# Service difficulty reports: Aerospatiale AS 355F1

A list on [Aerospatiale AS 355F1](https://openairdocs.org/model/aerospatiale-as-355f1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 203 reports

- [SDR TLLA205070200139](https://openairdocs.org/sdr/TLLA205070200139.md): Engine · making metal · Jun 26, 2025 · N355TH · Aerosp AS355F1 · Engine (Turbine/Turboprop)
  > #1 ENGINE CHIP LIGHT ILLUMINATED DURING FLIGHT. PILOT LANDED AT FIRST SAFEST SPOT AT SOUTHWEST WYOMING REGIONAL AIRPORT WITH NO INCIDENT. GROUNDED AC. SENT MECHANIC OUT AND FOUND CHIPS ON UPPER MAG. PLUG ON GEARBOX
- [SDR CA150411001](https://openairdocs.org/sdr/CA150411001.md): Control Cable · frozen · Mar 11, 2015 · Aerosp AS355F1 · Power Lever
  > (CAN) AIRCRAFT WAS PARKED OUTSIDE ON COLD MORNING. DURING START, PIC NOTED NOT BEING ABLE TO BRING ENGINES FROM IDLE TO FLIGHT RPM. SUBSEQUENT INSPECTION OF CONTROL SYSTEM FOUND MOISTURE PENETRATED AND FROZE INSIDE THE FLEXIBLE CONTROL CABLE RENDERING IT INO
- [SDR VMIA201506101671](https://openairdocs.org/sdr/VMIA201506101671.md): Bearing · failed · Jan 26, 2015 · N709AC · Aerosp AS355F1 · Turbine Engine Compressor Section
  > ENGINE FAILURE INFLIGHT DUE TO COMPRESSOR BEARING NR 2 FAILURE.
- [SDR CA111125001](https://openairdocs.org/sdr/CA111125001.md): Line · cracked · Nov 18, 2014 · Aerosp AS355F1 · Turbine Engine Oil System
  > (CAN) FLARED END OF OIL PRESSURE DELIVERY TUBE CRACKED UNDER FERRULE, CAUSING OIL PRESSURE LOSS AND SUBSEQUENT IN-FLIGHT SHUTDOWN OF RT ENGINE. US REG NR N355AG INCIDENT OCCURED 18 NOV 2011 ENGINE RECEIVED 23 NOV 2011 CRACK DISCOVERED 23 NOV 2011.
- [SDR CA150108008](https://openairdocs.org/sdr/CA150108008.md): Bearing · failed · Jul 9, 2014 · Aerosp AS355F1 · Engine (Turbine/Turboprop)
  > (CAN) ENGINE CHIP LIGHT ILLUMINATED. FOUND NR 5 BEARING BRINELLED.
- [SDR 2012FA0000808](https://openairdocs.org/sdr/2012FA0000808.md): Servo Control · worn · Dec 10, 2012 · N58020 · Aerosp AS355F1 · Rotorcraft Servo System
  > DURING THE ACCIDENT INVESTIGATION, ABNORMALITIES IN THE FORE & AFT SERVO ACTUATOR WERE NOTED. THE SERVO ACTUATOR WAS SENT TO THE NTSB LAB FOR EXAMINATION IN WHICH THERE IS A STRONG POSSIBILITY THAT THE UPPER ROD END ON THE FORE & AFT SERVO WAS A PROBLEM. THE
- [SDR MHIA082G001](https://openairdocs.org/sdr/MHIA082G001.md): Canopy · cracked · Sep 18, 2010 · N406LH · Aerosp AS355F1 · Fuselage Main, Structure
  > CANOPY FOUND DAMAGED AT THE UPPER LT DOOR FRAME.
- [SDR S9H2010F00000](https://openairdocs.org/sdr/S9H2010F00000.md): Structure · cracked · Apr 4, 2010 · N548SA · Aerosp AS355F1 · Rotorcraft Tail Boom
  > DURING ROUTINE 100 HR INSPECTION OF TAIL ROTOR DRIVE SHAFT BEARINGS, FOUND CRACK IN THE UPPER VERTICAL STABILIZER. REPLACED VERTICAL STABILIZER WITH SERVICEABLE UNIT.
- [SDR S9H2010F00002](https://openairdocs.org/sdr/S9H2010F00002.md): Cowling · loose · Dec 6, 2009 · N548SA · Aerosp AS355F1 · Engine Cowling System
  > LT ENGINE COWLING CAME LOOSE IN FLIGHT DAMAGING THE COWLING AND THE MAIN ROTOR BLADES. DAMAGED BLADES AND COWLING WERE R & R WITH SERVICEABLE UNITS AND IMPACT DAMAGE INSPECTION WAS PERFORMED IAW MM.
- [SDR S9H2010F00001](https://openairdocs.org/sdr/S9H2010F00001.md): Fuel Filter · unserviceable · Aug 5, 2009 · N548SA · Aerosp AS355F1 · Engine Fuel Distribution
  > RT ENGINE FLAMED OUT WHILE IN FLIGHT, AUTO RE-LIGHT, RE-ENGAGED THEN FLAMED OUT AGAIN, PERFORMED EP IAW POH. R & R ENGINE FUEL FILTER, BLED FUEL SYS AT BOOST PUMP AND FUEL NOZZLE.
- [SDR BAQA20070010](https://openairdocs.org/sdr/BAQA20070010.md): Oil System · defective · Mar 23, 2007 · N5797X · Aerosp AS355F1 · Main Rotor Gearbox
  > MAIN GEAR BOX OIL PUMP FAILED AD03-21-09-R1, DARK PURPLE COLORED OIL IN SIGHT GLASS. REMOVED AND REPLACED MAIN GEAR BOX CONTAINING OIL PUMP, COMBINER GEAR BOX, EPICYCLIC, AND ROTOR SHAFT ASSEMBLY IAW EMERGENCY ALERT SB 05.00.40 REV 2 DATED DECEMBER 20,2006
- [SDR BAQA20070006](https://openairdocs.org/sdr/BAQA20070006.md): Terminal · broken · Feb 28, 2007 · N5797X · Aerosp AS355F1 · Fire Protection System Wiring
  > DURING CRUISE FLIGHT PILOT OBSERVED THE NR 2 ENGINE FIRE LIGHT ILLUMINATE. PILOT DID A PRECAUTIONARY LANDING AT AIRPORT. MECHANIC DISPATCHED AND FOUND WIRE ON TERMINAL LUG ON FIRE DETECTOR BROKEN. REPLACED TERMINAL LUG AND COMPLIED WITH AN OPERATION CHECK OF
- [SDR MHI2005F00000](https://openairdocs.org/sdr/MHI2005F00000.md): Skin · cracked · Jul 21, 2005 · N406LH · Aerosp AS355F1 · Vertical Stabilizer, Plate/Skin
  > (REF NR: 104942) DURING INSPECTION, FOUND THE UPPER STABILIZER FIN, RT LWR DOUBLER AND NOSE SKIN CRACKED FROM THE 2ND FORWARD RIVET OF THE DOUBLER ACCROSS THE NOSE SKIN. REPLACED STABILIZER WITH SERVICEABLE STABILIZER. (K)
- [SDR MHIA104942](https://openairdocs.org/sdr/MHIA104942.md): Skin · cracked · Jul 21, 2005 · N406LH · Aerosp AS355F1 · Rotorcraft Tail Boom
  > DURING INSPECTION FOUND THE UPPER STABILIZER FIN, RIGHT HAND LOWER DOUBLER AND NOSE SKIN CRACKED FROM THE 2ND FORWARD RIVIT OF THE DOUBLER ACCROSS THE NOSE SKIN. REPLACED STABILIZER WITH SERVICEABLE STABILIZER.
- [SDR HE89099847](https://openairdocs.org/sdr/HE89099847.md): Starter Gen · unserviceable · Mar 17, 2005 · Aerosp AS355F1 · Starter-Generator
  > STARTER WOULDN'T START ENGINE
- [SDR CA040909005](https://openairdocs.org/sdr/CA040909005.md): Pitch Link · broken · Sep 5, 2004 · Aerosp AS355F1 · Main Rotor Head
  > (CAN) DURING CRUISE FLIGHT PILOT FELT SUDDEN VIBRATION IN THE M/R FLIGHT CONTROLS SYSTEM. A/C LANDED AT FIRST SUITABLE SITE. UPON INSPECTION, AME DISCOVERED THAT THE 'SCREW IN' RETAINING CUPS ON ONE OF THE M/R PITCH LINKS LOWER ROD ENDS DISINTEGRATED THUS AL
- [SDR CA040811008](https://openairdocs.org/sdr/CA040811008.md): Blower · damaged · Aug 5, 2004 · Aerosp AS355F1 · Rotorcraft Cooling Fan System
  > (CAN) DURING OPERATION A NOISE WAS HEARD FROM THE BACK OF THE AIRCRAFT, AIRCRAFT WAS LANDED AND DURING INSPECTION TO DETERMINE THE ORIGIN OF THE SOUND IT WAS NOTED THAT THE OIL COOLER BLOWER ASSY WAS DAMAGED AND HAD SEVERAL PIECES MISSING. THE AIRCRAFT WAS RET
- [SDR BAQA094102](https://openairdocs.org/sdr/BAQA094102.md): Pump · inoperative · Apr 23, 2004 · N652PM · Aerosp AS355F1 · Fuel Boost Pump
  > FUEL PRESSURE DROPPED TO ZERO, AND FUSE BLOWN. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/28/2004
- [SDR BAQA094005](https://openairdocs.org/sdr/BAQA094005.md): Fuel Control · failed · Apr 2, 2004 · N911KY · Aerosp AS355F1 · Fuel Controlling System
  > WARRANTY / EXCHANGE - CORE RETURN FOR WARRANTY/EXCHANGE PO 202317205. CORE S/N 333014 WAS RECEIVED UNDER EXCHANGE PO 202267101 AND INSTALLED ON ENGINE S/N 841012 ON 02/26/2004 AND FAILED 04/02/2004 FOR A TOTAL TSO OF 9.4 HOURS. PLEASE ADVISE WARRANTY MANAGER O
- [SDR CA040324004](https://openairdocs.org/sdr/CA040324004.md): Ring · worn · Mar 7, 2004 · Aerosp AS355F1 · Main Rotor Head
  > (CAN) ALL 3 DROOP RING YOKES WERE FOUND WITH WEAR DAMAGE ON OUTSIDE DIAMETER. THIS WEAR CORRESPONDS WITH WEAR FOUND ON THE DROOP RING CONTACT FITTINGS P/N 350A31-1852- 20 ON EACH STAR ARM. SUSPECT THAT THE YOKES WERE AT ONE TIME INSTALLED UNDER EACH STAR ARM
- [SDR CA040324003](https://openairdocs.org/sdr/CA040324003.md): Bellcrank · damaged · Mar 7, 2004 · Aerosp AS355F1 · Tail Rotor Control System
  > (CAN) TAIL ROTOR BELLCRANK FOUND WITH WEAR DAMAGE ON INSIDE YOKE AREA AT THE ATTACHMENT BOLT WITH THE TAIL ROTOR PITCH CHANGE SPIDER. THE WEAR CORRESPONDS TO THE BEARING SURFACE OF BALL END P/N 350A33-2150-01. IT IS SUSPECTED THAT THE ATTACHMENT BOLT WAS NOT T
- [SDR BAQA092581](https://openairdocs.org/sdr/BAQA092581.md): Valve · inoperative · Feb 4, 2004 · N652PM · Aerosp AS355F1 · Fuel Controlling System
  > VALVE ONLY LASTED 1.5 HOURS. SCRAPED ON SITE REPLACED WITH SERVICABLE UNIT. 02/10/2004
- [SDR BAQA092580](https://openairdocs.org/sdr/BAQA092580.md): Pressure Switch · failed · Feb 4, 2004 · N652PM · Aerosp AS355F1 · Fuel Pressure Indicating
  > PRESSURE SWITCH ONLY LASTED 1.5 HOURS REPLACED WITH SERVICABLE UNIT. 02/10/2004
- [SDR BAQA092100](https://openairdocs.org/sdr/BAQA092100.md): Altimeter · sticking · Jan 16, 2004 · N652PM · Aerosp AS355F1 · Altimeter, Barometric/Encoder
  > RADAR ALTIMETER UNIT INOPERATIVE, STICKING. FAILED OUT OF BOX. REPLACED WITH SERVICABLE UNIT. 01/20/2004
- [SDR BAQA091750](https://openairdocs.org/sdr/BAQA091750.md): Pump · failed · Jan 8, 2004 · N652PM · Aerosp AS355F1 · Fuel Boost Pump
  > FUEL BOOST PUMP PRODUCING INSUFFICIENT PRESSURE. UNIT FAILED OUT OF BOX, REPLACED WITH SERVICEABLE UNIT. 01/19/2004
- [SDR BAQA091886](https://openairdocs.org/sdr/BAQA091886.md): Governor · inoperative · Jan 5, 2004 · N5797X · Aerosp AS355F1 · Turbine Governor
  > GOVERNOR HAS SLUGGISH RESPONSE IN FLIGHT. 8130 ENCLOSED PART REPLACED WITH SERVICABLE UNIT 01/09/2004.
- [SDR BAQA090117](https://openairdocs.org/sdr/BAQA090117.md): Shaft · sheared · Oct 17, 2003 · N911KY · Aerosp AS355F1 · Starter-Generator
  > STARTER SHAFT SHEARED. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA031114007](https://openairdocs.org/sdr/CA031114007.md): Connector · burned · Oct 16, 2003 · Aerosp AS355F1 · Fuel System Wiring
  > (CAN) WHILE THE AIRCRAFT WAS IN CRUISE FLIGHT, A BURNING ODOR WAS NOTICED IN THE CABIN. THE PILOT LANDED THE AIRCRAFT UNEVENTFULLY. THE BURNING ODOR WAS TRACED TO THE OVERHEAD LT FUEL PUMP SWITCH. WHEN THE OVERHEAD PANELS WERE REMOVED A BURNED PUMP SWITCH CON
- [SDR BAQA089870](https://openairdocs.org/sdr/BAQA089870.md): Starter Gen · malfunctioned · Oct 13, 2003 · N5797X · Aerosp AS355F1 · Starter-Generator
  > STARTER GEN HAS INTERMITTENT ROTATION. REPLACED WITH SERVICEABLE UNIT.
- [SDR AUS20030944](https://openairdocs.org/sdr/AUS20030944.md): Skin · cracked · Sep 11, 2003 · Aerosp AS355F1 · Rotorcraft Tail Boom
  > (AUS) TAILBOOM SKIN CRACKED IN AREA LOCATED AFT OF THE TAIL ROTOR GEARBOX. CRACK ORIGINATED FROM RIVET HOLE IN TAIL ROTOR GEARBOX COWL BRACKET. CRACKED HAD EXTENDED AFT FOR APPROX 50.8MM TO 76. 2MM (2IN TO 3IN) IN AN AREA NOT NORMALLY VISIBLE WITH VERTICAL STA
- [SDR BAQA089028](https://openairdocs.org/sdr/BAQA089028.md): Pump · noisy · Sep 2, 2003 · N911KY · Aerosp AS355F1 · Fuel Boost Pump
  > BOOST PUMP MAKING EXTREMELY LOUD NOISES. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA040806008](https://openairdocs.org/sdr/CA040806008.md): Planetary Gear · spalled · Aug 30, 2003 · Aerosp AS355F1 · Main Rotor Gearbox
  > (CAN) EPI CYCLIC WAS MAKING METAL. SOURCE WAS THE PLANET GEAR INNER RACE WAS SPALLING AND MAKING METAL.
- [SDR BAQA088910](https://openairdocs.org/sdr/BAQA088910.md): Indicator · fluctuates · Aug 21, 2003 · N5797X · Aerosp AS355F1 · Fuel Quantity Indicator
  > RIGHT FUEL GUAGE FLUCTUATES IN FLIGHT. REPLACED WITH SERVICEABLE UNIT.
- [SDR EJYA566D](https://openairdocs.org/sdr/EJYA566D.md): Fire Detector · dirty · Aug 1, 2003 · N911NW · Aerosp AS355F1 · Fire Detection
  > ENG FIRE WARNING LIGHT ILLUMINATED IN FLT. PILOT PERFORMED REQUIRED EMER PROCEDURES AND PERFORMED EMER LANDING. WHEN MAINT ARRIVED, FIRE WARNING LIGHT HAD EXTINGUISHED. FIRE WARNING SYSTEM WAS INSPECTED AND NO DEFECTS FOUND. MECH CLEANED ALL FIRE DETECTORS
- [SDR BAQA088261](https://openairdocs.org/sdr/BAQA088261.md): Transmitter · failed · Aug 1, 2003 · N5797X · Aerosp AS355F1 · Fuel Quantity Sensor
  > INSTALLED UNIT AND FAILED ON FIRST FLIGHT OF.2 HOURS. GAGE FELL TO BELOW ZERO. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA088263](https://openairdocs.org/sdr/BAQA088263.md): Transmitter · reads low · Jul 31, 2003 · N5797X · Aerosp AS355F1 · Fuel Quantity Sensor
  > FUEL QUANTITY FLUCTUATES BETWEEN FULL AND LESS THAN 20 PERCENT. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA030617002](https://openairdocs.org/sdr/CA030617002.md): Rib · cracked · May 20, 2003 · Aerosp AS355F1 · Vertical Stabilizer, Spar/Rib
  > (CAN) DURING ROUTINE INSPECTION OF THE UPPER VERTICAL FIN ATTACHMENT FRAME, AME DISCOVERED RIB TO BE CRACKED. RIB REPLACED AS PER REPAIR MANUAL AND A/C RETURNED TO SERVICE.
- [SDR BAQA086321](https://openairdocs.org/sdr/BAQA086321.md): Adjuster · loose · May 2, 2003 · N911TM · Aerosp AS355F1 · Fuel Controlling System
  > ENGINE N1 IDLE ADJUSTMENT SCREW HAS FREE MOVEMENT EITHER RIGHT HAND OR LEFT HAND. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA085970](https://openairdocs.org/sdr/BAQA085970.md): Indicator · precesses · Apr 15, 2003 · N911KY · Aerosp AS355F1 · Navigation System
  > UNIT PRECESSES BADLY AT TIMES. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA085913](https://openairdocs.org/sdr/BAQA085913.md): Circuit Card · failed · Apr 4, 2003 · N911TM · Aerosp AS355F1 · DC Generating System
  > NR 2 GENERATOR DROPS OFF LINE. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA030305003](https://openairdocs.org/sdr/CA030305003.md): Nut · loose · Feb 28, 2003 · Aerosp AS355F1 · Main Rotor Brake
  > (CAN) FLT CREW REPORTED THAT THE ROTOR BRAKE HAD NO EFFECT WHEN APPLIED. THE ROTOR BRAKE PACK WAS BEING INSPECTED AND TO HAVE SHIMS ADJUSTED WHEN THE OUT PUT FLANGE LOCK NUT WAS FOUND ON THE DECK BELOW THE FLANGE. THE OUTPUT FLANGE WAS REMOVED AND INSPECTED WI
- [SDR BAQA082689](https://openairdocs.org/sdr/BAQA082689.md): Governor · malfunctioned · Dec 27, 2002 · N5797X · Aerosp AS355F1 · Turbine Governor
  > NR 2 ENGINE SN 841010 WOULD NOT TRIM. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA021119003](https://openairdocs.org/sdr/CA021119003.md): Hub · cracked · Oct 8, 2002 · Aerosp AS355F1 · Tail Rotor Blades
  > (CAN) IT WAS NOTED THAT ON THE LAST SHUTDOWN A NOISE WAS BEING GENERATED FROM THE T/R BLADE ASSY REGION. IT WAS MENTIONED TO AN ENGINEER AND THEY CARRIED OUT A EQUIVALENT TO A 30 HOUR INSPECTION AS PER AD 84-064-037(B)R3. (NO DISASSEMBLY) A VERY SLIGHT NOISE
- [SDR CA021031003](https://openairdocs.org/sdr/CA021031003.md): Bearing · worn · Sep 24, 2002 · Aerosp AS355F1 · Turbine Engine Compressor Section
  > (CAN) AIRCRAFT IN CRUISE FLIGHT. PILOT NOTICED NG FLUCTUATION BETWEEN ENGINES, FOLLOWED BY ENGINE AT NR 2 CHIP LIGHT AND AN UNUSUAL NOISE & HOWL. PILOT SHUTDOWN NR 2 ENGINE AND MADE UNSCHEDULED LANDING AT NEARBY AIRPORT. NR 2 ENGINE COMPRESSOR SAGS FOUND WORN
- [SDR CA020911002](https://openairdocs.org/sdr/CA020911002.md): Bushing · debonded · Sep 3, 2002 · Aerosp AS355F1 · Main Rotor Head
  > (CAN) ON A DAILY INSPECTION ONE BUSHING WAS FOUND TO BE DEBONDED. THE RETAINING BOLT WAS COMPLETELY PULED OUT OF THE STARFLEX. PILOT REPORTED NO ABNORMAL VIBRATION. STARFLEX ASSEMBLY REPLACED BEFORE NEXT FLIGHT.
- [SDR CA020828005](https://openairdocs.org/sdr/CA020828005.md): Bearing · elongated · Aug 9, 2002 · Aerosp AS355F1 · Tail Rotor Drive Shaft
  > (CAN) NOISE WAS HEARD FROM OIL COOLER FAN AREA ON SHUTDOWN. INSPECTION REVEALED NR 6 T/R DRIVESHAFT SUPPORT BEARING BOLT HOLES HAD ELONGATED AND ALLOWED THE T/R DRIVESHAFT AND FAN SHAFT TO MOVE OUT OF ALIGNMENT. NR 6 BEARING SUPPORT, BEARING AND BEARING TRAN
- [SDR CA020521008](https://openairdocs.org/sdr/CA020521008.md): Ball Joint · worn · May 14, 2002 · Aerosp AS355F1 · Rotorcraft Flight Control
  > (CAN) AFTER LAST FLIGHT INSPECTION THE LOWER ROD END WAS FOUND TO BE LOOSE. THE STAKED AREA AROUND THE BALL WAS WORN ENOUGH TO ALLOW IT TO COME OUT OF THE ROD END. NEW ROD END INSTALLED.
- [SDR AUS20020106](https://openairdocs.org/sdr/AUS20020106.md): Hook · faulty · Feb 14, 2002 · Aerosp AS355F1 · Passenger Compartment Equipment
  > (AUS) SAFETY HARNESS USED BY CAMERAMAN FAULTY. SNAP HOOK ON HARNESS MAY UNDER SOME CIRCUMSTANCES HAVE THE SPRING LOADED SAFETY CATCH FORCED OPEN ALLOWING THE SNAP HOOK TO SEPARATE FROM THE AIRCRAFT ATTACHMENT POINT.
- [SDR CA020213008](https://openairdocs.org/sdr/CA020213008.md): Pump · making metal · Feb 8, 2002 · Aerosp AS355F1 · Engine Fuel Pump
  > (CAN) NR 1 ENGINE FUEL BOOST PUMP WAS MAKING TOO MUCH NOISE AND VIBRATING AS COMPARED TO NR 2 FUEL BOOST PUMP. INSPECTED THE NR 1 ENGINE DRIVEN FUEL PUMP FILTER AND FOUND NON-FERROUS METAL IN THE FILTER. INSPECTED THE FUEL CONTROL FILTER FOR CONTAMINATION AN
- [SDR AUS20020060](https://openairdocs.org/sdr/AUS20020060.md): Gasket · faulty · Jan 25, 2002 · Aerosp AS355F1 · Main Rotor Gearbox
  > (AUS) MAIN ROTOR TRANSMISSION EPICYCLIC RING GEAR GASKET FAULTY. GASKET WAS EXTRUDING FROM BETWEEN THE UPPER AND LOWER CASES AND BREAKING INTO PIECES AND CAUSING AN OIL LEAK WHICH WAS PROGRESSIVELY WORSENING. ON DISASSEMBLY THE MATING CASE FLANGES SHOWEDSIGNS

Next page: https://openairdocs.org/model/aerospatiale-as-355f1/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 = 'AS355F1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/aerospatiale-as-355f1/reports

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