N281QS
Registered owner: 100 MILLION LLC, DE (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.
8 reports on file, 2005-01-28 – 2015-01-05.
Part: ARM — FAULTY (PAX DOOR SWITCH) · airframe 12,198 hrs · 7,713 cycles
DOOR LIGHT ILLUMINATED INFLIGHT AT FL350. AFTER RESETTING, IT ILLUMINATED FOUR MORE TIMES. NO LOSS OF PRESSURE NOTED. REMOVED FAULTY FORWARD CABIN DOOR PROXIMITY SWITCH STABILIZER ARM AND REPLACED. PERFORMED DOOR FUNCTIONAL CHECK. ALL WORK PERFORMED IAW MM 52-10-00-720-801, & 52-70-01-960-801. OPS CHECKS GOOD. PERFORMED PRESSURIZATION CHECK IAW TASK 21-32-000-710-801, OPS CHECKED GOOD.
Part: APU — FAILED · airframe 11,986 hrs · 7,575 cycles
FOUL ODOR COMING FROM ECS. R & R THE APU ASSEMBLY IAW MM 49-10-01-900-802. OPERATIONS & LEAK CHECKED GOOD. COMPLIED WITH TASK 05-50-00-700-801 CHECK & DECONTAMINATION OF THE AC SYS AFTER POLLUTION. NO DEFECTS NOTED.
Part: FADEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 9,997 hrs · 6,286 cycles
CRUISE ALTITUDE 43000', NR 2 ENGINE BEGAN TO SLOWLY LOSE POWER. POWER DECLINED TO APPROX 50 PERCENT. PRECAUTIONARY LANDING. AT LOWER ALTITUDES THROTTLE HAD LITTLE EFFECT CONTROLLING ENGINE. ENGINE WOULD NOT ACCELERATE ABOVE FLT IDLE REGARDLESS OF THROTTLE POSITION. AFTER TROUBLESHOOTING, FOUND RT ENGINE "B" FADEC FAILED, R & R UNIT IAW MM 76-10-05, GROUND RAN RT ENGINE, "B" FADEC TESTED GOOD IAW MM 72-00-00 & 73-20-01.
Part: ENGINE — SURGES (RIGHT) · airframe 9,991 hrs · 6,282 cycles
RT ENGINE WAS SURGING AFTER TAKEOFF. SURGING SHOWED ON ITT, N1, AND FUEL FLOW. SURGING WAS FIRST NOTICED AFTER POWER REDUCTION TO MAX CLIMB DETENT. CHECKED FOR FAULTS ON EIED NO FAULTS NOTED. ACCOMPLISHED ENGINE RUNS IAW MM 72-00-00. ACCOMPLISHED MULTIPLE ENGINE STARTS AND RUNS. RAN ENGINE FROM TAKEOFF POWER, REDUCING TO MAX CLIMB. REDUCING TO MAX CRUISE TO IDLE. NO DEFECTS NOTED. ENGINE RUNS WERE ACCOMPLISHED BOTH FADEC A & B CHECKED ENGINE PARAMETERS DURING RUN NO DEFECTS NOTED. CHECKED ELED FOR FAULTS NO FAULTS NOTED IAW MM 72-00-00.
Part: UNKNOWN — ODOR (COCKPIT) · airframe 8,546 hrs · 5,391 cycles
STRONG ODOR PRIMARILY ON CAPT SIDE OF COCKPIT. ELECTRICAL BURNING ODOR NOTICED ON ACFT SHUTDOWN. PULLED EFIS DISPLAYS AND FOUND ALL FANS CLEAN OF DEBRE AND OPERATION NORMAL. INSPECTED DV WINDOW HEAT CONNECTORS FOR ANY EVIDENCE OF ARCING, NOT FOUND. CHECKED IRU FAN BEHIND CAPTIAN IN CLOSET, CLEAN OPERATING NORMAL. CHECKED TURBO COOLER FOR EVIDENCE OF OIL AND APU FOR OIL LEAKS NONE.
Part: HYDRAULIC SYSTEM — READS LOW (NR 1) · airframe 7,241 hrs · 4,628 cycles
NR 1 HYDRAULIC SYSTEM QUANTITY INDICATED IN THE RED ZONE FOR QUANTITY DURING TAKEOFF RUN. ABORTED TAKEOFF ENSUED AS A RESULT OF LOW HYDRAULIC QUANTITY. SERVICED HYD SYSTEM IAW MM CH 29-112.
Part: UNKNOWN — UNKNOWN (MLG) · airframe 6,628 hrs · 4,244 cycles
AFTER TAKEOFF, UPON GEAR RETRACTION, LT MAIN GEAR DOOR LIGHT REMAINED RED. NO NOISE OR VIBRATION TO INDICATE DOOR WAS NOT CLOSED. ALL OTHER GEAR LIGHTS NORMAL. RETURNED TO AIRPORT, LANDED AND RED LIGHT STAYED ON. REMOVED & REPLACED DEFECTIVE LMLG DOOR LATCH W/ REPAIRED UNIT. JACKED AIRCRAFT CYCLED GEAR W/ NO DEFECTS NOTED. ALL WORK IAW F2000 M/M 32-130.
Part: ACTUATOR — MALFUNCTIONED (MLG) · airframe 4,632 hrs · 2,926 cycles
AFTER GEAR RETRACTION LEFT GEAR RED LIGHT INDICATOR DID NOT GO OUT. INSPECTION AFTER LANDING, GEAR DOOR WAS CLOSED BUT RED LIGHT REMAINED ON. REMOVED AND REPLACED THE LT MLG DOOR UPLOCK WITH A SERVICEABLE -REPAIRED- UNIT PER THE F-2000 M/M 32-300. ALL CHECKS WERE SATISFACTORY; NO DEFECTS WERE NOTED AT THIS TIME.