GE CF34-3B1

Service difficulty reports · 5,402

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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 = '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 VNAA0709010Intake · damagedCREW REPORTED A BIRD STRIKE ON APPROACH TO THE RIGHT HAND ENGINE INTAKE COWLING LEADING EDGE. MAINTENANCE INSPECTED AND FOUND THE DAMAGE TO BE 2 INCH LENGTH BY 1 INCH WIDTH BY .15 DEEP. DAMAGE WITHIN LIMITS IN ACCORDANCE WITH THE SHORTS CMA CMM 71-61-01. TSep 16, 2007 · N254PS · Cndair CL6002B19 · Engine Air Intake SystemSDR CA070913001Adg · unwanted deploy(CAN) DURING TAKEOFF, AS SOON AS A/C LEFT GROUND ADG DEPLOYED. CREW DECIDED TO CONTINUE FLIGHT USING ADG DEPLOY FLIGHT PROCEDURES. A/C LANDED WITHOUT INCIDENT. ADG AUTODEPLOY UNIT WAS FOUND TO HAVE BEEN REPLACED A FEW HOURS BACK DUE TO FAILURE OF UNIT`S SELF Sep 10, 2007 · Cndair CL604 · AC Generator-AlternatorSDR CHQA200700044Trim System · malfunctionedCHS TO IAH - AT 11,000FT DESCENDING TO 10,000FT, EXPERIENCED A STAB TRIM RUNAWAY. NOTICED STAB TRIM INDICATIONS FLUCTUATING EXCESSIVELY, FOLLOWED BY AN IMMEDIATE DISCONNECT OF THE AUTOPILOT AND TRIM RUNAWAY CLACKER. COMPLETED MEMORY ITEMS AND QRH DECLARED EMSep 9, 2007 · N484CA · Bombdr CL6002D15 · Stabilizer Control SystemSDR CHQA20070049Servo · malfunctionedTUL TO IAH - RECEIVED STEERING INOP MSG IN FLIGHT AND THE QRH INSTRUCTIONS WERE TO LAND WITH STEERING SWITCHED OFF. DECLARED EMERGENCY AS A PRECAUTION. LANDING WAS UNEVENTFUL AND A TUG WAS REQUESTED TO TOW THE AIRCRAFT BACK TO THE GATE. MAINTENANCE TROUBLESSep 9, 2007 · N483CA · Cndair CL6002B19 · Landing Gear Steering SystemSDR CA070911013Bpsu · faulted(CAN) THE CREW RECEIVED A FLAP FAIL MESSAGE AFTER SELECTING THE FLAP TO 0 DEGREE AFTER LANDING. THE FECU TO LT BPSU WIRING WAS INSPECTED AND NO FAULT WAS FOUND. FECU WAS REPLACED, FUNCTIONAL TEST COMPLETED AND THE AIRCRAFT RELEASED INTO SERVICE, FOUR FLIGHTSSep 8, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0709006Shutoff Valve · openCLT - FLT 2207 - CREW REPORTED A CABIN ALT CAS MESSAGE FOLLOWED BY CABIN ALT RWP MESSAGE ON CLIMB-OUT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OVERBOARD SHUTOFF VALVE OPEN. MAINTENANCE SECURED THE VALVESep 4, 2007 · N237PS · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR CA070905003Bpsu · inoperative(CAN) WING FLAPS FAILED TO FULLY EXTEND FOR LANDING. AFTER SELECTING FLAPS 8 THE CREW RECEIVED A FLAP FAULT CAUTION MESSAGE AND THE FLAPS WOULD NOT MOVE ANY FURTHER. THE CREW LANDED WITH FLAPS AT 8 DEGREES UNEVENTFULLY. FECU SHOWS LT BPSU AT FAULT. BPSU REPLACSep 4, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0709002Tire · separatedCREW REPORTED THE LEFT HAND INBOARD MAIN TIRE TREAD SEPARATED. MAINTENANCE INSPECTED AND FOUND THE TIRE FAILURE ALONG WITH A DENT IN THE NOSE COWL AND TWO DAMAGED FAN BLADES. MAINTENANCE REMOVED AND REPLACED THE DAMAGED FAN BLADES IN ACCORDANCE WITH THE AIRCSep 2, 2007 · N248PS · Cndair CL6002B19 · TireSDR VNAA0709004Oil System · overservicedWITH THE APU SUPPLYING AIR TO THE PACK, AN OIL SMELL WAS NOTED ALONG AN ANTI-ICE DUCT WING WARNING MESSAGE. MAINTENANCE INSPECTED AND PERFORMED AN OPERATIONAL TEST OF THE RIGHT HAND FUSELAGE LOOPS AND THE APU. MAINTENANCE REMOVED REPLACED THE LOOP A18WK. MASep 2, 2007 · N241PS · Cndair CL6002B19 · APU Oil SystemSDR CA080805004Heat Tape · burned(CAN) THE AFT WATER SUPPLY HEATER TAPE OVERHEATED AND BURNED. INVESTIGATION REVEALED WATER HEATER WAS RUNNING WITHOUT TEMP REGULATION. HEATER WAS REPLACED.Sep 1, 2007 · Cndair CL6002B19 · Water Line Anti-Ice SystemSDR CHQA20070043Trim Switch · malfunctionedIAH TO SDF - WHILE CLIMBING THROUGH 12,000FT EXPERIENCED A NOSE DOWN PITCH TRIM RUNAWAY. ACCOMPLISHED PITCH TRIM RUNAWAY MEMORY ITEMS AND DECLARED AN EMERGENCY. LANDED IN IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S PITCH TRIM SWITCHAug 31, 2007 · N638BR · Bombdr CL6002D15 · Stabilizer Control SystemSDR VNAA0708025Tire · separatedCREW REPORTED THE LEFT HAND INBOARD MAIN TIRE TREAD HAD PARTIALLY SEPARATED AND SHREDDED UPON LANDING. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE LEFT HAND FLAP. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND INBOARD MAIN TIRE. MAINTENANCE ISSUED TEMP REAug 30, 2007 · N260JS · Cndair CL6002B19 · TireSDR VNAA0708028Engine · bird ingestionCREW REPORTED A BIRD STRIKE TO THE RIGHT ENGINE COWL. MAINTENANCE VISUALLY INSPECTED FOR INGESTION INTO THE ENGINE AND FOUND NO DEFECTS ON FAN BLADES. NO FURTHER DEFECTS NOTED IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERAug 30, 2007 · N247JS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0708023Trim Switch · stickingCREW REPORTED THE CAPTAINS TRIM SWITCH STICKING AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 29, 2007 · N251PS · Cndair CL6002C10 · Flight Control SystemSDR VNAA0708020Tire · failedCREW REPORTED THE LEFT NOSE TIRE CAME APART ON TAKEOFF. CREW ELECTED TO CONTINUE ON TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CONFIRMED THE LEFT NOSE TIRE FAILURE AND DAMAGE TO THE NOSE LANDING GEAR FOLLOW UP DOOR. MAINTENANCE REMOVED ANAug 27, 2007 · N213PS · Cndair CL6002B19 · TireSDR CHQA200700042Apu · overservicedSDF TO IAH - DURING APPROACH INTO IAH, CREW RECEIVED "APU OVERTEMP" AURAL WARNING AND MESSAGE AFTER SWITCHING BLEEDS TO APU. CREW OBSERVED THE TEMPERATURE REACHED 999 DEGREES CELSIUS. COMPLETED THE QRH FOR APU OVERTEMP MSG. EGT WAS SUSTAINED AT 999 DEGREES Aug 26, 2007 · N642BR · Bombdr CL6002D15 · APU Oil SystemSDR A6WA200740482Check Valve · fluctuatesAT FLIGHT LEVEL 28 NOTED OIL FLUCTUATION ON RIGHT ENGINE. RAN QRH. FLUCTUATION MAINTAINED ABOVE 28-40 PSI INDICATED. DECLARED AN EMERGENCY. LANDED WITHOUT ANY PROBLEMS. FOUND LEAK ON ENGINE SERVICING LINE TO RT ENGINE, ALONG WITH AN OPEN OIL SERVICE CHECKAug 23, 2007 · N446AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0708014Static Wick · damagedCREW REPORTED A LIGHTNING STRIKE ON LEFT SIDE OF NOSE. MAINTENANCE PERFORMED A VISUAL EN ROUTE INSPECTION FOR LIGHTNING STRIKE DAMAGE. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE LEFT HAND HORIZONTAL STAB TIP AND STATAug 21, 2007 · N249PS · Cndair CL6002B19 · Static Discharge SystemSDR CA070823012Switch · failed(CAN) DURING LANDING ROLLOUT CREW RECEIVED MOMENTARY ILLUMINATION OF (BOTTLE ARMED PUSH TO DISCH) FOR RT ENG. CREW WAS CHECKING FOR TRAFFIC AS HAD BEEN CLEARED ACROSS ANOTHER RUNWAY. WHEN ACROSS THIS RUNWAY NOTICED RED (R ENG OIL PX) AND RT ENG N1 AND N2 (ZEROAug 21, 2007 · Cndair CL6002B19 · Fire DetectionSDR VNAA0708011Tire · separatedCREW REPORTED DURING LANDING ROLLOUT RECEIVING A WOW INPUT CAUTION AND A PROX SYSTEM FAULT STATUS MESSAGES. MAINTENANCE INSPECTED AND FOUND THE LEFT HAND INBOARD MAIN TIRE TREAD HAD SEPARATED FROM THE WHEEL ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE MAINAug 20, 2007 · N262PS · Cndair CL6002B19 · TireSDR CA070906009Blades · damaged(CAN) A/C DIVERTED DUE TO NR 2 ENG. VIBRATION AND LOUD NOISE. NR 2 ENGINE WAS SHUTDOWN IN FLIGHT. PILOT DECLARED AN EMERGENCY. CONTRACT MAINTENANCE FOUND THE EXHAUST TURBINE BLADES DAMAGED. PRELIMINARY INSPECTION THAT THE LAST STAGE TURBINE WITH TOTAL DAMAGEAug 13, 2007 · Cndair CL6002B19 · Turbine SectionSDR MASA200700500Compressor · seizedASH 7433 MHT-IAD ABORTED T/O DUE TO A NR 2 TR DISAGREE, AND POSSIBLE COMPRESSOR STALL. MX INSPECTED THE ENGINE, AND FOUND IT TO BE SEIZED. MX IS CURRENTLY TROUBLESHOOTING.Aug 12, 2007 · N650ML · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR VNAA0708007Tire · separatedCREW REPORTED THE RIGHT HAND NOSE TIRE TREAD SEPARATED ON TAKEOFF. CREW DECLARED AN EMERGENCY AND CONTINUED ON TO CLT WHERE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CONFIRMED THE RIGHT HAND NOSE TIRE TREAD HAD SEPARATED AND CAUSED DAMAGE TAug 11, 2007 · N260JS · Cndair CL6002B19 · TireSDR VNAA0708008Pump · failedCREW REPORTED RECEIVING A LOW OIL PRESSURE WARNING MESSAGE FOR THE RIGHT HAND ENGINE. CREW DECLARED AN EMERGENCY AND SHUT DOWN THE ENGINE. CREW LANDED IN PIT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SCAVENGE OIL PUMP IN ACCORDANCE WITH THE AIRAug 11, 2007 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0708009Tire · separatedCREW REPORTED THE RIGHT HAND MAIN TIRE LOST ITS TREAD. MAINTENANCE INSPECTED AND CONFIRMED THE TREAD LOSS IN ADDITION TO DAMAGE TO THE RIGHT HAND INBOARD FLAP BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND INBOARD TIRE IN ACCORDANCE WITH THE AIAug 11, 2007 · N207PS · Cndair CL6002B19 · TireSDR VNAA0708006Ecu · failedCREW REPORTED A FLAPS FAIL AT 20 DEGREES. CREW DIVERTED TO ILM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE FLAP ELECTRONIC CONTROL UNIT TO BE CAUSING ERRATIC MESSAGES. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE AIRAug 10, 2007 · N244PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0708004Fire Bottle · dischargedCREW REPORTED A CARGO BOTTLE LOW CAUTION MESSAGE ON CLIMBOUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED THE CARGO FIRE EXTINGUISHING SYSTEM PER MEL 26-25-01. MAINTENANCE REMOVED AND REPLACED THE CARAug 9, 2007 · N245PS · Cndair CL6002B19 · Fire Bottle, FixedSDR CA070812001Priority Valve · faulty(CAN) ON APPROACH, GEAR WAS SELECTED DOWN AND THE NOSE GEAR DID NOT COME DOWN. THE CREW THEN CYCLED THE GEAR, BUT THE NOSE GEAR STILL DID NOT COME DOWN. THE CREW SWITCHED 3B HYDRAULIC PUMP FROM AUTO TO ON AND 30 SECONDS LATER THE NOSE GEAR CAME DOWN. THE LAAug 9, 2007 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0760518Engine · malfunctionedFLIGHT 5141 - ON TAKEOFF ROLL, NR 1 ENGINE WOULD NOT ACCELERATE PAST 43 PERCENT. THE ITT WENT TO 500 DEGREES BUT NOT BEYOND. PERFORMED ENGINE GROUND RUNS. FOUND ENGINE TO RUN WITHIN LIMITS.Aug 4, 2007 · N416CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0708001Trim System · out of limitsCREW REPORTED ON TAKEOFF ROLL, RECEIVED A RED WARNING MESSAGE INDICATING A TAKEOFF CONFIGURATION. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE AILERON TRIM OUT OF LIMITS FOR TAKEOFF CONFIGURATION. MAug 1, 2007 · N259PS · Cndair CL6002B19 · Aileron Control SystemSDR VNAA0707019Thermocouple · faultyCREW REPORTED AN EICAS COMP MON IN FLIGHT WITH ERRATIC ITT INDICATIONS TO THE LEFT HAND ENGINE. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT THE LEFT HAND ENGINE OUTBOARD THERMO COUPLE ASSEMBLY. MAINTENANCE REMOVEDJul 31, 2007 · N258PS · Cndair CL6002B19 · Engine EGT/TIT Indicating SystemSDR A6WA200740425Skin · gougedRT WING IB FLAP LOWER SKIN GOUGED/DENTED APPROX 3 INCHES LONG X 3 INCHES WIDE X .205 INCH DEEP, ADJACENT TO RIB AT WS 74.8, APPROX 8 INCHES AFT OF LEADING EDGE OF FLAP. (K) MAINTENANCE REPAIRED FLAP LOWER SKIN IAW BSC EO 601R-57-12572. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200740426Skin · corrodedRT WING LOWER PLANK ACCESS HOLE NR 1 640BB HAS MINO CORROSION IN NON-CRITICAL AREAS APPPROX .003 DEEP AND 2.5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW BSC REO 601R-57-21-030 REV F. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740427Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 1 540BB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .003 INCH DEEP AND 5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740428Skin · corrodedLT WING PLANK LOWER ACCESS HOLE NR 2 510AB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .005 DEEP AND 5 INCHES LONG. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA0707018Flap · malfunctionedCREW REPORTED A FLAPS FAIL AT 20 DEGREES BOTH SIDES ON TAKEOFF. CREW FOLLOWED THE QRH, DIVERTED TO ILM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TESTS OF THE FLAPS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 27-54-0Jul 28, 2007 · N221PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200701071Seat Track · corroded2 SEAT TRACKS IN CARGO BAY CORRODED, 1 MARKED, 1 REMOVED. 10-18-07 INSTALLED SEAT RAIL, FOR RIGHT 9G WALL, PN 601R38779-9 IAW CRJ 200 53-01-11 MM13267 7-28-07. UPON INSTALLION OF SEAT TRACK FOR CENTER 9G WALL FOUND INCORRECT PART HAD BEEN OREDERED. REMOVJul 27, 2007 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200701072Web · crackedFS 280 WEB IS CRACKED OB OF RBL 9. REPAIRED 280 WEB RBL 9 C/W IAW EC/TC REO 601R-53-11-1218.Jul 27, 2007 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740429Drag Angle · crackedAFT PAX DOOR DRAG ANGLE (PN 601R31772-5) IS CRACKED AT PREVIOUS REPAIR APPROX .5 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED DRAG ANGLE ON AFT PAX DOOR IAW REO 601R-52-11-513. (M)Jul 27, 2007 · N420AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740430Skin · crackedSKIN UNDER PAX DOOR AFT DRAG ANGLE IS CRACKED AT 3RD FASTENER DOWN APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED AFT DRAG ANGLE IAW EO 601R-52-12354. (M)Jul 27, 2007 · N420AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740419Channel · crackedHYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL CRACKED APPROX .1 LONG IN LT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-159 IAW CRJ 200 SRM 51-42-06. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740421Angle · crackedRT 484 ANGLE IS CRACKED AT RBL 36 APPROX .25 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740422Angle · crackedRT 484 ANGLE IS CRACKED AT RBL 27 APPROX 1 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740423Angle · crackedLT 484 ANGLE IS CRACKED AT LBL 27 APPROX .5 INCHES LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740424Angle · crackedLT 484 ANGLE IS CRACKED AT LBL 36 APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740420Bracket · crackedHYDRAULIC PRESSURE BRACKET IS CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-157 IAW CRJ 200 SRM 51-42-06. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200701069Angle · crackedAAR-Z2020 280 AFT ANGLE COMMON TO THE EMERGENCY RELEASE CABLE OB OF LBL 9 IS CRACKED. (RESOLVED ON W/O: 65467 TASKCARD: N/R-00059 ) DUPLICATE WRITE-OFF. {SUPPLEMENTAL - SDR CLOSED 08/08/07}Jul 26, 2007 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740417Angle · crackedLT OBLIQUE ANGLE AT STA 625 HAS .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE CRJ SRM 51-42-06. (M)Jul 26, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740418Angle · crackedRT OBLIQUE ANGLE AT STA 625.00 HAS A .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06. (M)Jul 26, 2007 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740416Bulkhead · crackedFORWARD PRESSURE BULKHEAD AT FS 202.75 CRACKED AT HYDRAULIC SYS NR 3 RT IB BRAKE FITTING LT LOWER SIDE. (K) MAINTENANCE REPAIRED BULKHEAD IAW BOMBARDIER SERVICES CORP EO 601R-53-12466. (M)Jul 25, 2007 · N423AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
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