Saab SF340A

Service difficulty reports · 2,633

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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 MALA020686GcuDURING FLIGHT #3367, RH AC GEN FELL OFF LINE, CREW RESET THEN IT FELL OFF LINE SHORTLY AFTER. AIR RETURN TO MSP. MAINTENANCE CND, SWAPPED AC GCU'S SIDE TO SIDE PN 51634-002, SN/ON RH SIDE, 97005, SN/ON LH SIDE 96036. OPS CHECK GOOD. IAW SAAB AMM 24/21/10. INDec 16, 2002 · N27XJ · Saab SF340A · AC Generation SystemSDR 0212151Pin · bindingUPON LANDING GEAR EXTENSION CREW NOTED THAT THE NOSE GEAR WOULD NOT INDICATE DOWN AND LOCKED, WITH A LANDING GEAR CAUTION LIGHT ILLUMINATED. CREW RECYCLED GEAR AND GOT THE SAME EFFECT. CREW TRIED TO HAND PUMP GEAR DOWN FOR UP TO 20 MINUTES WITH NO EFFECT. CRDec 15, 2002 · N104CQ · Saab SF340A · Landing Gear Retraction/Extension SystemSDR 0212141Generator · failedRIGHT AC GENERATOR AND RIGHT INTAKE LIGHTS ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO FIELD. AFTER TROUBLESHOOTING THE AC SYSTEM, MECHANIC REMOVED AND REPLACED THE RIGHT AC GENERATOR. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.Dec 14, 2002 · N340SZ · Saab SF340A · AC Generation SystemSDR 0212133Display · faultyIN HGR BOTH EFIS AND MFD BLANKS OUT ON AND OFF CAPTAINS SIDE. THE SYSTEM WAS MEL. THE SYSTEM WAS OPERATIONAL IN DRIVE TRANSFER IAW THE MEL REQUIREMENTS. AWAITING TEARDOWN REPORT FOR CLOSER.Dec 13, 2002 · N108CQ · Saab SF340A · Flight Management Computing Hardware SystemSDR 0212131Connector · contaminatedPILOT REPORTED, OBSERVED THE LEFT TAILPIPE HOT LIGHT ILLUMINATED SHORTLY AFTER TAKE-OFF. PILOT SHUT DOWN THE LEFT ENGINE DECLARING AN EMERGENCY, AND RETURNED TO FIELD. CLEANED MOISTURE FROM LEFT TAILPIPE SENSOR CONNECTIONS AND RESEALED. PERFORMED GROUND RUDec 13, 2002 · N123XS · Saab SF340A · Overheat DetectionSDR MALA020685Generator · failedDURING FLIGHT 3155, RT AC GEN CAUTION LIGHT ON, QRH COMPLETED. AIR RETURN TO MSP. MAINTENANCE REPLACED RT AC GENERATOR IAW MM. ALL CHECKS GOOD OF AC GEN SYSTEM IAW MM.Dec 12, 2002 · N366XJ · Saab SF340A · AC Generator-AlternatorSDR MALA020684Battery PackEMERGENCY LIGHT AT 41LN, 42LN, 43LN, 3LN,4LN, 49LN, 50LN WOULD NOT COME ON. MAINTENANCE FOUND POWER SUPPLY/BATTERY PACK 24LN TO BE AT FAULT. NO OTHER INFORMATION AT THIS TIME.Dec 12, 2002 · N31XJ · Saab SF340A · Emergency LightingSDR 0212132Wire · shortedDURING TAKEOFF ROLL PILOT OBSEVRED THE LEFT TAILPIPE HOT LIGHT ILLUMINATED. PILOT ABORTED TAKEOFF AND RETURNED TO GATE. SENDING MECHANIC TO TROUBLESHOOT SYSTEM. MECHANIC ARRIVED, FOUND SHORT TO GROUND, REPAIRED WIRE IAW SF340 WM 20-20-00. PERFORMED GROUND RUDec 12, 2002 · N123XS · Saab SF340A · Overheat DetectionSDR 0212113Connector · corrodedRIGHT AFTER TAKEOFF, PILOT RECIEVED LEFT TAILPIPE HOT INDICATION. PILOT RETARDED POWER AND LEFT TAILPIPE HOT LIGHT EXTINGUISHED. PILOT RETURNED TO FIELD. MECHANIC FOUND CORROSION ON OUTBOARD TAILPIPE HEAT SENSOR CONNECTOR, REMOVED CORROSION. PERFORMED GROUDec 11, 2002 · N340SZ · Saab SF340A · Overheat DetectionSDR 0212111Engine · malfunctionedON TAKEOFF ROLL, EXPERIENCED A LOSS OF TORQUE INDICATION ON THE RIGHT POWERPLANT. AIRCRAFT ABORTED TAKEOFF AND WAS TOLD TO RETURN TO THE GATE BY MOC, MECHANIC WAS NOTIFIED TO MEET AIRCRAFT AT THE GATE.Dec 11, 2002 · N121CQ · Saab SF340A · Engine (Turbine/Turboprop)SDR UHLA10081Warning Light · illuminatedDURING TAKEOFF ROLL, PILOT REPORTED AT 60 KNOTS THE AUTOCOURSEN LIGHT ON CWP ILLUMINATED. ABORTED AND RETURNED TO GATE.Dec 5, 2002 · N123XS · Saab SF340A · Propeller Controlling SystemSDR CA021230004Fan · seized(CAN) AFTER ARRIVAL AND DURING UNLOADING OF THE PASSENGERS THE FLIGHT ATTENDANT NOTED AN ABNORMAL SMELL IN THE CABIN AND ALERTED THE FLIGHT CREW. THEY TOO NOTED THE ELECTRICAL TYPE SMELL AND ATTEMPTED TO DETERMINE THE SOURCE. THE RECIRCULATING FANS LOCATED UNDDec 3, 2002 · Saab SF340A · Air Distribution FanSDR AUS20021384Indicator · failed(AUS) MAIN HYDRAULIC SYSTEM PRESSURE INDICATOR FAILED.Dec 3, 2002 · Saab SF340A · Hydraulic Pressure IndicatorSDR UHL2002F00010Pushrod · dirtyDURING FLIGHT, PILOT CALLED, REPORTED THAT RIGHT MAIN GEAR DOOR EXTENDED IN FLIGHT . ADVISED PILOT TO REDUC AIRSPEED TO PREVENT DAMAGE TO DOOR UPON LANDING . MAINTENANCE WAS DISPATCHED TO REPAIR AND INSPECT DOOR FOR OVERSPEED DAMAGE IAW MM. CLEANED TELESCODec 2, 2002 · N152CQ · Saab SF340A · Landing Gear Door Retract SectionSDR 2003FA0000083Motor · failedFAN RETURNED TO MFG FOR OVERHAUL. WHEN FAN WAS TESTED, IT FAILED THE MINIMUM RPM REQUIREMENTS, WHEN IT WAS DISASSEMBLED, IT WAS DISCOVERED THAT THIS OVERHAULED UNIT HAS NOT BEEN OVERHAULED IAW THE MM. THE ARMATURE IS NOT OF DAE DESIGN. OVERHAUL MANUAL DOES Dec 1, 2002 · Saab SF340A · Air Distribution FanSDR UHLA100771Pressure Switch · failedPILOT REPORTS AUTOCOARSEN SYSTEM FAILED ON TAKEOFF ROLL AIRCRAFT RETURNED TO GATE. MECHANIC PERFORMED GROUND RUN AUTOCOARSEN SYSTEM ADJUSTMENT/TEST IAW MM. OPS CHECKED GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.Dec 1, 2002 · N123XS · Saab SF340A · Propeller Controlling SystemSDR UHL2002F00009Pressure Switch · inoperativePILOT REPORTS AUTOCOARSEN SYSTEM FAILED ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE. MECHANIC PERFORMED GROUND RUN ON AUTOCOARSEN SYSTEM ADJUSTMENT & TEST IAW MM. OPS CHECKED GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.Dec 1, 2002 · N123XS · Saab SF340A · Propeller Controlling SystemSDR 0212112Connector · contaminatedAIRCRAFT WAS ON TAKE-OFF ROLL AT 110 KNOTS WHEN THE PILOT OBSERVED THE RIGHT TAILPIPE HOT LIGHT WAS ILLUMINATED. PILOT ABORTED TAKE-OFF AND RETURNED TO GATE. MAINTENANCE FOUND MOISTURE IN THE RIGHT OUTBOARD TAILPIPE HEAT SENSOR CONNECTOR. MECHANIC DRIED CONNDec 1, 2002 · N152CQ · Saab SF340A · Overheat DetectionSDR UHL2002F00008Circuit Breaker · trippedON TAXI OUT, PILOT REPORTED NLG STEERING CIRCUIT BREAKER POPPED. AIRCRAFT RETURNED TO GATE.Nov 27, 2002 · N101CN · Saab SF340A · Landing Gear Steering SystemSDR 2003F00134Indicator · malfunctionedFLT 4480 - PIT-TOL - AIRCRAFT RETURNED TO GATE, CO-PILOTS AHARS FLAGGED / EADI 25 DEGREES PITCH DOWN AND 10 DEGREES LEFT, EHSI COMPASS SLEWS CLOCKWISE, NORMAL AFTER 30 MINUTES. SECOND OF 2 SQUAWKS FOR THIS FLIGHT. (M)Nov 25, 2002 · N118SD · Saab SF340A · Integrated Flight SystemSDR 2003F00133Pump · intermittentFLT 4480 - PIT-TOL, ON TAXI OUT, AIRCRAFT RETURNED TO GATE, HYDRAULIC PUMP INTERMITTENT IN AUTO AND OVERRIDE. FIRST OF TWO SQUAWKS THIS FLIGHT. (M)Nov 25, 2002 · N118SD · Saab SF340A · Hydraulic Pump (Electric/Engine), MainSDR MALA020663Engine · malfunctionedWHEN STARTING, RT ENGINE LIGHT-OFF TOOK LONGER THAN NORMAL BUT WAS WITHIN LIMITS. AFTER LIGHT-OFF ITT STABILIZED AT 775 AND NG AT 65. IT NEVER SEEMED TO FULLY START UPON SHUTDOWN, SMOKE CAME OUT INTAKE. MAINTENANCE RAN ENGINE TO CLEAR RESIDUAL FUEL OUT OF CONov 22, 2002 · N991XJ · Saab SF340A · Engine (Turbine/Turboprop)SDR 2003F00135Indicator · malfunctionedFLT 4468 - AIRTURN BACK AND RETURNED TO TTN - PILOT REPORTED HEADING MISMATCH BETWEEN CA AND FO 80-180 DEGREES FLAGGED IN FLIGHT HEADINGS MOMENTARILY LOCKED AND THEN FLAGGED AGAIN AND REMAINED SPLIT. (M)Nov 21, 2002 · N340SZ · Saab SF340A · Integrated Flight SystemSDR 2003F00132Controller · malfunctionedFLT 4472 - CLE-PIT - ABORTED TAKEOFF DUE TO AUTOCOARSEN WOULD NOT ARM DURING TAKEOFF ROLL. TORQUE WAS 90 PERCENT, AIRSPEED BETWEEN 90 AND 100 KNTS AND SWITCH IN THE ON POSITION. CONTRACT MAINTENANCE AND THE FLIGHT CREW PERFORMED THE P3 AND AUTOCOARSEN TEST, Nov 18, 2002 · N19XS · Saab SF340A · Propeller Controlling SystemSDR 2003F00063Anti-Ice Valve · malfunctionedFLT 4511 - PIT-CLE - DID AN AIRTURNBACK TO PIT DUE TO RIGHT ENGINE ANTI-ICE VALVE CAUTION LIGHT CYCLES ON AND OFF IN ONE MINUTE INTERVALS. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE VALVE ON THE RIGHT ENGINE. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 16, 2002 · N157SD · Saab SF340A · Engine Anti-Icing SystemSDR 2003F00066Door · obstructedFLT 4480 - DURING TAXI, PIT TO TOL, THE CARGO DOOR WARNING LIGHT CAME ON THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED THE CARGO DOOR PULL DOWN ROPE FROM UNDER THE DOOR. THE CARGO DOOR WARNING SYSTEM CHECKED GOOD, THE AIRCRAFT WAS RELEASED FOR SERVINov 14, 2002 · N43SZ · Saab SF340A · Cargo/Baggage DoorsSDR 2003F00065Weu · malfunctionedFLT 4471 - TTN-BED, ABORTED TAKEOFF, DUE TO A CONFIGURATION WARNING AND WHITE BITE LIGHT. MAINTENANCE REMOVED AND REPLACED THE WEU. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 14, 2002 · N121CQ · Saab SF340A · Central WarningSDR UHL2002F00006Indicator · erraticNR 2 TORQUE GAUGE ERRATIC ON TAKEOFF ROLL WHEN SET GAUGE WENT 100 PERCENT TO 120 PERCENT TORQUE AT 50-60 KNOTS. NO ENGINE POWER PROBLEMS NOTED. ABORTED TAKEOFF.Nov 12, 2002 · N138SD · Saab SF340A · Engine BMEP/Torque IndicatingSDR MALA020651Propeller · malfunctionedDURING CLIMBOUT OF FLIGHT 2907, RT ENGINE SURGED DURING CLIMB. TORQUE WENT TO 120 PERCENT FOR 10 SECONDS, TEMP WENT TO 968 DEGREES FOR 10 SECONDS. PROP RPM REMAINED STABLE. CTOT WAS OFF, AUTO COARSEN OFF, AUTO PILOT ON. PILOT WENT TO TORQUE MOTOR LOCK OUT PENov 12, 2002 · N89XJ · Saab SF340A · Propeller AssemblySDR 2003F00068Pump · failedFLT 4504 - IN CRUISE, THE MAIN HYDRAULIC PUMP FAILED. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO PIT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC PUMP. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 11, 2002 · N101CN · Saab SF340A · Hydraulic Pump (Electric/Engine), MainSDR 2003F00070Engine · power lossON TAKEOFF, TORQUE LAGGED POWER LEVER ADVANCEMENT, OBTAINED ONLY 80 PERCENT TORQUE ON BOTH ENGINES. ENGINE ANTI-ICE ON. ABORTED TAKEOFF IN PIT. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED A GROUND RUN UP. NO DISCREPANCIES NOTED. THE A/C WAS RETURNED TONov 6, 2002 · N149SZ · Saab SF340A · Engine (Turbine/Turboprop)SDR 2003F00069Engine · power lossON TAKEOFF, TORQUE LAGGED POWER LEVER ADVANCEMENT, OBTAINED ONLY 80 PERCENT TORQUE ON BOTH ENGINES. ENGINE ANTI-ICE ON. ABORTED TAKEOFF IN PIT. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED A GROUND RUN UP. NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNNov 6, 2002 · N149SZ · Saab SF340A · Engine (Turbine/Turboprop)SDR 2003F00080Smoke · detectedON CLIMB-OUT, AT IPT, GROUND PERSONNEL REPORTED AN ORANGE GLOW WITH PUFFS OF SMOKE COMING FROM THE LEFT ENGINE. ALL COCKPIT INDICATIONS WERE NORMAL. THE AC RETURNED TO IPT. MAINTENANCE INSPECTED THE LEFT ENGINE, PERFORMED A GROUND RUN. NO DISCREPANCIES NOTNov 5, 2002 · N123XS · Saab SF340A · Engine (Turbine/Turboprop)SDR MALA020630Brake · malfunctionedDURING POSTFLIGHT OF FLIGHT NR 3146, ALL FOUR MAIN TIRES FOUND FLAT ON POSTFLIGHT. MAINTENANCE REPORTED FUSE PLUGS BLOWN, BRAKES RED HOT AND GLOWING. MAINTENANCE COMPLETED INSPECTION IAW, AMM CHAP. 5-50-00. REPLACED ALL 4 WHEELS AND BRAKES IAW JC 3240-301 ANov 2, 2002 · N106XJ · Saab SF340A · Landing Gear Brake SystemSDR 2003F00081Strut · lowON CLIMB-OUT FROM FWA, COULD NOT RETRACT LANDING GEAR WITHOUT DEPRESSING DOWN LOCK RELEASE. UPON BRINGING CONDITION LEVERS BACK IN CLIMB, CONFIG WARNING HORN SOUNDED. AFTER GEAR RETRACTION, OAT WARNING LIGHT ILLUMINATED. FLIGHT 4505 RETURNED TO FWA, MAINTENAOct 31, 2002 · N118SD · Saab SF340A · Main Landing Gear Strut/Axle/TruckSDR MALA020627Boot · failedDURING TAXI OF FLIGHT NR 3294, LEFT PROP DEICE LIGHT ILLUMINATED DURING TAXI. DEICE BOOT ON ONE OF THE PROP'S WAS BAD. MAINTENANCE REMOVED AND REPLACED LEFT PROP ASSEMBLY IAW 340 JOB CARD 6110-303, ALL CHECKS GOOD.Oct 27, 2002 · N142XJ · Saab SF340A · Propeller Deice Boot SectionSDR 2003F00129Pdu · malfunctionedDURING APPROACH TO JST, PILOT REPORTED LOSS OF RIGHT ESS BUSS, RIGHT MAIN BUSS RESULTING IN LOSS OF FIRST OFFICERS EFFIS TUBE, PILOT ABORTED LANDING AND RETURNED TO PIT. MAINTENANCE REPLACED RIGHT PDU, NO FURTHER PROBLEMS, A/C RETURNED TO SERVICE.Oct 26, 2002 · N101CN · Saab SF340A · AC Power Distribution SystemSDR UHL2002F00007Pdu · inoperativeDURING APPROACH, PILOT REPORTED LOSS OF RT EFIS BUSS, RT MAIN BUSS RESULTING IN LOSS OF FIRST OFFICERS EFIS TUBE, PILOT ABORTED LANDING AND RETURNED. MAINTENANCE REPLACED RT PDU, NO FURTHER PROBLEMS, A/C RETURNED TO SERVICE.Oct 26, 2002 · N101CN · Saab SF340A · AC Power Distribution SystemSDR UHL2002F00005Control Valve · wornUPON LANDING, PILOT REPORTED BRAKES FELT WEAK ON STARBOARD SIDE. FELT OK, AIRCRAFT INSPECTED AIRCRAFT AND FERRIED FOR FURTHER INVESTIGATION. REMOVED AND REPLACED BRAKE CONTROL VALVE AND FURTHER PROBLEMS NOTED.Oct 24, 2002 · N360SZ · Saab SF340A · Master Cylinder/Brake ValveSDR 2003F00130Engine · malfunctionedFLT 4512, DURING CRUISE, ITT SPIKE ON RT ENGINE FROM 800 DEGREES TO 855 DEGREES FOR ONE MINUTE AT 88 PERCENT TORQUE, REDUCED TORQUE TO 83 PERCENT, ITT FLUX 766 DEGREES TO 826 DEGREES THEN STABILIZED AT 766 DEGREES, LT ENGINE AT 750 DEGREES, RETURNED TO BNA. POct 23, 2002 · N152CQ · Saab SF340A · Engine (Turbine/Turboprop)SDR MALA020616Ctot PanelDURING CLIMBOUT OF MSP ON FLIGHT #3038, RH ENGINE SURGED TO 108% AND ITT AT 955 WHILE CLIMBING THROUGH 11,700 MDL. A/C YAWED SEVERELY. CREW WAS NOT IN ICING CONDITIONS. FOLLOWED QRH AND LOCKED OUT TO MGR. NO FURTHER FAULTS NOTED. TEMP AND TORQUE FLUCTUATIONOct 23, 2002 · N89XJ · Saab SF340A · Engine ControlsSDR MALA020617Switch · malfunctionedON PUSHBACK OF FLIGHT NR 2751, PUFF OF SMOKE OUT OF FA'S CONTROL PANEL AND SMELL OF ELECTRICAL BURNING. AC RETURNED TO GATE. MAINTENANCE REPLACED FA'S PANEL DIMMER SWITCH. ALL CHECKS GOOD IAW SF340-MM CHAP 33.Oct 23, 2002 · N27XJ · Saab SF340A · Passenger Compartment LightingSDR CA021023005Fan · failed(CAN) THE AIRCRAFT LANDED AND WAS IN THE PROCESS OF UNLOADING WHEN THE FLIGHT ATTENDANT NOTED AN ELECTRICAL ODOR IN THE CABIN. THE REMAINING PASSENGERS EXITED THE AIRCRAFT AS INSTRUCTED AND THE PILOTS ALERTED TO A POSSIBLE PROBLEM. AT ABOUT THE SAME TIME AFTEOct 21, 2002 · Saab SF340A · Air Distribution FanSDR MALA020613Connector · brokenDURING LC1 INSPECTION, RT EXPLOSIVE BOLT CANNON PLUG BROKE IN HALF. MAINTENANCE REMOVED AND REPLACED RT EXPLOSIVE BOLT CANNON PLUG IAW SAAB WM 20-30-15. OPS CHECK GOOD.Oct 20, 2002 · N106XJ · Saab SF340A · Landing Gear Retraction/Extension SystemSDR MALA020612Connector · brokenDURING LC1 INSPECTION, LEFT EXPLOSIVE BOLT CANNON PLUG BROKE. MAINTENANCE REPLACED LEFT EXPLOSIVE BOLT CANNON PLUG IAW SAAB 340 WM 20/30-15.Oct 20, 2002 · N106XJ · Saab SF340A · Landing Gear Retraction/Extension SystemSDR MALA020611Battery PackDURING LC1, EMERGENCY LIGHTS 41LN, 42LN, 43LN, 4LN, AND 3LN WOULD NOT TURN ON. MAINTENANCE REPLACED 24LN, EMERGENCY BATTERY PACK pn 610478-9 SN/OFF 1948, SN/ON ELB018 IAW TASK CARD 335002 AND OPS CHECKED GOOD.Oct 20, 2002 · N106XJ · Saab SF340A · Emergency LightingSDR REX2002F00011Spring · brokenUPON GEAR EXTENSION RIGHT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED. EMERGENCY DECLARED, GEAR WAS CYCLED SEVERAL TIMES AND DOWN AND LOCK INDICATION WAS CONFIRMED. LANDING WAS UNEVENTFUL. UPON INVESTIGATION, FOUND DOWN LOCK ASSIST SPRING BROKEN AND INTEOct 17, 2002 · N401BH · Saab SF340A · Landing Gear Retraction/Extension SystemSDR 2003F00131Wheel · wornFLT 4522 - UPON LANDING AT PIT, PILOT REPORTED SEVERE NOSE WHEEL SHIMMY AT 40 KNTS UNTIL 20 KNTS. A/C FERRIED TO FWA MX BASE FOR TROUBLESHOOTING. AT FWA BOTH NOSE WHEELS CHANGED, NO FURTHER DEFECTS NOTED. A/C RETURNED TO SERVICE. (M)Oct 16, 2002 · N35SZ · Saab SF340A · Wheel/Ski/FloatSDR MALA020601Hydraulic Line · rupturedDURING FLIGHT NR 2782, MAIN HYDRAULIC QUANTITY AND PRESSURE INDICATED ZERO INFLIGHT. MAINTENANCE FOUND A RUPTURED HYDRAULIC LINE ON POST FLIGHT INSPECTION. REPLACED LEFT GEAR DOWN HYDRAULIC FLEX LINE AND SEPARATION BOLTS.Oct 10, 2002 · N46XJ · Saab SF340A · Hydraulic System, MainSDR MALA020603Spar · crackedRT FLAP REAR SPAR IS CRACKED AT STA 142, FLAP.Oct 6, 2002 · N27XJ · Saab SF340A · Trailing Edge Flaps
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