JASC 7250

Service difficulty reports · 3,624

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.

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 WISep 3, 2025 · N446L · Boeing 777*SDR 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 MEASURAug 29, 2025 · Boeing 777*SDR DALA2026062603800Turbine Wheel · damagedDURING ROUTINE DISASSEMBLY TWO (2) FASTENERS WERE FOUND LIBERATED IN THE SAME FASHION AS NOTED IN THE QUALITY ALERT. DAMAGE WAS SUBSEQUENTLY OBSERVED ON (BUT NOT LIMITED TO) THE HPT DISK, IPT DISK, IPT SHAFT, LPT DISKS STAGES 1 THROUGH 4 AND THE LPT SHAFT. TAug 4, 2025 · N417DX · Airbus A330941SDR JR2R20250719908Case · corroded#1 ENGINE CONTAINMENT CASE FLANGE HAS CORROSION ON LOWER THREE BOLT HOLES.Jul 19, 2025 · N85355 · Emb ERJ170200LRSDR 2025FA0000506Blades · separatedON DESCENT THROUGH FL 130 THE CREW REPORTED THE LEFT ENGINE POWER ROLLED BACK FOLLOWED BY A LOUD POP SOUND.ALL INDICATION ON THE MFD ENGINE PARAMETERS INDICATED NORMAL. THE ENGINE WAS SECURED AND THE FLIGHT DIVERTED TO NORTH TEXAS REGIONAL AIRPORT (KGYI). FUJul 13, 2025 · N712RH · Beech 200BEECHSDR 2025FA0000410Shaft · galledHAESL REPORTED A CASE OF EARLY RETIREMENT OF LOW-PRESSURE TURBINE (LPT) SHAFT ASSEMBLY (PN: FK21827, SN: BBAP1275). GALLS WERE FOUND AT INNER SURFACE ZONE AG AND AE WHICH EXCEED LIMIT. THE DIMENSION OF GALLS AS BELOW: AG AREA 1: 2.611" L X 0.453" W X 0.0112"Jun 19, 2025 · N41482SDR QEMY20250528001Turbine · wornDURING INCOMING INSPECTION AT GE WALES, A DEFECT ON THE SEAL-ROATING AFT HPT HAS BEEN NOTED. THE HPT AFT ROTATING SEAL EXHIBITS WEAR TO THE SUMP SEAL TEETH X2 AND X3, WITH WEAR/BURRS/DISCOLORATION OVER AN ARC OF 7.120" FOR TOOTH X3, AND AN ARC OF 6.165" FOR TOMay 28, 2025 · N446L · Boeing 777SDR CALA2025053005133Blade · brokenRIGHT ENGINE, EGT LIMIT EXCEEDED, MAINT MSG 77-62122, VISUAL CHECKED RIGHT ENGINE EXHAUST LAST STAGE TURBINE BLADE BROKEN.May 26, 2025 · N793UA · Boeing 777222SDR PCSA20250416001Turbine · damagedLEFT ENGINE FAILURE DURING FLIGHT. AFTER INSPECTION FOUND HOT SECTION DAMAGE.Apr 16, 2025 · N396CM · Boeing 767323SDR 2025FA0000230Seal · wornDURING INCOMING INSPECTION AT GE WALES, A DEFECT ON THE SEAL-INTERSTAGE HPT ROTOR (HPTR) HAS BEEN NOTED. THE HPTR INTERSTAGE SEAL EXHIBITS 1 AREA OF WEAR (CONSISTING OF 5 INDIVIDUAL SPOTS OF WEAR, GROUPED INTO 4 LOCATIONS) TO THE FILLET BETWEEN THE STG 2 DISK Apr 2, 2025 · N446LSDR QEMY2025040200229Case · crackedDURING INCOMING INSPECTION AT GE WALES, A DEFECT ON THE HIGH PRESSURE TURBINE (HPT) CASE HAS BEEN NOTED. CRACKS HAVE BEEN OBSERVED ON THE HPT CASE DURING SB 72-1197. THE CRACKS WERE NOT VISIBLE UNDER WHITE LIGHT ONLY BUT WERE OBSERVED DURING FPI INSPECTION. THApr 2, 2025 · N446LSDR 2025FA0000148Bolt · mismanufacturedWE HAVE BEEN INFORMED OF POTENTIAL INCORRECT CONFIGURATION INCORPORATED DURING SHOP MAINTENANCE ACTIVITY IN LEAP-1A FLEET. WE ARE CONFIRMING THAT WE ARE CONCERNED OF INCORRECT CONFIGURATION WHERE PRE-SB 72-0175 BOLT(S) P/N (649-778-537-0) WERE INSTALLED ON POMar 3, 2025SDR SWAA2025020491670Angle · crackedRIGHT ENGINE; LPT COOLING TUBE SUPPORT ANGLE BRACKET CRACKED 4OCLOCK POSITION <[01]. REMOVED AND REPLACED CRACKED LPT COOLING TUBE SUPPORT ANGLE BRACKET AT 4 O?CLOCK POSITION IAW SIP.Jan 31, 2025 · N7866A · Boeing 7377Q8SDR SWAA2025020391278Angle · crackedL/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 11:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] R/R L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET AT 11 O?CLOCK POSITION REF AMM 20-50-11.Jan 29, 2025 · N961WN · Boeing 7377H4SDR SWAA2025020391275Angle · crackedL/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 10:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] R/R L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET AT 10 O?CLOCK POSITION REF AMM 20-50-11.Jan 29, 2025 · N961WN · Boeing 7377H4SDR SWAA2025020391277Angle · crackedL/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 9:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] R/R L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET AT 9 O?CLOCK POSITION REF AMM 20-50-11.Jan 29, 2025 · N961WN · Boeing 7377H4SDR SWAA2025020391274Angle · crackedL/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 6:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] REMOVED AND REPLACED #1 ENG LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 6:00 O?CLOCK POSITION PER AMM 70-20-02.Jan 29, 2025 · N961WN · Boeing 7377H4SDR SWAA2025020391273Angle · crackedL/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 5:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] REPLACED L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 5:00 O?CLOCK POSITION; FORWARD FLANGE PER AMM 2Jan 29, 2025 · N961WN · Boeing 7377H4SDR SWAA2025020391276Angle · crackedL/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 4:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] REPLACED L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 4:00 O?CLOCK POSITION; FORWARD FLANGE PER AMM 2Jan 29, 2025 · N961WN · Boeing 7377H4SDR YENA2025012700104Blade · damagedFLT#20, LHR-JFK. (ETOPS) 'FOUND (2) ENG #2 FAN BLADES CRACKED; REFER TO LOG PAGES 4185631, ITEM 1 (REMOVED AND REPLACED FAN BLADE #14 ON ENG #2 PER AMM 72-11-03. S/N: LBDUB15815. OPS CHECKS TRANSFERRED TO L/P 4185632-1) AND ITEM 2 (REMOVED AND REPLACED FAN BLAJan 25, 2025 · N4064J · Airbus A321271NXSDR YENA2025011000034Engine · abnormalFLT1088, LAX-BOS. (ETOPS) '#2 ENG REQUIRED REMOVAL AND REPLACEMENT; #2 ENGINE REPLACED UNDER W/O 1384579 DUE TO #3 BEARING FWD SEAL FULLY WORN. THE ENGINE REPLACEMENT CAME AT THE RECOMMENDATION OF P&W & POWERPLANT ENGINEERING. A/C OK FOR SVC.Jan 6, 2025 · N2193J · Airbus A321271NXSDR YENA2024120401525Engine · failedFLT#524, LAX-JFK. '(ETOPS) 'FOUND OIL IN #1 ENGINE TURBINE EXHAUST; REMOVE & REPLACED #1 ENGINE REF WO 1377333 T/C A320-71-00-51-400-802A OK FOR CONT. SVC.'Dec 2, 2024 · N4048J · Airbus A321271NXSDR UIEA2024112201101Bearing · cokedENGINE 1, BEARING #5, LH/RH SUMP PIPES WITH LEAK EVIDENCE.(<P>DURING VISUAL EXAMINATION, OIL COKE BUILD-UP WAS FOUND, COKING WAS REMOVED AND NO OIL LEAK WAS FOUND IN LH/RH SUMP PIPES IAW AMM SUBTASK 72- 50-00-216-032-H00 REV. 143 DATE: 22 AUG 2024. C/W IDLE LENov 27, 2024 · N1997A · Boeing 76733ASDR YENA2024111801485Unknown · abnormalFLT#2288, JFK-AMS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'FLIGHT ATTENDANT DETECTED A STRONG AIRFRAME VIBRATION ON CLIMB OUT OFF DUTY PILOT CONFIRMED UNUSUAL NATURE OF VIBRATION NO DOORS OR PANELS INDICATED ABNORMAL PRESSURIZATION NORMAL THROUGH LEVEL ONov 17, 2024 · N4064J · Airbus A321271NXSDR 2024F00271Turbine Blades · damagedFLIGHT CREW CONTACTED WILLIAMS INTERNATIONAL (W.I.) OEM PRODUCT SUPPORT TO REPORT A VIBRATION ISSUE ON THE LEFT-HAND ENGINE INSTALLED ON THE AIRCRAFT. W.I. PRODUCT SUPPORT RECOMMENDED A VIBRATION SURVEY. AN AUTHORIZED SERVICE FACILITY COMPLETED THE VIBRATIONNov 1, 2024 · N125DG · Cessna 525BSDR 2024F00270Turbine Blades · damagedFLIGHT CREW CONTACTED WILLIAMS INTERNATIONAL (W.I.) OEM PRODUCT SUPPORT TO REPORT A VIBRATION ISSUE ON THE LEFT-HAND ENGINE INSTALLED ON THE AIRCRAFT. W.I. PRODUCT SUPPORT RECOMMENDED A VIBRATION SURVEY. AN AUTHORIZED SERVICE FACILITY COMPLETED THE VIBRATIONNov 1, 2024 · N125DG · Cessna 525BSDR QEMY20241004001Hp Turbine · damagedDURING THE INSPECTION PROCESS AT GE WALES, A DEFECT ON THE DISK HPT STG 2 HAS BEEN NOTED. SURFACE DT HAS INDENTATIONS (360°) CAUSED BY THE MATING OF THE STAGE 1 DISK. THIS IS A KNOWN FIELD CONDITION. DR #01996080 REJECTED BY THE OEM. 1ST TIME EXPOSURE OF THIS Oct 4, 2024 · Boeing 777*SDR FDEA202409251357Rail · failedON CLIMB OUT, PASSING 5K FEET, LEVEL 3, ENGINE 2 FIRE ALERTS WITH ALL LIGHTS, MASTER WARNING AND FIRE BELL. PHASE 1 COMPLETED. AFTER A FEW SECONDS LEVEL 3 ALERTS WENT AWAY AND LEVEL 1, FIRE DET 2 FAULT CAME ON. CONTINUED WITH QRH AND ENGINE SHUTDOWN PRSep 25, 2024 · N592FE · Doug MD11FSDR YENA2024090301199Seal · leakingFLT#128, MCO-EWR. STRONG ACRIT/METALLIC SMELL NOTED WHILE DESCENDING THROUGH 17,000 FT. PLEASE SEE ATTACHED FORM MX-270; FOLLOW INFO NOTICED 2017-T15K AND BY TSM 05-50-00-810-813-A. FOUND ENG #1 BEING THE SOURCE OF THE SMELL. INSPECTED ENG #1 AND FOUND OIL ON Aug 30, 2024 · N705JB · Airbus A320232SDR QEMY20240905001Hp Turbine · damagedINCOMING CONDITION HIGHLIGHTED IN THE INSPECTION PROCESS. THERE IS LOCALISED PITTING ON AREA UC3 BETWEEN DOVETAIL POST 26 AND 27. THE PITTING ENCROACHES PAST THE BREAKPOINT INTO THE FORWARD MIDDLE RADIAL RABBET. DR# 02035694 REJECTED. TO BE REPORTED IN LINE WIAug 29, 2024 · N446L · Boeing 777*SDR NACA2024082500001Turbine Case · crackedFOUND NR 2 ENGINE LPT CASE MANIFOLD CRACK AT 5 OCLOCK. REMOVED AND REPLACED #2 ENGINE LPT CASE MANIFOLD IAW AMM 75-29-03Aug 25, 2024 · N399CM · Boeing 767323SDR ASAA2024082552119Turbine · low pressureCLIMBING OUT OF 7,000, EXPERIENCED #1 ENGINE FAILURE: SUSPECT DAMAGE (NO FUEL FLOW N2 ROTATION) , QRC,QRH: S/E APPROACH AND LANDING. GROUNDED - YES. AIR TURNBACK - MIG-2C #40-0056987 INITIATED. THRU #40-0056989. PERFORMED CONDITIONAL INSPECTION REF AMM 05-51-5Aug 25, 2024 · N613AS · Boeing 737790SDR QEMY20240829001Turbine Wheel · failed inspTHE HPT STAGE 1 DISK HAS BEEN REMOVED FROM SERVICE EARLY DUE FAILED ULTRASONIC INSPECTION FOR SIGNAL NOISE RATIO IAW SP008. DR  #02018991 WAS REJECTED BY OEM. TO BE REPORTED IN LINE WITH MANDATORY REPORTING REQUIREMENT PART 145 AMC 20-8A 9.3.(J) ANY DEFECT INAug 15, 2024 · N446L · Boeing 777*SDR 2024FA0000588Engine · faultedMTU RECOGNIZED THAT CERTAIN OVERTEMPERATURE INSPECTIONS WERE NOT PERFORMED ON ESN 690328 IN THE PAST. THIS WAS NOTICED BECAUSE THE WORKSCOPE OF ESN 690328 WAS USED AS A REFERENCE DURING WORKSCOPE PREPARATION FOR ANOTHER ENGINE WHICH SUFFERED EGT OVERTEMPERATURAug 8, 2024SDR 2024FA0000547Bolt · undertorquedENGINE SERIAL NUMBER 599634 HAS BEEN INDUCTED AT SAE SQY SHOP FOR A SCHEDULED SHOP VISIT. DURING ENGINE DISASSEMBLY THE MECHANICS DISCOVERED A LACK OF TIGHTENING TORQUE OF THE BOLTS SITUATED INSIDE OF THE COMBUSTOR DIFFUSER NOZZLE ASSY. THIS MODULE IS PART OFJul 23, 2024SDR YENA2024071901012Engine · bird ingestionFLT#31, BOS-AMS. (ETOPS) 'AFTER LANDING AT THE GATE LOCAL MTC INFORMED US OF BIRD STRIKE ON #2 ENGINE; PERFORMED BIRD STRIKE INSPECTION OF BOTH THE AIRFRAME AND ENGINES IAW AMM 05-51-14-200-803-A & 05-51-19-200-001-A RESPECTIVELY. FOUND DAMAGE TO FOUR (4) OGV Jul 13, 2024 · N4077J · Airbus A321271NXSDR DALA2024071207046O-Ring · leakingSHIP 3225 DISC: AIRCRAFT HAS DIRTY SOCK SMELL. C/A: C/W AMDS W/C 7900-2001 UP TO STEP 4. (523380) R/R LPT SHAFT PLUG ORING ON NBR 2 ENG PER A320 AMM 72-55(7657010 FINISHED C/W AMDS W/C 7900-2001, AND 2100-2003. SMELL NO LONGER PRESENT. OK FOR SVC. (LP: 6130490Jul 9, 2024 · N325US · Airbus A320211SDR DALA2024070706832Blades · damagedSHIP 1812 - ATO - ABORTED TAKEOFF AT 150KTS DUE TO AN AIRCRAFT YAW AND SUDDEN ENGINE EGT EXCEEDANCE. LEFT ENGINE FOUND TO HAVE DAMAGE TO TURBINE BLADES. CORRECTIVE ACTION: ENGINE CHANGED. (6089112)Jul 3, 2024 · N836MH · Boeing 767432ERSDR 2024FA0000462Seal · damagedROLLS-ROYCE LEASING (ESN 11146) IS CURRENTLY IN ROLLS-ROYCE ENGINE OVERHAUL SERVICES. (RR EOS – DERBY) FOR SHOP VISIT. DURING STRIP, RR EOS FOUND OUT THAT SEVERAL SEAL. SEGMENTS AND THE IP CASE HAVE BEEN DAMAGED. THE ENGINE’S PREVIOUS SHOP VISIT WAS IN SAESL Jun 24, 2024SDR 20240612001Case · misrepairedGENX HIGH PRESSURE TURBINE (HPT) STATOR CASES THAT MAY HAVE A FORWARD FLANGE DIAMETER UNDER MINIMUM REQUIREMENTS. SPECIFICALLY, THE HPT STATOR CASES AT ISSUE HAVE FORWARD FLANGE DIAMETER MEASUREMENTS THAT ARE 0.009" UNDER THE MINIMUM LIMIT IN THE INSTRUCTIONS Jun 12, 2024 · Boeing 7878SDR 2024FA0000441Turbine Blades · wrong partTHE GENX-1B ENGINE WITH SERIAL NUMBER 956339, PROPERTY OF UNITED AIRLINES UNDERWENT MAINTENANCE AT GE. (EM4Y). OUR ENGINE RECORDS INDICATE THIS ENGINE WAS ASSEMBLED WITH 49EA. BLADES P/N 2305M35G12 (NEW MATERIAL) AND 13EA. BLADES P/N 2305M35G05 (REPAIRED MATERJun 11, 2024SDR QEMY20240624002Seal · crackedINCOMING CONDITION HIGHLIGHTED DURING THE INSPECTION PROCESS. THE HPTR FORWARD SEAL HAS BEEN REMOVED FROM SERVICE EARLY DUE TO RADIAL CRACKS AT 2 LOCATIONS ON THE OD SEAL SERRATION V3. KNOWN CONDITION. DR #01985853 WAS NOT APPROVED. FIRST TIME EXPOSURE OF THIMay 26, 2024 · Boeing 777*SDR QEMY20240617001Seal · deformedINCOMING CONDITION HIGHLIGHTED IN THE INSPECTIONPROCESS. THE FORWARD MIDDLE RABBET EXHIBITS A DENT WITH BULGING ONTO SURFACE SM AND THEREIS FRETTING TO SURFACE NJ. DR#01980345 REJECTED. FIRST TIME EXPOSURE OF THIS AREA FROMNEW MAKE. SERVICE RUN CONDITION, NOTMay 24, 2024 · N446L · Boeing 777*SDR YENA2024050300702Blade · damagedFLT#1926,LGW-BOS. (ETOPS) ' NO 2 ENG FAN BLADE 4 ABRASION AND DISCOLORATION ON TRAILING THIRD OF TIP APPARENT DELAMINATION OF VENEER ON BACK SIDE OF BLADE TIP; (RESOLVED ON W/O: 1330276 TASK CARD: NR-00001) PERFORMED FAN TRIM BALANCE OF #2 ENG IAW AMM 71-00-00May 2, 2024 · N2180J · Airbus A321271NXSDR YENA2024042200654Blade · failedFLT#1408, CDG-JFK. (ETOPS) FOUND NR 1 ENGINE FAN BLADE S/N JB1AEA1140 DAMAGED AND OUT OF LIMITS. REMOVED AND REPLACED NR 1 ENG FAN BLADE #8 IAW AMM 72-11-03. REF LP 3982379, ITEM #2 FOR REQUIRED ENG RUNS.Apr 21, 2024 · N4058J · Airbus A321271NSDR QEMY20240524001Seal · nickedON INCOMING INSPECTION, A NICK/SCRATCH HAS BEEN FOUND ON 1 OFF AIR HOLE AFT CHAMFER, MEASURING: CIRCUMFERENTIAL 0.018 RADIAL 0.005 AXIAL (DEPTH) 0.0009. IT WAS NOTED THAT A SHOT PEEN LAYER WAS PRESENT, INDICATING THE CONDITION HAD POTENTIALLY BEEN PREVIOUSLY RMar 19, 2024 · N446L · Boeing 777*SDR 7ORR2024031418598Blade · brokenDURING POST LEASE MAINTENANCE VISIT, A CUSTOMER REQUESTED BORESCOPE OF HPT STAGE 1 ROTOR BLADES WAS ACCOMPLISHED. DAMAGE WAS FOUND TO BE IN EXCESS OF SERVICEABLE LIMITS FOR HPT STAGE 1 ROTOR BLADES. UPON FURTHER EXAMINATION, SECONDARY DAMAGE WAS ALSO NOTED ONMar 14, 2024 · Bombdr BD7001A10SDR 2024FA0000137Shroud · missingDURING DISASSEMBLY PROCESS OF SM53, A NOTIFICATION OF NON CONFORMITY HAS BEEN RAISED BY MECHANIC REGARDING 14 EA SEALS PN 1873M84P01 THAT HAS BEEN FOUND TO BE MISSING ( REFER TO BELOW SCHEME) ENGINE HAS BEEN MAINTAINED IN SAESM BACK ON 2022 FOR FAN CASE REPLACFeb 9, 2024SDR YTRA202402020001Blades · separatedIN FLIGHT ENGINE SHUTDOWN. ON TEARDOWN INSPECTION IT WAS DISCOVERED THAT THE 1ST STAGE TURBINE WHEEL BLADES HAD SEPARATED FORM THE BODY OF THE WHEEL. SEE BLOCK 6 BELOW FOR DETAILED INFORMATION ON WHEEL.Jan 24, 2024 · N763MH · Skrsky S76ASDR HEFR202401160002Shaft · crackedTURBINE UNIT WAS RECEIVED FOR LOUD NOISE DURING IDLE AND BAD VIBRATIONS. DURING OVERHAUL INSPECTION THE PT OUTER SHAFT WAS IDENTIFIED WITH A CRITICAL ISSUE, A VISIBLE CRACK IN THE COMPONENT.Jan 16, 2024 · N812LH · Doug 600N
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