GE CT7-5A2

Service difficulty reports · 450

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'CT75A2'
  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 121271Chip Detector · malfunctionedDURING CLIMB THE LT ENGINE CHIP DETECTOR WARNING LIGHT ILLUMINATED FOR A FEW SECONDS THEN WENT OUT. THE CREW NOTIFIED MOC AND TURNED TO GO BACK TO IAD. ON 5 MILE FINAL THE LT CHIP DETECTOR LIGHT RE-ILLUMINATED AND WOULD NOT EXTINGUISH. THE CREW FOLLOWED THEAug 26, 2004 · N35SZ · Saab SF340A · Engine Oil Indicating SystemSDR 080963Engine · failedWHILE CLIMBING THROUGH 6500 LT ENGINE TORQUE WENT ERRATIC AND ITT SPIKED TO 940 POSSIBLY 960 SHUTDOWN AND RETURNED TO THE FIELD.Aug 16, 2004 · N123XS · Saab SF340A · Engine (Turbine/Turboprop)SDR 120411Warning Light · interferenceDURING CRUISE THE CREW NOTICED THE RT ENGINE OIL PRESSURE DROPPING TO THE LOW SIDE OF THE GREEN ARC. CREW FOLLOWED QRH AND CONTACTED MOC AND SOC. MOC ADVISED THE CREW TO MONITOR AND CONTINUE TO HPN. SHORTLY AFTER HANGING UP INDICATION CONTINUED TO DROP INTOAug 13, 2004 · N19XS · Saab SF340A · Engine Oil Indicating SystemSDR 066641Indicator · inoperativeON TAKEOFF ROLL, TQ INDICATOR REMAINED AT ZERO ON THE LT SIDE. AIRCREW RETURNED TO THE GATE.Aug 2, 2004 · N148SD · Saab SF340A · Engine BMEP/Torque IndicatingSDR 127712Engine · malfunctionedFLIGHT 7889 IAD-TYS. DURING CLIMBOUT OF IAD CREW REPORTED LOSS OF RT ENGINE POWER. CREW DECLARED AN EMERGENCY AND RETURNED TO IAD.Jul 29, 2004 · N360SZ · Saab SF340A · Engine (Turbine/Turboprop)SDR 079471Unknown · unknownFLIGHT 7966 IAD-HPN. DURING TAKEOFF ROLL AT ABOUT 90 KNOTS THE CREW NOTICED THE LT TORQUE INDICATOR FLUCTUATING APPROXIMATELY 8-10 PERCENT. CTOT WAS ARMED. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE. A/C TAKEN OUT OF SERVICE 7-28-04 AT 2320 (LT). IAD MJul 28, 2004 · N146SD · Saab SF340A · Engine (Turbine/Turboprop)SDR 119522Ahrs · failedFLIGHT 7941 IAD-BGM. DURING TAKEOFF ROLL THE FIRST OFFICER'S EADI SHOWED A 40 DEGREE TURN AND 10 DEGREES NOSE DOWN ATTITUDE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE. A/C TAKEN OUT OF SERVICE 7-27-04 AT 1745 (LT). IAD MX REMOVED AND REPLACED THE NJul 27, 2004 · N95 · Saab SF340A · Integrated Flight SystemSDR CA040805015Hub · cracked(CAN) ON LANDING, PILOTS FELT A LIGHT VIBRATION ON THE RT PROPELLER WHEN FEATHERING. AFTER INVESTIGATION FOUND PROPELLER HUB MATING FACE AND PGB FLANGE WITH A LIGHT PLAY. 6 ATTACH BOLTS OUT OF 12 WERE FOUND TO BE 1 TURN LOOSE ALTHOUGH THE SAFETY WIRE WAS STILJul 26, 2004 · Saab SF340A · Propeller Hub SectionSDR 213483Circuit Breaker · trippedFLIGHT 4574 LEX-PIT. DURING CRUISE CLOSE TO APPROACH INTO PIT THE RIGHT AVIONICS CIRCUIT BREAKER AHC-2 POPPED CAUSING THE FIRST OFFICER'S AVIONICS SYSTEM TO COMPLETELY BLANK OUT. THE CAPTAIN'S BOTTOM EFIS SCREEN WAS STARTING TO ALSO FADE. THE CREW ASKED ATCJul 1, 2004 · N150CN · Saab SF340A · Navigation SystemSDR 217671Indicator · inoperativeAPPROXIMATELY 1610 (UTC), FLT 4524 LEX-PIT, THE CREW HAD REJECTED TAKEOFF WHEN THE LT TORQUE GAUGE INDICATED ZERO WITH CONDITION LEVER MAX AND POWER LEVER ADVANCED.Jun 25, 2004 · N148SD · Saab SF340A · Power Indicating SystemSDR 071152Warning Light · illuminatedAPPROXIMATELY 1430 (UTC), FLT 7926 IAD-ABE. THE AIRCRAFT WAS EN ROUTE TO ABE WHEN THE CREW OBSERVED THE RIGHT FIRE DETECT FAIL INDICATION, FOLLOWED BY THE RIGHT FIRE WARNING. CREW FOLLOWED QRH PROCEDURES. BOTH EXTINGUISHERS WERE USED. THE ENGINE WAS SHUTDOJun 23, 2004 · N35SZ · Saab SF340A · Fire DetectionSDR 218651Warning Light · illuminatedAPPROXIMATELY 1220 (UTC), FLT 7993 HPN-IAD, AIRCRAFT WAS EN ROUTE TO IAD WHEN THE RT BLEED LIGHT ILLUMINATED. CREW FOLLOWED QRH, LIGHT REMAINED ON. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT.Jun 20, 2004 · N140CQ · Saab SF340A · Engine Bleed Air SystemSDR 210061Engine · bird ingestionFLIGHT 4556 PIT-FWA, DURING CLIMBOUT A DEADHEADING CREW MEMBER SAW A BIRD STRIKE THE LT NACELLE. FLIGHT ATTENDANT NOTIFIED THE CREW. THE LT TORQUE STARTED TO DROP WITH AN ASSOCIATED RISE IN TEMPERATURE. THE CREW WITH ADVICE FROM MOC TURNED BACK TO PIT. THEJun 18, 2004 · N152CQ · Saab SF340A · Engine (Turbine/Turboprop)SDR 022001AWarning Light · illuminatedFLIGHT 4644 PIT-BUF. DURING CRUISE AT 17K IFR ON TOP. THE RT ENGINE FIRE WARNING ON CWP ILLUMINATED ALONG WITH MASTER WARNING AND ASSOCIATED FIRE HANDLE ILLUMINATION. CREW FOLLOWED QRH AND PULLED RH FIRE HANDLE. THE CREW DID NOT NEED TO FIRE THE BOTTLE AS THMay 26, 2004 · N152CQ · Saab SF340A · Smoke DetectionSDR 227681Engine · malfunctionedON 05-17-04 APPROX. 1500 (UTC), FLT 9407, DURING CLIMB, THE CREW NOTICED RT OIL PRESSURE LIGHT ILLUMINATED IN CLIMB. RT ENGINE WAS SHUTDOWN, CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE.May 17, 2004 · N123XS · Saab SF340A · Turbine Engine Oil SystemSDR 010461Engine · surgesFLT 4563 FROM PIT TO AVP, 10 MINUTES INTO THE FLIGHT, AIRCREW FELT NR 1 ENGINE SURGE. AIRCREW REDUCED POWER TO 25 PERCENT AND THE ENGINE STEADIED ITSELF. AIRCRAFT RETURNED TO THE GATE.May 5, 2004 · N121CQ · Saab SF340A · Engine (Turbine/Turboprop)SDR 150711Warning Light · illuminatedAIRCRAFT HAD TAKEN OFF FROM LEX WHEN THE LT TAIL PIPE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO LEX WITHOUT INCIDENT.May 2, 2004 · N40SZ · Saab SF340A · Overheat DetectionSDR 150721Warning Light · illuminatedON 05-02-04, APPROX 1605 (UTC), FLT 8960 LEX-PIT ABORTED TAKEOFF WHEN THE LT TAIL PIPE HOT LIGHT ILLUMINATED.May 2, 2004 · N40SZ · Saab SF340A · Overheat DetectionSDR 115401Engine · malfunctionedDURING FLIGHT THE CREW RT ENGINE OIL PRESSURE DROPPED TO 30PSI WITH THE ASSOCIATED OIL PRESSURE WARNING ON THE CWP. CREW FOLLOWED THE QRH AND DIVERTED TO SCE. AFTER LANDING CREW CHECKED RH ENGINE OIL LEVEL. SIGHT GLASS SHOWED BELOW NORMAL. CREW NOTICED NO Apr 18, 2004 · N35SZ · Saab SF340A · Turbine Engine Oil SystemSDR 109161Governor · malfunctionedAIRCRAFT ABORTED TAKE OFF WHEN THE RT POWER WOULD NOT SET. POWER LEVERS BROUGHT TO 80 PERCENT, CTOT SET TO 90 PERCENT. LT WENT TO 90 PERCENT, RT STAYED AT 80 PERCENT.Apr 17, 2004 · N360SZ · Saab SF340A · Propeller GovernorSDR 150131Connector · disconnectedDURING CLIMB-OUT THE LH TAILPIPE HOT LIGHT ILLUMINATED ON THE CENTRAL WARNING PANEL. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT. A/C TAKEN OUT OF SERVICE 4-12-04 AT 1415 (LT). PIT MX REMOVED MOISTURE CONTAMINATION FROM LT TAILPIPE SENSOR CONNECTION AND RApr 12, 2004 · N150CN · Saab SF340A · Electrical ConnectorsSDR 150141Connector · dirtyDURING CLIMB OUTTHE LT TAILPIPE HOT LIGHT ILLUMINATED ON THE CWP. THE CREW FOLLOWED THE QRH AND SHUT THE ENGINE DOWN, DECLARED AN EMERGENCY AND LANDED SAFELY BACK IN PIT. A/C TAKEN OUT OF SERVICE 4-12-04 AT 1830 (LT) PIT MX INSPECTED AND CLEANED LH TAILPIPEApr 12, 2004 · N150CN · Saab SF340A · Electrical ConnectorsSDR 112161Engine · shutdownDURING CLIMB OUT THE CREW HEARD A LOUD BANG FROM THE LH ENGINE WHICH THEN HAD AN UNCOMMANDED SHUTDOWN. THE PROP FEATHERED AS IT SHOULD, THE CREW DECLARED AN EMERGENCY AND LANDED BACK IN BUF SAFELY. AFTER LANDING THE CREW INSPECTED THE LT ENG FOR SIGNS OF FOD IMar 30, 2004 · N148SD · Saab SF340A · Engine (Turbine/Turboprop)SDR 102851Warning System · erraticPILOT NOTICED THE TORQUE INDICATION BEING ERATIC ON THE RT ENGINE DURING TAKEOFF ROLLOUT AT ABOUT 70 KTS. PILOT RETARDED THE THROTTLES AND RETURNED TO THE GATE.Mar 22, 2004 · N35SZ · Saab SF340A · Engine BMEP/Torque IndicatingSDR 102831Engine · malfunctionedDURING TAKE-OFF ROLL AT APPROXIMATELY 80-90 KNOTS THE CREW NOTICED THE RT ENGINE TORQUE FLUCTUATING FROM 70-115 PERCENT. THE CREW RETARDED THE POWER LEVERS AND ABORTED THE TAKE-OFF. A/C TAKEN OUT OF SERVICE 3-21-04 AT 1755 (LT)Mar 21, 2004 · N35SZ · Saab SF340A · Engine (Turbine/Turboprop)SDR 027751Landing Gear · malfunctionedDURING CLIMBOUT FROM PIT THE AIRCREW RAISED THE GEAR HANDLE, THE TRANSIENT LIGHT REMAINED ON AND THE HYDRAULIC PUMP CONTINUED TO RUN. THE CREW ATTEMPTED ANOTHER GEAR CYCLE AND HAD THE SAME RESULTS. A/C RETURNED TO PIT.Feb 7, 2004 · N19XS · Saab SF340A · Main Landing GearSDR 189301Warning Light · illuminatedON 02-06-04, APPROX 1500 (UTC), FLT 4591 PIT-TOL. ON TAKEOFF ROLL, RT ENGINE OVERTEMP LIGHT ILLUMINATED. LP BLEEDS IN AUTO, HP BLEEDS OFF AND ANTI-ICE ON.Feb 6, 2004 · N140CQ · Saab SF340A · Engine Temperature Indicating SystemSDR 118161Warning Light · illuminatedON 02-06-04, APPROX 16450 (UTC), FLT 4591 PIT-TOL. ON TAKEOFF ROLL, RT ENGINE OVERTEMP LIGHT ILLUMINATED. LP BLEEDS IN AUTO, HP BLEEDS OFF AND ANTI-ICE ON.Feb 6, 2004 · N43SZ · Saab SF340A · Engine Temperature Indicating SystemSDR CA040210006Pressure Switch · leaking(CAN) DUE TO INTERNAL LEAKAGE OF DIFFERENTIAL PRESSURE SWITCH, A LOST OF FUEL WAS HAPPENING THRU THE OVERBOARD DRAIN WHICH WAS CREATING A PRESSURE DROP IN FUEL PUMP SYSTEM, THE AUX PUMP WOULD THEN COME ON AND OFF THUS CREATING A SMALL FLUCTUATIONIN THE ENGINE Feb 6, 2004 · Saab SF340A · Fuel Pressure SensorSDR 189661Propeller · malfunctionedON 02/05/04, APPROX 1630 (UTC), FLT 4518 ERI-PIT. CREW BEGAN TAKEOFF ROLL AND ENGAGED CTOT. ONCE THE CTOT WAS ENGAGED, THE LT TORQUE BECAME ERRATIC AND FLUCTUATED. CREW PULLED POWER BACK, ABORTED TAKEOFF AND RETURNED TO GATE.Feb 5, 2004 · N150CN · Saab SF340A · Propeller Controlling SystemSDR AUS20040066Sensor · faulty(AUS) LT ENGINE PROPELLER GEARBOX OIL PRESSURE SENSOR FAULTY.Feb 3, 2004 · Saab SF340A · Engine Oil PressureSDR 187531Engine · malfunctionedDURING CRUISE THE CREW SET THE RIGHT ENGINE POWER AT 80 PERCENT TQ. THE CREW HEARD A LOUD BANG, FELT A SLIGHT YAW AND NOTICED THAT THE RIGHT TQ HAD DROPPED TO APPROX 70 PERCENT. THE CREW ADJUSTED THE TQ AND THEN HEARD MULTIPLE BANGS ALONG WITH A DROP IN RIGHFeb 1, 2004 · N158SD · Saab SF340A · Engine (Turbine/Turboprop)SDR 187532Compressor · stalledFLIGHT 4593 PIT-TOL. AFTER THE A/C RETURNED TO PIT DUE TO MULTIPLE COMPRESSOR STALLS, THE A/C WAS PARKED WHEN A BAGGAGE CART CAME LOOSE FROM THE TUG THAT WAS PULLING IT AND SLAMMED INTO THE AFT PART OF THE A/C FUSELAGE BEHIND THE CARGO DOOR.Feb 1, 2004 · N158SD · Saab SF340A · Turbine Engine Compressor SectionSDR 181161Indicator · erraticON 01-28-04, APPROX 1535 (UTC), FLT 4501 PIT-LEX, AIRCRAFT RETURN TO FIELD WHEN THE CAPTAIN'S AIRSPEED INDICATOR HAS ERRATIC READING ALONG WITH THE RUDDER LIMIT ILLUMINATED ON THE CWP.Jan 28, 2004 · N118SD · Saab SF340A · Airspeed/Mach IndicatorSDR AUS20040053O-Ring · leaking(AUS) LT ENGINE POWER TURBINE (C) SUMP COVER O-RING SEAL LEAKING.Jan 28, 2004 · Saab SF340A · Turbine Engine Oil SystemSDR 002841Warning Light · illuminatedON 01-27-04, APPROX 1230 (UTC), FLT 4597 TOL-PIT. THE CREW EXPERIENCED AN AC GENERATOR FAIL LIGHT FOR THE RIGHT AC GENERATOR. WEATHER NOT PERMITTING THE FLIGHT TO CONTINUE, THE AIRCRAFT RETURNED TO TOL.Jan 27, 2004 · N340SZ · Saab SF340A · AC Generation SystemSDR 002701Fuel Control · inoperativeON 01-20-2004, APPROX 1130 (UTC), FLT 4633 BGM-PIT, NR 1 ENGINE HAD NO FUEL FLOW, ENGINE WOULD NOT START.Jan 20, 2004 · N340SZ · Saab SF340A · Fuel Controlling SystemSDR 002072Fuel Control · malfunctionedON 01-20-2004, APPROX 1400 (UTC), FLT 4568, PIT-LYH, NR 1 ENGINE HAS NO FUEL FLOW, ENGINE WILL NOT START.Jan 20, 2004 · N340SZ · Saab SF340A · Fuel Controlling SystemSDR 146951Warning Light · illuminatedON 01-16-2004, APPROX 1245 (UTC), FLT 4625 SCE-PIT, CREW RETURNED TO GATE WHEN THE GUST LOCK WARNING ILLUMINATED WITH THE GUST LOCK RELEASED.Jan 16, 2004 · N148SD · Saab SF340A · Gust Lock Damper SystemSDR 028741Autocoarsen Sys · inoperativeON 01-16-2004, APPROX. 1125 (UTC), FLT 4520 CMH-PIT. CREW ABORTED TAKEOFF WHEN THE AUTOCOARSEN SYSTEM DID NOT ARM.Jan 16, 2004 · N150CN · Saab SF340A · Propeller Feathering/ReversingSDR 002171Engine · malfunctionedON 01-16-2004, AT APPROX 1125 (UTC), FLT 4633, BGM-PIT, CREW HAD RETURNED TO GATE. THE LEFT ENGINE WOULD NOT LIGHT OFF. THERE WAS NO FUEL FLOW INDICATION ON THE LEFT ENGINE.Jan 16, 2004 · N146SD · Saab SF340A · Engine (Turbine/Turboprop)SDR 004851Warning Light · illuminatedON 01/02/2004 APPROX 1230 (UTC), FLT 4587 TTN-BED, CREW REPORTED THAT THE RT ENGINE INTAKE DE-ICE LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO TTN.Jan 2, 2004 · N340SZ · Saab SF340A · Air Intake Anti/De-Ice SystemSDR 000011Warning Light · illuminatedON 01/02/04, APPROX. 1530 (UTC), FLT 4632 CAK-PIT. THE CARGO AND LAV SMOKE LIGHT CAME ILLUMINATED ON THE GROUND. CREW BLEW THE CARGO FIRE EXTINGUISHER BOTTLE AND EVACUATED PASSENGERS.Jan 2, 2004 · N40SZ · Saab SF340A · Smoke DetectionSDR 011271Panel · malfunctionedTHE CREW ABORTED TAKEOFF WHEN THE CTOT ON THE RT SIDE ARMED AND THEN DISARMED.Dec 23, 2003 · N150CN · Saab SF340A · Propeller Controlling SystemSDR 035801Generator · failedWHEN A/C GOT TO CRUISE ALTITUDE THE RIGHT DC GEN FAILED BRIEFLY. THE CREW GOT IT TO RESET, THEN IT FAILED AGAIN AND WOULD NOT RESET. A/C RETURNED TO PIT. IT WAS TAKEN OUT OF SERVICE 12-10-03 AT 2310(LT).Dec 10, 2003 · N43SZ · Saab SF340A · DC Generating SystemSDR MALA030530Engine · malfunctionedDURING FLIGHT 3009, LT ENGINE SHOWING GRADUAL LOSS IN ITT MARGIN. LT ENGINE PLACED ON DERIVITIVE POWER FOR CONTINUED SERVICE. CTOT AND ANTI SKID SYSTEMS MUST BE OPERATIVE. MAINTENANCE PROCEDURES COMPLIED WITH FOR DERIVATIVE POWER PROGRAM. CHAP 2, SECTION 2Dec 3, 2003 · N110XJ · Saab SF340A · Engine (Turbine/Turboprop)SDR 030971Indicator · failedON 12/01/03, AT 1515Z FLT 4523, AIRCRAFT ABORTED TAKEOFF WHEN THE LEFT TORQUE INDICATOR WENT TO ZERO AT V1. CREW RETURNED AIRCRAFT TO FIELD.Dec 1, 2003 · N35SZ · Saab SF340A · Propeller Indication SystemSDR 008181Connector · damagedAIRCRAFT ABORTED TAKEOFF WHEN ERRATIC TORQUE INDICATIONS WERE OBSERVED ON THE NR 2 ENGINE. ENGINE TORQUE INDICATION WAS FLUCTUATING FROM 50 TO 120 WITH CTOT ENGAGED. AT 1350Z, FWA MX REPORTED OF TIGHTENING A LOOSE BACKSHELL ON A ECU CONNECTOR. THE AIRCRAFT WNov 29, 2003 · N138SD · Saab SF340A · Propeller Controlling SystemSDR 1409061Warning Light · illuminatedON 11/29/03, FLT 4624 CMH-PIT, AIRCRAFT N104CQ RETURNED TO GATE. PRIOR TO TAKEOFF WITH POWER LEVERS JUST ABOVE FLIGHT IDLE NR 2 ENGINE SUDDENLY MADE A LOUD ROARING SOUND AND ENGINE OVERTEMP LIGHT ILLUMINATED. AFTER MOVING NR 2 CONDITION LEVER TO FEATHER ENGINENov 29, 2003 · N104CQ · Saab SF340A · Engine Fuel Indicating SystemSDR 013042Yoke · vibrationON CLIMBOUT, A STRONG (FWD-AFT) VIBRATION WAS FELT ON THE CAPTAIN YOKE. CREW LEVELED OFF AT 2000 FT, VIBRATION CONTINUED FROM 150-200 KTS. CREW REDUCED SPEED TO 180 KTS, RETURNED TO FIELD WITH VIBRATION CONTINUING UNTIL FLAPS RETRACTED.Nov 28, 2003 · N152CQ · Saab SF340A · Control Column Section
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