N115QS

Cancelled 2014

Deregistered aircraft · Raytheon 400A · Pratt & Whitney Canada JT15D 5 series

Cancelled
April 7, 2014
Exported to
Singapore
Status when cancelled
Valid registration
Serial number
RK-383
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 31, 2004
Certificate issued
March 7, 2014
Last registry action
March 7, 2014
Mode S code
A04035
Owner when cancelled
Fort Lauderdale Aerospace
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 10

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR DXTR20130207002Attach Angle · crackedLT LOWER OTBD THRUST REVERSER CRACKED FROM RIVET. R & R THE LT LOWER OTBD THRUST REVERSER CRACKED ANGLE IAW THE A SRM 51-40-01 AND 51-41-00.Feb 5, 2013 · N115QS · Beech 400A · Engine Thrust ReverserSDR DXTA2012062505016Hinge · crackedDURING LANDING CHECKLIST, PUT LANDING GEAR DOWN WITH 3 POSITIVE GREEN LIGHT INDICATIONS WITH BOTH RED LIGHT IN THE GEAR HANDLE STAYED ILLUMINATED. EXECUTED CHECKLIST WITH NO POSITIVE RESULTS. BOTH RED LIGHT ON THE GEAR HANDLE STAYED ILLUMINATED AT ALL TIME.Jun 24, 2012 · N115QS · Beech 400A · Landing Gear DoorsSDR DXTA2012030804909Terminal · burnedDURING PREFLIGHT INSPECTION, WHEN CABIN SIGN IS PUSHED TO SAFETY RED, CABIN SIGN CIRCUIT BREAKER POPS OUT. HAD AN ELECTRICAL ODOR IN COCKPIT. TROUBLESHOT AND FOUND AFT LAV SEAT BELT LIGHT BAR WITH A SHORTED SOLDER JOINT. RESOLDERED LIGHT BAR IAW MM 20-20-0Feb 27, 2012 · N115QS · Raythn 400ARAYTHEON · Emergency LightingSDR DXTA2011050404573Hinge · vibrationTHERE IS AN INTERMITTENT VIBRATION IN THE CONTROL YOKE. THE VIBRATION IS BOTH TACTILE AND AUDIBLE. IT OCCURS INTERMITTENTLY IN FLIGHT AT ALL ALTITUDES AND AIRSPEEDS. REPLACED IND HINGE ASSY AND ECCENTRIC ON LT OTBD SPOILER. OPS CHECKED SATISFACTORY. ALL WMay 3, 2011 · N115QS · Beech 400A · SpoilersSDR DXTA2009121403895Check Valve · faultyAFTER STARTING BOTH ENGINES AND CALLING FOR TAXI CLEARENCE. THE TOWER INFORMED US THAT THERE WAS GRAYISH SMOKE COMING OUT OF ONE OF THE ENGINES (THEY THOUGHT THE LT SIDE, BUT COULD NOT BE 100 PERCENT CERTAIN) ALL ENGINE PARAMETERS APPEARED NORMAL. REMOVED ANDec 11, 2009 · N115QS · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR DXTA2009062503700Relay · burnedSTRONG ELECTRICAL ACRID ODOR COMING FROM THE LWR LT AFT CIRCUIT BREAKER PANEL. ODOR STARTED 30 MIN AFTER DEPARTURE. SEEMED TO DIMINISH AFTER 10 MIN, BUT ODOR RETURNED 15 MIN BEFORE LANDING AND REMAINED STRONG. REMOVED LT COCKPIT SEAT, LT LOWER AFT SIDEWALL. Jun 25, 2009 · N115QS · Raythn 400ARAYTHEON · Windshield/Door Rain/Ice RemovalSDR DXTA200702350Spoiler Sys · out of rigFLIGHT CONTROLS VERY SLACK/SLOPPY ABOUT THE ROLL AXIS. SPOILER BUZZ NOTED IN TURNS TO THE RT. EXECUTIVE CONTROL INPUT REQUIRED TO INITIATE AND ROLL OUT OF TURNS. ADJUSTED LT AND RT NEUTRAL POINT OF SPOILERS. RIGGED LT SPOILERS DOWN AND RIGGED RT SPOILERS UPJul 19, 2007 · N115QS · Beech 400A · Drag Control SystemSDR DXTA200702292Engine · unknownUPON SETTING TAKEOFF POWER, THE RT ENGINE ITT BEGAN FLUCTUATION BETWEEN 400 - 650 DEGREES. TAKEOFF ABORTED BELOW 70 KTS. [07-12-07] RAN AIRCRAFT TO TAKEOFF POWER FOUND NO FLUCTATION PERFORMED 5 POINT RUNS AND FAXED RESULTS TO MTX ALL PRAMITERS WITHIN LIMITSJun 24, 2007 · N115QS · Beech 400A · Engine Temperature Indicating SystemSDR DXTA200500844Bulb · burned outLOWERED GEAR HANDLE AND ONLY LEFT MAIN GEAR ILLUMINATED DOWN. RAN GEAR EXTENSION CHECKLIST AND STILL ONLY INDICATED LEFT MAIN DOWN. LANDING WAS UNEVENTFUL. REPLACED INDICATOR LIGHT BULBS WITH NEW AND PERFORMED LANDING GEAR RETRACTION TEST IAW HAWKER 400XP MJul 17, 2005 · N115QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200400458Duct · rupturedSMOKE AND EXHAUST APPEARED IN LAV WHEN ENG AND WING ANTI-ICE WAS PLACED ON. EXHAUST SMELLED LIKE OIL AND WAS VERY VISIBLE. IT LEFT A FILM ON LAV MIRROR. FOUND THE SMOKE AND ODOR CAUSED BY A RUPTURE IN THE WING ANTI-ICE BLEED AIR LINE. INSTALLED NEW BLEED ANov 22, 2004 · N115QS · Beech 400A · Airfoil Anti/De-ice System

Other aircraft with N115QS · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N115QS is registered now to the first aircraft listed.