THAT THE F/O'S EHSI TUBE BLANKED OUT AND HE NOTED AN ELECTRICAL SMOKE SMELL IN COCKPIT. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S EHSI TUBE, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE.. (M)
1997
Part: RT UNIT — INTERNAL FAILURE (AVIONICS BAY)
AIRSHUTTLE 5358 - ITH-PHL - AFTER TAKEOFF, CREW NOTICED SMOKE COMING FROM ANNUNCIATOR PANEL AREA. CREW RETURNED TO FIELD. MAINTENANCE INSPECTED AND FOUND NR 2 COMM CONTROL HEAD SHORTED OUT. AIRCRAFT WAS FERRIED TO PHI FOR REPLACEMENT. UPON BEING RETURNED TO SERVICE, THE CREW POWERED UP THE AVIONICS AND AGAIN SAW SMOKE COMING FROM THE NR 2 COMM CONTROL. AIRCRAFT WAS FERRIED TO RDG, WHERE MAINTENANCE REPLACED THE RECEIVER TRANSMITTER UNIT. 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, 7,235. ACFT TC, 7,235.