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 ASOA2012080102018Seat Track · corrodedIN PASSENGER COMPARTMENT, LBL 9.00 FS 396 TO 409+120, SEAT TRACK IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED IAJul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102019Seat Track · corrodedIN PASSENGER COMPARTMENT, RBL 9 BETWEEN FS 396 TO 409+120, SEAT TRACK IS CORRODED AT BS 409. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802 & LOCATED & DRILLED NEW SERVICEABLE TRACK IAW SRM 51Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102020Seat Track · corrodedIN PASSENGER COMPARTMENT SEAT TRACK, FS 409+112 TO 559, LBL 9.00 IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. DRILLED AND COUNTERSUNK NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102021Seat Track · corrodedPASSENGER COMPARTMENT SEAT TRACK AT FS 409+112 TO 559, RBL 9.00 IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. DRILLED AND COUNTERSUNK NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240730Door · lack of lubeMAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. INSPECTED AND FOUND LOCKING PINS TO BE DRY. LUBED, ROLLERS AND LOCKING PINS IAW REF AMM 52-11-00. OPS CHECKS WITH CREW 5 TIMES. OPS CHECK GOOD.Jul 26, 2012 · N407AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012081602067Floor Support · crackedIN PASSENGER COMPARTMENT, FLOOR STRUCTURE AT FS 280.00 RBL 9.00 OTBD ATTACHMENT ANGLE IS CRACKED. REPAIRED IAW REO 601R-53-11-926, REV B.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012081602068Seat Track · corrodedPASSENGER COMPARTMENT LT SIDE WALL SEAT TRACK AT FS 399.00 IS CORRODED. REPAIRED LT SIDEWALL SEAT TRACK IAW REO 601R-53-00-55. ECTC REQUIRED.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012081602069Floor Support · corrodedPASSENGER COMPARTMENT AT FS 559.00, LBL 36.00 FLOOR SUPPORT FINGER WEB IS CORRODED.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012081602070Floor Support · corrodedIN PASSENGER COMPARTMENT FLOOR SUPPORT BETWEEN FS 424.00 TO FS 559.00 RBL 42.00, AROUND FLOORBOARD ATTACHMENT HOLES, FLOOR SUPPORT CORRODED. COMPLIED WITH ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012081602071Web · corrodedIN PASSENGER COMPARTMENT AT FS 559.00, RBL 42.900 FLOOR SUPPORT FINGER WEB IS CORRODED.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240739Angle · crackedANGLE CRACKED AT APPROX FS 484, RBL 27. REMOVED CRACKED ANGLE AT FS 484, RBL 27, DUPLICATED ANGLE AND INSTALLED ANGLE IAW REO 601R-53-41-059, REV B.Jul 26, 2012 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012082002080Angle · corrodedFS 280.00 BETWEEN LBL 9.00 TO RBL 9.00, FWD AND AFT J ANGLES ARE CORRODED. REMOVED ANGLE IAW SRM 51-42-06, 51-42-21. LOCATED NEW ANGLE IAW SRM 51-40-11. INSTALLED NEW ANGLE IAW SRM 51-42-06 AND 51-42-21.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012080102014Seat Track · corrodedIN PASSENGER COMPARTMENT, RT SIDE SEAT TRACK AFT OF FS 409+128 IS CORRODED SEVERAL LOCATIONS. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV A.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012072701988Lamp · burned outNR 1 CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. RELAMPED NR 1 CABIN CEILING EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD IAW AMM 33-51-00.Jul 25, 2012 · N903EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012080102024Structure · corrodedPAX DOOR LOWER AFT CORNER CORRODED BEYOND LIMITS. INSTALLED NEW AFT CORNER IAW SRM 51-42-06, 51-42-21.Jul 25, 2012 · N904EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240738Skin · chafedINNER SKIN CHAFED ON BUTTE DOOR 694PB. R & R SKIN IAW SRM 51-42-06, 51-40-11, 51-25-16.Jul 25, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201240743Floor Support · corrodedCARGO FLOOR SUPPORT LBL 27 HAS CORRODED NUTPLATE HOLES BETWEEN FS 574 AND FS 605. REMOVED UNSERVICEABLE, LBL 27 FLOOR SUPPORT AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW 51-40-11, 51-42-06, 51-24-36. REMOVED UNSERVICEABLE WEB AND INSTALLED SERVICEABLE WEB IAJul 25, 2012 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240803Door · chafedLT MLG DOOR L/E CHAFED. LT MLG DOOR L/E PREVIOUS. R & R IAW REO 601R-52-82-016.Jul 25, 2012 · N447AW · Cndair CL6002B19 · Landing Gear DoorsSDR ASOA2012072701996Handle · obstructedMAIN PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. FOUND EXCESSIVE DEBRIS AND GREASE ON DOOR LOCKING HANDLE MECHANISM, CLEANED AND PERFORMED OPS TEST IAW AMM 52-11-00. OPS TESTED GOOD ACFT OK FOR SERVICE.Jul 24, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012072701997Lamp · burned outNR 6 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21, OPS CHECKED GOOD.Jul 24, 2012 · N932EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201240690Warning Message · illuminatedRIGHT WINDSHIELD HEAT CAUTION MESSAGE ON TAXI OUT. INSPECTED AND CLEANED RT WINDSHIELD, PERFORMED OPS CHECK IAW AMM 30-41-00, OPS CHECKED GOOD, ACFT OK FOR SERVICE.Jul 24, 2012 · N463AW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR A6WA201240729Warning Message · false activationRT WINDSHIELD HEAT CAUTION MESSAGE ON TAXI OUT. INSPECTED AND CLEANED RT WINDSHIELD. PERFORMED OPS CHECK IAW AMM 30-41-00. OPS CHECKS GOOD. ACFT OK FOR SERVICE.Jul 24, 2012 · N436AW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR ASOA2012081602066Angle · crackedFS 625 OBLIQUE LT CRACKED. REMOVED CRACKED OBLIQUE ANGLE COMMON TO LT SIDE FS 625 AND REPLACED IT WITH NEW PART IAW SRM 51-42-21.Jul 24, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240741Mount Bracket · crackedPAX DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED. R & R PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET IAW SRM 51-42-06 & 51-42-13.Jul 24, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012072701986Control Unit · failedFLAPS FAILED AT ZERO DEGREES, PRECEDED BY FLAPS HALF SPEED IN ROUTE. EMERGENCY DECLARED. R & R FECU IAW AMM 27-51-05. FLAPS OPS TESTED GOOD IAW AMM 27-54-00. NO FURTHER DEFECTS NOTED.Jul 23, 2012 · N972EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA2012073002008Angle · corrodedFOUR L ANGLES CORRODED AT PAX DOOR HINGE LOWER CAVITY. INSTALLED NEW L ANGLES ON ASD IAW SRM 51-42-06.Jul 23, 2012 · N904EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012080102023Bracket · crackedAFT EQUIPMENT BAY AFT PRESSURE BULKHEAD HAS ONE CRACKED BRACKET AT 625.00 RT SIDE. REMOVED AND REPLACED WITH SERVICABLE BRACKET IAW SRM 51-42-21.Jul 23, 2012 · N904EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240689Landing Gear · malfunctionedAFTER TAKEOFF, RECEIVED GEAR DISAGREE MESSAGE APPROX 6 SECONDS AFTER HANDLE SELECTION. IN TRANSIT MESSAGE CONFIRMED FOR ABOUT 20 MINUTES. MAINS SHOWED YELLOW DURING THE 20 MINUTES.Jul 23, 2012 · N458AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2012080902040Angle · corrodedFOUR ANGLES CORRODED AT PAX DOOR HINGE LOWER CAVITY. INSTALLED 4 EA NEW 'L' ANGLES ON ASD IAW SRM 51-42-06. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. SDR CLOSED.Jul 23, 2012 · N904EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240727Selector Valve · inoperativeAFTER TAKEOFF, RECEIVED GEAR DISAGREE MESSAGE APPROXIMATELY 6 SECONDS AFTER HANDLE SELECTION. IN TRANSIT MESSAGE CONFIRMED FOR ABOUT 20 MINUTES. MAINS SHOWED YELLOW DURING THE 20 MINUTES. R & R MLG SELECTOR VALVE IAW 32-32-10. OPS CHECK/LEAK CHECK GOOD. GJul 23, 2012 · N458AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2012072601971Bracket · damagedNOSE GEAR FAILED TO RETRACT ON CLIMB OUT. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. R & R NOSE GEAR CENTERED PROXIMITY SENSOR BRACKET IAW CMM 32-20-04 PERFORMED OPS CHECK IAW AMM 32-30-00. NO DEFECTS NOTED.Jul 22, 2012 · N859AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012072601972Sign · inoperativeLEFT INTERIOR OVERWING EMERGENCY EXIT FLOOR LEVEL SIGN IS INOPERATIVE. REMOVED AND INSTALLED A NEW SIGN IAW AMM 33-51-10, OPS CHECKED GOOD.Jul 22, 2012 · N906EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201240717Hinge Fitting · gougedLT OTBD FLAP, OTBD HINGE BOX IS GOUGED BY FAIRING ATTACHMENT FASTENER INBD FWD LT OTBD FLAP OTBD HINGE BOX BLENDED AND SHOT PEENED IAW REO 601R-57-21-1715, SRM 51-25-16, 51-12-00, 51-40-11, 51-24-11, 51-21-11, 51-25-06.Jul 21, 2012 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240718Hinge Fitting · gougedRIGHT OTBD FLAP, OTBD FORWARD HINGE BOX HAS A GOUGE BEHIND THE FORWARD INBD FLAP HINGE BOX FAIRING ATTACH POINT. BLENDED AND ROTO PEENED RT OTBD FLAP, OTBD FWD HINGE BOX IAW REO 601R-57-21-1715 SRM 51-40-11, 51-12-00, 51-28-11, 51-25-06, 51-25-16, 51-24-11.Jul 21, 2012 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240723Angle · corrodedPAX DOOR LOWER SURROUND STRUCTURE ANGLE BETWEEN FS 310.00 & FS 349.00 AT WL 73 CORRODED. R & R PAX DOOR LOWER SURROUND STRUCTURE ANGLE BETWEEN FS 310.00 AND FS 349.00 AT WL 73 IAW SRM 51-42-06 & 51-42-21.Jul 21, 2012 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA120727001Control Cable · damaged(CAN) THE ACFT WAS BEGINNING A DESCENT. THE PILOT HAS REDUCED THE THRUST LEVERS OF BOTH ENGINES. THE RT ENGINE HAS PRODUCED REDUCTION N1 AND N2 RPM NORMALLY. BUT THE LEFT ENGINE HAS CHANGED THE N1 AND N2 RPM ONLY A LITTLE AND COULD NOT BE REDUCED MORE WITH THEJul 21, 2012 · Cndair CL6002B19 · Power LeverSDR ASOA2012072601981Bracket · crackedAFT EQUIPMENT BAY, AFT PRESSURE BULKHEAD HAS CRACKED BRACKET AT BS 625. R & R BRACKET IAW SRM 51-42-21.Jul 20, 2012 · N904EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240716Support Bracket · crackedRT JETPIPE UPPER CORE COWL STANG ROD SUPPORT BRACKET ASSY MISSING RIVET AND STIFFENER AT XN214 CRACKED. R & R STIFFENER IAW CMM 78-11-00, SRS 042.Jul 20, 2012 · N448AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201240721Mount Bracket · crackedPAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET IS CRACKED. REMOVED CRACKED MOUNTING BRACKET THEN INSTALLED NEW SERVICEABLE BRACKET PN 601R317745-7 IAW SRM 51-42-06.Jul 20, 2012 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240715Support Bracket · crackedCARGO DOOR LOWER FWD SUPPORT BRACKET IS CRACKED. REMOVED CRACKED CARGO DOOR LOWER FWD SUPPORT BRACKET INSTALLED NEW SERVICEABLE CARGO DOOR LOWER FORWARD BRACKET IAW SRM 51-42-06.Jul 20, 2012 · N448AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240719Retainer · damagedCARGO DOOR SEAL RETAINER DAMAGED. REMOVED DAMAGED CARGO DOOR SEAL RETAINER AND REPLACED WITH NEW SERVICEABLE IAW SRM 51-42-06.Jul 20, 2012 · N448AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240726Flap System · malfunctionedFLAPS DEGRADED - WHILE DESCENDING THRU 17,000 FT A/P ENGAGED. VERT SPEED SET AT 1500 FPM & SPEED AT 280 KIAS, AIRPLANE PITCHED NOSE-DOWN MOMENTARILY. OVERSPEED TAPE APPEARED ON SPEED TAPE. RECEIVED FLAPS DEGRADED STATUS MESSAGE. RECEIVED HYD PUMP 2B & 3B CJul 20, 2012 · N429AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201240728Pump · malfunctionedDISAGREE WARNING MESSAGE AFTER TAKEOFF UPON RETRACTING GEAR. C/W QRH. R & R 3B HYD PUMP IAW 29-12-03. OPS CHECK AND LEAK CHECK GOOD. GEAR RETRACTION/EXTENSION GOOD.Jul 20, 2012 · N459AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR ASOA2012072001952Lamp · burned outNR 6 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21. OPS CHECKED GOOD.Jul 19, 2012 · N683BR · Cndair CL6002B19 · Emergency LightingSDR A6WA201240704Handle · crackedCARGO DOOR HANDLE CRACKED ON FLANGE. REMOVED DAMAGED HANDLE ASSY AND REPLACED WITH NEW SERVICEABLE HANDLE ASSY, PN H3415-31 IAW SRM 51-42-01, 51-42-21 AND AMM 52-31-03.Jul 19, 2012 · N448AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240722Handle · crackedPAX DOOR EXTERIOR OPEN HANDLE IS CRACKED. REMOVED CRACKED OUTER HANDLE FROM PAX DOOR AND INSTALLED NEW SERVICEABLE OUTER HANDLE IAW AMM 52-11-03.Jul 19, 2012 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240688Flap System · failedAFTER DEPARTURE, SELECTING FLAPS FROM 8 TO 0 DEG. RECEIVED FLAP FAIL CAUTION MESSAGE. FLAP FAILED AT 0 DEG. CIRCUIT BREAKER RESET FAILED.Jul 19, 2012 · N434AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA2012072001950Door · lack of lubeSERVICE DOOR CANNOT BE OPENED FROM THE OUTSIDE. LUBED SERVICE DOOR, OPS CHECKED GOOD, REF MM 52-41-00.Jul 18, 2012 · N823AS · Cndair CL6002B19 · Service DoorsSDR A6WA201240713Hinge · chafedPAX DOOR HINGE HAS CHAFED LUGS. COMPLIED WITH REO 601R-52-11-1347.Jul 18, 2012 · N448AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201240712Attach Angle · crackedPAX DOOR LATCH CAM COVER PLATE AFT ATTACH ANGLE IS CRACKED. R & R PAX DOOR LATCH CAM COVER PLATE AFT ATTACH ANGLE IAW SRM 51-41-02.Jul 18, 2012 · N448AW · Cndair CL6002B19 · Passenger/Crew Doors
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