Saab SF340A

Service difficulty reports · 2,633

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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 aircraft_model_key = 'SF340A'
  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 MALA020414Skin · damagedDURING 4K-CHECK IN CWA, RT UPPER TAIL SKIN AT APPROXIMATELY STA 812. 5 1/4 INCH BELOW RUDDER FAIRING 5/8 INCH DIA .036 INCH DEEP. MAINTENANCE COMPLETED REPAIR IAW SRM 53-90-10. PARA 2 AND MAL EO #S53127. RELEASE DATE 7/17/02Jul 6, 2002 · N112XJ · Saab SF340A · Fuselage Main, Plate/SkinSDR MALA020416Floor Support · corrodedDURING 4K-CHECK IN CWA, LT OUTBOARD FLOORBOARD ANGLE AFT OF WING BOX CORRODED. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. REFER TO 409 109862. RELEASE DATE 7/17/2002Jul 5, 2002 · N112XJ · Saab SF340A · Fuselage Miscellaneous StructureSDR MALA020415Floor Panel · corrodedDURING 4K-CHECK IN CWA, LT FLIGHT DECK FLOOR HAS CORROSION ON THE FLOOR AND RIVET HEADS. MAINTENANCE PERFORMED REPAIRS AND REMOVED CORROSION IAW SRM 51-70-40 AND 53-60-50-2. REMOVED CORRODED RIVETS IAW 51-40-21. REFER TO 409# 109814. RELEASE DATE 7/17/02.Jul 5, 2002 · N112XJ · Saab SF340A · Fuselage Floor PanelSDR MALA020413Floor Panel · corrodedDURING 4K-CHECK IN CWA, RT FLIGHT DECK FLOOR HAS CORROSION. MAINTENANCE REPAIRED CORROSION AROUND FLOOR "SNAP" FASTENERS IAW SAAB SRM 53-60-50 AND SAAB STATEMENT 340SDS004125. REFER TO 409 109815Jul 3, 2002 · N112XJ · Saab SF340A · Fuselage Floor PanelSDR MALA020388Engine · overtempLT ENGINE ITT WENT TO 930. INSPECTED ENGINE INLET AND FOUND DEBRIS THAT CAUSED BLOCKAGE. FOUND NO DAMAGE.Jul 2, 2002 · Saab SF340A · Engine (Turbine/Turboprop)SDR 000174Warning System · activatedCREW LOWERED GEAR ON FINAL INTO AOO AND GOT ANTI-SKID FAIL. OPS DEFERRABLE, DISPATCH ADVISED AIRCRAFT CAN'T TAKEOFF FROM AOO WITH THE ANTI-SKID MEL. DISPATCH RETURNED AIRCRAFT TO PIT.Jul 1, 2002 · N108 · Saab SF340A · Landing Gear Brake SystemSDR MALA020383Frame · crackedRT NACELLE FWD LOWER FRAME AT NS 197.00 CRACKED. R&R FRAME IAW EO S54058.Jun 30, 2002 · N119XJ · Saab SF340A · Nacelle/Pylon, Main FrameSDR MALA020382Skin · chafedRT AFT FUSELAGE SKIN CHAFED FROM ELEVATOR CANOE PANEL. REPAIRED SKIN IAW SAAB STATEMENT 340 SDS004056.Jun 30, 2002 · N119XJ · Saab SF340A · Fuselage Main, Plate/SkinSDR MALA020381Shaft · corrodedCORROSION FOUND AT RUDDER CONCENTRIC SHAFT ASSY. REMOVED AND REPLACED SHAFT.Jun 30, 2002 · N119XJ · Saab SF340A · Rudder Control SystemSDR MALA020380Fastener · corrodedSEVERAL AREAS AROUND FLT DECK FLOOR SNAP FASTENERS HAVE PITTING CORROSION. REMOVED AND TREATED IAW SRM 51-70-40. PERFORMED REPAIRS IAW SRM 53-60-50.Jun 30, 2002 · N119XJ · Saab SF340A · FastenersSDR MALA020379Floor Panel · corrodedPITTING CORROSION LOCATED ON THE FLOOR, LT SIDE OF CAPTAINS CONTROL COLUMN STA 177 TO STA 185. REMOVED AND REPAIRED DECK FLOOR IAW 177-185 EO S53124.Jun 30, 2002 · N119XJ · Saab SF340A · Fuselage Floor PanelSDR MALA020378Floor Panel · corrodedFLIGHT DECK FLOOR HAS LIGHT CORROSION. REMOVED AND TREATED IAW SRM 51-70-40.Jun 30, 2002 · N119XJ · Saab SF340A · Fuselage Floor PanelSDR MALA020377Seat Track · corrodedAISLE SEAT TRACK ANGLE FROM STA 339 TO STA 622 HAS LIGHT CORROSION.REMOOVED CORROSION IAW SRM 53-70-60.Jun 30, 2002 · N119XJ · Saab SF340A · Fuselage, Seat/Cargo Attach FittingsSDR MALA020376Galley Track · corrodedRT I/B GALLEY SEAT TRACK HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 53-70-40.Jun 30, 2002 · N119XJ · Saab SF340A · Fuselage, Seat/Cargo Attach FittingsSDR MALA020375Structure · corrodedCORROSION FOUND IN FWD RT GALLEY AREA UNDER PANEL 122AZ. REMOVED IAW SRM 53-70-40.Jun 30, 2002 · N119XJ · Saab SF340A · Fuselage Miscellaneous StructureSDR MALA020374Camlock · crackedRT OUTBOARD NACELLE AT FIG 8 CAMLOCK HAS HOLE AND CRACKS.REPAIRED IAW EO 54058.Jun 30, 2002 · N119XJ · Saab SF340A · Nacelle/Pylon, Main FrameSDR MALA020373Warning Light · illuminatedRT DUCT TEMP LIGHT ILLUMINATED IN FLIGHT. AIR TURNBACK TO DTW.R&R PRSOV.Jun 29, 2002 · N142XJ · Saab SF340A · Central WarningSDR MALA020372Connector · arcedFLIGHT ATTENDANT REPORTED SPARKS BEHIND FA PANEL. MX FOUND CONNECTOR PLUG ARCING TO SWITCHES. WRAPPED CONNECTOR PLUG WITH COMPRESSION TAPE. ALL CHECKS GOOD.Jun 29, 2002 · N110XJ · Saab SF340A · Electrical Power System WiringSDR MALA020371Lock · malfunctionedCONFIG LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF, NOT HIGH ENERGY ABORT. CLEANED FRICTION LOCKS, ALL CHECKS GOOD.Jun 29, 2002 · N109XJ · Saab SF340A · Power LeverSDR AUS20020983Propeller · faulty(AUS) N2 ENGINE PROPELLER AUTOCOARSEN. CAUSED BY INCORRECT SELECTION OF PROPELLER CONTROLS.Jun 27, 2002 · Saab SF340A · Propeller Controlling SystemSDR MALA020369Hmu · failedLT ENGINE OVERTEMP. HIGH ENERGY ABORT. MAX WAS 936. NO OVERTEMP LIGHT ILLUMINATED. REPLACED LT HMU AND T4.5 TRIMMER ADJUSTED, GPA CHECKS GOOD.Jun 27, 2002 · N991XJ · Saab SF340A · Fuel Controlling SystemSDR MALA020365Pump · leakingLOST HYDRAULIC PRESSURE ON TAXI OUT. HYDRAULIC CAUTION LIGHT CAME ON ON CWP. TRIED OVERRIDE, PUMP DID NOT COME ON THE MAIN, ACCUMULATORS DRAINED DOWN TO RED LINE. REPLACED HYDRAULIC PUMP. ALL CHECKS GOOD.Jun 25, 2002 · Saab SF340A · Hydraulic Pump (Electric/Engine), MainSDR AUS20020668Indicator · leaking(AUS) AIR SPEED INDICATOR (ASI) FAULTY. ASI FOUND TO HAVE A CASE LEAK.FOUND DURING INSTALLATION CHECK. THE ASI HAD BEEN RECENTLYREPAIRED. PERSONNEL/MAINTENANCE ERROR.Jun 20, 2002 · Saab SF340A · Airspeed/Mach IndicatorSDR MALA020361Control Valve · malfunctionedWHEN SELECTING GEAR DOWN DID NOT GET 3 GREEN LIGHTS, RESET LANDING GEAR CONTROL CB AND GOT 3 GREEN. R&R LANDING GEAR CONTROL VALVE IAW AMM32, PERFORMED GEAR SWING AND LEAK CHECKS. ALL CHECKS GOOD.Jun 20, 2002 · Saab SF340A · Landing Gear Retraction/Extension SystemSDR CA020626001Engine · leaking(CAN) TAKEOFF ABORTED DUE TO OIL FLUCTUATION. MAINTENANCE FOUND OIL LEVEL LOW. AS OIL HAD BEEN TOPPED UP 3 AIR HOURS BEFORE - LEAK RUNS WERE CARRIED OUT. ENGINE RUN FOR 1/2 HOUR WITH NO OIL CONSUMPTION.Jun 18, 2002 · Saab SF340A · Engine (Turbine/Turboprop)SDR MALA020356Computer · failedDURING FLIGHT 2767, ALTITUDE AND HEADING RED FLAGGED ON F/O'S SIDE. USED X-SIDE DATA AS PER QRH. AIR RETURN TO SUX. MAINTENANCE INSPECTED AC AND FOUND SAFE FOR ONE TIME FERRY FLIGHT FROM SUX TO MSP FOR INTERMITTANT F/O'S AHARS. MSP MAINTENANCE REMOVED AND Jun 18, 2002 · N115XJ · Saab SF340A · Integrated Flight SystemSDR REX2002F00006Squib · damagedWHILE INVESTIGATING REASON FOR CARGO SMOKE WARNING IT WAS FOUND THAT THE CARGO FIRE EXTINGUISHER BOTTLE WAS NOT FIRED. CREW REPORTED THAT THE BOTTLE WAS FIRED IAW EMERGENCY PROCEDURES. THE CARGO BOTTLE SQUIB WAS FOUND TO HAVE BENT ELECTRICAL PINS. SQUIB WASJun 13, 2002 · N407BH · Saab SF340A · Extinguishing SystemSDR MALA020341Seat Track · corrodedDURING 4Y/2Y-CHECK IN CWA, RH GALLEY SEAT TRACK HAS CORROSION. MAINTENANCE INSTALLED A NEW RH GALLEY SEAT TRACK PN 7253721-459. REF: 409 #140299 FOR DETAILS.Jun 10, 2002 · N114XJ · Saab SF340A · Fuselage Miscellaneous StructureSDR UHL2002F00002Hose · chafedAFTER DEPARTURE, UPON SELECTING GEAR UP HYDRAULIC WARNING LIGHT ILLUMINATED WITH ASSOCIATED (2620) PRESSURE READING ON GAUGE LANDING GEAR EXTENDED RETRUNED TO FIELD, MAINTENANCE INSPECTED, FOUND NOSE RETRACT CYLINDER HOSE CHAFFED THROUGH. REPLACED HOSE, SERVIJun 10, 2002 · N340SZ · Saab SF340A · Landing Gear Retraction/Extension SystemSDR MALA020340Angle · corrodedDURING 4Y/2Y-CHECK IN CWA, RT SIDE OF FRAME STA 272 TOP ANGLE AND FRAME TOP HAVE CORROSION. MAINTENANCE REMOVED CORROSION IAW 51-70-40, INSTALLED NEW ANGLE IAW SRM 51-20.Jun 9, 2002 · N114XJ · Saab SF340A · Fuselage Miscellaneous StructureSDR MALA020339Frame · corrodedDURING 4Y/2Y-CHECK IN CWA, FOUND FRAME TOP CORRODED AT STA 272. MAINTENANCE COMPLETED REPAIR IAW EO S53102.Jun 9, 2002 · N114XJ · Saab SF340A · Fuselage Main, FrameSDR MALA020338Frame · corrodedDURING 4Y/2Y-CHECK IN CWA, WEB TOP OF FRAMES 294 & 288 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.Jun 7, 2002 · N114XJ · Saab SF340A · Fuselage Main, FrameSDR MALA020337Seat Track · corrodedDURING 4Y/2Y-CHECK IN CWA, RT GALLEY SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED GALLEY TRACK.Jun 7, 2002 · N114XJ · Saab SF340A · Fuselage, Seat/Cargo Attach FittingsSDR MALA020336Seat Track · corrodedDURING 4Y/2Y-CHECK IN CWA, RT I/B GALLEY SEAT TRACK TOP AND PROFILE HAVE CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40 ON PROFILE.Jun 7, 2002 · N114XJ · Saab SF340A · Fuselage, Seat/Cargo Attach FittingsSDR MALA020314Wire · brokenDURING CONTINUITY CHECK OF SEPARATION BOLTS CIRCUITY, FOUND CANNON PLUG AT THE LT SEPARATION BOLT BAD AND WIRE BROKE. MAINTENANCE REMOVED AND REPLACED CANNON PLUG AT THE LT SEPARATION BOLT IAW SAAB WM20-30-00, REPAIRED BROKEN WIRE IAW SAAB WM20-20-01. OPS CHJun 2, 2002 · N31XJ · Saab SF340A · Landing Gear System WiringSDR MALA020309Switch · failedDURING FLIGHT 2824, HYDRAULIC SYSTEM WARNING INBOUND TO MSP. CREW PERFORMED EMERGENCY GEAR EXTENSION AND USED HYDRAULIC PUMP IN OVERRIDE TO GET RT MLG DOWN AND LOCKED. FROM LOG PAGE 1078212, HYDRAULIC CAUTION LIGHT ON INFLIGHT, PUMP INOP IN AUTO. EMERGENCY May 31, 2002 · N46XJ · Saab SF340A · Hydraulic System, MainSDR 000147Warning System · malfunctionedRT ENGINE O/T ON TAKEOFF, LT ALPHA VANE LIGHT. CHECKED ALL L/P AND H/P BLEED LINES, PRESSURE TESTED AND FOUND NO LEAKS. RAN ENGINE TO 108 PERCENT TORQUE. ALL PARAMETERS INCLUDING TEMP WITHIN LIMITS.May 29, 2002 · N104 · Saab SF340A · Engine Temperature Indicating SystemSDR 000146Audio Panel · faultyCREW REPORTED FEEDBACK IN AUDIO PANELS. REMOVED AND REPLACED RT & LT AUDIO PANEL AND OPS CHECK GOOD WITH CHAUTAUQUA HEAD SET A ND STATIC WICK.May 29, 2002 · N152 · Saab SF340A · HF Communications SystemSDR MALA020301Connector · dirtyLT TORQUE MOTOR LOCKOUT INOP. WOULD NOT COME OUT OF START FEATHER PROP RPM NEVER OVER 800 AND WOULD NOT GO INTO BOTTOM GOVERNOR. MAINTENANCE CLEANED CANNON PLUG ON OVERSPEED GOVERNOR. PERFORMED SEVERAL STARTS ON LT MOTOR. OPS CHECK GOOD.May 29, 2002 · N119XJ · Saab SF340A · Propeller GovernorSDR MALA020300Wire · looseFLIGHT IDLE OVERRIDE PULLED ON LANDING ROLL. F1 FAILED TO OPEN. MAINTENANCE FOUND SPLICE 306VS-DF HAD A WIRE PULLED AND LOOSE. REPAIRED SPLICE PER SF340W/M CHAP 20. OPS CHECK F1 STOP SYSTEM. ALL CHECKS GOOD IAW SF-340 MM CHAP 76/10.May 28, 2002 · N991XJ · Saab SF340A · Engine Control System WiringSDR MALA020298Servo · failedDURING FLIGHT AT CRUISE, AUTO PILOT YAW DAMPER INOP. AP DISENGAGED AND CAN NOT BE REENGAGED. MAINTENANCE REMOVED AND REPLACED RUDDER SERVO IAW AMM 22-10-21-4. OPS CHECKS GOOD.May 26, 2002 · N109XJ · Saab SF340A · Autopilot Main ServoSDR MALA020305Connector · faultyDURING CONTINUITY CHECK/FUNCTION CHECK, OF SEPARATION BOLTS AND EMERGENCY EXTENSION OF MLG AND NLG FOUND BAD CONNECTORS AT BOTH LT & RT SEPARATION BOLTS. MAINTENANCE REMOVED AND REPLACED BOTH LT & RT CONNECTORS.May 25, 2002 · N68XJ · Saab SF340A · Landing Gear Retraction/Extension SystemSDR MALA020296Warning System · false activationDURING FLIGHT 2797 LT BLEED AIR LEAK LIGHT ILLUMINATED DURING TAXI. CREW RAN QRH REMAINED ON UNTIL ENGINE SHUTDOWN. A/C RETURNED TO GATE. MAINTENANCE TROUBLESHOT, INSPECTED BLEED LEAK DETECTION LOOP, INSPECTED FOR LEAKS OR CHAFES, RAN FOR 15 MINUTES, CHECKIMay 23, 2002 · N89XJ · Saab SF340A · Pneumatic Indicating SystemSDR REX2002F00009Tube · crackedJUST AFTER ATTAINING V1 SPEED DURING TAKEOFF, THE LEFT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. THE CLIMB OUT CONTINUED TO SIX THOUSAND FEET AND THE FLIGHT CREW DETERMINED THAT WAS NOT AN INDICATION PROBLEM. THE FLIGHT CREW DECLARED AN EMERGENCY AND PERFMay 17, 2002 · N111PX · Saab SF340A · Engine Oil Distribution (Airframe Furnished)SDR AUS20020437Frame · cracked(AUS) LT ENGINE NACELLE FRAME (FIGURE 8 FRAME) CRACKED. CRACK LENGTH IS AT LEAST 100MM (4IN) LONG. SUSPECT AREA HAD BEEN SUBJECTED TO HIGH TEMPERATURES AND DISTORTION AT SOME STAGE.May 10, 2002 · Saab SF340A · Nacelle/Pylon, Frame/Spar/RibSDR UHL2002F00001Engine · failedAFTER TAKE OFF, SURGED BETWEEN 40 PERCENT TO 70 PERCENT, HAPPENED 3 TIMES. PILOT DECLARED EMERGENCY RETURNED TO AIRPORT. MECHANIC CHECKED BIRDCATCHER AND INLETS FOR DAMAGE. PERFORMED OPS CHECK ON GROUND AND COULD NOT DUPICATE. TOOK A GPA READING AND READINMay 9, 2002 · N158SD · Saab SF340A · Engine (Turbine/Turboprop)SDR MALA020271Fire Loop · faultyDURING FLIGHT 2801, LEFT BLEED AIR LEAK LIGHT ILLUMINATED INFLIGHT FOLLOWED QRH AFTER BLEEDS CLOSED 10 MINUTES LIGHT EXTINGUISHED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED FIRE WIRE IAW 36-23-10-2 AND PERI SEALS ON LT FLAP COVE, OPS CHECK AND LEAKMay 8, 2002 · N991XJ · Saab SF340A · Fire DetectionSDR MALA020268Actuator · out of adjustDURING FLIGHT FLAPS WERE DROOPING 2-3 DEGREES, THEN POPPING BACK UP, CAUSING PITCH OSCILLATIONS. AIR RETURN TO MSP. MAINTENANCE ADJUSTED FLAP ACTUATOR, LEFT AND RIGHT FLAP INTERCONNECT PUSHRODS AND FLAP POTS IAW AMM 27-51-00. PERFORMED FLAP FUNCTIONAL TEST,May 6, 2002 · N142XJ · Saab SF340A · Trailing Edge Flap ActuatorSDR 000999Computer · malfunctionedBOTH CAPTAINS DISPLAYS WENT BLANK. MX REMOVED AND REPLACED DPU.May 6, 2002 · N35 · Saab SF340A · Central DisplaySDR MALA020284Smoke Detector · malfunctionedCARGO SMOKE LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED CARGO SMOKE DETECTOR PN CGAB1201-01, SN/ON 755, SN/OFF 92 AMM 26-13-15-4. ALL CHECKS GOOD.May 5, 2002 · N89XJ · Saab SF340A · Smoke Detection
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