N88
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
FLAPS FAILED @ 43 DEGREES ON APPROACH @ KAFW. FULL STOP LANDING AND FLAP RESET SUCCESSFUL.
UNABLE TO PRESSURIZE AIRCRAFT CABIN DURING CLIMBOUT. SWITCH POSITIONS VERIFIED CORRECTLY AND SYSTEM WOULD NOT TEST AFTER LANDING
PILOT WINDSHIELD CRACKED APPROX 25 MIN AFTER TAKEOFF
APU OIL PRESSURE LIGHT. APU AUTO SHUTDOWN ON ARRIVAL
FLAPS FAIL UNSUCCESSFUL RESET. MAINTENANCE DISCOVERED A POTENTIOMETER ON PDU TO BE OUT OF LIMITS. POTENTIOMETER WAS REPLACED. NO OTHER ITEMS FOUND.
FLAPS FAIL AT 20 DEGREES AFTER T.O ACTION TAKEN: PERFORMED OPERATIONAL CHECK OF FLAPS. NO DEFECTS NOTED. WILL CONTINUE TO MONITOR
EICAS INDICATED GEAR DISAGREE WITH NOSE GEAR DOOR OPEN. INSPECTION AND EXTENSIVE TROUBLESHOOTING/TESTING RESULTED IN NO FAULT BEING FOUND. WILL CONTINUE TO MONITOR.
"WOW OUTPUT" CAUTION & "GND SPLR NOT ARMED" ADVISORY IN FLIGHT. WOW OUTPUT EXTINGUISHED IN 5 MIN THEN SPLR MSG STAYED ON UNTIL ENGINE SHUTDOWN. MAINTENANCE COMPLIED WITH GROUND CHECKS, SPOILERS, NO DEFECT WAS FOUND. NO FAULT INDICATED AT POWER UP. WILL CONTINUE TO MONITOR.
AMBER CAS MESSAGE, WOW INPUT AND GND SPLRS WOULD FLASH AND STAY ON FOR ABOUT 5 SECONDS DURING GEAR DOWN OPERATIONS/CYCLING THE GEAR DURING LOW APPROACHES 5 TIMES. AFTER RESEATING THE PSEAU, A (BITE TEST) WAS PERFORMED AND THE AIRCRAFT JACKED AND GEAR CYCLED WITH NO WOW INPUT OR GROUND SPOILER CAS MESSAGES. SYSTEM CHECKS WERE GOOD.
OXY LOW PRESS CAUTION. 800 PRESS ON GAUGE. FOUND SYSTEM TO OXYGEN LEVEL LOW. RESOLVED ISSUE BY SERVICING OXYGEN SYSTEM.
OXY LOW PRESS CAUTION. 800 PRESS ON GAUGE. FOUND OXYGEN SYSTEM LEVEL LOW. RESOLVED ISSUE BY SERVICING OXYGEN SYSTEM.
RIGHT 14TH STAGE DUCT FAIL LIGHT ILLUMINATED IN FLIGHT.
REPORTED FLAP FAIL AT 42 DEGREES DURING APPROACH, THE FLAPS CHECKED GOOD AFTER FLAP SYSTEM WAS RESET.
WING OVERHEAT WING HEAT ON IN NORMAL L A/ICE CAUTION LIGHT ILLUMINATED & OVERHEAD GREEN ANNUNCINTOR OUT. REPLACING THE WING ANTI-ICE TEMPERATURE CONTROLLER CORRECTED THIS ISSUE. A VISUAL INSPECTION OF AIRCRAFT FOR WING LEADING EDGE OVERHEAT DAMAGE WAS PERFORMED. NO DEFECTS NOTED.
RIGHT MAIN LANDING GEAR DID NOT RETRACT AFTER PLANNED LOW APPROACH, WITH THE GEAR HANDLE UP. GEAR DISAGREE ILLUMINATED. FOLLOWED CHECKLIST PROCEDURE FOR GEAR DISAGREE, HANDLE UP, RESULTING IN THREE GEAR DOWN AND LOCKED.
OBSERVED VERTICAL CRACK IN THE OUTER PANE OF THE LT FRONT WINDSHIELD.
RT 14TH STAGE DUCT LIGHT RED ILLUMINATED WITH RED MASTER CAUTION LIGHT. REPAIRED LEAK AT 14TH STAGE BLEED AIR VLV.
14TH DUCT FAIL LIGHT ILLUMINATED TWICE. RT 14TH STAGE BLEED AIR VLV LEAKING AT ENG SIDE OF VLV, LOOSENED CLAMPS, REPOSITIONED VLV & TIGHTENED CLAMPS.
RED ENGINE WARNING MESSAGE ON TAKEOFF ROLL (ABORTED APPROX 100 KIAS) AUTO THROTTLES ENGAGED. NO INDICATION OF ENGINE LIMITS EXCEEDED. DOWN LOADED MDC AND FOUND THAT BOTH ENGINES HAD REACHED 900C DURING TAKEOFF ROLL. SUSPECT AUTO THROTTLES DID NOT ENGAGE OR THE WRONG DATA WAS INPUT. RED ENGINE WARNING LIGHT SHOULD NOT HAVE ILLUMINATED UNTIL 929C WITH AUTO THROTTLES AND THE CORRECT DATA.