IAE V2500-A1

Service difficulty reports · 306

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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 engine_model_key = 'V2500A1'
  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 AWXA200601767Wire · brokenFLIGHT 180; - DURING CLIMB OUT, THE CREW REPORTED THE LOSS OF AILERONS. ON MEL THE OPPOSITE SIDE FAULTED WHICH RESULTED IN THE REPORT OF THE (LOSS OF AILERONS). THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITH NO REPORT OF DIFFICULTIES CONTROLLINOct 13, 2006 · N621AW · Airbus A320232 · Flight Control System WiringSDR AWXA200601620Valve · faultyON APPROACH, THE CREW MADE 3 ATTEMPTS TO EXTEND THE GEAR WITH NO SUCCESS. IAW THE QRH, THE CREW PERFORMED A MANUAL GEAR EXTENSION. EXTENSION WAS SUCCESSFUL. AS A PRECAUTIONARY MEASURE, THE CREW PERFORMED A TOWER FLYBY. THE TOWER VERIFIED THAT THE GEAR WAS DOWNSep 13, 2006 · N647AW · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR AWXA200600809Eec · malfunctionedPHX - FLT 551 - CREW REPORTED, "ABOVE 10000 MSL IN CLIMB-OUT, GMT 227, ENGINE 2 STALL". ALSO REPORTED ENG 2 FADEC AND ENG 2 SENSOR FAULT. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED THE NR 2 ENGINE FOR EVIDENCE OF FOD, NONE May 13, 2006 · N626AW · Airbus A320231 · Fuel Control/Turbine EnginesSDR AWXA200600018Slide · faultyDURING OVERNIGHT INSPECTION THE L2 DOOR SLIDE FAILED STEP 5 OF THE 4-DAY TASK CARD. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR SLIDE IAW TASK CARD R1C25304.Jan 6, 2006 · N634AW · Airbus A320231 · Escape SlideSDR AWXA200600010Proximity Switch · unresponsivePILOT REPORTED THAT THE AIRCRAFT LT FORWARD ENTRY DOOR SLIDE WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR SLIDE ARM PROX SWITCHES, 4WN1 AND 13WV1 IAW AMM 52-73-11 AND AMM 52-71-11. OPERATIONAL CHECKS WERE GOOD.Jan 4, 2006 · N816AW · Airbus A319132 · Passenger/Crew DoorsSDR AWXA200600014Door Actuator · out of adjustDURING BC4 CHECK DISCOVERED THE R2 DOOR EMERGENCY ASSIST MECH DIMENSION A WAS .4125 INCH, WHICH IS OUT OF LIMITS IAW TASK CARD I1C52307. MAINTENANCE ADJUSTED THE R2 DOOR EMERGENCY ASSIST MECH TO A NEW DIMENSION OF .291 INCHES, WHICH IS IN LIMITS IAW MM 52-13-Dec 27, 2005 · N814AW · Airbus A319132 · Passenger/Crew DoorsSDR AWXA200501485Connector · defectiveEEL-DURING OVERNIGHT INSPECTION DISCOVERED THE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 24L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR PLUG FOR THE EMERGENCY LIGHT ASSEMBLY AT ROW 24L IAW MM. OPERATIONAL CHECKS WERE GOOD.Dec 6, 2005 · N628AW · Airbus A320231 · Emergency LightingSDR AWXA200501486Battery · dischargedEEL - CREW REPORTED THAT THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY IS DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT BATTERY. OPERATIONAL CHECKS WERE GOOD.Dec 6, 2005 · N625AW · Airbus A320231 · Emergency EquipmentSDR YENA200584Computer · faultyGEAR FAULT MASTER WARN, COULD NOT CANCEL, RETARD COULD NOT CANCEL, RETURNED 5-8 MIN CONTINUOUS. DEBRIEF FLT CREW FOR FAULT DETAILS, AFTER GEAR UP NLG MASTER WARN ILLUM, NR 1 ENG FIRE TEST ILLUM BRIEFLY. NO AUTO THR OR AP. ON APPR LGB NO RA CALLOUTS. CREW STATEDec 3, 2005 · N544JB · Airbus A320232 · Central ComputersSDR YENA200583Control Unit · malfunctionedMOMENTARY CARGO SMOKE WARNING FOLLOWED BY DISCH 1 LIGHT ON CARGO SMOKE PANEL. FOLLOWED BY AGENT 2 DISCH LIGHT. (BOTTLE 2 NOT DISC.) AND ECAM CALLING FOR NR 2 DISCH. REMOVED AND INSTALLED FWD CARGO FIRE ESTINGUISHER IAW 26-23-41. OPS CHECK GOOD. A/C GOOD FOR FNov 25, 2005 · N565JB · Airbus A320232 · Smoke DetectionSDR YENA200582Cooling Fan · failed10 MIN INTO FLT, AFT AVIONICS COMPARTMENT, RACK POWER WARNING , LIGHT IN BUTTON AND HORN . TURNED POWER OFF, NO FURTHER WARNING. LEFT IN OFF POSITION FOR REST OF FLT. REMOVED AND REPLACED COOLING FAN ASSY IAW MM 23-39-00. LTV OPS CK GOOD IAW LTV MM 23-39-00.Nov 23, 2005 · N606JB · Airbus A320232 · Air Distribution FanSDR AWXA200501376Blades · failedCREW REPORTED ON CLIMB-OUT ECAM MSG ENG 2 STALL. PILOTS RAN QRH PROCEDURE & RAN ENGINE AT IDLE. STALL RETURNED WHEN THEY ADVANCED THRUST LEVER ABOVE IDLE. RETURNED & LANDED WITHOUT FURTHER EVENT. NR 2 ENGINE BOROSCOPED. HPC NR 6, BLADES BENT & OUT OF LIMITNov 12, 2005 · N621AW · Airbus A320231 · Turbine SectionSDR YENA200580Radio · inoperativeCAPT' RMP (DIGIT WINDOW) BLANK/SLIGHT ODOR OF SMOKE/BURNING TURNED IT OFF. PERFORMED TSM 24-00-00-810-823 FOR ELECTRICAL BURNING SMELL IN COCKPIT. PERFORMED INTERNAL SURVEY (REPORT OF COCKPIT CABIN ODOR). TRACED SMELL TO RMP 1 WHICH IS INOP WITH BLANK DISPLANov 1, 2005 · N516JB · Airbus A320232 · Communications SystemSDR AWXA200501119Eec · malfunctionedDURING CLIMB CREW REPORTED "COMPRESSOR STALL ON THE NR 2 ENG ON CLIMB-OUT OF KCLE-RETURN TO KCLE ENG RAN FINE DURING DESCENT." ACFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MX PERFORMED BOROSCOPE OF NR 2 ENG & VISIUAL INSP WITH NO DEFECTS BEING NOTED. R&R NRSep 26, 2005 · N621AW · Airbus A320231 · Fuel Controlling SystemSDR AWXA200501092Fmu · malfunctionedCREW REPORTED THAT DURING TAKE OFF, NR 2 ENGINE SPOOLED MUCH SLOWER THAN NR 1. ABORTED TAKEOFF AT 30 KNOTS & RETURNED TO GATE WITHOUT FURTHER INCIDENT. MX R & R LP/HP FUEL PUMP IAW AMWEST TASK CARD R5M73304. ALSO R & R FUEL FLOW METERING UNIT IAW AWA TASKSep 19, 2005 · N819AW · Airbus A319132 · Fuel Controlling SystemSDR AWXA200500963Compressor · stalledCLE - AIR TURNBACK - FLT 281 - DURING TAKEOFF CREW REPORTED COMPRESSOR STALL ON THE NR 2 ENGINE. AIRCRAFT RETURNED TO CLE LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IS REMOVING AND REPLACING THE NR 2 ENGINE AT THIS TIME.Aug 15, 2005 · N631AW · Airbus A320231 · Turbine Engine Compressor SectionSDR AWXA200500954Blades · failedDURING CLIMBOUT, 500 AGL, LOUD BANG ACCOMPANIED WITH ACFT YAWING LT 5-10 FT. ENG RECOVERED IMMEDIATELY. ACFT CONTINUED & LANDED WITHOUT FURTHER EVENT. NO EMERGENCY ACTION TAKEN/DECLARED. MX BORESCOPED BOTH ENGINES TO ENSURE INTEGRITY. NO DEFECTS NOTED ON Aug 12, 2005 · N646AW · Airbus A320231 · Turbine SectionSDR AWXA200500757Compressor · dirtyODOR DETECTED. DURING FLIGHT, PACKS CREATING GYM SOCK ODOR WITH PASSENGERS COMPLAINING. MAINTENANCE OPERATED PACKS WITH APU BLEED AIR AND ENGINE BLEED AIR. DISCOVERED ODOR COMING FROM NR 1 ENGINE BLEED AIR SOURCE, ABOVE IDLE. INSPECTED NR 1 ENG AND UNABLE TJun 26, 2005 · N644AW · Airbus A320231 · Turbine Engine Compressor SectionSDR YENA200531Odor · detectedELECTRICAL ODOR THROUGHOUT CABIN JUST PRIOR TO DESCENT. COULD ODOR ON FLIGHT DECK ALSO. TURNED OFF TV'S, BEGAN DESCENT, ODOR WENT AWAY. PERFORMED INSPECTION IAW TSM 24-00-00-810-823, 71-00-00-810-801 EXCEPT FOR STEP 3, AND 26-15-00-810-804. NO DEFECTS NOTED. May 20, 2005 · N543JB · Airbus A320232 · Air Distribution SystemSDR AWXA200500568Interface Unit · faultyEN ROUTE TO EWR PILOTS REPORTED A NR 2 ENGINE EIU FAULT. ACFT RETURNED TO PHX WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ENGINE INTERFACE UNIT IAW AMM 73-25-3-04 AND PERFORMED A POWER ASSURANCE TEST IAW AWA TASKCARD NR F5M71302. OPERMay 17, 2005 · N636AW · Airbus A320231 · Fuel Controlling SystemSDR AWXA200500527Engine · failedON TAKEOFF AT SEA EN ROUTE FOR PHX AFTER APPLYING TAKEOFF THRUST FLIGHT CREW HEARD A LOUD BANG ON LT SIDE OF AIRCRAFT FOLLOWED BY A BURNING ODOR, REJECTED TAKEOFF AT 20 KTS, ANOTHER AIRCRAFT REPORTED SEEING FIRE COMING OUT OF THE NR 1 ENGINE, FIRE FIGHTERS RESMay 2, 2005 · N624AW · Airbus A320231 · Turbine Engine Compressor SectionSDR YENA200524Bottle · dischargedDURING DAILY CHECK FOUND R-2 DOOR SLIDE BOTTLE PRESSURE TO BE LOW AND IN RED. REMOVED AND REPLACED R-2 SLIDE.Mar 22, 2005 · N527JB · Airbus A320232 · Escape SlideSDR CA050321004Compressor · failed(CAN) THE CAPTAIN REPORTED HEARING A LOUD BANG FROM ENG NR 2 WITH INCREASED EGT, 2 RESTARTS WERE ATTEMPTED WITH NO SUCCESS AND THE FIRE HANDLE WAS PULLED (BOTTLES WERE NOT DISCHARGED). DAMAGE TO THE 3RD AND 4TH STAGE HIGH PRESSURE COMPRESSOR WAS CONFIRMED.Mar 18, 2005 · Airbus A320231 · Turbine Engine Compressor SectionSDR GTIA050042Compressor · stalledNR2 ENGINE COMPRESSOR STALL AT 10,000 LEVEL FLIGHT, PERFORMED QRH REST ENGINE TO MATCH NR1 AND ENGINE STALLED AGAIN, DIVERTED. REMOVED AND REPLACED NR2 ENGINE, PERFORMED IDLE LEAK CHECK, OPS CHECK GOOD. (K)Feb 18, 2005 · N586NK · Airbus A321211 · Turbine Engine Compressor SectionSDR AWXA200500032Actuator · malfunctionedON TAKEOFF ROLL AT PDX EN ROUTE FOR PHX AT APPROXIMATELY 40 KTS RECEIVED ECAM MESSAGE ENG 1 COMPRESSOR VANE FAULT, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORJan 12, 2005 · N832AW · Airbus A319132 · Compressor Bleed ControlSDR AWXA200500016Bleed Valve · malfunctionedCLIMBOUT 8000 FT LOUD BANG LT SIDE, ALL ENG IND NORM. TURNED BACK. A SECTION OF NR 1 ENG I/B C-DUCT INNER LINER FOUND MISSING IN AREA OF 10TH STAGE BLEED VALVE. FOUND SMALL DENT IN L/E OF STAB 10 INCHES FROM OB END. R&R LT HORIZONTAL STAB END CAP, NR 1 ENGJan 7, 2005 · N626AW · Airbus A320231 · Compressor Bleed ValveSDR DLM90041120Relay · failedAPU SMOKED THE CABIN CAUSING AN EMERGENCY EVACUATION. REPLACED BAD APU STARTER AND START RELAY.Dec 19, 2004 · N903DA · Doug MD9030 · APU Start/Ignition SystemSDR AWXA200401225Filter · cloggedON TAKEOFF AT LAS EN ROUTE TO PHX, WHEN TAKEOFF POWER WAS APPLIED RECEIVED NR 2 ENGINE OIL FILTER CLOG MESSAGE ON ECAM, OIL PRESSURE WAS VERY HIGH, REJECTED TAKEOFF LESS THAN 40 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL SCAVENGE FILTER IAW AMMNov 4, 2004 · N625AW · Airbus A320231 · Turbine Engine Oil SystemSDR CA041026010Fan · failed(CAN) DURING FLT THE ACRFT HAD BEEN DIVERTED DUE TO FUMES DETECTED IN THE COCKPIT & CABIN. AIRFRAME VIBRATIONS FROM RT WERE REPORTED IN CONJUNCTION WITH THE FUMES. CAPTAIN HAD SELECTED OFF PACK NR 2 AND ECAM MESSAGE VENT BLOWER FAULT OCCURRED SIMULTANEOUSLY, FOct 25, 2004 · Airbus A320231 · Air Distribution FanSDR AWXA200401215Seat Track · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND IN 5 PLACES ON RT CABIN SEAT TRACK Y1292 BETWEEN FR 36 AND FR 41. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y1292 FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLEOct 18, 2004 · N628AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200401193Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 9-12.Oct 17, 2004 · N628AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200401194Seat Track · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9-12.Oct 17, 2004 · N628AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200401195Seat Track · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT IB SEAT TRACK Y765 FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-72-11Oct 17, 2004 · N628AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200401196Seat Track · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON OB SEAT TRACK Y1292 RT FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-42Oct 17, 2004 · N628AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200401197Shear Plate · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE, OB OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT Y1292 FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INOct 17, 2004 · N628AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200401198Sill · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER OB EDGE OF R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546, FROM FR 66 TO FR 6Oct 17, 2004 · N628AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200401201Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11.Oct 17, 2004 · N628AW · Airbus A320231 · Fuselage Main, Floor BeamSDR CA041015007Blade · failed(CAN) ON TAKE OFF WITH THROTTLES BETWEEN IDLE AND FLEX MCT. LOUD BANG FROM LT ENGINE HEARD IN THE COCKPIT. TAKE OFF ABANDONED AT 115 KTS. ACRFT RETURNED WITH ENGINE RETARDED TO IDLE. NO UNUSUAL PARAMETERS. BORESCOPE INSPECTION REVEALED ONE FAILED HPC STAGE 4 BOct 14, 2004 · Airbus A320231 · Turbine Engine Compressor SectionSDR AWXA200401111Wire Harness · damagedON CLIMB-OUT AT FL 300, CLIMBING 1200 FPM, 290 KTS ECAM INDICATED ENG 2 COMP VANE WITH INSTRUCTION AVOID THRUST CHANGE, IF ENGINE STALL, ENG MASTER 2 OFF. REDUCED VERT SPEED AS ACRFT CLIMBED THRU FL 310 TO MINIMIZE LEVEL OFF THRUST CHANGES. WITHIN 100 FT OFOct 6, 2004 · N626AW · Airbus A320231 · Turbine Engine System WiringSDR AWXA200401041Wire · brokenDURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN GROUND WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD.Sep 20, 2004 · N637AW · Airbus A320231 · Light System WiringSDR AWXA200401033Fmu · malfunctionedON DESCENT INTO LAS EN ROUTE FROM ORD AT APPROXIMATELY 17,000 FT, RECEIVED ECAM MESSAGE NR 2 ENGINE VANE FAILURE, ENGINE THEN SPOOLED DOWN AND ECAM INDICATED NR 2 ENGINE FAILED. FOLLOWED ECAM INSTRUCTIONS AND SECURED NR 2 ENGINE; DECLARED EMERGENCY AND LANDEDSep 17, 2004 · N626AW · Airbus A320231 · Fuel Controlling SystemSDR AWXA200401027Wire · shortedARCHING / SMOKE, FLIGHT CREW REPORTED WIRES IN CAPTAINS SLIDING WINDOW POST CONNECTED TO READING LIGHT SHORED OUT WITH VISIBLE ARCHING AND SMOKE, A SMALL HOLE BURNED THROUGH PLASTIC COVER. MAINTENANCE PULLED AND COLLARED CAPTAINS READING LIGHT CIRCUIT BREAKERSep 15, 2004 · N622AW · Airbus A320231 · Light System WiringSDR AWXA200401031Floorbeam · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD AND AFT SIDE OF BEAM Y1292 LTAFT OF FR 67. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT AT FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11.Sep 10, 2004 · N656AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200400970Spur Gear · galledABORT T/O, NR 1 ENG ROLLED BACK TO IDLE WHEN BRAKES RELEASED. PRIOR, NR 1 ENG SHUTDOWN WHEN THROTTLES ADV & BRAKES RELEASED. INSP INLET & EXHAUST, BITE TEST OF CFDS & FADEC 1A&1B, HI PWR ENG RUN GOOD. *S/D* 10TH STG SOLENOID VLV INPUT LINE HAND TIGHT, TORQSep 2, 2004 · N620AW · Airbus A320231 · Fuel Controlling SystemSDR AWXA200400941Epsu · failedFLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS IN AFT GALLEY WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT GALLEY EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD.Aug 30, 2004 · N628AW · Airbus A320231 · Emergency LightingSDR AWXA200400934Odor · detectedON CLIMB OUT, AN ELECTRICAL BURNING ODOR NOTICED IN COCKPIT FOLLOWED BY SMOKE COMING FROM AIR CON VENTS IN COCKPIT & CABIN, DONNED O2 MASKS & TURNED BACK, WHEN EXITING RUNWAY RECEIVED PACK 1 OVRHT IND. A/C OUT OF SERVICE. MX FOUND ACM FROZEN, R & R ACM IAW AAug 25, 2004 · N627AW · Airbus A320231 · Air Distribution SystemSDR DLM90040824Engine · failedAS POWER WAS PUSHED UP FOR TAKEOFF RIGHT ENGINE OIL PRESSURE LO LIGHT CAME ON AND OIL PRESSURE INDICATED ZERO. SHUT DOWN ENGINE AFTER APPROX 10 SECONDS. REPLACED ACCESSORY GEARBOX.Aug 24, 2004 · N904DA · Doug MD9030 · Engine (Turbine/Turboprop)SDR AWXA200400951Floor Panel · crackedDURING C-04 CHECK A 4 INCH CRACK WAS FOUND IN FLOOR PANEL 251 AF, FR 47 - FR 51, Y254 LT - Y254 RT. MAINTENANCE REMOVED CRACKED FLOOR PANEL 251 AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670022 AND A320 SRM 53-02-00, FIG. 209.Aug 21, 2004 · N631AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200400953Beam · corrodedDURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y765 LT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT AT FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00.Aug 20, 2004 · N655AW · Airbus A320232 · Fuselage Main, StructureSDR AWXA200400944Sill · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SHAPE SILL ASSEMBLY AT Y1750 RT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SHAPE SILL AT Y1750 RT, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAAug 18, 2004 · N631AW · Airbus A320231 · Fuselage Miscellaneous Structure
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