Textron 560XL

Service difficulty reports · 3,810

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '560XL'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DXTA2016081206279Brake Cable · frayedRIGHT BRAKE PEDAL TRAVEL, INPUT NEEDS TO BE EVALUATED. TOE PEDAL HAS TO BE PRESSED FULLY TO MECHANICAL STOP TO EVEN BEGIN A BRAKING RESPONSE AND WILL NOT STOP ACFT DURING TAXI WITHOUT USE OF OTHER BRAKE. NO FLUID LEAKS NOTED. FOUND 2 PILOT RT BRAKE PEDAL CAAug 12, 2016 · N554QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2016081206278Coalescer Bag · dirtySMOKE IN COCKPIT/CABIN AFTER TAKEOFF. SLIGHT BURNING OF EYES AND THROAT. REPLACED COALESCER BAG, PN: 83237-12.Aug 12, 2016 · N629QS · Cessna 560XL · Humidity Control SystemSDR DXTA2016081206277Brake Sys · malfunctionedON TAXI OUT, THE CB POPPED OUT FOR THE POWER BRAKES, AFTER A FEW MINUTES, RESET CB AND RETURNED TO RAMP. AFTER STOPPED ON RAMP, PULLED CB FOR POWER BRAKES. INSPECTED POWER BRAKE AND ANTI-SKID BRAKE SYSTEM, NO DEFECTS NOTED. IAW CUSTOMER REQUEST, REPLACED HYAug 12, 2016 · N583QS · Cessna 560XL · Landing Gear Brake SystemSDR J4YR201608081463Bolt · shearedDURING THE TAKEOFF ROLL THE PILOT NOTICED A VERY MODERATE SHIMMY OF THE ACFT NOSE WHEEL AND ELECTED TO ABORT THE TAKEOFF AND RETURN TO THE RAMP. UPON A VISUAL INSPECTION OF THE NOSE WHEEL STEERING SYS 2 OUT OF THE 3 BOLTS ATTACHING THE STEERING GEAR, PN 66426Aug 5, 2016 · N470SK · Cessna 560XL · Landing Gear Steering SystemSDR CWQR20160803027Cable · frayedELEVATOR FORWARD TRIM CABLE ASSEMBLY LOCATED BELOW COCKPIT FLOOR, WAS REPLACED, FOUND NUMEROUS WIRES BROKEN.Aug 3, 2016 · N663QS · Cessna 560XL · Elevator Tab Control SystemSDR 9JLA2016102010768Circuit Board · failedTHE FLIGHT CREW REPORTED INTERMITTENT TROUBLE WITH THE NR 1 ENGINE NOT STARTING. MAINTENANCE TROUBLESHOT AND FOUND THE START CONTROL PCB WAS DEFECTIVE. THE DEFECTIVE PCB WAS REMOVED AND A NEW PCB INSTALLED P/N 6318324-5Jul 28, 2016 · N560HN · Cessna 560XL · Engine Starting System WiringSDR JGVR20160808001Attach Fitting · corrodedCENTER WING TO FUSELAGE, FWD ATTACH FITTING HAS DEEP CORROSION ON THE BOTTOM.Jul 28, 2016 · N618QS · Cessna 560XL · Wing, Attach FittingsSDR DXTA2016072706274Antenna · detachedTHE HF ANTENNAE IS DETACHED FROM THE VERTICAL STABILIZER AND IS HANGING FROM TOP OF FUSELAGE. TECH DISCOVERED DAMAGE TO TAILCONE WHILE PERFORMING MEL PROCEDURE. REMOVED HF ANTENNA SUPPORT SLEEVE & ELBOW AND INSTALLED HF ANTENNA, HF ANTENNA SUPPORT SLEEVE, ELJul 28, 2016 · N602QS · Cessna 560XL · HF Communications SystemSDR O2GA2016082250301Horn · defectiveHIGH SPEED BUFFET EXPERIENCED BETWEEN 250 AND 290 KTS AT FL160. BUFFET INCREASES WITH SPEED. ALSO, NOTICED LT AILERON SHUTTERING. MAINTENANCE REPLACED LT AILERON TRIM TAB HORN ASSEMBLY AND HARDWARE. A SUCCESSFUL OPS CHECK FLIGHT WAS PERFORMED. ACFT WAS REJul 27, 2016 · N503UP · Cessna 560XL · Aileron Tab Control SystemSDR CWQR20160725026Skin · corrodedCORROSION WAS DISCOVERED ON THE VERTICAL STABILIZER SKIN. THE CORROSION WAS REMOVED AND VERTICAL STABILIZER SKINS WERE REPAIRED IAW ERO-850036, REV IR.Jul 25, 2016 · N678QS · Cessna 560XL · Vertical Stabilizer, Plate/SkinSDR CWQR20160725025Skin · corrodedCORROSION WAS DISCOVERED ON THE VERTICAL STABILIZER SKIN. THE CORROSION WAS REMOVED AND VERTICAL STABILIZER SKINS WERE REPAIRED IAW ERO-850036, REV IR.Jul 25, 2016 · N678QS · Cessna 560XL · Vertical Stabilizer, Plate/SkinSDR DXTA2016072206269Display · malfunctionedPILOT SIDE PRIMARY FLIGHT DISPLAY GOT EXCESSIVELY HOT AND BURNED A HOLE IN THE IMAGE. R & R NR 1 PFD WITH NEW, REPAIRED UNIT IAW AMM 34-26-00. OPS CHECK GOOD INSPECTED CONNECTOR BEHIND PFD 1 WITH NO DEFECTS.Jul 22, 2016 · N558QS · Cessna 560XL · Central DisplaySDR CWQR20160720024Cable · unserviceableTHIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLED.Jul 20, 2016 · N651QS · Cessna 560XL · Elevator Tab Control SystemSDR CWQR20160720023Cable · brokenTHIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLED.Jul 20, 2016 · N651QS · Cessna 560XL · Elevator Tab Control SystemSDR CWQR20160720022Cable · brokenTHIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLEDJul 20, 2016 · N696QS · Cessna 560XL · Elevator Tab Control SystemSDR CWQR20160720021Cable · frayedTHIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLED.Jul 20, 2016 · N696QS · Cessna 560XL · Elevator Tab Control SystemSDR O2GA2016071551101Actuator · intermittentUPON GEAR RETRACT NOSE GEAR LIGHT WOULD NOT EXTINGUISHED. MAINTENANCE REPLACED THE NOSE LANDING GEAR ACTUATOR. GEAR SWINGS PERFORMED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RTS.Jul 13, 2016 · N511UP · Cessna 560XL · Landing Gear ActuatorSDR O2GA2016071850001Wire Harness · defectiveLEFT ENGINE ITT GUAGE INOPERATIVE IN FLIGHT. MAINTENANCE REPLACED DEFECTIVE ENGINE T1 HARNESS. ENGINE RUNS PERFORMED AND OPERATIONAL CHECKS WERE GOOD. A SUCCESSFUL OPERATIONAL CHECK WAS ALSO PERFORMED. AIRCRAFT WAS RTS.Jul 12, 2016 · N500UP · Cessna 560XL · Engine Indicating System WiringSDR O2GA2016071551501Switch · intermittentFLAPS DO NOT ALWAYS MOVE TO POSITION WITH FLAP HANDLE. MUST BE JIGGLED FOR THEM TO MOVE. MAINTENANCE REPLACED THE FLAP RETRACT SWITCH. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Jul 10, 2016 · N515UP · Cessna 560XL · Trailing Edge Flap Control SystemSDR CWQR20160701020Hose · blownDURING A SCHEDULED MAINTENANCE GEAR SWING THE RT GEAR UP-LOCK HOOK EXTEND HOSE ASSY, BLEW A HOLE IN IT ABOUT .5 INCH FROM THE SWEDGED FITTING HOSE END. THIS IS THE HOSE END THAT ATTACHES TO THE UP-LOCK ACTUATOR FITTING. NO MAINTENANCE PERSONNEL WERE HURT OR DAJul 1, 2016 · N696QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR CWQR20060622019Hinge Bracket · crackedDURING A SCHEDULED INSPECTION, WE FOUND THE LT OTBD ELEVATOR HINGE BRACKET CRACKED. THE BRACKET IS A CASTING AND IS CRACKED IN THE RADIUS WHERE IT ATTACHES TO THE HORIZONTAL STABILIZER. THE RADIUS CRACK IS .20" LONG WAS FOUND VISUALLY AND CONFIRMED WITH EDDYJun 22, 2016 · N651QS · Cessna 560XL · Elevator StructureSDR CWQR20060622018Stringer · crackedDURING A SCHEDULED INSPECTION, WE FOUND STR 6612026-3 CRACKED WHERE IT IS ATTACHED TO THE AFT CANTED FUSELAGE BULKHEAD. THE CRACK IS THE LENGTH OF VERTICAL LEG AND STARTS AT THE END OF THE STR EXCURSION BULB AREA.Jun 22, 2016 · N607QS · Cessna 560XL · Fuselage Main, Longeron/StringerSDR 9JLA201609308428Windshield · crackedFLIGHT CREW REPORTED THAT THE RIGHT HAND FORWARD FACING WINDSHIELD OUTER PANEL CRACKED DURING FLIGHT. THE WINDSHIELD WAS REPLACED WITH A NEW UNIT AND THE AIRCRAFT WAS RETURNED TO SERVICE.Jun 20, 2016 · N212CE · Cessna 560XL · Flight Compartment WindowsSDR CWQR20160616017Attach Bracket · crackedDURING SCHEDULED MAINTENANCE, WE FOUND THIS RT AVIONICS ATTACH BRACKET CRACKED .7500", HALF OF THE BRACKETS LENGTH. REPLACED ATTACH BRACKET WITH NEW.Jun 16, 2016 · N609QS · Cessna 560XL · Electronic Shelf SectionSDR DXTA2016061406256Brake Sys · contaminatedON TAXI OUT, THE BRAKE PEDALS TRAVEL APPROXIMATELY 3 QUARTERS OF THE WAY BEFORE THE BRAKES CATCH. AFTER PUMPING THE BRAKES THE BRAKES WILL CATCH APPROXIMATELY 1 QUARTER OF THE WAY THROUGH THE TRAVEL THEN BLEED BACK DOWN TO NOT CATCHING UNTIL 3 QUARTERS OF THEJun 14, 2016 · N677QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2016061406257Brake Sys · contaminatedLEFT BRAKE PEDAL DEFLECTED 2-3" MORE THAN THE RIGHT, UPON LANDING. LEFT BRAKE PEDAL REQUIRES MORE DEFLECTION AND FEELS SPONGY COMPARED TO THE RIGHT. PERFORMED MLG BRAKE BLEED PROCEDURE IAW AMM 32-44-00. OPS CK GOOD. PERFORMED BRAKE CABLE INSPECTION IAW AMMJun 14, 2016 · N611QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2016060306253Engine · unserviceableDURING CLIMBOUT AT APPROXIMATELY 12,000 FT, THE RT ENGINE OIL PRESSURE WENT TO ZERO. IT WAS IMMEDIATELY FOLLOWED BY A RED MASTER WARNING LIGHT AND A LOW OIL PRESSURE LIGHT. AFTER COMPLETING THE EMERGENCY CHECKLIST, THE GAUGE RETURNED TO NORMAL WITH A REDUCEDJun 9, 2016 · N624QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR CVGA2016F00138Brake Sys · malfunctionedWITH APU RUNNING, TECH NOTED, LOW BRAKE PRESSURE/ANTI-SKID ANNUNCIATOR ILLUMINATED, THIS WAS THE INCOMING DISCREPANCY. VERIFIED PARKING BRAKE WAS SET AND PROPER/NORMAL BRAKE PEDAL PRESSURE WHEN BRAKE PEDALS ACTUATED. CHOCKED AC. STARTED RT AND LT ENGINE, PJun 8, 2016 · N503QF · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2016060506251Unknown · fumesFUEL FUMES DETECTED IN FLIGHT. MOST PRONOUNCED FROM LT SUPPLY COCKPIT ARM REST HOLES BY WINDOW, OVERHEAD VENTS DON'T SEEM TO HAVE FUEL ODOR. UNABLE TO DETECT FUMES IN CABIN, ONLY COCKPIT. INSPECTED BOTH ENGINES AND THE APU FOR FUEL AND OIL LEAKS. CHECKED BJun 6, 2016 · N669QS · Cessna 560XL · Air Distribution SystemSDR 9JLA201609308425Button · disengagedSHORTLY AFTER T/O FOR A REPOSITION FLT FROM SDL TO LAS, EXPERIENCED A FAULT WITH THE FLT DIR CONTROLLER IN THE VERTICAL MODE ON BOTH PILOTS A COPILOTS CONTROLLERS. CREW REPORTED, WERE UNABLE TO ENGAGE EITHER V/S OR F/C MODES ON EITHER SIDE. CREW INDICATED THJun 3, 2016 · N212CE · Cessna 560XL · Autopilot SystemSDR DXTA2016052006242Apu · smokeWHILE STARTING APU, CABIN IMMEDIATELY FILLED UP WITH THICK, ACRID SMOKE. REMOVED APU IAW MM 49-10-00. DRAINED REMOVED APU OF OIL. CLEANED APU CONTAINMENT BOX & FLUSHED DRAIN LINES. INSTALLED APU IAW MM 49-10-00. R&R CONDENSER SOCK, PN 83237-12, IAW MM 21-May 25, 2016 · N609QS · Cessna 560XL · APU Core EngineSDR CWQR20160519016Control Cable · frayedDURING A SCHEDULED INSPECTION WE FOUND THE ELEVATOR TRIM CABLE FRAYED BEYOND LIMITS. THIS CABLE IS LOCATED UNDER THE PILOTS SEAT & ROLLS OVER A SMALL DIAMETER PULLEY. THIS CONDITION HAS BEEN FOUND ON EIGHTEEN AIRPLANES IN THE FLEET. THIS CONDITION HAS BEEN May 19, 2016 · N691QS · Cessna 560XL · Elevator Tab Control SystemSDR CWQR20160519015Bracket · crackedDURING A SCHEDULED INSPECTION WE FOUND THIS AVIONICS BAY SHELF BRACKET CRACKED ABOUT 50% OF ITS LENGTH. R & R BRACKET. THIS IS THE TENTH ACFT WHERE WE HAD SEEN THIS SAME BRACKET CRACKED. A SERVICE CONDITION REPORT HAS BEEN SENT TO MFG UNDER SCR 758186.May 19, 2016 · N691QS · Cessna 560XL · Electronic Shelf SectionSDR 2016FA0000276Spring · missingDURING AN UNSCHEDULED INSPECTION OF THE FLIGHT CONTROL GUST LOCK SYSTEM, IT WAS NOTED THAT THE LT AILERON STOP ARM SPRING WAS MISSING. AN INSPECTION OF THE RELEVANT ZONE DID NOT FIND THE SPRING IN THE AREA. IT APPEARS THAT THE SPRING HAS BEEN MISSING SINCE TMay 13, 2016 · N95NB · Cessna 560XL · Flight Control SystemSDR 17GR2016051600005Skin · abnormalCOMPLING WITH THE INSPECTION IN ACFT, WE FOUND THAT THE PAINT HAD FLAKED OFF OF THE TOP OF THE SECTOR LEAVING EXPOSED METAL. ONCE REMOVED WE COULD FLAKE THE REMAINING PAINT WITH A FINGER NAIL. IT APPEARED THAT THE PAINT HAD BEEN APPLIED WITH A BRUSH RATHER THMay 13, 2016 · N851AC · Cessna 560XL · AileronsSDR 9JLA2016092814774Control Handle · defectiveAFTER DEPARTURE THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR WHEN THE GEAR CONTROL HANDLE WAS SELECTED UP. THE CREW WAS ABLE TO RETURN AND LAND WITHOUT INCIDENT. TROUBLESHOOTING IDENTIFIED THE LANDING GEAR CONTROL HANDLE FAULTY. INSTALLED NEW CONTROL AND REMay 12, 2016 · N909LA · Cessna 560XL · Landing Gear SelectorSDR O2GA2016042550701Proximity Switch · out of adjustNO TAKEOFF WARNING HORN & MASTER CAUTION ILLUMINATED DURING TAKEOFF. ABORTED TAKEOFF. ADJUSTED ELEVATOR TRIM POINTER & PROXIMITY SWITCH. TAKEOFF WARNING SYS OPERATIONAL CHECKED GOOD DURING ENG RUNS & HIGH SPEED TAXI. ACFT WAS RETURNED TO SERVICE.Apr 20, 2016 · N507UP · Cessna 560XL · Elevator Control SystemSDR DXTA2016041306231Torque Tube · corrodedLEFT ELEVATOR TORQUE TUBE CORRODED OUT OF LIMITS. FOUND DURING COMPLETE PAINT PROCESS. REMOVED TORQUE TUBE, PN UNKNOWN, FROM LT ELEVATOR PN 6634200-9, SN 0000106 DUE TO LEVEL 2 CORROSION. INSTALLED NEW TORQUE TUBE PN 6634002-15 IAW SRM 51-40-03, 51-40-04, 5Apr 13, 2016 · N648QS · Cessna 560XL · Elevator Control SystemSDR DXTA2016041306230Torque Tube · corrodedRIGHT ELEVATOR TORQUE TUBE CORRODED OUT OF LIMITS. FOUND DURING COMPLETE PAINT PROCESS. REMOVED TORQUE TUBE DUE TO LEVEL 2 CORROSION. INSTALLED NEW TORQUE TUBE PN 6634002-16 IAW SRM 51-40-03, 51-40-04, 51-40-05, 51-40-06, 55-20-01 & MM 20-32-00. THIS IS COApr 13, 2016 · N648QS · Cessna 560XL · Elevator Control SystemSDR DXTA2016041306225Skin · damagedAIRCRAFT HAS HAIL DAMAGE. R & R THE LT & RT AILERONS IAW MM 27-10-01 & SRM 51-60-00 & 51-60-01. R & R THE LT & RT ELEVATORS IAW MM 27-31-01 & SRM 51-60-00 & 51-60-02. PARTS REPLACED RT AILERON PN 6624032-3, SN 0000070, ELEVATOR PN 6634200-9 & SN 0000313 & EApr 13, 2016 · N589QS · Cessna 560XL · AileronsSDR DXTA2016040606222Control Handle · inoperativeLANDING GEAR WOULD NOT RETRACT. GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RAN APPROPRIATE CHECKLIST & RETURNED FOR LANDING. REMOVED NON-FUNCTIONING LG CONTROL HANDLE, PN 9912550-1 SN 025 & INSTALLED A OVERHAULED LG CONTROL HANDLE, PN 049801-001 SN H546Apr 10, 2016 · N682QS · Cessna 560XL · Landing Gear SelectorSDR DXTA2016041006222Not Reported · unknownLANDING GEAR WOULD NOT RETRACT. GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RAN APPROPRIATE CHECKLIST & RETURNED FOR LANDING.Apr 10, 2016 · N682QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR DXTA2016040106219Shutoff Valve · unserviceableAFTER TURNING XFEED OFF, THERE WAS A LOW FUEL PRESS LIGHT, THEN MASTER CAUTION, THEN R BOOST PUMP ON. RAN CHECKLIST N2 THEN M5 & COULD NOT GET R BOOST LIGHT TO EXTINGUISH. R BOOST PUMP LEFT ON IAW M5 CHECKLIST. R & R RT MOTIVE FLOW SHUTOFF VLV IAW MM 28-21-Apr 1, 2016 · N583QS · Cessna 560XL · Fuel Selector/Shut-Off ValveSDR DXTA2016032506216Pin · backed outACM PRODUCES EXTREMELY HOT AIR REGARDLESS OF MODE, MANUAL OR AUTO, & REGARDLESS OF TEMP SETTING. STRONG ODOR THROUGHOUT ACFT AS TEMP RISES. DISCONNECTED CONNECTOR PTO 49 FROM THE ECU LOW LIMIT CONTROLLER, FOUND PIN F PUSHED BACK, REPOSITIONED PIN. OPERATED Mar 25, 2016 · N577QS · Cessna 560XL · Air Conditioning System WiringSDR W9FA2016032500001Pcb · burnedFOUND RESISTOR R1 BURNED ON PCB NZ021 AND NZ020, BOTH SIDES OF THE BOARD WERE BROWN/BLACK DUE TO EXTREME HEAT. REPLACED BOTH NZ021 AND NZ020 AS PRECAUTIONARY MEASURE. RETURNED ACFT TO SERVICE WITH NO FURTHER PROBLEMS. Mar 24, 2016 · N3 · Cessna 560XL · Engine ControlsSDR DXTA201632306208Pressure Switch · unserviceableUPON LIFT OFF THE ACFT HAD EXCESSIVE PITCH UP. IT REQUIRED EXCESSIVE FULL FWD YOLK PRESS TO MAINTAIN LEVEL FLIGHT & FULL NOSE DOWN TRIM. TROUBLE SHOT EXCESSIVE PITCH UP DISCREPANCY & FOUND THE AIRSPEED SWITCH FAILED. R & R AIRSPEED SWITCH. SYS PASSED LEAK Mar 23, 2016 · N683QS · Cessna 560XL · Stabilizer Control SystemSDR DXTA2016032306208Unknown · not reportedUPON LIFT OFF THE ACFT HAD EXCESSIVE PITCH UP. IT REQUIRED EXCESSIVE FULL FWD YOLK PRESS TO MAINTAIN LEVEL FLIGHT & FULL NOSE DOWN TRIM.Mar 23, 2016 · N683QS · Cessna 560XL · Stabilizer Control SystemSDR CWQR20160323013Attach Bracket · crackedDURING A SCHEDULED INSPECTION WE FOUND THE AVIONICS SHELF FWD OTBD ATTACH BRACKET, PN 9256023-16, CRACKED ABOUT AN INCH LONG, HALF THE LENGTH OF THE ATTACH BRACKET. REPLACED BRACKET & SENT SUBMITTED SERVICE CONDITION REPORT 750316 TO MFG.Mar 23, 2016 · N579QS · Cessna 560XL · Electronic Shelf SectionSDR CWQR20160311012Stringer · crackedDURING A SCHEDULED INSPECTION WE FOUND STRINGER 15L, CRACKED IN THE TAIL CONE SECTION OF THE ACFT. THE CRACK WAS AT THE AFT EDGE OF THE STRINGER WHERE THE BULB PORTION OF THE EXTRUDED STRINGER STOPS & THE STRINGER IS TAPER CUT BEFORE TERMINATING. A REPORT HAMar 11, 2016 · N677QS · Cessna 560XL · Aerodynamic FairingsSDR RT5R2016031100001Fire Loop · chafedFOUND THE ENGINE FIRE DETECTION WIRE HAD BEEN CONTACTING THE AIRFRAME LT SIDE YOKE, ENGINE ATTACH YOKE, IN THE AREA WHERE THE FIRE DETECTION WIRE IS ROUTED ON THE INBD SIDE OF THE ENGINE AROUND THE ENGINE FLANGE, FAN CASE TO ENGINE INTERMEDIATE CASE. THE FIREMar 10, 2016 · N643QS · Cessna 560XL · Fire Detection
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