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 P5CA0501330Engine · vibrationEXCEEDANCE REPORT ON ENGINE NR 4 VIBRATION, .4 AFTER ENGINE START. REPLACED NR 4 ENGINE DUE TO VSV LEVER ARM BROKEN ON 5TH STAGE IAW P71-00-001A/2A POLAR ENGINE CHANGE WORK CARDS.SDR DXTA200500632Engine · failedRT ENGINE FAIL IN FLIGHT DURING CRUISE AT FL340. RUN CHECKLIST ATTEMPTED RESTART, RESTART FAIL. FADEC FAIL RT A, FADEC FAULT RT A-B CAS MESSAGE. ITEM IS UNDER INVESTIGATION.SDR C2XA05CL016Engine · smokeCLE - FLIGHT 2115 THE CREW REPORTED SMOKE IN CABIN AND FLIGHT DECK FROM PACKS. THE AIRCRAFT RETURNED TO LGA AND MAINTENANCE PLACED PACK NR 1 ON MEL. THE AIRCRAFT HEATING AND AIR CONDITIONING SYSTEM WAS TESTED THE NEXT DAY AND FOUND TO BE OPERATING CORRECTLY,SDR DL76G050162Engine · leakingENGINE SHUTDOWN BY CREW AT CRUISE DUE TO OIL QTY DROPPED TO 0 AND OIL PRESSURE STARTED FLICKERING. REPLACED ENGINE.SDR ASMF200503015Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, N1 WAS INCREASED SLOWLY AFTER EGT INDICATION. THE FAULT ISOLATION PROCEDURE 80-07, TASK 802 WAS PERFORMED AND THE RIGHT ENGINE WAS STARTED IAW MM 71-00-00, TESTED CORRECT.SDR CA050329005Engine · malfunctioned(CAN) DURING DESCENT THE ENGINE WAS REPORTED AS NOT RESPONDING TO THROTTLE INPUT. THE ENGINE WAS SHUTDOWN IN FLIGHT. THE ENGINE WAS INSPECTED AND INSTALLED ON A SECOND AIRCRAFT. DURING A SUBSEQUENT FLIGHT, THE PROBLEM RE-OCCURRED WITH THE ENGINE AGAIN BEINGSDR CA050321007Engine · making metal(CAN) AFTER TAKEOFF, CREW NOTICED NR2 ENG CHIP DETECTOR WARNING LITE ON, FOLLOWED SHORTLY BY NR 2 ENGINE OIL FILTER LITE (WARNING). PILOT REDUCED THRUST ON NR2 ENGINE AND RETURNED TO AIRPORT. MAINTENANCE INSPECTION DISCOVERED METAL ON CHIP DETECTOR AND IN FISDR CA050323003Engine · failed(CAN) FOUND BETA CNTRL SYS WAS JAMMED. BETA CNTRL SLEEVE HAD WORN AGAINST PROPSHAFT DIA. RGB WAS REBUILT, IDENTICAL FAILURE IN TEST CELL. RGB WAS REBUILT, TESTED, RETURNED. NOT INSTALLED BUT RETURNED BECAUSE OF LOOSE MOUNT RING ON RGB. CORRECTED, ENG TESTED SDR ASMF200503014Control Valve · failedAIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTED WITH CROSSED FEEDING, EICAS MESSAGES R HYD R SUR PRESS, R ENG REV CONE, L ENG REV CONE, L ENG FIRE LOOP 2, EPR DET LOOP 2 INCHES AND (RT ENGINE EPR OUT OF SERVICE) WERE SHOWN AND PNEUMATIC AUXILIARY POWER UNISDR CA050311005Engine · unknown(CAN) DURING TAKEOFF AND CLIMB OUT PILOT REPORTED A CHANGE IN THE SOUND OF THE ENGINE. AIRCRAFT RETURNED. PILOT REPORTED ENGINE INDICATION NORMAL, NO ENGINE PERFORMANCE ABNORMALITIES. MAINTENANCE INSPECTED THE ENGINE OIL FILTER, NO FINDINGS, ENGINE WAS RUN WISDR AT0500012Engine · inoperativeLEFT ENGINE COMPRESSOR STALLS AND ROLL BACK AT FL310. REMOVED AND REPLACED LEFT ENGINE.SDR CHQA200500053Engine · unserviceableFLIGHT 6236 GSO-MCO - ON INITIAL CLIMB AT APPROXIMATELY 800 FEET, A LAV SMOKE WARNING APPEARED ON EICAS. THE TOWER WAS NOTIFIED AND THE FLIGHT ATTENDANT CHECKED THE CABIN FOR SIGNS OF FIRE OR SMOKE. NO EVIDENCE WAS FOUND. ON SHORT FINAL AN E1 LOW OIL PRESS SDR 03102005Engine · failedDURING CLIMB THE LEFT ENGINE FAILED.SDR CHQA200500051Engine · unserviceableFLIGHT 6236 MCO-GSO - AT APPROXIMATELY 400 FEET A LAV SMOKE MESSAGE APPEARED ON EICAS. THE TOWER WAS ALERTED AND AFTER TWO MINUTES THE MESSAGE DISAPPEARED. THE FLIGHT ATTENDANT FOUND NO EVIDENCE OF SMOKE OR FIRE ANYWHERE IN THE CABIN. THE AIRCRAFT RETURNED SDR AJC2005F00001Engine · vibrationAC DEPARTED, ENROUTE, AT FL360 THE RT ENG DEEC COMPUTER TRIPPED TO MANUAL MODE, FOLLOWED BY LOSS OF N1 GGE INDICATION. FLIGHT CONTINUED NORMALLY, EXPERIENCED A RT ENG VIBRATION WHICH CLIMBED TO .8 ON THE VIBRATION INDICATOR. REDUCED POWER ON RT ENG TO 75 PERSDR AALA20050184Engine · making metalDFW INFLIGHT T1304/6 MAR LOUD BAND AND SHUTTER. LEFT ENGINE LOST POWER. ROLLED BACK TO IDLE. ENGINE RAN AT IDLE UNTIL AFTER LANDING. ENGINE WAS SHUT DOWN AFTER LANDING. FOUND METAL IN TAILPIPE. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL SDR SWIA200514662Engine · leakingNR 1 ENGINE HAS OIL LEAKING, FOUND A SUMP DRAIN LEAKING BEYOND LIMITS. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY IAW 71-00-00, OPERATIONAL CHECK GOOD.SDR GTIA050049Engine · malfunctionedLOST OIL IN LT ENGINE, QTY 0, PRESSURE 40 PSI, TEMP RISING, SHUT DOWN LT ENGINE BEFORE LOSING ALL OIL PRESSURE, OIL PRESSURE BELOW 10 PSI WHILE WINDMILLING. REMOVED AND REPLACED NR1 ENGINE. (K)SDR CA050308011Engine · failed(CAN) DURING TAKE-OFF THE CREW HEARD A LOUD BANG FOLLOWED BY A DROP IN N1 FROM 80 PERCENT TO 19 PERCENT ON THE NR 1 ENGINE. AT 70 KNOTS FORWARD SPEED A REJECTED TAKE-OFF WAS INITIATED WITHOUT INCIDENT. ON RETURN TO THE GATE, OIL PRESSURE DROPPED TO ZERO. NRSDR CA050323004Engine · making metal(CAN) IN CRUISE THE ENGINE EXPERIENCED A POWER LOSS ACCOMPANIED BY A GEARBOX CHIP DETECTOR INDICATION. THE PILOT CARRIED OUT AN EMERGENCY LANDING ON A ROAD-WAY WHICH RESULTED IN DAMAGE TO THE AIRCRAFT. MFG WILL MONITOR THE INVESTIGATION OF THIS INCIDENT AND SDR GAIA05013OPAir Cleaner · crackedDURING CLIMBOUT THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. THE AC RETURNED TO AIRPORT AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE NR 1 ENGINE AIR CLEANER DUE TO CRACKED FLANGES. LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETSDR ARWA20050304Compressor · stalledNR 2 ENGINE COMPRESSOR STALL ON TAKEOFF ABORT AT 30 KNOTS. INSPECTED INLET AND EXHAUST AREA OF ENGINE NR 2; FOUND -PAPER FOD-. REMOVED SMALL RESIDUE IN ACCORDANCE WITH PRATT & WHITNEY 72-00; OPERATIONAL CHECK ON RUN-UP IN ACCORDANCE WITH M/M 71-00. NO COMPRSDR A6WA200540083Smoke · detectedEXCESSIVE SMOKE OUT OF RT ENGINE ON SHUTDOWN ALL INDICATIONS WERE NORMAL. PERFORMED ENGINE RUN OF ENGINE NR 2 IAW CRJ AMM TASK 71-00-00-848-806. NO DEFECTS NOTED. AIRCRAFT SAFE FOR SERVICE. (M)SDR 2005UALA00207Compressor · stalledNR 1 ENGINE COMPRESSOR STALL AND AUTO SHUTDOWN. ABORTED TAKEOFF AT 50 KIAS DUE TO COMPRESSOR SURGE. CAPT REPORTED STRONG X-WIND AT 20 GUSTING 33. FOUND METAL IN THE TAILPIPE. ENGINE REPLACED AT IAD. ENGINE RETURNED TO LESSOR ON 06/08/05 WITHOUT BEING DISASDR CA050323006Engine · malfunctioned(CAN) ON APPROACH THE ENGINE EXPERIENCED AN UNCOMMANDED POWER (TORQUE) REDUCTION ACCOMPANIED BY A LOUD NOISE AND LOSS OF ENGINE OIL PRESSURE. THE CREW SECURED THE ENGINE IN FLIGHT AND ACCOMPLISHED A SINGLE-ENGINE LANDING. SUBSEQUENT INSPECTION REVEALED DAMAGSDR DL777050136Engine · making metalMETAL DISCOVERED IN MCD AND SCAVAGE FILTER NR 2 ENGINE. REPLACED ENGINE.SDR MALA050233Engine · making metalDURING CRUISE FLIGHT RT ENGINE CHIP DETECTOR LIGHT ILLUMINATED AND THEN IT CYCLED ON AND OFF. ANOTHER 6 TO 8 TIMES BEFORE LANDING IN ROA. REMOVED AND REPLACED RT ENGINE IAW 71000-301, S/N ON GE-E785738, S/N OFF GE-E285693 IAW 7100-301. ALL CHECKS GOOD.SDR CA050228003Engine · fod(CAN) DURING TAKE-OFF, NR 1 ENGINE STALL SURGE AND 2 AUDIBLE STALLS HEARD. N1 REACHED 107 PERCENT FOR 3 TO 4 SECONDS. REJECTED TAKE-OFF INITIATED WITHOUT INCIDENT AND AIRCRAFT RETURNED TO THE GATE. SUSPECT FOD DUE TO ICE. ENGINE CHANGE IN PROCESS.SDR DL73S050135Engine · odorFRONT LAV SMOKE ALARM CAME ON SHORTLY AFTER TAKEOFF AND SMOKE THIN AND WISPY, CAME FROM LAV. SMOKE SMELL EVIDENT THROUGHOUT ENTIRE AIRCRAFT. WASHED NR 1 ENGINE AND RAN ENGINE WITH PACKS. NO SMELL NOTEDSDR COMA0560141Engine · malfunctionedFLIGHT 5121 DURING TAXI OUT WITH BOTH ENGINES OPERATING CREW RECEIVED AN EICAS "COMP MON" MESSAGE LOOSING ALL NR 2 ENGINE INDICATIONS. WHEN INDICATIONS RETURNED 15 SECONDS LATER, ENGINE NR 2 ITT INDICATED 990C WITH ABNORMAL N1 AND N2 INDICATIONS. THE CREW NOSDR GTIA050040Engine · malfunctionedNR 1 ENGINE SLOW TO SPOOL, TAIL SWAP WITH AIRCRAFT 810. REMOVED AND REPLACED NR 1 ENGINE. (K)SDR CA050228001Engine · fluctuates(CAN) IN-FLIGHT SHUTDOWN OF NR 2 ENGINE DUE TO OIL PRESSURE FLUCTUATION. AIRCRAFT WAS ENROUTE WHEN THE EVENT OCCURRED, AT WHICH AN EMERGENCY WAS DECLARED AND THE AIRCRAFT HAD TO COMPLETE AN UNSCHEDULED LANDING. AFTER LANDING INSPECTION, AIR CREW REPORTED AN ESDR CA050307007Engine · failed(CAN) DURING CLIMB, THE ENGINE EXPERIENCED AN INCREASE IN TURBINE TEMPERATURE ACCOMPANIED BY VIBRATION AND NOISE. THE CREW SHUT THE ENGINE DOWN IN FLIGHT AND DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED DEBRIS ON THE TURBO MACHINERY AND REDSDR CA050224008Engine · shutdown(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN IN CRUISE. SUBSEQUENT RELIGHT ATTEMPTS WERE UNSUCCESSFUL. THE CREW DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED. MFG WILL INVESTIGATE THE EVENT AND SUPPLEMENT THIS REPORT TO REFLECT ROOT CAUSE ONCE ESTABSDR CA050228013Engine · unknown(CAN) A/F 18258 HOURS. HELI SKIING OPERATION. PILOT WAS DESCENDING DOWN A HILL AND SETTING UP HIS APPROACH TO LAND HELICOPTER. THE PILOT PULLED IN POWER TO CONTROL HIS DESCENT RATE AND NOTICED THAT THE ENGINES REMAINED IN FLIGHT IDLE. HE CHECKED HIS THROTTLE SDR CA050307001Engine · unresponsive(CAN) ON APPROACH NEITHER ENGINE RESPONDED TO INCREASED COLLECTIVE. THE AIRCRAFT AUTOROTATED TO A HEAVY LANDING. MFG WILL MONITOR THE INVESTIGATION INTO THIS EVENT AND WILL SUPPLIMENT THIS REPORT TO REFLECT ROOT CAUSE, ONCE ESTABLISHED.SDR 022405N523CS1Engine · malfunctionedDURING CRUISE AT ALTITUDE 40,000 FEET, THE RIGHT ENGINE DID A UNCOMMANDED SHUTDOWN. THE CREW PUT THE AIRCRAFT INTO THE RESTART ENVELOPE AND ATTEMPTED TWO INFLIGHT RESTARTS. THE ENGINE WOULD NOT START SO AN EMERGENCY WAS DECLARED AND THE AIRCRAFT SAFELY LANDESDR DL76L050127Engine · surgesDURING T/O FROM ATL, NR 2 ENGINE SURGED APPROX 5 TIMES. AIRCRAFT RETURNED TO ATL. REPLACED ENGINE.SDR UIEA200500009Engine · vibrationFLT GT 9991 - ENGINE NR 2 VIBRATION OCCURRED DURING CLIMB-OUT AND INTERMITTENTLY DURING FLIGHT. AFTER 4 HOURS FLIGHT TIME THE LEVEL OCCASIONALLY EXCEEDED 5.0, NR 3 EGT AVERAGED ABOUT 18 DEG HIGHER THAN THE OTHER THREE. REMOVED AND REPLACED NR 3 ENGINE IAW ATSDR P5CA0501324Engine · malfunctionedCREW REPORTED NR 1 ENGINE WOULD NOT MAKE TAKEOFF EPR. INSPECTED NR 1 ENGINE PER MM 71-00-00, OPENED MEL 77-4-1 FOR EPR UNRELIABLE.SDR DL76L050124Engine · stalledRIGHT ENGINE STALLED DURING CLIMB, BUT CONTINUED TO OPERATE. DIVERTED FLT TO LGW. REPLACED ENGINE.SDR SWIA200514623Engine · smokeAFTER APPLYING TAKEOFF THRUST, NOTICED A STRONG OIL SMOKE SMELL IN THE AIRCRAFT. SMELL DISAPPEARED AFTER SEVERAL MINUTES IN FLIGHT. RECEIVED SMOKE TOILET MESSAGE DURING INITIAL CLIMBOUT. REMOVED AND REPLACED RIGHT ENGINE. OPERATIONAL CHECK GOOD.SDR UPS05143914Engine · crackedNR 1 ENGINE INLET SKIN CRACKS. R&R LT ENGINE NOSE COWL IAW A300 MM THRU STEP 3B (10). INSTALLED LT NOSE COWL LEAK CHECK GOOD REF MM. THIS CLEARS D296652 INSPECTION.SDR CA050224010Engine · failed(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN IN DESCENT. MFG WILL INVESTIGATE THE INCIDENT AND WILL SUPPLEMENT THIS REPORT TO REFLECT ROOT CAUSE ONCE ESTABLISHED.SDR DXTA200500601Engine · leakingDURING FLIGHT CREW & PASSENGERS NOTICED FUMES IN CABIN. AFTER LANDING FOUND OIL LEAKING FROM NR 1 ENGINE & NO OIL SHOWING ON SIGHT GAUGE. ENGINE CHANGE CURRENTLY IN WORK.SDR CA050224009Engine · power loss(CAN) THE ENGINE WAS REPORTED TO HAVE LOST POWER SHORTLY AFTER DEPARTING THE RUNWAY. THE AIRCRAFT SUBSEQUENTLY IMPACTED THE GROUND. MFG WILL MONITOR INVESTIGATION OF THE INCIDENT AND WILL SUPPLEMENT THIS REPORT TO REFLECT ROOT CAUSE, ONCE DETERMINED.SDR 05FDEA00312Engine · vibrationON TAKEOFF NR 2 THROTTLE REQUIRED ONE KNOB WIDTH BEYOND 1 & 3 ON CLIMBOUT AT 3000 FT AGL RECEIVED AIR MANF 2 FAIL WITH NOTICEABLE AIRFRAME VIBRATION. ENG 2 OIL TEMP HIGH ALERT FOLLOWED WITH PEAK OIL TEMP OF 201 DEGREES C. ENGINE WAS SHUTDOWN AND NR 2 ENGINE SDR CA050224012Engine · failed(CAN) ON TAKEOFF ROLL THE AIRCRAFT EXPERIENCED A YAW ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN ENGINE TORQUE AND TUBINE OVER TEMPERATURE AND LOW OIL PRESSURE WARNING ANNUNCIATIONS. TAKEOFF WAS ABORTED. MFG WILL INVESTIGATE THE INCIDENT AND WILL SUPPLIMENT TSDR 2005F00023Engine · malfunctionedON TAKEOFF ROLL, AIRCRAFT PULLED TO THE LEFT AND TORQUE INDICATION FLUCTUATED FOLLOWED BY HIGH ITT INDICATION. UPON POWER REDUCTION, THE OIL PRESSURE WARNING LIGHT CAME ONE. REMOVED ENGINE FOR INVESTIGATION. (M)SDR CA050221001Torque Shaft · cracked(CAN) DURING CLIMB, NR1 PEC CAUTION LIGHT ILLUMINATED FOLLOWED BY A DROP IN NP AND TQ. A FEW SECONDS LATER THE NR1 ENG FADEC FAIL WARNING LIGHT ILLUMINATED AND ALL PARAMETERS BECAME (DASHES). THE PILOTS ELECTED TO SHUTDOWN NR1 ENGINE AND RETURN TO BASE. SI
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