N76
Registered owner: FEDERAL AVIATION ADMINISTRATION, OK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Flight Program Operations (RU3A) | Certificate holder | — | Matched by certificate designator |
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.
17 reports on file, 2002-09-10 – 2026-03-17.
Part: BLEED AIR SYS — FAULTED (RT ENGINE) · airframe 18,491 hrs · 9,078 cycles
RIGHT BLEED AIR FAIL RED SEGMENT LIGHT ILLUMINATED AT FL 200 EMERGENCY CHECK LIST RUN LIGHT EXTINGUISHED DECENDING THROUGH 7000 MSL
Earlier reports · 2002–2020 · 16 reports
2020
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 16,380 hrs · 8,476 cycles
CABIN ALT WARNING ILLUMINATED IN FLIGHT CABIN DIFF SHOWS "0". AIR PRESSURE CONTROLLER REPLACEMENT CORRECTED ISSUE.
2019
Part: DOOR — NOISY (CABIN) · airframe 15,715 hrs · 8,139 cycles
PASSING 11,000 MSL, CABIN LOST PRESSURE. MS REPORTS HISSING SOUND FROM CABIN DOOR.
2018
Part: PCB — LOOSE (LOGIC RELAY) · airframe 15,550 hrs · 8,062 cycles
RUDDER BOOST OFF LIGHT ILLUMINATED. RUNNING THE ABNORMAL CHECKLIST MADE NO DIFFERANCE. DISCOVERED LOOSE RELAY AND SOCKET. REPLACED LOGIC RELAY PCB. RUDDER BOOST LAMPS WORKING CORRECTLY. NO FURTHER ACTION REQUIRED.
2017
Part: FILTER — RESTRICTED (SAFETY VALVE) · airframe 15,218 hrs · 7,911 cycles
DUE TO A RESTRICTED SAFETY VALVE FILTER, PRESSURIZATION SYSTEM FAILED IN FLIGHT. SYSTEM PERFORMED WITHOUT FURTHER ISSUE AFTER FILTER WAS CLEANED. NO NOTED TREND
2013
Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 14,090 hrs · 7,369 cycles
THE IN TRANSIT LIGHT REMAINED ON WHEN THE GEAR WAS RETRACTED. WHEN MOVED TO THE DOWN POSITION, RECEIVED THREE GREEN, NO RED. GEAR DOWN AND LOCKED, LANDED WITHOUT INCIDENT.
Part: AUTOFEATHER SYS — MALFUNCTIONED (PROPELLER) · airframe 13,780 hrs · 7,213 cycles
DURING RUN UP AUTO FEATHERS CHECKED SAT. DURING POWER UP ON TAKEOFF ROLL AUTO FEATHERS ARMED AT APPROX 80 KTS PLUS LEFT AUTO FEATHER LIGHT WENT OUT. TAKEOFF ABORTED. STOPPED ON RUNWAY, DID A RUN UP AND AUTO FEATHER ARMED. BEGAN A SECOND TAKEOFF ROLL AND AT APPROX 80 KTS PLUS LEFT AUTO FEATHER LIGHT WENT OUT AGAIN. TAKEOFF ABORTED.
2012
Part: WIRE — BROKEN (FIRE BOTTLE) · airframe 13,496 hrs · 7,068 cycles
ON TAKEOFF ROLL AT APPROX 60 KIAS, PNF OBSERVED DISCHARGED LIGHT ILLUMINATION ON LEFT FIRE BOTTLE. PNF CALLED OUT AN ABORT AND PF ABORTED TAKEOFF. CREW TAXIED AIRCRAFT TO HANGAR WITH NO FURTHER INCIDENT. FOUND BROKEN WIRE TO NR 1 FIRE BOTTLE. REPAIRED BROKEN WIRE, SYSTEM OPS CHECKED GOOD.
2011
Part: PROXIMITY SWITCH — DEFECTIVE (RT PROPELLER) · airframe 12,592 hrs · 6,621 cycles
IN CRUISE FLIGHT AT 16000 MSL, RIGHT PROP PITCH ANNUNCIATOR ILLUMINATED. NO OTHER INDICATIONS ON INSTRUMENTS. NO AFFECTS ON AIRCRAFT HANDLING WERE DETECTED IN FLIGHT. CREW ELECTED TO RETURN TO HOME BASE. IN ANTICIPATION OF POSSIBLE ASYMMETRIC THRUST ON LANDING, DECLARED EMERGENCY SO THAT EMERGENCY EQUIPMENT WOULD BE STANDING BY. LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED DEFECTIVE RIGHT PROP PROXIMITY SWITCH.
Part: LANYARD — BROKEN (FUEL CAP) · airframe 12,532 hrs · 6,588 cycles
AFTER TAKEOFF FUEL WAS STREAMING FROM RIGHT MAIN FUEL CAP WITH FUEL CAP FLUSH WITH AIRCRAFT SURFACE. REQUESTED PRIORITY HANDLING FROM TOWER, LANDING WAS UNEVENTFUL. MAINTENANCE DISCOVERED LANYARD WAS BROKEN AND CAUGHT BETWEEN FUEL CAP AND SEALING SURFACE.
Part: SHRADER VALVE — LEAKING (LANDING GEAR) · airframe 12,492 hrs · 6,568 cycles
ON APPROACH, LOWERED LANDING GEAR AND NO AUDIBLE SOUND HEARD NOR ANY LIGHTS INDICATED IN GEAR HANDLE OR ON POSITION LIGHTS. FLAPS LOWERED TO FULL POSITION IN ORDER TO CONFIRM ABNORMAL INDICATION. LANDING GEAR HORN SOUNDED INDICATING GEAR WAS NOT IN DOWN POSITION. WHILE COMPLETING ABNORMAL CHECKLIST NOTED LANDING GEAR C/B WAS POPPED. CHOSE TO DIVERT BACK TO BASE AIRPORT. ON APPROACH, EMERGENCY DECLARED, ABNORMAL CHECKLIST REVIEWED, LANDING GEAR MANUALLY LOWERED AND CORRECT GEAR DOWN/LOCKED INDICATION OBTAINED. GEAR VISUALLY CONFIRMED DOWN BY TOWER. MAINTENANCE FOUND VALVE ASSY ON ACCUMULATOR LEAKING AT BASE. REMOVED/REPLACED VALVE ASSY AND SERVICED ACCUMULATOR.
2010
Part: CONNECTOR — LOOSE (ZONE 700) · airframe 12,338 hrs · 6,489 cycles
FLAPS AT APPROACH POSITION. SELECTED LANDING GEAR DOWN. POSITION INDICATORS SHOWED GREEN FOR NOSE AND LEFT MAIN GEAR. NO INDICATION ON RIGHT MAIN GEAR. CHECKED ANNUNCIATOR, GOOD. SELECTED FLAPS FULL DOWN AND RECEIVED CONFIGURATION WARNING HORN. DECLARED EMERGENCY WITH APPROACH. FOLLOWED ABNORMAL PROCEDURES CHECKLIST. OBTAINED DOWN AND LOCKED INDICATION AFTER MANUALLY PUMPING DOWN THE GEAR. CONDUCTED TOWER FLY BY TO VERIFY. VERIFIED THAT CONFIGURATION WARNING HORN DID NOT OCCUR WITH FULL FLAPS SELECTED. CONDUCTED UNEVENTFUL LANDING. AIRCRAFT TOWED TO HANGAR AND PLACED ON JACKS. DUPLICATED DISCREPANCY. INSPECTED RT DOWNLOCK SWITCH AND WIRING. FOUND S506 CONNECTOR LOOSE. SECURED CONNECTOR. OPERATION FOUND GOOD ON SEVERAL GEAR RETRACTION CYCLES.
2005
Part: WARNING LIGHT — FALSE INDICATION (MLG)
ON FINAL APPROACH, LOWERED GEAR AT FAF - NO LEFT MAIN GEAR LIGHT. CYCLED GEAR ONCE INSIDE FAF - STILL NO LIGHTS, EXECUTED FLY BY RWY 4R. 2 AIRLINE CREWS ADVISED ALL 3 GEARS APPEAR DOWN. FLEW LT TRAFFIC, CYCLED GEAR 3RD TIME, OBSERVED GEAR RETRACT AND EXTEND. (K)
Part: ODOR — DETECTED (COCKPIT)
ON DOWNWIND AFTER BPC RUN, SMELLED ELECTRICAL BURNING. NOTICED NUMBER 2 COMM NO LED READOUT. PULLED CB NR 2 COMM DUMPED CABIN. SMELL DID NOT DISPERSE TO OUR EXPECTATION. LANDED AIRCRAFT. (M)
Part: POWER SUPPLY — BURNED (NR 2 COMM)
ON DOWNWIND AFTER BPC RUN, SMELLED ELECTRICAL BURNING. NOTICED NUMBER 2 COMM NO LEAD READOUT. PULLED CB NUMBER 2 COMM DUMPED CABIN. SMELL DID NOT DISPERSE TO OUR EXPECTATION. LANDED AIRCRAFT. FOUND NR 2 COMM POWER SUPPLY BURNED, REPLACED NR 2 COMM. (M)
2004
Part: COOLING FAN — BURNED (INERTIAL REF UNT)
WHILE SETTING UP FOR FLIGHT INSPECTION MANEUVER, GOT A RED MASTER CAUTION LIGHT WITH AN AP TRIM DISC LIGHT. TEMPORARILY LOST TCAS, PILOTS FLIGHT DIRECTOR, AND THE PILOTS NCU. AT THE SAME TIME HEARD ELECTRICAL SHORTING SOUND. STRONG ELECTRICAL FUMES WERE DETECTED AND THE CREW DONNED O2 MASK. COPILOT INFORMED APPROACH OF THEIR STATUS AND REQUESTED A FULL STOP LANDING. SHORTLY AFTER THE POWER INTERRUPTION, PILOTS NCU CAME BACK UP. COPILOT TURNED OFF THE MISSION EQUIPMENT AND THE MSU TO REDUCE CHANCES OF ELECTRICAL FIRE AND THE AIRCRAFT WAS DEPRESSURIZED ON FINAL IN AN ATTEMPT TO REDUCE FUMES. THE CREW MADE AN UNEVENTFUL LANDING. FOUND LASER REFERENCE COOLING FAN SHORTED.
2002
Part: INDICATOR — FALSE INDICATION (COCKPIT)
ON TAKEOFF ROLL AT 70KIAS, THE 1 TORQUE GAUGE JUMPED FROM 35 TO 120 WITH THROTTLES ALIGNED. RIGHT TORQUE DID NOT EXCEED 70 TAKEOFF ABORTED. REMOVED AND REPLACED NR 1 TORQUE INDICATOR. OPS CHECK SATISFACTORY. (M)