GE CF34 series

Service difficulty reports · 1,368

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 = '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 A6WA201040939Bulkhead · crackedFS 202 BULKHEAD CRACKED AROUND BRAKE PUSH-PULL ROD. REPAIRED BULKHEAD AT FS 202.00 BY FULLY INCORPORATING REO 601R-53-11-2009.Nov 1, 2010 · N448AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001693Light · inoperativeRT EXTERIOR THIRD FROM FRONT EMERGENCY LIGHT INOP. R & R RT EXTERIOR EMERGENCY LIGHT 3RD FROM FRONT IAW AMM 33-51-21. OPS CK GOOD. R & R RT EXTERIOR EMERGENCY LIGHT 3RD FROM FRONT IAW AMM 33-51-21. OPS CK GOOD. (CLOSED)Oct 30, 2010 · N844AS · Cndair CL6002B19 · Emergency LightingSDR A6WA201040801Bulkhead · damagedFOUND MISLOCATED FUEL QTY CONNECTOR PLUG HOLE ON RT 559 REPAIR. REPAIRED MISLOCATED FUEL QTY CONNECTOR PLUG HOLE ON RT 559 IAW DEVIATION REO 601R-53-41-1303.Oct 30, 2010 · N448AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR N6WA20101006Warning Light · false activationLEFT EMERGENCY DOOR CAUTION FLASHED ON/OFF ABOUT 10 TIMES AFTER LANDING TO PARK AT GATE. PERFORMED GROUND OPS CHECK ON LT EMERGENCY DOOR CAUTION INDICATION. OPS CHECK GOOD NO FUTHER DISCREPANCY NOTED AT THIS TIME IAW AMM 52-21-00.Oct 29, 2010 · N151GJ · Cndair CL6002C10 · Door Warning SystemSDR ASOA201001688Pdu · unserviceableFLAPS FAIL CAUTION MSG ON APPROACH AT 22 DEG (EMERGENCY DECLARED -- EMERGENCY VEHICLES WERE STANDING BY AS A PRECAUTION) COMPLIED WITH AD 2009-06-12. ACFT RETURNED TO SERVICE. CLEARED, PLACARD REMOVED. R & R FLAP PDU IAW AMM 27-52-01,OPS CK GOOD. (CLOSED)Oct 29, 2010 · N839AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR 2010F00216Receiver · defectiveRNA-34BF "LOCKS UP" WHEN IN VICINITY OF FM RADIO STATIONS BROADCASTING ON 107.9 MHZ. INDICATIONS TO THE USER ARE THAT THE RADIO CANNOT BE TUNED TO ANOTHER FREQUENCY AND ALL OUTPUTS BECOME FROZEN OR ABSENT. MFG HAS BEEN MADE AWARE OF THE PROBLEM BY CANADA, SWOct 28, 2010 · N85 · Cndair CL6002B16 · Localizer/VOR SystemSDR ASOA201001681Door · bindingARRIVING AT GATE, F/A COULD NOT OPEN PASSENGER DOOR. RAMP ALSO COULD NOT OPEN PASSENGER DOOR. OPENED DOOR AND OPS CHECKED GOOD IAW AMM 52-11-01, MX READY. (CLOSED)Oct 28, 2010 · N447CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001683Seat Track · corrodedRT CTR FLOOR SEAT TRACK CORRODED AT SEAT LOCATIONS 3,4, AND 5. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. EVALUATED DAMAGE AND FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REPLACED SEAT TRACK IAW AMM 53-0049-400-801.Oct 28, 2010 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001684Seat Track · corrodedRT CTR FLOOR SEAT TRACK CORRODED BETWEEN SEAT LOCATIONS 6 THRU 9 RT. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. SEAT TRACK IS OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Oct 28, 2010 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001685Seat Track · corrodedLEFT CENTER SEAT TRACK CORRODED BETWEEN SEAT LOCATIONS 6 THRU 9 RT. REMOVED SEAT TRACK IAW AMM 3-00-49-000-801. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM-53-31-49-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Oct 28, 2010 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001686Floorbeam · crackedSUPPORT ANGLE FOR RT WEB AT FS 280, RBL26 FOUND CRACKED. R & R SUPPORT ANGLE FOR RT WEB AT FS280, RBL 26 IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. (CLOSED)Oct 28, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR A6WA201040800Panel · corrodedFUEL C/O FOR PNL 550CB REQUIRE AWAC E06/021/457 CURRENT REV TO BE C/W INDICATION FOUND ON AFT OTBD SIDE. REPAIRED FUEL PANEL C/O PNL 550CB IAW REO 601R-57-21-030 REV H, AT APT OTBD SIDE DETAIL III.Oct 28, 2010 · N448AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201040809Skin · chafedRT INBD FLAP, FLAP VANE SKIN L/E CHAFED AT INBD CTR OTBD ENDS BLENDED CTR AND OTBD LOCATIONS ARE WITHIN LIMITS, INBD VANE L/E LOCATION REPLACED L/E SKIN COMPLETING WORK IAW REO 601R-57-52-004, REV C, SRM 51-42-13.Oct 28, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR V0XR413Y102710002Angle · corrodedSERVICE DOOR ANGLE PN SM670-31996-3 UNDER SILL PLATE HAD SURFACE CORROSION OUT OF LIMITS. R & R SERVICE DOOR ANGLE. IAW SRM 51-10-06 & SRM 51-21-23.Oct 27, 2010 · N151GJ · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XR413Y102710003Bulkhead · corrodedBULKHEAD LOWER WEB PN 670-53-11-052-1 AND -2 CORRODED, SURFACE, BEYOND LIMITS ABOVE 280 BEAM. REMOVED AND REPLACED LT AND RT SIDE OF LOWER FWD BULKHEAD AT FS 280 IAW REO NR 670-53-11-052. W/C 2113.Oct 27, 2010 · N151GJ · Cndair CL6002C10 · Fuselage Main, BulkheadSDR V0XR413Y102710004Sill · corrodedRT SILL HAD CORROSION, SURFACE AND PITTING OUT OF LIMITS. R & R RT SILL AT FS 280 IAW SRM 51-42-06 W/C 2114.Oct 27, 2010 · N151GJ · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XR413Y102710005Seat Track · corrodedSEAT RAIL LT AND RT HAD CORROSION, SURFACE AND PITTING AT SEAT 12A FWD AND 12D FWD ATTACHMENT POINTS. R & R SEAT RAILS IAW SRM 51-42-01 AND 53-00-49 W/C 2119.Oct 27, 2010 · N151GJ · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XR413Y102710006Floorbeam · corroded280 BEAM HAD EXFOLIATION CORROSION ACROSS TOP. R & R 280 BEAM IAW REO 670-53-11-047.Oct 27, 2010 · N151GJ · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR V0XR413Y102710007Angle · corrodedPASSENGER DOOR MID CAP ANGLE AND FWD ANGLE AT STR 18 BOTH CORRODED OUT OF LIMITS. R & R PASSENGER DOOR MID CAP ANGLE AND FWD IAW SRM 51-41-02.Oct 27, 2010 · N151GJ · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201001679Stringer · cracked3L STRINGER CRACKED AT FS 280 AFT OF BULKHEAD. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSPECTION PROCEDURE ET-2. CRACK EXTENDING TO BUT NOT PAST THIRD FASTENER. REMOVED DAMAGED SECTION AND CLEANED EDGES IAW STEPS 1 & 2 OF REO 670-53-21-493. COMPLIEOct 27, 2010 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201001680Hydraulic System · lowHYD 3 LOW PRESS CAUTION MESSAGE IN FLIGHT. RAN CHECKLIST AND HAD TO MANUALLY EXTEND GEAR. DECLARED EMERGENCY. (EMERGENCY DECLARED -- EMERGENCY EQUIPMENT REQUESTED TO BE STANDING BY) (CLOSED)Oct 27, 2010 · N850AS · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA201040804Seat Track · corrodedNR1 FLOOR SEAT TRACK ON RBL9 IS CORRODED. REMOVED UNSERVICEABLE NR1 FLOOR SEAT TRACK AT RBL9 DUPLICATED SEAT TRACK FROM BULK PN N126-2075, INSTALLED SEAT TRACK IAW SRM 51-41-02 & AMM 53-01-11.Oct 27, 2010 · N453AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001739Stringer · corrodedLOOKING FWD FROM AVIONICS BAY STR 26, RT HAS CORROSION IN SEVERAL PLACES GOING FWD (MARKED) AVIONICS BAY . REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. FABRICATED NEW STRINGER IAW REO 670-53-21-262. REPLACED STRINGER IAW REO 670-53-21Oct 27, 2010 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR A6WA201040808Angle · crackedRT OBLIQUE ANGLE AT FS 625.00 IS CRACKED. R & R RT OBLIQUE ANGLE IAW REO 601R-53-61-100.Oct 27, 2010 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040861Bulkhead · chafedAFT PRESSURE BULKHEAD FWD SKIN HAS CHAFE AT FS 621.00 BETWEEN LBL 36.20 AND LBL 27.50. REPAIRED FWD FACE OF FS 621.00 BULKHEAD IAW REO 601R-53-61-3865.Oct 27, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040856Housing · chafedCARGO DOOR HANDLE CUT OUT IS CHAFED IN 3 PLACES. REPAIRED CHAFED DAMAGE ON CARGO DOOR HANDLE 3 PLACES CUT OUT IAW REO 601R-52-31-141.Oct 27, 2010 · N453AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201040857Vane · chafedLT INBD FLAP VANE HAS CHAFING DAMAGE ON L/E IN 3 PLACES. REPAIRED CHAFE DAMAGE ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-004.Oct 27, 2010 · N453AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040940Fitting · crackedLBL9 INBD CLIP FS 280 CRACKED. R & R CLIP AT FS 280, INBD SIDE OF LBL 9.0 IAW SRM 51-42-21.Oct 27, 2010 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040941Bulkhead · chafedFS 280, RBL 9 APPROX 18" FROM FLOOR ON BACKSIDE OF BULKHEAD HAS 2 AREAS OF CHAFING. REPAIRED FS 280 BULKHEAD AT RBL 11.0 BETWEEN STR 13A & 14A REO 601R-53-11-1727, REV D.Oct 27, 2010 · N448AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001647Bulb · burned outCEILING EMERGENCY LIGHT OUT BETWEEN ROWS 4 AND 5. R & R CTR EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD. R & R CTR EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OPS CHECKED, GOOD. (CLOSED)Oct 26, 2010 · N667BR · Cndair CL6002B19 · Emergency LightingSDR ASOA201001669Bulb · burned outRT AFT OVERWING EMERGENCY LIGHT OUT. R & R RT AFT EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD. R & R RT AFT EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD. (CLOSED)Oct 26, 2010 · N667BR · Cndair CL6002B19 · Emergency LightingSDR ASOA201001670Crossbeam · corrodedFS 280.00 CROSSBEAM CORRODED FWD OF LT AND RT DRIP TRAYS. REMOVED CROSSBEAM IAW SRM 51-42-06-001-001-A01. DRILLED & DEBURRED NEW CROSSBEAM IAW SRM 51-42-06-001-001-A01.Oct 26, 2010 · N712EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201001671Placard · damagedCREW ESCAPE HATCH EXTERNAL PLACARD "EMERGENCY EXIT HANDLE INSTRUCTIONS" AND OPEN TO CLOSE ARROW MISSING PIECES, AND UNREADABLE. APPLIED "EMERGENCY EXIT HANDLE INSTRUCTIONS" SILKSCREEN PRINT IAW AMM 20-60-11-000-801.Oct 26, 2010 · N712EV · Cndair CL6002C10 · Placards and MarkingsSDR ASOA201001672Placard · damagedCREW ESCAPE HATCH EXTER PLACARDS (OPEN, CLOSED, EMER EXIT, AND ARROW) REQUIRE REPLACEMENT. APPLIED "EMERGENCY EXIT HANDLE INSTRUCTIONS" SILKSCREEN PRINT IAW AMM 20-60-11-000-801 ALSO RE-APPLIED "ARROW" FOR OPEN TO CLOSE".Oct 26, 2010 · N744EV · Cndair CL6002C10 · Placards and MarkingsSDR ASOA201001673Channel · corrodedFWD J-CHANNEL AT FS 280 IS CORRODED BEYOND LIMITS. REMOVED FWD "J" CHANNEL IAW SRM 51-42-06. INSTALLED FWD "J" ANGLE IAW SRM 51-42-06.Oct 26, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001674Web · corrodedFS 280 WEB HAS SEVERAL AREAS OF CORROSION. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926 REV B.Oct 26, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001675Post · failedFS 409+128, LBL 18, VERT POST FAILS NDT WITH AN INDICATION ON OTBD POST AFT RADIUS (UPPER) GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .3" LONG. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926 REV B.Oct 26, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001676Post · crackedFS 409+128 RBL 18 VERT POST FAILS NDT WITH AN INDICATION ON BOTH INBD AND OTBD POST IN AFT RADIUS (UPPER) BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .3 LONG. REMOVED POST IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED POST IAW REO 601R-53-41-889, 5Oct 26, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001677Lamp · burned outEMERGENCY LIGHT ON RT SIDE (1) FWD OF DOOR INOP. RELAMPED EMERGENCY LIGHT AS REQUIRED IAW AMM 32-42-01, OPS CHECK GOOD.Oct 26, 2010 · N902EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001678Light · damagedWARDROBE CLOSET FLOOR LEVEL EMERGENCY FLOOD LIGHT BASE DAMAGED. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD. (CLOSED)Oct 26, 2010 · N975EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040806Rib · crackedRT BATT RIB CRACKED. REPAIRED BATT RIB ASSY, AT WS 53.60 IAW REO 601R-57-51-046, REV B, REPAIR NR 3.Oct 26, 2010 · N453AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201001648Crossbeam · corrodedFS 280, CROSSBEAM CORRODED IN SEVERAL PLACES. REMOVED DAMAGED CROSSBEAM IAW SRM 51-42-06 AND 51-42-21. CUT NEW CROSSBEAM IAW SRM 51-40-11-001-001-A01. COMPLIED WITH STEP 2 OF REO 670-53-11-047. NO INDICATIONS NOTED. COMPLIED WITH STEPS 3-7 OR REO 670-53-Oct 25, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201001649Web · corrodedLT FS 280 WEB CORRODED AT LBL 12. REMOVED DAMAGED WEB IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED NEW WEB IAW SRM 51-40-11-001-001-A01. WEB. INSTALL LT FS280, AT INSTALLED WEB IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. Oct 25, 2010 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001650Web · corrodedRT FS 280 WEB CORRODED AT RBL 12. REMOVED WEB DAMAGED FROM CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED NEW WEB IAW SRM 51-40-11-001-001-A01. INSTALLED WEB IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. RESTORED FINIOct 25, 2010 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001651Floor Support · corrodedCOCKPIT FLOOR SUPPORT CORRODED BEYOND LIMITS. REMOVED COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Oct 25, 2010 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001652Structure · corrodedPLATE ASSY, PN 601R38957-119, SHOWS HEAVY CORROSION. AFTER PAINT REMOVAL FOUND TO BE LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-21-06. ALODINED, PRIMED, AND TREATED AREA IAW SRM 51-32-00 AND 51-25-00. REMOVED OLD CORROSION NUTPLATE AND INSTALLED NEW ONOct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001653Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AND INSTALLED A NEW DRAG ANGLE 601R31772-5S IAW SRM 51-42-06.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001654Rib · crackedLT INBD L/E HAS A CRACKED RIB UNDER PANEL 520CZ. REMOVED DAMAGED RIB IAW SRM 51-42-06 AND 51-42-13. LOCATED HOLES IN NEW RIB IAW SRM 51-40-11. INSTALLED NEW RIB IAW SRM 51-42-06 AND 51-42-13.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201001655Angle · corrodedSERVICE DOOR SILL ANGLE CORRODED IN SEVERAL AREAS. FOUND CORROSION TO BE APPROX .002" DEEP AND WITHIN ALLOWABLE LIMITS IAW SRM 51-21-23 AND 53-00-00. REMOVED THE LIGHT CORROSION IAW SRM 51-21-06.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001656Fitting · crackedRBL 9, FS 460 OTBD FITTING CRACKED. REMOVED CRACKED FITTING AND ALL THE RIVETS AND LOCK FASTENERS AT RBL 9, FS 460 OTBD AND LOCATED, DRILLED AND FITTED THE NEW PART IAW SRM 51-42-06. REMOVED LOCK FASTERNERS IAW SRM 51-42-23 AND SRM 51-40-11. INSTALLED FITTIOct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
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