N892QS
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.
7 reports on file, 2003-10-02 – 2013-09-24.
Part: BRAKE — UNKNOWN (MLG) · airframe 6,908 hrs · 4,897 cycles
PILOTS SIDE LT BRAKES FEEL "SPONGY" HAVE TO BE PRESSED ALMOST TO THE FLOOR BEFORE ADEQUATE BRAKING IS ACHIEVED. OPERATED BRAKES SEVERAL TIMES AND TAXIED ACFT AROUND. FOUND PILOTS SIDE LEFT BRAKE TO BE FUNCTIONING CORRECTLY. BRAKES APPLIED EVENLY, PRESSURES WERE GOOD. NO DEFECTS NOTED AT THIS TIME. ALL WORK DONE IAW MM 32-40-51, OK FOR CONTINUED SERVICE. COULD NOT DUPLICATE.
Part: BRAKE ASSY — WEAK (MLG) · airframe 6,749 hrs · 4,754 cycles
LEFT BRAKE PEDAL SPONGEY ON CAPTAIN AND F/O SIDE. PEDAL WILL TRAVEL SEVERAL INCHES BEFORE GRABBING. A FAINT SOUND CAN BE HEARD FROM CAPTAINS SIDE PEDAL AREA. REMOVED NR 1 BRAKE ASSY, AND INSTALLED OVERHAULED BRAKE ASSY. REMOVED NR 2 BRAKE ASSY, SN AND INSTALLED OVERHAULED BRAKE ASSY, IAW AMM 32-40-114. OPS AND LEAK CHECKS NORMAL WITH NO DEFECTS NOTED.
Part: UNKNOWN — CORRODED (WING) · airframe 6,342 hrs · 4,486 cycles
PERFORMED AN NDT INSPECTION AFTER CORROSION WAS REMOVED AROUND SOME SCREW HOLES. NDT WAS READING AN ANOMALY UNDER THE SURFACE ABOUT .020 DEEP. STARTED BLENDING THE AREA THERE WAS SIGNIFICANT CORROSION AND THE METAL JUST KIND OF DISINTEGRATED. COMPLIED WITH FIELD REPAIR FR-HK-05408. CUT OUT CORROSION IAW DRAWING, FABRICATE SKIN FILLER AND DOUBLER. PRIME AND INSTALL ALL PARTS IAW THE FIELD REPAIR. PROTECT FUEL BAYS AS REQUIRED.
Part: WIRE HARNESS — SHORTED (APU) · airframe 4,905 hrs · 3,421 cycles
INVESTIGATED PATS STC INSTALLATION GTCP36-150W FAILING TO START. APU HANGS AT 60 PERCENT, WILL NOT ACCELERATE OR LOAD. FOUND INTERMITTENT OPEN CONNECTION IN WIRING BETWEEN SPEED SENSOR CONNECTOR P6 PIN C AND ECU CONNECTOR P2. ALSO REPLACED EXHAUST TEMPERATURE THERMOCOUPLE WITH OUT OF SERVICE LIMITS RESISTANCE READINGS. REQUIRED EXTENSIVE TROUBLESHOOTING AND COMPONENT REMOVAL/REPLACEMENTS TO VERIFY. TRANSIENT ACFT, MX RECORDS NOT AVAILABLE. PN 3800304-1 MODEL GTCP36-150W APU, SN P-709. TSN: 4764.8
Part: BRAKE SYS — CONTAMINATED (LANDING GEAR) · airframe 4,027 hrs · 2,805 cycles
BRAKES ARE VERY MUSHY AND GO TO THE FLOOR. INSPECTED SYS FOR LEAKS, NONE NOTED. PERFORMED OPS CHECK, ALL CHECK GOOD. BLED BRAKE SYS AND PERFORMED TAXI CHECK, ALL CHECK GOOD. ALL WORK IAW MM 32-40-00.
Part: BRAKE ASSY — FAILED · airframe 4,027 hrs · 2,805 cycles
BRAKES ARE VERY MUSHY AND GO TO THE FLOOR. INSPECTED SYSTEM FOR LEAKS NONE NOTED. PERFORMED OPS CHECK ALL CHECK GOOD BLEED BRAKE SYSTEM AND PERFORM TAXI CHECK ALL CHECK GOOD. ALL WORK IAW MM 32-40-00.
Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 303 hrs · 235 cycles
AT FLIGHT LEVER 370, NR 1 ENGINED EXPERIENCE A LOUD BANG WITH ITT SPIKING AT 1016 DEGREES WITH AIRFRAME VIBRATION. N1 AND N2 ROSE, ITT THEN FELL TO 450 DEGREES WITH N1 AND N2 DROPPING. SHUT DOWN ENGINE. TROUBLESHOT NR 1 ENGINE FOUND THE LOW PRESSURE COMPRESSOR DAMAGED, HARD TO ROTATE BY HAND. REMOVED NR 1 ENGINE AND INSTALLED A SERVICEABLE LOANER ENGINE IAW RAYTHEON HAWKER 800XP MM AND HONEYWELL TFE 731-5BR LMM CHAPTER 72-02-96. PERFORMED OPERATIONAL, FUNCTIONAL & LEAK CHECKS, ALL CHECKED GOOD.