# Service difficulty reports: Pratt & Whitney Canada JT15D-1 series

A list on [Pratt & Whitney Canada JT15D-1 series](https://openairdocs.org/engine/pratt-whitney-canada-jt15d-1-series.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 84 reports

- [SDR 5JHA20250930231](https://openairdocs.org/sdr/5JHA20250930231.md): Compressor · stalled · Sep 30, 2025 · N16NL · Cessna 501 · Turbine Engine Compressor Section
  > WHILE IN CRUISE FLIGHT AT FL370 (37,000 FT) THE LEFT ENGINE SUFFERED A SUSPECTED COMPRESSOR STALL WHICH SUBSEQUENTLY LEAD TO THE COMPLETE FAILURE/FLAMEOUT OF THE LEFT ENGINE. ALL REQUIRED QRH PROCEDURES WERE ACCOMPLISH ALONG WITH AN ATTEMPTED RELIGHT/RESTART
- [SDR 2017FA0000394](https://openairdocs.org/sdr/2017FA0000394.md): Pump · failed · Feb 13, 2017 · N91VB · Cessna 550 · Turbine Engine Oil System
  > LEFT ENGINE OIL PUMP HAD INTERNAL FAILURE. UPON START OF THE LEFT ENGINE, NO TURBINE SPEED OR OIL PRESSURE INDICATION.
- [SDR CA141218002](https://openairdocs.org/sdr/CA141218002.md): Engine · shutdown · Dec 3, 2014 · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE, PILOT OBSERVED NR 1 ENGINE OIL PRESSURE LIGHT ON AND A FEW SECONDS LATER THE OIL PRESSURE GAUGE SHOWED "ZERO" PSI. PILOT IN COMMAND SHUT DOWN THE ENGINE AND CONTINUED FLIGHT TO THE INTERNATIONAL AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADE
- [SDR CA140318001](https://openairdocs.org/sdr/CA140318001.md): Tube · defective · Mar 18, 2014 · Turbine Engine Oil System
  > (CAN) MS9382-04 TEE TUBE, AN OIL LEAK WAS NOTED DURING A ROUTINE LEAK CHECK PERFORMED BY ASSEMBLY AND TEST. FOLLOWING INVESTIGATION, THE LEAK WAS ATTRIBUTED TO A TEE TUBE, PN MS9382-04 ASSEMBLED INTO A TUBE ASSEMBLY. RECEIVED THIS INDUSTRY STANDARD PART FROM
- [SDR 2013FA0000056](https://openairdocs.org/sdr/2013FA0000056.md): Transmitter · broken · Jan 25, 2013 · N84EC · Cessna S550 · Engine Fuel Indicating System
  > ACFT DECLARED AN EMERGENCY, LANDING WITH THE RT ENGINE SHUTDOWN AND REPORTED THAT THE ENGINE FLAMED OUT ON TAKEOFF. THERE WAS A SMALL AMOUNT OF FUEL IN THE COWLING. ON REMOVAL OF THE COWLING IT WAS DISCOVERED THAT THE FUEL FLOW TRANSMITTER WAS BROKEN (TWO SC
- [SDR L7OA2012F00165](https://openairdocs.org/sdr/L7OA2012F00165.md): Indicator · inoperative · Aug 14, 2012 · N347MH · Cessna 501 · Engine Indicating System
  > LEFT ENGINE INSTRUMENT DISPLAY INOPERATIVE.
- [SDR K45A2012070202](https://openairdocs.org/sdr/K45A2012070202.md): Skin Panel · dented · Jun 29, 2012 · N980AG · Cessna 560CESSNA · Wing, Plate/Skin
  > ACFT WAS INSPECTED TO CHECK OUT BASE MX (FOD INSPECTION). A 3" BY 5" DENT.125" DEEP WAS DISCOVERED 2 FT INBD OF STALL STRIP UNDER THE DEICE BOOT. DAMAGE WILL BE REPAIRED IAW EA RECOMMENDATIONS.
- [SDR K45A2012070201](https://openairdocs.org/sdr/K45A2012070201.md): Liner · damaged · Jun 29, 2012 · N980AG · Cessna 560CESSNA · Turbine Engine Compressor Section
  > ENGINE WAS INSPECTED TO CHECK OUT BASE MX (FOD INSPECTION). ABRADABLE MATERIAL WAS FOUND MISSNG FROM LOW COMPRESSOR CASE FTO 9 O`CLOCK THROUGH OUT 10:30 O`CLOCK POSITION. BELIEVE THE MATERIAL WAS LOOSENED BY THE BIRD STIKE BUT NOT EASILY DETECTED. THE MATER
- [SDR DXTR2012009](https://openairdocs.org/sdr/DXTR2012009.md): Inlet · cracked · Jan 31, 2012 · N819QS · Cessna 560CESSNA · Engine Air Intake System
  > LT ENGINE INLET FAN FLANGE CRACKED APPROX AT 9 OCLOCK POSITION, CRACK IS 4" IN LENGTH.
- [SDR CA110928011](https://openairdocs.org/sdr/CA110928011.md): Line · damaged · Sep 7, 2011 · Cessna 500CESSNA · Passenger Oxygen System
  > (CAN) OPERATOR REPORTED PERSISTENT SERVICING REQUIREMENT OF THE OXYGEN SYSTEM. INVESTIGATION FOUND A PINHOLE LEAK IN THE SOLDER JOINT AT THE BULKHEAD ATTACH END OF THE LINE ASSY-PRESSURE BULKHEAD TO OXYGEN GAGE. PN 9912057-7 (ALT S1721-20).
- [SDR CA110412003](https://openairdocs.org/sdr/CA110412003.md): Line · misinstalled · Apr 11, 2011 · Cessna 560XL · Aircraft Fuel Distribution System
  > (CAN) RIGID FUEL LINE, WAS MAKING CONTACT WITH THE LOWER COWL ASSY AND SUBSEQENTLY WEARING THE SKIN. INVESTIGATION SHOWS THE FUEL LINE MAY NOT HAVE BEEN INSTALLED CORRECTLY. THE FUEL LINE HAS 1 SHORTER TUBE THAT SHOULD BE SECURED TO THE ENGINE DRIVEN FUEL P
- [SDR FDEA201010264174](https://openairdocs.org/sdr/FDEA201010264174.md): Valve · inoperative · Oct 26, 2010 · N466FE · Boeing 727225 · Cabin Pressure Control System
  > RT AIR MIX VALVE STUCK FULL COLD. FOLLOWED BY LOSS OF CABIN PRESSURIZATION. RAN PACKS INDIVIUALY AND TOGETHER. PERFORMED LEAK CK OF DUCTS, PACKS, MIX VLVS. NO DEFECTS NOTED. PERFORMED BITE TEST OF 35 DEG VALVE AND WATCHED VALVES OPERATE. PULLED C/B ON
- [SDR DXTA2010081804198](https://openairdocs.org/sdr/DXTA2010081804198.md): Engine · flamed out · Aug 17, 2010 · N348QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)
  > ENGINE 1 HAD A UNCOMMANDED FLAME OUT ON THE RAMP PRIOR TO TAXI. ALL ENGINE INDICATIONS WERE NORMAL PRIOR TO THE FLAMEOUT. REMOVED COWL, INSPECTED ENGINES, FOUND THE IDLE DETENT FRICTION OUT OF ADJUSTMENT. AJUSTED IDLE DETENT FRICTION TO PROPER AJUSTMENT. RA
- [SDR FDEA201008032789](https://openairdocs.org/sdr/FDEA201008032789.md): Skin · gouged · Aug 3, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620-630, STR 16L. REPAIRED MCD INNER SURROUND SKIN IAW EA 7-5330-135571.
- [SDR DXTA20082870](https://openairdocs.org/sdr/DXTA20082870.md): Landing Gear · malfunctioned · Feb 12, 2008 · N375QS · Cessna 560CESSNA · Landing Gear Retraction/Extension System
  > UPON RETRACTION OF LANDING GEAR, GEAR UNSAFE LIGHT ILLUMINATED. JACKED AND SWUNG GEAR TEN TIMES WITH NO FAULTS. LUBED ALL UP LOCK ROLLERS AND GEAR. OPS CHECKED GOOD IAW MM CH32-01-00.
- [SDR DXTA200802810](https://openairdocs.org/sdr/DXTA200802810.md): Hose · leaking · Jan 30, 2008 · N375QS · Cessna 560CESSNA · Landing Gear Brake System
  > DURING TOUCHDOWN AT PDK, COPILOT'S LT BRAKE PEDAL WENT COMPLETELY TO THE FLOOR. REMOVED AND REPLACED BOTH CO-PILOTS UPPER MASTER CYLINDER HOSES. IAW MM CHAP 32-42-02. ALSO COMPLETED APPROVED BLEEDING PROCEDURES CHAP 32-42-00.
- [SDR DXTA200702661](https://openairdocs.org/sdr/DXTA200702661.md): Brake Assy · weak · Dec 8, 2007 · N348QS · Cessna 560CESSNA · Landing Gear Brake System
  > BRAKES PULL AIRCRAFT NOSE HARD LT WHEN EQUAL PRESSURE IS APPLIED TO BOTH BRAKE PEDALS DURING LANDING ROLLOUT. BLED BRAKES IAW C560 M/M 32-42-00. TAXI CHECKED/BRAKE CHECKED A/C. OPS CHECKS NORM.
- [SDR DXTA200702370](https://openairdocs.org/sdr/DXTA200702370.md): Engine · malfunctioned · Jul 31, 2007 · N303QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)
  > LT ENGINE QUIT AFTER NORMAL START SEQUENCE AND STABILIZATION. AFTER PERFORMING GENERATOR CHECK NOTICED LT FUEL BOOST PUMP ANNUNCIATOR ON, THEN N2 ROLLING DOWN. THROTTLE LEVER WAS PLACED ON GATE AND NEVER MOVED. PERFORMED LEFT ENGINE START PROCEDURES PER NJ
- [SDR 2007FA0000070](https://openairdocs.org/sdr/2007FA0000070.md): Attach Fitting · cracked · Jan 8, 2007 · N117TW · Cessna 500CESSNA · Passenger Compartment Equipment
  > UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR. (K)
- [SDR 2006FA0001196](https://openairdocs.org/sdr/2006FA0001196.md): Line · corroded · Nov 29, 2006 · N501LH · Cessna 500CESSNA · Hydraulic System, Main
  > INVESTIGATING SOFT BRAKE CONDITION IT WAS NOTED THAT BRAKE FLUID WAS LEAKING FROM AROUND THE BELLY BEACON AND THE BEACON LENS WAS FULL OF FLUID. REMOVED THE INTERIOR AND THE CENTER AISLE FLOOR PANELS. HYDRAULIC FLUID WAS NOTED DRIPPING FROM RIDGE BRAKE LINE
- [SDR CA060706003](https://openairdocs.org/sdr/CA060706003.md): Connecting Rod · worn · Jul 4, 2006 · Compressor Bleed Valve
  > (CAN) PRATT & WHITNEY CANADA OVERHAUL MANUAL 3037323 REV.22, SECTION 72-30-07, PARAGRAPH 88-4 MISTAKENLY CALLS FOR NICKEL PLATING IN ACCORDANCE WITH SPOP 62. SPOP 62 IS A FLORESCENT PENETRANT INSPECTION PROCEDURE. IT IS UNDERSTOOD THAT THE MANUAL SHOULD RATHER
- [SDR 2006FA0000168](https://openairdocs.org/sdr/2006FA0000168.md): Actuator · leaking · Feb 16, 2006 · N502BE · Cessna 500CESSNA · Landing Gear Actuator
  > HYDRAULIC LEAK AT SWITCH ACTUATOR ENTRY INTO NLG ACTUATOR AT 231 CYCLES INSTALLED AND 4224 CYCLES SOH/NEW. DEPELETED HYDRAULIC SYSTEM ON LANDING. (K)
- [SDR 2006FA0000000](https://openairdocs.org/sdr/2006FA0000000.md): Tire · leaking · Dec 21, 2005 · N94LH · Beech 400A · Tire
  > REPLACED THE FRONT TIRE, WITH THIS NEW TIRE AND HAVE HAD A SLOW LEAK EVER SINCE. TOOK THE TIRE BACK OFF AND SUBMERGED THE TIRE AND WHEEL UNDER WATER, FOUND 10 VERY SMALL PINHOLES IN THE TIRE SIDEWALL CLOSE TO THE RIM EQUALLY SPACED AROUND THE SIDEWALL, THE PI
- [SDR 2005FA0001457](https://openairdocs.org/sdr/2005FA0001457.md): Transmitter · out of adjust · Oct 10, 2005 · N419CW · Beech 400A · Trailing Edge Flap Control System
  > FLAP ASYMMETRY ANNUNCIATOR ILLUMINATED DURING APPROACH. FOUND MIDBOARD ASYMMETRY DETECTOR READING 5.7 VOLTS. FOUND IB ASYMMETRY DETECTOR READING 7.8 VOLTS. ADJUSTED LT AND RT FLAP POSITION TRANSMITTERS AS REQUIRED IAW MM TO BRING VOLTAGES TO 5.8 VOLTS +/- 0
- [SDR 2005FA0001369](https://openairdocs.org/sdr/2005FA0001369.md): Torque Tube · cracked · Sep 23, 2005 · N561JS · Cessna 560CESSNA · Nose/Tail Landing Gear
  > NOSE LANDING GEAR DOORS WERE OBSERVED TO BE DROOPING SLIGHTLY. NOSE GEAR RETRACT LINKAGE WAS INSPECTED AND TORQUE TUBE WAS OBSERVED TO HAVE A BROKEN WELD AT ONE END CAP. RECOMMEND INSPECTING WELDS CAREFULLY DURING PERIODIC INSPECTIONS. (K)
- [SDR 2005FA0001321](https://openairdocs.org/sdr/2005FA0001321.md): Line · damaged · Sep 12, 2005 · N907JE · Beech 400A · Landing Gear Brake System
  > DURING COMPLIANCE WITH INSPECTION PORTION OF SB NOTED CHAFE DAMAGE TO PN 128580101-1 NOTED CHAFE DAMAGE TO PN 128-580101-1 HYDRAULIC BRAKE LINE FROM ADJACENT FLOORBOARD ATTACH SCREW. DAMAGE FOUND LESS THAN 10 PERCENT OF TUBING WALL THICKNESS. RECOMMEND THAT
- [SDR AJC2005F00012](https://openairdocs.org/sdr/AJC2005F00012.md): Squat Switch · defective · Aug 26, 2005 · N400HS · Beech 400A · Landing Gear Position and Warning
  > DEPARTED, ENROUTE, AFTER TAKEOFF THE CREW REPORTED THAT THE LANDING GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND THEY COULD NOT RETRACT THE GEAR. THE LANDING GEAR DOWN LOCK OVER RIDE WAS ENGAGED AND THE GEAR RETRACTED NORMALLY. ON DESCENT, THE CREW REPORT
- [SDR AJC2005F00009](https://openairdocs.org/sdr/AJC2005F00009.md): Valve · failed · Jul 27, 2005 · N127BW · Beech 400A · Cabin Temperature Control System
  > AIR RETURNED DUE TO AIR CONDITIONING FAIL LIGHT ILLUMINATED AND CABIN REVERTED TO EMERGENCY PRESSURIZATION MODE. AIRCRAFT ISSUED SPECIAL FLIGHT PERMIT, FOR MAINTENANE AT SERVICE CENTER. MAINTENANCE FOUND THE CABIN TEMPERATURE CONTROL VALVE TO BE DEFECTIVE. R
- [SDR SFO2005F00003](https://openairdocs.org/sdr/SFO2005F00003.md): Heat Shield · failed · Jun 21, 2005 · N27SF · Cessna 500CESSNA · Engine (Turbine/Turboprop)
  > INSP, A LOUD SCRAPING NOISE WAS HEARD WHEN FAN WAS TURNED. BORESCOPE OF TURBINE SEC., AFTER EXHAUST DUCT WAS REMOVED, NR 4 BRG HSG HEAT SHIELD WAS FOUND BROKEN, TWISTED, IN 3 SEPARATE PIECES, WAS RUBBING ON AFT FACE OF NR 3 LOW PRESSURE TURBINE DISC. DISC WA
- [SDR 2005FA0000864](https://openairdocs.org/sdr/2005FA0000864.md): Clamp · defective · May 21, 2005 · N234DK · Beech 400A · Pneumatic System
  > DURING FLIGHT, THE CREW HEARD A POP AFTER WING DEICE HAD BEEN TURNED ON. THEY PERFORMED THE NESSARY PROCEDURES ACCORDING TO THE CHECKLIST. DETAILED INSPECTION REVEALED THAT THE SUSPECT CLAMP HAD SEPARATED AND CAUSED ENGINE BLEED AIR TO DUMP INTO THE AFT EQUI
- [SDR 2005FA0000630](https://openairdocs.org/sdr/2005FA0000630.md): Relay · loose · Jan 27, 2005 · N430CW · Beech 400A · Windshield/Door Rain/Ice Removal
  > CREW SQUAWKED ELEC FUMES AND FOUL ODOR IN COCKPIT. ODOR SEEMED TO LET UP AFTER BATTERY PLACED IN EMERG AND BOTH GENERATORS PLACED IN EMERG. MAINT FOUND RT WINDSHIELD HEAT CURRENT SENSE RELAY (L102S) TERMINAL B AND APPROX 2 INCHES OF WIRE INSULATION TO OVERHE
- [SDR 2005FA0000098](https://openairdocs.org/sdr/2005FA0000098.md): Heat Shield · damaged · Nov 7, 2004 · N567EA · Cessna 500CESSNA · Tire
  > PILOT REPORTED, HE HAD HIT AN OBJECT ON RUNWAY DUE TO IMPACT SOUND HEARD ON LT SIDE OF AC AND BRAKE ANTI-SKID FAIL INDICATION. INVESTIGATED LT WHEEL AREA AND DISCOVERED THAT TIRE HEAT SHIELD HAD PARTIALLY DISLOGED FROM WHEEL ASSY. INSPECTED AREA AND FOUND PA
- [SDR O2G2004F00008](https://openairdocs.org/sdr/O2G2004F00008.md): Bearing · worn · Oct 22, 2004 · N23YZ · Cessna 560CESSNA · Wheel/Ski/Float
  > RUMBLE FROM LT MAIN GEAR. REMOVED AND REPLACED MAIN WHEEL BEARING, WHEEL AND TIRE.
- [SDR 2004FA0000676](https://openairdocs.org/sdr/2004FA0000676.md): Battery · exploded · Aug 6, 2004 · N999AM · Cessna 500CESSNA · Battery/Charger System
  > WHILE ATTEMPTING TO PERFORM AN ENGINE START A LOUD NOISE WAS HEARD AND THE START WAS ABORTED. AN INVESTIGATION REVEALED THE MAIN BATTERY HAD EXPLODED. SEVEN OF THE TWELVE CELL CAPS WERE BLOWN OFF AND THE TOP COVER WAS BROKEN AND BLOWN OFF. BATTERY ELECTROLY
- [SDR R2J2004F00000](https://openairdocs.org/sdr/R2J2004F00000.md): Brace · mismanufactured · Jun 29, 2004 · N501CF · Cessna 501 · Trailing Edge Flaps
  > WHILE REINSTALLING LT WING FLAP CABLES DURING PHASE 5 INSPECTION, NOTICED CABLE RUN TOO CLOSE TO STRUCTURE. INVESTIGATION AND NOTIFIED MFG TECH SUPPORT. IT WAS DETERMINED LT BRACE 5511037-3 AND RIB 5525130, CABLE PASS THRU WERE INCORRECTLY LOCATED DURING MAN
- [SDR R2J2004F00001](https://openairdocs.org/sdr/R2J2004F00001.md): Control Cable · misinstalled · Jun 29, 2004 · N501CF · Cessna 501 · Trailing Edge Flap Control System
  > DURING PHASE 5 INSPECTION, UPON REINSTALLING LT WING FLAP CABLES, NOTICED AIRCRAFT WAS DIFFERENT THAN MM DATA AS TO ROUTING OF FLAP CABLES ON LT OB BELLCRANK. EXPERIMENTED AND CONTACTED MFG TECH SUPPORT. FOUND DATA ON PG 27-50-01 PG 203 FIG 201 (SHEET 2) SHO
- [SDR JEM2004F00001](https://openairdocs.org/sdr/JEM2004F00001.md): Bracket · cracked · Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer Structure
  > DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED U
- [SDR JEM2004F00002](https://openairdocs.org/sdr/JEM2004F00002.md): Bracket · cracked · Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer Structure
  > DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED U
- [SDR JEM2004F00003](https://openairdocs.org/sdr/JEM2004F00003.md): Rib · cracked · Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED
- [SDR JEM2004F00004](https://openairdocs.org/sdr/JEM2004F00004.md): Rib · cracked · Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPISHED U
- [SDR JEM2004F00005](https://openairdocs.org/sdr/JEM2004F00005.md): Rib · cracked · Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED
- [SDR JEM2004F00006](https://openairdocs.org/sdr/JEM2004F00006.md): Rib · cracked · Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED
- [SDR YNO2004F00002](https://openairdocs.org/sdr/YNO2004F00002.md): Uplock Switch · inoperative · Apr 12, 2004 · N62NS · Cessna S550 · Landing Gear Position and Warning
  > ON APRIL 12, 2004 AT APPROX 10:30 AM, AIRCRAFT WAS DEPARTING WHEN GEAR WAS SELECTED UP, THE RT MAIN GEAR WOULD NOT COME UP AND LOCK. THE PILOTS COMPLETED THE CHECKLIST, THE GEAR WAS SELECTED DOWN AND HAD AN ALL GEAR SAFE CONDITION. THE AIRCRAFT DIVERTED AND
- [SDR CWQ2004F00008](https://openairdocs.org/sdr/CWQ2004F00008.md): Piccolo Tube · corroded · Mar 3, 2004 · N348QS · Cessna 560CESSNA · Airfoil Anti/De-ice System
  > DURING ROUTINE PHASE 1-4 INSP, THE MECH GRABBED THE LIP BLEED AIR FEED TUBE NR 1 ENGINE AND APPLIED PRESSURE BACK AND FORTH, A NOISE WAS HEARD BANGING AT EACH STROKE. AFTER FURTHER DISASSEMBLY (REMOVAL OF LIP) FOUND THE 6552502-3, PICCOLO ASSY ATTACH LEGS (2
- [SDR 40188138](https://openairdocs.org/sdr/40188138.md): Bracket · cracked · Feb 26, 2004 · N26NS · Cessna 500CESSNA · Elevator Structure
  > BALANCE WEIGHT ARM FOR ELEVATOR CONTROL SYSTEM IS CRACKED.
- [SDR GVR2004F00000](https://openairdocs.org/sdr/GVR2004F00000.md): Seat Back · cracked · Jan 15, 2004 · N13ST · Cessna 501 · Passenger Compartment Equipment
  > UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. ALSO, CHAIR BASE HAS HAD PREVIOUS INAPPROPRIATE REPAIR MADE. CHAIR WAS REPAIRED.
- [SDR KBM2003F00080](https://openairdocs.org/sdr/KBM2003F00080.md): Window · cracked · Oct 29, 2003 · N677JM · Cessna 501 · Flight Compartment Windows
  > LT FORWARD WINDOW CRACKED AND CRAZED. REMOVED AND REPLACED.
- [SDR CA030604002](https://openairdocs.org/sdr/CA030604002.md): Hose · ruptured · May 20, 2003 · Cessna 560CESSNA · Engine Thrust Reverser
  > (CAN) WHILE PREPARING TO REFUEL THE AIRCRAFT, PILOT NOTED A LARGE QUANTITY OF HYDRAULIC FLUID ON THE RT ENGINE/THRUST REVERSER AREA. THE AFT HYDRAULIC HOSE CONNECTING THE TAIL ROTOR TO THE PYLON HAD BURST AT APPROXIMATELY MID LENGTH. (THIS IS THE AREA WHERE TH
- [SDR AUS20030484](https://openairdocs.org/sdr/AUS20030484.md): Engine · seized · Apr 17, 2003 · Cessna 500CESSNA · Engine (Turbine/Turboprop)
  > (AUS) RT ENGINE FAILED AND COULD NOT BE RESTARTED. INVESTIGATION FOUNDTHE ENGINE SEIZED.
- [SDR 03FDEA00386](https://openairdocs.org/sdr/03FDEA00386.md): Warning Light · failed · Apr 4, 2003 · N234FE · Boeing 727200 · Cabin Temperature Indicator
  > EQUIPMENT COOLING LIGHT CAME ON IN FLIGHT. PULLED RADIO ALT CB VIA THE QRH AND LIGHT WENT OUT FOR A FEW MINUTES. LIGHT THEN CAME BACK ON STEADY. QHR SAID LAND, ASAP. ON RETURN TO MEMPHIS, LIGHT WENT OUT A COUPLE OF TIMES IN THE DESCENT BUT WAS ON MOST OF

Next page: https://openairdocs.org/engine/pratt-whitney-canada-jt15d-1-series/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 engine_model_key = 'JT15D1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-jt15d-1-series/reports

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