Saab 340B

Service difficulty reports · 8,975

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 aircraft_model_key = '340B'
  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 MALA020475Channel · corrodedDURING 4K/2Y/4Y INSPECTION IN CWA, LBL 11 CHANNELS BETWEEN FRAMES 236 AND 258 HAVE CORROSION. MAINTENANCE REMOVED CORROSION, REPLACED BEAM AND ANGLE IAW SRM 51-40-20.Aug 14, 2002 · N448XJ · Saab 340B · Fuselage Miscellaneous StructureSDR MALA020479Seat Track · corrodedDURING 4K/2Y/4Y INSPECTION IN CWA, GALLEY AREA SEAT RAIL HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.Aug 14, 2002 · N448XJ · Saab 340B · Fuselage, Seat/Cargo Attach FittingsSDR MALA020478Structure · corrodedDURING 4K/2Y/4Y INSPECTION IN CWA, LEFT FWD SEAT TRACK WRAP AROUND HAS CORROSION. MAINTENANCE REMOVED AND REPLACED WRAP AROUND.Aug 14, 2002 · N448XJ · Saab 340B · Fuselage Miscellaneous StructureSDR MALA020477Seat Track · corrodedDURING 4K/2Y-4Y INSPECTION CARGO AREA SEAT TRACK SIDES HAVE CORROSION AT INFILL PANEL AREA. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.Aug 14, 2002 · N448XJ · Saab 340B · Fuselage, Seat/Cargo Attach FittingsSDR MALA020468Connector · not seatedDURING FLIGHT 3247, EN ROUTE TO CMX, RIGHT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE UPON GEAR DOWN SELECTION. PILOT TRIED TO RELAMP, THIS DID NOT HELP. OVERFLEW CMX WENT ON TO MSP AND LANDED. UPON LANDING IN MSP CREW HAD NO GREEN INDICATION. DIVERSION TO MAug 14, 2002 · N441XJ · Saab 340B · Landing Gear Position and WarningSDR MALA020467Power Supply · looseDURING FLIGHT 2756 EMERGENCY POWER SUPPLY CAUTION LIGHT ILLUMINATED. AIR TURNBACK TO MSP. MAINTENANCE RESECURED EMERGENCY POWER SUPPLY (JET PACK) IN AVIONICS RACK. OPS CHECK GOOD.Aug 14, 2002 · N366PX · Saab 340B · Battery/Charger SystemSDR MALA020474Seat Track · corrodedDURING 4K/2Y-4Y INSPECTION IN CWA, CARGO AREA SEAT TRACK LBL 18.3 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.Aug 13, 2002 · N448XJ · Saab 340B · Fuselage, Seat/Cargo Attach FittingsSDR CX7A194J18Access DoorLav service door opened in flight. Causing A/C not to hold pressurization.Aug 12, 2002 · N304CE · Saab 340B · Fluid Service DoorsSDR SIMA200224010Trunnion · damagedABI - DURING INSPECTION DAMAGE WAS NOTED ON THE RIGHT MLG FORWARD TRUNNION, FORWARD OUTBOARD ATTACHMENT HOLE. THE DAMAGE WAS IN THE FORM OF THREAD MARKS OVER THE ENTIRE LENGTH OF THE HOLE. DAMAGED HOLE WAS REAMED TO .5646 DIAMETER. REAMING THREAD MARKS WEREAug 12, 2002 · N373AE · Saab 340B · Main Landing Gear Attach SectionSDR CX7A194J16O-Ring · cutENGINE OIL PRESSURE (RT) CWP LIGHT ILLUMINATED INNTERMITTENTLY IN FLIGHT. RT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 25 PSI-60 PSI. REPLACED O-RING ON OIL BYPASS SENSOR IAW GE MM.Aug 9, 2002 · N300CE · Saab 340B · Engine Oil PressureSDR SIMA200222701Seat Track · corrodedMBV - FOUND PREVIOUS REPAIR ON FORWARD END OF SEAT TRACK 18.3L CORRODED. PREPARED AND INSTALLED EXTRUSION (P/N 7253799381) AND U-BEAM (P/N 7253799379) IAW SAAB 340 SRM 72LKS 3079 REV 40 53-70-60 PG 204/205. (M)Aug 9, 2002 · N334AE · Saab 340B · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200222103Frame · dentedABI - DURING INSPECTION, FOUND FRAME 630.112 DENTED. FABRICATED AND INSTALLED A DOUBLER IAW SAAB REPAIR STATEMENT 340SDS004197 PARA 3, AND STANDARD SRM PRACTICES. (M)Aug 8, 2002 · N334AE · Saab 340B · Fuselage Main, FrameSDR SIMA200222102Frame · dentedABI - DUIRNG INSPECTION, FOUND FRAME 677 DENTED. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SAAB REPAIR STATEMENT 340SDS004197 PARA 3 AND STANDARD SRM PRACTICES. (M)Aug 8, 2002 · N334AE · Saab 340B · Fuselage Main, FrameSDR SIMA200222101Frame · dentedABI - DURING INSPECTION, FOUND FRAME 686.66 DENTED. FABRICATED AND INSTALLED A DOUBLER IAW SAAB REPAIR STATEMENT 340 SDS 004197 PARA 3, AND STANDARD SRM PRACTICES. (M)Aug 8, 2002 · N334AE · Saab 340B · Fuselage Main, FrameSDR AUS20020883Engine · failed(AUS) LT ENGINE FAILURE. LIMITED INFORMATION PROVIDED.Aug 7, 2002 · Saab 340B · Engine (Turbine/Turboprop)SDR MALA020465Seat Track · corrodedDURING 4K INSPECTION IN CWA, BL 0 SEAT TRACK HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION, TREATED, PRIMED AND PAINTED SEAT TRACK IAW E SF340 SRM 51-70-40.Aug 7, 2002 · N410XJ · Saab 340B · Fuselage, Seat/Cargo Attach FittingsSDR MALA020464Seat Track · corrodedDURING 4K INSPECTION IN CWA, LBL 18.3 SEAT TRACK HAS CORROSION ON SIDE IN CARGO INFILL PANEL AREA. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.Aug 7, 2002 · N410XJ · Saab 340B · Fuselage, Seat/Cargo Attach FittingsSDR MALA020463Seat Track · corrodedDURING 4K INSPECTION IN CWA, LBL 18.3 SEAT TRACK HAS CORROSION AT FWD SECTION AND CENTER SECTION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.Aug 7, 2002 · N410XJ · Saab 340B · Fuselage, Seat/Cargo Attach FittingsSDR MALA020466Angle · corrodedDURING 4K INSPECTION IN CWA, RIGHT O/B FLOORBOARD ANGLE FROM STA 258-294 HAS CORROSION. REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENTS AND COATINGS IAW SRM 51-70-40.Aug 6, 2002 · N410XJ · Saab 340B · Fuselage Miscellaneous StructureSDR MALA020462Angle · corrodedDURING 4K INSPECTION IN CWA, FRAME ANGLE STA 272 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENTS AND COATINGS.Aug 6, 2002 · N410XJ · Saab 340B · Fuselage Miscellaneous StructureSDR MALA020461Support · corrodedDURING 4K INSPECTION IN CWA, SUPPORT AT LBL 11 BETWEEN STA 225 AND 236 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENTS AND COATINGS IAW SAAB SRM 51-70-40.Aug 6, 2002 · N410XJ · Saab 340B · Fuselage Miscellaneous StructureSDR MALA020460Angle · corrodedDURING 4K INSPECTION IN CWA, FRAME ANGLE AT STA 258 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENTS AND COATINGS IAW SAAB SRM 51-70-40.Aug 6, 2002 · N410XJ · Saab 340B · Fuselage Miscellaneous StructureSDR MALA020459Seat Track · corrodedDURING 4K INSPECTION IN CWA, I/B GALLEY SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENTS AND COATINGS IAW SAAB SRM 51-70-40.Aug 6, 2002 · N410XJ · Saab 340B · Fuselage, Seat/Cargo Attach FittingsSDR MALA020458Channel · corrodedDURING 4K-CHECK IN CWA, AIRSTAIR U-CHANNEL HAS CORROSION. MAINTENANCE REMOVED CORROSION SRM 51-70-40.Aug 6, 2002 · N410XJ · Saab 340B · Entrance StairsSDR MALA020452Angle · corrodedDURING 4K-CHECK IN CWA, FRAME ANGLE AT STA 225 HAS LIGHT SURFACE CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.Aug 6, 2002 · N410XJ · Saab 340B · Fuselage Miscellaneous StructureSDR CX7A194J15Engine · seizedAFTER ROTATION LT ENGINE OIL PRESSURE CWP- OIL PRESSURE GAUGE READ 0 PSI WHILE RUNNING ENGINE OIL PRESSURE CHECKLIST (TWO MINUTES MAX) ENGINE FAILED. RAN MEMORY ITEM AND CHECKLIST RETURNED FOR LANDING. REMOVED AND REPLACED LT ENGINE IAW GE AND SAAB AMM.Aug 5, 2002 · N318CE · Saab 340B · Engine (Turbine/Turboprop)SDR MALA020441Transponder · failedDURING FLIGHT 3016, WEATHER RADAR INOP. AIR TURNBACK TO DTW. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR TRANSPONDER. OPS CHECK GOOD IAW THE SF340 MM.Aug 1, 2002 · N425XJ · Saab 340B · Weather Radar SystemSDR CX7A194J14Sensor · will not testRT TAILPIPE HOT SENSOR DOES NOT TEST.Jul 31, 2002 · N307CE · Saab 340B · Overheat DetectionSDR PNSA020707Hub · crackedProp was removed to reseal blades and during repair rear hub half was found cracked.Jul 31, 2002 · N675PA · Saab 340B · Propeller Hub SectionSDR CX7A194J13Engine · stoppedDuring T/O roll, Tq was 94% on both engines, ITT below 890 degrees. After rotation at 80-100 feet, a bang and shudder was felt and ITT on the right engine ran away to max. Tq reduced to zero, prop autocoarsened. Engine had failed. Emergency declared.Mx R/RJul 30, 2002 · N306CE · Saab 340B · Powerplant SystemSDR MALA020440Control Valve · failedON FINAL APPROACH ON FLIGHT 3167, LANDING GEAR WOULD NOT EXTEND. ON ARRIVAL SELECTED GEAR DOWN, NO LIGHTS (GREEN) ILLUMINATED, INTRANSIT LIGHT ILLUMINATED. PERFORMED QRH, DIRECTED TO PULL EMERGENCY GEAR EXTENSION HANDLE. PULLED HANDLE AND GOT THREE GREEN. Jul 30, 2002 · N425XJ · Saab 340B · Landing Gear Retraction/Extension SystemSDR MALA020439Sensor · malfunctionedDURING TAXI OUT ON FLIGHT 2943, LT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. PRESSURE AND TEMPERATURE NORMAL. AFTER RETURNING, MAINTENANCE REPLACED LT ENGINE OIL PRESSURE SENSOR, OPS CHECK GOOD AMM 79-30-05-4.Jul 29, 2002 · N447XJ · Saab 340B · Engine Oil PressureSDR PNSA020706Fastener · looseON CLIMBOUT FROM ANC AN UNUSUAL VIBRATION WAS FELT IN CONTROL YOKE AND RUDDER PEDALS. AIRCRAFT RETURNED TO ANC. MAINTENANCE FOUND TAIL CONE ACCESS PANEL 317AB FORWARD TWO CAM LOCK FASTENERS LOOSE AND HANDLE FOR PANEL WAS STOWED WHICH MADE PANEL APPEARED INSTJul 28, 2002 · N675PA · Saab 340B · FastenersSDR MALA020438Engine · power lossDURING FLIGHT 3392, EXPERIENCED ROLLBACK AT 21,000 FT. -11 DEGREES CELSIUS, 59 PERCENT TORQUE. IN ICING CONDITIONS NO SHIFT IN ITT OR TORQUE WAS NOTICED. IGNITION LIGHT DID NOT ILLUMINATE. CREW COULD NOT DETERMINE WHICH ENGINE HAS THE ROLLBACK BUT BELIEVE IJul 26, 2002 · N411XJ · Saab 340B · Engine (Turbine/Turboprop)SDR MALA020437WeuDURING FLIGHT #2736 THE WHITE BITE LIGHT, LH FIRE WARNING AND CONFIG WARNING LIGHT ON. AIR RETURN TO MEM. MAINTENANCE REPLACED WARNING ELECTRICAL UNIT. WEU OPS CHECK GOOD. PN 005WS00 SN/ON 1394 SN/OFF 1586. AC OK FOR SERVICE IAW 31-50-05-4.Jul 26, 2002 · N404XJ · Saab 340B · Central WarningSDR MALA020433Structure · puncturedFOUND RT FUSELAGE PUNCTURED AT STA 363 BELOW PAX WINDOW REINFORCEMENT DOUBLER. COMPLETED REPAIR IAW EO S53009.Jul 24, 2002 · N362XJ · Saab 340B · Fuselage Miscellaneous StructureSDR SIMA200220502Fastener · elongatedFOUND RIGHT HORIZONTAL STABILIZER UPPER FORWARD SPAR CAP FASTENERS HOLE AT THE INBOARD END WAS FOUND TO BE ELONGATED. REMOVED HORIZONTAL STAB. LEADING EDGE RIB AND MOUNTING ANGLE ON THE SPAR WEB. FABRICATED A REPLACEMENT SECTION SPAR WEB, TWO DOUBLER, ANGLE Jul 23, 2002 · N352SB · Saab 340B · Fuselage Structure (General)SDR SIMA200220303Smoke · detectedFLIGHT ATTENDENT REPORTED SMOKE IN CABIN AT ROW 11 WITH FAINT BURNED SMELL IN CABIN CREW ELECTED TO RETURN. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. NO SOURCE OF SMOKE WAS FOUND. AIRCRAFT WAS RETURNED TO SERVICE.Jul 22, 2002 · N340RC · Saab 340B · Air Distribution SystemSDR MALA020435Transceiver · malfunctionedDURING FLIGHT 3384, CREW REPORTED THE LT INTAKE HEAT IS INOP. THE WEATHER RADAR IS INOP AND THE ENGINE POWER ROLLED BACK INFLIGHT. MAINTENANCE REPLACED WEATHER RADAR TXCVR, THE LT ENGINE ANTI-ICE MASTER CAUTION, LT INTAKE LIGHT ON. CND ON GROUND, RAN A/C FOJul 21, 2002 · N429XJ · Saab 340B · Weather Radar SystemSDR MALA020429Skin · dentedRT FUSELAGE TWO SKIN DENTS STA 340, WL 78.0 .035 DEPTH. STA 340, WL 94.5 , .032 DEPTH. MAINTENANCE REPAIRED BOTH DENTS IAW EO #S53009.Jul 20, 2002 · N368PX · Saab 340B · Fuselage Main, Plate/SkinSDR CX7A194J12HmuDuring climbout of MDW noticed that L/H engine torque was fluctuating 3%. Fluctuations then went to 5% swings. Ran checklist and put in T/M lockout. With T/M lockout engine still fluxed +/- 3% with prop sync on and off.R/R L/H engine HMU IAW SAAB AMMJul 20, 2002 · N304CE · Saab 340B · Fuel Controlling SystemSDR SIMA200220004Battery · inoperativeEMERGENCY FLOOR LIGHTS, INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY SUPPLY IAW MM. OPS CHECK GOOD.Jul 19, 2002 · N266AE · Saab 340B · Emergency LightingSDR MALA020427Connector · failedDURING FLIGHT 3054 CREW REPORTED FALSE AND WILD INDICATIONS AND FLUXUATIONS IN THE RADIO ALTIMETER. AIR RETURN TO DTW. MAINTENANCE FOUND AFT ALT. BAD ATENNA CONNECTOR BAD. REPLACED CONNECTOR. OPS CHECK GOOD.Jul 19, 2002 · N439XJ · Saab 340B · Independent Position Determining SystemSDR MALA020426Gcu · failedINFLIGHT ON 3238, THE RT GEN LIGHT CAME ON FOLLOWED QRH GEN RESET APPROXIMATLEY 5 MINUTES RT GEN LIGHT COMES ON, FOLLOWED QRH GEN WOULD NOT RESET. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED RT DC GEN AND RT GCU.ALL CHECKS GOOD AT THIS TIME.Jul 19, 2002 · N433XJ · Saab 340B · DC Generating SystemSDR MALA020411Indicator · failedON CLIMB AND IN CRUISE OF FLIGHT 2936, RT ENGINE ITT INDICATION. FUNCTIONED INTERMITTANTLY INDICATING BETWEEN 400 AND 700. IRRATICALLY ALL OTHER ENGINE INDICATIONS WERE NORMAL. AIR RETURN TO DTW. MAINTENANCE CND. INSTALLED SERICEABLE RT ITT INDICATOR SN/OFFJul 18, 2002 · N408XJ · Saab 340B · Engine Temperature Indicating SystemSDR SIMA200220514Frame · damagedNO DOCUMENTATION COULD BE FOUND FOR DOUBLER REPAIR ON LT AFT FUSELAGE, FORWARD OF CARGO DOOR. REMOVED PREVIOUS INSTALLED REPAIR DOUBLER AND PERFORMED A CUT OUT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM.Jul 17, 2002 · N352SB · Saab 340B · Fuselage Main, FrameSDR SIMA200220501Skin · crackedFOUND RT NACELLE OUTBOARD FORWARD SKIN HAS POSSIBLE CRACK AT RIVET. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND INDICATION OF A CRACK. PERFORMED CUT TO INNER SKIN TO GAIN ACCESS TO DAMAGE AREA. REMOVED DAMAGED SKIN BY CUTOUT AND PERFORMED AN NDT INSPEJul 17, 2002 · N352SB · Saab 340B · Nacelle/Pylon, Plate/SkinSDR MALA020410AcmDURING FLIGHT #2701, INFLIGHT BURNING SMELL IN COCKPIT NOT IN CABIN. COCKPIT DID NOT COOL DOWN, AUTO OR MANUAL. ON FINAL, BURNING SMELL INTENSIFIED. WAS TOLD BY FLIGHT ATTENDANT SHE COULD SMELL IT ALSO. NON-NORMAL SOUND COMING FROM BACK OF THE A/C. MAINTEJul 17, 2002 · N447XJ · Saab 340B · Cabin Cooling SystemSDR CX7A194J11Terminal · brokenRIGHT TAILPIPE HOT, DOES NOT TEST. REPLACED BROKEN TAILPIPE SENSOR TERMINAL RING.Jul 17, 2002 · N303CE · Saab 340B · Overheat DetectionSDR SIMA200220001Skin · damagedFOUND RT NACELLE INBOARD FORWARD SKIN HAS THREE RIVETS RECESSED THROUGH SKIN. PERFORMED CUT TO INNER SKIN TO GAIN ACCESS TO DAMAGED AREA. FABRICATED AN INNER SKIN SPLICE DOUBLER. REPAIR DONE IAW SRM PRACTICES.Jul 16, 2002 · N352SB · Saab 340B · Nacelle/Pylon, Plate/Skin
Back to Saab 340B