GE CF34-3B1

Service difficulty reports · 5,402

Newest first. General aviation reporting is voluntary.

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 = 'CF343B1'
  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 A6WA200540112Rib · crackedLT MLG WHEEL WELL AT WS 48.30 FS 523.8 BATT RIB IS CRACKED APPROX 1 INCH.Mar 16, 2005 · N415AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540097Intercostal · crackedRT SIDE FS 621-FS 625.3 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .60 INCH. INSTALLED NEW RT INTERCOSTAL AT FS 621-625.3, STR 14R IAW BRAS EO 601R-53-6157. (K)Mar 15, 2005 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540098Intercostal · crackedLT SIDE FS621-FS625.3 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS, APPROX .70 INCH. INSTALLED NEW LT INTERCOSTAL AT FS 621-625.3, STR 14L IAW BRAS EO 601R-53-6157. (K)Mar 15, 2005 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540099Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513 REV A BY CUTTING OUT (CRACKED ANGLE AND INSTALLING NEW ANGLE).Mar 15, 2005 · N413AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540118Angle · crackedLT FS 625, WO OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED LT 621.00 ANGLE AT STR 14 LT IAW SRM. (K)Mar 14, 2005 · N413AW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR A6WA200540094Pump · failedUPON FINAL APPROACH EXTENDED GEAR RECEIVED HYD 3 LO PRESSURE CAUTION MESSAGE. ASSOC WITH GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. EXECUTED GO AROUND. GEAR CAME UP AFTER ABOUT A MINUTE. RAN ASSOCIATED QRH PUT GEAR DOWN. ALL NORMAL. REMOVED AND REMar 13, 2005 · N403AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CA050322004Anti-Ice Valve · closed(CAN) IN CRUISE ENGINE ANTI-ICE WAS SELECTED ON THE NR 2 ENGINE BUT VALVE WOULD NOT OPEN. UPON RETURNING TO BASE VALVE WAS REPLACED AND TESTED FUNCTIONAL.Mar 12, 2005 · Cndair CL604 · Engine Anti-Icing SystemSDR CA050312004Windshield · cracked(CAN) LT WINDSHIELD CRACKED DURING LEVEL FLIGHT. DIVERTED FLIGHT. LT WINDSHIELD WAS REPLACED IAW AMM.Mar 10, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA050312001Apu · damaged(CAN) AFTER APU SHUTDOWN, FIRE AND SMOKE OUT OF EXHAUST, FOUND OIL-SYSTEM EMPTY AND OIL BURNING AT APU EXHAUST: APU EXTINGUISHED WITH FIRE X BOTTLE. FIRE DAMAGE INSPECTION APU EXHAUST HEATSHIELD, LOWER TRANSLATING, COWL AND ACCESS PANEL NR 422DB,422BB, 422CB, Mar 9, 2005 · Cndair CL6002B19 · APU Core EngineSDR VNAA0503005Detection Sys · failedDURING CLIMB (SDF TO LGA) THE FLAPS DEGRADED STATUS MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2588 DIVERTED TO DAY, MADE AN UNEVENTFUL LANDING. AFTER TROUBLESHOOTING THE FLAP SYSTEM PER CRJ 200 FIM 27-50-00, PSA MAINTENANCE REMOVED AND REPLACED THE SKEW DETECTMar 6, 2005 · N216PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR ASOA05210Doubler · crackedDURING AN A-CHECK IN BTR, THE FS 640 DOUBLER AT STRINGER 10, FRAME FS 640 AND THE SKIN BUTT JOINT STRAP LEFT FS 640, STRINGER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 640 DOUBLER AT STRINGER 10 AND THE FS 640 FMar 6, 2005 · N824AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA200514662Engine · leakingNR 1 ENGINE HAS OIL LEAKING, FOUND A SUMP DRAIN LEAKING BEYOND LIMITS. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY IAW 71-00-00, OPERATIONAL CHECK GOOD.Mar 5, 2005 · N936SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0503004Pump · failedINBOUND TO DCA THE HYD 2 LOW PRESS MESSAGE ILLUMINATED. WHILE FOLLOWING THE QRH THE MESSAGE WENT OUT AND THE HYD EDP 2A MESSAGE APPEARED. THE CREW OF FLIGHT 2344 CONTINUED TO DESTINATION AND MADE AN UNEVENTFUL LANDING AT DCA. PSA MAINTENANCE REMOVED AND REPMar 4, 2005 · N228PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CA050309009Windscreen · broken(CAN) A/C , WAS ENROUTE AT FL 360 WHEN THE CREW ADVISED ATC THAT THEIR WINDSCREEN SHATTERED AND REQUESTED DESCENT. A SHORT TIME LATER, THE CREW REQUESTED DIVERSION . THE FLIGHT LANDED SAFELY AT 2313Z. NO EMERGENCY WAS DECLARED BUT AFF RESPONDED. A/C WAS FEMar 4, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA050308020Window · cracked(CAN) ON APPROACH THE CO-PILOT'S WINDOW CRACKED. WINDOW REPLACED IAW AMM AND THE AIRCRAFT RETURNED TO SERVICE.Mar 4, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200540087Angle · crackedRT FS 625 OBLIQUE ANGLE CRACKED IN RADIUS .3750 INCH LONG. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE IAW SRM. (K)Mar 4, 2005 · N407AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0503002Warning Horn · activatedDURING CLIMB (PIT TO IND) AT FL 280 AND 320 KTS IAS THE FLAP OVERSPEED WARNING HORN SOUNDED. AS THE CREW OF FLIGHT 2358 SLOWED THE AIRCRAFT PER THE QRH, HYDRAULIC PUMP 2B & 3B CAUTION MESSAGES ILLUMINATED. THE CREW TURNED ON ALL HYDRAULIC PUMPS. THE EICAS FMar 3, 2005 · N216PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA0503003Control System · malfunctionedTHE CREW OF FLIGHT 2396 REPORTED THAT THE FLAPS FAILED AT ZERO DEGREES ON APPROACH TO BTV. THE CREW DECLARED AN EMERGENCY, PREPPED THE CABIN, AND MADE AN UNEVENTFUL ZERO FLAP APPROACH AND LANDING AT BTV. CONTRACT MAINTENANCE RESET THE FLAP CONTROL UNIT IAW RMar 3, 2005 · N260JS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540083Smoke · detectedEXCESSIVE SMOKE OUT OF RT ENGINE ON SHUTDOWN ALL INDICATIONS WERE NORMAL. PERFORMED ENGINE RUN OF ENGINE NR 2 IAW CRJ AMM TASK 71-00-00-848-806. NO DEFECTS NOTED. AIRCRAFT SAFE FOR SERVICE. (M)Mar 2, 2005 · N429AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0503001Pitot Head · bird ingestionAT ROTATION DURING TAKEOFF ROLL (DCA TO SDF) THE CAPTAIN'S AIRSPEED TAPE FAILED SHOWING NO INDICATION. SHORTLY THEREAFTER THE YAW DAMPNER, MACH TRIM, AND STAB TRIM, ALSO FAILED. THE CREW OF FLIGHT 2573 RETURNED TO DCA AND MADE AN UNEVENTFUL LANDING. CONTRACMar 1, 2005 · N247JS · Cndair CL6002B19 · Pitot/Static SystemSDR MASA200500167Engine · leakingEMERGENCY DECLARED. SHUTDOWN NR 2 ENGINE AND DIVERTED TO IAD DUE TO LOSS OF OIL PRESSURE. MX IS IN THE PROCESS OF TROUBLESHOOTING.Mar 1, 2005 · N591ML · Cndair CL6002B19 · Turbine Engine Oil SystemSDR 05055656Carbon Seal · leakingEVENT SUMMARY STATED LAV SMOKE. REMOVED AND REPLACED RT ENG NR 1 CARBON SEAL.Feb 24, 2005 · N656BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA050223013Buss · damaged(CAN) IN CRUISE, EICAS MESSAGES AC BUSS 1 AND AC UTILITY BUSS 1 APPEARED SIMULTANEOUSLY WITH A CHATTERING NOISE WHICH COULD BE IDENTIFIED. THE AIRCRAFT LANDED AS SCHEDULED. INSPECTION BY MAINTENANCE REVEALED THAT: C/BS J4 CBP-1 AND 2 (AC UTIL CONT) AND C/B AFeb 23, 2005 · Cndair CL6002B19 · Electrical Power System WiringSDR 2005FA0000182Track · looseTRACK/CHANNELS, 600-380091, ARE U CHANNELS THAT FACE EACH OTHER ALLOWING STRUT, 600-38008-17 AND CAMS, TO MOVE UP AND DOWN INSIDE OF THESE TRACKS. THE TRACKS ARE MANUFACTURED WITH SMALLER SIDES AND POOR ENGAGEMENT/ LOOSE FIT OF THE STRUT/CAMS ALLOW THE CAMS TFeb 22, 2005 · N43R · Cndair CL6002B16 · Passenger/Crew DoorsSDR CA050226001Gearbox · making metal(CAN) NR 2 ENGINE SELF SHUTDOWN AT 11,000 FEET. DECLARED AN EMERGENCY AND LANDED WITH ONE ENGINE. NO OTHER PROBLEMS NOTED. MAINTENANCE FOUND THE GEARBOX TO BE AT FAULT. REPLACED THE GEARBOX AND RETURNED THE AIRCRAFT TO SERVICE.Feb 16, 2005 · Cndair CL6002B19 · Accessory GearboxesSDR MASA200500125Gearbox · making metalASH 7169 IAD-GSP- E2 SHUTDOWN AT 11OOO FEET IN LEVEL CRUISE. CAPTAIN DECLARED AN EMERGENCY AND LANDED WITH ONE ENGINE. MAINTENANCE IS TROUBLESHOOTING 2/18/05 MAINTENANCE CHANGED THE AGB.Feb 16, 2005 · N75995 · Cndair CL6002B19 · Turbine Engine Reduction GearSDR VNAA0502012Screen · dirtyDURING CRUISE AT FL 360 (PHL TO MSP) THE CREW OF FLIGHT 2501 REPORTED THAT THE RT ENGINE OIL PRESSURE WAS FLUCTUATING BETWEEN 25-35 PSI. OIL TEMPERATURE WAS 132 DEGREES. THE CREW DECENDED TO FL 290 WHERE THE OIL PRESSURE STABILIZED AT 42 PSI AND ALL ENGINE IFeb 15, 2005 · N223JS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA050216006Attach Fitting · separated(CAN) FORWARD RT WING ATTACH FITTING FORWARD SIDE FLANGED BUSHING HAS COMPLETE SEPARATION OF FLANGE FROM BUSHING SLEEVE. RECTIFICATION REQUESTED FROM MFG.Feb 15, 2005 · Cndair CL6002B19 · Wing, Attach FittingsSDR ASOA05130Oil System · lowFLT 4151 - DURING CRUISE FROM FPO-ATL, WHILE IN HOLDING PATTERN OVER ATL, CREW OBSERVED THE RT ENG OIL PRESS FLUCTUATING FROM APPROX 37 TO 50 PSI. THE CREW WAS INSTRUCTED TO DIVERT TO BHM AND THEN THEY RECEIVED A 'RT ENGINE OIL PRESSURE' MESSAGE ACCOMP BY A RFeb 14, 2005 · N883AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR MASA200500108Fuel Control · fluctuatesASH 6108 PHX TO PSP, RETURNED TO THE FIELD WITH NR 1 ENGINE FUEL FLOW, ITT, AND OVERSPEED SITUATION. MAINTENANCE IS IN WORK. 2/13/05 MAINTENANCE REMOVED AND REPLACED NR 1 FCU, OPS CHKD GOOD.Feb 12, 2005 · N17358 · Cndair CL6002B19 · Fuel Controlling SystemSDR VNAA0502011Warning Light · false indicationAT THE START OF TAKEOFF ROLL AT DCA THE CREW REPORTED A TAKEOFF CONFIG WARNING AND THE GND SPLR DEPLOY CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2428 ABORTED THE TAKEOFF AND RETURNED TO THE GATE. CONTRACT MAINTENANCE PERFORMED TAKEOFF CONFIG OPERATIONAFeb 11, 2005 · N242JS · Cndair CL6002B19 · Central WarningSDR CA050215008Bolt · seized(CAN) ON CLIMB OUT, CREW RECEIVED A (PAX DOOR LATCH) MESSAGE, AND THEN A (PASSENGER DOOR WARNING MESSAGE). CREW FOLLOWED QRH PROCEDURES AND COMPLETED AN UNEVENTFUL OVERWEIGHT LANDING. TROUBLESHOOTING FOUND BOLT P/N NAS6207-54D SEIZED IN BUSHING P/N NAS74A7E302Feb 9, 2005 · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA0502006Seal · leakingDURING CLIMB AFTER TAKEOFF, AT 1000 FEET, THE CABIN STARTED CLIMBING WITH THE AIRCRAFT AND A LOUD SQUEAL WAS HEARD COMING FROM THE FORWARD CABIN. THE CREW OF FLIGHT 2321 RETURNED TO DAY AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE FOUND THE PASSENGER DOORFeb 8, 2005 · N202PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA0502007Bpsu · failedDURING CRUISE FLIGHT WITH FLAPS SELECTED TO ZERO DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLLUMINATED. THE CREW OF FLIGHT 2292 (YOW TO PHL) DIVERTED THE FLIGHT TO YUL AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY WHERE PSA MAINTENANCE REMOVEFeb 8, 2005 · N230PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0502005Outflow Valve · failedDURING CLIMB AFTER TAKEOFF (MSP TO PHL) CABIN ALT CAUTION LIGHT ILLUMINATED. CREW OF FLIGHT 2473 FOLLOWED QRH PROCEDURES. PRESSURIZATION WOULD NOT RESET AND INOPERATIVE IN AUTO AND MANUAL MODES. THE CREW ELECTED TO DIVERT TO DAY WHERE THE AIRCRAFT MADE AN UFeb 7, 2005 · N248PS · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR A6WA200540043Apu · seizedAPU FAILED, REQUESTED INSPECTION. COMPLIED WITH APU INSPECTION FOUND APU TO BE SEIZED. APU INLET EXHAUST NO DEFECTS NOTED. ALSO SUSPECT BAD FCU. COMPLIED WITH ACTION PLACARD PLACED ON MEL. MAINTENANCE VERIFIED APU SEIZED. REMOVED AND REPLACED APU ASSEMBLYFeb 7, 2005 · N415AW · Cndair CL6002B19 · APU Core EngineSDR VNAA0502004Control Unit · failedAFTER LANDING AT CAK THE CREW OF FLIGHT 2286 REPORTED A FLAPS HALFSPEED STATUS MESSAGE. PSA MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW CRJ 200 AMM 27-51-05-400-801. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FORFeb 6, 2005 · N226JS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0502002Warning Light · illuminatedON DESCENT INTO PIT, WITH FLAPS STILL AT ZERO, THE FLAPS DEGRADED STATUS MESSAGE ILLUMINATED AND THE OVERSPEED RASTOR APPEARED ON THE AIRSPEED READ OUT. THE FLAPS OPERATED NORMALLY ON EXTENSION AND THE CREW MADE AN UNEVENTFUL LANDING. CONTRACT MAINTENANCE ATFeb 5, 2005 · N258PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0502003Trim System · malfunctionedTHE CREW OF FLIGHT 2405 REPORTED THAT APPROXIMATELY 25 PERCENT LEFT AILERON TRIM AND 15 - 20 PERCENT LEFT RUDDER TRIM WAS REQUIRED FOR STRAIGHT AND LEVEL FLIGHT. CONTRACT MAINTENANCE IN PIT PERFORMED AN OPERATIONAL TEST OF THE AILERON TRIM SYSTEM IAW CRJ 200 Feb 5, 2005 · N258PS · Cndair CL6002B19 · Aileron Tab Control SystemSDR A6WA200540044Doubler · mismanufacturedWHILE PERFORMING SB 601R57037 (WING SPAR MOD) IT WAS DISCOVERED THAT THE JOINT STRAP ON THE RT WING LACKS PROPER LENGTH FOR EDGE DISTANCE. COMPLIED WITH BRAS EO 601R575944A, BY FABRICATING DOUBLER FROM 2024T3, .050 INCH AND USING TO EXTEND CUTLINES TO OBTAIN Feb 5, 2005 · N412AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA200540042Compressor · vibrationRETURNED TO DEPARTURE, DUE TO HIGH N1 FAN VIBRATION 2.8 IN CLIMB POWER SET ITT AND N1 NORMAL. INSPECTED NR 2 ENGINE INLET FAN BLADES, EXHAUST AND CHIP DETECTORS. NO DEFECTS FOUND. GROUND RAN ENGINE VIBRATION .8 MILS WITHIN LIMITS REF CF34 ENG MANUAL 72-00-0Feb 4, 2005 · N432AW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR VNAA0502001Warning Light · illuminatedDURING TAKEOFF ROLL AT PHL THE CREW OF FLIGHT 2470 RECEIVED A CONFIG AILERON WARNING WHEN THE YOKE WAS MOVED FOR CROSSWIND CORRECTION. THE CREW ABORTED THE TAKEOFF AND TAXIED BACK TO THE GATE. PSA MAINTENANCE FOUND THE AILERON TRIM SET OUT OF THE TAKEOFF RANFeb 3, 2005 · N254PS · Cndair CL6002B19 · Aileron Control SystemSDR A6WA200540040Fastener · mislocatedUNABLE TO ACHIEVE EDGE DISTANCE ON JOINT STRAP (PN 601R1004654) WHILE COMPLYING WITH SB 601R57037 DUE TO EXISTING FASTENER BEING MISLOCATED. PERFORMED A MAJOR ALTERATION TOO, BY SHIFTING THE CUTLINE TO PROVIDE MINIMUM EDGE DISTANCE ON THE EXISTING FASTENERS, Feb 2, 2005 · N414ZW · Cndair CL6002B19 · FastenersSDR A6WA200540041Skin · dentedSKIN IS DENTED ON THE LT SIDE SKIN PANEL BETWEEN RS 108.25 AND 113.98 THE DENT MEASURES 2.2 INCHES LONG X 2 INCHES WIDE. PERFORMED A MAJOR REPAIR TO THE RUDDER SKIN ON LT SIDE BY TRIMMING OUT DAMAGE, LPI, FABED DOUBLER AND INSTALLED IAW EO. (K)Feb 2, 2005 · N414ZW · Cndair CL6002B19 · Rudder, Plate/SkinSDR VNAA0501012Control Unit · failedWHILE IN CRUISE FLIGHT AT 29,000 FEET THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2286 FOLLOWED QRH PROCEDURES AND CONTINUED THE FLIGHT TO CAK, DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE REMOVED AND REPLACED THE Jan 31, 2005 · N230PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0501013Smoke Detector · false activationTHE SMOKE TOILET WARNING MESSAGE ILLUMINATED IN FLIGHT AND WENT OUT AFTER ONE MINUTE. PSA MAINTENANCE PERFORMED AN INSPECTION OF THE LAVATORY AND THE AUTOMATIC FIRE EXTINGUISHER. NO EVIDENCE OF SMOKE, FIRE, OR DEFECTS WERE FOUND. THE LAVATORY SMOKE DETECTOJan 31, 2005 · N221PS · Cndair CL6002B19 · Smoke DetectionSDR A6WA200540029Angle · crackedLT FS 621.00 ANGLE IS CRACKED. CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED A REPAIR ANGLE IAW REO. (K)Jan 31, 2005 · N414ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540037Access Panel · corrodedLT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL TANK PANELS 550BB, 540ED, 540BB, 510AB. REMOVED MINOR CORROSION FROM LT WING LOWER PLANK AT FUEL ACCESS PANELS 550BB, 540FB, 540EB, 540BB AND 510AB IAW MFG REO 601R-57-21-030 REV C. (M)Jan 31, 2005 · N412AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540023Manifold · chafedSTRONG ODOR OF JET FUEL IS PRESENT WITH PACKS ON WHILE ON GROUND. FOUND APU PRIMARY MANIFOLD CHAFED THROUGH BY STARTER CONTROL VALVE. REPLACED MANIFOLD IAW AMM AND REPOSITIONED CONTROL VALVE. GROUND RAN AND LEAK AND OPS CHECK GOOD. (K)Jan 29, 2005 · N411ZW · Cndair CL6002B19 · APU Bleed Air SystemSDR VNAA0501011Outflow Valve · dirtyDURING CLIMBOUT FROM YOW THE AIRCRAFT FAILED TO PRESSURIZE. THE CREW OF FLIGHT 2269 CONTINUED TO DESTINATION (PHL) UNPRESSURIZED. PSA MAINTENANCE CLEANED THE PRIMARY OUTFLOW VALVE. THE SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ 200 AMM 21-31-00-710-802. THEJan 28, 2005 · N258PS · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
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