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 ASOA2012071201888Isolator · crackedBULKHEAD WEB FWD FACE HAS FIVE CRACKED ISOLATORS. REMOVED DAMAGED ISOLATORS AND INSTALLED NEW ISOLATORS IAW SRM 51-42-13.Jul 9, 2012 · N861AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2012071301896Cargo Track · corrodedCARGO TRACK AT RBL 9 FS 559+12 IS CORRODED. REMOVED CORRODED CARGO TRACK. LOCATED & DRILLED NEW CARGO TRACK IAW SRM 51-40-11. INSTALLED NEW CARGO TRACK IAW SRM 51-41-04.Jul 9, 2012 · N861AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012071301898Seat Track · corrodedSEAT TRACK CORRODED AT BS 559+96, LBL 9, . REMOVED SEAT TRACK IAW SRM 51-41-02. REPLACED CORRODED SEAT TRACK IAW SRM 51-41-02.Jul 9, 2012 · N861AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012071301899Lamp · burned outFWD WARDROBE FLOOR FLOOD EMERGENCY LIGHT HAS SEVERAL BULBS INOPERATIVE. RELAMPED FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE. OPS CHECKED GOOD.Jul 9, 2012 · N841AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012071301900Unknown · odorON DESCENT F/A SMELLED AN ELECTRICAL ODOR IN GALLEY AREA, NO VISABLE SMOKE, ODOR WENT AWAY ONCE THE ACFT IS ON THE GROUND. PERFORMED OP'S CK OF LT AND RT PACK IAW AMM 21-51-00. OP'S CK GOOD. NO FURTHER DEFECT NOTED AT THIS TIME.Jul 9, 2012 · N871AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA2012071801922Structure · corrodedANGLE HAS MULTIPLE AREAS OF CORROSION FROM FS 409.00+128 THRU 559.00 AT LBL 36-45 IN PASSENGER COMPARTMENT UNDER FLOORBOARDS. REMOVED SURFACE FINISH FROM AREAS OF CORROSION IAW SRM 51-20-00. PREPPED AND PAINTED REPAIR AREA IAW CORROSION AT FS 449.85 FLOOR SIJul 9, 2012 · N861AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012072301961Bulkhead · crackedFS 621 BULKHEAD FAILS NDT WITH AN INDICATION AT TOP OF CARGO TRACK LBL 27.50. FULL SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-1541 AND SRM 51-42-06.Jul 9, 2012 · N861AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2012072301962Floorbeam · corrodedFLOORBEAM STRAP FS 559.00, RBL 27 - 43 IS CORRODED. REMOVED CORRODED STRAP IAW SRM 51-42-06. LOCATED AND DRILLED NEW SERVICEABLE FLOORBEAM STRAP IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FLOORBEAM STRAP IAW SRM 51-42-06.Jul 9, 2012 · N861AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201240788Panel · chafedPYLON PANEL 422DB HAS 2EA CHAFED SEPARATION. R & R IAW SRM 51-42-06 & 51-40-11.Jul 9, 2012 · N450AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR ASOA2012071101887Charger · unserviceableALL EMERGENCY LIGHTS ON NR 2 BATTERY INOPERATIVE. R & R NR 2 BATTERY AND BATTERY CHARGER IAW AMM 33-51-04 AND AMM 33-51-05, OPS CHECKED GOOD.Jul 7, 2012 · N880AS · Cndair CL6002B19 · Emergency LightingSDR A6WA201240695Skin · dentedRIGHT CENTER WING LOWER SKIN HAS A DENT AFT OF REFUEL RECEPTACLE DOOR. FOUND TO BE WITHIN LIMITS IAW REO 601R-57-11-060.Jul 6, 2012 · N445AW · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2012071101885Bracket · unserviceableGEAR DISAGREE WARNING MESSAGE CLIMBING THROUGH 14,000 FT. COMPLETED QRH PROCEDURE. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE, LANDED NORMALLY. R & R NLG WOW AND CENTERING SENSOR HARNESS BRACKET IAW AMM 32-61-25. ADJUSTED IAW AMM 32-61-05. PERFORMED GJul 5, 2012 · N832AS · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR A6WA201240691Threshold · corrodedSERVICE DOOR THRESHOLD CORRODED. REMOVED UNSERVICEABLE SERVICE DOOR THRESHOLD AND REPLACED WITH SERVICEABLE DOOR THRESHOLD IAW SRM 51-41-02.Jul 5, 2012 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012070601867Uplock · unserviceableCOMPLETED LANDING CHECKLIST, NOTICED THE NOSE GEAR INDICATOR SHOWED YELLOW DASHED BOX FOLLOWED BY RED DASHED BOX FOLLOWED BY ASSOCITATED MESSAGES. FOLLOWED QRH PROCEDURES. AFTER THIRD ATTEMPT TO LOWER GEAR, HAD 3 GREEN INDICATIONS. LANDED WITHOUT INCIDENT. Jul 3, 2012 · N929EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2012070601864Bulb · burned outRT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R EXTERNAL EMERGENCY LIGHT BULB. OP'S CHECKED GOOD.Jul 2, 2012 · N860AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012070601866Light · unserviceableELECTRICAL BURNING ODOR IN COCKPIT. DIVERTED. FOUND CAPTAIN`S MAP LIGHT HAD BURNING ODOR. R & R CAPT'S MAP LIGHT IAW AMM 33-13-07 OK FOR SERVICE.Jul 2, 2012 · N906EV · Cndair CL6002B19 · Flight Compartment LightingSDR A6WA201240755Support Angle · crackedPAX DOOR ASSIST MOTOR FWD SUPPORT ANGLE IN DOOR CRACKED. R & R PAX DOOR ASSIST MOTOR FWD SUPPORT ANGLE IAW SRM 51-40-11 & 51-42-06.Jul 2, 2012 · N451AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240768Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. R & R NEW DRAG ANGLE ON PAX DOOR IAW REO 601R-52-11-513, REV A.Jul 2, 2012 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012070501860Torque Link · unserviceableGEAR DISAGREE MESSAGE AFTER TAKE OFF, EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R TORQUE LINKS.Jul 1, 2012 · N682BR · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2012070301858A/C Pack · odorIN CRUISE FLT, AT 260, LEFT PACK HIGH TEMP MESSAGE. SMELLED OVERHEAT ODOR FROM LT PACK. PERFORMED OPS CHECK ON LT PACK IAW AMM 21-51-00. OPS CHECKED GOOD. NO FURTHER DEFECTS AT THIS TIME.Jun 30, 2012 · N836AS · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA201240644Transducer · failedON SHORT FINAL, LT ENGINE OIL PRESSURE READ ZERO, ALL OTHER INDICATIONS NORMAL. R & R LOW OIL PRESSURE SWITCH IAW AMM 79-31-01. R & R OIL PRESSURE TRANSDUCER IAW AMM 79-31-01 ON LT ENGINE. OPS CHECKED GOOD.Jun 30, 2012 · N7910 · Cndair CL6002B19 · Engine Oil Indicating SystemSDR A6WA201240697Skin · gougedLEFT FUSELAGE SKIN GOUGED JUST FWD OF FS 559.0 CUT OUT DAMAGED AREA, NDT, FABRICATE AND INSTALL REPAIR PARTS IAW REO 601R-53-41-610, REV, SRM 51-21-11, 51-25-06, 51-25-16, 51-42-06, 51-41-02, 51-42-13, 51-41-00.Jun 30, 2012 · N445AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2012070301857Lever · failedFLAPS FAILED AT 20 DEGREES. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. COMPLIED WITH FLAP FAIL AD 2009-06-12, R & R FLAP CONTROL LEVER, OPS CHECKED OK IAW AMM 27-51-01.Jun 29, 2012 · N920EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA2012070901877Floor Support · corrodedSEVERAL AREAS OF CORROSION ALONG RT CARGO FLOOR SUPPORT FROM FS 559+80 TO 559+112 AROUND FASTENER HOLES. FOUND DAMAGE DEPTH TO BE APPROX 0.30 WHICH EXCEEDS 10 PERCENT OF LOCAL THICKNESS OF 0.063. REMOVED FLOOR SUPPORT IAW SRM 51-42-06. FABRICATED A NEW FLOJun 28, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240696Vane · chafedLEFT INBD FLAP VANE L/E CHAFED FOUR SPOTS. REPAIRED CHAFED AREAS AT OTBD AND CENTER LOCATION ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C. R & R LT INBD FLAP VANE INBD L/E SKIN IAW SRM 51-42-13.Jun 28, 2012 · N445AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240753Striker · gougedPAX DOOR CUT OUT FWD SEAL STRIKER GOUGED AT FS 310.00. REPAIRED PAX DOOR CUT OUT FWD SEAL STRIKER IAW REO 601R-53-22-033, TYPE I REPAIR.Jun 28, 2012 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240754Cargo Track · corrodedCARGO TRACKS ON LBL 9 & RBL 9 AT FS 559+112 HAVE CORROSION. R & R CORRODED SEAT TRACKS AT FS 559+112 AT LBL9 & RBL9 IAW AMM 53-01-11.Jun 27, 2012 · N451AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR CA120628009Line · cracked(CAN) APU HAD HIGH ITT ON START, HIGH ITT WHEN AIR CONDITIONING PACK AIR DEMAND APPLIED AND APU AUTO SHUTDOWN. REMOVED APU AND FOUND THE COMPRESSOR DISCHARGE SENSE LINE, PN 3884967-1 TO THE VARIABLE GUIDE VANE ACTUATOR, PN 126842-2-1, BROKEN AT THE B-NUT FLAIJun 27, 2012 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA201240692Floor Support · corrodedFLOOR SUPPORT CORRODED FOUND AROUND SCREW HOLES ON TOP OF CAP ON LBL 27 BETWEEN FS 574 & FS 621. R & R WITH SERVICEABLE FLOOR SUPPORT CAP IAW REO 601R-53-61-3778.Jun 26, 2012 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2012062400007Engine · malfunctionedDURING INITIAL CLIMB AT 600 FEET, CREW REPORTED COMPRESSOR STALL AND POWER SURGE IN LEFT ENGINE. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND DETERMINED LEFT ENGINE NEEDED TO BE REMOVED AND REPLACED. PERFORMED VISJun 24, 2012 · N226JS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA2012062801830Oil System · fluctuatesLEFT ENGINE OIL PRESSURE EICAS MESSAGE FOR FIVE SECONDS ON CLIMBOUT THRU 8000. OIL PRESSURE READOUT FLUCTUATED BETWEEN 26-45 EMERGENCY DECLARED RETURNED TO DEPARTURE, SHUTDOWN NR 1 ENGINE ON GROUND DURING TAXI. SERVICED LT ENGINE IAW AMM 12-13-79. NO DEFJun 24, 2012 · N916EV · Cndair CL6002B19 · Engine Oil Indicating SystemSDR A6WA201240603Smoke Detector · malfunctionedRECEIVED SMOKE TOILET AMBER CAS MESSAGE IN FLIGHT. COMPLIED WITH "QRH" NO EVIDENCE OF SMOKE OR FUMES EVIDENT. RECEIVED AT CRUISE FL 290 MESSAGE POSTS INTERMITTENTLY ON GROUND. R & R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD.Jun 24, 2012 · N459AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA201240700Panel · damagedPANEL NR422 DB DIVIDER PANEL KNIFE EDGED. REMOVED UNSERVICEABLE DIVIDERS AND REPLACED WITH SERVICEABLE IAW SRM 51-42-06.Jun 24, 2012 · N445AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201240698Trunnion · damagedLEFT LOWER AFT, LOWER FLANGE OF MLG TRUNNION FITTING HAS ONE OVERSIZE HOLE. REPAIRED HOLE ON LT LOWER MLG TRUNNION FLANG IAW REO 601R-57-21-1699, REV.Jun 24, 2012 · N445AW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR A6WA201240699Retainer · crackedPANEL 422BT, AFT DIVIDER PANEL RETAINER CRACKED. REMOVED UNSERVICEABLE AFT DIVIDER ON PANEL 422BT AND REPLACED WITH SERVICEABLE DIVIDER 601R37003-180 IAW SRM 51-42-06.Jun 24, 2012 · N445AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201240756Bracket · crackedSYS 3 BRAKE ACCUMULATOR FWD OTBD BRACKET CRACKED. R & R BRACKET WITH NEW SERVICEABLE BRACKET SRM 51-42-06 AND 51-41-11.Jun 24, 2012 · N451AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240703Skin · gougedPAX DOOR CUT OUT FWD SEAL STRIKER AT FS 310.00 IS GOUGED. C/W REO 601R-53-22-033, REV C BY TRIMMING OUT DAMAGE & INSTALLING STRAP DOUBLER.Jun 23, 2012 · N445AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201240701Stiffener · crackedLEFT JET PIPE FWD STIFFENER AT 3 O`CLOCK POSITION IS CRACKED BEYOND STOP DRILL. REPAIRED LT JET PIPE FWD STIFFENER AT 3 O`CLOCK POSITION IAW CMM 78-11-00, SRS 042.Jun 22, 2012 · N445AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201240693Structure · chafedLEFT AND RIGHT MLG DOORS L/E CHAFED. CUTTING AWAY DAMAGED INNER SKIN ON LT MLG DOOR. BLENDED AND SMOOTHED MINOR CHAFING IAW REO 601R-52-82-034 & 601R-52-82-102Jun 22, 2012 · N455AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240694Handle · crackedCARGO DOOR OUTER HANDLE CRACKED. R & R CARGO DOOR OUTER HANDLE IAW SRM 51-42-21.Jun 22, 2012 · N445AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240596Warning Message · illuminatedCOOL CAUTION MESSAGE AFTER TAKEOFF, APROX 800 FT, COMPLIED WITH QRH, MESSAGE PERSISTED.Jun 21, 2012 · N464AW · Cndair CL6002B19 · Air Distribution SystemSDR AA6WA201240595Computer · failedON TAKEOFF ROLL, F/O RECEIVED RED FLT DIRECTOR FLAG ON PFD AND AIRSPEED INDICATION WAS ERRATIC. ABORTED TAKEOFF AT 117 KNOTS, BTMS 7786. TROUBLESHOT SYSTEM AND FOUND FCC2 FAILING. REPLACED FCC 2 IAW AMM 22-12-04. PERFORMED OPS CHECKS. NO DEFECTS AT THIS TJun 21, 2012 · N403AW · Cndair CL6002B19 · Flight Management Computing Hardware SystemSDR A6WA201240595Computer · failedON TAKEOFF ROLL, F/O RECEIVED RED FLT DIRECTOR FLAG ON PFD AND AIRSPEED INDICATION WAS ERRATIC. ABORTED TAKEOFF AT 117 KNOTS, BTMS 7786, TROUBLESHOT SYS AND FOUND FCC 2 FAILING. REPLACED FCC2 IAW AMM 22-12-04. PERFORMED OPS CHECKS. NO DEFECTS AT THIS TIME.Jun 21, 2012 · N403AW · Cndair CL6002B19 · Flight Management Computing Hardware SystemSDR A6WA201240650Control Unit · failedDURING GEAR RETRACTION, AFTER DEPARTURE, STABILIZER TRIM CAUTION MESSAGE ON ED1, RESET FAILED AS SOON AS YOKE TRIM WAS MOVED, ANOTHER RESET WAS ATTEMPTED AND FAILED WITH TRIM SWITCH MOVEMENT, CONTROL FORCES WERE HARD AND GETTING WORSE WITH INCREASE IN SPEED, AJun 21, 2012 · N450AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA2012070201849Frame · corrodedFRAME AT FS 33.00 HEAVILY CORRODED. REMOVED AND REPLACED FRAME SECTION IAW SRM 51-42-06 & 51-42-21.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2012070901875Angle · corrodedCORROSION ON SERVICE DOOR LOWER SILL ANGLE FWD EDGE. REMOVED SERVICE DOOR LOWER SILL ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 51-42-06 & 51-42-21, 53-00-00. S DRILLED, LOCATED AND INSTALLED NEW SILL ANGLE, IAW SRM 51-40-11.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012070901876Frame · corrodedFRAME AT FS 364.00 IS HEAVILY CORRODED. REMOVED FS 364.00 FRAME IAW SRM 51-42-06 AND 51-42-21. DRILLED UP NEW FRAME IAW SRM 51-40-11. INSTALLED NEW FRAME IAW SRM 51-42-06 & 51-41-21.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201240681Floorbeam · crackedFLOORBEAM, FS 280.00 IS CRACKED JUST OTBD OF RBL 9. REPAIRED IAW REO 601R-53-11-2338 BY CUTTING AWAY DAMAGE AND INSTALLING REPAIR ANGLE AND FILLERS.Jun 17, 2012 · N444ZW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2012061600848Engine · vibrationABORTED TAKEOFF AT 60-70 KIAS. FOR HIGH ITT (948) AND N2 SHOWING VIBRATION ALONG WITH FEELING VIBRATION IN THROTTLES AND AIRFRAME. NO EMERGENCY DECLARED, RETURNED TO GATE WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RIGHT ENGINE IAW AMM 71-00-00 AND CHECKJun 16, 2012 · N8948B · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201240675Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE WITH NEW SERVICEABLE DRAG ANGLE IAW REO 601R-52-11-513, REV A.Jun 15, 2012 · N444ZW · Cndair CL6002B19 · Passenger/Crew Doors
Back to GE CF34-3B1