GE CF34 series

Service difficulty reports · 1,368

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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 = 'CF34'
  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 ASOA04328Bpsu · malfunctionedDURING APPROACH, THE CREW RECEIVED A FLAPS FAIL AMBER CAUTION MESSAGE. THE FLAPS INDICATED ZERO DEGREES ON THE PRIMARY EICAS AND SYNOPTIC PAGES AND THE FLAPS HAD NOT BEEN CALLED FOR PRIOR TO THE CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND EMERGENCY VEHICLMay 3, 2004 · N923EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA04329Light · inoperativeDURING A GROUND INSPECTION, THE LT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.May 3, 2004 · N853AS · Cndair CL6002B19 · Emergency LightingSDR ASOA04325Light · missingDURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT NEAR ROW 8 WAS FOUND MISSING. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT NEAR ROW 8. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE.May 1, 2004 · N863AS · Cndair CL6002B19 · Emergency LightingSDR ASOA04326Actuator · out of rigDURING CRUISE, AT APPROXIMATELY 26,000 FEET THE CREW RECEIVED A LT REVERSER UNLOCK MESSAGE. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT DIVERTED. FIRE AND RESCUE VEHICLES WERE REQUESTED TO BE ON STAND BY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENAMay 1, 2004 · N908EV · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA04338Step · crackedDURING C-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP.Apr 30, 2004 · N707EV · Cndair CL6002C10 · Entrance StairsSDR WVE2004F00010Angle · crackedRT WING STA 48.30 ANGLE PN 600-1020428 IS CRACKED , 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06.Apr 26, 2004 · N408SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR WVE2004F00011Angle · crackedLT WING STA 48.30 ANGLE PN 600-1020427 IS CRACKED 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06.Apr 26, 2004 · N408SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR WVE2004F00012Sill · corrodedLT FLOOR SILL PN 601R3114863 BETWEEN FS 364 AND FS 379 IS SEVERELY CORRODED. PROBABLE CAUSE: POSSIBLE WATER INTRUSION. (EA09200402076)Apr 26, 2004 · N408SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR F03053Mechanism · lack of lubeMAINTENANCE WAS CALLED OUT TO THE PLANE BECAUSE THE CREW COULD NOT GET THE MAIN CABIN DOOR REOPENED AFTER CLOSING IT. MAINTENANCE DISASSEMBLED THE DOOR, LUBED AND CLEANED, REASSEMBLED AND ALL FUNCTIONAL AND OPS CHECKS GOOD. CONTROL NR 112617.Apr 25, 2004 · N906FJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR WVE2004F00004Bushing · lack of lubeLT VERTICAL STABILIZER PIVOT FITTING FOR THE HORIZONTAL STABILIZER HAS BUSHING (PN 601R55310025) MIGRATED AT WL 235.00, LBL 4.10. PROBABLE CAUSE: PIVOT PIN LUBRICATION NOT ADEQUATE. (EA09200401997)Apr 20, 2004 · N408SW · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous StructureSDR WVE2004F00005Attach Angle · crackedENGINE SUPPORT BEAM LEFT UPPER ATTACHMENT ANGLE (PN 6013500661) AT FS 640, WL 115, LBL 45, STRINGER 9 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200401997)Apr 20, 2004 · N408SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR WVE2004F00013Bulkhead · crackedBULKHEAD FS 202.75 LBL 24 BETWEEN STRINGERS 20L AND 21L IS CRACKED PROTRUDING FROM CUTOUT FOR PARKING BRAKE CONTROL ROD. VIBRATION AND STRESS FROM CABLE ARE THE PROBABLE CAUSE. INSTALL DOUBLER ON BULKHEAD.Apr 20, 2004 · N408SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR WVE2004F00006Attach Angle · crackedFS 484 WATERLINE 73 LBL 27 OB INTERCOSTAL ATTACHMENT ANGLE (PN 601R3117117) IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997)Apr 19, 2004 · N408SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR WVE2004F00007Skin · crackedFUSELAGE SKIN IS CRACKED AT THE CORNERS OF THE NOSE LANDING GEAR CUT OUT AT FS 235, RBL 6 AND LBL 6, STINGERS 26 R AND 26L. PROBABLE CAUSE: STRESS (EA09200401997)Apr 19, 2004 · N408SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR WVE2004F00008Attach Angle · crackedFS 484 WATERLINE 73 RBL 27 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R311719 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESSApr 19, 2004 · N408SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR WVE2004F00009Attach Angle · crackedFS 484 WATERLINE 73 RBL 9 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R311719 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997)Apr 19, 2004 · N408SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440045Skin · dentedFORWARD SERVICE DOOR JAMMED. TWO DENTS FORWARD OF RT FORWARD SERVICE DOOR. DENTS OUT OF LIMITS. COMPLIED WITH REPAIR BRAS EO 601R-53-4835 STEPS 1, 2, 3, 4 AND 5. PERFORMED REPAIR OF SERVICE DOOR STRINGER 16/17 OF FIG 245 AND STRINGER 13/14 FIG 295. (M)Apr 17, 2004 · N463AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR USA2004F00026Control Lever · malfunctionedCREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER TO THE (UP) POSITION AFTER TAKEOFF. FLIGHT RETURNED WITHOUT INCIDENT. MAINTENANCE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE. OPERATIONALLY CHECKS SATISFACTORY.Apr 16, 2004 · N802MD · Emb ERJ170100 · Landing Gear SelectorSDR USA2004F00027Module · faultyCREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER TO THE (UP) POSITION AFTER TAKEOFF. FLIGHT RETURNED WITHOUT INCIDENT. MAINTENANCE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE OPERATIONALLY CHECKS SATISFACTORY.Apr 16, 2004 · N802MD · Emb ERJ170100 · Landing Gear Retraction/Extension SystemSDR ASOA04327Light · inoperativeDURING A (C) CHECK, THE FORWARD 3 SECTIONS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD 3 SECTIONS OF EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD.Apr 15, 2004 · N910EV · Cndair CL6002B19 · Emergency LightingSDR A6WA200440044Flap · inoperativeFLAP FAIL MESSAGE. FLAPS AT ZERO, COMPLIED WITH QRH-WEIGHT AT TOUCHDOWN 41,800 LBS, APPROXIMATE SPEED 115 KNOTS. BRAKE APPLICATION 55 MAX BRAKE TEMP 2. RESET FLAPS IAW SUPPLEMENT 98-18 FLAPS OPERATE NORMAL AT THIS TIME.Apr 14, 2004 · N418AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200440042Bushing · failedWHILE REMOVING LT MLG FOR FITTING REPLACEMENT IT WAS DISCOVERED THAT LT MLG AFT TRUNNION BUSHING IS MIGRATED. REMOVED MIGRATED BUSHING, INSTALLED 1ST OVERSIZE BUSHING AND LINE REAMED TO 2.4379 INCHES ALL WORK DONE IAW BRAS EO 601R-32-4827 AND MFG SB 601R-32-0Apr 13, 2004 · N427ZW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200440043Bushing · failedWHILE REMOVING RT MLG FOR FITTING REPLACEMENT, IT WAS DISCOVERED THAT RT MLG AFT TRUNNION BUSHING IS MIGRATED. REMOVED MIGRATED BUSHING, INSTALLED 2ST OVERSIZE BUSHING AND LINE REAMED TO 2.4379 INCH ALL WORK DOEN IAW BRAS EO 601R-32-4827 AND MFG SB 601R-32-05Apr 13, 2004 · N427ZW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASO2004F00002Warning Light · illuminatedDURING TAKEOFF, THE CREW RECEIVED A GEAR DISAGREE WARNING AFTER SELECTING THE GEAR UP POSISTION. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFELY. MAINT FOUND MAINTENANCE DIAGNOSTIC COMPUTER (MDC) FAULTS FOR ALL TApr 13, 2004 · N724EV · Cndair CL6002C10 · Landing Gear Position and WarningSDR USA2004F00028Antenna · lightning strikePILOT LOST VHF 1, 2 AND 3 SHORTLY AFTER TAKEOFF. PILOT REPORTED STATIC DISCHARGE AT 12,000 FT. MAINTENANCE FOUND LIGHTENING STRIKE THAT DAMAGED VHF 1, 2 AND 3 ANTENNA`S. MAINTENANCE ACTION: COMPLIED WITH LIGHTENING STRIKE INSPECTION. REPAIRED VHF 1 AND 2 AApr 13, 2004 · N803MD · Emb ERJ170100 · VHF Communications SystemSDR USA2004F00032Bellcrank · damagedWHILE ATTEMPTING TO OPEN THE MAIN ENTRY DOOR, THE FLIGHT ATTENDANT NOTICED THE SLIDE DROPPING OUT OF ITS COVER. MAINTENANCE WAS CALLED TO DISCONNECT THE GIRT BAR AND REPLACE THE SLIDE. REMOVED SLIDE GIRT BAR BUT UNABLE TO INSTALL SAME GIRT BAR DUE TO DAMAGEDApr 8, 2004 · N801MA · Emb ERJ170100 · Emergency EquipmentSDR CA040413001Spring · missing(CAN) PASSENGER SEATBELT BUCKLE WAS FOUND TO HAVE NO SPRING TENSION IN THE LOCK POSITION. THE DRIVE SCREW PIN HAD BACKED OFF .0312 WHICH ALLOWED TENSION TO RELEASE. BELT ASSEMBLY IS SAFTEY PRODUCTS. THE BUCKLE IS STAMPED. THIS IS A MID COAST STC INTERIOR IApr 4, 2004 · Cndair CL604 · Passenger Compartment EquipmentSDR ASO2004F00003Engine · contaminatedDURING CLIMB OUT, THE CREW RECEIVED A FORWARD LAVATORY SMOKE MESSAGE ACCOMPANIED BY SMOKE INTO THE COCKPIT ALONG WITH AN ODOR IN THE COCKPIT AND CABIN. THE SMOKE DISSIPATED FOLLOWING COMPLIANCE WITH THE LAVATORY SMOKE CHECKLIST. AN EMERGENCY WAS DECLARED WITApr 2, 2004 · N717EV · Cndair CL2151A10 · Engine (Turbine/Turboprop)SDR VNAA0404002Warning Light · illuminatedDURING TAKEOFF, THE CREW RECEIVED A RED ANTI-ICE DUCT MESSAGE AND ABORTED TAKEOFF. AS THE POWER LEVERS WERE RETARDED, THE MESSAGE CLEARED BY ITSELF AND FLIGHT 2228 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT.Apr 1, 2004 · N229PS · Cndair CL6002B19 · Central WarningSDR VNAA0404003Fire Loop · out of positionDURING TAKEOFF, THE CREW RECEIVED A RED ANTI-ICE DUCT MESSAGE AND ABORTED TAKEOFF. MAINTENANCE WAS DISPATCHED FROM DAY TO CLE. MAINTENANCE THEN INSPECTED AND FOUND THE LEFT HAND FIRE LOOP PUSHED DOWN ON THE BLEED DUCT. MAINTENANCE RELOCATED THE FIRE LOOP Apr 1, 2004 · N229PS · Cndair CL6002B19 · Fire DetectionSDR VNAA0403019Power Supply · failedAIRCRAFT N209PS WAS A SPARE AIRCRAFT IN DAY. THE NR 1 EMERGENCY BATTERY POWER SUPPLY WAS FOUND TO BE BAD. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY BATTERY POWER SUPPLY IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKMar 31, 2004 · N209PS · Cndair CL6002B19 · Emergency LightingSDR VNAA0403017Indicator · inoperativeAIRCRAFT N229PS HAD ITS STANDBY ATTITUDE INDICATOR MEL'D. THE DESTINATION CITY, PHL, WAS REPORTING FOG. THEREFORE, FLIGHT 2233 HAD TO DIVERTED TO PIT DUE TO WEATHER.Mar 28, 2004 · N229PS · Cndair CL6002B19 · Attitude Gyro and Indicating SystemSDR ASOA04244Skin · crackedDURING HANGER MAINTENANCE, THE SKIN UNDER THE RT IB MULTIFUNCTIONAL SPOILER AT THE IB BRACKET WAS FOUND CRACKED. MAINT IS TO PERFORM A DETAILED VISUAL INSP FOR PROGRESSION OF THE CRACK AT EVERY SUBSEQUENT SERVICE CHECK, UP TO A MAX OF 100 FLIGHT HRS IAW REO 6Mar 27, 2004 · N709EV · Cndair CL6002C10 · Wing, Plate/SkinSDR WVE2004F00003Attach Angle · crackedFS 484 WATERLINE 73 LBL 9 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R3117127 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997)Mar 19, 2004 · N408SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 2004FA0000318Oxygen System · failedDURING A 12 MONTH OXYGEN SYS OPERATIONAL TEST, FOUND NO OXYGEN FLOW TO LT SIDE CABIN MASKS (6 EA) LOCATED IN LT CABIN OVERHEAD PASSENGER SERVICE UNIT. (PSU) 6 MASKS SUPPLY EMERGENCY OXYGEN FOR 4 LT CABIN SEATS. THERE WAS SUFFICIENT PRESSURE IN THE SYSTEM FOR Mar 16, 2004 · N316FX · Cndair CL6002B16 · Passenger Oxygen SystemSDR VNAA0403010Odor · detectedTHE CREW REPORTED A CARGO OVERHEAT MESSAGE AND A STRONG ELECTRICAL ODOR IN THE CABIN. OUSTATION MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DISCREPENCIES. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS IN ACMar 15, 2004 · N218PS · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200440030Warning Light · false activationSMOKE CARGO WARNING WHILE TAXIING. RETURN TO GATE. CARGO PIT CHECK FOR SMOKE, NONE NOTED. NO ODOR NOTED. COMPLIED WITH OPS TEST OF CARGO SMOKE DETECTION SYSTEM. IAW MM 26-15-00. OPS CHECK GOOD.Mar 11, 2004 · N425AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA200440029Torque Link · disconnectedAFTER TAKEOFF SELECTED GEAR UP, GOT GEAR UP DISAGREE. RAN THROUGH CHECKLIST AND RETURNED. ALSO, GOT NWS INOPERATIVE, WOW INPUT CAS MESSAGE. INSPECTED AND FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS (PN 16144-101UPPER, 16154-101 LOWER).Mar 10, 2004 · N446AW · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA200440028Bushing · looseLT MLG AFT TRUNNION BUSHING IS MIGRATED .058. REMOVED AND REPLACED LEFT MLG AFT TRUNNION BUSHING USING FIRST OVERSIZE BUSHING P/N 601R-5721003-21 IAW CRJ SB 601R-32-054 REV B PART B STEP 3A-3E. (M)Mar 10, 2004 · N424AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200440027Warning Light · illuminatedSMOKE CARGO WARNING MESSAGE DURING TAXI. COMPLIED WITH IMMEDIATE ACTION CHECKLIST QRH. CARGO BOTTLE LOW CAUTION MESSAGE. MESSAGE SMOKE CARGO EXTINGUISHED. REMOVED AND REPLACED BOTH FIRE BOTTLES AND SQUIBS IAW MM. REMOVED FROM MEL AND PLACARD. REMOVED AND Mar 8, 2004 · N425AW · Cndair CL6002B19 · Smoke DetectionSDR SIMA200406402Wire · damagedDURING PREFLIGHT THE CREW REPORTED THE EMERGENCY LIGHT OVER THE SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE REPAIRED THE WIRING NEAR THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200404816)Feb 29, 2004 · N507AE · Cndair CL6002C10 · Light System WiringSDR SWIA200412947Switch · dirtyCLIMBING OUT OF SLC, AUTOPILOT WOULD NOT ENGAGE ON EITHER CAPT'S OR F/O'S SIDE. F/O'S WORKED BOTH SIDES. NO WARNING OR CAUTION MESSAGE DISPLAYED. CLEANED AUTOPILOT DISENGAGE SWITCHES. OPS CHECKS GOOD.Feb 27, 2004 · N597SW · Cndair CL6002B19 · Autopilot SystemSDR SWIA200412951Turbine Blades · tornNUMEROUS RIGHT ENGINE 7TH STAGE ROTOR BLADES DAMAGED, TORN. REMOVED AND REPLACED RIGHT ENGINE IAW RII 71-401.Feb 25, 2004 · N907SW · Cndair CL6002B19 · Turbine SectionSDR COMA0460169Door · openFLIGHT 5109 CARGO DOOR WARNING DURING T/O. CLOSED CARGO DOOR PROPERLY. NO DEFECTS NOTED.Feb 23, 2004 · N982CA · Cndair CL6002B19 · Cargo/Baggage DoorsSDR COMA0460170Warning Light · illuminatedFLIGHT 5049 ANTI SKID MESSAGE DURING T/O. DEFERRED MAINTENANCE ON ANTI SKID IAW MEL.Feb 23, 2004 · N781CA · Cndair CL6002B19 · Brake Anti-Skid SectionSDR COMA0470026Door · unsecureFLIGHT 5075 CABIN ALTITUDE CAUTION, AIRCRAFT WOULD NOT PRESSURIZE. FOUND CARGO DOOR NOT CLOSED PROPERLY. INSPECTED DOOR, NO DEFECTS NOTED. SECURED DOOR CLOSED.Feb 23, 2004 · N354CA · Cndair CL6002C10 · Cargo/Baggage DoorsSDR COMA0460166Floor Support · crackedCARGO FLOOR ANGLE AT FS 621 LT SIDE CRACKED. REMOVED DAMAGED AREA OF LT CARGO FLOOR ANGLE. INSTALLED LT REPAIR ANGLE. ALL REPAIR AND FABRICATION WAS IAW REO 601R-53-61-004, CRJ SRM 51-23-00, CRJ SRM 51-25-06 AND CRJ SRM 51-25-16.Feb 22, 2004 · N819CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 04049673Bulb · burned outDURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Feb 18, 2004 · N673BR · Cndair CL6002B19 · Emergency LightingSDR COMA0460168Frame · crackedLT FRAME FLANGE CRACKED BETWEEN STRINGERS 11 AND 12. REPAIRED REO 601R-53-61-193.Feb 16, 2004 · N971CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0460146Wire · chafedFLIGHT 5422, EMERGENCY FLOOR LIGHTS INOPERATIVE ROWS 6,7, AND 8. REPAIRED CHAFED WIRING AT ROW 5.Feb 15, 2004 · N977CA · Cndair CL6002B19 · Light System Wiring
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