# Service difficulty reports: N318QS, cancelled May 13, 2011 A list on [N318QS, cancelled May 13, 2011](https://openairdocs.org/deregistered/N318QS-2011-05-13.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2010030504014](https://openairdocs.org/sdr/DXTA2010030504014.md): Brake · malfunctioned · Mar 4, 2010 · N318QS · Cessna 560CESSNA · Landing Gear Brake System > ON TAXI OUT THE CO PILOTS RT BRAKE WAS GRABBING AND WAS DIFFICULT TO KEEP THE ACFT STRAIGHT ON TAXIWAY. THE RT BRAKE SEEMED HARDER PRESSURE THAN LT. THE LT BRAKE ACTION SEEMED TO BE REACTING APPROPRIATELY. (LT SEAT POSITION BRAKES SEEMED ALMOST NORMAL, WITH - [SDR DXTA2010012703957](https://openairdocs.org/sdr/DXTA2010012703957.md): Master Cylinder · weak · Jan 26, 2010 · N318QS · Cessna 560CESSNA · Master Cylinder/Brake Valve > COPILOT SIDE, RT BRAKE PEDAL GOES SOFT DURING TAXI. AFTER PEDAL WAS ALMOST TO THE FLOOR, RELEASED PRESSURE, AND BRAKING WAS RESTORED. THIS HAPPENED 5 TIMES ON A 2 MILE TAXI. R & R COPILOTS RT MASTER CYLINDER IAW MM CHP 32-42-01. BLEED SYS IAW MM CHP 32-42-20. - [SDR DXTA2010012503956](https://openairdocs.org/sdr/DXTA2010012503956.md): Pedal · failed · Jan 24, 2010 · N318QS · Cessna 560CESSNA · Landing Gear Brake System > WHILE TAXIING FROM RT SEAT, THE RT BRAKE PEDAL WENT ALL THE WAY DOWN TO THE FLOOR. PERFORMED RT BRAKE BLEEDING PROCEDURES 4 TIMES IAW MM CH 32-42-00. - [SDR DXTA2010012203950](https://openairdocs.org/sdr/DXTA2010012203950.md): Brake Assy · weak · Jan 21, 2010 · N318QS · Cessna 560CESSNA · Landing Gear Brake System > DURING TAXI FO SIDE RT BRAKE PEDAL WENT ALL THE WAY DOWN WITH NO PRESSURE. BLED RT BRAKE IAW MM 32-42-00. PERFORMED TAXI CHECK. OPS CHECK GOOD IAW MM 32-42-01. - [SDR DXTA2009121603898](https://openairdocs.org/sdr/DXTA2009121603898.md): Rod · out of adjust · Dec 6, 2009 · N318QS · Cessna 560CESSNA · Fuel Control/Reciprocating Engines > WHEN RT THROTTLE WAS RETARDED TO IDLE AFTER SPEED BRAKE CHECK, RT ENGINE FLAMED OUT. N1, N2, AND ITT WENT SMOOTHLY TO ZERO. OPERATED RT ENG AND DUPLICATED DISCREPANCY. CHECKED RIGGING OF RT ENG. ADJUSTED FCU/FLOW DIVIDER INTERCONNECT ROD AND SET FWD CUTOFF - [SDR DXTA2009090303771](https://openairdocs.org/sdr/DXTA2009090303771.md): Display · inoperative · Sep 4, 2009 · N318QS · Cessna 560CESSNA · Flight Environment Data > DISPLAY FAILED ON TAXI, SEC FLT DISPLAY CIRCUIT BREAKER POPPED, ACRID ODOR IN COCKPIT BREAKER WAS NOT RESET. CONFIRMED FAILURE INSIDE INDICATOR. INSPECTED ALL SECONDARY FLIGHT DISPLAY WIRING. NO FAULTS FOUND. SECONDARY FLIGHT DISPLAY OPS CHECKS GOOD PER MM 3 - [SDR DXTA200809103272](https://openairdocs.org/sdr/DXTA200809103272.md): Control Valve · inoperative · Sep 10, 2008 · N318QS · Cessna 560CESSNA · Windshield/Door Rain/Ice Removal > DURING TAKEOFF ROLL AT 50 KNOTS W/S AIR O-HEAT ANNUNCIATOR LIGHT ILLUMINATED, PERFORMED ABORT. WHEN POWER WAS REDUCED LIGHT WENT OUT. REMOVED WINDSHIELD BLEED AIR CONTROL VALVES DUE TO "OVERHEAT" ON TAKE OFF. INSTALLED OVERHAULED VALVE IAW MM 30-41-00, OPS - [SDR DXTA200803272](https://openairdocs.org/sdr/DXTA200803272.md): Warning Light · illuminated · Sep 10, 2008 · N318QS · Cessna 560CESSNA · Central Warning > DURING TAKEOFF ROLL AT 50 KNOTS W/S AIR O-HEAT ANNUNCIATOR LIGHT ILLUMINATED, PERFORMED ABORT. (K) - [SDR DXTA200803022](https://openairdocs.org/sdr/DXTA200803022.md): Brake Sys · malfunctioned · Apr 24, 2008 · N318QS · Cessna 560CESSNA · Landing Gear Brake System > COPILOT'S LT BRAKE PEDAL REQUIRES SIGNIFICANTLY MORE TILT TO ENGAGE BRAKE THAN RT PEDAL, NO VISIBLE FLUID OR LEAKS. BLED BRAKES IAW MM 32-42-00. OPS CHECK GOOD. - [SDR DXTA200702100](https://openairdocs.org/sdr/DXTA200702100.md): Brake · weak · Apr 11, 2007 · N318QS · Cessna 560CESSNA · Landing Gear Brake System > CO-PILOT LT BRAKE IS (SOFT). [SUP 4-19-07] USED BRAKE BLEED PROCEDURE FOR ANTI-SKID SYSTEM FOR CO-PILOTS LT BRAKE IAW. CESSNA 560 MM 32-42-00 CHECKS GOOD. - [SDR DXTA200601757](https://openairdocs.org/sdr/DXTA200601757.md): Squat Switch · out of adjust · Nov 25, 2006 · N318QS · Cessna 560CESSNA · Cabin Pressure Control System > LEVEL AT 13,000 MSL, RAPID PRESSURIZING OCCURRED. CABIN CLIMBED AT 6000 FPM. RATE OF CLIMB OR SOURCE SELECT KNOB HAS NO EFFECT. CABIN ATITUDE SELECTOR SET AT 400 MSL (BASICLLY SEA LEVEL). CABIN ALTITUDE STABILIZED AT AIRCRAFT ALTITUDE AND 13,000 MSL. OXYG - [SDR 2006FA0000497](https://openairdocs.org/sdr/2006FA0000497.md): Threshold · cracked · May 9, 2006 · N318QS · Cessna 560CESSNA · Fuselage Main, Structure > CABIN ENTRY THRESHOLD CRACKED AT AFT STEP ATTACH BOLT HOLE. COMBINATION OF BOLT HOLE LOCATED IN RADIUS OF FRAME AND MATERIAL THICKNESS NOT SUFFICIENT TO SUPPORT WEIGHT OF PERSON ENTERING OR EXITING AIRCRAFT. RECOMEND STRENGTHING STRUCTURE, USING THICKER META - [SDR DXTA200601198](https://openairdocs.org/sdr/DXTA200601198.md): Wire · broken · Jan 16, 2006 · N318QS · Cessna 560CESSNA · Landing Gear System Wiring > LEFT MAIN LANDING GEAR FAILED TO RETRACT AFTER T/O. RED -UNLOCK- LIGHT REMAINED ILLUMINATED AS WELL AS THE LEFT MAIN -DOWN & LOCKED- LIGHT. AFTER RECYCLING THE GEAR, IT RETRACTED NORMALLY. THE -HYDRAULIC PRESS- LIGHT EXTINGUISHED AT THE NORMAL SEQUENCE. HE - [SDR DXTA200500737](https://openairdocs.org/sdr/DXTA200500737.md): Retract Cylinder · damaged · May 22, 2005 · N318QS · Cessna 560CESSNA · Landing Gear Retraction/Extension System > LEFT MAIN WOULD NOT RETRACT. - PERFORMED GEAR SWINGS AND TROUBLESHOOTING IAW CE560 MM CHAPTER 32-30-00 WITH NO DISCREPANCIES NOTED. SUSPECTED MLG RETRACT ACTUATOR, REMOVED LEFT MAIN GEAR ACTUATOR AND INSTALLED AN INSPECTED ACTUATOR IAW CE 560 MM 32-31-04. PERF - [SDR DXTA200400335](https://openairdocs.org/sdr/DXTA200400335.md): Motor · burned out · Jul 12, 2004 · N318QS · Cessna 560CESSNA · Cabin Cooling System > DURING SHUT DOWN, VERY STRONG BURNING RUBBER ODOR DETECTED COMING FROM OVERHEAD VENTS. AFTER SHUTDOWN INSPECTED AFT EQUIPMENT BAY AND NOTED VERY STRONG BURNING SMELL BUT COULD NOT DETERMINE WHICH COMPONENT. FOUND AIR CONDITIONING DRIVE MOTOR TO BE AT FAULT. - [SDR DXTA200400263](https://openairdocs.org/sdr/DXTA200400263.md): O-Ring · failed · Mar 15, 2004 · N318QS · Cessna 560CESSNA · Brake Anti-Skid Section > BRAKES FAILED WHILE TAXIING, POWER BRAKE AND ANTI-SKID INOP, ANNUNCIATOR ILLUMINATED. FOUND BRAKE SYSTEM LEAKING FROM THE ANTI-SKID SYSTEM PUMP. REPLACED O-RING, BLED BRAKES & PERFORMED OPS AND LEAK CHECK, NO FURTHER DEFECTS NOTED. ALL WORK WAS DONE IAW CES - [SDR 99ZZZX10](https://openairdocs.org/sdr/99ZZZX10.md): Igniter · damaged · Mar 19, 1998 · N318QS · Cessna 560CESSNA · Spark Plug/Igniter > REMOVED IGNITER FOR PHASE 4 INSPECTION. DETERMINED CENTER ELECRTRODE MISSING. SUBMITTER STATED THIS IS SUPPOSED TO BE NEW STYLE PLUG, TO PREVENT THIS. REPLACED PLUG WITH NEW. BORESCOPED ENGINE. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 n_number = 'N318QS' AND deregistration_id = 'N318QS-2011-05-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N318QS-2011-05-13/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.