JASC 7200
Service difficulty reports · 14,730
Reports filed under 7200 · Engine (Turbine/Turboprop), newest first.
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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 CA061106003Engine · shutdown(CAN) THE ENGINE WAS REPORTED TO HAVE EXPERIENCED THREE INCIDNETS OF TORQUE FLUCTUATION RESULTING IN EITHER PROPELLER FEATHERING OR IN-FLIGHT SHUT-DOWN BETWEEN OCTOBER 15TH AND 17TH. THE ENGINE FUEL SYSTEM COMPONENTS WERE SUBSEQUENTLY REMOVED FOR INVESTIGATIOSDR SWIA200617352Engine · vibrationLT N2 CORE VIB AT 26,500 IN ICING CONDITION. SHUTDOWN LT ENGINE, DIVERTED TO BOI. RAN ENGINES IAW 72-00-00 AND VIBES STAYED NEAR .2 TO .3 MILS. WITHIN LIMITS OF MM.SDR ASMF200610008Engine · making metalAIRCRAFT RETURNED, DUE TO LOW OIL PRESSURE ON LT ENGINE. CAPTAIN REPORTED THAT DURING DESCENT THE TEMPERATURE REACHED 630 DEGREE (C) AND VIBRATION WAS PRESENT, LT ENGINE WAS SHUTDOWN. DURING MAINTENANCE CHECK, METALLIC CHIPS WERE DETECTED ON ENGINE CHIP DETECTSDR DL76L060853Flange · crackedFOUND CRACKED R FLANGE ON NR 2 ENG OUT OF M/M LIMITS. REPLACED NR 2 ENG PER TRANS 1T149.SDR WRNA200600035Engine · unserviceableDURING CLIMB-OUT OF MIA AT APPROX 18,000 FEET, THERE WAS A LOUD BANG FROM NR 3 ENGINE WITH A SPIKE IN EGT TO 780C AND FLUCTUATING EPR. ENGINE WAS SHUT DOWN, 19,000 POUNDS OF FUEL WERE DUMPED AND AIRCRAFT RETURNED TO MIA AND MADE A SAFE LANDING. VISUAL INSPECSDR KPVA200621Engine · smokeSMOKE IN COCKPIT AND CABIN IN FLIGHT. (MX) MAINT DETERMINED THE CAUSE WAS FROM ENGINE BLEEDS AND AUTHORIZED A FERRY FLIGHT WITH BLEEDS OFF, BACK FOR MAINTENANCE. THE FINDINGS WERE THAT THE SMOKE/FUMES WAS FROM THE NR 2 ENGINE. MAINT REPLACED THE NR 2 ENGINE.SDR ANCF200600036Engine · flamed outLT ENG SHUTDOWN, RESTARTING NOT ATTEMPTED DUE TO HIGH EGT (652 DEGREES) HIGH VIBRATION AND NO OIL PRESS, AIRPLANE WAS ON CRZ AT 36000 WITH SPEED MACH 0.79. NO APPARENT REASON FOR FLAMEOUT. WAS PERFORMED VISUAL AND BOROSCOPE INSPECTION AND CHECK, THE DIGITAL FSDR NSVA200600172Engine · surgesDURING TAKEOFF LEFT ENGINE SURGES. PERFORMED ENGINE RUNS AT T/O POWER IAW 71-00-00, NO DEFECTS NOTED AT THIS TIME.SDR UPS06548203Engine · vibrationAT FL370 HAD IND OF HI N1 VIBRATION ON NR 1 ENG 2.6 VIB IND. DESCENDED TO FL260. IND'S WERE IN NORMAL RANGE AT THIS ALT DIVERSION WAS DETERMINED TO BE BEST COURSE OF ACTION.SDR CA061016003Clamp · cracked(CAN) ENGINE CONTROL CLAMP FOUND CRACKED ON ENGINE INSPECTION. REFERENCE AIRCRAFT IPC 71-00-02 FIG 15, ITEM NR 6 THE PART WAS NOT IDENTIFIED BY A SPECIFIC PN MARKED ON THE CLAMP. SUSPECT POSSIBLE UNAPPROVED PART PREVIOUSLY INSTALLED. (TC NR 20061016003)SDR CA061103009Engine · failed(CAN) ON TAKEOFF ENGINE POWER REDUCED UNCOMMANDED FOLLOWED BY SMOKE IN THE CABIN AIR. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION FOUND THE PROPELLER SEIZED AND METAL DEBRIS IN THE ENGINE CASES. MSDR AMTA200600597Engine · malfunctionedON TAKEOFF EGT RAPIDLY ROSE BEYOND 855C HAD TO REDUCE POWER TO STAY WITHIN LIMITS ON CLIMB-OUT. CLIMB 2 SELECTED EGT 810C, N3 997 PERCENT COULD NOT HOLD MAX CONTINUOUS OR CLIMB POWER. (M)SDR MAC100602Seal · deterioratedCCAS ENGINE 2 OIL AND LOW ENGINE OIL PRESSURE DETECTED ON NR 2 ENGINE.SDR UPS06548178Engine · stalledAIR TURN BACK, LT ENG. EXPERIENCED APPROX. 5 COMPRESSOR STALLS IN APPROX 5 SECONDS. PASSING 1,300 FT. SHORTLY AFTER SELECTING V-NAV S SWITCHING FROM T/O TO CLB THRUST. EGT OVERTEMPED (RED) WENT TO 907 PEAK TEMP. ENGINE STABILIZED AND OPERATED NORMALLY WITH THRSDR CA061002001Bolt · wrong part(CAN) NON APPROVED AS21040 BOLT WAS FOUND. BOLT HEAD WAS MACHINED TO ADD PN AS21040. BOLT END ALSO MACHINED WITH A CENTER HOLE, THREAD LENGTH SHORTER AND DIAMETER OF BOLT IS UNDERSIZE. BOLT LOCATIONS ON ENGINE; CLIPPING POINT FOR P3 AIR TUBE TO FFR UNION P3 LSDR HALA0600782Fairing · missingNR 2 ENG INTERMEDIATE CASE STRUT FAIRING AT 6:30 POSITION IS MISSING. NR 2 ENG I/B BLOCKER DOOR AT 8:00 POSITION DAMAGED (REMOVED AND PLACED IN W/B). NR 2 ENG I/B REVERSER COWL DAMAGE JUST FWD OF ATTACH LINK FITTING AT 7:00 POSITION (3" LONG, 3/8" WIDE, 1/2"SDR 06FDEA03542Engine · bird ingestionON ROTATION SUSPECT BIRD STRIKE, MODERATE ENGINE VIBRATION EVM COMP 5.0 CARRIED-OUT BIRDSTRIKE INSPECTION CHECK PER MM 5-52-01-6 1 - SATISFACTORY; THIS ENGINE WAS APPROVED FOR REPLACEMENT. REPLACED THE NR 1 ENGINE AND NOSE COWL.SDR TRBA2006077Eec · surgesEN ROUTE AT 5,000 MSL, NR 2 ENGINE EXPERIENCED LARGE POWER SURGES. RT TQ WAS BETWEEN 50-102.5 PERCENT ON DIGITAL INDICATOR. POWER WAS REDUCED BELOW THE `NOTCH` AND ENGINE STABILIZED AND RAN NORMAL WITH NO FURTHER PROBLEMS. SWAP EEC`S FROM LT TO RT ENGINE FOSDR DXTA200601623Engine · making metalON TAKEOFF ROLL, RT OIL FILTER BYPASS ANNUNCIATOR ILLUMINATED. OIL TEMP AND PRESS INDICATIONS NORMAL. ABORTED TAKEOFF JUST AFTER TAKEOFF ROLL STARTED. REMOVED NR 2 ENGINE, INSTALLED REPAIRED ENGINE IAW MM 71-00-00. PERFORMED GROUND OPERATIONAL CHECKS AND LEASDR UPS06548170Engine · stalledLEFT ENGINE ON T/O STALLED AND EGT LIMIT WENT TO AROUND 855C FOR 7 SECS. ATB WAS ACCOMPLISHED. ACCOMPLISHED ALL STEPS OF POWERPLANT INSP AFTER A SURGE PER MM 71- 32-00/101 FIG 103. REMOVED AND REPLACED BVCU REF LP 532320, I2 AND TPCU REF LP 542316, I2. ACCSDR QXEA200602619Engine · smokePDX FLIGHT NR 2231, OBSERVED LARGE PLUME OF BLUE SMOKE FROM THE TAILPIPE OF NR 2 ENGINE WHEN SELECTING NR 2 CONDITION LEVER TO FUEL OFF AFTER 30 SECOND COOL DOWN. ALL ENGINE INDICATIONS NORMAL. MAINTENANCE REPLACED NR 2 ENGINE IAW TASK CARDS 9710003 AND 9710SDR UPS06M48169Engine · inoperativeAT 1500 FT ON FINAL, NR 1 ENG ROLLED BACK TO EPR=.8, N1=14.1; EGT-512 N2 14.0 FF BELOW 1000 LBS. ENGINE 1 RPM LO =LEVEL 2 ALERT ILLUMINATED. NO RESPONSE ON THROTTLE MOVEMENT. CONTINUED APPROACH. ON LANDING, ROLLOUT WHEN NR 1 BROUGHT BACK. DRAINED FUEL FORSDR IXXA060603OEngine · flamed outDURING CLIMBOUT FROM RJTY AT FL390 NUMBER THREE ENGINE FLAMED OUT. THE CREW DESCENDED TO FL320 WITH IGNITERS IN BOTH AND OVERRIDE IN ALL ENGINES. APPROXIMATELY AT FL340 THE ENGINE RESTARTED, ALL INDICATIONS RETURNED TO NORMAL AND THE CREW CONTINUED THE FLIGHSDR CA061103003Engine · overheated(CAN) DURING TAXI FOLLOWING LANDING THE ENGINE EXPERIENCED AN ITT OVER-TEMPERATURE. SUBSEQUENT INSPECTION REVEALED DEBRIS IN THE EXHAUST AND HEAT DISCOLORATION OF THE AIRCRAFT COWLING IN THE EXHAUST REGION. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOSDR CA061011003Controller · defective(CAN) DURING A FLIGHT, THERE WAS A LOSS OF LT ENGINE OIL PRESSURE. THE AFFECTED ENGINE WAS SHUTDOWN AND AN UNSCHEDULED LANDING ACCOMPLISHED. AFTER INVESTIGATION, THE DENSITY CONTROLLER WAS FOUND DEFECTIVE. THE SEAL WAS RUPTURED ON THE (INTAKE) SIDE AND OIL WASSDR CA061006018Engine · fire(CAN) ON TAXI FOLLOWING LANDING, FLAMES WERE SEEN COMING FROM THE ENGINE EXHAUST. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20061006018)SDR KNK2006F00009Manifold · cokedENGINE HARD TO ROTATE AT START DUE TO FUEL COKING IN THE INJECTION MANIFOLD LABYRINTH AREA. (K)SDR CA061006020Engine · seized(CAN) ENGINE OIL TEMPERATURE WAS SEEN TO INCREASE IN FLIGHT ACCOMPANIED BY A LOSS OF OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED OIL IN THE ENGINE DRAINS AND SEIZURE OF THE POWER SECTION. MFG WILL INVESTIGATE THE EVENT ANSDR 2006UALA01850Engine · vibrationHIGH N2 VIBRATION ON NR 2 ENGINE. ONE HPT STAGE-2 BLADE HAD CORDWISE AIRFOIL FRACTURE AT THE MID-SPAN. THIS WAS THE RESULT OF INTERNAL SULFIDATION THAT CHOKES-OFF COOLING AIR FLOW WITHIN THE BLADE AIRFOIL. THIS RESULTS IN OVERHEATING OF THE PARENT MATERIAL SDR QXEA200602594Fan Blade · vibrationTUL- RIGHT ENGINE FAN VIBRATION 2.1. REDUCED THRUST PER THE CHECKLIST, VIBRATION MONITOR MOVED INTO GREEN ARC. ALL OTHER INDICATIONS NORMAL. MAINTENANCE REPLACED THE FAN BLADES PER MTC R722101. OPERATIONAL CHECKS GOOD, VIBRATIONS ARE NOTED AT 0.3. AIRCRAFTSDR CHQA200600126Engine · inoperativeFLIGHT 3007-CMH-CLT - A FEW MOMENTS AFTER TAKEOFF, DURING CLIMB FROM CMH, LAVATORY SMOKE DETECTOR WENT OFF. THIN LAYER OF SMOKE AND SMELL OF SMOKE IN TOP OF CABIN. DECIDED TO RETURN TO AIRPORT. DURING DESCENT, THE SMOKE CLEARED AND LAVATORY SMOKE DETECTOR SSDR HAEA200600194Engine · flamed outRT ENGINE FLAMED OUT ON DESCENT INTO YIP. PILOT REPORTED THAT THE RT ENGINE THROTTLE WAS RETARDED TO LOWER THAN NORMAL IDLE. ENGINE RELIGHT WAS ACCOMPLISHED. AIRCRAFT CONTINUED DESCENT INTO YIP LANDING NORMAL. MAINTENANCE PERFORMED PROCEDURES CONTAINED IN SDR DL757060767Engine · malfunctionedON T/O ROLL RT ENG OIL PRESS LIGHT FLICKERED FOLLOWED BY OIL QTY DROPPING TO 3 AND RT ENG OIL PRESS LIGHT ILLUMINATED, ABORTED T/O AT 90-100 KTS/ T/S OIL PRESS SYSTEM REPLACED RT ENG MAIN OIL PRESS T.X. AS PRECAUTION. OPS CHECKS AND LEAK CHECK GOOD. DRAINED NSDR DLM8K060764Engine · malfunctionedDURING APPROACH INTO LGA 5000 FT SLOWING TO 170 KTS FLAPS 15THE NR 2 ENGINE RACED TO MAX EGT NEAR 660C, N1 OVER 102 PERCENT ALL PARAMETERS EXCEEDED. SHUTDOWN RT ENGINE. DID NOT PULL FIRE HANDLE. NORMAL SHUTDOWN AND DECLARED EMERGENCY. REPLACED NR 2 ENG IAW RSDR 0925200603Compressor · stalledDURING TO ROLL (SKBO), APPROX. 125 KTS., NR 4 ENGINE COMPRESSOR STALLED - ABORTED TO, RETURN TO GATE. FINDINGS - CORRECTIVE ACTIONS - TBD.SDR CA061006014Blade · damaged(CAN) ON CLIMB, THE ENGINE EMITTED A LOUD NOISE AND FLAMED OUT. SUBSEQUENT INSPECTION REVEALED HPT1 BLADE DAMAGE. P&WC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20061006014)SDR KNK2006F00008Manifold · cokedENGINE HARD TO ROTATE FOR START DUE TO FUEL COKING IT. THE INJECTION MANIFOLD LABYRINTH SEAL. (K)SDR 2006FA0000929Engine · making metalENGINE CHIP LIGHT CAME ON APPROACH TO LANDING. REMOVED GAS GENERATOR MAG PLUG FOUND COVERED WITH METAL CHIPS. PROBABLE CAUSE BEARING FAILURE.SDR 2006FA0000928Engine · making metalENGINE CHIP LIGHT CAME ON APPROACH TO LANDING. REMOVED GAS GENERATOR MAG PLUG FOUND COVERED WITH METAL CHIPS. PROBABLE CAUSE BEARING FAILURE.SDR 2006F00040Engine · fireENGINE SURGE WITH FLAMES OUT OF THE EXHAUST DURING FINAL APPROACH TO LAND.SDR DXTA200601605Engine · shutdownRIGHT ENGINE SHUT DOWN WHEN DOING THE SPEEDBRAKE CHECK. - PERFORMED ENGINE GROUND RUN, EXTENDED SPEED BRAKES SEVERAL TIMES WITH NO DEFECTS TO ENGINES. PERFORMED RAPID DECELERATION OF THE THROTTLES WITH NO DEFECTS ON ENGINES. CYCLED T/R, MOVED FLAPS AND CYCLESDR 06FDEA03336Engine · malfunctionedON TAKEOFF ROLL, WHEN SETTING TAKEOFF POWER (STANDARD EPR) NR 1 THRUST LEVER WAS 4 INCHES BEHIND OTHER TWO WITH TAKE OFF POWER SET. REJECTED TAKEOFF MAX SPEED ON TAKEOFF ROLL PRIOR TO REJECT 100KTS INDICATED AIRSPEED. R&R NR 1 FUEL PUMP AND ENGINE FUEL CONTRSDR CA060928002Engine · vibration(CAN) T/O REJECTED AT APPROX 110 KTS DUE SERIOUS VIBRATIONS (SUSPECT RT MAIN GEAR). AUTO BRAKE USED MAX BRAKE TEMP IND 480 DEG FOR NR 2, OTHERS WERE 450-480. ON STARTING NR 2 ENGINE, FELT HIGH VIBRATION AND HIGH EGT, ABORTED ENGINE START. WHEN TURNING NR 2 FASDR CA060919001Shutoff Valve · leaking(CAN) DEPARTING THE CREW OBSERVED A STRUT OVERHEAT CONDITION ON NR 3 ENGINE. THE AIRCRAFT DIVERTED WHERE MAINTENANCE DETECTED A LEAK AT THE WING ANTI ICE SHUT-OFF VALVE (SOV). GASKETS WERE REPLACED AND NO FURTHER FAULT APPEARED EVIDENT AT GROUND RUN. DURING THSDR HALA0600728Engine · malfunctionedATB: ENGINE FAILURE ON CLIMB-OUT DUE TO HIGH EGT OF 1135. N1 AND N2 STILL SPINNING AT IDLE RPM. ENGINE SHUTDOWN BY ITSELF FOLLOWED BY MANUAL EMERGENCY PROCEDURE. FOUND METAL PIECE IN NR 1 ENG EXHAUST. REMOVED NR 1 ENG PER HALM144-717 9/15/06. INSTALLED NRSDR 2006UALA01771Engine · shutdownCREW REPORTED NR 1 ENGINE AUTO SHUT DOWN ON APPROACH. POST FLIGHT SHOWS FUEL CTL FAULT. PERFORMED TROUBLE SHOOTING. DID NOT FIND FAULT CODE. FOUND CHANNEL (A) CANNON PLUG TO FMU, LOOSE NOT COMPLETELY INSERTED INTO CONNECTOR. REPLACED FMU. ACCOMPLISHED POSDR SA06072Engine · shutdownFLT1408 - DURING CRUISE, EN ROUTE FROM SFO TO CLT, CREW RECEIVED ECAM MESSAGE "ENG 2 HI TEMP FADEC OVHT" AND "ENG 2 FADEC B FAULT" ALONG WITH OTHER ASSOCIATED FAULT MESSAGES. CIRCUIT BREAKER FOR ENG 2 FADEC TRIPPED, AND MOMENTS LATER, THE NR 2 ENGINE AUTOMATISDR UPS06447985Engine · shutdownNR 3 ENG SHUT DOWN DUE TO AN OIL FILTER BYPASS LIGHT AND SPIKE IN OIL TEMP. AN EMERGENCY WAS DECLARED. REMOVED OIL FILTER DIFFERENTAIL PRESSURE SWITCH ON NR 3 ENGINE PER B747 MM 79-35-01. THIS CLEARS M333490. ENGINE RUN & LEAK CHECK COMPLIED WITH. CLOSING LPSDR NSVA200600140Engine · failedAT APPROXIMATELY 100 FT AGL, LT ENGINE TEMP WENT TO 1170 DEGREES WITH ASSOCIATED "LOUD BANG" AND L ENGINE OIL PRESSURE LIGHT. DECLARED EMERGENCY RAN CHECK LIST, SHUT DOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW 71-00-00-04 SN ON GE-E-785342, SN OFF GE-ESDR 06FDEA03265Engine · smokeON CLIMBOUT DEPARTURE CONTROL INFORMED US THAT TOWER SAID WE WERE EMITTING BLACK SMOKE OUT OF NR 1 ENGINE. ALL ENGINE PARAMETERS INDICATED NORMAL. ELECTED TO MAKE A PRECAUTIONARY LANDING. PER CREW DEBRIEF- CAPT REPORTED ALL NORMAL INDICATIONS, ON INBND LEG
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