N711QS
Registered owner: CIENA CORP, OK (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.
6 reports on file, 2008-06-02 – 2014-04-24.
Part: CONTROL COLUMN — CHAFED (COCKPIT) · airframe 6,618 hrs · 4,003 cycles
LEFT AND RIGHT CONTROL COLUMNS CHAFED FROM THE AILERON CABLES INSIDE COLUMNS. REMOVED CONTROL COLUMNS, REWORKED IAW EO4AS5320110-502A02. REINSTALLED CONTROL COLUMNS IAW AMM 27-10-06 AND EO4AS5320110-502A02.
Part: WARNING MESSAGE — ILLUMINATED (ENGINE OIL) · airframe 6,098 hrs · 3,699 cycles
WHILE AT FL400 AND ONE HOUR INTO THE FLIGHT, RT ENG OIL PRESSURE HIGH EICAS ILLUMINATED. OBSERVED RED 111PSI AND IMMEDIATELY RETARDED THROTTLE TO IDLE. ATTEMPTED TO INCREASE POWER BUT OIL PRESSURE INCREASED PROPORTIONATLEY TO THROTTLE MOVEMENT.
Part: WARNING LIGHT — ILLUMINATED (HYD SYSTEM) · airframe 4,846 hrs · 2,944 cycles
DURING CLIMB OUT, GEAR UP & LOCKED, SLATS & KRUEGERS OUT, RECEIVED AN "AUX HYD PUMP ON" MESSAGE EACH TIME, POWERED ABOVE MAX CRUISE. BETWEEN 8 & 10,000 & AIRSPEED BETWEEN 180 & 235. BROUGHT SLATS & KRUEGERS UP, COULD NOT REPRODUCE PROBLEM. SWAPPED LT & RT MAIN HYD PRESSURE SWITCHES & REPLACED TIME DELAY RELAY 497C1 & 242P1 IAW MM G200 29-10-16. PERFORMED TEN NORMAL CLEAR SWINGS, SLATS & KRUEGERS DOWN, USING RT HYD PRESSURE & HAD POWER ABOVE MAX CRUISE. COULD NOT DUPLICATE MAX HYD PUMP LIGHT. VERIFIED PROXIMITY SWITCH GAP CLEARANCE 0.0394 IAW MM 32-10-11 & MM 32-30-00. RECONNECTED LT & RT MLG DOORS & TORQUED HARDWARE IAW MM 32-10-11. SWUNG GEAR AGAIN, NO DEFECTS NOTED IAW 32-30-00.
Part: WINDSHIELD — FAILED (COCKPIT) · airframe 3,566 hrs · 2,168 cycles
RT WINDSHIELD SHATTERED DURING FLIGHT. REPLACED COPILOT WINDSHIELD WITH NEW. OPS/LEAK CHECKS GOOD. DONE IAW MM 56-10-05.
Part: SWITCH — INOPERATIVE (BLEED AIR SYS) · airframe 2,526 hrs · 1,494 cycles
IMMEDIATELY UPON THROTTLES BEING PUT IN TAKEOFF DETENT, BLEED AIR OVERTEMP/OVER PRESSURE WARNING LIGHT ILLUMINATED. INSTALLED NEW BLEED AIR OVER TEMPERATURE SWITCH (AFT) IAW MM CHAPTER 21-11-07.
Part: FIRE WARNING — FALSE ACTIVATION (NR 1 NACELLE) · airframe 2,348 hrs · 1,396 cycles
DURING THE START OF ENGINE NR 1 RECEIVED AN "APU FIRE" WARNING WITH THE FIRE BELL. FIRED THE APU FIRE BOTTLE. INSPECTED APU CONTAINMENT AREA AND PERFORMED APU FIRE LOOP INSP, NO DEFECTS FOUND. RAN APU TO CHECK FOR BLEED AIR LEAKS, NONE FOUND, PERFORMED OPS CHECK OF APU FIRE DETECTION, NO FAULT FOUND. PERFORMED ENGINE RUN AND COULD NOT DUPLICATE PROBLEM AT THIS TIME. R&R RT FIRE BOTTLE IAW MM 26-20-05. COMPLIED WITH CMP 261005-ENGINE FIRE AND OVERHEAT DETECTION SYSTEM. OPS TEST IAW MM REF: 26-10-20.