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 ASOA05658Step · brokenDURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AND MATERIAL MISSING. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K)Aug 7, 2005 · N860AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05654Sign · crackedDURING C-CHECK, THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR IAW AMM. (K)Aug 6, 2005 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05657Light · crackedDURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Aug 6, 2005 · N908EV · Cndair CL6002B19 · Emergency LightingSDR A6WA200540279Idg · lack of lubeDURING TAKEOFF ROLL 70 KNOTS IDG NR FAIL, GEN NR 2 OFF APPEARED MODERATE BREAKING BTMS READOUT 4, 5,6,7 FOUND NR 2 IDG OIL LEVEL LOW SERVICED NR 2 IDG RAN ENGINE NO LEAKS NOTED OPS CHECK GOOD IAW MM. PERFORMED RTO INSPECTION. (K)Aug 5, 2005 · N420AW · Cndair CL6002B19 · Alternator-Generator DriveSDR COMA0560428Engine · surgesFLIGHT 5063 - LEFT ENGINE SURGE 5-6 PERCENT. DEFERRED MAINTENANCE PER MEL.Aug 5, 2005 · N484CA · Cndair CL6002B19 · Engine Cowling SystemSDR ASOA05651Placard · wornDURING AN A-CHECK, THE EXIT PLACARD ON THE PASSENGER DOOR WAS FOUND NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE EXIT PLACARD ON THE PASSENGER DOOR. (K)Aug 5, 2005 · N856AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA05656Doubler · crackedDURING HANGAR MAINTENANCE, THE RT SIDE FS 640 DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT SIDE FS 640 DOUBLER IAW SRM AND EO. (K)Aug 5, 2005 · N878AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA0508007Pin · failedDURING CLIMBOUT THE CREW REPORTED THAT THE LT ENGINE THRUST LEVER WOULD NOT RETARD BELOW 93 PERCENT. THE AIRCRAFT DIVERTED TO DAY, FOLLOWED THE QRH, AND LANDED SAFELY. MAINTENANCE FOUND THE UPPER CORE COWL SUPPORT STRUT UNSECURED AND INTERFERING WITH THROTTLAug 4, 2005 · N259PS · Cndair CL6002B19 · Power LeverSDR A6WA200540277Fuel Cap · misinstalledFUEL VENTED OUT L-WING ON TAKEOFF AFTER MANUAL OVERWING FUELING LANDED AT 48000 ORD MLW 47. LT FUEL CAP FOUND TO BE INSTALLED IMPROPERLY. INSTALLED LT WING FUEL CAP PROPERLY COMPLIED WITH OVERWEIGHT INSPECTION . NO DEFECTS NOTED. (K)Aug 4, 2005 · N421ZW · Cndair CL6002B19 · Fuel StorageSDR A6WA200540278Connector · unsecureSHORTLY AFTER TAKEOFF, STRONG SMELL OF SMOKE IN COCKPIT AND CABIN. NO VISUAL SMOKE, PACK TEMP NORMAL. (AIR RETURN) DURING TAXI PACK NR 2 HI TEMP INDICATION. INSPECTED AFT EQUIPMENT BAY AREA AND FOUND RT PACK ACM TEMP SWITCH HANGING FROM CONNECTOR PLUG. NO Aug 4, 2005 · N429AW · Cndair CL6002B19 · Air Conditioning System WiringSDR ASOA05648Lamp · burned outDURING A GROUND INSPECTION, THE LOWER INTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LOWER INTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (KAug 4, 2005 · N912EV · Cndair CL6002B19 · Emergency LightingSDR ASOA05650Warning Light · illuminatedDURING APPROACH, THE CREW RECEIVED (PARKING BRAKE SOV) AND (ANTI SKID) CAUTION MESSAGES. CREW EXECUTED A GO-AROUND AND COMPLIED WITH THE QRH. UPON LOWERING THE GEAR FOR LANDING THE MESSAGES EXTINGUISHED. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY ASAug 4, 2005 · N823AS · Cndair CL6002B19 · Landing Gear Brake SystemSDR CA050923003Pin · broken(CAN) FLIGHT CREW HAD TO SHUT DOWN THE LT ENGINE ON FINAL AS THE LT THROTTLE WOULD NOT RETARD BELOW 93 PERCENT. THE THROTTLE WAS ABLE TO ADVANCE TO PROVIDE MORE POWER, BUT WOULD NOT RETARD BELOW 93 PERCENT. FOUND THAT THE UPPER COWL PIN HOLDING THE ROD HAD BAug 4, 2005 · Cndair CL6002B19 · Engine Cowling SystemSDR ASOA05653Handle · corrodedDURING A C-CHECK, THE CREW ESCAPE HATCH OUTER HANDLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH OUTER HANDLE ASSY IAW SRM. (K)Aug 3, 2005 · N854AS · Cndair CL6002B19 · Emergency ExitsSDR VNAA0508004Switch · failedDURING CRUISE THE STAB TRIM CAUTION MESSAGE ILLUMINATED. THE CREW SUCCESSFULLY RE-ENGAGED THE SYSTEM AND CONTINUED TO DTW. MAINTENANCE REMOVED & REPLACED THE CAPTAIN'S PITCH TRIM DISCONNECT SWITCH IAW CRJ200 AMM 27-41-30-000(400)-802. OPERATIONAL CHECKS WERAug 2, 2005 · N246PS · Cndair CL6002B19 · Stabilizer Position IndicatingSDR VNAA0508006Outflow Valve · malfunctionedDURING CLIMBOUT THE OVERBOARD COOL CAUTION MESSAGE ILLUMINATED AND THE CABIN DID NOT PRESSURIZE. THE CREW RETURNED TO DAY. MAINTENANCE FOUND THE OVERBOARD EXHAUST SHUTOFF VALVE OPEN. THE SOV WAS SECURED CLOSED IAW CRJ200 AMM 21-24-00-040-806 AND MEL 21-24-0Aug 2, 2005 · N253PS · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR REX2005F00001Control System · malfunctioned(REF NR: 05-093) FLAPS FAIL AT 20 WHEN SELECTED ON TAXI. RESET SYSTEM AND PLACED 72 HOUR WATCH IAW AD 98-20-01. (K)Aug 2, 2005 · N8965E · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00002Acm · inoperative(REF NR: 05-094) IN FLIGHT CABIN HAD FUMES AND POSSIBLE SMOKE. QRH FOLLOWED DIVERTED WITH UNEVENTFUL LANDING. TROUBLESHOT AIRCRAFT AND ENGINES DOWN TO THE RT AIR CYCLE MACHINE (ACM). REMOVED AND REPLACED RT ACM IAW AMM. OPS CHECKED GOOD. (K)Aug 2, 2005 · N8698A · Cndair CL6002B19 · Cabin Cooling SystemSDR ASOA05646Battery Pack · dischargedDURING A GROUND INSPECTION, THE EXTERIOR EMERGENCY LIGHTS AND THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE DIM. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT EMERGENCY BATTERY PACKS. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Aug 2, 2005 · N919EV · Cndair CL6002B19 · Emergency LightingSDR VNAA0508001Structure · lightning strikeEVIDENCE OF LIGHTNING DAMAGE ON THE RIGHT WINGLET WAS FOUND DURING THE SERVICE CHECK. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-220-803. NO OTHER DEFECTS WERE FOUND. THE WINGLET WAS TEMP REPAIRED IAW BOMBARDIER REO 601R-Aug 1, 2005 · N213PS · Cndair CL6002B19 · Wing Main, Frame StructureSDR VNAA0508002Sensor · failedNR 2 ENGINE N1 STARTED FLUCTUATING +/-10% WHILE CLIMBING THROUGH 21,000 FT. THE AIRCRAFT RETURNED TO PHL WHERE MAINTENANCE REMOVED AND REPLACED THE T2C COMPRESSOR INLET TEMPERATURE SENSOR IAW CRJ200 AMM 73-21-09-000(400)-801. ALL GROUND OPERATIONAL CHECKS WEAug 1, 2005 · N230PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0507024A/C Pack · malfunctionedDURING CRUISE, WITH THE LT PACK DEFERRED, THE RT PACK HIGH PRESS CAUTION MESSAGE ILLUMINATED. THE CREW RETURNED TO CLT. MAINTENANCE OPERATIONALLY TESTED THE AIR CONDITIONING SYSTEM IAW CRJ200 AMM 21-51-00-710-801. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS REJul 30, 2005 · N237PS · Cndair CL6002B19 · Cabin Cooling SystemSDR ASOA05647Anchor Fitting · crackedDURING HANGAR MAINTENANCE, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. (K)Jul 30, 2005 · N913EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA0507023Cowling · damagedAFTER POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT ENGINE LOWER NOSE ACCESS COWL WAS MISSING. THE COWL WAS FOUND ON THE RUNWAY. MAINTENANCE INSTALLED A SERVICEABLE NOSE ACCESS COWL IAW CRJ200 AMM 71-14-01-400-802. THE AIRCRAFT WAS THEN RELEASED FOJul 29, 2005 · N226JS · Cndair CL6002B19 · Powerplant SystemSDR ASOA05642AACable · bindingDURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN OR LOCK AND TH DOOR ASSIST MOTOR WOULD NOT OPERATE THE DOOR ALL THE WAY. MAINTENANCE FOUND THE DOOR ASSIST CABLE WRAPPED AROUND THE DOOR HINGE AND REMOVED IT FROM AROUND THE HINGE. OPERATIONAL HECJul 29, 2005 · N836AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05643Lamp · burned outDURING OVERNIGHT MAINTENANCE, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT OVERWING EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 29, 2005 · N842AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05644Lamp · burned outDURING HANGAR MAINTENANCE, THE RT FWD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT FWD EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 29, 2005 · N880AS · Cndair CL6002B19 · Emergency LightingSDR VNAA0507020Radome · lightning strikeTHE CREW REPORTED A POSSIBLE LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801 & 05-51-05-220-801. MINOR PAINT DAMAGE ON THE RADOME WAS DAI'D. THE AIRCRAFT WAS RELEASED FOR SERVICE.Jul 28, 2005 · N223JS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540271Rib · crackedLT MLG WHEEL WELL BATT RIB AT WS 48.30, FS 523.8 IS CRACKED AT UPPER RADIUS APPROX 1.25 INCH LONG. REPAIRED IAW REO. (K)Jul 28, 2005 · N405AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR REX2005F00000Proximity Switch · loose(REF NR: 05-092) GEAR DISAGREE WARNING AFTER TAKEOFF, DURING GEAR RETRACTION. RT MAIN SHOWS IN TRANSIT. FOLLOWED QRH WITH UNEVENTFUL LANDING. INTERROGATED PSEU, FOUND TARGET FOR RT MLG UPLOCK PROXIMITY SWITCH LOOSE. TIGHTENED TARGET IAW AMM AND PERFORMED Jul 27, 2005 · N8525B · Cndair CL6002B19 · Landing Gear Position and WarningSDR REX2005F00012Control System · failed(REF NR: 05-091) FLAPS FAIL AT 30 DEGREES ON APPROACH, QRH FOLLOWED. LANDING UNEVENTFUL. FOUND FCL NOT IN 30 DETENT. RESET FLAPS AND COMPLIED WITH AD-98-20-01. MONITORING FLAPS FOR 72 HOURS. (K)Jul 27, 2005 · N8495B · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA05639Handle · bindingDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND HARD TO OPEN FROM THE OUTSIDE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR OUTER HANDLE. OPS CHECK GOOD. AIRCRAFT OF FOR SERVICE. (K)Jul 27, 2005 · N868AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05640Step · brokenDURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY AND STEP RETRACTION ARM ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 27, 2005 · N839AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540269Angle · crackedLT FS 484, LBL27, ANGLE IS CRACKED APPROX 1.25 INCH L THRU THICKNESS OF MATERIAL AT UPPER END OF RADIUS. REMOVED CRACKED ANGLE, FABED NEW ANGLE FROM ANGLE TO SMPLE AND INSTALLED IAW SRM. (K)Jul 26, 2005 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05637Seat Track · corrodedDURING C-CHECK, THE LT SIDE WALL SEAT RAIL (TRACK) AT FS 559 +64 ABOVE THE BLOWOUT PANEL WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT SIDE WALL SEAT RAIL (TRACK) AT FS 559 +64 IAW SRM. (K)Jul 26, 2005 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA05638Lamp · burned outDURING A ROUTINE OVERNIGHT CHECK, THE LT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LT FORWARD EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 26, 2005 · N912EV · Cndair CL6002B19 · Emergency LightingSDR A6WA200540261Clip · crackedFS 280, RBL 9, IB CLIP ANGLE IS CRACKED 1 INCH LONG. REMOVED AND REPLACED FS 280, RBL9, IB CLIP IAW SRM. (K)Jul 25, 2005 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR CA050726006Wire Harness · burnedDURING CLIMB, IDG NR 2 DROPPED OFF LINE. MAINTENANCE FOUND THE GENERATOR NR 2 CABLE AND TERMINAL BURNT IN JB1. THE TERMINAL ATTACHMENT HARDWARE WAS FOUND LOOSE ON THE TERMINAL BLOCK STUD INSIDE THE JB1. DAMAGED PARTS, ELECTRICAL HARNESS, 601R57640-1PE- PHENJul 25, 2005 · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA200540262Clip · crackedFS 280, LBL 9, IB CLIP ANGLE IS CRACKED, 1 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9, IB CLIP IAW SRM. (K)Jul 25, 2005 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540263Angle · crackedFS 280, LBL 9, CLIP ANGLE IS CRACKED, 1 INCH LONG. REMOVED AND REPLACED CLIP ANGLE FS 280, LBL 9, OB, IAW SRM. (K)Jul 25, 2005 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540273Clip · crackedFS 280, RBL 9, OB, CLIP ANGLE IS CRACKED 1 INCH LONG. REMOVED AND REPLACED ANGLE IAW EO AND SRM. (K)Jul 25, 2005 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA0507022Fire Bottle · dischargedTHE CARGO BTL LOW CAUTION MESSAGE ILLUMINATED IN FLIGHT. THE CREW RETURNED TO CLT WHERE MAINTENANCE DEFERRED THE CARGO FIRE EXTINGUISHING SYSTEM IAW MEL 26-25-01C AND RELEASED THE AIRCRAFT FOR SERVICE. MAINTENANCE IN TYS REMOVED & REPLACED THE LT CARGO COMPAJul 25, 2005 · N221PS · Cndair CL6002B19 · Extinguishing SystemSDR ASOA05634Light · inoperativeDURING INSPECTION, THE GREEN EMERGENCY LIGHTING FORWARD OF ROW 5 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE SECTION OF EMERGENCY FLOOR STRIP LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 25, 2005 · N847AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05635Step · separatedDURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO HAVE A BROKEN ATTACH BRACKET. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. AIRCRAFT OK FOR SERVICE. (K)Jul 25, 2005 · N834AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540264Skin · dentedLT WING IB FLAP INNER SKIN IS DENTED BETWEEN FLAP STATION 142 AND 147 AT THE INTERCOSTAL SPAR AREA. DEN MEASURES .850 INCH LT X .800 INCH X .067 INCH DEEP. PERFORMED REPAIR BY CUTTING OUT DAMAGE AND INSTALLING 11.5 INCH X 3 INCH FLUSH REPAIR IAW SRM REPAIR Jul 24, 2005 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200540265Skin · chafedLT WING IB FLAP, IB END AT FLAP STA 50.498 IB BELOW THE LEADING EDGE IS CHAFED FROM THE STUB FAIRING. CHAFE MEASURES 1.50 INCH LONG X .50 INCH WIDE X .035 INCH DEEP. (K)Jul 24, 2005 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR CA050726007Cowl Door · missingAIRCRAFT DIVERTED AFTER DEPARTURE, FOR NR 1 ENGINE OIL PRESSURE INDICATION PROBLEM. UPON ARRIVAL AT GATE FOUND UPPER HALF OF LT CORE COWL MISSING.Jul 24, 2005 · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR VNAA0507018Door · openDURING CLIMB PASSING 10,500 FT THE FLIGHT ATTENDANT NOTICED AN INCREASE IN NOISE LEVEL AROUND THE SERVICE DOOR. THE F/A REPORTED THAT THE GREEN INDEX MARKS ON THE INDICATOR WINDOW WERE NOT ALIGNED. COCKPIT INDICATIONS WERE NORMAL. THE FLIGHT RETURNED TO PHLJul 24, 2005 · N218PS · Cndair CL6002B19 · Service DoorsSDR A6WA200540266Fitting · looseHORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 3 LOOSE MOUNT BOLTS ON LT SIDE OF FITTING. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K)Jul 24, 2005 · N420AW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR A6WA200540267Drag Angle · crackedPASSENGER DOOR STAIR AFT DRAG ANGLE IS CRACKED, .5 INCH LONG IN RADIUS (ADJACENT TO MOUNT FOR PASSENGER DOR ASSIST CABLE PULLEY). REMOVED DAMAGED SECTION OF ANGLE, FABRICATED REPAIR ANGLE AND INSTALLED ANGLE IAW REO. (K)Jul 24, 2005 · N420AW · Cndair CL6002B19 · Passenger/Crew Doors
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