GE CF34-3B1

Service difficulty reports · 5,402

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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 A6WA201240676Step · crackedPAX DOOR STAIR STRUCTURE IS CRACKED ON FWD SIDE OF 4TH STEP. REPAIRED FWD SIDE PANEL AT 4TH STEP ON PAX DOOR IAW REO 601R-52-11-702.Jun 15, 2012 · N444ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240674Step · crackedPAX DOOR STAIR STRUCTURE CRACKED ON AFT SIDE PANEL @ 3RD STEP. REPAIRED PAX DOOR AFT SIDE PANEL @ 3RD STEP IAW REO 601R-52-11-702, REV C.Jun 15, 2012 · N444ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240679Floor Support · corrodedCARGO DOOR FLOOR SILL HAS CORROSION AROUND SCREW HOLES UPPER LOWER SIDES. REMOVED UNSERVICEABLE CARGO DOOR FLOOR SILL AND REPLACED WITH SERVICEABLE FLOOR SILL PN 60135011-63 IAW SRM 51-42-06, 51-40-11.Jun 14, 2012 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240643Sill · corrodedPAX DOOR LOWER SILL FWD AND AFT CLEATS CORRODED. REMOVED FWD CLEAT, REMOVED CORROSION, RESTORED FINISH. REINSTALLED, REMOVED OUT OF LIMITS AFT CLEAT. LOCATED AND INSTALLED NEW CLEAT IAW SRM 51-21-06, 51-21-16, 51-42-13, 51-42-06.Jun 13, 2012 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240678Floor Support · corrodedPAX DOOR SILL FLOOR SUPPORT STRUCTURE HAS CORROSION. REMOVED PAX DOOR SILL FLOOR SUPPORT ANGLE AND REPLACED WITH SERVICEABLE ANGLE IAW SRM 51-24-21, 51-42-06, 51-42-21.Jun 13, 2012 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA120615005Line · leaking(CAN) DURING A LEAK CHECK OF THE FUEL SHROUD, PN C68C37, FOLLOWING RE-INSTALLATION, THE APU FUEL FEED LINE WAS FOUND TO BE LEAKING. UPON CLOSER INSPECTION, THIS APU FUEL FEED LINE WHICH IS PART OF THE FUEL TUBE ASSY, PN 601R62662-5 WAS FOUND BADLY CORRODED ANJun 13, 2012 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR A6WA201240672Structure · damagedPAX DOOR AFT CORNER DAMAGED. REPAIRED PAX DOOR AFT CORNER IAW REO 601R-52-11-2066.Jun 12, 2012 · N444ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012070601862Glowstrip · missingRT AFT PHOTOLUMINESCENT AISLE PATH MARKER IS MISSING THE CHEVRON MARKER. INSTALLED NEW SERVICEABLE CHEVRON MARKER IAW AMM 33-51-01-400-806. (SDR CLOSED)Jun 11, 2012 · N901EV · Cndair CL6002B19 · Emergency EquipmentSDR A6WA201240669Fitting · crackedPILOTS SIDE POST LOWER FITTING CRACKED. REMOVED UNSERVICEABLE WINDOW POST LOWER FITTING. REPLACED WITH SERVICEABLE FITTING, PN 601R33235-3S.Jun 11, 2012 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240680Floor Support · corrodedFLOOR SUPPORT LBL27 IN CARGO AREA HAS CORROSION. REMOVED UNSERVICEABLE LBL27 FLOOR SUPPORT CAP AND INSTALLED SERVICEABLE LBL 27 FLOOR SUPPORT CAP IAW SRM 51-42-06, 51-42-27, REO 601R-53-61-3778, REV A.Jun 9, 2012 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240670Cargo Track · corrodedRIGHT 9G INBD CARGO TRACK HAS CORROSION. R & R RT 9G CARGO TRACK IAW AMM 53-01-11.Jun 7, 2012 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240673Exhaust Duct · dentedLEFT JET PIPE HAS SMALL SHARP DENT ON THE TOP SIDE. PERFORMED REPAIR ON LIGHT JET PIPE TOP SIDE IAW CMM 78-11-00.Jun 7, 2012 · N444ZW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201240677Cargo Track · corrodedLT 9G INBD AND OTBD TIE DOWN TRACKS HAS CORROSION. R & R LT 9G CORRODED TIE DOWN TRACKS IAW AMM 53-01-11.Jun 7, 2012 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240671Cargo Track · corrodedTWO TIE DOWN TRACKS ON LBL 9 IN CARGO AREA HAS CORROSION. R & R TIE DOWN TRACKS ON LBL 9 IAW AMM 53-01-11.Jun 7, 2012 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240682Bulkhead · gougedPRESSURE BULKHEAD FS 202.75 IS GOUGED JUST OTBD OF PARKING BRAKE CONTROL CABLE PASS THRU. REPAIRED BULKHEAD IAW REO 601R-53-11-563, REV B, REPAIR TYPE V.Jun 7, 2012 · N444ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240629Attach Fitting · crackedFS 484 CLIP AT LBL27 CRACKED. R & R CRACKED CLIP AT FS 484.00 IAW SRM 53-41-43, REO 601R-53-41-059.Jun 5, 2012 · N402AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR CA120605012Link · cracked(CAN) WHILE CARRYING OUT A DETAILED INSPECTION OF THE RT WING ATTACHMENT LINK IAW TASK RJ2-53-160-501, THE AME FOUND WHAT LOOKED LIKE CRACKS ON THE UPPER SPHERICAL BEARING IN THE LINK. THIS WAS CONFIRMED BY HAVING A EDDY CURRENT INSPECTION PERFORMED IN-SITU. Jun 4, 2012 · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA201240582Diode · failedRECEIVED RT THRUST REVERSER UNLOCK CAUTION MESSAGE, TESTED AFTER ROTATION INDICATION ONLY. NO PERFORMANCE CHANGE. COMPLIED WITH QRH MESSAGE PERSISTED. R & R DIODE MODULE TB207-7-2CR7KE IAW WIRE MANUAL 78-30-00. THRUST REVERSERS OPS CHECKED GOOD IAW 78-30-0Jun 3, 2012 · N462AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240628Cargo Track · corrodedCARGO COMPARTMENT TIE DOWN TRACKS FS 559.00+96, RBL9 & LBL9 AND LBL27 HAVE CORROSION. R & R RBL9 & LBL9 TIE DOWN TRACKS DUE TO HEAVY CORROSION. PN N126-1075 IAW CRJ 200 51-40-11, AMM 53-01-11. REMOVED CORROSION LBL 27, 559.00+96 IAW SRM 51-21-06, 51-12-00. Jun 3, 2012 · N402AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240660Bulkhead · dentedREPAIR BULKHEAD AT WL 76.5, LBL 13.80, 601R-53-61-4481. REPAIR BULKHEAD COMPLIED WITH CARD DMI16232 AT WL 76.5, LBL 13.80, 601R-53-61-4481. FABRICATED AND INSTALLED FILLER, SHIM AND DOUBLER IAW REO 601R-53-61-4526.Jun 3, 2012 · N402AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240634Floor Support · corrodedFLOOR SUPPORT CAP CORRODED IN SEVERAL PLACES FROM FS 574 TO FS 621 LBL 27. R & R FLOOR SUPPORT CAP IAW SRM 57-61-43 & REO 61R-53-61-3778, REV A & REPAIRED CORROSION DAMAGE AROUND NUTPLATE HOLES ON INBD & OTBD SIDE OF LBL 27.0 AT FS 615 IAW REO 601R-53-61-453Jun 2, 2012 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240632Floor Support · corrodedFLOOR SUPPORT CAP BS 569-610 IS CORRODED. R & R FLOORBEAM CAP IAW SRM 51-42-21.Jun 1, 2012 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012071701910Sill · corrodedSERVICE DOOR SILL IS CORRODED BETWEEN FS 319-349. R & R SERVICE DOOR SILL IAW EO 600-53-0724.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240633Cargo Track · corrodedLAST SECTION OF CARGO TRACK ON LBL 9 JSUT FWD OF THE 621 BULKHEAD CORRODED. REPLACEED CARGO TRACK.May 31, 2012 · N449AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240637Trunnion · damagedDURING COLD WORKING OF MLG TRUNNION LOWER FLANGES, FOUND 2 TOTAL OVERSIZED HOLES 1 LT, 1 RT. COLD WORKED IAW REO 601R-57-21-1687.May 30, 2012 · N449AW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR ASOA201201706Engine · oil consumptionLOW OIL PRESSURE WARNING ENROUTE, DIVERTED. EMERGENCY DECLARED. SERVICED RT ENGINE OIL SYS IAW AMM 12-13-79. ADDED 5.5 QTS. PERFORMED OIL CONSUMPTION CHECK ON RT ENG IAW AMM 71-00-00-710-810. RAN ENGINE 18 MINS- 0 QTS CONSUMPTION. CHECKED GOOD. ACFT OK May 29, 2012 · N971EV · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201240702Support Bracket · crackedHYS SYSTEM NR 1 ACMP CASE DRAIN FILTER SUPPORT BRACKET CRACKD AND WARPED. R & R BRACKET IAW SRM 51-42-06.May 28, 2012 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR CA120528007Pcu · cracked(CAN) DURING A SCHEDULED HEAVY CHECK INSPECTION TASK RJ2-27-900-150 FOR FUNCTIONAL CHECK OF EACH AILERON POWER CONTROL UNIT, PCU, THE AME FOUND THE OUTPUT LINK ON THE RT SIDE OTBD AILERON PCU CRACKED. THE LINK WILL BE REPLACED BEFORE ACFT DEPARTS HEAVY.May 27, 2012 · Cndair CL6002B19 · Aileron Control SystemSDR ASOA2012071701908Battery Pack · dischargedPERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-801, FAILED OPS CHECK. TROUBLESHOT EMERGENCY LIGHTS AND FOUND ALL 4 BATTERY PACKS FULLY DISCHARGED IAW AMM 33-51-00-00. REPLACED ALL 4 EMERGENCY LIGHT BATERY PACKS IAW AMM 33-51-04-000-801 & 33-51-May 26, 2012 · N824AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012071701909Battery Pack · dischargedPERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-801 FAILED OPS CHECK. TROUBLESHOT EMERGENCY LIGHTS AND FOUND ALL 4 BATTERY PACKS FULLY DISCHARGED IAW AMM 33-51-00-00. REPLACED ALL 4 EMERGENCY LIGHT BATERY PACKS IAW AMM 33-51-04-000-801 & 33-51-04May 26, 2012 · N824AS · Cndair CL6002B19 · Emergency LightingSDR A6WA201240641Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513, REV A.May 25, 2012 · N449AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240638Vane · chafedLEFT INBD FLAP VANE IS CHAFED. REPAIRED LT INBD FLAP VANE IAW ROE 601R-57-52-004, REV C AND SRM 51-12-00, 51-21-11, 51-25-06, 51-25-16 AND 51-25-26.May 25, 2012 · N449AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240639Vane · chafedRT INBD FLAP VANE HAS 3 CHAFED SPOTS ON L/E. REPAIRED RT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C AND SRM 51-12-00, 51-21-11, 51-25-06, 51-25-16, 51-25-26.May 25, 2012 · N449AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240575Warning Message · illuminatedON CLIMB OUT, RECEIVED RT THRUST REVERSER UNLOCK MESSAGE. COMPLIED WITH QRH, SELECTED EMERGENCY STOW, RT THRUST REVERSER UNLOCK MESSAGE PERSISTS, WITH THRUST LEVER AT IDLE, FELT SLIGHT VIBRATION IN AIRFRAME, NO ABNORMAL N1 OR N2 VIBRATION INDICATIONS. VIBRATMay 24, 2012 · N462AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240630Attach Fitting · crackedRBL 9 INBD ATTACH FITTING CRACKED AT FS 280. R & R CRACKED ATTACH FITTING IAW SRM 51-42-06 & 51-42-21.May 24, 2012 · N449AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR CA120529011Blade · cracked(CAN) WHILE PERFORMING A SCHEDULED BOROSCOPE INSPECTION OF THE LT ENGINE COMPRESSOR BLADES, VARIABLE GUIDE VANES AND STATIONARY VANES IAW TASK RJ2-72-430-107, THE AME FOUND THE STAGE 9 COMPRESSOR HAD SEVERAL BLADES MIGRATING AT THE ROOT AT THE AFT SIDE OF THE May 24, 2012 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA201240640Structure · chafedLT MLG DOOR CHAFED L/E CORNER BY DOOR BRUSH. REMOVED UNSERVICEABLE EXISTING FILLER AND REPLACED WITH SERVICEABLE FILLER IAW REO 61R-52-82-034, REV NC.May 23, 2012 · N449AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240642Structure · chafedRT MLG DOOR L/E CHAFED. REMOVED UNSERVICEABLE FILLER AND REPLACED WITH SERVICEABLE FILLER IAW REO 601R-52-82-034.May 23, 2012 · N449AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240631Threshold · corrodedSERVICE DOOR THRESHOLD HAS CORROSION ON UPPER MOUNTING HOLES. REPLACED UNSERVICEABLE SERVICE DOOR THRESHOLD (BLENDED 0.062, 0.042" MATERIAL REMAINING WITH SERVICEABLE SERVICE DOOR THRESHOLD IAW SRM 53-00-00, FIG 102, SRM 51-40-11.May 23, 2012 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA120524011Shaft · failed(CAN) FLT DECK HAD BURNED RUBBER SMELL AND PUFF OF BLUE SMOKE FROM VENTS IN FLT DECK ON START RT PACK AT FAULT FOR SMOKE, INSPECTION OF ACM DETERMINED SHAFT FAILURE OF ACM, REPLACED ACM AND OPS CHECKS C/O WITH NO FUTHER FAULTS NOTED IAW AMM 21-51-10-04. TEARDOMay 23, 2012 · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA201240558Attach Fitting · gougedPANEL 444AT GOUGED IN INBD SIDE ATTACH FITTING. REPAIR GOUGE ON INBD SIDE ATTACH FITTING IAW REO 601R-78-33-3992 REV, NC.May 19, 2012 · N437AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240557Attach Fitting · gougedPANEL 444AB GOUGED ON INBD ATTACH FITTING. REPAIR GOUGE ON PANEL 444AB ATTACH FITTING IAW REO 601R-78-33-3992, REV NC.May 19, 2012 · N437AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA120518001Wire · burned(CAN) WHILE INVESTIGATING AN UNRELATED ADG DEFECT ON THE ACFT, AN AME MADE DISCOVERY OF SOME BURNED WIRES ON THE WIRING FOR THE 3A HYD. PUMP POWER RELAY K1DB. WIRE DB18B12WHT HAS OVERHEATED AND BURNED APPROXIMATELY THE LAST 8" FROM THE END. IT MAYBE A RESULMay 16, 2012 · Cndair CL6002B19 · Electrical Power System WiringSDR REXA2012051500744Engine · malfunctionedFLT 4147 CVG-PHL HAD ITT ON NR 2 ENGINE RISE CREW HEARD LOUD BANG AND A/C STARTED SHAKING. CREW FOLLOWED QRH PROCEDURES SHUT DOWN NR 2 ENG AND RETURNED TO CVG. CREW DID DECLARE EMERGENCY. MX ONSITE INSPECTED OUTSIDE OF ENGINE NO DEFECTS FOUND. PERFORMED DFMay 15, 2012 · N8869B · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201240608Structure · damagedCORE COWLING 435AB INBD L/E CORNER DAMAGED. CUTOUT DAMAGED CORNER OF 435AB CORE COWL INBD L/E IAW CMM 71-12-01. SEE FORM 412 FOR FAB AND INSTALL OF FILLER AND DOUBLER.May 15, 2012 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201240610Structure · gougedCORE COWL 435AB DAMAGE ON INNER CENTER STIFFENER. BLENDED GOUGE ON INNER CENTER HOT CHANNEL .050. REMOVED .008 REMAINING, .042 WITHIN LIMITS USING AMM 51-21-400 IAW CMM 71-12-01, SRM 51-21-11, 57-25-06, 51-25-26.May 15, 2012 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201240609Structure · damagedCORE COWLING 435AT INBD L/E CORNER DAMAGED CUTOUT DAMAGED AREA OF 435AT CORE COWLING INBD L/E CORNER IAW CMM 71-12-01. SRS18 SEE FORM 412 FOR INSTALL, FAB OF DOUBLER AND FILLER.May 15, 2012 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR CA120517003Engine · overtemp(CAN) NR 2 ENGINE ITT SHOW UP IN RED 798 DEGREE , FOLLOWED BY A SHUDDERED WITH A LOUD BANG. ENGINE WOULD NOT RESPONSIVE TO THROTTLE ADVANCE IAW QRH, RETURN TO IDLE AND SHUTDOWN.May 15, 2012 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA2012051400731Switch · failedRIGHT THRUST REVERSER NOT DEPLOYING, DEFER OUTBOARD IAW MEL 78-30-01 AUT NR 63568. REMOVED AND REPLACED DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECK GOOD, CLEAR DM X63568 PLACARD REMOVED.May 14, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust ReverserSDR CA120515006Oil System · leaking(CAN) AFTER ARRIVAL, RAMP CREW ADVISED CAPTAIN THAT SMOKE WAS COMING FROM APU EXHAUST. APU WAS SHUTDOWN AND SMOKE STOPPED. MAINTENANCE NOTED HISTORY OF HIGH OIL CONSUMPTION FOR THIS APU. UNIT WAS DEFERRED IAW MEL AND DEPARTED WITH MINIMAL DELAY. APU WAS CHMay 14, 2012 · Cndair CL6002B19 · APU Oil System
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