N722QS
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.
13 reports on file, 2005-08-16 – 2012-01-23.
Part: GENERATOR — BURNED (LEFT) · airframe 6,022 hrs · 3,684 cycles
IN FLIGHT, THE LT GENERATOR INDICATED 201 AMPS AND THE RT GENERATOR INDICATED 137 AMPS. THIS IS TWICE THE NORMAL TOTAL LOAD FOR THE ACFT. THIS IS A REPEAT WRITE UP. ON APPROACH THERE WAS A FAINT "BURNED WIRE SMELL". WE TURNED OFF THE BAGGAGE HEAT AND CABIN SWITCHES AND LANDED NORMAL. SUP: REPLACED THE NOW NR 1 DC STARTER/GENERATOR IAW MM 24-30-06. OPS CHECK GOOD IAW MM 24-30-00. INSPECTED HEAT BLANKETS AND RAN DH7 WIRING. ALL CHECK GOOD. WHILE PERFORMING EMERGENCY RUN FOUND NO BURNING SMELL WHILE HAVING BAGGAGE HEAT AND CABIN SWITCHES ON.
Earlier reports · 2005–2011 · 12 reports
2011
Part: COMPUTER — MALFUNCTIONED (FUEL QTY) · airframe 5,969 hrs · 3,651 cycles
FUEL LEAK AMBER EICAS MESSAGE 1 HR INTO FLIGHT. FIRST HOUR FUEL BURN 2900. FUEL TOTAL ERRATIC FOR 15 MINUTES AFTER EICAS MESSAGE. LANDED WITH 7100 LBS AFTER 1.7 FLIGHT TIME. REMOVED FQMC AND REPLACED WITH REPAIRED FQMC REF MM 28-40-05 AND EO 4AS8840001. OPS CHECKED GOOD.
Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 5,780 hrs · 3,524 cycles
AIRPLANE PULLS HARD TO THE RT ON LANDING WHEN BRAKES ARE APPLIED.
Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 5,780 hrs · 3,524 cycles
AIRCRAFT PULLS HARD TO THE RT ON LANDING WHEN BRAKES ARE APPLIED. SERVICED THE NOSE WHEELS AND BLED THE ACFT BRAKES AS REQUIRED IAW MM CHP 32-40-20.
2009
Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 4,579 hrs · 2,787 cycles
ELECTRICAL ODOR THROUGHOUT THE CABIN AND COCKPIT. NO SMOKE NOTED. DESCENDED TO LOWER FLT LEVEL AND ODOR WENT AWAY. ACCOMPLISHED EMERGENCY LANDING. ERRATIC BEHAVIOR NOTED OF RT AVIONICS MASTER AND CABIN ENTERTAINMENT SYS. INSPECTED WIRES AND ASSOCIATED EQUIPMENT BEHIND THE OVERHEAD SWITCH PANEL, CIRCUIT BREAKER PANEL, SIDE WALLS, GALLEY, AND LAV IAW MM 24 AND WDM GA21-20022. PERFORMED THE OP'S CHECKS OF THE WINDSHIELD HEAT AND BAGGAGE HEAT REFERENCING THE QRH. PERFORMED THE GENERATOR LOAD SHED OP'S CHECK IAW MM 24-30-00. PERFORMED EMERGENCY LIGHTS OP'S CHECK IAW MM 33-50-00. NO DEFECTS NOTED AT THIS TIME.
Part: FAN BLADE — DAMAGED (LT ENGINE) · airframe 4,376 hrs · 2,666 cycles
ON PREFLIGHT WE DISCOVERED DAMAGE TO 2 OF THE LT ENGINE FAN BLADES THERE IS ALSO DAMAGE TO THE ENGINE SHROUD AT THE 7 O`CLOCK POSITION. REPLACED 3 FAN BLADES, FAN EXIT VANE RING, FAN CASE, AND INLET COWL. PERFORMED A SATISFACTORY 5 POINT GROUND PERFORMANCE RUN AND LEAK CHECK. NOTE THE FOLLOWING PARTS WERE ALSO CHANGED, ALL FOR FOD. FAN BLADE PN 30B5117-01, SN'S 50D940, 50D992, 50D953. CASE, FAN ASSY POST 25083 PN 30B4795-01, SN 14L534.
Part: FAN BLADE — DAMAGED (LT ENGINE) · airframe 4,376 hrs · 2,666 cycles
DISCOVERED DAMAGE TO TWO OF THE LT ENGINE FAN BLADES. THERE IS ALSO DAMAGE TO THE ENGINE SHROUD AT THE 7 O-CLOCK POSITION.
2008
Part: TIE ROD — WORN (PAX DOOR) · airframe 4,360 hrs · 2,657 cycles
CABIN DOOR OPENS AND CLOSES STIFF FWD GAS STRUT HANGING UP. T/S FOUND FWD TELESCOPIC ROD STICKING. REMOVED INOP ROD AND INSTALLED A NEW ROD ASSY. DOOR OPS CHECKS GOOD. WORK DONE IAW MM 52-10-05.
Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 4,360 hrs · 2,657 cycles
CABIN DOOR EICAS MSG AFTER TAKE-OFF.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 4,193 hrs · 2,557 cycles
CO-PILOT WINDSHIELD SHATTERED WHILE IN CRUISE FLIGHT AT FL350.
Part: WINDSHIELD — FAILED (COCKPIT) · airframe 4,193 hrs · 2,557 cycles
CO-PILOT WINDSHIELD SHATTERED WHILE IN CRUISE FLIGHT AT FL350. REPLACED COPILOTS WINDSHIELD AND WINDSHIELD TEMP CONTROLLER OPS CHECKED AND FUNCTIONAL TESTED SATISFACTORY. ALL WORK IAW MM CONTROLLER REF 30-40-05.
2006
Part: FIRE DETECTOR — BROKEN (RT ENGINE) · airframe 2,016 hrs · 1,232 cycles
RT ENG FIRE DETECT ILLUMINATED DURING CRUISE FLIGHT. TROUBLESHOT AND CONFIRMED DISCREPANCY. FOUND RT ENGINE ZONE 2 OVERHEAT DETECTOR BROKEN. REMOVED AND REPLACED RT ENGINE ZONE 2 OVERHEAT DETECTOR WITH NEW DETECTOR IAW G-200 M/M CHAP 26-10-10. OPS CHECK GOOD
2005
Part: STRUCTURE — BIRD STRIKE · airframe 1,115 hrs · 639 cycles
BIRD STRIKE DURING T/O ROLL OUT OF KSAV. ABORTED AT ABOUT 100 KTS. ACCOMPLISHED BIRD STRIKE INSPECTION IN ACCORDANCE WITH G200 MAINTENANCE MANUAL CHAPTER 05-55-00, NO DISCREPANCIES NOTED.