JASC 7200
Service difficulty reports · 14,730
Reports filed under 7200 · Engine (Turbine/Turboprop), newest first.
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 jasc_code = '7200' 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.
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 jasc_code = '7200' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA116927Engine · failedDIVERSION/INFLIGHT SHUTDOWN - LOAD VIBRATIONS ON LT SIDE FOLLOWED BY COMPRESSOR STALL, THEN ENGINE SHUTDOWN WITH OIL PRESSURE ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW MT.SDR CA111011006Engine · smoke(CAN) DURING CLIMB, THE PILOT HEARD A NOISE FROM NR 2 ENGINE ACCOMPANIED BY SEVERE VIBRATION AND TORQUE FLUCTUATIONS. HE DECIDED TO RETURN TO THE DEPARTURE AIRPORT DURING WHICH TIME A BURNING/SMOKE SMELL WAS DETECTED IN THE COCKPIT. THE ENGINE WAS SECURED UPSDR CA111011005Engine · failed(CAN) SHORTLY AFTER TAKEOFF, THE PILOT REPORTED A LOW OIL PRESSURE ALARM FOLLOWED BY AN ENGINE FIRE ALARM. PULLED FIRE HANDLE AND SHUT THE ENGINE DOWN AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED AT THE DEPARTURE AIRPORT. POST FLIGHT INSPECTION FOUND A SDR 2011F00206Engine · malfunctionedRIGHT ENGINE SURGED AND OVER TORQUED, RT ENGINE SHUTDOWN IN THE AIR.SDR QMLA2011093011097Engine · power lossTHE PILOT REPORTED, AFTER PREFLIGHT AND CONFIRMATION CHECKS WERE CONDUCTED, LIFTED TO HOVER. USED THE ENGINE BEEP SWITCH TO SLIGHTLY INCREASE THE NR/N2 RPM TO 100 PERCENT. ON CLIMBOUT REACHING 900 FEET MSL, REDUCED COLLECTIVE TO 50 % ENGINE TORQUE TO ASSESSSDR CHQA201100395Engine · leakingCREW REPORTED THAT DURING TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT-HAND ENGINE. ALL LEAK CHECKS AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECSDR 2011FA0000653Bearing · failedWHILE IN CRUISE FLIGHT, ENGINE CHIP LIGHT ILLUMINATED, PILOT LANDED IN FIELD. INSP OF BOTH ENGINE CHIP DETECTORS REVEALED MULTIPLE CHIPS. THE SOURCE OF THE METAL WAS DUE TO FAILURE OF THE PTO BEARING, PN (M250-10121) THE ENGINE GEARBOX IS AN "ON CONDITION" ISDR CA111011003Engine · malfunctioned(CAN) PREPARING FOR A REPOSITIONING FLIGHT, AS THE THROTTLES WERE ADVANCED TO TAKE THE RUNWAY, THE CREW RECEIVED AN ENGINE FAIL CAS MESSAGE. THE ENGINE SHUT ITSELF DOWN AND AUTO RE-LIT A FEW SECONDS LATER. THE T/O WAS ABORTED AND THE AIRCRAFT TAXIED BACK TO THSDR DXTA2011102004757Engine · flamed outAS THROTTLES ADVANCED, RECEIVED A RED "RIGHT ENGINE FAIL" CAS MESSAGE. THE ENGINE FAILED (SHUTDOWN) AND A FEW SECONDS LATER RE-LIT. PERFORMED TROUBLESHOOTING PROCEDURE OUTLINED IN MM 72-00-00. NO DEFECTS NOTED. PERFORMED A SATISFACTORY 5 POINT GROUND PERFOSDR CA111014003Engine · making metal(CAN) OPERATOR FOUND METALLIC DEBRIS IN THE RGB SCAVENGE OIL FILTER, WHICH DEBRIS RE-OCCURRED IN SUBSEQUENT OPERATION AFTER THE FILTER WAS CLEANED. MATERIAL ANALYSIS CONFIRMED THE PRESENCE OF M50 BEARING MATERIAL AND THE ENGINE WAS REMOVED FOR INVESTIGATION ASDR TX9Y20110928006Valve · malfunctionedAIRCRAFT DEPARTED AIRPORT TO PERFORM A FUNCTIONAL TEST FLT, AFTER HEAVY CHECK. ON CLIMBOUT, ACFT DEVELOPED PROBLEMS WITH THE NR 1 ENGINE NACELLE OVERHEAT RUNNING HIGH WHICH INDICATED ON BOTH A AND B DETECTION SYSTEM INDICATORS, ALSO AT THIS TIME A "BURNING ODSDR C2XA11SH146Frame · corrodedSHV - DURING C-CHECK NR 1 ENGINE FORWARD FRAME ASSY AFT FLANGE CORRODED IN VARIOUS AREA. MAINTENANCE REPAIRED NR 1 ENGINE FORWARD FRAME ASSY AFT FLANGE IAW ROLLS-ROYCE TECHNICAL VARIANCE NO. 116298 ISSUE 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR CA111011002Engine · malfunctioned(CAN) TWO SEPARATE IFSD`S OCCURRED, THE 1ST ONE, IN CLIMB, PASSING FL70, THE LOW OIL PRESSURE WARNING CAME ON. RETARDING THE POWER LEVER HAD NO EFFECT AND THE OIL PRESSURE KEPT FALLING. THE ENGINE WAS SHUTDOWN. POST FLIGHT INSP RESULTED IN ADDING 2 QTS OF OILSDR CHQA201100388Engine · smokeAFTER TAKEOFF, RECEIVED A LAVATORY SMOKE INDICATION ON EICAS. F/A VERIFIED SMOKE COMING FROM LAVATORY. RETURNED AND LANDED WITHOUT INCIDENT. FIRE DEPT. INFRARED IMAGING LOCATED HOT AREA IN FLOOR OF CARGO BAY TO FLOOR OF LAVATORY. MAINTENANCE FOUND RT ENGSDR COMA2011092750072Engine · vibrationON CLIMBOUT FROM DTW CONSTANT LEFT ENGINE N1 VIB INDICATION, AT NORMAL CRUISE POWER IN EXCESS OF 3.2. NORMAL INDICATION AT REDUCED LESS THAN 60 PERCENT POWER SETTINGS. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. PERFORMED INSPECTION OF LEFT ENGINSDR CA110927006Engine · overtemp(CAN) DURING CLIMB THE CREW HEARD BANG SOUND FOLLOWED BY ACFT VIBRATION. LT ENGINE ITT INDICATING OVERTEMP WITH DECREASING N1 & N2, THE CREW SHUTDOWN THE LT ENGINE, DECLARED EMERGENCY THEN BACK TO THE ORIGIN. MX CONFIRMED ITT 1149 DEGREE CELSIUS MAXIMUM. SDR C2XA11CL217Engine · vibrationEWR FLT 4683 THE CREW REPORTED A ENGINE NR 1 HP VIBRATION AMBER INDICATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT NR 1 ENGINE VIB INDICATION PER RRFIM 77-41-00-810-802. VIBES WERE WITHIN SDR AALA20110924DFW02Engine · failedDFW - CREW REPORTED DURING CLIMBOUT, LEFT ENGINE OIL PRESSURE INDICATION DROPPED TO ZERO WITH QUANTITY NORMAL. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 7 MINS). EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SDR R61A20110275Engine · vibrationCREW REPORTED HIGH E-2 LP VIBES IN FLIGHT. CREW DECLARED AN EMERGENCY AND DIVERTED TO LAS, THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE IS CURRENTLY IN PROCESS OF REPLACING E-2 PER EMB AMM.SDR CA110929007Engine · failed(CAN) DURING TEST FLIGHT, AFTER INSTALLATION OF THE FRESHLY O/H P/S, DURING AN AUTO-ROTATION MANEUVER, THE PILOT HEARD A LOUD NOISE AND RECEIVED A CHIP DETECTOR WARNING. HE WAS ABLE TO SAFELY LAND THE ACFT. POST FLIGHT INSPECTION FOUND THE P/S GAS GENERATORSDR CA110929006Engine · fluctuates(CAN) AFTER T/O AT AN ALTITUDE OF 350-400 FT, THE ENGINE TORQUE AND SPEEDS BEGAN TO FLUCTUATE FOLLOWED BY AN UNCOMMANDED POWER LOSS. THE PILOT DUMPED THE CONTENTS OF THE HOPPER AND RETURNED TO THE DEPARTURE STRIP WHERE HE LANDED SAFELY. TROUBLESHOOTING IS ON-SDR CA110929005Engine · making metal(CAN) DURING CLIMB, AN UNCOMMANDED PROPELLER FEATHER OCCURRED. THE CREW ELECTED TO SHUT THE ENGINE DOWN BEFORE RETURNING TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. POST FLIGHT INSPECTION REVEALED SIGNIFICANT AMOUNT OSDR CA110928001Engine · malfunctioned(CAN) DURING FLIGHT, THE MASTER WARNING LIGHT ILLUMINATED FOLLOWED BY TORQUE PRESSURE AND OIL PRESSURE DROP TO ZERO. THE PILOT SHUT THE ENGINE DOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. THE ENGINE CONDITION IS UNKNOWN BUT IT WILL BE REMOVED ASDR UALA2011092105109Engine · surgesNR 2 ENGINE HAS PERFORMANCE PARAMETER SHIFT. RIGHT ENGINE CONDITION MONITORING (ECM) DETECTED A SURGE ON ROLL OUT, THIS IS A RING CASE ENGINE, VISUALLY CHECK INLET & EXHAUST, 2.5 BLEED AND 2.9 BLEED OPENINGS FOR DAMAGE OR UNUSUAL MATERIAL, CHECK IP CHECK VALVSDR QMLA2011092111094Engine · making metalNR 2 ENG CHIP LIGHT ILLUMINATED, FOUND MINOR DEBRIS ON GEARBOX CHIP DETECTOR AT 13137 ACFT TT. CLEANED DETECTOR IAW LTS 101 2.2MM CHAP 72-00-00, RETURNED ACFT TO SERVICE. NR 2 ENG CHIP LIGHT ILLUMINATED 2ND TIME INTERMITTENTLY WITH TURBINE CHIP LIGHT ALSO ILLSDR C2XA11IA223Engine · shutdownFLIGHT 2335, CREW REPORTED AN UNCOMMANDED ENGINE NE SHUTDOWN AT 7700FT. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURSDR CA110921001Bearing · failed(CAN) ENGINE WAS SENT FOR A SCHEDULED O/H. DISASSEMBLY OF ENGINE REVEALED THAT THE ENGINE HAD METAL CONTAMINATION IN THE OIL FILTER AND OIL FILTER HSG. THE SOURCE OF THE METAL CONTAMINATION WAS THE DUPLEX BEARING ON THE AGB INPUT DRIVE GEAR WHICH HAD A THOUSDR CA110921005Engine · shutdown(CAN) AIR RETURN NR 1 ENG SHUTDOWN IN FLT CREW HEARD A LOUD BANG AT V1, UNCOMMANDED FEATHER OF THE NR 1 ENGINE ON ROTATION, (TOWER REPORTED SEEING SMOKE). CREW CONTINUED THE FEATHER PROCEDURE, AND AT 1000" SHUTDOWN & SECURED THE ENGINE. ENGINE, PROP AND OIL CSDR CA110929002Engine · smoke(CAN) DURING FINAL, THE POWER ON THE RT ENGINE WAS RETARDED TO IDLE. SMOKE AND THE ODOR OF OIL SMOKE ENTERED THE CABIN. THE LANDING WAS CARRIED OUT AND AN EMERGENCY EVACUATION WAS CARRIED OUT AFTER TOUCH DOWN. POST EVENT TROUBLESHOOTING FOUND NO EXPLANATION SDR FDEA201109173927Engine · malfunctioned2 HRS AFTER TAKEOFF, NR 2 ENGINE ROLLED BACK. RPM AND EGT ROLLEDBACK, PERFORMED ENGI 2 SHUTDOWN IN FLIGHT. CHECKED NR 2 EEC A & B, NO CURRENT FAULTS. CARRIED OUT DETAIL AND WINDMILLING INSPECTION, CHECKED ALL MAGNETIC CHIP DETECTORS, NO ABNORMALITIES FOUND. SDR C2XA11CL208Engine · faultyIAD FLT 5861 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.SDR DATR001632Bolt · failedRT SIDE ENGINE EXPERIENCED A LOW OIL PRESSURE LIGHT 1.5 HOURS INTO MISSION AND SUBSEQUENT PRESSURE LOSS. ENGINE WAS SHUTDOWN IN FLIGHT AND ACFT DIVERTED. THE ENGINE WAS RECEIVED AT THIS FACILITY FOR INVESTIGATION. THE PROPELLER SHAFT WAS HARD TO TURN AND A SDR UHLA2011091600336Engine · leakingSTRONG SMELL OF TURBINE OIL IN CABIN DURING TAKEOFF CLIMBOUT. FOUND A SUMP LEAKING, REPLACED DRAIN LINE O-RINGS, OIL SMELL STILL PRESENT, OIL CONSUMPTION WITHIN LIMITS. REMOVED AND REPLACED LT ENGINE IAW SHUTTLE JOB CARD.SDR KCSA11053Engine · surgesNR 4 ENGINE SURGED DURING CONSTANT POWER. ENGINE WAS SHUT DOWN. ENGINE WAS SURGING AT CLIMB THRUST PRIOR TO SHUTDOWN. ENGINE WIND MILLED FOR 40 MINUTES. EGT EXCEEDANCE WARNING 730°. FAILURE OCCURRED AT 0545Z DURING CLIMB. SYSTEM NR 2 IGNITION. ZERO RESTSDR AALA20110916LAX01Engine · malfunctionedLAX INFLIGHT SAN-DFW. CREW REPORTED LEFT ENGINE LOST OIL QUANTITY AND OIL PRESSURE AFTER TAKEOFF. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 23 MINS). EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACEDSDR ALGA20110916001AEngine · faultyNR 2 ENGINE OUT LIGHT FLASHED DURING CRUISE WITH N1 OSCILLATIONS FOR ABOUT 2 SECONDS. DETECTED FAULT CODES WERE 2 DECU A FAULT MINOR - COLL POSITION LVL-1. MX REPLACED FAULTY COLLECTIVE TRANSDUCER. OPS CHECKED GOOD.SDR CA110928008Engine · making metal(CAN) AFTER T/O, CLIMBING AND PASSING FL90, THE PILOT NOTICED A LOW OIL PRESSURE INDICATOR ON AND CAS MESSAGE. HE ELECTED TO SHUT THE ENGINE DOWN. AN UNEVENTFUL SINGLE ENGINE LANDING WAS THEN MADE AT THE POINT OF DEPARTURE. POST FLIGHT INSPECTION REVEALED NOSDR UALA2011091504986Engine · malfunctionedCREW REPORTS DURING TAXI AFTER NORMAL CROSSBLEED START, CABIN CREW AND TOWER REPORTED SMOKE AND FLAMES FROM NR 2 ENG. JUST PRIOR TO REPORTS, HAD RT ELEC HYD PUMP, RT CTR FUEL PUMP AND RT GEN EICAS MESSAGES. CREW ACP'D QRC AND EVACUATED ACFT. ENG WAS AT STABSDR NSVA2011189Engine · smokeGRAY SMOKE FROM RT ENGINE TAIL PIPE. MX INSPECTED RT ENGINE, DRAINED EPA CAN AND PERFORMED RUNS COULD NOT DUP.SDR C2XA11TY142Engine · overtempGSP - ENG 2 COMMANDED SHUTDOWN DUE TO HIGH ITT. REMOVED AND REPLACED NR 2 ENG OPS CHECK GOOD.SDR CA110928006Engine · power loss(CAN) DURING LEVEL CRUISE FLIGHT AT FL370, THE RT ENGINE POWER ROLLED BACK AND SHUTDOWN. IT WAS NOT SUDDEN, AND THE TIMING WAS SIMILAR TO A NORMAL SHUTDOWN. THE PILOT DID NOT NOTICE ANY VIBRATIONS OR NOISE. THERE WERE NO CAS MESSAGES BEFORE THE SHUTDOWN. TSDR CA110928005Oil System · low pressure(CAN) 10 MINUTES INTO THE FLIGHT, A LOSS OF OIL PRESSURE OCCURRED AND THE ENGINE WAS SHUTDOWN. AN UNEVENTFUL EMERGENCY LANDING WAS PERFORMED. POST FLIGHT INSPECTION FOUND NO OIL ON THE SIGHT GLASS. OIL WAS ADDED AND A SUBSEQUENT GROUND RUN FOUND SOME NOISE ISDR CA110915001Bearing Race · damaged(CAN) AFTER LEVELING OFF, THE PILOT GOT AN ENGINE CHIP LIGHT ON THE RT ENGINE, ALL OTHER ENGINE INDICATIONS WERE NORMAL SO THE PILOT PROCEEDED TO NEAREST BASE FOR MX TO HAVE A LOOK AT IT. MX PULLED THE CHIP DETECTOR OUT AND THERE WAS EVIDENCE OF SOME METAL ONSDR C2XA11CL205Engine · malfunctionedGSP FLT 2243 THE CREW REPORTED A COMMANDED NR 2 ENGINE SHUTDOWN DUE TO HIGH ITT. THE AIRCRAFT RETURNED TO GSP AND LANDED WITHOUT FURTHER INCIDENT. SUPPLEMENT TO FOLLOW.SDR 2011F00201Engine · making metalDURING ENGINE MINOR INSP, SENT OIL FILTER TO LAB FOR ROUTINE ANALYSIS, LAB REPORTED METAL IN OIL. CONTACTED MFG FOR EVALUATION, MFG INSTRUCTED TO INSTALL NEW OIL AND FILTER, PERFORM GROUND RUN FOR 1 HOUR, AND SEND FILTER OUT FOR REPEAT ANALYSIS. SECOND ANALYSSDR CA110928002Engine · power loss(CAN) ON A DELIVERY FLIGHT, WHILE AT CRUISE, THE ENGINE LOST POWER WITH TORQUE DROPPING TO APPROXIMATELY 200 FT-LB. AS HE WAS GETTING NO RESPONSE FROM THROTTLE MOVEMENTS, THE PILOT RECOVERED POWER BY THE USE OF THE EMERGENCY POWER LEVER. THE FLIGHT WAS DIVERTSDR CA110921008Engine · making metal(CAN) RT CHIP DETECTOR LIGHT ILLUMINATED AFTER TAKEOFF. CREW IMMEDIATELY ENTERED CIRCUIT AND RETURNED TO POINT OF ORIGIN AND LANDED. RGB CHIP PLUG WAS REMOVED. CONFIRMED METAL CONTAMINATION. FERROUS FLAKES ABOUT 2-4MM-SQUARE. RGB FINGER SCREEN REMOVED. NOSDR CA110914004Engine · power loss(CAN) DURING REVENUE FLIGHT, CREW REPORTED LT ENGINE WAS AT 87 PERCENT N1 AND THEY WERE NOT ABLE TO MODULATE THRUST. CREW ELECTED TO SHUTDOWN ENGINE AND WERE UNSUCCESSFUL AT RE-STARTING THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. TROUBLESHSDR IXXA110060OEngine · slowREJECTED TAKEOFF DUE TO ASSYMETRICAL THRUST ON TAKEOFF ROLL. THE NR 4 ENGINE SLOW TO ACCELERATE, DID NOT REACH MAX POWER. THE CREW RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PREFORMED ACCELERATION CHECK, OPS CHECKED GOOD IAW ERH 72.01.1. PREFORMED REJESDR FDEA201109103817Engine · overtempNR 3 ENGINE OVERTEMP. R & R NR 3 ENGINE IAW WORKCARD 70T0001-03,70T003-03 AND 70T0301-03, OPS CHECKED GOOD.
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