JASC 7230

Service difficulty reports · 5,066

Reports filed under 7230 · Turbine Engine Compressor 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 = '7230'
  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 2005FA0001566Blade · debondedDURING ROUTINE ENGINE A-CHECK INSPECTION, FOUND 15 OUT OF 24 (CHOCKING PADS) ON BASE OF ENGINE FAN BLADE TO HAVE MIGRATED AFT OF NORMAL POSITION DUE TO DEBONDING OF (CHOCKING PAD). THIS CONDITION WAS CAUSING ABNORMAL ENGINE VIBRATION DURING ENGINE GROUND OPERNov 30, 2005 · N888CW · Gulstm GULFSTREAMGVSDR REXA200500141Compressor · failedPASSING THROUGH 2500 FT MSL ON CLIMBOUT FROM, THE FLIGHT CREW HEARD SEVERAL LOUD (BANGS) FROM THE RT ENGINE. THIS WAS FOLLOWED BY ERRATIC ENGINE INDICATIONS AND A REPORT FROM THE FLIGHT ATTENDANT OF A (BURNING SMELL) IN THE CABIN. THE FLIGHT CREW PERFORMED THENov 29, 2005 · N8588D · Cndair CL6002B19SDR CA051128001Turnbuckle · fractured(CAN) TO DATE, (3) CF34-3B1 STAGE 2 HPC TURNBUCKLES AFFECTING 2 ENG HAVE FAILED DURING SERVICE. SEPARATION OF VG SHAFT SIDE TURNBUCKLE ROD END. SEPARATION POINT ON ROD END OCCURRED IN THREADED PORTION WHERE IT MEETS JAM NUT ON TURNBUCKLE ASSY. CAUSE CONFIRMEDNov 25, 2005SDR AALA20050774Fan Blade · bird ingestionJFK - ON TAKEOFF FROM LGA TOOK BIRD INTO LEFT ENGINE. DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. PERFORMED BOROSCOPE AND REPLACED COMPLETE SET OF FAN BLADES. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 23, 2005 · N977AN · Boeing 737823SDR BB05100Compressor · stalledAFTER TAKEOFF, LEFT ENGINE COMPRESSOR STALL. REDUCED LEFT ENGINE THRUST TO IDLE AND RETURNED TO FIELD AMS. MAINTENANCE ACTION PENDING. (OPEN)Nov 22, 2005 · N656US · Boeing 767200SDR ARWA20051102Blades · damagedUPON ENGINE SPOOL UP FOR TAKEOFF, NR 4 ENGINE COMPRESSOR STALLED. PERFORMED BOROSCOPE TO NR 4 ENGINE; FOUND BLADES DAMAGED, SECURED NR 4 ENGINE FOR FERRY FLIGHT IN ACCORDANCE WITH ARROW GMM 6-3-4/5.Nov 17, 2005 · N661AV · Doug DC863FSDR SWAA053699Compressor · stalledAIR TURNBACK/DECLARED EMERGENCY, 2 LOUD BANGS HEARD, ALONG WITH MODERATE TO SEVERE VIBRATIONS FELT FROM NR 2 ENGINE. NR 2 ENGINE FUEL FLOW ERRATIC. ALL OTHER INDICATIONS NORMAL. FLAME SEEN FROM NR 2 ENGINE EXHAUST. REMOVED AND REPLACED NR 2 EEC, T12 SENSORNov 17, 2005 · N782SA · Boeing 7377H4SDR CA051223005Compressor · damagedDURING A MAINTENANCE CHECK FLIGHT, THE ENGINE EMITTED A LOUND NOISE ACCOMPANIED BY AN UNCOMMANDED POWER REDUCTION. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED DAMAGE TO THE COMPRESSOR AND INLET AREA. P&WC WILL INVESTIGATE THE EVENT ANNov 14, 2005 · Bell 212SDR CA051111001Engine · bird ingestion(CAN) EVIDENCE OF BIRD STRIKE AT FAN BLADES. NO SIGNS OF BIRD REMAINS OR DAMAGE ON CORE OF ENG FAN BLADES, LP/IP SPLITTER FAIRING, OGV'S AOHE AIR INLET IDG OIL COOLER INLET INSPECTED. (A) DUE TO ENG SURGE OUT OF AIRPORT ON 01/09/2005. BOROSCOPE INSPECTION CARRNov 11, 2005 · Airbus A330342SDR DXTA200501075Sense Line · leakingLEFT ENGINE FLAMED OUT (STOPPED RUNNING) APPROXIMATELY 7-10 MINUTES AFTER A NORMAL START. THROTTLE WAS AT IDLE AND HAD NOT BEEN MOVED. ADJUSTED FCU AND FDU LINKAGES PER PRATT & WHITNEY JT15D-5D MM CHAPTER 73-20-01. OPERATIONAL CHECK SATISFACTORY. FOUND COMNov 11, 2005 · N306QS · Cessna 560CESSNASDR LNX2006F00000Impeller · crackedRT ENGINE WAS UNABLE TO REACH TAKEOFF TARGET TORQUE. ENGINE WAS REMOVED AS A PRECAUTION AND SENT FOR TEARDOWN. ENGINEERING HAS DETERMINED CAUSE TO BE A CRACKED SECOND STAGE IMPELLER RESULTING FROM CYCLIC FATIGUE. THIS IS A FOLLOW UP REPORT AND IS NOW CLOSEDNov 8, 2005 · N438MA · Swrngn SA227ACSDR REXA200500134Guide Vane · brokenTHE AIRCRAFT DEPARTED, ON A FERRY FLIGHT TO THE MAINTENANCE BASE, DUE TO A MISSING RT THRUST REVERSER BLOCKER DOOR. AT FL230 AND 80 MILES OUT, THE RT ENGINE FLAMED OUT. THE FLIGHT CREW EXECUTED THE SINGLE ENGINE OPERATION PORTION OF THE QRH AND DECLARED AN EMENov 2, 2005 · N8751D · Cndair CL6002B19SDR 05134Guide Vane · brokenFLIGHT LEFT SBN ON A FERRY FLIGHT TO THE TYS MAINTENANCE BASE DUE TO A MISSING RIGHT HAND ENGINE THRUST REVERSER BLOCKER DOOR. AT FL230 AND 80 MILES OUT OF KNOXVILLE, THE RIGHT HAND ENGINE FLAMED OUT. THE FLIGHT CREW EXECUTED THE SINGLE ENGINE OPERATION QRH Nov 2, 2005 · N8751D · Cndair CL6002B19SDR CA051109001Compressor · damagedFOLLOWING A REPORT OF HIGHER THAN NORMAL TOT ON NR 2 ENGINE A POWER CHECK WAS CONDUCTED AND TROUBLESHOOTING LED TO SPLITTING THE COMPRESSOR FOR INSPECTION. SUBSTANTIAL DAMAGE WAS FOUND ON THE 5TH AND 6TH ROW STATOR VANES AND 6TH STAGE ROTOR BLADES. NO DAMAGEOct 29, 2005 · Bolkms BO105SSDR AT0500039Compressor · stalledINDICATIONS OF COMPRESSOR STALL FOLLOWED BY RED BOXED OIL PRESS LOW ON LEFT ENGINE. COMPLIED W/QRT AND SHUT DOWN LEFT ENGINE. REMOVED AND REPLACED LEFT ENGINE PER TASK CARD 603.Oct 28, 2005 · N985AT · Boeing 717200SDR ARWA20051004Compressor · stalledLOG PAGE NR 117333, DURING TAKEOFF, NR 2 ENGINE COMPRESSOR STALLED. PERFORM NR 2 ENGINE INLET AND EXHAUST SECTION INSPECTION FOR DAMAGE IAW M/M 71-00 AND PERFORMED OPERATIONAL RUN IAW M/M 71-00; FOUND ALL PARAMETERS IN LIMITS, COULD NOT DUPLICATE FAILURE. NOTOct 22, 2005 · N661AV · Doug DC863FSDR QXEA200501358Compressor · vibrationPDX - ON FLIGHT 2455 (PDX-SBA) 30 MINUTES OUT OF PORTLAND NR 2 ENGINE N1 FAN VIBRATIONS. FLIGHT RETURNED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. NO EMERGENCY DECLARED.Oct 18, 2005 · N610QX · Cndair CL6002C10SDR CA051017011Bearing · failed(CAN) SEE REPORT ATTACHEDOct 17, 2005SDR SWAA053190Blade · tornDURING SCHEDULED HC2 CHECK, NR 1 ENGINE FAILED BOROSCOPE INSP 2ND STAGE COMPRESSOR HAD TWO BLADES TORN AND SEVERAL BLADES HAD MATERIAL MISSING ON LEADING EDGES. REMOVED AND REPLACED NR 1 ENGINE PER MM.Oct 13, 2005 · N467WN · Boeing 7377H4SDR CA060211003Turnbuckle · separated(CAN) WHEN STARTING APPROACH, THROTTLES WERE PULLED BACK, A LOUD BANG WAS WITNESSED AND FELT IN A/C. ENG NR 1 STARTED TO LOSE POWER IMMEDIATELY, FOLLOWED BY LOW OIL PRESSURE WARNING. ITT ROSE UP TO 1230 DEG CELSIUS AND HIGH ENGINE VIBRATION WERE FELT. ENG WAOct 12, 2005 · Cndair CL6002B19SDR CA051014002Blades · damagedGII SERIAL 236 IN NR 1 POSITION HAS EXPERIENCED FOD DAMAGE. THE DAMAGE HAS BEEN FOUND TO THE LPC5 BLADES AND HPC1 BLADES. THE REST OF THE HP COMPRESSOR HAS YET TO BE INSPECTED. THE DAMAGE HAS BEEN CAUSED BY THE RELEASE OF ONE LP OGV INNER BOLT WASHER AND NUOct 12, 2005 · Gulstm G1159SDR CA060211004Blades · damaged(CAN) FLIGHT CREW REPORTED SEEING HIGH NR 1 ENGINE ITT > 900 DEG CELSIUS, TOGETHER WITH ENGINE VIBRATION. N1 STARTED TO SPOOL DOWN AND FLUCTUATING N2 WAS SEEN. CREW SHUTDOWN THE ENGINE AND RETURNED TO DEPARTURE. SUCCESSFUL SINGLE ENGINE LANDING WAS PERFORMED.Oct 11, 2005 · Cndair CL6002B19SDR 2005FA0001428Plenum · corrodedWHILE REMOVING THE ENGINE FOR A SCHEDULED OVERHAUL, WE NOTICED 5 RIVETS SHEARED OF THE TOP HALF OF THE INDUCTION AIR PLENUM BAND ASSY. A SHEARED RIVET HEAD CAN EASILY FIT THRU THE ENGINE INLET SCREEN AND COULD BE INGESTED BY THE ENGINE CAUSING GREAT DAMAGE OROct 10, 2005 · N701SE · Cessna 208BSDR 2005FA0001427Plenum · damagedWHILE REMOVING THE ENGINE FOR A SCHEDULED OVERHAUL, WE NOTICED 5 RIVETS SHEARED OFF THE TOP HALF OF THE INDUCTION AIR PLENUM BAND ASSEMBLY. A SHEARED RIVET HEAD CAN EASILY FIT THRU THE ENGINE INLET SCREEN AND COULD BE INGESTED BY THE ENGINE CAUSING GREAT DAMAOct 10, 2005 · N701SE · Cessna 208BSDR DL757050602Compressor · stalledNR 1 ENGINE COMPRESSOR STALL ON CLIMBOUT AT FL140. PULLED PWR BACK AND ENGINE INDS NORMAL. VISUALLY SAW SPARKS FROM TAILPIPE. DID NOT SHUT ENG DOWN. REPLACED ENGINE DUE TO INTERNAL DAMAGE.Oct 9, 2005 · N681DA · Boeing 757232SDR AWXA200501196Actuator · faultyDURING TAKEOFF, AT 70 KNOTS, RECEIVED NR 1 ENG COMPRESSOR VANE FAULT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VSV ACTUATOR IAW AMERICA WEST AIRLINES TASK CARD F5M71312. OPERATIOct 9, 2005 · N813AW · Airbus A319132SDR 2005FA0001392Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 160.5 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. WE SUSPECT THAT THE CAUSE OFOct 3, 2005SDR 2005FA0001391Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 160.5 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISK) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCOct 3, 2005SDR 2005FA0001390Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2824.2 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISK) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. WE SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABSOct 3, 2005SDR 2005FA0001389Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2824.2 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. WE SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABOct 3, 2005SDR 2005FA0001388Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2824.2 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISK) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOOct 3, 2005SDR 2005FA0001387Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2824.2 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOct 3, 2005SDR 2005FA0001385Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 1493.7 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. WE SUSPECT THAT THE CAUSE OOct 3, 2005SDR 2005FA0001384Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 1493.7 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISK) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. WE SUSPECT THAT THE CAUSE OFOct 3, 2005SDR 2005FA0001383Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 1493.7 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. WE SUSPECT THAT THE CAUSE OOct 3, 2005SDR 2005FA0001382Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 1493.7 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EOct 3, 2005SDR 2005FA0001381Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2824.2 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOct 3, 2005SDR 2005FA0001380Compressor · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2824.2 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOct 3, 2005SDR 2005FA0001379Compressor · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2824.2 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOct 3, 2005SDR 2005FA0001378Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2407.9 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. WE SUSPECT THAT THE CAUSE OOct 3, 2005SDR 2005FA0001377Compressor Wheel · corrodedTHESE PART WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2407.9 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXOct 3, 2005SDR 2005FA0001376Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2407.9 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPSRSSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EOct 3, 2005SDR 2005FA0001375Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2407.9 HOURS (PRIOR TO THE ENGINE TBO OF 3000 HOURS). THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EOct 3, 2005SDR 2005FA0001374Compressor Wheel · corrodedTHES PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2998.9 HOURS. THE FOLLOWING PART (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BE ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOT BEOct 3, 2005SDR 2005FA0001373Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2998.9 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOct 3, 2005SDR 2005FA0001372Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2997.3 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOct 3, 2005SDR 2005FA0001371Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2997.3 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THAT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOct 3, 2005SDR 2005FA0001370Compressor Wheel · corrodedTHESE PARTS WERE REMOVED FROM SERVICE AT ENGINE TSO OF 2997.3 HOURS. THE FOLLOWING PARTS (COMPRESSOR DISKS) WERE DEEMED SCRAP DUE TO NOT BEING ABLE TO READ PN AND/OR SN BECAUSE OF CORROSION. SUSPECT THE CAUSE OF EXCESSIVE CORROSION IS THE WINDAGE TABS NOT BEOct 3, 2005SDR ASMF200510003Blade · damagedDURING TRANSIT CHECK, DETECTED A BLADE DAMAGED, LT ENGINE LPC 1ST STAGE. THE BLADE WAS OUT OF LIMITS WITH A DAMAGE OF 4 X 0.750 AT LEADING EDGE. DURING OVERNIGHT CHECK, THE TWO BLADES SET OF LPC 1 ST STAGE WAS REPLACED IAW MM 72-31-02, VIBRATION TEST NR 8 WAOct 3, 2005 · N804AM · Boeing 7572Q8SDR ASAA0540516Compressor · contaminatedOKC - FOUND TAKEOFF ROLL POWER SET, COCKPIT FILLED WITH SMOKE. TAKEOFF ABORTED LESS THAN 45 KTS. REMOVED SMOKE FUMES FROM CABIN PER B737-400 AMM 21-00-01 AND AMM SUPPLEMENT 72-00-00. PARTIAL WORK ACCOMPLISHED ON MIG-2C 057320. ENGINE COMPRESSOR WASH PERFORSep 29, 2005 · N772AS · Boeing 7374Q8
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