N401QS
Registered owner: CITY SERVICE AIR HOLDINGS LLC, 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.
24 reports on file, 2004-12-10 – 2016-06-23.
Part: STRAP — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
HORIZONTAL STABILIZER T/E LT UPPER OVERHANG STRAPS HAVE CORROSION AROUND SEVERAL SCREW HOLES. REQUIRES MAJOR REPAIR DOCUMENTED ON FORM 8100-9.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 12,961 hrs · 6,423 cycles
BS 169 CHANNEL CRACKED BETWEEN MAIN ENTRANCE DOOR ACTUATOR ATTACH POINTS. APPROXIMATE LENGTH IS 0.75 INCH.
Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
RIGHT ELEVATOR HINGE NR 3, HORIZONTAL STABILIZER SIDE, CORRODED INSIDE ATTACH BOLT BORE.
Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
LEFT ELEVATOR HINGE NR 4, ATTACHED TO HORIZONTAL STABILIZER SIDE, CORRODED INSIDE ATTACH BOLT BORE.
Part: ATTACH FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
HORIZONTAL STABILIZER PIVOT FITTING CORRODED AND BLEEDING RUST FROM LT AND RT LUG ATTACH POINTS. REQUIRES MAJOR REPAIR DOCUMENTED ON FAA FORM 8100-9.
Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · airframe 12,961 hrs · 6,423 cycles
RIGHT ELEVATOR HINGE NR2, HORIZONTAL STABILIZER SIDE, CORRODED INSIDE ATTACH BOLT BORE.
Part: FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
LEFT VERTICAL STABILIZER FITTING FOR HORIZONTAL STABILIZER ATTACHMENT BLEEDING RUST FROM PIVOT BEARING BORE.
Part: FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
RIGHT VERTICAL STABILIZER FITTING FOR HORIZONTAL STABILIZER ATTACHMENT BLEEDING RUST FROM PIVOT BORE.
Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
RIGHT ELEVATOR HINGE NR 2, HORIZONTAL STABILIZER SIDE. CORRODED INSIDE ATTACH BOLT BORE.
Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
RIGHT ELEVATOR HINGE NR 4, HORIZONTAL STABILIZER SIDE, CORRODED INSIDE ATTACH BOLT BORE.
Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
LEFT ELEVATOR HINGE NR 2, HORIZONTAL STABILIZER SIDE, CORRODED INSIDE ATTACH BOLT BORE.
Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 12,961 hrs · 6,423 cycles
LEFT ELEVATOR HINGE NR 3, ATTACHED TO HORIZONTAL STABILIZER SIDE, CORRODED INSIDE ATTACH BOLT BORE.
Earlier reports · 2004–2014 · 12 reports
2014
Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 11,547 hrs · 5,731 cycles
LT FLAP TRACK CORRODED, REPLACED FLAP TRACK.
Part: FITTING — CORRODED (ZONE 500) · airframe 11,547 hrs · 5,731 cycles
LEFT FLAP TRACK LOWER ATTACH FITTING CORRODED, R & R FITTING.
Part: ACM — MALFUNCTIONED (AC BAY) · airframe 11,546 hrs · 5,730 cycles
COCKPIT FILLED WITH SMOKE RAPIDLY 10 MINUTES AFTER APU STARTED UP FOLLOW BY BURNING SMELL. WE SHUT DOWN THE ACFT RIGHT AWAY. ALSO SMOKE IN THE MAIN CABIN. UNABLE TO DETERMINE WHERE THE SMOKE IS COMING FROM. COMPLIED WITH AIR CYCLE MACHINE REPLACEMENT IAW CMP 215012. OPERATIONS TEST WAS GOOD.
2012
Part: BRAKE SYS — FAILED · airframe 10,256 hrs · 5,031 cycles
BRAKES ARE VERY HARD AND UNRESPONSIVE. PEDALS DEPRESS ALMOST FULL TRAVEL WITH SOFT LIMITED BRAKING. AT THE VERY END OF TRAVEL, BRAKE PEDALS TAKE A LARGE AMOUNT OF EFFORT TO GET ANY SUBSTANTIAL EFFECT. WITH LOTS OF FORCE, BRAKES DO FINALLY ACHIEVE 3000PSI. NO OTHER CAS OR FAULT MESSAGES ASSOCIATED WITH THIS. CLEARED BRAKE ECU GROUND FAULT. JACKED ACFT AND PERFORMED NUT CRACKER SYS FAULT ISOLATION IAW GAC GIV MSG3 MM CH 32-07-00. NO DEFECTS NOTED. PERFORMED WHEEL BRAKES FUNCTIONAL TEST IAW MM CH 32-43-00. STEPS 1-12. NO DEFECTS NOTED. TAXIED ACFT CHECKED BRAKE PRESSURE RECHECKED BRAKE ECU FOR FAULTS, NONE DETECTED. BRAKING AND PRESSURE CHECKED GOOD.
Part: LUG — CORRODED (RIGHT WING) · airframe 10,099 hrs · 4,960 cycles
RT AFT LUG ON SPONSON RIB HAS PITTING IN BORE.
2010
Part: OVEN — SMOKE (GALLEY) · airframe 8,936 hrs · 4,407 cycles
OVEN SMOKES WHEN BEING OPERATED. MX PERFORMED OPS CHECK OF OVEN AND FOUND NO DISCREPANCIES. SUSPECT FOOD HAD BEEN SPILLED INSIDE OVEN.
2005
Part: WINDSHIELD — CRACKED (COCKPIT)
LEFT WINDSHIELD HAS 3 SMALL CRACKS IN OUTER PANE.
Part: CONTROL SYSTEM — MALFUNCTIONED (SPOILERS) · airframe 4,720 hrs · 2,323 cycles
DURING FLIGHT AT 250-290 KIAS, MOVING THE FLIGHT SPOILER HANDLE .5 - 1 INCH FROM CLOSED RESULTED IN AN ABRUPT ROLL TO THE LEFT.
Part: SEAL — DEFLATED (DOOR) · airframe 4,374 hrs · 2,171 cycles
DOOR SEAL HAD PARTIAL DEFLATION AT FLIGHT LEVEL 410.
Part: MANIFOLD — MALFUNCTIONED (NLG STEERING)
NOSE STEERING PULLING TO LEFT.
Part: ACTUATOR — FAILED (TE FLAPS) · airframe 4,275 hrs · 2,120 cycles
IN FLIGHT FLAPS SELECTED 10 DEGREES, MOVED 7-8 DEGREES, STAB DID NOT MOVE AT ALL.
2004
Part: CONVERTER — FAILED (AC SYSTEM) · airframe 4,121 hrs · 2,048 cycles
1.5 HOURS INTO FLT LEFT AC POWER AND LT DC POWER FAILED.