JASC 7250
Service difficulty reports · 3,622
Reports filed under 7250 · Turbine Section, 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 = '7250' 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 = '7250' 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 DXTR2026101701Turbine Blades · cracked2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.SDR 2026FA0000874Blade · unknownON 13 OCTOBER 2026, A RECORDS REVIEW IDENTIFIED 14 UNIQUE AUTHORISED RELEASE CERTIFICATE (ARC) RECORDS FOR COMPONENT LPT BLADE STG 1, PART NUMBER 1647M61P03. THE ARCS WERE ISSUED WITH AN "OVERHAULED" STATUS, WHEREAS THE CAPABILITY LIST SPECIFIED "INSPECTION, RSDR 2026FA0000873Blade · unknownON 13 OCTOBER 2026, A RECORDS REVIEW IDENTIFIED 4 UNIQUE AUTHORISED RELEASE CERTIFICATE (ARC) RECORDS FOR COMPONENT LPT BLADE STG 7, PART NUMBER 362-062-810-0. THE ARCS WERE ISSUED WITH AN "OVERHAULED" STATUS, WHEREAS THE CAPABILITY LIST SPECIFIED "INSPECTION"SDR 2026FA0000869Blade · unknownON 13 OCTOBER 2026, A RECORDS REVIEW IDENTIFIED 1 UNIQUE AUTHORISED RELEASE CERTIFICATE (ARC) RECORD FOR COMPONENT LPT BLADE STG 3, PART NUMBER 9373M33P09. THE ARCS WERE ISSUED WITH AN "OVERHAULED" STATUS, WHEREAS THE CAPABILITY LIST SPECIFIED "INSPECTION, MODSDR 2026FA0000868Blade · unknownON 13 OCTOBER 2026, A RECORDS REVIEW IDENTIFIED 12 UNIQUE AUTHORISED RELEASE CERTIFICATE (ARC) RECORDS FOR COMPONENT LPT BLADE STG 3, PART NUMBER 9373M33P08. THE ARCS WERE ISSUED WITH AN "OVERHAULED" STATUS, WHEREAS THE CAPABILITY LIST SPECIFIED "INSPECTION, MSDR 2026FA0000865Blade · unknownON 13 OCTOBER 2026, A RECORDS REVIEW IDENTIFIED 3 UNIQUE AUTHORISED RELEASE CERTIFICATE (ARC) RECORDS FOR COMPONENT LPT BLADE STG 3, PART NUMBER 6016T62P04. THE ARCS WERE ISSUED WITH AN "OVERHAULED" STATUS, WHEREAS THE CAPABILITY LIST SPECIFIED "INSPECTION, RESDR 2026FA0000864Blade · unknownON 13 OCTOBER 2026, A RECORDS REVIEW IDENTIFIED 20 UNIQUE AUTHORISED RELEASE CERTIFICATE (ARC) RECORDS FOR COMPONENT LPT BLADE STG 4, PART NUMBER 1778M94G06. THE ARCS WERE ISSUED WITH AN "OVERHAULED" STATUS, WHEREAS THE CAPABILITY LIST SPECIFIED "INSPECTION, RSDR 2026FA0000830Duct · misinstalledEEC COOLING DUCT NOT CONNECTED. DURING INSPECTION OF ENG NR 2 LP COMPRESSOR CASE (FAN CASE) FOUND EEC COOLING INLET DUCT NOT CONNECTED TO INLET COWL AND SUPPORT CLAMP DAMAGED. ACCORDING AMM AND IPC FIGURES THE INLET PIPE SHOULD BE ATTACHED WITH 4EA BOLTS TO TSDR QEMY20260923001Turbine Wheel · shearedTHE SUBJECT DISK-HPT STG 1, HAS SHEARED INTERSTAGE ID BAYONET TABS WHICH WERE IDENTIFIED AT LOCATIONS 8,9,10 &11 PRIOR TO DISASSEMBLY. THE CONDITION IDENTIFIED HAS BEEN EVALUATED AND REQUESTED FOR THE HARDWARE TO BE TAKEN OUT OF SERVICE AND SENT FOR FURTHER TSDR YENA2026091700807Vane · damagedFLT 220, SAN-BOS. (ETOPS) ENG 2 SECOND STAGE TURBINE VANE LE HAS EROSION WITH BURN THROUGH IN AREA B. OPENSDR DXTR2026091102Turbine Blades · cracked2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. R&R ENGINE PER CE-680A AMM 72-00-05, OPS CHK GOOD.SDR DXTR2026091101Turbine Blades · cracked2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. CORRECTIVE ACTION: R&R ENGINE PER CE-680A AMM 72-00-05, OPS CHK GOOD.SDR QEMY20260911002Disk · indication
THE CONDITION IDENTIFIED HAS BEEN EVALUATED AND A RECOMMENDATION TO RETURN TO SERVICE CANNOT BE PROVIDED.
TO BE REPORTED I.A.W AMC-20 8A (J) ANY DEFECT IN A LIFE-CONTROLLED CRITICAL PART THAT CAUSES ITS RETIREMENT BEFORE THE COMPLETION OF ITS FULL-SERVICE LSDR DXTR2026090311Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.SDR DXTR2026090310Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.SDR DXTR2026090308Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHK GOOD.SDR DXTR2026090307Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. R&R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.SDR DXTR2026090306Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.SDR DXTR2026090305Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.SDR DXTR2026090304Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R&R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.SDR DXTR2026090303Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00.SDR DXTR2026090302Blades · crackedBLADE S/N PMOXM75 SUCTION SIDE CRACK .155 INCH. PRESSURE SIDE CRACK .407 INCH (OPEN) THROUGH COOLING HOLE WITH CRACK PRESENT ON TOP OF COOLING HOLE R&R ENGINE.SDR DALA2026090104926Blades · damagedDISCONTINUED TAKEOFF AT 60 KNOTS DUE TO RIGHT ENGINE HIGH VIBE WARNING. PERFORMED BORESCOPE FOUND HPT BLADE DAMAGE. REPLACED NR 2 ENGINE. (LP 7531667, 7531668 - AIRCRAFT WAS GROUNDED)SDR QEMY20260820001Turbine Wheel · failed inspTHE SUBJECT DISK HPT STAGE 1 FAILED NDT ULTRASONIC INSPECTION ON SURFACE SM AT POST NUMBER 54 (AS PER SP007), BETWEEN SLOT NUMBERS 16 & 17, DR 02338861 IS UNDER INVESTIGATION WITH THE OEM FOLLOWING UTI INDICATIONS DURING INCOMING INSPECTION. PART RETIRED FROMSDR SWAA2026073134647Strut · crackedLPT REAR FRAME HAD 2 ADDITIONAL CRACKS FOUND TOTALING 5 WHEN PERFORMING 7256-I-11716-NG. FRAME ASSEMBLY, TURBINE REAR FRAME MOUNT STRUT INSPECTION) [TTG8Q01BASK1] KNOWN FAULTS: NR 2 ENGINE TRF STRUT NR 1 AT LOCATION C1 HAS A CRACK MEASURING .200 LONG. TTG8Q01BSDR SWAA2026073160152Strut · crackedNR 2 ENG, LPT REAR FRAME, TRF STRUT NR 15 LOCATION C2 LARGEST CUMULATIVE CRACK LENGTH OF 0.170 INCH. TRANSFERRED TO [TTG8Q01DDT54] FOR M-21-172-00810 [TTG8Q01DDSQ9] 1300 REINSPECTION INTERVAL.SDR 2026FA0000785Turbine Wheel · meltedTHE MENTIONED PART WAS SEND AS PIECE PART FROM THE CUSTOMER (DELTA) TO MTU BB FOR OVERHAUL. DURING THE INCOMING INSPECTION OF THE COMPONENT AN UNUSUAL FINDING WAS DETECTED IN THE AREA OF THE FIR-TREE PRESSURE FACE,- DEPOSITED MATERIAL/METAL EXHIBITING A MELTESDR 2026FA0000502Turbine · damagedON 2024 THE RYR ENGINE ESN802794 HAS BEEN INDUCTED FOLLOWING BIRDSTRIKE AT TKOF WHICH HAS CAUSED THE OVERTEMPT OF THE ENGINE (PEAK 988°C FOR LESS THAN 1 MINUTE – AREA D). THE RECIEVED WORKSCOPE WAS REQUESTING SPECIFIC INSPECTIONS AFTER EGT EXCEEDANCE (TASK 72-SDR DALA2026060903495Turbine · damagedDIV- DIVERTED TO RDU DUE TO #2 ENGINE HIGH N2 VIBRATION. CARRIED OUT BOROSCOPE INSPECTION ON RT ENGINE. FOUND LPT DAMAGE, REQUIRES ENGINE CHANGE. ENGINE REPLACED. (LP# 8761056, 8761058; AIRCRAFT WAS GROUNDED)SDR SIMA20260531001Engine · vibrationE2 LP VIBRATION IN AMBER AT 4,0 APPROX AT FL180, COULD NOT MAINTAIN CLIMB WITHOUT ENG 2 IN THE CAUTION ABOVE 4.0. WE RAN THE QRH PROCEDURE AND VIBRATIONS IMMEDIATELY CAME BACK EMERGENCY DFECLARED. PERFORMED HIGH POWER RUN ON E2 IAW LMM72-00-00-760-041 HIGHEST SDR 2026FA0000429Turbine · defectiveTHE ENGINE ABY ESN 577716 WAS SLOTTED IN SAESM THE 17 APRIL 2026. DURING THE MM03 LEVEL INSPECTION OF THE LPT CASE, A DEFECT WAS IDENTIFIED ON 28TH MAY 2026. FOLLOWING THIS FINDING, A CSC CASE WAS RAISED TO CFM (TCH) REQUESTING AN APPROPRIATE REPAIR DISPOSITIOSDR YENA2026052000472Liner · burnedFLT #8648 MZJ-JFK (ETOPS) "BSI ON ENG 2 S/N P772492 REQUIRED PER EC 724000-W2-1; DURING BSI FOUND ENG 2 REAR OUTER LINER WITH BURN-THROUGH IN LINER SEGEMENT THAT CAUSE MORE THAN 50% & LESS THAN 75% SEPERATION OF STUD CRACK & BURN-THROUGH ON SHELL EXTEND TO STUSDR QEMY20260421001Turbine Wheel · dentedDISK-HPT STG 1 DISPLAYS 111 SEPARATE INDENTATION TO SURFACE DT ON THE AFT SHAFT SPLINE AREAS. DR #02396459 STATES: THE CONDITION IDENTIFIED DEPARTS FROM THE INSTRUCTION FOR CONTINUED AIRWORTHINESS (ICA). THE CONDITION HAS BEEN EVALUATED AND A RECOMMENDATION TSDR 2026FA0000265Blades · mismanufacturedTHE ENGINE (PT6A-60A, P/N 3102700-01 S/N PCE-PK0793) WAS UNDERGOING A REPAIR I.A.W. P&WC LIGHT OVERHAUL CRITERIA AND WAS TESTED AT EURAVIA. THE ENGINE SUBSEQUENTLY PASSED TEST AND AS PER EURAVIA STANDARD PRACTICE A BORESCOPE POST-TEST WAS PERFORMED. DURING THESDR CALA2026030414305Plug · damagedREMOVED PLUG HPNGVN IN REF TO L/P4936131 FOUND PLUG DAMAGE INSTALLED PLUG HPNGVN IN REF TO AMM 72-00-00-846-191-R02 VERIFIED INSTALLATION OF PLUG HPNGVN IN REF TO AMM 72-00-00-846-191-R02SDR QEMY20260224001Case · crackedHPT STATOR CASE, THE SUBJECT HPT STATOR CASE HAS A CRACK FOUND TO THE BORESCOPE BOSS MEASURING APPROX. 0.600” IN LENGTH, REF SUBTASK 72-51-01-220-068. DR 02299847 STATES THE HPT CASE HAS BEEN SHIPPED TO THE FAILURE ANALYSIS LAB. TO BE REPORTED IAW AMC-20 8A SDR 2026F00012Turbine Blades · damagedTHE FLIGHT-CREW HAD NOTICED SMOKE IN THE CABIN, WHICH THEY ISOLATED TO THE NR 1 ENGINE, PROMPTING IN-FLIGHT SHUTDOWN OF ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. POST-FLIGHT INSPECTION REVEALED NO OIL VISIBLE IN THE NR 1 ENGINE’S OIL LEVEL SIGHT-GLASS. SUPPSDR CALA2026021013659Stator · damagedON CLIMB OUT ENG 1 VIBE IND 4.3. TOMC CONTACTED.RETURN TO KDEN. AT CRUSIE VIB CAME DOWN TO 1.8- 2.3 PER CREW FOUND DAMAGE TO TURBINE BLDS LABOR HOURS UPDATE. PICTURES INCLUDED PICTURES INCLUDED. PICTURES INCLUDED. DUE DAMAGE TO AFT STAGE 4 ATP BLADE STATOR DAMSDR 2026F00008Turbine Blades · damagedINDIA-BASED SERVICE CENTER (AIRWORKS INDIA ENGINEERING PVT) ENGINEER CONTACTED WILLIAMS INTERNATIONAL (W.I.) OEM PRODUCT SUPPORT TO REPORT A POST-FLIGHT FINDING OF AN OIL LEAK IN THE HOT-SECTION AREA OF THE ENGINE. THE OBSERVED OIL LEVEL IN THE ENGINE SIGHT-GSDR Z3EY202601250001Rotor · damagedDURING ENGINE SHOP VISIT LPT DISASSEMBLY (STAGE 7 ROTOR REMOVAL), THE LPT STAGE 7 AIR SEAL WAS FOUND PARTIALLY LIBERATED.SDR 2026FA0000014Blade · brokenCREW HEARD A LOUD POP AND #1 ENGINE VIBRATION WENT INTO YELLOW ON INDICATOR. CREW SHUT DOWN ENGINE WITH NO FURTHER INCIDENT. HAD ENGINE BORESCOPED AND FOUND A HPT 2 BLADE HAD BROKENSDR SWAA2026011356284Support Bracket · crackedNR 1 ENGINE COOLING TUBE SUPPORT BRACKETS ARE CRACKED AT 03:00; 10:00; AND 09:00. REMOVED NR 1 ENGINE COOLING TUBE SUPPORT BRACKETS IAW SRM 51-40-02-0G-0. INSTALLED REPAIRED NR 1 ENGINE COOLING TUBE SUPPORT BRACKETS (LPTACC) IAW AMM 75-24-03, PARAGRAPH 3, SDR 2025FA0000834Hp Turbine · crackedRH ENGINE HAS EVIDENCE OF AXIAL CRACKING ON HPT STAGE 1 BLADES (4 TOTAL BLADES).SDR QEMY20251120001Seal · failedSEAL-ROTATING AIR HPT FRONT (FOS) THE SUBJECT FOS HAS FAILED FPI FOR CRACKS ON DIM E SEAL TEETH. FPI INDICATION "1 OFF CRACK 0.06" IN LENGTH GOING OVER INNER SEAL TEETH. 3 OTHER INDICATIONS ALSO OBSERVED; 0.04", 0.025", 0.015".
DR 02298827 WAS REJECTED BY TSDR 2025F00251Blades · fracturedFLIGHT AR1526, CREW REPORTED FEELING A LOUD EXPLOSION AND SEVERE VIBRATION IN THE AIRCRAFT, IN ENGINE NUMBER 1. AFTER ARRIVAL, THE ENGINE WAS INSPECTED WITH THE FOLLOWING RESULTS: EXTERNAL VISUAL INSPECTION REVEALED DAMAGE TO THE LPT STG 4 BLADES. THERE WAS SDR 2025FA0000669Module · making metalAFTER LANDING, THE PILOT IDENTIFIED AN ABNORMAL SOUND FROM THE REAR PORTION OF THE ENGINE. THE PILOT RECORDED A VIDEO TO CAPTURE THE SOUND. AFTER THE ROTOR STOPPED SPINNING, THE PILOT CALLED MAINTENANCE TO INVESTIGATE. THE REDUCTION GEAR CHIP PLUG WAS CHECKED,SDR QEMY20250911001Turbine Wheel · failedTHE SUBJECT LIFE LIMITED STAGE 1 DISK (P/N: 1865M13G08 S/N: GWN13G35) HAS FAILED SNR INSPECTION IN AREA A BY EXCEEDING MANUAL LIMITS ON GE90-100 ESM 72-53-02 SP008. THE INDICATION IS 0.770 INCH DEEP INTO THE DISK.
DR #02244037 WAS REJECTED BY THE OEM. THE CONSDR 6CBA2025090725001Turbine Blades · brokenDURING A ROUTINE TAKEOFF AT KLUK, THE CREW REPORTED: DURING T/O AT 12 PSI HEARD BANG / (NP) WENT BELOW 1000 / BLACK SMOKE CAME OUT THE RIGHT EXHAUST STACK & AMBER ENGINE NP (CAS) DISPLAYED. THE CREW REPORTS THEY SHUT THE ENGINE DOWN AND IT DID NOT SEIZE AFTER SDR QEMY20250903001Seal · dentedDURING INCOMING INSPECTION AT GE WALES, DEFECTS ON THE INTERSTAGE SEAL HAVE BEEN NOTED. THE INTERSTAGE SEAL HAS 6 DENTS TO 5 CROSSOVER PAD HOLE EDGES. DR # 02214321 WAS REJECTED BY THE OEM AS THE CONDITION COULD NOT BE SUBSTANTIATED. PLEASE NOTE, THE PART WISDR QEMY20250901001Hp Turbine · dentedDURING INCOMING INSPECTION AT GE WALES, DEFECTS ON THE HPT STAGE 2 DISK HAVE BEEN NOTED. CONDITION 1: THE HPT STAGE 2 DISK HAS 1 OFF NICK TO THE INTERSTAGE SEAL INTERFACE INBOARD OF THE DOVETAIL FORWARD END FACE. IT IS ADJACENT TO DOVETAIL #18. THE NICK MEASUR
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