GE CF6-50C2

Service difficulty reports · 719

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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 = 'CF650C2'
  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 XN0A1220Engine · malfunctionedAFTER ENG START ENG NR 1 REMAINED IN FLT IDLE. TRANSFERRED TO DMI 5011 PER MEL 73-30-02. CATC PLACARDS INSTALLED. (STATUS:ORIG/OPEN)Jan 6, 2005 · N224KW · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR WRLA2005001Panel · corrodedLEFT SIDE UNDER WING TO FUSELAGE PANEL NR 153DB ON BOTTOM SURFACE HAS EXFOLIATE CORROSION BETWEEN STATIONS 1239 AND 1321. REMOVED WING TO FUSELAGE PANEL NR 153DB AND ACCOMPLISHED REPAIR TO LT WING FUSELAGE PER ERA 05-53-001 REV NC DATED 01/07/05 PART 1. ACCOJan 2, 2005 · N352 · Doug DC1030 · Wing, Plate/SkinSDR P5CA0401292Valve · dirtyENGINE NR 2 FUEL VALVE MSG FUEL SPAR VLV 2 STATUS MSG. REMOVED NR 2 FUEL SPAR VALVE. CLEANED SHAFT AND REINSTALLED SPAR VALVE. OPERATION CHECKS OK PER MM 28-22-01.Dec 26, 2004 · N452PA · Boeing 74746NF · Aircraft Fuel Distribution SystemSDR WLDA2004110Oven · contaminatedCENTER GALLEY OVERHEAD LIGHT EMITTED ELECTRICAL SMELL. INVESTIGATED ELECTRICAL SMELL IN MID GALLEY AREA. CHECKED OVERHEAD LIGHTS AND ELECTRICAL CONNECTIONS, NO EVIDENCE OF ARCING OR BURNT CONNECTIONS, CHECKED ELECTRICAL CABLES FOR SIGNS OF DAMAGE, NONE EVIDEDec 13, 2004 · N352 · Doug DC1030 · Buffet/GalleysSDR 04FDEA03389Filter · cloggedAFTER T/O DURING LANDING GEAR RETRACTION, OBSERVED BOTH NR 1 AND 3 ENG FUEL FILTER PRESSURE DROP LIGHTS WERE ILLUMINATED. AFTER SELECTING CLIMB POWER. THE NR 3 LIGHT EXTINGUISHED AND NR 1 REMAINED ILLUMINATED. LEVELED OFF AT 5000 FT AND WHEN THE POWER WAS Dec 7, 2004 · N306FE · Doug DC1030F · Engine Fuel DistributionSDR WLDA2004109Engine · fireBBR/BGR ON LANDING TOWER ADVISED THAT NR 2 ENGINE IS ON FIRE, ACCOMPLISHED ENGINE FIRE CHECKLIST AND FIRED BOTH BOTTLES. ALL FIRE INDICATIONS REMAINED ILLUMINATED, ACCOMPLISHED EVACUATION CHECKLIST AND EXITED L1 DOOR VIA THE ESCAPE SLIDE. REMOVED AND REPLACEDDec 7, 2004 · N304 · Doug DC1030F · Engine (Turbine/Turboprop)SDR WLDA2004106Structure · vibrationDAY/BRU ABORTED TAKEOFF AT 70 KTS DUE TO VIBRATION. INSPECTED ALL WHEELS AND BRAKES, FLAPS AND SPOILERS, NOSE GEAR AND NR 1 & 3 INLETS, NO DEFECTS NOTED. REVERIFIED ALL TIRE PRESSURE, ALL CHECKED NORMAL.Nov 27, 2004 · N304 · Doug DC1030F · Aircraft StructuresSDR 2004000015Cowling · departedAT CLIMB-OUT, NR 3 ENG LOST ENGINE COWLING DUMPED FUEL RETURNED TO EDDF.Nov 24, 2004 · N59083 · Doug DC1030 · Nacelle/Pylon, Main FrameSDR 2004FA0000909Retainer · mislocatedDURING A ROUTINE "A-CHECK", FINNAIR FAA REPAIR STATION WAS REQUESTED TO PERFORM FAN BLADE LUBRICATION OF POSITION NR 3 ENGINE ON DA-10,N303WL. INSPECTION OF THE FAN BLADES REVEALED THAT ALL FAN BLADE SPACERS WERE IMPROPERLY INSTALLED. THE SPACER RETAINER LIPNov 19, 2004 · Doug DC1030F · Turbine Engine Compressor SectionSDR P5CA0401276Cadc · ingestedNR 1 CADC INOPERATIVE. REPLACED NR 1 CADC, OPS CHECK OK PER AMM 34-12-01.Nov 16, 2004 · N355MC · Boeing 747341 · Air Data ComputerSDR DHL2004365005Control Unit · inoperativeWHILE NORMAL BRAKES ARE BEING APPLIED, IF ANY AUTOBRAKE MODE IS SELECTED, EXPERIENCE A 3 SEC LOSS OF NORMAL BRAKES. IT IS AS IF THE ANTI SKID SYSTEM IS RELEASING THE BRAKES BUT THE ANTI SKID PANEL SHOWS NORMAL. REPLACED AUTOBRAKE CONTROL UNIT IAW MM 32-42-54Nov 3, 2004 · N365DH · Airbus A300B4203 · Landing Gear Brake SystemSDR XNOA1208Gyro · fluctuatesON CLIMB, ATT LIGHT ON ADI CAME ON. CAPT ADI SHOWED 6 DEGREE NOSE HIGH. CAPT AND F/O HSI SHOW 6 DEGREE DIFFERENCE. LINE-UP AFTER 5 MINUTE LEVEL FLIGHT. REMOVED AND REPLACED NR 1 VERTICAL GYRO AND NR 3 DIRECTIONAL GYRO, BOTH SYSTEMS OPS CK GOOD IAW AMM 34-25Nov 2, 2004 · N373PC · Airbus A300B4203 · Directional Gyro and Indicating SystemSDR DHL2004362015Connector · dirtyRT MAIN GEAR GREEN DOWN LIGHT ON FORWARD PANEL COMES ON INTERMITTENT WITH MWP ANTI-SKID OFF LIGHT. LANDING GEAR LEVER LOCK ON SYSTEM 1. COULD NOT DUPLICATE ON GROUND. CLEANED PROX SENSORS AND CONNECTOR ON RT GEAR. PERFORMED TEST OF PROXIMITY DETECTOR UNIT IOct 26, 2004 · N362DH · Airbus A300B4203 · Electrical ConnectorsSDR WRNA200400015Valve · leakingNR 2 ENGINE EXCEEDED 960 DEGREE C DURING TAKE OFF (REACHED 962 DEGREE C FOR APPROX. 10 SECONDS W9TH AMBER EGT LIGHT) N1 WAS INDICATING 100.2 PERCENT. ABORTED THE TAKE OFF. AT IDLE NR 2 ENG 24.8 N1, 601 EGT, 66.4N2, 1700 F/F. CHECKED NR 2 ENGINE INLET AND EXHAOct 15, 2004 · N820SC · Airbus A300B4203 · Pneumatic SystemSDR P5CA0401251Wire · chafedNR 3 ENGINE BLEED VALVE CLOSED, LIGHT STAYS ON AT CRUISE PWR & POPPED C/B AT LANDING. REPAIRED CHAFED WIRE PYLON TO HIGH STAGE BLEED VALVE PER WPM CH 20-10-13, OPERATIONAL CHECK OK.Oct 12, 2004 · N508MC · Boeing 747230B · Pneumatic System WiringSDR DHL2004363534Skin · dentedDURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3912, AFT. FUSELAGE SKIN HAS DENT AT FR 77 AND STR 22R. BLENDED OUT AREA, FOUND DENT BEYOND LIMITS IAW SRM 53-10-10. CUT OUT DAMAGE AREA SRM 53-10-10. PERFORMED HFEC OF CUT-OUT AREA NTM PT 1 51-31-05. NO DISCREOct 12, 2004 · N363DH · Airbus A300B4203 · Fuselage Main, Plate/SkinSDR WRNA200400014Dampener · inoperativeAFTER TAKE OFF UNABLE TO MOVE GEAR HANDLE TO UP POSITION. FOLLOWED ABNORMAL PROCEDURES. AIRCRAFT LANDED NORMAL. REMOVED AND REPLACED RT PITCH DAMPENER IAW 32-11-15. AIRCRAFT JACKED AND GEAR SWING COMPLIED WITH OP'S CHECK GOOD IAW 7-11-00. AIRCRAFT RETURNOct 7, 2004 · N505TA · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR DHL2004363509Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3898, RBL 36 BETWEEN FRAME AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORROSION FROM AREA/FRAME IS TO FRAME 19 RBL 36 FOUND OUT OF LIMITS SRM 53-10-00. REMOVED SEAT TRACK FROM FR 15 TO FR. 19 AT RBL 36 IAW SRM 51-30-Oct 5, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02868Blanket · burnedIN CENTER ACCESSORY COMPARTMENT AT THE LT AND RT FUSELAGE FEED THROUGH FOR THE PNEUMATIC SUPPLY DUCTS 1-2 AND 1-3 HAVE FUSELAGE INSULATION BLANKETS SEVERELY BURNED AROUND THE DUCT. A/C FUSELAGE WAS INSTALLED WITH OLD TYPE OF INSULATION BLANKET. (P/N 392945Oct 4, 2004 · N316FE · Doug DC1030F · Accessory CompartmentSDR DHL2004363518Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3892, FR. 26.5 - FR. 35.5 RBL 36 INCH MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS IAW A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 26.5 TO FR. 35.5 AT RBL 36 INCHES IAW A-300 51-30-30. REPLACED SEAT TRACK IAW A-Sep 30, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004363520Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, 3891, FR18 - FR26.5 RBL 38 INCH MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR18 - FR26.5 AT RBL 38 INCH IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW Sep 30, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004363527Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3893, FR. 18 - FR. 26.5 RBL 18 MAIN CABIN SEAT TRACK CORRODED OUT LIMITS IAW A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 18 - FR. 26.5 RBL 18 IAW A-300 SRM 53-10-10 / 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM Sep 30, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004363530Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3887, FR.18-FR. 26.5 RBL 98 SEAT TRACKS MAIN CABIN CORRODED BEYOND LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACKS FROM FR 18 TO FR 26.5 AT RBL 98 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEWSep 30, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004363510Seat Track · corrodedDURING C-CHECK, NR 3868 FRAME 34-FRAME 38.2 LBL 78 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW SRM 51-40-11. NR 3868, REMOVED SEAT TRACK FROM FR 34-FR. 38.2 LBL 78 INCHES IAW SRM 53-10-10 OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW Sep 28, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004363517Seat Track · corrodedDURING-C CHECK, DISCREPANCY AS FOLLOWS, N/R 3876, FR. 34 TO FR. 38.2 RBL 78 SEAT TRACK FLANGES OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR34 TO FR38.2 RBL 78 IAW A-300 SRM 53-10-20 / 51-30-30. INSTALLED NEW SEAT TRACK FROM FR34 TO FR38.2 Sep 28, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004363524Seat Track · corrodedDURING C-CHECK, N/R, 3870 FR. 30 - FR 35 LBL 36 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 30 TO FR. 35 AT LBL 36 IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACSep 28, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004363529Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3883, BL 0 FR. 26 TO FR. 30 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 26 - FR. 30 AT BL 0 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW SEASep 28, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004363535Seat Track · corrodedDURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3871, FR. 30 - FR. 38.2 LBL 18 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 30- FR 38.2 AT LBL 18 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW SEASep 28, 2004 · N363DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02802Skin · damagedNR 1 ENGINE IB COE COWL IS DAMAGED AT LEADING EDGE. REMOVED CORE COWL, CUT OUT DAMAGE, REMOVED FRAME AND RUBSTRIP, FABRICATED DOUBLER AND FILLER, DRILLED AND FITTED NEW FRAME AND RUBSTRIP, INSTALLED DOUBLER AND FILLER, FRAME AND RUBSTRIP IAW DC10 SRM 54-0Sep 22, 2004 · N321FE · Doug DC10 · Nacelle/Pylon, Plate/SkinSDR XNOA1201Valve · malfunctionedON PUSH BACK NR 5, 7 BRAKES LOCKED UP. REMOVED AND REPLACED ELECTRO VALVE IAW A300MM 32-42-11, BLED BRAKING SYS FROM FL COMPT. (STATUS: ORIG/CLOSED)Sep 20, 2004 · N474AS · Airbus A300B4203 · BrakeSDR XNOA1200Tire · failedDURING TAXI, HEARD LOUD BANG. SUSPECT TIRE BLOWN. (STATUS: ORIG/OPEN)Sep 16, 2004 · N474AS · Airbus A300B4203 · TireSDR 04FDEA02699Fitting · corrodedNR 1 PYLON TOMBSTONE FITTING UPPER BEARING STIFF AND PITTED. REMOVED UPPER SPHERICLE BEARING FROM NR 1 PYLON TOMBSTONE CHECKED DIAMETRICAL CLEARANCE OF NEW BEARING INSIDE DIA AND PLUG IS .0001 MAX CLEARNCE .012. CLEARANCE CHECK OK IDENTIFIED MOUNT BOLT TO BESep 16, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Attach FittingsSDR WRNA200400011Actuator · unserviceableAFTER TAKE OFF AC REQUIRED A LOT OF AILERON TO KEEP LEVEL, 35 DEGREES. RETURNED TO AIRFIELD, WHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY. OVERWEIGHT LANDING ACCOMPLISHED. LANDING NORMAL. FOUND NR 3 LT SPOILER SERVO BSep 8, 2004 · N501TR · Airbus A300B4203 · Fuel Dump SystemSDR WRNA200400012Dump Valve · failedWHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY SELECTED. CLEANED C/P AT RT FUEL JETTISON VALVE ACTUATOR. SECONDARY SYS CHECK'S OK IAW 28-31-00. PRIMARY DEFERRED IAW MEL 28-31-02 CAT-C.Sep 8, 2004 · N501TR · Airbus A300B4203 · Fuel Dump SystemSDR WLDA200491Floor Support · corrodedDURING "B4" CHECK IN BYH, FOUND RBL30 F/S 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATELY .002 OF MATERIAL RBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01.Sep 5, 2004 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WLDA200492Floor Support · corrodedDURING "B4" CHECK IN BYH, FOUND LBL30 FS 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATELY .002 OF MATERIAL LBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01.Sep 5, 2004 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WLDA200493Floor Panel · corrodedDURING "B4" CHECK IN BYH, FOUND FLOOR PANEL FWD OF LEFT FWD STORE CLOSET HAD EXFOLIATION CORROSION. REMOVED AND REPLACED FLOOR PANEL FWD OF LEFT STORE CLOSET IAW DC-10 MM 53-22-01.Sep 5, 2004 · N14075 · Doug DC1030 · Fuselage Floor PanelSDR XNOA1197Pitch Control · malfunctionedON TAXI PITCH TRIM INOPERATIVE. TRANSFERED TO DMI NR 4527, IAW ENA A300 MEL REF 22-11-03, PLACARDS INSTALLED. (STATUS: ORIG/OPEN)Aug 27, 2004 · N373PC · Airbus A300B4203 · Auto Flight SystemSDR DHL2004366005Aileron · malfunctionedON DEPARTURE AFTER SLAT RETRACTION AND COMPLETION OF LT TURN, A/C REQUIRED 30 DEG LT AILERON TO MAINTAIN WINGS LEVEL. FCPI CONFIRMED PROPER CONTROL DEFLECTIONS. JETTISONED FUEL AND RETURNED. DEFERRED RT NR 3 ROLL SPOILER IAW MEL 27-62-01-1, CAT. (C) CONTAug 24, 2004 · N366DH · Airbus A300B4203 · Aileron Control SystemSDR DHL2004364014Landing Gear · slowLT MAIN GEAR TOOK 15 SECONDS LONGER THAN OTHER GEAR TO EXTEND,TO LOCK.Aug 20, 2004 · N364DH · Airbus A300B4203 · Landing Gear Retraction/Extension SystemSDR 2004F00237Sleeve · crackedNR 3 ENGINE IB THRUST REVERSER EXTRUDED TORQUE RING, AT THE LEADING EDGE OF TRANSLATING SLEEVE, CRACKED AROUND FASTENER HOLE AT 10 O'CLOCK (REVERSER DEPLOYED). REFERENCE NON-ROUTINE 39502.Aug 14, 2004 · N322FE · Doug DC1030F · Engine Thrust ReverserSDR 2004F00236Fuse Link · shearedRT OB SLAT RETAINER MECHANISM MECHANICAL FUSE SHEARED. (REFERENCE MM 27-83-08 PAGE 202 FIGURE 201) REFERENCE NON-ROUTINE 39546.Aug 14, 2004 · N322FE · Doug DC1030F · Leading Edge Slat Control SystemSDR WRNA200400009Smoke Detector · unserviceableDURING TAKEOFF ROLL FLIGHT DECK SMOKE LIGHT ILLUMINATED ON F/E PANEL ALONG WITH SMOKE LIGHT ON MWP AND CONTINUOUS CHIME. TAKEOFF WAS REJECTED AT 105KTS AND AIRCRAFT RETURNED TO GATE. FOUND E&E SMOKE DETECTOR SATURATED WITH WATER. INVESTIGATION REVEALED THAT Aug 14, 2004 · N505TA · Airbus A300B4203 · Smoke DetectionSDR 2004FA0000679Attach Fitting · corrodedLOWER AFT WING TO CENTER BOX ATTACH SKATE FITTING IS EXFOLIATED, LT WHEEL WELL, FUSELAGE STATION 1366 TO 1381. REFERENCE NON-ROUTINE NR 39431.Aug 6, 2004 · N322FE · Doug DC1030F · Fuselage, Wing Attach FittingsSDR 2004FA0000678Fuse Pin · shearedRT WING OB SLAT CONTROL MECHANISM HAS ANTI-DROOP FUSE PIN SHEARED. REFERENCE NON-ROUTINE 39501.Aug 6, 2004 · N322FE · Doug DC1030F · Leading Edge Slat ActuatorSDR DHL2004366003Pump · failedMLG WOULD NOT EXTEND ON LANDING. COMPLETE M/G EXT ABNORMAL PROCEDURE. LANDED WITH NO NOSEWHEEL STEERING. EXT TOOK 20 TURNS. WOULD NOT EXTEND DUE TO ITEM 1P. LOSS OF GREEN SYS HYD. RESTORED EXT/RET SYS TO NORMAL IAW MM. MANUAL HANDLE RETURNED TO NORMAL W/ Jul 18, 2004 · N366DH · Airbus A300B4203 · Hydraulic Pump (Electric/Engine), MainSDR 2004000007Engine · failedON T/O ROLL, NR 1 ENGINE MADE LOUD BANG, ENGINE FAIL LIGHT ILLUMINATED AND EGT PEGGED. N1 WAS 130 PERCENT AND SPEED WAS 125 KIAS. T/O ABORTED. TOWER NOTED FIRE FROM INTAKE.Jun 13, 2004 · N59083 · Doug DC1030 · Engine (Turbine/Turboprop)SDR XNOA1186Duct · looseFIRE INDICATION ON NR 2 ENG. QRH COMPLETED, FIRE BOTTLE NOT DISCHARGED. OPS CHECK FIRE DETECTION SYSTEM IAW A300 MM REF 26-12-00, NO DEFECTS NOTED, OPS CHECKS GOOD. FOUND NR 2 ENGINE RECOUP DUCT RUPTURED. REMOVED AND REPLACED BOTH SECTIONS OF DUCT IAW A300May 12, 2004 · N372PC · Airbus A300B4203 · Pneumatic Distribution SystemSDR UIEA200400090Bleed Valve · malfunctionedDURING CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. NR 2 ENGINE SUSTAINED 6 OR MORE HARD COMPRESSOR STALLS WHILE CLIMBING THROUGH 18,000 FT TO 24,000 FT. INSPECTED INTAKE/EXHAUST AREAS, NIL DISCREPANCIES. CHIP DETECTORS CLEAN REMOVED AND REPLACED SAME 8TH STAMay 4, 2004 · N536MC · Boeing 747228F · Compressor Bleed ValveSDR 04FDEA01130Bulb · faultyENG 1 OIL TEMP HIGH, TEMP 226; ABOVE RED LINE. READJUSTED POWER, TEMP REMAINED ABOVE RED LINE. SHUT DOWN NR 1 ENGINE AND LANDED. OIL TEMP SLOWLY RETURNED TO A LOWER SETTING. OIL PRESSURE & QTY NORMAL. NO VIBRATIONS. RAN ENG NR 1, OIL TEMP AT 4 MIN WAS 14May 1, 2004 · N312FE · Doug DC1030F · Engine Oil Temperature
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