# Service difficulty reports: N371QS, cancelled Jun 2, 2011 A list on [N371QS, cancelled Jun 2, 2011](https://openairdocs.org/deregistered/N371QS-2011-06-02.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2010071204148](https://openairdocs.org/sdr/DXTA2010071204148.md): Trim System · loose · Jul 9, 2010 · N371QS · Cessna 560CESSNA · Stabilizer Control System > ON TAKEOFF WITH PITCH TRIM IN TAKEOFF RANGE REQUIRED EXCESSIVE AFT YOKE FORCE TO GET NOSE OFF GROUND. AFTER AIRBORNE FULL NOSE UP TRIM APPLIED & REQUIRES EXCESSIVE AFT YOKE FORCE AT 200 KTS. UPON INITIAL INSP, FOUND ELEVATOR TRIM TAB IN FULL NOSE UP POSITION - [SDR DXTA200902020348A](https://openairdocs.org/sdr/DXTA200902020348A.md): Brake · unserviceable · Jan 31, 2009 · N371QS · Cessna 560CESSNA · Landing Gear Brake System > DURING TAXI, AIRPLANE PULLS LT WHILE BRAKING FROM THE PILOTS SIDE. R&R RT BRAKE ASSY IAW MM 32-42-00. - [SDR 2008FA0000790](https://openairdocs.org/sdr/2008FA0000790.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000789](https://openairdocs.org/sdr/2008FA0000789.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000788](https://openairdocs.org/sdr/2008FA0000788.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000787](https://openairdocs.org/sdr/2008FA0000787.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000786](https://openairdocs.org/sdr/2008FA0000786.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000785](https://openairdocs.org/sdr/2008FA0000785.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000784](https://openairdocs.org/sdr/2008FA0000784.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000783](https://openairdocs.org/sdr/2008FA0000783.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000782](https://openairdocs.org/sdr/2008FA0000782.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000781](https://openairdocs.org/sdr/2008FA0000781.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000780](https://openairdocs.org/sdr/2008FA0000780.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000779](https://openairdocs.org/sdr/2008FA0000779.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR 2008FA0000778](https://openairdocs.org/sdr/2008FA0000778.md): Rib · cracked · Oct 29, 2008 · N371QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/Rib > WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 5 CRACKED RIBS ON THE RT SIDE AND 8 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TH - [SDR DXTA200803065](https://openairdocs.org/sdr/DXTA200803065.md): Actuator · malfunctioned · May 17, 2008 · N371QS · Cessna 560CESSNA · Landing Gear Actuator > UPON LOWERING LANDING GEAR, BOTH MAIN GEAR LIGHTS WERE GREEN, BUT THE NOSE GEAR LIGHT DID NOT ILLUMINATE. REPLACED NLG ACTUATOR WITH REPAIRED UNIT PERFORMED PROPER FUNCTION CHECKS. FUNCTION CHECK SATISFACTORY AT THIS TIME CE560 M/M 32-31-03. - [SDR DXTA200702648](https://openairdocs.org/sdr/DXTA200702648.md): Arm · out of rig · Dec 4, 2007 · N371QS · Cessna 560CESSNA · Landing Gear Retraction/Extension System > AFTER TAKEOFF GEAR WOULDN'T RETRACT. SECURED GEAR AND FOUND BLOW DOWN BOTTLE ARM AND HANDLE/CABLE OUT OF PROPER RIG. RE-RIGGED AND SERVICED BOTTLE. COMPLETED SEVERAL GEAR OPS CHECKS AND GEAR BLOW DOWN. ALL CHECKS GOOD PER CE560 M.M. 32-31-08. - [SDR DXTA200702403](https://openairdocs.org/sdr/DXTA200702403.md): Brake Assy · unknown · Aug 14, 2007 · N371QS · Cessna 560CESSNA · Landing Gear Brake System > COPILOT BRAKE PEDALS NEED TO BE PUSHED ALMOST FULL DOWN BEFORE ANY BRAKE APPLICATION IS FELT. ONCE YOU REACH THAT POINT, THE BRAKE PEDAL "FEEL" IS NORMAL. BLED BRAKE SYSTEM 10 TIMES PER CE560M/M. OPS CHECKS GOOD. PEDALS FEEL NORMAL. SERVICED RESERVOIR. I/A/W C - [SDR DXTA200702398](https://openairdocs.org/sdr/DXTA200702398.md): Master Cylinder · bypassing · Aug 12, 2007 · N371QS · Cessna 560CESSNA · Landing Gear Brake System > DURING TAXI BRAKE CHECK, FOUND COPILOT BRAKE PEDALS WERE VERY SPONGY AND THE PEDAL TRAVEL IS 3 TIMES MORE THAN THE CAPTAINS SIDE. THE RIGHT COPILOT PEDAL IS WORSE AND TRAVELS FARTHER. REMOVED AND REPLACED PILOT AND COPILOT BRAKE MASTER CYLINDERS WITH NEW DUE T - [SDR DXTA200702395](https://openairdocs.org/sdr/DXTA200702395.md): Brake Assy · weak · Aug 9, 2007 · N371QS · Cessna 560CESSNA · Landing Gear Brake System > RT SEAT BRAKES VERY MUSHY WHEN BRAKE PRESSURE APPLIED. M2B- BLED BRAKE SYSTEM PER CHAPTER 32-42-00 OF THE CITATION 560 MM OPERATIONAL AND LEAK CHECK GOOD. - [SDR CWQR200708](https://openairdocs.org/sdr/CWQR200708.md): Support Channel · cracked · Jul 31, 2007 · N371QS · Cessna 560CESSNA · Instrument Panel > DURING MAINTENANCE FOUND THE RUDDER UPPER SUPPORT CHANNEL CRACKED WHERE IT ATTACHES TO THE INSTRUMENT PANEL. THIS AIRCRAFT HAD SL560-27-13 COMPLIED WITH 826.6 HOURS PRIOR TO FINDING THE CRACKED CHANNEL. THIS SL UPGRADED THE ATTACHING HARDWARE BUT DOES NOT CHA - [SDR DXTA200702327](https://openairdocs.org/sdr/DXTA200702327.md): Brake Assy · weak · Jul 10, 2007 · N371QS · Cessna 560CESSNA · Landing Gear Brake System > BRAKES ARE VERY SPONGY USING BOTH SETS OF RUDDER PEDALS. INSPECTED AND BLEED BOTH LT AND RT BRAKE ASSY. NO DEFECTS FOUND, OPS CK GOOD IAW MM CH 32-42-00. - [SDR DXTA200702258](https://openairdocs.org/sdr/DXTA200702258.md): Brake · malfunctioned · Jun 12, 2007 · N371QS · Cessna 560CESSNA · Landing Gear Brake System > ANTI SKID SEEMS TO ACTIVATE AROUND 40 KNOTS. BRAKES SEEM TO GRAB AND RELEASE SERVERAL TIMES. TAXIED AIRCRAFT WITH ANTI-SKID ON. WHEN TAXI WAY WET AND DRY. SYSTEM OPERATIONAL CHECKS GOOD. NO DEFECTS NOTED. WORK DONE IAW. CE 560 MM CHAP. 32-41-00. - [SDR DXTA200702223](https://openairdocs.org/sdr/DXTA200702223.md): Controller · inoperative · May 29, 2007 · N371QS · Cessna 560CESSNA · Windshield/Door Rain/Ice Removal > WITH THE W/S BLEED ANTI ICE ON LOW (APPROX 3-5 MINUTES AFTER BEING SWITCHED ON) THE W/S O'HEAT ILLUMINATED WITH SMOKE/HAZE IN THE COCKPIT AND CABIN ALONG WITH STRONG BURNING ODOR. VERIFIED RIGGING AND OPERATION OF W/S BLEED AIR VALVES, FOUND GOOD. VERIFIED OP - [SDR DXTA200601189](https://openairdocs.org/sdr/DXTA200601189.md): Pump · malfunctioned · Jan 10, 2006 · N371QS · Cessna 560CESSNA · Fuel Boost Pump > LEFT FUEL BOOST PUMP CAME ON DURING TAKEOFF ROLL, ABORTED. PERFORMED RUN UP AFTER RESETTING PUMP, CAME ON AGAIN. PERFORMED 3RD RUN UP ON RAMP, DID NOT COME ON. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200500752](https://openairdocs.org/sdr/DXTA200500752.md): Transducer · inoperative · Jun 2, 2005 · N371QS · Cessna 560CESSNA · Brake Anti-Skid Section > DURING TAXI BOTH PEDALS ON RT SEAT BECAME SOFT, ANTI-SKID LIGHTS CAME ON. AFTER PUMPING THE PEDALS THE LIGHT WENT OUT, AND THE BRAKES FELT NORMAL. THIS HAPPENED THREE SEPERATE TIMES DURING TAXI. REPLACED LT ANTI-SKID TRANSDUCER AND BLED BRAKES. OPS CHECK G - [SDR DXTA200500748](https://openairdocs.org/sdr/DXTA200500748.md): O-Ring · leaking · Jun 1, 2005 · N371QS · Cessna 560CESSNA · Landing Gear Brake System > LOST BRAKE PRESSURE ON TAXI. BRAKE FLUID LEAKING OUT OF RIGHT BRAKE ASSEMBLY. REMOVED AND REPLACED LEAKING O-RING ON BRAKE LINE FITTING. OPS AND LEAK CHECK GOOD IAW BF GOODRICH CMM 32-46-13. - [SDR DXTA200300029](https://openairdocs.org/sdr/DXTA200300029.md): Indicator · malfunctioned · May 6, 2003 · N371QS · Cessna 560CESSNA · Attitude Gyro and Indicating System > DURING TAKEOFF ROLL CAPTAIN'S ATTITUDE INDICATOR INDICATED 5 DEGREES NOSE DOWN WITH 3 DEGREES RIGHT BANK. REJECTED TAKEOFF. FOUND NR 1 VERTICAL GYRO DEFECTIVE. REPLACED UNIT AND OPS CHECKED GOOD. ## 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 = 'N371QS' AND deregistration_id = 'N371QS-2011-06-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N371QS-2011-06-02/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.