# Service difficulty reports: Saab SF340A

A list on [Saab SF340A](https://openairdocs.org/model/saab-sf340a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 53 · 2,633 reports

- [SDR UATA2026032602701](https://openairdocs.org/sdr/UATA2026032602701.md): Rivet · sheared · Mar 25, 2026 · N906RA · Saab SF340A · Ailerons
  > FLIGHT CONTROL STUCK FULL LEFT AILERON. REPLACED SHEARED RIVETS FROM AILERON TO AILERON POSITION INDICATING HORN USING MS20470AD RIVETS WITH REFERENCE TO SAAB 340 MM SRM 51-40-21-001 AND 40-30-001B.
- [SDR 2026F00027](https://openairdocs.org/sdr/2026F00027.md): Swivel Fitting · broken · Mar 11, 2026 · N631BC · Saab SF340A · Hydraulic System, Main
  > HYDRAULIC CWP LIGHT ILLUMINATED AFTER TAKEOFF. HYDRAULIC QUANTITY APPEARED TO INDICATE BELOW RED LINE, AND MAIN HYDRAULIC PRESSURE APPEARED TO BE INDICATING 0. COMPLIED WITH QRH. DIVERTED BACK TO KMIA. THE SWIVEL IS LOCATED ON THE RH MLG DRAG BRACE AND PORTS H
- [SDR OZCA2025002641](https://openairdocs.org/sdr/OZCA2025002641.md): Downlock Switch · loose · May 31, 2025 · N641BC · Saab SF340A · Landing Gear Position and Warning
  > ON APPROACH INTO SNU, THE CREW SELECTED THE LANDING GEAR DOWN AND FAILED TO GET A DOWN AND LOCKED INDICATION ON THE LH MLG. THE CREW NOTIFIED THE TOWER AND ABORTED THE LANDING. A FLYBY PAST THE TOWER CONFORMED ALL 3 GEAR DOWN AND LOCKED. THE AIRCRAFT RETURNED
- [SDR OZCA2024091706641](https://openairdocs.org/sdr/OZCA2024091706641.md): Engine · erratic · Sep 16, 2024 · N641BC · Saab SF340A · Engine (Turbine/Turboprop)
  > TAKING OFF FROM RUNWAY 06 IN FREEPORT, CLIMB OUT TO 1000 FT, CREW STARTED THE CLIMB CHECKLIST. UPON TURNING OFF CTOT AND SETTING CONDITION LEVERS TO CLIMB, THE RIGHT ENGINE LOST POWER AND THE OVER TEMPERATURE LIGHT ILLUMINATED. CREW PERFORMED MEMORY ITEMS,AND
- [SDR OZCA2024004641](https://openairdocs.org/sdr/OZCA2024004641.md): Engine · overtemp · Aug 12, 2024 · N641BC · Saab SF340A · Engine (Turbine/Turboprop)
  > DURING DESCENT, SEVERAL LOUD BANGS WERE HEARD FROM THE RH ENGINE WITH VIBRATIONS. MAJOR FLUCTUATIONS ON THE TORQUE AND ITT. OVERTEMP LIGHT CAME ON FOR APPROX. 5 SECONDS. TORQUE SET AT 40% THEN REDUCED TO 20%. ENGINE STABILIZED AROUND 30% TORQUE. AIRCRAFT DECLA
- [SDR OZCA20240219001](https://openairdocs.org/sdr/OZCA20240219001.md): Bleed Air Sys · loose · Feb 16, 2024 · N641BC · Saab SF340A · Engine Bleed Air System
  > AT FL240 RIGHT TQ AND RIGHT PROP RPM GAUGES AT ZERO. UNABLE TO MAINTAIN AIRSPEED. RIGHT ENGINE BECAME ROUGH, FUEL FLOW DECREASED. GAUGES THEN RETURNED TO NORMAL WITH HIGH RIGHT ITT. TURNED R HP OFF, ENGINE STABILIZED. MAINTENANCE INSPECTED BLEED SYSTEM AND FOU
- [SDR OZCA340088230207](https://openairdocs.org/sdr/OZCA340088230207.md): Unknown · unknown · Feb 7, 2023 · N901BC · Saab SF340A · Hydraulic Power System
  > DURING CRUISE, HYD PUMP TURNED ON & NO MAIN ACCUM PRESS INCREASED. RETURNED TO MIA. FOLLOWED QRH. HYD CWP LIGHT ILLUM. R/R MAIN HYD RES. PERFORMED AIR BLEED SYS AT HYD SYS IAW 29-00-00 OPS & LEAK CHECK SAT. TAXI OUT, HYD PUMP MULTIPLE TIMES PER MINUTE: PRESS
- [SDR OZCA340076221212](https://openairdocs.org/sdr/OZCA340076221212.md): Trimmer · faulty · Dec 12, 2022 · N671BC · Saab SF340A · Engine EGT/TIT Indicating System
  > CROSSING 11,000 FT, RIGHT ENGINE ITT INCREASE UNCOMMANDED TO 872C (802C BEFORE INCREASE). PROCEEDED WITH QRH - REDUCING POWER POWER LEVERS BROUGHT TEMPERATURES BACK DOWN TO NORMAL LEVELS. BLEED VALVES HAD NO INFLUENCE ON ENGINE ITT. WHILE DESCENDING, ITT ON R
- [SDR OZCA340084221207](https://openairdocs.org/sdr/OZCA340084221207.md): Periseal · unserviceable · Dec 7, 2022 · N671BC · Saab SF340A · Cylinder Head Temperature (CHT) Indicating System
  > #2 ENGINE IN CRUISE, ITT OUT OF LIMITS. C/W QRH. - REMOVED AND REPLACED R/H SIDE UNDER WING FLAP PERI-SEAL IAW SF340A AMM 36-11-40-04. RUN CHECKS SATISFACTORILY.
- [SDR OZCA340076221103](https://openairdocs.org/sdr/OZCA340076221103.md): Chip Detector · activated · Nov 3, 2022 · N651BC · Saab SF340A · Engine Oil Indicating System
  > DURING CRUISE FLIGHT AT 17000 FT LEFT ENGINE CHIP DETECT LIGHT ILLUMINATED A8-15 QRH. NO OTHER ABNORMALITIES. -- REMOVED AND REPLACED LT HAND ENGINE CHIP DETECTOR I/AW GE-CT-5 AMM 79-30-35-04. RUN AND LEAKS CHECK SATISFACTORY
- [SDR OZCA340076220128](https://openairdocs.org/sdr/OZCA340076220128.md): Wire Harness · none · Jan 28, 2022 · N651BC · Saab SF340A · Turbine Engine System Wiring
  > WHILE INCRISING POWER LEVERS AT START OF T/O ROLL, L ENGINE TORQUE UNCOMANDED TO 120% ( RED LIGHT ON) REDUCED POWER LEVER, ENGINE DID NOT RESPOND. SHUT ENGINE DOWN. ASYMETRIC THRUST FROM RUNNING RIGHT ENGINE QUICKLY CAUSED PLANE TO ROTATE TO THE LEFT. RIGHT E
- [SDR OZCA06102DEC2021](https://openairdocs.org/sdr/OZCA06102DEC2021.md): Hmu · faulted · Dec 2, 2021 · N631BC · Saab SF340A · Engine (Turbine/Turboprop)
  > SUPPLEMENTAL - ON GO AROUND RWY 26R AT MIA ENG 1 OIL PRESS LT CAME ON, LOST POWER, MEMORY ITEMS, DECLARED EMERGENCY AND QRH COMPLY. - DURING T/S FOUND AT BOTTOMING GOVERNOR CONNECTED NP OVER SHOOTS 140 RPM NEED TO 1500 RPM AND RETURNED TO NORMAL READINGS. PRO
- [SDR OZCA340088211109](https://openairdocs.org/sdr/OZCA340088211109.md): Clamp · cracked · Nov 9, 2021 · N901BC · Saab SF340A · Engine Bleed Air System
  > DURING TO/O ROLL @ V1, PLANE DISPLAYED HIGH TEMP + LOW PROP OIL PRESSURE IN #2 ENG PROP RPM DROPPED, ENGINE SHUTDOWN. COMPLIED W/QRH, RETURNED TO LAND AT MYNN. ON INVESTIGATION FOUND THAT THE HP BLEED LINE V-BAND CLAMP FAILED P/N 12J63-125 AT THE RETAINER SEGM
- [SDR OZCA2021072600001](https://openairdocs.org/sdr/OZCA2021072600001.md): Downlock · disconnected · Jul 23, 2021 · N631BC · Saab SF340A · Main Landing Gear Attach Section
  > ON APPROACH TO LANDING RT MAIN GEAR LIGHT INOP. C/W QRH. - AFTER 2 ABORTED LANDINGS, LANDED SAFELY AND GEAR WAS DOWN AND LOCKED WITH NO INDICATION OF DOWN AND LOCKED. - FOUND RH DOWNLOCK SWITCH HAD BECOME DISCONNECTED. RECONNECTED/SECURED DOWNLOCK SWITCH IAW S
- [SDR OZCA90130MAR21](https://openairdocs.org/sdr/OZCA90130MAR21.md): Propeller · low pressure · Mar 30, 2021 · N901BC · Saab SF340A · Propeller Indication System
  > DURING CRUISE FLIGHT AT 13000, WE HAD PROP OIL PRESSURE LOW ON #1 ENGINE. PROCEEDED ACCORDING TO QRH PG E3-6
- [SDR UATA202101219076](https://openairdocs.org/sdr/UATA202101219076.md): Terminal Block · overheated · Jan 21, 2021 · N907RA · Saab SF340A · Windshield/Door Rain/Ice Removal
  > ON A RETURN FLIGHT, ON BASE LEG, DESCENDING BETWEEN 2600FT AND 1000FT, SMOKE WAS SMELLED, AND THEN OBSERVED BELOW THE OUTBOARD LOWER CORNER OF THE RT WINDSHIELD. THIS SMOKE QUICKLY DEVELOPED INTO FLAME AND FIRE VERY SOON DEVELOPED. THE CREW TOOK ACTION AND D
- [SDR OZCA202011190001](https://openairdocs.org/sdr/OZCA202011190001.md): Unknown · haze · Nov 16, 2020 · N651BC · Saab SF340A · Air Distribution System
  > CREW REPORTED, ATOMIZED OIL HAZE IN COCKPIT UNABLE TO SEE OUTSIDE OF INSTRUMENTS, AFTER HP'S WERE TURNED ON AND RECIRCLE SWITCH. MAINTENANCE PERFORMED, INSPECTED LT AND RT ACM'S FOR LEAKS AND OPERATIONS CHECK. INSPECTED LT AND RT ENGINE FOR INTERNAL OIL LEA
- [SDR OZCA202011060001](https://openairdocs.org/sdr/OZCA202011060001.md): Shaft · sheared · Nov 2, 2020 · N631BC · Saab SF340A · Propeller Feathering/Reversing
  > 2020 NOV 2ND, N631BC (AS CSQ 726) FLYING FROM GRAND CAYMAN (MWCR) TO MIAMI (KMIA) EXPERIENCED AN UNSCHEDULED PROP FEATHERING AT ALTITUDE. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK (QRH) AND EXECUTED AN ENGINE SHUTDOWN. CREW PRUDENTLY CONDUCTED AN EMERGENCY
- [SDR OZCA20201014](https://openairdocs.org/sdr/OZCA20201014.md): Smoke Detector · false activation · Oct 14, 2020 · N671BC · Saab SF340A · Smoke Detection
  > WRITE UP, MASTER WARNING, AVIONICS SMOKE LIGHT ON. MIR STATEMENT, CLIMBING OUT OF 2000 FT DEPARTING FROM KMIA TO MBPV, AVIONICS SMOKE LIGHT ON. THE CREW PERFORMED MEMORY ITEMS AND RETURNED BACK TO MIAMI SAFELY. AFTER LANDING I SMELLED A SMALL HINT OF SMOKE.
- [SDR OZCA20200811001](https://openairdocs.org/sdr/OZCA20200811001.md): Oil System · low pressure · Aug 7, 2020 · N611BC · Saab SF340A · Engine Oil Pressure
  > OIL LOW PRESSURE ON CWP AND FLIGHT CREW SHUT DOWN ENGINE IN CRUISE. SERVICED ENGINE OIL AND FILL QUANTITY EXCEEDED LIMITS IN CMM. ENGINE BEING REMOVED FOR EVALUATION.
- [SDR OZCA202008100356](https://openairdocs.org/sdr/OZCA202008100356.md): Oil System · low pressure · Aug 7, 2020 · N611BC · Saab SF340A · Engine Oil Pressure
  > OIL LOW PRESSURE ON CWP AND FLIGHT CREW SHUT DOWN ENGINE IN CRUISE. SERVICED ENGINE OIL AND FILL QUANTITY EXCEEDED LIMITS IN CMM. ENGINE BEING REMOVED FOR EVALUATION.
- [SDR OZCA202006290001](https://openairdocs.org/sdr/OZCA202006290001.md): Engine · shutdown · Jun 26, 2020 · N611B · Saab SF340A · Engine (Turbine/Turboprop)
  > WHILE CONDUCTING FLIGHT CSQ702,ON 26JUN2020, UTILIZING AIRCRAFT N611BC THE LEFT HAND ENGINE DURING CLIMB AT 9000FT HAD AN UNCOMMANDED INFLIGHT SHUTDOWN. CREW RAN THE QRH AND ATTEMPTED A RESTART THAT WAS UNSUCCESSFUL. AIRCRAFT PERFORMED AN AIR RETURN TO PAP.
- [SDR OZCA2020033100000](https://openairdocs.org/sdr/OZCA2020033100000.md): Pressure Switch · faulty · Mar 24, 2020 · N681BC · Saab SF340A · Propeller Feathering/Reversing
  > FLIGHT CREW WRITE UP - AUTOCOARSEN FAILURE IN FLIGHT. LEFT ENG FEATHERED. "AUTOCOARSEN" CWP ILLUMINATED. LATER AFTER SPEAKING WITH CAPTAIN HE STATED THAT THE PROP DID NOT FEATHER IT WAS INDICATION ONLY.
- [SDR 2018FA0000501](https://openairdocs.org/sdr/2018FA0000501.md): Seal · crushed · Nov 30, 2018 · N631BC · Saab SF340A · Engine (Turbine/Turboprop)
  > STRONG ENGINE FUMES SMELL IN FLIGHT DECK. CORRECTIVE ACTION: INSPECTED AND FOUND LH ENGINE CONICAL SEALS CRUSHED AND AC GENERATOR DRIVE SHAFT BENT. R/R AC AC GENERATOR, FOUR CONICAL SEALS ON PGB, AND FUEL OIL HEATER IAW SAAB 340 AMM LEAK AND OPS CHECK OK.
- [SDR 2018FA0000499](https://openairdocs.org/sdr/2018FA0000499.md): Dpu · abnormal · Nov 29, 2018 · N691BC · Saab SF340A · Pneumatic System
  > RH EHSI FAILED ABOVE 10000 FEET, RETURNED TO KMIA. CORRECTIVE ACTION: R/R RH DPU IAW SAAB AMM OPS CHECKED GOOD
- [SDR OZCA20180516123](https://openairdocs.org/sdr/OZCA20180516123.md): Boot · burned · May 16, 2018 · N681BC · Saab SF340A · Air Intake Anti/De-Ice System
  > WHEN CONNECTED ENGINE ANTI-ICE, ELECTRICAL SMOKE ODOR APPEARED. SMELL DISAPPEARED WHEN SYSTEM WAS DEACTIVATED. TROUBLESHOT SYSTEM AND FOUND RT ENGINE INTAKE BOOT BURNT. REPLACED ENGINE INTAKE ASSEMBLY IAW MAINTENANCE MANUAL, OPS CHECK OK.
- [SDR OZCA20170208111](https://openairdocs.org/sdr/OZCA20170208111.md): Bearing · failed · Feb 8, 2017 · N691BC · Saab SF340A · Wheel/Ski/Float
  > AFTER PARKING ON MAIN RAMP FOUND THE RIGHT WHEEL ASSEMBLY OF THE NOSE LANDING GEAR MISSING. INSTALLED RIGHT HAND NOSE WHEEL ASSEMBLY IN ACCORDANCE WITH APPLICABLE MAINTENANCE MANUAL. REMOVED AND REPLACE LEFT HAND NOSE WHEEL ASSEMBLY AS A PRECAUTION DUE TO OVER
- [SDR 2016F00217](https://openairdocs.org/sdr/2016F00217.md): Transformer · failed · Oct 31, 2016 · N135GU · Saab SF340A · Flight Compartment Lighting
  > UPON INITIAL AIRCRAFT ELECTRICAL POWER UP E26 CIRCUIT BREAKER POPPED. FLT CREW RESET CIRCUIT BREAKER AND THERE WAS SLIGHT SMOKE AND NOTICEABLE BURNING SMELL. MAINTENANCE TROUBLESHOT AND DISCOVERED OVERHEAD COCKPIT LIGHT TRANSFORMER WAS SOURCE OF ISSUE. TRAN
- [SDR PNSA2016092901](https://openairdocs.org/sdr/PNSA2016092901.md): Swivel · broken · Sep 29, 2016 · N340AQ · Saab SF340A · Landing Gear Retraction/Extension System
  > HYDRAULIC LIGHT ILLUMINATED WHEN GEAR SELECTED UP ON TAKEOFF. FOUND RT MLG DOWNLOCK SWIVEL BROKEN.
- [SDR OZCA20160917113](https://openairdocs.org/sdr/OZCA20160917113.md): Adc · odor · Sep 17, 2016 · N611BC · Saab SF340A · Air Data Computer
  > STRONG ELECTRICAL ODOR IN CABIN AND COCKPIT BUT NO NOTICABLE INDICATION PROBLEM. REMOVED AND REPLACED AIR DATA COMPUTER DUE TO HEAVY BURNED ODOR. ALSO REMOVED AND REPLACED MPU AND MFD AS PRECAUTION. COMPLIED WITH ALL OPS AND LEAK CHECKED. NO DEFECTS NOTED.
- [SDR OZCA20160505114](https://openairdocs.org/sdr/OZCA20160505114.md): Wire · shorted · May 5, 2016 · N641BC · Saab SF340A · Fire Protection System Wiring
  > ON CRUISE, LT TAIL PIPE HOT LIGHT ILLUMINATED ON WARNING PANEL. TROUBLE SHOT LT ENG TAIL PIPE, FOUND SHORT CIRCUIT ON WIRE 508-22. REPAIRED WIRE AS REQUIRED. OPERATIONAL CHECKED OK.
- [SDR OZCA20160504112](https://openairdocs.org/sdr/OZCA20160504112.md): Test Switch · intermittent · May 4, 2016 · N641BC · Saab SF340A · Fire Detection
  > ON VECTORS FOR APPROACH LT TAIL PIPE HOT ILLUMINATED ON CENTRAL WARNING PANEL. TROUBLE SHOT PROBLEM, FOUND TEST 1 PANEL FIRE TEST SWITCH INTERMITTENT. R & R TEST 1 PANEL IAW MM. OPERATIONAL CHECKED OK.
- [SDR OZCA20160504111](https://openairdocs.org/sdr/OZCA20160504111.md): Sensor · faulty · May 4, 2016 · N641BC · Saab SF340A · Overheat Detection
  > LEFT TAIL PIPE HOT LIGHT ILLUMINATED. R & R LT TAIL PIPE HOT SENSORS. INSPECTED ALL TERMINALS & WIRES WITH NO DEFECTS NOTED. OPERATIONAL CHECKED OK AT THIS TIME.
- [SDR TSAA2016042519](https://openairdocs.org/sdr/TSAA2016042519.md): Hmu · damaged · Apr 25, 2016 · N845KH · Saab SF340A · Fuel Control/Turbine Engines
  > ABORTED TAKEOFF DUE TO NR 2 ENG ISSUE NG, NP, TEMP HIGH ON NR 2 ENG WITH LITTLE TORQUE. NR 2 ENG DAMAGED DUCT GASKET REPLACED AT LOW PRESS BLEED CHECK VLV & PRSOV IAW AMM 36-11-15-04 & 71-00-00-05, BUT OPERATION CHECK NG. R & R NR ENG HMU & ADJUSTED NR 2 ENG
- [SDR OZCA20160324050](https://openairdocs.org/sdr/OZCA20160324050.md): Tire · departed · Mar 24, 2016 · N611BC · Saab SF340A · Tire
  > AFTER TAKEOFF, TOWER ALERTED ACFT THAT NR 2 TIRE ASSEMBLY DEPARTED ACFT. ACFT LANDED WITH NO ISSUES AT ITS DESTINATION. AFTER FURTHER INSPECTION, NO DAMAGE WAS NOTED TO THE LT MLG AXLE OR SHOCK STRUT. NR 2 BRAKE WAS REPLACED ALONG WITH NR 1 TIRE ASSEMBLY.
- [SDR OZCA20160310113](https://openairdocs.org/sdr/OZCA20160310113.md): Relay · failed · Mar 3, 2016 · N641BC · Saab SF340A · Electrical Power System
  > ENROUTE LOST LT MAIN BUS & ALL ASSOCIATED BUSES. R & R LT MAIN BUS RELAY. ALL OPERATIONAL CHECKED OK.
- [SDR CA160219001](https://openairdocs.org/sdr/CA160219001.md): Clutch · mismanufactured · Feb 18, 2016 · Saab SF340A · Autopilot System
  > (CAN) AUTOPILOT CLUTCH ASSY ORDERED AND RECEIVED AT ARE FACILITY FOR 1 OF OUR CUSTOMER WITH AN FAA FORM 8130-3 ATTACHED TO IT, STATUS REPAIRED. THE PN ON THE DOCUMENT WAS EFFECTIVE FOR THE ACFT MODEL AND MSN, BUT THE ACTUAL ASSY WAS WRONG ACCORDING TO OUR TECH
- [SDR PNSA2016021201](https://openairdocs.org/sdr/PNSA2016021201.md): Bleed Valve · malfunctioned · Feb 12, 2016 · N340AQ · Saab SF340A · Pneumatic Distribution System
  > LEFT LP BLEED WILL NOT OPEN. R & R LT BLEED VALVE.
- [SDR OZCA20160128020](https://openairdocs.org/sdr/OZCA20160128020.md): Connector · loose · Jan 28, 2016 · N661BC · Saab SF340A · Pneumatic System Wiring
  > RIGHT BLEED LEAK LIGHT ILLUMINATED, JUST PRIOR TO SELECTING, TAKE OFF INHIBIT, ON TAKEOFF. INSPECTED BLEED DUCTS & LOOP IN RT FLAP COVE. NO LEAKS NOTED ON DUCTS & NO DAMAGE NOTED TO LOOP. FOUND LOOSE CONNECTION IN FLAP COVE LOOP. SECURED IAW MM. OPERATION
- [SDR TSAA20151208006](https://openairdocs.org/sdr/TSAA20151208006.md): Engine · shutdown · Dec 8, 2015 · N845KH · Saab SF340A · Engine (Turbine/Turboprop)
  > ON LANDING ROLLOUT, NR 2 ENG SHUTDOWN AUTOMATICALLY. POWER LEVERS WERE INTO SLIGHT REVERSE WHEN NR 2 ENG FAILED. FOLLOWED FAULT ISOLATION MANUAL 71-00-00, VISUALLY INSPECTED NR 2 ENG INLET FOR OBSTRUCTION & IGV RING & ACTUATING LINKAGE ASSEMBLY FOR DAMAGE.
- [SDR OZCA20150921020](https://openairdocs.org/sdr/OZCA20150921020.md): Pump · failed · Sep 21, 2015 · N671BC · Saab SF340A · Hydraulic Pump (Electric/Engine), Main
  > DURING CRUISE, HYD PUMP FAILED. LANDED WITH NO INCIDENT. R & R MAIN HYD PUMP IAW MM. OPERATIONAL CHECKED SATISFACTORY.
- [SDR OZCA20150903019](https://openairdocs.org/sdr/OZCA20150903019.md): Control Handle · inoperative · Sep 3, 2015 · N611BC · Saab SF340A · Landing Gear Selector
  > LANDING GEAR NOT COMING UP. ACFT WAS FERRIED BACK FOR REPAIRS. R & R LG CONTROL HANDLE IAW MM. OPERATIONAL CHECKED SATISFACTORY.
- [SDR OZCA20150831018](https://openairdocs.org/sdr/OZCA20150831018.md): Relief Valve · faulty · Aug 31, 2015 · N651BC · Saab SF340A · Engine Oil Temperature Regulator
  > ABOUT 10 MINUTES AFTER TAKEOFF, RT ENG OIL TEMP WENT ABOVE RED LINE. REDUCED POWER & FOLLOWED QRH. TEMP SLOWLY STARTED TO REDUCE, OIL PRESS WAS 48 PSI. TROUBLE SHOT SYS & FOUND COLD OIL RELIEF VLV INOPERATIVE. R & R RT COLD OIL RELIEF VLV. GND OPERATIONAL
- [SDR OZCA20150811017](https://openairdocs.org/sdr/OZCA20150811017.md): Actuator · intermittent · Aug 10, 2015 · N691BC · Saab SF340A · Elevator Tab Control System
  > MAIN TRIM FAILURE IN FLIGHT, TESTS OK ON THE GND. PERFORMED OPERATIONAL CHECK OF MAIN & STAND-BY TRIM SYS IAW MM. PROBLEM COULD NOT BE DUPLICATED. R & R LT MAIN TRIM ACTUATOR IAW MM. OPERATIONAL CHECKED SATISFACTORY.
- [SDR OZCA20150710016](https://openairdocs.org/sdr/OZCA20150710016.md): Wire · broken · Jul 10, 2015 · N631BC · Saab SF340A · Engine Oil System Wiring
  > RIGHT SIDE PROPELLER OIL PRESSURE LIGHT CAME ON BETWEEN 0-25 PSI. TROUBLE SHOT PROBLEM & FOUND BROKEN WIRE AT RT SIDE PROPELLER GEAR BOX OIL PRESS TRANSDUCER. REPAIRED WIRE IAW APPLICABLE MM. OPERATIONAL CHECKED SATISFACTORY.
- [SDR TSAA2015032004](https://openairdocs.org/sdr/TSAA2015032004.md): Swivel · leaking · Mar 20, 2015 · N843KH · Saab SF340A · Hydraulic System, Main
  > FLIGHT 1101, DURING CLIMB OUT AFTER DEPARTING, HYD LIGHT ILLUMINATED ACCOMPANIED BY DECREASING HYD QTY. TEFERENCE LOG PAGE 260535. FOUND RT MLG SWIVEL PN L38710SA LEAKING. MX ACTION, R & R RT LG ICA AMM 32-33-10-02.
- [SDR TSAA20150206001](https://openairdocs.org/sdr/TSAA20150206001.md): Tube · cracked · Feb 6, 2015 · N843KH · Saab SF340A · Engine Fuel and Control
  > FLIGHT 5503, NR 1 ENG FAILED AT 8,000 FEET AFTER DEPARTING. NO INDICATIONS OF PROBLEMS BEFORE THE ENG FAILED. REPLACED CRACKED HMU P3 TUBE.
- [SDR OZCA201501160013](https://openairdocs.org/sdr/OZCA201501160013.md): Hmu · malfunctioned · Jan 16, 2015 · N671BC · Saab SF340A · Fuel Control/Turbine Engines
  > LEFT ENG FAILED ON LANDING ROLL AFTER USING MODERATE REVERSE THRUST. R & R LT ENG HMU IAW APPLICABLE MM. OPERATIONAL CHECKS SATISFACTORY.
- [SDR OZCA20140102012](https://openairdocs.org/sdr/OZCA20140102012.md): Latch · open · Jan 2, 2015 · N691BC · Saab SF340A · Engine Cowling System
  > AFTER TAKEOFF RT COWLING LATCH POPPED OPEN. COWLING STAYED ATTACHED, LANDED WITHOUT INCIDENT. INSPECTED RT ENG COWLING & FOUND COWLING OTBD FWD LATCH OPEN. R & R RT ENG COWLING ASSEMBLY IAW MM.
- [SDR OZCA20141219009](https://openairdocs.org/sdr/OZCA20141219009.md): Smoke Detector · inoperative · Dec 19, 2014 · N611BC · Saab SF340A · Smoke Detection
  > CARGO SMOKE DETECTOR NR 2 NOT TESTING. FOUND NR 2 SMOKE DETECTOR UNIT AT FAULT. R & R SMOKE DETECTOR UNIT IAW MM. OPERATIONAL CHECKED SATISFACTORY.

Next page: https://openairdocs.org/model/saab-sf340a/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/saab-sf340a/reports

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