N413QS
Registered owner: NETJETS SALES INC, 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.
18 reports on file, 2005-02-24 – 2016-09-19.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 9,744 hrs · 4,796 cycles
UPON CLOSING, FLOORBOARDS FOUND CRACK IN LIGHTNING HOLE AT FS 512 UNDER FLOORBOARD 56 MARKED WITH RED STREAMER.
Part: LUG — CORRODED (ZONE 500) · corrosion level 2 · airframe 9,744 hrs · 4,796 cycles
DURING MLG STRUCTURAL INSPECTION, FOUND LT FWD SPONSON LUG CORRODED IN ID. DURING MLG STRUCTURAL INSPECTION FOUND LT AFT SPONSON LUG CORRODED IN ID.
Part: LUG — CORRODED (LT WING) · corrosion level 2 · airframe 9,744 hrs · 4,796 cycles
DURING MLG STRUCTURAL INSPECTION FOUND LT FWD SPONSON LUG CORRODED IN ID. DURING MLG STRUCTURAL INSPECTION FOUND LT AFT SPONSON LUG CORRODED IN ID.
Part: ANGLE — CRACKED (LT WING) · airframe 9,744 hrs · 4,796 cycles
THE VERTICAL BREATHER ANGLE BEHIND THE RT MLG UNDER PANEL 22-LOWER-T/E-2 IS CRACKED.
Part: LUG — CORRODED (ZONE 500) · airframe 9,744 hrs · 4,796 cycles
DURING MLG STRUCTURAL INSPECTION FOUND LT FORWARD SPONSON LUG CORRODED IN ID. DURING MLG STRUCTURAL INSPECTION FOUND LT AFT SPONSON LUG CORRODED IN ID.
Part: LUG — CORRODED (ZONE 500) · airframe 9,744 hrs · 4,796 cycles
DURING MLG STRUCTURAL INSPECTION FOUND RT FORWARD SPONSON LUG CORRODED IN ID. DURING MLG STRUCTURAL INSP FOUND RT AFT SPONSON LUG CORRODED IN ID.
Part: LUG — CORRODED (ZONE 600) · corrosion level 2 · airframe 9,744 hrs · 4,796 cycles
DURING MLG STRUCTURAL INSP FOUND LT FWD SPONSON LUG CORRODED IN ID. DURING MLG STRUCTURAL INSPECTION FOUND LT AFT SPONSON LUG CORRODED IN ID.
Part: ANGLE — CRACKED (LT WING) · airframe 9,744 hrs · 4,796 cycles
THE VERTICAL BREATHER ANGLE BEHIND THE LT MLG UNDER PANEL 21 LOWER T/E-2 IS CRACKED.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 9,744 hrs · 4,796 cycles
UPON CLOSING FLOORBOARDS FOUND CRACK IN LIGHTNING HOLE AT FS 512 UNDER FLOORBOARD 56 MARKED WITH RED STREAMER.
Part: ANGLE — CRACKED (RT WING) · airframe 9,744 hrs · 4,796 cycles
THE VERTICAL BREATHER ANGLE BEHIND THE RT MLG UNDER PANEL 22-LOWER T/E-2 IS CRACKED.
Part: PIN — WORN (THRUST REVERSER) · airframe 9,436 hrs · 4,626 cycles
RIGHT REVERSER UNLOCK CAS MSG CLIMBING THRU 28000 FT AT 300 KT. COMPLIED WITH QRH CHECKLIST & LANDED. ACTIVATED RT THRUST REVERSER IAW CMP 780012. PERFORMED T/R UNLOCK OPERATIONAL TEST IAW MM 78-00-00, ALL SWITCHES CHECKED GOOD. DURING OPERATIONS CHECK FOUND T/R ACTUATOR & UPPER & LOWER PUSH ROD ATTACH POINTS HAVE EXCESSIVE PLAY. REMOVED WORN T/R PINS FROM FWD & AFT POSITIONS OF RT T/R PUSH RODS & WORN PIN FROM FWD ACTUATOR ATTACH POINT IAW MM 78-00-00. INSTALLED NEW PINS IN RT T/R PUSH RODS FWD & AFT POSITIONS & FWD ACTUATOR ATTACH POINT IAW MM 78-00-00. PERFORMED T/R OPERATIONAL TEST IAW CMP 783010. OPERATIONS CHECKED GOOD AT THIS TIME. PN 1159PM41561-47, NSN 1159PM41561-49, NSN 1159PM41561-43, NSN.
Earlier reports · 2005–2014 · 7 reports
2014
Part: UNKNOWN — SMOKE (CABIN) · airframe 7,687 hrs · 3,756 cycles
EXTREME SMOKE IN CABIN WHEN AIR IS ON. COULD NOT DUPLICATE PILOT DISCREPANCY. PERFORMED BORESCOPE OF APU INLET & NOTED SOME COKING ON STATOR BLADE BETWEEN THE 4 & 8 O'CLOCK POSITION. SERVICED APU WITH .9 QTS OF BP2380 ENG OIL. PERFORMED 1.5 HOUR APU RUNS WITH BLEED AIR IN AUTO, MAN & HOT & COLD. PERFORMED SECOND BORESCOPE OF APU INLET, NO OIL DETECTED. CHECKED POST RUN APU OIL LEVEL & NOTED ZERO CONSUMPTION. POWERED UP CABIN & GALLEY SYSTEMS FOR 5 HOURS WHILE PERFORMING OTHER MX, NO SMOKE NOTED. INSPECTED APU LOAD CNTRL VLV FOR OIL RESIDUE, NO DISCREPANCY NOTED. CLEANED COALESCE SOCKS LAW 21-01-12 & REINSTALLED. OPERATIONS & LEEK CHECKED GOOD. PERFORMED LT & RT ENGINE RUNS WITH WING & ENGINE COWL ANTI-ICE SELECTED & CHECKED FOR CABIN SMOKE, NO DISCREPANCY NOTED.
2012
Part: UNKNOWN — ODOR (CABIN) · airframe 6,866 hrs · 3,325 cycles
ON TAKEOFF FROM ASE ABOUT 10000 FT, A STRONG EXHAUST ODOR CAME FROM THE CABIN. AT A SAFE ALTITUDE, WENT BACK AND CHECKED EVERYTHING- THE ODOR HAD DISAPPEARED 2 MINUTES LATER. SPOKE WITH PAX AND ASKED IF THEY WOULD LIKE TO RETURN TO DEPARTURE. CONTINUED TO DESTINATION WITH OUT INCIDENT. INSPECTED AFT BAGGAGE AREA FOR FUEL LEAKS. NO DEFECTS NOTED. REMOVED LOWER COWLING FROM RT ENGINE AND INSTALLED DEFUEL HOSE. TRANSFERRED FUEL FROM BOTH WINGS TO FUSELAGE TANK. LET ACFT SIT OVERNIGHT. NO DEFECTS NOTED. TRANSFERRED FUEL BACK TO WINGS IAW MM 28-41-00. RECONNECTED FUEL LINE ON RT ENGINE AND LEAK CHECKED. NO LEAKS NOTED. REINSTALLED ITEMS REMOVED FOR INSPECTION OF BAGGAGE COMPARTMENT.
2007
Part: PRESSURE SWITCH — UNKNOWN (NLG STEERING) · airframe 3,262 hrs · 1,504 cycles
AFTER TAKEOFF, STEER BY WIRE FAIL LIGHT, ILLUMINATED THEN WENT OUT AFTER 5 MINUTES
Part: UNKNOWN — WARNING LIGHT (NLG STEERING)
AFTER TAKEOFF, NOSE WHEEL STEERING FAIL MESSAGE ILLUMINATED. OPEN
Part: SHUTOFF VALVE — FAILED (NLG STEERING) · airframe 2,996 hrs · 1,428 cycles
NOSE WHEEL STEERING FAIL MESSAGE, FOUND STEERING SHUTOFF VALVE INOP.
2005
Part: PDB — BURNED (DC VOLTAGE) · airframe 1,429 hrs · 698 cycles
RIGHT DC VOLTAGE WENT TO ZERO. FOUND PDB TERMINAL BURNED.
Part: SOLENOID VALVE — UNKNOWN (MLG) · airframe 548 hrs · 281 cycles
STEER BY WIRE FAIL, CAS MESSAGE CAME ON WHEN LANDING GEAR EXTENDED.