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 CA190515015Engine · surges(CAN) R/H ENGINE SURGE AT 200 FT FOR 3 SECONDS AND LOSS OF THRUST. JA BASEL WILL ARRIVE 31/01 TO BEGIN TROUBLESHOOTING. ABORTED TAKE OFF AT 100KTS DUE TO BRAKE #4 STARTED TO DRAG (ANTISKID KICKED IN). TAXIED BACK AND BRAKE WAS SMOKING. NO CAS MESSAGES POSTED.SDR DALA2019051002928Engine · failedRT. ENGINE FAILED DURING CLIMB AT 5000 MSL. (0) OIL PRESSURE, EGT 980 AND RISING. SHUTDOWN NORMAL. REPLACED NUMBER 2 ENGINE ON LOG 1063040. (LP# 5691956)SDR CA190530010Engine · odor(CAN) ODOUR FROM ECS WITH ENGINE POWER CHANGE. #1 ENGINE REPLACED. AIRCRAFT BACK INTO SERVICE. (TC# 20190530010)SDR MASA2019050711844Oil System · low pressureENGINE 2 SHUTDOWN IN FLIGHT- LOW OIL PRESSURE. STILL IN WORK.SDR AALA201905079006Engine · malfunctionedAIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF NUMBER 1 ENGINE OVER TEMPERATURE CONDITION AND COMPRESSOR VANE PROBLEM. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 ENGINE IAW CARD 26L40071001.SDR CA190506004Engine · making metal(CAN) IT WAS REPORTED TO BELL:PILOT WENT TO START THE HELICOPTER AND THE ENGINE 1 CHIP LIGHT ILLUMINATED. PICTURES FROM THE CHIP DETECTOR INDICATE IT IS CONSISTENT WITH OTHER BEARING FAILURES ON THE ARRIUS ENGINES. ++X++ (TC# 20190506004)SDR ASMF2019061309Unknown · vibrationCAPTAIN REPORTED THAT DURING TAKEOFF AND CRUISE, THE LEFT ENGINE VIBRATION REACHED 4.1 UNITS. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED FIM 71-05 TASK 808 PROCEDURE, CHIP DETECTORS AND SCAVENGE SCREENS INSPECTION, BY MISSING OR UNBOUNSDR DALA2019050602866Engine · malfunctionedSHIP 696 OIL QUANTITY REDUCED TO ZERO ASSOCIATED LIGHTS AND MESSAGES APPEARED. CREW PERFORMED DIVERSION DUE TO ABNORMAL LEFT ENGINE PARAMETERS, HIGH VIBRATIONS AND OIL LOSS. CORRECTIVE ACTION: MTC FOUND METAL ON MASTER MCD AND THE OIL TANK EMPTY. ENGINE CHANGESDR CA190507004Engine · failed(CAN) L/H ENGINE OIL DEBRIS ABOVE LIMITS YESTERDAY THERE WAS AN IMPENDING BYPASS MESSAGE POSTED. PER MANUAL RECOMMENDATION AIRCRAFT WAS RELEASED AND INSPECTION WAS PLANNED FOR THE EVENING. DURING MOF REPLACEMENT FOUND 1 LARGE METALLIC SLIVER WHICH PROMPTED ISDR AALA201905049007Engine · fireAIRCRAFT WAS GROUNDED: UPON PARKING A/C, RECEIVED SIGNAL FROM RAMPERS OF A SMALL TAIL PIPE FIRE FROM NR 2 ENGINE. MOTORED ENGINE, FIRE EXTINGISHED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW CARD 26L40071001SDR DALA2019050302784Engine · malfunctionedCLB PWR @ APPROX 6500 CLIMBING RT OIL QUANTITY WENT TO ZERO FOLLOWED BY RT OIL LOW MESSAGE. FOLLOWED QRH AND SHUT DOWN PER CHECKLIST. NO ABNORMAL APPROCH AND LANDING INTO MCO. OIL PX WENT TO ZERO FOR APPROX 2 MIN. REMOVED AND REPLACED NR 2 ENGINE PER WC 7100-4SDR CA190509007Guide Vane · worn(CAN) ON DEPARTURE R26L AT APPROX 80KTS, CREW ENCOUNTERED A LOUD BANG FROM RIGHT ENGINE. AIRCRAFT RAPIDLY TORQUED TO THE RIGHT.CREW SHUT ENGINES TO IDLE AND STOPPED. CFR DEEMED AIRCRAFT WAS OK TO TAXI TO GATE ON IT`S OWN POWER. RESOLUTION STAGE 10 REPLACED ASSDR CA190502002Engine · failed(CAN) R/H ENGINE OIL CONSUMPTION ISSUE R/H ENGINE INCREASED OIL CONSUMPTION, OIL SIGNS IN TURBINE EXHAUST CASE AS PER PRATT INSTRUCTIONS, RH ENG POWER ASSURANCE TEST NO REMARKS. OIL CONSUMPTION WITHIN LIMITS. ADDITIONAL BORESCOPE INSPECTION IAW CAS-44587 PESDR ASAA2019050129203Nut Plate · corrodedREF T/C 78472000 NR 2 ENG INLET AND FAN BLADES DETAILED INSP FOUND 25 EA NUTPLATES ON O/B SIDE OF FAN FRAME FROM 1 O'CLOCK TO 6 O'CLOCK POS BEHIND OIL TANK, ALF, WITH 1 NUTPLATE BEHIND HMU HAVE CORROSION UNDER NUTPLATES. GROUNDED - YES. REMOVED AND REPLACED ENSDR CA190628009Engine · deteriorated(CAN) AIRCRAFT REPORTED STALL/SURGE AROUND 60-70% DURING ACCELERATION AND DECELERATION. PILOTS REPORTED THE DEFECT ON THE#1 ENGINE, HOWEVER UPON INVESTIGATION THE ENGINEERS REPORTED IT ON BOTH ENGINES. CUSTOMER CHECKED THE BLEED SYSTEM AND CONDUCTED A CAPPED RSDR ASAA2019043029204Boss · looseNR 2 ENGINE B6-B7 FAN FRAME SHROUD TEST BOSS IS LOOSE AT TWO O'CLOCK AFT FACING FORWARD. GROUNDED - YES. REMOVED AND REINSTALLED BOSS ASSY AT 2 O'CLOCK POSITION ON NR 2 ENG. REF SHOP MANUAL 72-23-31. NO DAMAGE NOTED ON THE FAN CASE. INSTALLED AFT ACOUSTIC PANESDR CA190521024Chip Detector · activated(CAN) THE CREW WAS JUST FINISHING UP THE COLLECTIVE PITCH STOP CHECK WHEN ENG #2 CHIP ILLUMINATED. CONDUCTED THE ENG CHIP PROCEDURE AS LISTED IN THE QRH. CHIP DID NOT CLEAR AFTER FIRST ATTEMPT OF PULSE CHIP DETECTOR SYSTEM. ADVISED ATC OF SITUATION AND REQUESTSDR YENA201904290252Engine · contaminatedFLT 2850, UIO-FLL. DESCENDING THRU 7,000 FEET IN CLEAR AIR EXPERIENCED MUSTY DIRTY SOCK SMELL IN FLIGHT DECK AND CABIN. SHUT CROSS BLEED AND TURNED PACK 1 OFF PER ODOR ISOLATION CHECK LIST. ODOR DIMINISHED IN ABOUT 90 SECONDS. LANDED PRIOR TO ANY FURTHER TROUBSDR CALA2019042900672Seal · damagedPDA 2 ENGINE 2 INBOARD FLEX SEAL SEGMENT IS BENT, BROKEN, CRACKED, WITH PIECE MISSING.SDR DALA2019042982730Engine · power lossSHIP 655- IFSD - LEFT ENGINE ROLL BACK AND IFSD ON APPROACH INTO MCO. CORRECTIVE ACTION: MTC FOUND EGT EXCEEDANCE OF 703 DEGREES, REPLACED LEFT ENGINE.SDR UIEA2019042974054Engine · fluctuatesAFTER POWER WAS REDUCED TO IDLE FOR DESCENT, THE LEFT ENGINE WOULD FLUCTUATE FROM 45% TO 52% N1. N2 AND FUEL FLOW WOULD FLUCTUATE AS WELL.(<P>PERFORMED VISUAL INSPECTION OF ENG IAW AMM 71-00-00, NO DEFECTS NOTED @ THIS TIME. PERFORMED VISUAL INSP AT CONNECTORSSDR CA190426021Engine · power loss(CAN) REPORTED TO HAVE A POWER LOSS SHORTLY AFTER TAKEOFF AND CRASHED INTO RESIDENTIAL BUILDINGS AIRCRAFT CAME TO REST ON THE LEFT SIDE. EXTENT OF INJURIES NOT REPORTED BUT NO FATALITIES INVOLVED. (TC# 20190426021)SDR ANCF2019042601Engine · abnormalABR 6. DURING TAKE OFF EGT ON ENGINE #2 OVERLIMIT 970° UNTIL THE TRUSH REDUCTION. CORRECTIVE ACTIONS: ABR 7. IN ACCORDANCE WITH TSM 77-00-00-810-849-A STEP 4.A.1 AND AMM 72-00-00-200-008 STEP 4.B.1 AND 3 THE POWER RANGE WHERE THE ENGINE OVERTEMPERATURE OCCUREDSDR QMLA2019043059043Chip Detector · activatedDURING 2ND START OF THE DAY WITH PATIENT AND MEDICAL CREW LOADED, WITH ENGINE AT GROUND IDLE, ENG CHIP CAUTION ILLLUMINATED, EXTINGUISHED, THEN REAPPEARED. AIRCRAFT WAS SHUT DOWN AND MAINTENANCE NOTIFIED. AIRCAFT WAS PLACED OUT OF SERVICE FOLLOWING INSPECTION SDR DALA2019042982690Engine · failedON SHORT FINAL HEARD A LOUD BANG FOLLOWED BY NOTICEABLE YAW MOMENT TO THE LEFT. LEFT ENGINE INSTRUMENTS ROLLED BACK TO 1.02 EPR 20 PERCENT N1 EGT 525, N2 48 PERCENT WITH THROTTLE @ APROX 1.3 ENGINE UNRESPONSIVE TO THROTTLE MOVEMENT ON GROUND. REMOVED AND REPLASDR CA190429022Engine · making metal(CAN) ENGINE CHIP LIGHT ILLUMINATED, FOLLOWING FLIGHT AME EXAMINED CHIP PLUG AND FOUND METAL BEYOND LIMITS ON MAGNETIC PLUG. (TC# 20190429022)SDR CA190425013Liner · burned(CAN) R/H ENGINE COMBUSTION CHAMBER BORESCOPE SPECIAL REINSPECTION. LINER SEGMENT BURN THROUGH DAMAGE, ENGINE TO BE REPLACED. R/H ENGINE REPLACED (TC# 20190425013)SDR DALA2019042402714Fitting · damaged#2 R/H ENG DRAG FITTING #2 HOLE HAS 2 INDICATIONS OF DEFECTS CLOCKED AT 10 OCLOCK AND 3 OCLOCK POSITIONS IN THE UPPER SKIN. REPAIRED #2 R/H ENGINE DRAG FITTING #2 HOLE PER ER/A 576658-14AD REV ORIGINAL. (1043395)SDR DALA2019042402601Engine · malfunctionedCLIMBING THROUGH 11000 FEET FELT STRONG YAW TO LEFT, N1 AND N2 ROLLED BACK, EGT HIGH ALL ON NBR 1 ENG. LOUD BANG. SHUT DOWN ENGINE PER QRH AND RETURNED TO PHL. REMOVED AND REPLACED ENGINE.SDR CA190501003Engine · damaged(CAN) RIGHT ENG N2 VIB ICON WHEN BRINGING THRUST LEVERS UP NEAR 73% N2, ABORTED TAKEOFF LOW SPEED NO EXCEEDANCES. FELT SHUDDER THROUGH AIRFRAME DURING THROTTLE INCREASE. CORRECTIVE ACTION: REF AMM 05-51-27 NO HIGH ENERGY STOP/RTO INSPECTION REQUIRED BTMS OPS SDR UIEA2019042603990Nut · brokenN0.4 ENG RH FAN COWL FWD HOIST POINT ATTACHMENT SCREW 2 EA A/NUT FOUND BROKEN.(<P>N0.4 RH FAN COWL HOIST PLATE REPAIRED IAW RL-71-11-13526 REV.A<BR /></P>)SDR HALA201904230198Engine · making metalETOPS SIGNIFICATION - UPON ENG START WHEN START SWITCH TO IGN/START, ECAM ENG 1 OIL CHP DETECT ILLUMINATED. ABORTED START, ECAM CLEARED, MX CONTROL IN HNL SAID OK TO START. NEXT START NORMAL. // PERFORMED TSM 79-35-00-810-808-A, FOUND 2 "MAGNETIC FINE" PARTICLSDR CALA2019042200634Engine · surges2822-2 ESN 222036 EXPERIENCED SURGE DURING TAKEOFF RUN AT 60KTS. ON RETURN TO GATE GRUMM REPORTED METAL IN TAILPUPE. ACCOMPLISH BORESCOPE INSPECT HPC STG 5,6,9,AND HPT STG 1 AND 2. REF AMM72-00-00 P6XX CFG2. IF SIGNS OF IMPACT, INSPECT OTHER STAGES. PERFORMEDSDR AALA2019042329001Engine · fireAIRCRAFT NOT GROUNDED: PILOT REPORTS AFTER GATE ARRIVAL IN KIN, AND ENGINES AND APU SHUTDOWN. GROUND CREW REPORTED FIRE IN #'2 ENGINE. THERE WAS NO FIRE OR OVERHEAT INDICATION IN COCKPIT. FIRE WENT OUT, DURATION UNKNOWN, BUT LESS THAN 5 MINUTES CONTINUED. AISDR UIEA2019042203925Engine · vibrationLEFT ENGINE FAN VIBES REACHED 4.3 DURING CLIMB OUT.(<P>PERFORMED ENGINE RUN AND VIBE INDICATIONS NML PER AMM 71-00-00 PER FIM 71-05 FT 805. NOTE: VIB LEVELS CAN SUDDENLY SPIKE AT TRANSIENT LEVELS OF ENGINE SPEEDS.</P>)SDR SIMA20190420002Engine · vibrationNUMBER ONE ENGINE LP VIB AMBER 4.0 IN FLIGHT APPROX 14,000 FT IN CLIMB ,COMPLIED W/QRH PROCEDURE , POWER REDUCTION TO 75% N1 NESSORY TO BRING LP BACK TO GREEN RANGE ,DID NOT OCCURE WHILT TL WAS IN MOTION ,DID NOT OCCURE WHILE IN ICING CONDITIONS.-C/A-COMPLIED SDR SWAA2019042331879Engine · smokeAT 500 AGL. A STRONG SMOKE ODOR WAS NOTICED. FLT ATT CALLED SHORTY AFTER SAYING THEY SMELLED ODOR. AFTER TOUCH DOWN/CLEAN UP, SMOKE ODOR DISSAPITED. NO VISIBLE SMOKE WAS SEEN BY PILOTS OR FLT ATTENDANTS. REMOVED AND REPLACED #1 ENGINE OPS CHECK GOOD I/A/W MSDR 9WGA201904190001Engine · failed#1 ENGINE FAILURE @ FL200 ENG 1 FADEC MAINT LEVEL 1 ALERT - INTERMITTENT ROUGH VIBRATION EVERY 10-15 SECONDS WITH NO INDICATION ON SYNOPTIC PAGESDR CA190425019Engine · fire(CAN) THERE WAS EVIDENCE OF A FIRE IN THE #1 ENGINE. INITIAL INSPECTIONS INDICATE THE POSSIBLE ORIGIN BEING BETWEEN THE ENGINE DRIVEN FUEL PUMP AND THE FUEL LINE FITTING. THE DAMAGES ARE AS FOLLOWS: THERE WAS DISCOLORATION ON THE W2 BLUE ENGINE HARNESS - CONTISDR UIEA2019041703899Engine · malfunctionedR ENGINE NO LIGHT OFF WITH SINGLE IGNITER, SWITCHED TO BOTH IGNITERS.(<P>PERFORMED ENGINE START / RUN W. SINGLE IGNITER SELECTED. ENGINE START UP NORMAL THROUGH ALL PARAMETERS. ALSO PERFORMED IGNITER CHECK PRIOR TO START. NO FAULTS NOTED IAW AMM 74-00-00 & 80-SDR CA190426001Engine · vibration(CAN) THE CREW REPORTED A HIGH VIBRATION CAS MESSAGE WAS RECEIVED ON #3 ENGINE WHEN THE THROTTLES WERE ADVANCED (PRIOR TO TAKE-OFF). THE TAKE-OFF WAS ABORTED JUST AS THEY STARTED TO ROLL, WELL BELOW V1. TROUBLESHOOTING IS GOING ON. (TC# 20190426001)SDR CA190417002Engine · failed(CAN) INCREASE OF R/H ENGINE OIL CONSUMPTION INCREASE OF RHE OIL CONSUMPTION NOTICED BY MAINTENANCE. NO EXTERNAL OIL LEAK REPORTED. A/C RELOCATED FOR FURTHER TROUBLESHOOTING TROUBLESHOOTING CARRIED OUT. EVIDENCE OF LEAK FROM #4 BEARING COMPARTMENT FWD SEALSDR CA190415003Bearing Seal · leaking(CAN) R/H ENGINE OIL CONSUMPTION ISSUE CREW REPORTED RH ENG LOW OIL QTY ADVISORY MESSAGE AFTER TAKE OFF, OIL LEVEL 8.8L. AFTER PITCH DECREASED MESSAGE DISAPPEARED, OIL LEVEL 10-12L. ENGINE OIL CONSUMPTION MONITORING EXAMINATION PERFORMED IAW AMP (RESULT 1.26SDR CALA2019041200569Fairing · missingLEFT ENGINE INTERMEDIATE CASE STRUT FAIRING MISSING, 9 O''CLOCK STRUT UPPER SIDE. INTERMEDIATE CASE FAIRING MISSING FROM L/H ENG 9 O CLOCK POSITION NEEDS TO BE REPLACED BEFORE 51 HOURS OF OPERATION. PER TABLE 601 AMM 72-34-05-206-005. NO OTHER DAMAGE OR LOOSE SDR CALA2019041200566Fairing · missingINTERMEDIATE CASE STRUT FAIRING MISSING FROM LT ENG S/N 724379 AT THE 9 O CLOCK POSITION LOOKING FWD FROM THE AFT OF ENGINE. REF GMM 02-30-95 PDA PROGRAM CAT 2 APPROX SIZE OF PANEL 14" X 6" IAW AMM 72-34-05 MISSING FAIRING IS TO BE REPLACED BEFORE THE 51ST HOUSDR JJBA201904110806Engine · shutdownE2 SHUTOFF DURING CRUISE FLIGHT (UNCOMMANDED). R&R #2 ENGINE. OPS AND LEAK CHECK SAT.SDR AALA201904099001Engine · shutdownAIRCRAFT WAS GROUNDED: PILOT REPORTS THAT ENG 1 SHUTDOWN UNCOMMANDED AFTER ENG START, WHEN APU WAS STARTED AND APU BA VALVE OPEN. MAINTENANCE ACCOMPLISHED BORESCOPE INSP. OF LPT IAW AMM 72-54-00-290-005, 72-54-00-290-006, 72-54-00-290-007, 72-54-00-290-008 ANDSDR MASA2019040511799Warning Light · illuminatedENG 1 VIBE ICON IN FLT AT CRUISE SETTING- RTF.SDR IPXA2019040540794Engine · fireEMERGENCY DECLARED - LEVEL 2 ENGINE OIL PRESS LOW ON ENGINE #2 2 PSI RED BOXED ON ENGINE INSTRUMENT. TOWER NOTIFIED US THAT ANOTHER UPS AIRCRAFT REPORTED A FIRE #2 ENGINE. TOWER NOTIFIED US AGAIN THAT WE NEEDED TO EVACUATE .R & R #2 ENG OIL PRESSURE TRANSMITTESDR CA190425011Engine · making metal(CAN) ON ENGINE START CHIP LIGHT ILLUMINATED, CHIP PLUG AND OIL FILTER FOUND TO CONTAIN UNACCEPTABLE AMOUNT OF METAL CONTAMINATION. (TC# 20190425011)
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