# Service difficulty reports: Aerospatiale SA330J

A list on [Aerospatiale SA330J](https://openairdocs.org/model/aerospatiale-sa330j.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 69 reports

- [SDR 39LA201906254185](https://openairdocs.org/sdr/39LA201906254185.md): Fan · seized · Jun 24, 2019 · N814AR · Snias SA330J · Air Distribution Fan
  > AFTER LANDING FOR PAUSE IN VERTREP, PILOTS REPORTED SMOKE SMELL IN COCKPIT. SMOKE WAS THEN NOTED COMING FROM COCKPIT FRESH AIR VENTS. TROUBLESHOOTING REVEALED FRESH AIR VENTILATION FAN/MOTOR SIEZED AND PRODUCED SMOKE. REMOVED AND REPLACED DISCREPANT FRESH AIR
- [SDR 9EKA20181120004](https://openairdocs.org/sdr/9EKA20181120004.md): Compass · failed · Nov 20, 2018 · N902R · Snias SA330J · Magnetic Compass
  > AIRCRAFT N902R AND CREW WERE FLYING A ROUTINE VERTICAL REPLENISHMENT MISSION IN THE SOUTH PACIFIC OCEAN. WEATHER WAS CLEAR AND 28 DEGREES CELSIUS. A LITTLE OVER ONE HOUR INTO THE FLIGHT THE FLIGHT CREW DECLARED TO THE SHIP THAT THEY COULD SMELL SMOKE IN THE CO
- [SDR 39LA201810085176](https://openairdocs.org/sdr/39LA201810085176.md): Reinforcement · cracked · Oct 5, 2018 · N330KW · Snias SA330J · Fuselage Main, Frame
  > CRACKS WERE DISCOVERED IN THE MGB ATTACH REINFORCEMENT AT FRAME 3855. THE MAXIMUM CRACK LENGTH IS APPROXIMATELY 3.0 INCHES IN THE VERTICAL LEG OF THE FITTING. REF SRM TABLE 11, FIGURE 17, ITEM 18 P/N 330A-22-9701-22. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CUR
- [SDR 39LA201810051175](https://openairdocs.org/sdr/39LA201810051175.md): Floorbeam · corroded · Oct 1, 2018 · N330KW · Snias SA330J · Fuselage Main, Floor Beam
  > WHILE PERFORMING A P2 INSPECTION, CORROSION WAS DISCOVERED ON THE FLOORBEAM END CAP IN TWO LOCATIONS AT FRAME 5295. THE CORROSION REMOVAL RESULTED IN A MAXIMUM MATERIAL LOSS IN THE PRIMARY STRUCTURE OF 0.035 INCHES IN DEPTH. TECHNICAL DATA PACKAGE PR2018023 WA
- [SDR 9EKA20180329002](https://openairdocs.org/sdr/9EKA20180329002.md): Hook · broken · Mar 29, 2018 · N339EV · Snias SA330J · Agricultural Spray System
  > WHILE FLYING, THE PILOTS FELT A BUMP IN THE AIRCRAFT AND LOOKED DOWN USING THE CARGO MIRRORS TO SEE THE LOAD IMPACT THE WATER. INSPECTION OF THE HOOK SYSTEM WAS DONE AND WAS FOUND TO BE BROKEN, INTERNAL STEEL CABLE STILL INTACT, ALLOWING FOR THE HOOK TO B
- [SDR 9EKA20180126001](https://openairdocs.org/sdr/9EKA20180126001.md): Drive Shaft · sheared · Jan 26, 2018 · N339EV · Snias SA330J · Tail Rotor Drive Shaft
  > AFTER THE FLIGHT HAD BEEN COMPLETED AND THE AIRCRAFT WAS BACK ON THE SHIP AND CHOCKED AND CHAINED THE CREW PROCEEDED TO PERFORM THE FRESH WATER RINSE OF THE ENGINES. WITH THE #2 ENGINE AT FLIGHT IDLE AND THE #1 ENGINE AT GROUND IDLE THE FOR THE ENGINE RINSE T
- [SDR 9EKA20170616003](https://openairdocs.org/sdr/9EKA20170616003.md): Relay · failed · Jun 16, 2017 · N902R · Snias SA330J · AC Generation System
  > WHILE ON APPROACH FOR A SLING LOAD PICK THE AIRCRAFT EXPERIENCED A DUAL ALTERNATOR FAILURE. THE NR 2 TRANSFORMER RECTIFIER UNIT WAS INDICATING IT REMAINED ONLINE. THE NR 1 ALTERNATOR DISPLAYED 116 VAC ON ALL PHASES. "ELEC" AND "NAV" LIGHTS ON THE 7 ALPHA PAN
- [SDR 39LA20170518172](https://openairdocs.org/sdr/39LA20170518172.md): Plate · corroded · May 18, 2017 · N814AR · Snias SA330J · Fuselage Main, Structure
  > CORROSION FOUND DURING P2 INSPECTION ON THE TRANSMISSION DECK UNDER THE MAIN GEARBOX FLEXIBLE MOUNTING PLATE BETWEEN STATION 4175 AND STATION 4555 EXCEEDING ALLOWABLE REPAIR CRITERIA IN THE STRUCUTRAL REPAIR MANUAL RESULTING IN SKIN REMOVAL AND REPLACEMENT. A
- [SDR 9EKA20161122020](https://openairdocs.org/sdr/9EKA20161122020.md): Bearing · failed · Nov 22, 2016 · N1624S · Snias SA330J · Main Rotor Mast/Swashplate
  > THE PILOTS REPORTED THE TORQUE FLUCTUATING. SHUT DOWN OF THE A/C TO TROUBLESHOOT THE UPPER PORTION OF THE SWASHPLATE ASSEMBLY WAS NOTICED TO HAVE COLLAPSED AND HAD CONTACTED THE LOWER PORTION CREATING DAMAGE TO BOTH COMPONENTS.
- [SDR 39LA20160728164](https://openairdocs.org/sdr/39LA20160728164.md): Bracket · corroded · Jul 28, 2016 · N330KW · Snias SA330J · Main Rotor Blades
  > DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
- [SDR 39LA20160728163](https://openairdocs.org/sdr/39LA20160728163.md): Bracket · corroded · Jul 28, 2016 · N330KW · Snias SA330J · Main Rotor Blades
  > DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
- [SDR 39LA20160728162](https://openairdocs.org/sdr/39LA20160728162.md): Bracket · corroded · Jul 28, 2016 · N330KW · Snias SA330J · Main Rotor Blades
  > DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
- [SDR 39LA20160728161](https://openairdocs.org/sdr/39LA20160728161.md): Bracket · corroded · Jul 28, 2016 · N330KW · Snias SA330J · Main Rotor Blades
  > DURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.
- [SDR 39LA20160716165](https://openairdocs.org/sdr/39LA20160716165.md): Connector · dirty · Jul 16, 2016 · N815AR · Snias SA330J · Fire Detection
  > WHILE OPERATING, THE PILOT REPORTED THE NR 1 ENGINE FIRE WARNING LIGHT FLICKERING DURING FLIGHT. MAINTENANCE CLEANED THE WIRE CONNECTION POSTS ON ALL THE FIRE DETECTORS. GROUND OPS CHECKED. NO FAULTS WERE DETECTED.
- [SDR 39LA20160618160](https://openairdocs.org/sdr/39LA20160618160.md): Angle · corroded · Jun 18, 2016 · N330KW · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE FORWARD AND REAR.
- [SDR 39LA20160618159](https://openairdocs.org/sdr/39LA20160618159.md): Bracket · corroded · Jun 18, 2016 · N330KW · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE BRACKET.
- [SDR 39LA20160618158](https://openairdocs.org/sdr/39LA20160618158.md): Angle · corroded · Jun 18, 2016 · N330KW · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING AN AGING INSPECTION, AREAS OF CORROSION WERE FOUND ON THE LT DECK ANGLE.
- [SDR 39LA20160618157](https://openairdocs.org/sdr/39LA20160618157.md): Angle · corroded · Jun 18, 2016 · N330KW · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE MAIN FRAME OF STRUCTURE AT JACK SUPPORT.
- [SDR 9EKA20160227003](https://openairdocs.org/sdr/9EKA20160227003.md): Compressor · stalled · Feb 27, 2016 · N300EV · Snias SA330J · Turbine Engine Compressor Section
  > DURING THE LAST FLIGHT OF THE DAY, THE ACFT WAS DESCENDING WITH 7.5% PITCH. AS SOON AS PITCH WAS PULLED IN, NR 1 ENG WENT INTO COMPRESSOR STALL WITH A TEMP OF 780F. A LOWER PITCH SETTING OF 8% WAS SET & PULLED IN POWER WITH THE SAME RESULT. ENG FLIGHT IDLES
- [SDR 9EKA2015052721](https://openairdocs.org/sdr/9EKA2015052721.md): Fuel Filter · clogged · May 27, 2015 · N300EV · Snias SA330J · Aircraft Fuel Filter/Strainer
  > DURING THE FIRST TAKEOFF FROM THE SHIP AS SOON AS THE ACFT CAME OFF THE DECK, THE RT LOW PRESS FILTER CLOGGED LIGHT ILLUMINATED AS THE HELICOPTER WAS TRANSITIONING TO A HOVER. WHILE IN A HOVER THE FILTER CLOGGED LIGHT FLICKERED ON & OFF, THE PILOTS REQUESTED
- [SDR 39LA20150522136](https://openairdocs.org/sdr/39LA20150522136.md): Unknown · smoke · May 22, 2015 · N10248 · Snias SA330J · Air Distribution System
  > DURING ILS APPROACH TO PGUM THE FLIGHT CREW NOTICED SMOKE COMING FROM THE OVERHEAD PANEL. AN EMER WAS DECLARED & ACFT DIVERTED WITHOUT FURTHER INCIDENT.
- [SDR 9EKA20150612008](https://openairdocs.org/sdr/9EKA20150612008.md): Structure · corroded · Mar 8, 2015 · N366EV · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING AN ACFT INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON EXTRUSION AT FRAME 2480 UNDER PILOTS SEATS IAW SRM 53-12 PG 13 FIG 7 ITEM 24.
- [SDR 9EKA20150612007](https://openairdocs.org/sdr/9EKA20150612007.md): Angle · corroded · Mar 5, 2015 · N300EV · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON UPPER LT FUSELAGE ANGLE IAW 53-12 PG 32 & E3 FIG 17 ITEM 26.
- [SDR 9EKA20150612006](https://openairdocs.org/sdr/9EKA20150612006.md): Beam · corroded · Mar 5, 2015 · N300EV · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON LT & RT BEAMS AT THE HOOK WELL AREA IAW SRM 53-12 PG 35E FIG 18A ITEMS 21 & 22.
- [SDR 9EKA20150612005](https://openairdocs.org/sdr/9EKA20150612005.md): Beam · corroded · Mar 5, 2015 · N300EV · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND BELOW MAIN GEARBOX LT BEAM A-38. IAW SRM 53-13 PG 77 & 78 ITEM 6.
- [SDR 9EKA20150612004](https://openairdocs.org/sdr/9EKA20150612004.md): Structure · corroded · Mar 5, 2015 · N300EV · Snias SA330J · Fuselage Miscellaneous Structure
  > DURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON EXTRUSION AT FRAME 2480 UNDER PILOTS SEATS IAW SRM 53-12 PG 13 FIG 7 ITEM 24.
- [SDR 9EKA20140527001](https://openairdocs.org/sdr/9EKA20140527001.md): Pipe · leaking · May 23, 2014 · N366EV · Snias SA330J · Hydraulic System, Main
  > DURING A POST FLIGHT INSPECTION OF THE TAIL BOOM DECK NEAR FRAME STATION 9000 HYD FLUID WAS NOTICED UNDER THE TAIL ROTOR HYD RETURN PIPE. UNABLE TO DETERMINE THE SOURCE OF LEAK SO A GND POWER HYD TEST UNIT WAS HOOKED TO THE LT HAND SYS. AS SOON AS PRESS WAS
- [SDR 9EKA20140314001](https://openairdocs.org/sdr/9EKA20140314001.md): Fcu · damaged · Mar 27, 2014 · N405R · Snias SA330J · Engine (Turbine/Turboprop)
  > DURING FLIGHT, NR 2 ENGINE HAD AN NON-COMMANDED PARTIAL POWER LOSS. A LOUD BANG WAS HEARD, THE NR 2 ENGINE NG DROPPED FROM 91 TO 72 PERCENT, T4 DROPPED FROM 568 TO 441. AFTER 90 SECONDS, ENGINE SPOOLED BACK UP TO 80 PERCENT NG. ACFT LANDED WITHOUT FURTHER
- [SDR 39LA2014011751](https://openairdocs.org/sdr/39LA2014011751.md): Engine · overspeed · Jan 17, 2014 · N605R · Snias SA330J · Engine (Turbine/Turboprop)
  > DURING HOVER NR 2 ENG BEGAN TO OVER SPEED. TOOK MANUAL CONTROL OF THE ENG, FOLLOWED EMERGENCY CHECKLIST & PERFORMED NORMAL LANDING.
- [SDR 39LA2013111516](https://openairdocs.org/sdr/39LA2013111516.md): Rod · failed · Nov 15, 2013 · N10248 · Snias SA330J · Engine Cowling System
  > UPON LANDING THE NR 2 ENGINE COWLING WAS FOUND UNSECURED & DAMAGED. INSPECTION OF THE NR 2 ENGINE COWLING REVEALED THE COWLING ROD ASSEMBLY HAD FAILED. AFTER FURTHER INSPECTION THE NR 1 ENGINE COWL & SWASH PLATE ALSO HAD DAMAGE DUE TO THE UNSECURED NR 2 ENGI
- [SDR 39LA2013111514](https://openairdocs.org/sdr/39LA2013111514.md): Doubler · corroded · Nov 15, 2013 · N902R · Snias SA330J · Fuselage, Equipment Attach Fittings
  > MOORING RING EXTERNAL DOUBLER RT FUSELAGE FS 6815 FOUND TO BE CORRODED. REPAIRED DOUBLER BY ADDING A REPAIR DOUBLER IAW STS EA 10-2013-124.
- [SDR 39LA2013111513](https://openairdocs.org/sdr/39LA2013111513.md): Skin · corroded · Nov 15, 2013 · N902R · Snias SA330J · Fuselage Main, Plate/Skin
  > CORROSION FOUND LT FUSELAGE SKIN JUST BELOW CABIN WINDOW BETWEEN FS 6405 AND 6815. REPAIRED IAW STS EA 10-2013-070.
- [SDR 39LA2013111512](https://openairdocs.org/sdr/39LA2013111512.md): Skin · corroded · Nov 15, 2013 · N902R · Snias SA330J · Fuselage Main, Plate/Skin
  > CORROSION FOUND RT FUSELAGE SKIN FS 5905 AND 7225. REPAIRED IAW STS EA 10-2013-071.
- [SDR 39LA2013111500011](https://openairdocs.org/sdr/39LA2013111500011.md): Beam · corroded · Nov 15, 2013 · N902R · Snias SA330J · Fuselage Main, Structure
  > CORROSION FOUND ON NLG WELL BEAM AT FS 3223, WL 0, LT BUTT LINE 310. REPAIRED IAW DWG 13021-2029.
- [SDR 39LA2013111500010](https://openairdocs.org/sdr/39LA2013111500010.md): Frame · corroded · Nov 15, 2013 · N902R · Snias SA330J · Fuselage Main, Frame
  > CORROSION FOUND LT FRAME FS 2480, WL 1010 TO 1100 AND WL 1200 TO 1265. REPAIRED IAW STS EA 10-2013-069.
- [SDR 39LA2013111500009](https://openairdocs.org/sdr/39LA2013111500009.md): Angle · corroded · Nov 15, 2013 · N902R · Snias SA330J · Fuselage Main, Bulkhead
  > CORROSION FOUND ON BULKHEAD HORIZONTAL ANGLE FLANGE AT FS 2480. REPAIRED IAW STS EA 10-2013-068.
- [SDR 39LA2013111500008](https://openairdocs.org/sdr/39LA2013111500008.md): Structure · cracked · Nov 15, 2013 · N902R · Snias SA330J · Fuselage Main, Structure
  > WHILE PERFORMING P4 INSPECTION, FOUND UPPER DECK STRUCTURE CRACKED IN THREE PLACES AT FS 6405, RT SIDE, BUTT LINE RBL260. REPAIRED IAW AIRLIFT DWG 13021-2027 AND 13021-2028.
- [SDR 39LA2013111500007](https://openairdocs.org/sdr/39LA2013111500007.md): Structure · cracked · Nov 15, 2013 · N902R · Snias SA330J · Fuselage Main, Structure
  > WHILE PERFORMING P4 INSPECTION, FOUND UPPER DECK STRUCTURE CRACKED IN FOUR PLACES BETWEEN FS 6138 AND 6405, LT SIDE. REPAIRED IAW DWG 13021-2026.
- [SDR 9EKA2013081200001](https://openairdocs.org/sdr/9EKA2013081200001.md): Engine · failed · Aug 12, 2013 · N1623S · Snias SA330J · Engine (Turbine/Turboprop)
  > THE NR 2 FAILED IN FLIGHT. THE ENGINE HAS BEEN SENT FOR EVALUATION.
- [SDR 2013FA0000042](https://openairdocs.org/sdr/2013FA0000042.md): Oil Cooler · leaking · Jan 18, 2013 · N366EV · Snias SA330J · Engine Oil Cooler
  > NR 2 ENGINE OIL COOLER LEAKS. FOUND DURING DAILY INSPECTION PRIOR TO FLIGHT. REPLACED WITH O/H UNIT.
- [SDR 2013FA0000043](https://openairdocs.org/sdr/2013FA0000043.md): Oil Cooler · leaking · Jan 16, 2013 · N366EV · Snias SA330J · Engine Oil Cooler
  > NR 1 ENGINE OIL COOLER LEAKAGE FOUND DURING DAILY INSPECTION PRIOR TO FLIGHT. COOLER REPLACED WITH A SERVICEABLE UNIT FROM ANOTHER ENGINE. COOLERS ARE BEING REPAIRED/REBUILT.
- [SDR 2013F00033](https://openairdocs.org/sdr/2013F00033.md): Oil Cooler · leaking · Jan 16, 2013 · N366EV · Snias SA330J · Engine Oil Cooler
  > NR 1 ENGINE OIL COOLER LEAKAGE FOUND DURING DAILY INSPECTION PRIOR TO FLIGHT. COOLER REPLACED WITH A SERVICEABLE UNIT FROM ANOTHER ENGINE. COOLERS ARE BEING REPAIRED/REBUILT BY PACIFIC OIL COOLERS OF LA VERNE, CA, CERTIFICATE # RF3R813L.
- [SDR LCFA2012F00105](https://openairdocs.org/sdr/LCFA2012F00105.md): Blade · damaged · May 26, 2012 · N1622S · Snias SA330J · Turbine Section
  > DURING FLIGHT, CREW HEARD A "LOUD BANG" AND NOTED A CORRESPONDING RISE OF THE NR 1 ENGINE EGT. REDUCED POWER TO STABILIZE NR 1 ENGINE EGT AND SUBSEQUENTLY MADE A SAFE RUNNING LANDING AT HOME BASE. A POST SHUTDOWN BORESCOPE INSPECTION OF ENGINE REVEALED THA
- [SDR 3S8R2011041600018](https://openairdocs.org/sdr/3S8R2011041600018.md): Bushing · corroded · Apr 16, 2011 · N505R · Snias SA330J · Fuselage, Landing Gear Attach Fittings
  > RIGHT MLG STRUT EXTERNAL FITTING BUSHING CORRODED BEYOND LIMITS. PART WAS REPLACED WITH NEW IAW MFG RE-WORK SHEET 330 21 505 00 BY FACTORY TECHS. ASSEMBLY, CORROSION WAS REMOVED OUTSIDE THE BALL BUSHING SEAT IAW SAME RE-WORK SHEET.
- [SDR 3S8R2011041600017](https://openairdocs.org/sdr/3S8R2011041600017.md): Bushing · corroded · Apr 16, 2011 · N505R · Snias SA330J · Fuselage, Landing Gear Attach Fittings
  > LEFT MLG STRUT, EXTERNAL FITTING BUSHING CORRODED AND WORN BEYOND DIMENSIONAL LIMITS. PART WAS REPLACED WITH NEW IAW MFG RE-WORK SHEET 330 21 505 00 BY FACTORY TECHS. ADDITIONALLY, CORROSION WAS REMOVED OUTSIDE THE BALL BUSHING SEAT IAW SAME RE-WORK SHEET.
- [SDR 3S8R2011041600016](https://openairdocs.org/sdr/3S8R2011041600016.md): Beam · damaged · Apr 16, 2011 · N505R · Snias SA330J · Fuselage Main, Structure
  > RT LONGITUDINAL BEAM LOWER SKIN AND BEAM DAMAGED. REPAIR TO BE CARRIED OUT IAW MX 20-03-05-420. DAMAGE IS BETWEEN FS 3855 AND 5295.
- [SDR 3S8R2011041600015](https://openairdocs.org/sdr/3S8R2011041600015.md): Beam · damaged · Apr 16, 2011 · N505R · Snias SA330J · Fuselage Miscellaneous Structure
  > LEFT LONGITUDINAL BEAM LOWER SKIN AND BEAM DAMAGED. REPAIR TO BE CARRIED OUT IN ACCORDANCE WITH EUROCOPTER MTC 20 03 05 420.
- [SDR 3S8R2011041600014](https://openairdocs.org/sdr/3S8R2011041600014.md): Frame · corroded · Apr 16, 2011 · N505R · Snias SA330J · Fuselage Main, Frame
  > FRONT UPPER ANGLE OF FRAME AT FS X5295 CORRODED. TO BE REPLACED WITH NEW.
- [SDR 3S8R2011041600013](https://openairdocs.org/sdr/3S8R2011041600013.md): Stringer · deformed · Apr 16, 2011 · N505R · Snias SA330J · Fuselage Main, Longeron/Stringer
  > STRINGER IN REAR TRANSVERSAL FUEL TANK COMPARTMENT DEFORMED. TO BE REPLACED WITH NEW.
- [SDR 3S8R2011041600012](https://openairdocs.org/sdr/3S8R2011041600012.md): Stringer · deformed · Apr 16, 2011 · N505R · Snias SA330J · Fuselage Main, Longeron/Stringer
  > STRINGER IN REAR TRANSVERSAL FUEL TANK COMPARTMENT DEFORMED. TO BE REPLACED WITH NEW.

Next page: https://openairdocs.org/model/aerospatiale-sa330j/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 = 'SA330J'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/aerospatiale-sa330j/reports

---
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