GE CF6-80A2

Service difficulty reports · 307

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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 engine_model_key = 'CF680A2'
  ORDER BY difficulty_date DESC"

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SDR HALA2014082700122Engine · hotDURING START, EGT FOR LT ENGINE REACHED 724 DEGREES. ACCOMPLISHED VISUAL INSPECTION OF NR 1 ENGINE AND NO DISCEPANCIES NOTED; TEMPERATURE NOTED IS WITHIN LIMITS IAW 71-00-00-862-020 STARTED AND RAN NR 1 ENGINE AND START TEMPERATURE WAS BELOW 750 DEGREES C. EAug 27, 2014 · N594HA · Boeing 767322 · Engine (Turbine/Turboprop)SDR HALA2014082700123Engine · hotDURING CLIMB, EGT REACHED 920 DEGREES, EVENT WAS UNDER 5 MINUTES, PERFORMED ENGINE INSPECTION IAW 71-00-00-212-161 AND NOTED NO DISCREPANCIES ON NR 1 ENGINE. NOTED TEMP IS WITHIN LIMITS AND OUTSIDE OF AREA 1 OR 2 IAW 71-00-00-862, FIG 211, MOC NOTIFIED AND Aug 27, 2014 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2014082700124Engine · hotDURING START, LT ENGINE EGT REACHED 724 DEGREES. ACCOMPLISHED VISUAL INSPECTION OF NR 1 ENGINE AND NO DISCRIPANCIES NOTED, TEMPERATURE NOTED IS WITHIN LIMITS IAW 71-00-00-862-020, STARTED AND RAN NR 1 ENGINE AND START TEMPERATURE WAS BELOW 750 DEGREES C. ENGAug 27, 2014 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2014050900063Oil System · leakingDUE TO DECREASING OIL QTY ON NR 1 ENGINE. REPLACED NR 1 ENGINE.May 9, 2014 · N597HA · Boeing 767332 · Turbine Engine Oil SystemSDR ABXA2014021114Case · corrodedFAN EXIT CASE INNER SKIN CORRODED AT NR 7 FAN FRAME STRUT. BLENDED AREA IAW GECF6-80A ESM 70-42-00. REPAIRED AREA IAW ABX AIR REA-C072- 60864 RFTS NR E-46177 REVISION DATE 2-11-14. SDR INFO PN 9295M34G15, SN 3HY20080, AFT FAN CASE, CORRODED, RT, NAC 160.0. Feb 11, 2014 · N745AX · Boeing 767232 · Turbine Engine Compressor SectionSDR HALA2013110100162Engine · bird ingestionNR 2 ENGINE BIRD INGESTION PLUS RT WING MAIN FLAP, INBD T/E FLAP, BIRD STRIKE DAMAGE. INSTALLED NR 2 ENG IAW M1139-767. OPS AND LEAK CHECK GOOD.Nov 1, 2013 · N597HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2013100400128Pmc · malfunctionedDURING SHORT FINAL, EICAS MESSAGE RT EEC AND AUTO THROTTLE DISCONNECT ILLUMINATED. R & R RT ENG PMC. OPS NORMAL IAW AMM73-21-07. R & R RT ENGINE T12 SENSOR, IAW AMM 73-21-10.Oct 4, 2013 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR ABXA20130813521Support Fitting · crackedRIGHT WING REAR SPAR FITTING AT WS 700, A SUPPORT FITTING FOR THE NR 11 SPOILER AND THE FLAP DRIVE TORQUE TUBE, AFT SUPPORT LEG IS CRACKED IN HALF. R & R NR 11 SPOILER INBD SUPPORT FITTING IAW SRM 51-40-02. PN: 113T1566-26, NSN, FITTING, CRACK 1.5", RIGHT WINAug 13, 2013 · N742AX · Boeing 767232 · Wing Miscellaneous StructureSDR HALA2013040700034Pressure Switch · failedAIR TURN BACK, RT OIL FILTER ANNUNCIATOR CAME ON IN CLIMB. FOLLOWED SHUTDOWN PROCEDURE RETURNED TO DEPARTURE. REPLACED SCAVANGE OIL FILTER ELEMENT AND OIL PRESSURE DIFFERENTIAL PRESSURE SWITCH IAW FIM TASK 79-35 FAULT TREE 803. LEAK CHECK OPS CHECK PENDINGApr 7, 2013 · N594HA · Boeing 767332 · Turbine Engine Oil SystemSDR HALA2012121000233Engine · hung startLEFT ENGINE HUNG START, N1 18.37. EGT 740. N2 56.47 F/F 1,200. REPLACED LT ENGINE MEC & LEAK CHECKED IAW AMM 73-21-01. REPLACED LT ENGINE T2 SENSOR IAW AMM 73-21-05. REPLACED CIT SENSOR. COMPLIED WITH ALL COMPONENT REPLACEMENT TESTS IAW AMM 71-00-00 TESTS Dec 10, 2012 · N596HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR IXXA20121011030OSpinner · damagedDURING TAKEOFF ROLL, THE ACFT HAD A VIBRATION ON THE RT ENGINE (BIRD STRIKE) AND THE CREW REJECTED TAKE OFF AT 100 KTS. THE ACFT RETURNED BACK TO THE GATE WHERE MX PERSONNEL PERFORMED A HIGH ENERGY STOP INSPECTION IAW AMM 5-51-14. FURTHER INSP OF THE RT ENGINOct 11, 2012 · N763CX · Boeing 767232 · Turbine Engine Air Inlet SectionSDR IXXA20120919026OO-Ring · failedDURING CRUISE, CENTER HYD QUANTITY DECREASED TO ZERO AND SYS PRESSURE AND (RSVR,QTY) LIGHTS ON. EICAS MESSAGE: CENTER HYD SYS PRESSURE AND CENTER HYD QUANTITY DISPLAYED. INFLIGHT EMERGENCY WAS DECLARED PRIOR TO LANDING. UPON INSPECTION FOUND RT WING NR 2 Sep 19, 2012 · N762CX · Boeing 767232 · Hydraulic System, MainSDR HALA2012091700209Circuit Card · malfunctionedON GROUND TAXI WITH BOTH ENGINES ON LT ENGINE N1 23, RT ENG N1 36.6 ALSO RT ENGINE EGT IS LOWER THAN LT. IAW AMM 73-32-06 FLIGHT GROUND IDLE SOLENOID CHECK NR 28 VDC AT SOLENOID REPLACED EEC DISCRETE CIRCUIT CARD IAW AMM 73 -2-12 MCDP TETS 52 TMC RLY SW IS GOSep 17, 2012 · N597HA · Boeing 767332 · Engine Fuel and ControlSDR IXXA20120911025OCircuit Breaker · failedAFTER TAKEOFF AIRCREW RECEIVED 2 EICAS MESSAGES. RT FORWARD FUEL PUMP FAULT AND LT AFT FUEL PUMP FAULT. RETURNED TO STATION. R & R RT FWD/ LT AFT CIRCUIT BREAKER M16 IAW WDM 28-22-11. OPS CHECKED GOOD.Sep 11, 2012 · N763CX · Boeing 767232 · AC Power Distribution SystemSDR HALA2012082000193Fire Detector · malfunctionedEICAS MESSAGE "RT ENG FIRE LP 2" APPEARED IN STATUS PAGE AFTER T/O UP TO 16,000' AGL, MESSAGE CLEARED ITSELF. CLEANED NR2 ENG FIRE DETECTOR CONNECTORS IAW AMM 26-11-02. INSPECTED NR 2 ENG DUCTS IAW FIM 26-11-00 FAULT TREE 804. NO FAULTS NOTED. PERFORMED GRAug 20, 2012 · N594HA · Boeing 767332 · Fire DetectionSDR IXXA20120808020OSensor · failedRIGHT ENGINE OIL TEMP HIGH, 185-200 DEGREES, OIL PRESSURE NORMAL AT 60. ENGINE WAS SHUTDOWN. PERFORMED FIM PROCEDURE 79-34 FAULT TREE 804 BLOCK 1. R & R OIL TEMP BULB IAW MM 79-34-01. CLEANED & RESECURED BACKSHELL. OPS AND LEAK CHECKED GOOD ON ENGINE RUN. Aug 8, 2012 · N763CX · Boeing 767232 · Engine Oil TemperatureSDR HALA2012080500190Circuit Card · faultyRIGHT FIRE LOOP MESSAGE DISPLAYED DURING CLIMB OUT AT APPROXIMATELY 9,200 FT, WENT OUT ON ITS OWN AT 24,000 FT. R & R PRINTED CIRCUIT CARD IAW AMM 26-10-01. ENGINE RUN OPS CHECKED OK ON GROUND. OK FOR SERVICE. ACCOMPLISHED FIM 26-11. FAULT TREE 804 WIRINAug 5, 2012 · N594HA · Boeing 767332 · Fire DetectionSDR HALA2012080400191Fire Warning · false activationRIGHT FIRE LOOP NR 2, MESSAGE DISPLAYED ON CLIMB OUT FROM 8000'-16000'. WENT OUT ON IT'S OWN. ALL OTHER INDICATIONS NORMAL. TROUBLESHOOTING FOUND TWO CLAMPS ON INTERMEDIATE BLEED AIR DUCT AND CHECK VALVE LOOSE. ALSO FOUND ONE CLAMP ON TURBINE CASE COOLING Aug 4, 2012 · N594HA · Boeing 767332 · Fire DetectionSDR IXXA20120830019OProximity Sensor · out of adjustDURING TAKEOFF ROLL, RT ENGINE THRUST REVERSE AMBER LIGHT REMAINED ON AFTER FORWARD THRUST WAS SELECTED. THRUST LEVERS WERE ADVANCED AND CREW REJECTED TAKEOFF AT 30 KTS. PERFORMED HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. ADJUSTED LT CENTER THRUST REVERAug 3, 2012 · N762CX · Boeing 767232 · Engine Thrust ReverserSDR HALA2012072700184Ground Stud · arcedETOPS SIGNIFICANT SYS - UPON APU START, ARCING WAS NOTICED AT APU BATTERY GROUNDING STUDS/LUGS. REPLACED GROUND LUG IAW SWPM 20-30-11. R & R APU BATTERY GROUND BRACKET AND STUD ASSY SECURITY CK GOOD.Jul 27, 2012 · N598HA · Boeing 767332 · APU System WiringSDR HALA2012072700185Terminal · shortedETOPS SIGNIFICANT SYSTEM, UPON APU START, ARCING WAS NOTICED AT APU BATTERY GROUNDING STUDS/LUGS. REPLACED GROUND LUG IAW SWPM 20-30-11. R & R APU BATTERY GROUND BRACKET AND STUD ASSY, SECURITY CHECKED GOOD.Jul 27, 2012 · N598HA · Boeing 767332 · Electrical Power System WiringSDR HALA2012072400180Engine · power lossON INITIAL THROTTLE UP FOR TAKE OFF PUSHED THROTTLES UP TO APPROX 23 PERCENT N1 RT ENG SPOOLED UP NORMAL, LEFT ENG LAGGED APPROX 2-3 SECONDS BEFORE SPOOLING UP FOR NORMAL THROTTLE POSITION. ACCOMPLISHED TEST NR 4 - GROUND TEST FOR TAKEOFF POWER, ACCELERATION Jul 24, 2012 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2012071700175Warning Light · false activationAFTER RT ENGINE START, RT GENERATOR OFF EICAS. RESET IAW QRH. RAN RT ENGINE, GENERATOR OPERATED NORMALLY. OK FOR SERVICE.Jul 17, 2012 · N594HA · Boeing 767332 · AC Generator-AlternatorSDR HALA2012060300156Blade · damagedNR 2 ENGINE BOROSCOPE INDICATES ENGINE DAMAGED. FOUND FIRST STAGE HPT BLADES DAMAGED BEYOND AMM LIMITS. CHANGED NR 2 ENGINE. LEAK CHECK & OPS CHECK GOOD. OK FOR SERVICE.Jun 3, 2012 · N598HA · Boeing 767332 · Turbine Engine Compressor SectionSDR HALA2012052200144Fuel Filter · warning lightDURING CLIMB, AFTER 1000 FT AGL. EICAS DISPLAY RT ENGINE FUEL FILTER. R & R RT ENGINE FUEL FILTER IAW AMM73-11-02 ENG RUN. OPS & LEAK CHECKED GOOD, OK FOR SERVICE.May 22, 2012 · N598HA · Boeing 767332 · Engine Fuel DistributionSDR HALA2012011600028Eec · malfunctionedETOPS SIGNIFICANT SYS - AFTER ENGINE START, RIGHT EEC INOPERATIVE, LIGHT ILLUMINATED. RESET RT EEC. PERFORMED ENGINE RUN. ALL OPS CHECKED GOOD.Jan 16, 2012 · N597HA · Boeing 767332 · Fuel Controlling SystemSDR HALA2011122900620Warning Light · false activationETOPS SIGNIFICANT SYS - BTB RT EEC EICAS. RT ENGINE EEC ON STARTUP. INFO NOTED. BITE EEC NO FAULTS NOTED. RAN ENGINES AT GATE, ALL OK IAW FIM 71 EEC MX MONITOR UNIT BITE PROCEDURE, FIG 104 ALL SYS OK.Dec 29, 2011 · N597HA · Boeing 767332 · Fuel Controlling SystemSDR HALA2011120500567Warning Light · false activationETOPS SIGNIFICANT SYS - DURING DESCENT THROTTLES AT IDLE. ENGINES INDICATIONS - LT ENGINE N1=33 & RT ENG =47, LT ENGINE TGT=253 & RT ENGINE = 321, LT ENGINE N2 = 65 & RT ENGINE = 79, LT ENGINE FF = .500 & RT ENGINE = 1.4. FROM TOP OF DESCENT (36000) TO 180000Dec 5, 2011 · N594HA · Boeing 767332 · Engine Indicating SystemSDR HALA2011120100558Filter · failedETOPS SIGNIFICANT SYS - AFTER ENGINE START, EICAS STATUS PAGE RT OIL FILTER. INSPECTED NR 2 ENGINE CHIP DETECTOR, NO DEFECTS. R & R RT ENGINE OIL FILTER ELEMENT, LEAK CHECKED NORMAL IAW AMM 79-21-04, OK FOR CONT SERVICE.Dec 1, 2011 · N594HA · Boeing 767332 · Turbine Engine Oil SystemSDR HALA2011114000517Blade · damagedETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK, FOUND NR 2 ENGINE, NR 33 BLADE FR. INDEX ON SPINNER HAS FOD DAMAGE. ACCOMPLISHED AMM 72-31-02, NR 2 ENGINE NR 33 BLADE FROM INDEX ON SPINNER.Nov 14, 2011 · N596HA · Boeing 767332 · Turbine Engine Compressor SectionSDR HALA2011111100516Blade · damagedETOPS SIGNIFICANT SYS - FOUND .2500 X .2500 BLADE DAMAGE ON NR 2 ENGINE FAN. IAW AMM 72-31-02-801 WITHIN LIMITS AREA B, 4" BELOW BLADE SHROUD. BLENDED IAW AMM 72-31-02-801. OK FOR SERVICE.Nov 11, 2011 · N596HA · Boeing 767332 · Turbine Engine Compressor SectionSDR ABXA20111107135Frame · crackedOUTBD CORE COWL DOUBLER CRACKED ON INSIDE NEAR EXHAUST DUCT. INSTALLED REPAIR DOUBLER IAW SRM 51-40-02 AND DRAWING 314T1210, WELDED REPAIRED DOUBLER IAW ABX PROCESS STANDARDS MANUAL CHAPTER 900-7 REV 49, AWG.Nov 7, 2011 · N742AX · Boeing 767232 · Engine Cowling SystemSDR IXXA1100730Sensor · malfunctionedLT ENGINE SHUTDOWN IN-FLIGHT DUE TO HIGH OIL TEMP - ENGINE OIL TEMP INDICATED 175 DEGREES CELSIUS, OIL PRESSURE WAS 58 PSI. MX R & R NR 1 ENGINE OIL TEMP BULB IAW MM 79-34-00, BLOCK 1 AND 79-34-99, FIG 101, PG 101 & 102, STEPS 1 THRU 10. VERIFED, ACFT RELEANov 2, 2011 · N761CX · Boeing 767223 · Engine Oil TemperatureSDR HALA2011101400461Engine · hung startETOPS SIGNIFICANT SYS - LT ENGINE HUNG START AT EGT 739 DEG; N2 53 PERCENT; FUEL FLOW 1500; OAT 14DEG C. ABORTED START, RESTARTED SUCCESSFUL. ACCOMPLISHED LT ENG START & IDLE RUN TEST 3 IAW AMM 71-00-00, ALL LT ENG PARAMETERS WITHIN LIMITS IAW AMM 71-00-00-8Oct 14, 2011 · N596HA · Boeing 7673G5 · Engine (Turbine/Turboprop)SDR HALA2011100700440Engine · failedETOPS SIGNIFICANT SYS - ON APPROACH, AT APPROX 2,400, FLAPS 20, STEADY THROTTLE POSITION, BOTH PILOTS HEARD A MUTED THUD OR BANG AND SHORTLY NOTICED THE LT ENGINE WAS NOT PRODUCING POWER, 21.7 PERCENT N1 AND 697 EGT. LANDED ON RT ENGINE. R & R LT ENGINE PER MOct 7, 2011 · N598HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR IXXA110061OFan · lack of lubeDURING TAKEOFF ROLL, THE LT ENGINE FAN VIBRATION 2.5. WHEN INFLIGHT AT 370 ENGINE VIBRATION IS 5.1. THE CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FAN LUBE IAW AMM 72-31-02. AFTER FAN LUBE ENGINE VIBRATION AT .9, WITH IN LIMITS IAW ERSep 21, 2011 · N763CX · Boeing 767232 · Turbine Engine Compressor SectionSDR HALA2011070600310Oil System · leakingETOPS SIGNIFICANT SYS - NR 1 ENG HAS OIL COMMING OUT OF "B" SUMP DRAIN. REPLACED NR 1 ENG IAW HAL M1139 OPS AND LEAK CHECK GOOD. OK FOR SERVICE.Jul 6, 2011 · N598HA · Boeing 767332 · Turbine Engine Oil SystemSDR HALA2011070500309Lamp · inoperativeETOPS SIGNIFICANT SYS - LT FWD FUEL PUMP PRESSURE LIGHT DOES NOT ILLUMINATE PUMP OFF, ALSO DOES NOT TEST. RELAMPED L FWD FUEL PUMP SWITCH, OPS CK OK.Jul 5, 2011 · N597HA · Boeing 767332 · Engine Fuel DistributionSDR HALA2011061800270None · noneETOPS SIGNIFICANT SYS - DURING OVERNIGHT INSP, FOUND NR 1 ENGINE FAN BLADE ABRADABLE SHROUD TO HAVE MATERAL GONE MEASURING .3125 AT 9 O'CLOCK POS. FOUND TO BE IN SERVICEABLE LIMITS IAW AMM 72-33-04-601. NO FUTHER ACTION IS REQUIRED.Jun 18, 2011 · N598HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2011061800271Shroud · noneETOPS SIGNIFICANT SYS - DURING OVERNIGHT CHECK FOUND NR2 ENGINE TO HAVE MATERIAL MISSING FROM ABRADABLE SHROUD 2 AREAS .3125 EA AT 12 O'CLOCK POS. FOUND TO BE WITH IN LIMITS IAW AMM 72-33-04-601. NO FUTHER ACTION IS REQUIRED.Jun 18, 2011 · N598HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2011050400180Shroud · damagedETOPS SIGNIFICANT SYS - FAN CASE SHROUD DAMAGED AT 7 O`CLOCK POSITION NR 1 ENG. REPAIRED FAN CASE SHROUD IAW AMM 72-34-01 AND HAL M105 594140. PERFORMED IDLE VIBRATION RUN M105 594140. OPS CK GOOD.May 4, 2011 · N594HA · Boeing 767332 · Turbine Engine Compressor SectionSDR HALA2011050400181Blades · damagedETOPS SIGNIFICANT SYS - ON OVERNIGHT NR 1 ENG FOUND NR 4, 5, 6, 7, 8, 9 AND 10 BLADES INBEDDED IN ACOUSTIC. REMOVED BLADES NR 4, 5, 6, 7, 8, 9 AND 10 IAW AMM 72-31-02. REPAIRED ACOUSTIC LINER IAW M105 594140. REINSTALLED FAN BLADES NBR 4,5,6,7,8,9 AND 10 IAW May 4, 2011 · N594HA · Boeing 767332 · Turbine Engine Compressor SectionSDR DALA1119280136Rib · crackedNR 1 ENGINE AFT FAN ASSY / AFT FAN CASE FWD RIB CRACKED AT 12 O'CLOCK POSITION DURING INSTALLATION. NR 1 ENGINE AFT FAN CASE CRACKED FWD T RIB REPAIRED IAW ER/A 488809-14 REV ORIGINAL.Mar 7, 2011 · N136DL · Boeing 767332 · Turbine Engine Compressor SectionSDR HALA2011020200080Floor Support · crackedPAX FLOOR STRUCTURE INTERCOSTAL AT STN 347, RBL 35 CRACKED ALONG UPPER RADIUS. REPLACEMENT OF UPPER CORD BY FABRICATION OF NEW PART PN 141T2200-7 IAW DWG 141T2200 AND SRM 51-40-02, REV 84.Feb 2, 2011 · N594HA · Boeing 767332 · Fuselage Miscellaneous StructureSDR HALA2011011300081Seat Track · corrodedLEVEL 2 CORROSION AT SEAT TRACK RGL 20, STA 348-434 CORROSION EXCEEDED OUT OF SRM LIMITS IAW SRM 53-00-52-1A, REV 84. SEAT TRACK, RBL 20 348-434 REPLACED IAW SRM 51-40-02, REV 84.Jan 13, 2011 · N594HA · Boeing 767332 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011010800019Turbine Blades · damagedOPEN - ETOPS SIGNIFICANT SYS - LT ENG BORESCOPE - FOD DAMAGE ON 11TH STAGE HPC BLADES. OK IAW M105 R0081. PERFORM BLENDING W/IN 5 CYCLES. OK FOR SERVICE.Jan 8, 2011 · N594HA · Boeing 767322 · Turbine SectionSDR HALA2011010800020Turbine Blades · nickedOPEN - ETOPS SIGNIFICANT SYS - LT ENGINE BORESCOPE - 12TH STAGE HPC HAS NUMEROUS NICKS - (BLADES). OK IAW M105 R0081. PERFORM BLENDING W/IN 5 CYCLES. OK FOR SVC.Jan 8, 2011 · N594HA · Boeing 767300 · Turbine SectionSDR HALA2011010800021Turbine Blades · nickedOPEN - ETOPS SIGNIFICANT SYS - LT ENG BORESCOPE - 13TH STAGE BLADES HAD NUMEROUS NICKS. OK IAW M105, R0081 PERFORM BLENDING W/IN 5 CYCLES. OK FOR SVC.Jan 8, 2011 · N594HA · Boeing 767332 · Turbine SectionSDR HALA2010121600590Controller · malfunctionedETOPS SIGNIFICANT SYS - AIR CONDITIONING SYS DRIVES TO FULL COLD IN AUTO, HAD TO TURN OFF TRIM AIR & OP PACKS MANUALLY. R & R LT PACK CONTROLLER IAW AMM TASK 21-51-14. NO FAULTS NOTED. OK TO CONTINUE.Dec 16, 2010 · N597HA · Boeing 767332 · Cabin Cooling SystemSDR HALA2010121400587Rib · crackedOPEN - ETOPS SIGNIFICANT SYS - CRACK MEASURING 8.5 INCHES FOUND ON AFT FAN CASE RIB AT 4:00 ON NR1 ENG SN 580320. REPAIR IN WORKDec 14, 2010 · N596HA · Boeing 767332 · Turbine Engine Compressor Section
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