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 VNAA0601009Structure · lightning strikeTHE CREW REPORTED A LIGHTNING STRIKE DURING APPROACH INTO CLT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RADOME, LT NLG DOOR, FUSELAGE, RT ELEVATOR, RT HORIZONTAL STJan 11, 2006 · N259PS · Cndair CL6002B19 · Aircraft StructuresSDR VNAA0601007Structure · lightning strikeTHE CREW REPORTED A LIGHTNING STRIKE DURING DESCENT INTO CLT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE LT HORIZONTAL STABILIZER TIP FAIRING AND TWO STATIC WICKS. AJan 11, 2006 · N246PS · Cndair CL6002B19 · Aircraft StructuresSDR VNAA0601008Flap System · malfunctionedDURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 8 DEGREES. THE CREW FOLLOWED THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD.Jan 11, 2006 · N254PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA06088Angle · crackedDURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT ANGLE, ABOVE THE ASSIST PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR AFT ANGLE, ABOVE ASSIST PULLEY, IAW REO 601R-52-11-513. (K)Jan 11, 2006 · N875AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA060112003Insulation · burnedBURNT INSULATION BLANKET FOUND IN CARGO UNDERFLOOR AREA ON RT SIDE OF AIRCRAFT AROUND HEATED LAV WATER SERVICE PORT.Jan 11, 2006 · Cndair CL6002B19 · LavatoriesSDR ASOA06087Door · noneDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND TO BE DIFFICULT TO CLOSE. MAINTENANCE REMOVED DEBRIS AND CYCLED PASSENGER DOOR WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 10, 2006 · N868AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200640004Windshield · failedLT WINDSHIELD CENTER PANE SHATTERED AT FL320 UNDER NORMAL FLIGHT CONDITIONS. REMOVED AND REPLACED LT WINDSHIELD. OPS CHECK GOOD. (K)Jan 9, 2006 · N457AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200640003Handle · out of positionAFTER TAKEOFF, ROTATION GEAR DISAGREE RED WARNING MESSAGE CAME ON, WAITED 20-30 SECONDS, LOOKED AT GEAR HANDLE, IT SEEMED WAS NOT UP ALL THE WAY. RECYCLED LANDING GEAR HANDLE AND GEAR CAME UP. PULLED OUT QRH, C/W ALSO CHECK HYD PRESSURE WAS NORMAL. (K)Jan 9, 2006 · N411ZW · Cndair CL6002B19 · Landing Gear SelectorSDR ASOA06083Light · brokenDURING A GROUND INSPECTION, THE EMERGENCY LIGHT STRIP HOUSING, NEAR THE PASSENGER DOOR ENTRANCE, WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K)Jan 9, 2006 · N909EV · Cndair CL6002B19 · Emergency LightingSDR ASOA06082Power Supply · inoperativeDURING A GROUND INSPECTION, THE CENTER SECTION OF THE EMERGENCY FLOOR STRIP LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR STRIP LIGHTS POWER SUPPLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 9, 2006 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA06075Unknown · unknownDURING C-CHECK, A SUSPECTED CRACK WAS FOUND ON THE LT SIDE OF FS 718. MAINTENANCE REPAIRED THE CRACK ON THE LT SIDE OF FS 718 IAW REO. (K)Jan 8, 2006 · N844AS · Cndair CL6002B19 · Aircraft StructuresSDR ASOA06074Angle · corrodedDURING C-CHECK, CORROSION WAS FOUND ON THE SERVICE DOOR LOWER SILL FORWARD CORNER ANGLE, AT FS 311. MAINTENANCE DETERMINED AFTER FURTHER INSPECTION THAT THE SERVICE DOOR LOWER SILL FORWARD CORNER ANGLE, AT FS311, WAS NOT CORRODED. (K)Jan 8, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06071Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FLOOR BEAM END, AT FS 34B, RBL 44. MAINTENANCE REPAIRED THE TRANSVERSE FLOOR BEAM END, AT FS 346, RBL44, IAW REO. (K)Jan 8, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR CA060112013Windshield · crackedLT WINDSHIELD FOUND CRACKED BEFORE FLIGHT. LT WINDSHIELD REPLACED AND TESTED IAW TO AMM PROCEDURE.Jan 8, 2006 · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA06076Nut Plate · corrodedDURING A C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 536, LBL42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 536, LBL 42, IAW REO. (K)Jan 7, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06040SStructure · corrodedDURING C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 450, RBL 42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 450, RBL 42, IAW REO. (K)Jan 7, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06044Structure · corrodedDURING A C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 550, RBL42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 550, RBL42, IAW REO. (K)Jan 7, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06055Structure · corrodedDURING C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 531, LBL 42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 531, LBL 42, IAW REO. (K)Jan 7, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0601004Flap System · malfunctionedDURING APPROACH WITH FLAPS 20 DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN FLAPS WERE SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FAULT ISOLATION PROCEDURES. NO FAULTS WERE FOUND. THE FLAJan 6, 2006 · N254PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA06023Doubler · corrodedDURING C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 467-473, LBL 43-37. THE MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06022Doubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 460-462, RBL 44-42. THIS WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06021Doubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 427-425, LBL 44-37. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06020Doubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS425, RBL 39. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASOA06019Doubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLERS AT FS 513-517, LBL AND RBL 37-44. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06018Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FLOORBEAM CAP AT FS559.112, RBL27-45. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA06017Frame · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FRAME CAP AT FS559, LBL38-42. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA06016Frame · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FRAME CAP AT FS559, RBL 38-40. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA06015Nut Plate · corrodedDURING A C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 542, RBL 42. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06014Finger Doubler · corrodedDURING A C-CHECK, THE FINGER DOUBLER, AT FS 439, BL 42R, WAS FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA06006Inverter · inoperativeDURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR TRACK LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR4 INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 6, 2006 · N981EV · Cndair CL6002B19 · Emergency LightingSDR ASOA06005Uplock Roller · seizedDURING APPROACH, THE CREW ATTEMPTED TO LOWER THE LANDING GEAR WHEN THEY RECEIVED A GEAR DISAGREE WARNING AND A NOSE GEAR UNSAFE INDICATION. THE CREW TERMINATED THE DESCENT AND ENTERED A TRAFFIC PATTERN. THE CREW COMPLIED WITH THE QRH AND CYCLED THE GEAR WITHJan 6, 2006 · N976EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA06014SFinger Doubler · corrodedDURING A C-CHECK, THE FINGER DOUBLER, AT FS 439, BL 42R, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FINGER DOUBLER, AT FS 439, BL 42R IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06015SNut Plate · corrodedDURING C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 542, RBL 42. MAINTENANCE REPAIRED THE NUT PLATE AT FS 542, RBL 42, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06016SCap · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FRAME CAP AT FS 559, RBL 39-40. MAINTENANCE REPAIRED THE TRANSVERSE FRAME CAP AT FS 559, RBL 38-40, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA06017SCap · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FRAME CAP AT FS 559, LBL 38-42. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA05018SCap · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FLOORBEAM CAP AT FS 559.112, RBL 27-45. AFTER MAINTENANCE ALODINED, PRIMED, AND BLENDED THE TRANSVERSE FLOORBEAM CAP AT FS 559, RBL 27-45, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA06019SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLERS AT FS 513-517, LBL AND RBL 37-44. MAINTENANCE REPAIRED THE DOUBLERS AT FS 513-517, LBL AND RBL 37-44, IAW EO AND REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06020SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 425, RBL39. MAINTENANCE REPAIRED THE DOUBLER AT FS 425, RBL 39, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06021SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 427-425, LBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 427-425, LBL 44-37, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06022SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 460-462, RBL 44-42. MAINTENANCE REPAIRED THE DOUBLER AT FS 460-462, RBL 44-42, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06023SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 467-473, LBL 43-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 467-473, LBL 43-37, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06024SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 470-477, RBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 470-477, RBL 44-37, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06025SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 473-477, LBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 473-477, LBL 44-37, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06026SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS498-513, RBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 498-513, RBL 44-37, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06027SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 513-517, LBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 513-517, LBL 44-37, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06036SFinger Doubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ONTHE FINGER DOUBLERS AT FS 538-540, LBL 44-42. MAINTENANCE REPAIRED THE FINGER DOUBLERS AT FS 538-540, LBL 44-42, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06037SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE ON THE DOUBLER AT FS 543-545, LBL 44-42. MAINTENANCE REPAIRED THE DOUBLER AT FS 543-545, LBL 44-42, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06038SFinger Doubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ONTHE FINGER DOUBLER AT FS 544, RBL 44-41. MAINTENANCE REPAIRED THE FINGER DOUBLER AT FS 544, RBL 44-41, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 06FDEA00035Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR ASOA06013Floorbeam · crackedDURING A C-CHECK, THE FS280 FLOOR SUPPORT ANGLE, OB OF LBL9, AT ALTERNATE GEAR EXTENSION PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENEANCE REMOVED AND REPLACED THE FS280 FLOOR SUPPORT ANGLE, OB OF LBL9, AT ALTERNATE GEAR EXTENSION PULLEY, IAW REO 60Jan 5, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
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