N869AV
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.
5 reports on file, 2009-10-04 – 2016-11-17.
Part: LOOP — DEFECTIVE (RT ENGINE) · airframe 4,525 hrs · 2,456 cycles
KILG TO MDPC, DIVERT BACK TO KILG. DECLARED EMERGENCY, RIGHT "ENG FIRE PULL" LIGHT ILLUMINATED IN FLIGHT. BROUGHT THRUST LEVER TO IDLE FOR 15 SECONDS AND INDICATION CONTINUED. SHUT ENGINE DOWN & DEPRESSED RIGHT HAND "ENG EXT ARMED" LIGHT. IN WORK. OVERWEIGHT LANDING C/W. R&R ANTI-ICE VALVE AND REMOVING RT ENG NOW TO EASE R&R OF RT ENG TAIL CONE BLEED LOOP FOR LOW RESISTANCE.
Part: FUEL LINE — SEPARATED (RT ENGINE) · airframe 2,101 hrs · 1,153 cycles
135 REPOSITIONING FLIGHT, NO PASSENGERS: AFTER LANDING IN KILG, WHILE TAXIING, GROUND PERSONNEL RECOGNIZED A FUEL LEAK FROM RIGHT ENGINE. SETUP MX. DISCOVERED RIGID FUEL LINE FROM FUEL EJECTOR TO FUEL PUMP SEPARATED AT THE SWEGED CRIMP THAT SECURES THE "B" NUT. R2 FUEL LINE (P/N 30B1787), A/C RTS ON 8/14/12. LEARJET IS ACTIVELY INVESTIGATING THIS ISSUE.
Part: STARTER GEN — FAILED (ENGINE) · airframe 1,464 hrs · 813 cycles
DURING FLIGHT FROM KILG TO MMUN (CANCUN MEXICO) THE CREW OBSERVED AN R GEN FAIL LIGHT. CREW WAS UNABLE TO RESET GENERATOR. CREW ELECTED TO DIVERT TO KFXE WHERE GENERATOR WAS REPLACED.
Part: REGULATOR — FAILED (HYDRAULIC SYS) · airframe 1,319 hrs · 735 cycles
AIRCRAFT DEPARTED KSUA TO MMTO. SHORTLY AFTER REACHING CRUISE ALTITUDE (FL430), RIGHT HYD PRES LIGHT ILLUMINATED AND THEN SHORTLY AFTER THE LEFT HYD PRES LIGHT ILLUMINATED. CREW DIVERTED TO KMIA. HYDRAULIC PRESSURE INDICATOR REMAINED IN GREEN UNTIL GEAR WAS SELECTED DOWN. ALL THREE GEAR CAME DOWN AND LOCKED. AUX HYDRAULIC PUMP WAS USED AND THEY HAD NORMAL BREAKING. CREW REPORTED RIGHT SIDE OF AIRCRAFT AND RIGHT ENGINE COWL COVERED IN HYDRAULIC FLUID. MAINTENANCE CONFIRMED FLEX LINE FAILURES AT HYDRAULIC PUMP PRESSURE PORT. MAINTENANCE PERFORMED FUNCTIONAL TEST OF THE HYDRAULIC RESERVOIR PRESSURE REGULATOR IAW MM 29-00-02 AND REGULATOR FAILED TEST. SUSPECT FAILED REGULATOR CAUSED RESERVOIR TO REMAIN UNPRESSURIZED, CAUSING HYDRAULIC FLUID TO FOAM AND ENGINE DRIVEN PUMPS TO ACTIVATE AND BLOW OUT FLEX LINES ON RIGHT PUMP AND EMPTY FLUID FROM RESERVOIR.
Part: REGULATOR — FAILED (HYD SYSTEM) · airframe 817 hrs · 478 cycles
AT FL410 L HYD PRESS AMBER ANNUNCIATOR ILLUMINATED. R HYD PRESS AMBER ANNUNCIATOR ILLUMINATED APPROX 15 MINUTES LATER. HYD SYS PRESSURE REMAINED NORMAL. DESCENDED TO FL370 DIVERT FOR LONGER RUNWAY. BOTH WARNING LIGHTS EXTINGUISHED AFTER 10 MINUTES, SYS PRESSURE REMAINED NORMAL. DECIDED TO CONTINUE TO DESTINATION. ALL SYSTEMS CONTINUED TO FUNCTION NORMAL. MADE NORMAL LANDING. MX PERFORMED VISUAL CHECK OF HYD SYS AND SERVICE LEVEL, ALL OK. NO VISIBLE LEAKS. MX PERFORMED FUNCTION CHECK OF HYD SYS RESERVOIR PRESSURE REGULATOR, FILTER AND CHECK VALVE. VALVE AND REGULATOR AND FILTER FAILED TO PRESSURIZE RESERVOIR WITH ENGINES RUNNING ON GROUND. REPLACED VALVE, REGULATOR AND FILTER. RESERVOIR PRESSURE SYS TESTED NORMAL AFTER REPAIR. THE FOLLOWING PARTS WERE REPLACED. PN 859A-48T CHECK VALVE, PN 2702-13 SN 0919 REGULATOR, PN 4301-2 FILTER. NOT SURE IF REGULATOR OR CHECK VALVE IS PROBLEM.