N436YV
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
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.
58 reports on file, 1997-05-05 – 2012-02-28.
Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 34,878 hrs · 34,372 cycles
BAG SMOKE WARNING. MX INSPECTED AND NO DEFECTS WERE NOTED.
Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 34,714 hrs · 34,215 cycles
AIRCRAFT EXPERIENCED NR 2 HYDRAULIC SYSTEM FLUID LOSS AFTER DEPARTURE FROM GYM EN ROUTE TO PHX. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD. CURRENTLY AWAITING ARRIVAL OF CONTACT MAINTENANCE TO TROUBLESHOOT AND ISOLATE SOURCE OF LEAK. R&R HYDRAULIC LINE. GEAR SWING AND LEAK CHECK.
Earlier reports · 1997–2011 · 56 reports
2011
Part: BUTTON — STUCK (CABIN) · airframe 34,515 hrs · 34,036 cycles
FLIGHT ATTENDANT PA BUTTON STUCK. CLEANED BUTTON.
Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 34,254 hrs · 33,772 cycles
FLIGHT DECK FLASHLIGHT MISSING. R2 FLASHLIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,841 hrs · 33,328 cycles
FLOOR TRACK LIGHTING DAMAGED AT ROW 7 & 8; R2 FLOOR TRACK LIGHTING.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,781 hrs · 33,258 cycles
LEFT FWD EGRESS LIGHT INOP. R2 E-LIGHT POWER SUPPLY.
Part: STRUT — UNKNOWN (PAX DOOR) · airframe 33,737 hrs · 33,217 cycles
PAX DOOR GAS STRUTS REQ CHANGED. PER MX GAS STRUTS ARE SERVICEABLE.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,645 hrs · 33,116 cycles
LEFT FWD EXTERIOR E-LIGHT INOP. RELAMPED EMERGENCY LIGHT.
Part: OIL COOLER — DEFECTIVE (NR 1) · airframe 33,633 hrs · 33,107 cycles
ABNORMAL PWR NR 1 ENG OIL TEMP 120 C. R2 OIL COOLER.
Part: ROLLER — MISSING (CARGO DOOR) · airframe 34,307 hrs · 34,849 cycles
CARGO DOOR LWR FWD ROLLER MISSING. INSTALLED ROLLER.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 33,054 hrs · 32,556 cycles
NR 2 T-HANDLE FIRE WARNING INDICATOR INOP. R2 HANDLE LAMP ASSY.
Part: POTENTIOMETER — MALFUNCTIONED (AILERON TRIM) · airframe 33,007 hrs · 32,510 cycles
NO FULL DEFLECT LWD AILERON TRIM. R2 TRIM TAB POTENTIOMETER.
Part: BRAKE — DRAGGING (MLG) · airframe 33,001 hrs · 32,506 cycles
BRAKES DRAGGING. R2 NR 3 & 4 BRAKES.
Part: STATIC WICK — BROKEN (ELEVATOR) · airframe 32,965 hrs · 32,472 cycles
LT ELEVATOR STATIC WICK BROKEN. R2 STATIC WICK.
Part: FLOW DIVIDER — LEAKING (NR 2 ENGINE) · airframe 32,908 hrs · 32,422 cycles
FUEL DRIPPING FROM GANG DRAIN AT NR 2 ENGINE. R2 FLOW DIVIDER.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,842 hrs · 32,360 cycles
F/A'S FLASHLIGHT INOP. MX REPLACED BATTERY.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,842 hrs · 32,360 cycles
UPPER AIRSTAIR DOOR LIGHT INOP. MX RELAMPED, OPS CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 32,842 hrs · 32,360 cycles
FWD OVERHEAD E-LIGHT INOP. MX REMOVED AND REPLACED E-LIGHT BATTERY, OPS TEST GOOD.
Part: BRAKE — LEAKING (MLG) · airframe 33,839 hrs · 34,386 cycles
NR 2 BRAKE LEAKING. MX REMOVED AND REPLACED BRAKE.
Part: ACTUATOR — FAULTY (NR 2 PROPELLER) · airframe 33,839 hrs · 34,386 cycles
NR 2 PROP SLOW TO COME OUT OF FEATHER. MX REMOVED AND REPLACED PROP ACTUATOR.
Part: ROD — BROKEN (MAIN DOOR) · airframe 32,620 hrs · 32,172 cycles
MAIN DOOR AFT HANDRAIL ROD BROKEN. MX REPLACED HANDRAIL ROD, OPS NORMAL.
2010
Part: BRAKE ASSY — LOOSE (NR 1) · airframe 32,228 hrs · 31,805 cycles
NR 1 BRAKE ASSY LOOSE. MX REPLACED BRAKE.
Part: B-NUT — LOOSE (NR 1 ENGINE) · airframe 31,755 hrs · 31,313 cycles
FUEL LEAK NR 1 ENG ON A-15 LEAK CHECK. MX TIGHTENED B-NUT ON WASTE FUEL RETURN LINE ON NR 1 ENG LEAK CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 31,455 hrs · 30,991 cycles
DEAD EMERGENCY LIGHT BATTERY. MX R&R EMERGENCY LIGHT BATTERY OPS GOOD.
2008
Part: ROD — BROKEN (PAX DOOR)
ASH FLT 7098 - ASE-DEN - PASSENGER DOOR FWD SUPPORT ROD BROKEN. MAINTENANCE REMOVED AND REPLACED STRUT. OPS CHECK GOOD. (S)
Part: PRESSURE VALVE — MALFUNCTIONED (DOOR SEAL) · airframe 27,244 hrs · 26,252 cycles
FLT 7075 - PASSENGER DOOR HARD TO OPEN. INFLATABLE DOOR SEAL NOT DEFLATING PROPLERLY. REPLACED PRESSURE VALVE, ELBOWS, AND TUBING. OPS CHECKED GOOD.
2007
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,984 hrs · 25,953 cycles
ASH FLT 7150 COD - PILOT REPORTED A RAPID DEPRESSURIZATION WITH O2 MASK DROP IN FLIGHT. REPLACED THE CABIN PRESSURE CONTROLLER
Part: CONTROL UNIT — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 26,025 hrs · 24,806 cycles
ASH 7106 DEN - EMERGENCY EXIT LIGHTS WILL NOT TURN ON FROM F/A'S PANEL. MX REPLACED THE PANEL CONTROL UNIT.
Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 25,404 hrs · 24,031 cycles
ASH 7059 DEN - BAGGAGE COMPARTMENT SMOKE LIGHT ILLUMINATED ON GROUND. MX REMOVED AND REPLACED FWD SMOKE DETECTOR.
2006
Part: CIRCUIT BREAKER — TRIPPED (STALL WARNING) · airframe 24,152 hrs · 22,491 cycles
ASH 7079 GJT - LT AND RT STALL WARNING CAUTION LIGHT. MX RESET C/B.
Part: POTENTIOMETER — OUT OF ADJUST (AILERON TRIM) · airframe 24,058 hrs · 22,377 cycles
ASH 7039 DEN - AILERON TRIM REQUIRES FULL LEFT WING DOWN FOR LEVEL FLIGHT. THE AILERON POTENTIOMETER WAS ADJUSTED AND THE SYSTEM OPERATED NORMALLY.
Part: HOSE — LEAKING (HYD SYSTEM) · airframe 23,622 hrs · 21,850 cycles
LOSS OF NR 1 AND NR 2 HYD QTY AND PRESSURE DUE TO LEAK AT LT MLG. MAINTENANCE REMOVED AND REPLACED FLEX LINE AND SERVICED HYD.
Part: LAMP — INOPERATIVE (NLG INDICATOR) · airframe 23,340 hrs · 21,524 cycles
ASH 7066 DEN - NLG DOWN LOCK LIGHT NOT ILLUMINATED. MAINTENANCE RELAMPED THE NLG DOWN SWITCH LIGHT.
2004
Part: WINDSHIELD — SPARKS (COCKPIT) · airframe 20,635 hrs · 18,592 cycles
AIRCRAFT DIVERTED TO GJT DUE TO THE FIRST OFFICERS WINDSHIELD HEAT CAUSING SMOKE IN THE FLIGHT DECK. AIRCRAFT IS CURRENTLY AOG FOR A WINDSHIELD, SDR OPEN FOR FURTHER INVESTIGATION. 10/29 MX REPLACED WINDSHIELD.
2001
Part: LIGHT — INOPERATIVE (CABIN)
FLT 6333 - AN EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE DETERMINED THE BULB WAS UNSERVICEABLE. THE BULB WAS REMOVED AND REPLACED AND OPS CHECKED GOOD. (M)
2000
Part: LIGHT — BROKEN (CABIN)
FOUND NR 2 TRACK LIGHT PLASTIC HOUSING BROKEN DURNIG A ROUTINE INSPECTION. MAINTENANCE REMOVED AND REPLACED NR 2 TRACK LIGHT ASSEMBLY. OPS CHECK GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6333 - BFL-PHX - THE PILOT REPORTED THAT THE MID CABIN OVERHEAD EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED 6 BATTERY PACKS. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M)
Part: POWER SUPPLY — FAILED (CABIN)
DURING AN A-17 LINE CHECK INSPECTION, SEVERAL EMERGENCY EXIT LIGHTS WERE NOT ILLUMINATION DURING TEST. THE NR 1 AND NR 3 EMERGENCY POWER SUPPLIES WERE FOUND TO BE INOPERATIVE. BOTH POWER SUPPLIES WERE REPLACED. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
1999
Part: LAMP — FAILED (EMERGENCY EXIT)
DURING A ROUTINE MAINTENANCE INSPECTION, MAINTENANCE PERSONNEL FOUND THE NR 3 OVERHEAD EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE REPLACED THE BURNED OUT BULBS, OPS CHECKED GOOD. (X)
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)
FLT 6348 - PSP-PHX - AFTER DEPARTURE FROM PSP, CREW REPORTED A CARGO BAY SMOKE DETECTOR ANNUNCIATOR ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO THE FIELD. NO EVIDENCE OF FIRE OR SMOKE WAS NOTED. MAINTENANCE REPLACED THE SMOKE DETECTOR. AIRCRAFT WAS RETURNED TO SERVICE. (M)
1998
Part: TRIM — MALFUNCTIONED (ELEVATOR)
FLT 5254 - DRO-PHX - AFTER DEPARTURE, CREW REPORTED UNABLE TO TRIM THE ELEVATOR AFTER REACHING FLIGHT ALTITUDE. THE CREW ELECTED TO RETURN TO DRO, AND EMERGENCY EQUIPMENT WAS REQUESTED BY THE CAPTAIN. ATC DECLARED AN EMERGENCY. AIRCRAFT LANDED IN DRO WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE SYSTEM COMPONENTS, NO DEFECTS WERE NOTED. MAINTENANCE PERFORMED IN OPERATIONAL SYSTEM CHECK, BUT COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERIES — DISCHARGED (COCKPIT)
DURING A ROUTINE MAINTENANCE CHECK, MAINTENANCE PERSONNEL FOUND THE PORTABLE EMERGENCY LIGHT TO BE DIM. MAINTENANCE REMOVED THE BATTERIES, DEEP CYCLED AND REINSTALLED THEM IN THE LIGHT ASSEMBLY. OPS CHECKED GOOD. (M)
Part: BULB — FAILED (CABIN)
DURING ROUTINE MAINTENANCE, FOUND 'NORMAL SWITCH EMERGENCY LIGHT AT FLIGHT ATTENDANT'S PANEL WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, OPS CHECK GOOD. (X)
Part: LAMP — FAILED (CABIN)
FLT 7529 - DRO-DEN - UPON ARRIVAL IN DEN, CREW NOTICED LEFT FORWARD EMERGENCY EXIT LIGHT INOP. MAINTENANCE RESET LAMP, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: CABLE — WORN (PAX DOOR)
FLT 7561 - SHR-DEN - UPON ARRIVAL IN DEN, THE AIRSTAIR DOOR WOULD NOT OPEN DUE TO THE CABLE BINDING. MAINTENANCE REMOVED AND REPLACED THE DOOR CABLE. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: CABLE — OUT OF ADJ (PAX DOOR)
FLT 7573 - GCC-SHR- AIRCRAFT LANDED IN SHR AND THE CREW HAD TROUBLE OPENING THE AIRSTAIR DOOR. MAINTENANCE LUBED CABLES AND PULLEYS. OPS CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BULB — FAILED (CABIN)
DURING LINE CHECK INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. (M)
1997
Part: BULB — FAILED (CABIN)
DURING MAINTENANCE INSPECTION, FOUND THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH WOULD NOT ILLUMINATE WHEN SELECTED ON. MAINTENANCE REMOVED AND REPLACED THE BULB IN THE SWITCH. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BULB — FAILED (COCKPIT)
FLT 7489 - CPR-DEN - CREW FOUND EMERGENCY OVERHEAD COCKPIT FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LAMP — FAILED (CABIN)
DURING ROUTINE LINE INSPECTION, RIGHT FORWARD EMERGENCY EXIT UPPER 'EXIT' SIGN WAS DIM. MAINTENANCE REMOVED AND REPLACED THE BULBS. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LENS — MISSING (CABIN)
DURING ROUTINE LINE INSPECTION, AFT EMERGENCY EXIT LOWER 'EXIT' SIGN WAS MISSING LENS. MAINTENANCE REPLACED THE LENS. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: CABLE — OUT OF ADJ (PAX DOOR)
FLT 7491 - CPR-DEN - CREW REPORTED THAT THE PASSENGER DOOR CABLE WOULD NOT ALLOW THE DOOR TO OPEN. DEN MAINTENANCE INSPECTED AND RIGGED THE DOOR CABLE. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — MALFUNCTIONED (CABIN)
AIRSHUTTLE - FLT 7538 - DEN-DRO - AFTER LANDING IN DRO, THE CREW NOTICED THAT TWO ADJACENT RED FLOOR EMERGENCY ESCAPE PATH LIGHTING FAILED TO ILLUMINATE. MAINTENANCE DEPOWERED/REPOWERED THE AIRCRAFT AND COULD NOT DUPLICATE THE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LIGHT — CRACKED (CABIN)
DURING A ROUTINE LINE CHECK, MAINTENANCE PERSONNEL FOUND THE FIRST TWO EMERGENCY FLOOR TRACK LIGHT ASSEMBLYS CRACKED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLYS, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LIGHT — CRACKED (CABIN)
DURING A ROUTINE LINE CHECK, MAINTENANCE PERSONNEL FOUND THE FIRST TWO EMERGENCY FLOOR TRACK LIGHT ASSEMBLY CRACKED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLIES, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LIGHT — FAILED (CABIN)
AIRSHUTTLE NR 7568 - DEN-GJT - IN DEN, THE CREW REPORTED THAT ONE RED FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT FAILED TO ILLUMINATE. MAINTENANCE DEFERRED THE LIGHTING SYSTEM PER MEL 33-13. IN SUBSEQUENT MAINTENANCE, ONE RED EMERGENCY FLOOR ESCAPE PATH LIGHT TUBE WAS REMOVED AND REPLACED. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LIGHT — MALFUNCTIONED (CABIN)
AIRSHUTTLE 7576 - DEN-GJT - IN DEN, THE CREW FOUND THAT ONE RED EMERGENCY ESCAPE PATH LIGHT AT ROW 4 WOULD NOT ILLUMINATE. MAINTENANCE DEFERRED THE LIGHTS PER MEL 33-13. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE ALL RED LIGHTS WERE FOUND TO BE WORKING. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: PITCH LEVER ASSY — LOOSE (CONTROL COLUMN)
DURING NIGHT MAINTENANCE, INSPECTED AND FOUND LOOSE BOLTS ONE EACH END OF THE PITCH CONTROL TORQUE TUBE THAT INTERCONNECTS THE TWO CONTROL COLUMNS. RETORQUED BOLTS AS REQUIRED. NO FURTHER DISCREPANCIES, AIRCRAFT WAS RELEASED FOR SERVICE. (X)