# Service difficulty reports: Cessna 560

A list on [Cessna 560](https://openairdocs.org/model/cessna-560.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 64 reports

- [SDR 2024F00188](https://openairdocs.org/sdr/2024F00188.md): Fcu · unresponsive · Aug 12, 2024 · N579BJ · Gulstm 560 · Fuel Controlling System
  > WHILE EN-ROUTE FROM KJAC TO KMSO, CREW WAS FLYING A NORMAL DESCENT OUT OF FL220 AND WAS CLEARED TO FL150. ENGINES WERE POWERED BACK AS NORMAL. AT LEVEL OFF BOTH ENGINES WERE POWERED UP TO 80%. THE RIGHT ENGINE SPOOLED UP NORMALLY, BUT THE LEFT ENGINE DID NOT.
- [SDR R3WA202401220001](https://openairdocs.org/sdr/R3WA202401220001.md): Seal · leaking · Jan 19, 2024 · N331BR · Gulstm 560 · Passenger/Crew Doors
  > CREW HEARD LOUD SQUEAL FROM PAX DOOR SEAL AREA ALONG WITH SLOW DEPRESSURIZATION. UNDER INVESTIGATION FOR PROBABLE CAUSE.
- [SDR 2023FA0000118](https://openairdocs.org/sdr/2023FA0000118.md): Boot · torn · Mar 8, 2023 · N917TL · Gulstm 560 · Nose/Tail Landing Gear
  > THE NOSE GEAR DEICE BOOT P.N. 6542002-2 WAS WEDGED BETWEEN THE NOSE GEAR CHROME PISTON P.N. 66452100-2 AND BEARING P.N. 6642307-1 RESULTING IN THE STRUT STAYING COMPRESSES AFTER TAKEOFF AND WHEN THE GEAR WAS RETRACTED THE NOSE GEAR UP LOCK ROLLERS DID NOT ENGA
- [SDR 3EJA202209130001](https://openairdocs.org/sdr/3EJA202209130001.md): Switch · malfunctioned · Aug 15, 2022 · N761JS · Gulstm 560 · Landing Gear Position and Warning
  > GEAR UNLOCK LIGHT ILLUMINATED INFLT, DURING CRUISE PROFILE AT CRUISE ALTITUDE. LANDING GEAR OPERATED NORMALLY ON APPROACH.
- [SDR DBCA202206100005](https://openairdocs.org/sdr/DBCA202206100005.md): Transducer · faulted · Jun 10, 2022 · N210CM · Gulstm 560 · Landing Gear Position and Warning
  > ON APPROACH CREW NOTED BRAKE FAILURE WITH ANTI-SKID INOP ANNUNCIATOR. CREW STOPPED THE AIRCRAFT WITH EMERGENCY BRAKE LEVER. PERFORMED ROTARY TEST OF ANTISKID SYSTEM, NO FAULTS NOTED. MAINTENANCE PERFORMED OHM READINGS OF LT AND RT WHEEL TRANDUCERS AND NOTE
- [SDR DXTA2022040859970](https://openairdocs.org/sdr/DXTA2022040859970.md): None · defective · Apr 7, 2022 · N642QS · Gulstm 560 · Emergency Lighting
  > CABIN EMERG LIGHT: FRONT HALF OF EMERGENCY LIGHTS IN THE CABIN NOT WORKING THE EXIT LIGHT, FLOOR LIGHTS IN, OVERHEAD LIGHTS ON INITIAL PREFLIGHT. AFTER COLD SOKE PROCEDURE TR 21-04 APU RAN GOR 30 MINUTES LIGHTS CAME ON BRIEFLY FOR LESS THAN 20 SECONDS AND THEN
- [SDR DXTA2022040759820](https://openairdocs.org/sdr/DXTA2022040759820.md): None · none · Apr 6, 2022 · N565QS · Gulstm 560 · Passenger/Crew Doors
  > MAIN DOOR: MED IS HARD TO LOCK, AND VERY DIFFICULT TO UNLOCK BOTH INSIDE AND OUTSIDE THE AIRCRAFT. HAD DIFFICULTY OPENING DOOR FROM INSIDE, HAD TO CYCLE HANDLE 2 X'S TO RELEASE DOOR PINS // SIGNOFF // PERFORMED MAIN ENTRY DOOR LUBRICATION AND PERFORMED OPERAT
- [SDR DXTA2022040459570](https://openairdocs.org/sdr/DXTA2022040459570.md): Socket · defective · Apr 2, 2022 · N647QS · Gulstm 560 · Emergency Lighting
  > EMERG EXIT SIGN/LIGHT: VERTICAL EMERGENCY EXIT SIGN ON FORWARD SIDE OF MAIN CABIN DOOR (ABOVE PRE-CATCH RELEASE HANDLE) DOES NOT ILLUMINATE WITH PAX SAFETY ON OR WHEN EMERGENCY LIGHTS ARE SLECTED TO ON. THERE ARE ALSO SMALL WIRES VISIBLE NEAR THE EXIT PYRAMID
- [SDR DXTA2022033159410](https://openairdocs.org/sdr/DXTA2022033159410.md): None · none · Mar 30, 2022 · N614QS · Gulstm 560 · Engine (Turbine/Turboprop)
  > ENGINE COMPRESSOR STALL: AT CRUISE ALTITUDE 410 HEARD A LOUD BANG AND FELT A THUMP IN OUR FEET. N1 DROPPED FROM 91.0 TO 85 THEN RETURNED TO 91.0. REST OF FLIGHT WAS NORMAL. 2ND WRITEUP. ENGINE SYNC WAS OFF. // SIGNOFF// BEGAN TO TROIBLESHOOTING THE R/H ENGI
- [SDR DXTA2022032959240](https://openairdocs.org/sdr/DXTA2022032959240.md): None · defective · Mar 29, 2022 · N609QS · Gulstm 560 · Fuel Pressure Indicator
  > FUEL PRESSURE INDICATION: REPEAT WRITEUP. DURING CROSSFEED FROM LEFT TANK TO RIGHT ENGINE, CROSSFEED WORKED NORMALLY. AFTER MOVING CROSSFEED TO OFF POSITION, THE RIGHT LOW FUEL PRESSURE ANNUNCIATOR FLASHED MOMENTARILY FOLLOWED BY THE RIGHT FUEL BOOST ON ANNUNC
- [SDR 2022F00152](https://openairdocs.org/sdr/2022F00152.md): None · none · Mar 21, 2022 · N560BL · Gulstm 560 · Elevator Tab Control System
  > WHILE ON-ROUTE TO KMDT WE RECEIVED AN AP PITCH MISTRIM ANNUNCIATION AND ASSOCIATED MASTER CAUTION. IN ACCORDANCE WITH THE CHECKLIST, AUTOPILOT WAS DISCONNECTED AND THE PITCH TRIM WAS COMMANDED MANUALLY NOSE-DOWN. THE TRIM WHEEL HOWEVER FAILED TO ROTATE VIA THE
- [SDR 2022F00155](https://openairdocs.org/sdr/2022F00155.md): None · none · Mar 8, 2022 · N17FA · Gulstm 560 · Ice/Rain Protection System
  > DURING TAKEOFF ROLL ON RWY 34 AT KHKS, AT APPROXIMATELY 80 KTS, WE RECEIVED THE WINDSHIELD OVERHEAT ANNUNCIATOR. TAKE OFF WAS ABORTED WITHOUT INCIDENT. AS POWER WAS RETARDED DURING THE ABORT, THE ANNUNCIATOR EXTINGUISHED AS ENGINES APPROACHED IDLE THRUST. ROTA
- [SDR DXTA2022030357830](https://openairdocs.org/sdr/DXTA2022030357830.md): Cable · abnormal · Mar 3, 2022 · N556QS · Gulstm 560 · Doors
  > MAIN DOOR CABLE: OPENED MAIN CABIN DOOR FROM OUTSIDE. HEARD A TWANG, AND DISCOVERED HALF THE STRANDS ON THE FORWARD DOOR CABLE BROKEN, WITH LOOSE ENDS EXTENDING INTO STAIRWAY. // SIGNOFF// REMOVED AND REPLACED WITH A NEW PART THE FORWARD MED COUNTERBALANCE CAB
- [SDR DXTA2021122854320](https://openairdocs.org/sdr/DXTA2021122854320.md): Unknown · defective · Dec 27, 2021 · N557QS · Gulstm 560 · Landing Gear Brake System
  > POWER BRAKE CB: UPON TAXING IN TO THE RAMP. WE LOST BRAKES THE PWR BRKS CB POPPED AND THE ANTISKD INIP LIGHT CAME ON. WE ROLLED TO A STOP AND CHOCKED THE PLANE. // SIGNOFF// GAINED ACCESS AS REQUIRED, CHECKED POWER BRAKE MOTOR SPLICES FOR CONDMON AND CORRECT
- [SDR DXTA2021122754260](https://openairdocs.org/sdr/DXTA2021122754260.md): None · defective · Dec 26, 2021 · N556QS · Gulstm 560 · Emergency Lighting
  > MAIN EXIT SIGN/LIGHT: FWD EMERGENCY LIGHTING SYSTEM IS INOPERATIVE. // SIGNOFF// REMOVED AND REPLACED FAULTY FWD EMERGENCY LIGHTING BATTERY PACK IAW CE560XL MM 33-50-01 FAILED OPS CHECK
- [SDR R3WA202108130001](https://openairdocs.org/sdr/R3WA202108130001.md): Engine · flamed out · Aug 11, 2021 · N63FF · Gulstm 560 · Engine (Turbine/Turboprop)
  > AT 43000 AIRCRAFT WAS CROSSING A SMALL LINE OF WEATHER. ENCOUNTERED SOME MODERATE TURBULENCE. RIGHT ENGINE SHUT OFF. CREW DECLARED AN EMERGENCY AND STARTED A DESCENT. CREW REPORTED RIGHT ENGINE LOOKED TO BE IN GOOD SHAPE STILL SHOWING ABOUT 8.7% AND TWO. CREW
- [SDR 2021071945450](https://openairdocs.org/sdr/2021071945450.md): Battery Pack · faulty · Jul 17, 2021 · N648QS · Gulstm 560 · Emergency Lighting
  > EMERGENCY LIGHTING: WITH SHIP POWER OFF PASSENGER SAFETY LIGHTS EMERGENCY EXIT LIGHT OVER MAIN DOOR AND FORWARD HALF OF FLOOR LIGHTS DO NOT WORK, BUT ALL THE LIGHTS WORK WITH BATTERY OR GPU OR SHIPS POWER ON. // SIGNOFF // REMOVED AND REPLACED EMERGENCY LIGH
- [SDR CA120619007](https://openairdocs.org/sdr/CA120619007.md): Unknown · odor · Jun 13, 2012 · Gulstm 560 · Air Distribution System
  > (CAN) DURING DESCENT, VIBRATIONS WERE FEL, ACCOMPANIED WITH THE ODOR OF OIL IN THE CABIN. ENG PARAMETERS WERE DECREASING WITH NO RESPONSE TO THROTTLE LEVER MOVEMENT. THE ENGINE WAS SHUTDOWN & AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. POST FLIGHT
- [SDR 2002FA0000400](https://openairdocs.org/sdr/2002FA0000400.md): Torque Tube · worn · Mar 15, 2002 · N2705B · Gulstm 560 · Rudder Control System
  > DURING AN ANNUAL INSPECTION, WHILE MEASURING RUDDER TRAVELS IT WAS FOUND THAT IF A LITTLE EXTRA PRESSURE WAS APPLIED TO THE RUDDER TRAILING EDGE, ONCE IT HAD REACHED ITS STOP, THE RUDDER TRAVELED AN EXTRA INCH PAST THE SPECIFIED TRAVELS. WHILE THE STOP REMAIN
- [SDR UUM2002F00000](https://openairdocs.org/sdr/UUM2002F00000.md): Beam · cracked · Mar 15, 2002 · N2705B · Gulstm 560 · Engine Mount Section
  > DURING AN ANNUAL INSPECTION, THE LEFT ENGINE, ENGINE MOUNT BEAM ASSEMBLY WAS FOUND CRACKED. THE CRACK WAS MIDWAY IN THE BEAM AND WAS 60-70 PERCENT OF THE WAY THROUGH THE BEAM. THERE WAS A CLAMP ON THE ENGINE DIRECTLY BEHIND THE CRACK, AND THE BEAM MAY HAVE B
- [SDR 99ZZZX3966](https://openairdocs.org/sdr/99ZZZX3966.md): Elt · failed · Sep 20, 1999 · N356WC · Gulstm 560 · Emergency Equipment
  > WHILE PERFORMING A PHASE 18 INSPECTION, THE ELT WAS FOUND INOPERABLE. INSPECTION OF THE ELT REVEALED A BURNED AREA ON THE PRINTED CIRCUIT BOARD APPROXIMATELY THE SIZE OF A NICKEL. IN ADDITION, THE BATTERY CASE HAD CRACKED IN THE MIDDLE AND THE BATTERIES INSI
- [SDR 99ZZZX3743](https://openairdocs.org/sdr/99ZZZX3743.md): Cartridge · failed · Sep 17, 1999 · N3760S · Gulstm 560 · Fire Bottle, Fixed
  > DURING SCHEUDLED REMOVAL PROCESS OF THIS PART, IT WAS FOUND TO BE INOPERATIVE. AIRCRAFT WAS SCHEDULED FOR FIRE EXTINGUISHER CARTRIDGE TIME REPLACEMENT. THIS FACILITY DISCHARES ALL FIRE EXTINGUISHER CHARGES PRIOR TO DISPOSAL.
- [SDR 99ZZZX3630](https://openairdocs.org/sdr/99ZZZX3630.md): Arm · worn · Aug 17, 1999 · N356WC · Gulstm 560 · Landing Gear Retraction/Extension System
  > PILOTS SQUAWKED A NOISE FROM NOSE WHEELWELL WHILE TAXIING. INSPECTION REVEALED EXCESSIVE CLEARANCE BETWEEN THE ARM THAT ATTACHES THE STEERING BUNGEE TO THE NOSE STEERING UNIVERSAL JOINT. THIS CLEARANCE ALLOWED THE BUNGEE TO CONTACT THE PULLEY BRACKET LOCATED
- [SDR 99ZZZX3589](https://openairdocs.org/sdr/99ZZZX3589.md): Fan Assy · damaged · Aug 17, 1999 · N357WC · Gulstm 560 · Turbine Engine Compressor Section
  > ON PRE-FLIGHT, THE COPILOT DISCOVERED DAMAGE TO THE RIGHT FAN ASSY WHICH RESULTED IN THE FLIGHT BEING CANCELLED. FOUND DAMAGE TO 12 BLADES RANGING FROM SMALL NICKS TO A SECTION MISSING FROM THE TIP OF ONE BLADE THAT WAS APPROX.25 SQUARE INCH IN SIZE. THE I
- [SDR 99ZZZX3588](https://openairdocs.org/sdr/99ZZZX3588.md): Cable · broken · Aug 17, 1999 · N356WC · Gulstm 560 · Passenger/Crew Doors
  > THE FORWARD STEP CABLE BROKE AS A MAINTENANCE WAS BOARDING AIRCRAFT. OCCURRED JUST AFTER ACFT CAME IN FROM A FLIGHT. THE CABLE BROKE IN THE THREADS OF THE TURNBUCKLE WHERE IT ATTACHES TO THE BOTTOM OF THE STEP. THIS IS THE THIRD CABLE THAT HAS BROKEN IN THE
- [SDR 99ZZZX3587](https://openairdocs.org/sdr/99ZZZX3587.md): Exciter Box · failed · Aug 17, 1999 · N356WC · Gulstm 560 · Exciter
  > DURING PHASE 3 AND 4 INSPECTION, THE RIGHT INBOARD IGNITER WAS NOT FIRING. INSPECTION OF THE PLUG REVEALED THERE WAS LITTLE WEAR ON THE PLUG AND RECORDS SHOWED IT WAS INSTALLED 150 HOUR PREVIOUS ON A PHASE 1 AND 2 INSP. VOLTAGE CHECKED TO THE BOX AND THERE W
- [SDR 2000ZZZX402](https://openairdocs.org/sdr/2000ZZZX402.md): Display · damaged · Aug 5, 1999 · N40WP · Gulstm 560 · Central Display
  > EFIS HSI DISPLAY TUBE HAS SEVERELY ETCHED SCREEN CAUSING GHOSE IMAGES. REMOVED AND REPLACED DISPLAY UNIT.
- [SDR 98ZZZX4582](https://openairdocs.org/sdr/98ZZZX4582.md): Stain Cover · worn · Oct 7, 1998 · N356WC · Gulstm 560 · Engine Thrust Reverser
  > STAIN COVER WORN ON THRUST REVERSER.
- [SDR 98ZZZX4259](https://openairdocs.org/sdr/98ZZZX4259.md): Exciter Box · failed · Oct 7, 1998 · Gulstm 560 · Exciter
  > PILOT REPORTED LT ENG WOULD NOT LIGHT OFF ON START AND THERE WAS NO AUDIBLE SNAPPING SOUND. THE BOX HAD 24 VOLTS AND GOOD GROUND. ANOTHER EXCITER BOX INSTALLED AND IGNITER CHECKED. A SNAP FROM INBD IGNITER HEARD AND ENG WAS COWLED UP, ENG STARTED, AND AIRPL
- [SDR 98ZZZX4258](https://openairdocs.org/sdr/98ZZZX4258.md): Exciter Box · failed · Oct 7, 1998 · Gulstm 560 · Exciter
  > PILOT REPORTED LT ENG WOULD NOT LIGHT OFF ON START AND THERE WAS NO AUDIBLE SNAPPING SOUND. THE BOX HAD 24 VOLTS AND GOOD GROUND. ANOTHER EXCITER BOX INSTALLED AND IGNITER CHECKED. A SNAP FROM INBD IGNITER HEARD AND ENG WAS COWLED UP, ENG STARTED, AND AIRPL
- [SDR 98ZZZX4064](https://openairdocs.org/sdr/98ZZZX4064.md): Cable · broken · Oct 7, 1998 · N356WC · Gulstm 560 · Entrance Stairs
  > THE FWD DOOR CABLE BROKE AS PILOT GOT OFF AIRPLANE. THIS NEW COMPOSITE STEP HAS 2 SUPPORT CABLES, 1 FWD AND 1 AFT. THIS IS 3RD CABLE THAT HAS BROKEN. THE 1ST CABLE BROKE AT 151.8 HRS; FWD CABLE. THE 2ND BROKE AT 358.4 HRS; AFT CABLE. CABLES HAVE BEEN BREA
- [SDR 98ZZZX4650](https://openairdocs.org/sdr/98ZZZX4650.md): Bolt · broken · Jun 26, 1998 · N30PC · Gulstm 560 · Landing Gear Doors
  > TORQUE TUBE, NLG DOORS, ATTACH BOLT, RT SIDE, BROKE IN-FLIGHT CAUSING NLG DOORS TO OPEN. CREW DIVERTED TO VALDOSTA, GA. EITHER BOLT IS TOO LONG OR NO WASHER WAS INSTALLED AT FACTORY. SUBMITTER RECOMMENDED CHECK P/N ON BOLT AND INSURE WASHER IS PRESENT. BOL
- [SDR 98ZZZX2577](https://openairdocs.org/sdr/98ZZZX2577.md): Skin · cracked · Jun 2, 1998 · N269CM · Gulstm 560 · Rudder, Plate/Skin
  > A 1 INCH CRACK BETWEEN TWO RIVET HOLES ON THE LOWER FORWARD RUDDER LEADING EDGE SKIN.
- [SDR 98ZZZX2581](https://openairdocs.org/sdr/98ZZZX2581.md): Window · cracked · May 10, 1998 · N772AA · Gulstm 560 · Flight Compartment Windows
  > DURING SCHEDULED INSPECTION, FOUND WINDOW CRACK APPROXIMATELY SIX INCHES LONG IN UPPER FORWARD CORNER CONNECTING FOUR ATTACH HOLES. COULD NOT DETERMINE CAUSE OF CRACK. REPLACED WITH NEW WINDOW. CRACKED WINDOW HAD DATE OF 5-1-91 STAMPED BELOW PART NUMBER.
- [SDR 98ZZZX1863](https://openairdocs.org/sdr/98ZZZX1863.md): Outflow Valve · malfunctioned · May 7, 1998 · N777KY · Gulstm 560 · Pressure Regulator/Outflow Valve
  > OPERATOR HAD PRESSURIZATION PROBLEM ON CESSNA 560. THIS INFORMATION MAY BE PREMATURE, BUT HE HAS NOT HEARD BACK FROM CESSNA OR ALLIED-SIGNAL ON THE PROBLEM. SUBMITTER SUSPECTS THAT AD 96-17-10 SHOULD HAVE INCLUDED MORE DASH NUMBERS. OUTFLOW VALVE WAS A 1036
- [SDR 98ZZZX2157](https://openairdocs.org/sdr/98ZZZX2157.md): Bracket · broken · May 1, 1998 · N500UB · Gulstm 560 · Passenger/Crew Doors
  > AFTER A FLIGHT, THE PILOT COULD NOT OPEN THE CABIN DOOR AND HAD TO CLIMB OUT THE EMERGENCY WINDOW. THE DOOR COULD NOT BE OPENED FROM THE OUTSIDE EITHER. DISASSEMBLED THE DOOR, AS WELL, AND FOUND THE AFT LATCH PIN BELLCRANK BRACKET BROKEN WHICH CAUSED THE AFT
- [SDR 98ZZZX3588](https://openairdocs.org/sdr/98ZZZX3588.md): Blower · inoperative · Apr 20, 1998 · N500UB · Gulstm 560 · Air Distribution System
  > BLOWER MOTOR FAILED BEFORE ITS 3,500 HOUR TBO. THIS BLOWER CLEARS THE WINDSHIELD AND COCKPIT SIDE WINDOWS ON THE INSIDE.
- [SDR 98ZZZX1538](https://openairdocs.org/sdr/98ZZZX1538.md): Bearing · failed · Mar 31, 1998 · N94TX · Gulstm 560 · Starter-Generator
  > PILOTS REPORTED A VIBRATION IN THE LEFT ENGINE AFTER TAKEOFF. THEY RETURNED TO THE AIRPORT WITH NO FURTHER PROBLEM. INSPECTION REVEALED THE LT STARTER/GENERATOR ANTI-DRIVE END BEARING WAS BEGINNING TO FAIL. THE GENERATOR WAS STILL OPERATING; HOWEVER, PIECES
- [SDR 98ZZZX1169](https://openairdocs.org/sdr/98ZZZX1169.md): Ground Connect · loose · Mar 13, 1998 · N19PV · Gulstm 560 · DC Generating System
  > PILOTS REPORTED A PARALLELING PROBLEM WITH THE GENERATORS. INSPECTION REVEALED BOTH STARTER/GENERATOR GROUND CONNECTIONS WERE LOOSE. MINOR ARCING WAS NOTED ON LEFT GROUND. BOTH CONNECTIONS WERE CLEANED AND RESEATED. THIS CONDITION RESULTED FROM IMPROPER TO
- [SDR 98ZZZX882](https://openairdocs.org/sdr/98ZZZX882.md): Panel · malfunctioned · Feb 16, 1998 · N335QS · Gulstm 560 · Emergency Exits
  > DURING INSPECTION, ATTEMPTED TO REMOVE THE EMERGENCY EXIT DOOR. FOUND NUMEROUS PROBLEMS. EXTERIOR HANDLE ROTATION DIFFICULT. HATCH HAD TO BE HIT HARD AT TOP TO MAKE IT RELEASE FROM OPENING. DETERMINED RUBBER SEAL THAT IS GLUED TO DOOR WITH 1300L, WAS ADHER
- [SDR 98ZZZX878](https://openairdocs.org/sdr/98ZZZX878.md): Coupling · cracked · Feb 16, 1998 · N31RC · Gulstm 560 · Pneumatic Distribution System
  > DURING ENGINE CHANGE, FOUND BLEED AIR CLAMP CRACKED IN RADIUS OF BOLT GUIDE SLEEVE, ALMOST COMPLETELY AROUND THE CIRCUMFERENCE.
- [SDR 98ZZZX984](https://openairdocs.org/sdr/98ZZZX984.md): Connector · mismarked · Feb 10, 1998 · N314QS · Gulstm 560 · Engine Oil Temperature
  > CONNECTOR FOR OIL TEMPERATURE AT ENGINE MISLABELED, P.93. PER MANUFACTURER, CONNECTOR SHOULD BE LABELED P.87.
- [SDR 98ZZZX881](https://openairdocs.org/sdr/98ZZZX881.md): Actuator · broken · Feb 10, 1998 · N361QS · Gulstm 560 · Trailing Edge Flap Actuator
  > DURING PHASE 2 INSPECTION, FOUND HEAD OF BOLT SHEARED CLEAN. THIS IS ONE OF FOUR BOLTS HOLDING BARREL TO BASE OF THE FLAP ACTUATOR. BOLT HEAD WAS HELD CAPTIVE BY SAFETY WIRE IN CONJUNCTION WITH THREE REMAINING BOLTS. DID NOT APPEAR TO BE OVERTORQUED. POSSIB
- [SDR 98ZZZX880](https://openairdocs.org/sdr/98ZZZX880.md): Line Assy · chafe · Feb 10, 1998 · N341QS · Gulstm 560 · Airfoil Anti/De-ice System
  > TWO WING DEICE LINES AND CLAMPS LOCATED AT FUSELAGE AND WING LEADING EDGE, CHAFE FUSELAGE SKIN. SUBMITTER STATED SHRINK WRAP AND THERMOPROTECTION TAPE SHOULD BE EXTENDED FORWARD.
- [SDR 98ZZZX879](https://openairdocs.org/sdr/98ZZZX879.md): Line Assy · chafe · Feb 10, 1998 · N341QS · Gulstm 560 · Airfoil Anti/De-ice System
  > TWO WING DEICE LINES AND CLAMPS LOCATED AT FUSELAGE AND WING LEADING EDGE, CHAFE FUSELAGE SKIN. SUBMITTER STATED SHRINK WRAP AND THERMOPROTECTION TAPE SHOULD BE EXTENDED FORWARD.
- [SDR 98ZZZX847](https://openairdocs.org/sdr/98ZZZX847.md): Starter · failed · Feb 2, 1998 · N356WC · Gulstm 560 · Starter-Generator
  > WHILE T/S A VIBRATION, THE RT STARTER/GEN WAS FOUND TO HAVE A BAD VIBRATION. LISTENING TO RUN DOWN OF THE ENGINES AFTER MOTORING THEM TO 10 PERCENT, THE RT STARTER MADE AN UNUSUAL NOISE. WHEN STARTER WAS REMOVED, INSP REVEALED THE BRUSH END BEARING HAD FAILE
- [SDR 98ZZZX490](https://openairdocs.org/sdr/98ZZZX490.md): Axle · corroded · Jan 12, 1998 · N356WC · Gulstm 560 · Main Landing Gear Strut/Axle/Truck
  > WHILE PERFORMING A PHASE 1 AND PHASE 2 ON BOTH MLG AXLES, FOUND CORROSION ON THEM. THIS SPECIFIC INSPECTION ITEM IS ITEM CODE NR A324040 IN THE PHASE 2 INSPECTION. THE AXLE IS TO BE INSPECTED FOR PRESENCE OF PRIMER ON THE AXLE AND AXLE ADAPTER WHERE THE BRAK
- [SDR 98ZZZX316](https://openairdocs.org/sdr/98ZZZX316.md): Switch · leaking · Dec 22, 1997 · N500UB · Gulstm 560 · Engine Oil Pressure
  > LARGE AMOUNTS OF OIL WERE LEAKING FROM THE RT ENGINE. FOUND THE OIL PRESSURE SWITCH INTERNAL SEAL HAD FAILED.
- [SDR 97ZZZX2074](https://openairdocs.org/sdr/97ZZZX2074.md): Hose · leaking · Apr 21, 1997 · N500UB · Gulstm 560 · Landing Gear Brake System
  > PILOT NOTED HYDRAULIC PRESSURE LOW ON FINAL. UPON LANDING HAD NO RIGHT BRAKE. MAINTENANCE FACILITY FOUND BRAKE HOSE SUPPLYING RT BRAKE ASSY WAS LEAKING THROUGH THE BRAID ON THE SIDEWALL. THERE IS NO TIME CHANGE REQUIREMENTS TO THE HOSES. THESE ARE TEFLON,
- [SDR 96ZZZX6121](https://openairdocs.org/sdr/96ZZZX6121.md): Flap · skin separated · Dec 11, 1996 · N1217V · Gulstm 560 · Trailing Edge Flaps
  > ON FIRST FLIGHT AFTER AIRCRAFT WAS REPAINTED, AT AN ALTITUDE OF 15,000 FEET, RIGHT INBOARD FLAP SKIN SEPARATED INTERNALLY FROM THE FLAP RIBS. AIRCRAFT MADE EMERGENCY LANDING AT RIC. INVESTIGATION REVEALED VENT HOLES IN FLAP WERE CLOGGED WITH FOREIGN MATTER W

Next page: https://openairdocs.org/model/cessna-560/reports.md?page=2

## 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 aircraft_model_key = '560'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-560/reports

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