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 F3LA2012020700705Engine · making metalABORTED TAKEOFF. UNUSUAL VIBRATION NOTED ON START OF NR 2 ENGINE DURING TAXI. NO ECAMS NOTED. ON APPLICATION OF TAKE OFF THRUST, A LOUD COMPRESSOR STALL, FLAMES NOTED BY TOWER FROM ENGINE REAR. ECAM FOR NR 2 OIL FILTER CLOGGED. IMMEDIATELY SECURED NR 2 ENSDR UALA2012020200635Engine · failedRETURN TO GATE DUE TO NR 1 ENGINE WON'T START IN AUTO AND MANUALLY. AIR START VALVE MR80102 OFF:43, ON: 1. DUE TO MIS FOUND ON MASTER CHIP DETECTOR AND MAIN GEARBOX CHIP DETECTOR, REPLACE NR 1 ENGINE ESN 777019. ENGINE REPLACED.SDR USAA2012020100012Bolt · looseCLT FLT 885 EN ROUTE CLT TO CUN. LEFT ENGINE LO OIL PRESS LIGHT. LEFT ENGINE OIL QUANTITY 0. COMPLIED WITH QRH PROCEDURE TO SHUT DOWN LEFT ENGINE. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. ALL ENGSDR CA120130005Engine · vibration(CAN) 10 MINUTES BEFORE "TOP OF DESCENT" ENGINE VIBRATION FROM THE RT ENGINE AND COMPRESSOR STALL. CREW REDUCED POWER AND CONTINUED DESCENT. AT 3000 FT AND IDLE POWER THEY AGAIN FELT VIBRATION ON RT WHEN THEY TRIED TO INCREASE POWER BY 5 PERCENT. CONTINUED THSDR CA120130001Engine · malfunctioned(CAN) DURING CLIMB, PASSING FL 50, A LOUD NOISE WAS HEARD WITH NR 2 FADEC FAIL WARNING. THE CREW SECURED THE ENGINE AND RETURNED TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING TOO PLACE. THE ENGINE WILL BE REPLACED, NO DETAILS ON ENGINE COSDR UALA2012012600548Engine · surgesNR 2 ENG SURGE DURING T/O. ABORTED T/O AT 40KTS. RPLC NR 2 ENG SN 717690 DUE ENGINE SURGE, RESULTING IN ABORTED TAKEOFF & RECENT PARAMETER SHIFT. RMV'D NR 2 ENG SN 717690. INSTALLED ENG 727968.SDR UALA2012013000591Engine · contaminatedLARGE OIL LEAK ON ENG 2 SAMC TEXT: IDENTIFY FLUID TYPE & LEAK SOURCE. ACP CHECK OF THE ENGINE. FOUND NO LEAK SOURCE. CHECKED OIL AT TANK, TANK IS FULL. COCKPIT INDICATION INDICATES 21 QTS. REVIEW OF PLN OIL SHOWS OIL USE AT 0.07 QTS PER HR (WELL WITHIN LISDR CA120125001Engine · surges(CAN) ON FINAL APPROACH, CAPTAIN AND F/O OBSERVED THAT THE RIGHT HAND ENGINE WAS NOT RESPONDING PROPERLY TO THROTTLE INPUTS. EGT LIMITS EXCEEDED. ENGINE SURGING WAS NOTED AND PASSENGER REPORTED HAVING OBSERVED TORCHING.SDR CA120124005Engine · shutdown(CAN) DURING PUSHBACK BOTH ENGINES STARTED NORMALLY, NR 1 ENGINE SHUTDOWN WITHOUT WARNING.SDR ASOA20120123007Engine · leakingTHE CREW REPORTED SMOKE IN THE CABIN AFTER TAKEOFF AFTER PACK WAS WAS SELECTED. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 2 ENGINE. OPS CHECKED GOOD.SDR DALA1203189004Engine · malfunctionedFLIGHT DIVERTED DUE TO THE RIGHT ENGINE NEEDING TO BE SHUT DOWN FOLLOWING COMPRESSOR STALL WITH LOSS OF OIL QUANTITY. UPON ARRIVAL, MAINTENANCE FOUND 4TH STAGE TURBINE DAMAGE, THRUST REVERSER DAMAGE, AND OIL IN THE TAIL PIPE. THE ENGINE WAS REPLACED.SDR HNAA2012012300494Unknown · failedDURING CRUISE, NR 2 ENGINE TORQUE REDUCED TO 30 TO 50 PERCENT WITH NOTICEABLE POWER LOSS. ALSO 7 TO 10 PERCENT POWER LOSS DURING APPROACH. NO CAUTION OR WARNING LIGHTS ILLUMINATED. R & R NR 2 EEC IAW PM MM72-01-10. GROUND RAN ACFT, COULD NOT DUPLICATE DISCRESDR CA120213009Engine · power loss(CAN) DURING CLIMB, THE ACFT LOSS ENGINE POWER AND THE PILOT MADE A FORCED LANDING INTO A FIELD. THE ACFT SUSTAINED SUBSTANTIAL DAMAGE. NO INVESTIGATION WAS REPORTEDLY UNDERTAKEN BY THE ATSB.SDR YYFA2012F00039Acoustic Liner · delaminatedON TAKE OFF ADVANCEMENT OF THROTTLE TO 1.4 EPR, AUTO THROTTLE ON, ADVANCED THROTTLE TO TAKE OFF POWER RT ENGINE SURGED -600+ EGT- FLUCTUATIONS CONTINUED-ABORTED TAKE OFF. F/A'S REPORTED STRONG BURNING ODOR. MX ACCOMPLISHED AN ENGINE INSPECTION AND FOUND NR SDR SWIA201229400Engine · failedAT TAKEOFF ROTATION RIGHT ENGINE N1 DROPPED TO 79.37. LEFT ENGINE APR FIRED FOR APPROXIMATELY 5 SECONDS. SHORTLY AFTER TAKEOFF ALL ENGINE INDICATIONS RETURNED TO NORMAL. RIGHT ENGINE OIL LOW PRESSURE STATUS MESSAGE ALSO APPEARED SHORTLY THEN WENT AWAY. (FLSDR ZZDA2012098Case · crackedLEFT ENGINE CASE FLANGE B, CRACKED. ACCOMPLISHED CASE FLANGE B FLANGE REPAIR PER EA 37-72-03696IR/CFM SB 72-0580R2.SDR HALA2012011900045Engine · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT ENGINE STARTED NORMALLY TILL 50 PERCENT, THEN REMAINED AT 50 PERCENT FOR 50 SECOUNDS BEFORE SLOWLY ACCELERATING - TOTAL TIME FROM FUEL ON TILL ENGINE STABLE TOOK 110 SECONDS, PEAK TEMP EGT WAS 397. TROUBLESHOT IAW FIM 73-21-00/SDR UALA2012011800380Engine · smokeWHITE SMOKE COMING FROM RT ENGINE EXHAUST DURING TAXI IN AFTER ENGINE SHUTDOWN REPORTED BY ANOTHER ACFT. AS PRECAUTION CREW CALLED FIRE SERVICES. INBOUND CREW DID NOT OBSERVE ANY ABNORMAL FLIGHT DECK INDICATION. CKD INLET AND EXHAUST NO DISCREPANCIES. MAT SSDR UALA2012011800374Engine · wornNR 1 ENG BULB SEAL BOLTS BETWEEN EXHAUST NOZZLE TO PYLON REQUIRE REPAIR, WEAR ON GATOR BACKS. A/C IS GOOD TO GO. CHANGE ENGINE BEFORE MAX LIMIT, ACCT TIME, CHANGE ENGINE 222162-PW POS 001. *REPLACED NR 1 ENG.SDR UALA2012011600354Engine · faultyDUE TO CHRONIC OIL HIDING AND OIL TEMP RISING WITH OIL PRESSURE DECREASING REPLACE NR 1 ENGINE. REPLACE NR 1 ENGINE. INSTALL ESN 222027. REPLACED NR 1 ENG PER MMOV. INSTALLED ESN 222027.SDR MYWA120004Engine · hung startETOPS SIGNIFICANT SYSTEM: INFO: NR 1 ENG HUNG START CROSS BLEED SECOND ATTEMPT OK. PERFORMED 2 SUCCESSFUL ENGINE START WITH APU AS PER AMM 71-0-00 NO HUNG START WAS NOTED STARTING OPERATION ARE WITHIN LIMITS 1ST AT 70 SECONDS 2ND AT 60 AS PER AMM 71-00-00 PASDR SWAA201201130267Unknown · faultyINFLIGHT SHUT DOWN AND AIR TURNBACK WITH DECLARED EMERGENCY. ON DEPARTURE NR 1 ENGINE EXHAUST WAS DARKER. NR 1 EGT WAS APPROXIMATELY 50 DEG ABOVE NR 2 F FLOW WAS SLIGHTLY HIGHER. ABOVE 10,000FT NR 1 BLEED TRIP OFF CAME ON RAN CHECK LIST, WOULD NOT GO OUT. SDR REXA201200114Engine · vibrationAIR RETURN AT 10,000 FEET AIRCRAFT STARTED SMALL VIBRATION, UNUSUAL SOUND FROM RIGHT SIDE OF AC, RIGHT ENGINE ITT WAS POINTING TO 12 O`CLOCK, RAN QRH, SHUTDOWN ENGINE, RETURNED TO DTW. REMOVED AND REPLACED RT ENGINE IAW AMM 71-00-00. REFERENCE DISC NR 1 AML SDR QMLA2012011212004Module · defectiveDURING ROUTINE ENGINE INSPECTION OF THE MAGNETIC CHIP DETECTORS, THE OIL CHECK VALVE FOR THE MAGENETIC CHIP DETECTOR FOR THE M05 MODULE WOULD NOT CLOSE. REMOVED THE HSG ASSY AND FOUND A METAL TAB STUCK TO THE CHIP DETECTOR. THIS ACFT IS CURRENTLY OUT OF SERVSDR CA120118007Engine · vibration(CAN) IFSD AND AIR TURNBACK. ACFT WAS AT 11,000 FT WHEN RT ENGINE VIBRATION LEVEL INCREASED THEN ITT WENT TO 1100.SDR HALA2012011100015Clamp · brokenETOPS SIGNIFICANT SYS - ON EXTERNAL INSPECTION OF NR 1 ENGINE, FOUND TWO TCC SUPPORT BRACKET CLAMPS BROKEN. REPLACED TCC SUPPORT BRACKET CLAMPS AT 3 O'CLOCK POSITION. OK FOR SERVICE.SDR UALA2012011000222Plug · unknownNR 2 ENGINE DRIVE PAD & BOROSCOPE PLUGS REMOVED. PLUGS AT 1, 5, AND 10 O`CLOCK POSITIONS. REPLACED BOROSCOPE PLUGS AND DRIVE PAD.SDR CA120116007Engine · contaminated(CAN) THE CREW REPORTED FUMES IN THE COCKPIT. AN EMERGENCY WAS DECLARED, THE FLIGHT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. THE ODOR WAS ATTRIBUTED TO INGESTION OF ANTI-ICING FLUID THAT HAD BEEN APPLIED PRIOR TO THE DEPARTURE.SDR USAA2012011100010Engine · malfunctionedDURING DESCENT, ALL THREE FLIGHT ATTENDANTS REPORTED A "DIRTY SOCKS" SMELL TO BE VERY STRONG IN CABIN. UPON THEIR REQUEST, PASSENGER O2 MASKS WERE DROPPED. FLIGHT ATTENDANTS ALSO WENT ON O2. APU BLEED AIR SWITCH WAS OFF. FLIGHT LANDED AT CLT WITHOUT FURTHESDR SIMA201201106Engine · failedON FLIGHT 3560 THE CREW REPORTED AT FLIGHT LEVEL 370 RECEIVED E1 OIL IMP BYPASS MESSAGE WITH ENGINE 1 OIL LOW PRESS WARNING. OIL QUANTITY DROPPED TO 3 QUARTS AND GOT SMOKE IN COCKPIT. CREW SHUT DOWN ENGINE 1 AND SMOKE CLEARED. THE CREW DELCARED AN EMERGENCYSDR LR7A2012020200352Housing · wornDURING DESCENT NR 1 ENGINE RPM LOSS FOLLOWED BY FLAMEOUT. SHUTDOWN ENGINE. REPLACED NR 1 VALVE HOUSING IAW LAC HN 61135, LP 35212.SDR UALA2012010600140Engine · overtempECM PARAMETER SHIFT HIGH EGT. REPLACED NR 1 ENGINE RAN ENGINE, NO DEFECTS NOTED.SDR UALA2012010300071Blade · damagedCREW REPORT ON T/O ROLL HEARD BANGING SOUND AT V1 FOLLOWED BY ACRID BURNING SMELL IN CABIN THAT LASTED 20 SECONDS. CREW SUSPECT BIRD STRIKE, DEN AIRPORT GND CREW CHECKED AND FOUND DEAD HAWK REMAINS ON RUNWAY. FOUND EVIDENCE OF BIRD STRIKE TO NR 2 ENGINE. ISDR SWIA201229089Unknown · malfunctioned(FLT 4456) DURING CLIMBOUT, CREW REPORTED A SERIES OF LOUD NOISES AND THE AIRCRAFT YAWED LEFT. LEFT ENGINE ITT CLIMBED. CREW PULLED POWER BACK TO IDLE AND RETURNED TO THE FIELD. REMOVED AND REPLACED LEFT ENGINE.SDR CA120104012Vent Line · distorted(CAN) LEFT ENGINE CENTER VENT TUBE REPLACED ON SPV CHECK AND RELEASED FOR SERVICE ON DECEMBER 22, 2011. FLIGHT CREW DISCOVERED CVT DISTORTED ON WALK AROUND.SDR USAA2012010400015Engine · vibrationON TAKEOFF THROUGH CLIMBOUT, CREW NOTICED A STRANGE SOUND. OUT OF APPROXIMATELY 10,000 MCL, VIBRATION INDICATOR ON NR 1 ENGINE CLIMBED STEADILY THROUGH 4.0 TO 5.0 AND EGT CLIMBED TO APPROXIMATELY 910 DEGREE C. BEFORE PULLING BACK ENGINE NR 1. ACCOMPLISHED QSDR UALA2012010300054Engine · malfunctionedNR 1 ENGINE ISSUE. FOUND ON EPDC THAT ENG NR 1 EEC SHOWS POWERED ON EICAS DISPLAY, ALL ENG INDICATIONS ARE ON, ON GROUND FOR LEFT ENG WITHOUT EEC TEST SWITCH ENGAGED. DEPOWERED ACFT. CIRCUT BREAKERS RESET FROM EEC CONTROL. EDIU LT & RT. SWAPPED LT & RT EDIUSSDR CA120115006Engine · malfunctioned(CAN) WHILE ON THE RAMP WITH INTENT TO FLY, WHEN ENGINES WERE STABLE AT IDLE, THE PILOT RECEIVED A NR 2 DC GEN. CAUTION FOLLOWED BY LOSS OF TORQUE, NG AND OIL PRESSURE, SLOWLY DECREASING TO ZERO. TROUBLESHOOTING IS ON-GOING.SDR CA120115005Signal Cond Unit · malfunctioned(CAN) DURING T/O ROLL, AN UNCOMMANDED AUTOFEATHER OCCURRED RESULTING IN AN OVERTORQUE. THE FDR DATA CONFIRMED THE OVERTORQUE AND THE TORQUE SIGNAL CONDITIONER UNIT FAULT INDICATOR WAS TRIGGERED. TROUBLESHOOTING IS ON-GOING.SDR CA120115001Engine · power loss(CAN) WHILE ENROUTE, THE ENGINE LOST POWER AND THE PILOT OF THE FLOATPLANE MADE A FORCED LANDING ON WATER. THERE WERE NO INJURIES AND THE AC WAS NOT DAMAGED. IT WAS TOWED TO SHORE WHERE THE ENGINE WILL BE REPLACED. THE OPERATOR HAS YET TO DECIDE WHERE THE ENSDR USAA2011123000010Engine · failedNR 1 ENGINE SURGED PLUS TO MINUS 3 PERCENT N1 DURING CLIMB TO ALTITUDE. EGT, N2, FF SURGED AS WELL. AUTOTHROTTLES WERE IN USE. THRUST LEVER DID NOT FOLLOW ENGINE SURGE ALSO NR 1 THRUST LEVER 1 KNOB WIDTH PAST NR 2 DURING CLIMB. OK IN CRUISE AND DESCENT. RSDR CA120217006Engine · making metal(CAN) INTERMITTENT CHIP LIGHT ON NR 2 ENGINE. CHIP DETECTOR INSPECTED POST SHUTDOWN. METAL DEBRIS DISCOVERED WAS BEYOND MFG RECOMMENDATION FOR CONTINUED SERVICE. ENGINE REPLACED.SDR UALA2011122707116Engine · hung startHUNG START ON LEFT ENGINE. SECOND START UNSATISFACTORY. 3RD ATTEMPT MADE WITH IGNITION IN BOTH. ENGINE HANGS AT 60% N2 AND WILL NOT ACCELERATE TO IDLE. NO LIMITS EXCEEDED. STARTER CUTOUT WAS NORMAL. REFER TO MM 73-21-00 FIG 111 ON PG125 FOR FAULT ISOLATION. FSDR MALA110297Engine · contaminatedAFTER TAKEOFF, AFT LAVATORY WARNING LIGHT CAME ON AND ENTIRE CREW COULD DETECT SMOKE. PERFORMED CHECKLIST AND RETURNED TO DEPARTURE. FOUND ODOR TO BE COMPRESSOR WASH SOLUTION. PERFORMED PACK RUN IAW AMM 21-00 AND ENGINE RUNS IAW 71-00.SDR NSVA2011360Unknown · malfunctionedFLT 4930 YHZ-EWR A/C 783 / 199Q ABORTED TAKEOFF DUE TO MX (NR 1 ENG TORQUE REACHED 96 PERCENT).SDR TRBA201136101Engine · shutdownTHE NR 1 ENGINE FAILED DURING INITIAL CLIMB AT 5000 FT. NO UNUSUAL NOISES OR SURGES OR FIRE INDICATIONS DURING FAILURE. SECURED ENGINE IAW EPC AOM VOL 1 . DECIDED TO RE-START IAW AOM. ENGINE STARTED NORMALLY. LANDED WITH BOTH ENGINES OPERATIONAL. ENGINE SHSDR CA111227003Oil System · low pressure(CAN) DURING FLIGHT THE OIL PRESSURE ON THE NR 2 ENGINE FLUCTUATED AND THE LOW OIL PRESSURE CAUTION LIGHT CAME ON. THE CREW ELECTED TO SHUTDOWN THE ENGINE AND PERFORMED AN UNEVENTFUL SINGLE ENGINE LANDING. PRELIMINARY INSPECTION REVEALED METALLIC PARTICLES OSDR CA111227002Engine · power loss(CAN) 10 MINUTES INTO CRUISE, THE PILOT REPORTED AN UNCOMMANDED ACCELERATION OF THE ENGINE AND ALL PARAMETERS. TORQUE ESTABLISHED AT 2200 FT LB, NG 108 PERCENT. THE PILOT INCREASED ALTITUDE AND CONTINUED TOWARDS HERVY BAY AIRPORT. ONCE WITHIN SAFE GLIDING RSDR QOCF2012F00034Engine · flamed out(B-16462) NR 2 ENGINE FLAMEOUT DURING LANDING AT SPEED 50 KNOTS WITH FULL REVERSER IN ANC.SDR QMLA2011122311121Engine · contaminatedUPON CLIMBOUT, NOTICED STRANGE ODOR IN CABIN. ENSURED HEAT AND DEMIST OFF AND CIRCLED BACK TO MAKE UNEVENTFUL LANDING. INSPECTION DETERMINED RESIDUAL SOAP FROM ENGINE WASH.
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