# Service difficulty reports: Textron 408

A list on [Textron 408](https://openairdocs.org/model/textron-408.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 133 reports

- [SDR FXGA202610140001](https://openairdocs.org/sdr/FXGA202610140001.md): Skin · cracked · Oct 14, 2026 · N408RE · Textrn 408 · Wing, Plate/Skin
  > FOUND 2 CRACKS ON LT WING UPPER SKIN. 1ST CRACK 2.3" LONG BETWEEN RIBS AT LBL 142.3 & 157.95, APPROXIMATELY 17.5 INCHES FORWARD OF WING TRAILING EDGE. 2ND CRACK 4.5" LONG BETWEEN RIBS AT LBL 157.95 & 173.6, APPROXIMATELY 14.25 INCHES FORWARD OF WING TRAILING E
- [SDR 2026FA0000836](https://openairdocs.org/sdr/2026FA0000836.md): Fairing · separated · Oct 14, 2026 · N703BA · Textrn 408 · Vertical Stabilizer
  > UPPER VERTICAL TIP CAP FAIRING SEPARATED IN FLIGHT, SUBSEQUENTLY DAMAGING UPPER PORTION OF RUDDER, UPPER VERTICAL SKIN, ELEVATOR PUSH RODS AND ELEVATOR HORNS.
- [SDR FXTA20261016001](https://openairdocs.org/sdr/FXTA20261016001.md): Rib · cracked · Oct 12, 2026 · N409BA · Textrn 408 · Wing, Rib/Bulkhead
  > 3 CRACKED RIBS RIGHT FLAP COVE. RIB P/N: 7822265-10 @ WS 100.5", RIB P/N: 7822265-12 @ WS 116.0", RIB P/N: 7822265-12 @ 131.5"
- [SDR COEA2026101213738](https://openairdocs.org/sdr/COEA2026101213738.md): Armature · cracked · Oct 7, 2026 · N738FX · Textrn 408 · Ice/Rain Protection System
  > DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED ON THE LT FWD INERTIAL SEPERATOR ARMATURE. REPLACED INERTIAL SEPERATOR FWD TORQUE TUBE IAW C408 MM 30-20-16. OPS CHECK GOOD.
- [SDR COEA2026101212767](https://openairdocs.org/sdr/COEA2026101212767.md): Skin · cracked · Oct 7, 2026 · N767FX · Textrn 408 · Wing, Plate/Skin
  > DURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK ON THE RT UPPER WING SKIN BETWEEN WS 224.32 AND WS 241.68. OPEN
- [SDR COEA2026101211767](https://openairdocs.org/sdr/COEA2026101211767.md): Skin · cracked · Oct 7, 2026 · N767FX · Textrn 408 · Wing, Plate/Skin
  > DURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK IN THE LT UPPER WING SKIN BETWEEN WS 157.95 AND WS 142.30. OPEN
- [SDR COEA2026100109708](https://openairdocs.org/sdr/COEA2026100109708.md): Skin · cracked · Sep 30, 2026 · N708FX · Textrn 408 · Wing, Plate/Skin
  > EVIDENCE OF A CRACK ON THE R/H WING AFT SIDE TOWARDS THE OUTBOARD PORTION OF THE FLAP. OPEN
- [SDR COEA2026100108708](https://openairdocs.org/sdr/COEA2026100108708.md): Panel · dented · Sep 29, 2026 · N708FX · Textrn 408 · Wing, Plate/Skin
  > DENT UNDER LT SPONSON PANEL. OPEN
- [SDR COEA2026091707734](https://openairdocs.org/sdr/COEA2026091707734.md): Light · failed · Sep 17, 2026 · N734FX · Textrn 408 · Exterior Lighting
  > FLIGHT 204, GEG - MFR AIR TURNBACK, REMOTE CAB CASS MESSAGE DURING FLIGHT. AIRCRAFT WAS RETURNED TO GEG. REPLACED LT WING TIP LIGHT ASSY. OPS CHKD GOOD.
- [SDR FXTA20260904001](https://openairdocs.org/sdr/FXTA20260904001.md): Skin · cracked · Sep 4, 2026 · N703BA · Textrn 408 · Vertical Stabilizer, Plate/Skin
  > INSPECTION PANEL ON TOP OF THE VERTICAL STABILIZER ATTACHMENT FLANGE CRACKED ALLOWING THE PANEL TO DEPART AIRCRAFT. THIS INSPECTION PANEL IN UNDER THE RUDDER HORN. TOP PANEL P/N: 7831102-23, ONCE ATTACHMENT FAILS HITS RUDDER AND PIECE FOUND IN ELEVATOR CONTROL
- [SDR COEA2026090306783](https://openairdocs.org/sdr/COEA2026090306783.md): Exhaust Stack · broken · Sep 2, 2026 · N783FX · Textrn 408 · Engine Collector/Tailpipe/Nozzle
  > RIGHT INBD EXHAUST STACK PORT FOR THE HEATED INTAKE DUCT BROKEN OFF. RT INBD EXHAUST STACK REPLACED IAW MM 78-10-05. MINOR REPAIR.
- [SDR COEA2026082705738](https://openairdocs.org/sdr/COEA2026082705738.md): Master Cylinder · failed · Aug 26, 2026 · N738FX · Textrn 408 · Master Cylinder/Brake Valve
  > FLIGHT 7804, PILOT SIDE RIGHT BRAKE PEDAL INEFFECTIVE. REPLACED ALL 4 MASTER CYLINDERS AND RT BRAKE ASSEMBLY. FLUSHED ENTIRE SYSTEM. ALL CHECKS GOOD.
- [SDR COEA2026081904738](https://openairdocs.org/sdr/COEA2026081904738.md): Brake · contaminated · Aug 18, 2026 · N738FX · Textrn 408 · Landing Gear Brake System
  > RIGHT BRAKE INEFFECTIVE DURING ROLLOUT. BLED AIR FROM RT BRAKE ASSY. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR COEA2026100810759](https://openairdocs.org/sdr/COEA2026100810759.md): Stringer · damaged · Aug 5, 2026 · N759FX · Textrn 408 · Fuselage Main, Longeron/Stringer
  > ON SKIN REMOVAL, FOUND OVERSIZED HOLE IN FRAME 3, ON STRINGER 13L. FREEZE BUSHING REPAIR TO OVERSIZED HOLE, FRAME 3, ON STRINGER 13L IAW FR-408-00-15-54161.
- [SDR FXTA20260804001](https://openairdocs.org/sdr/FXTA20260804001.md): Strut · damaged · Aug 4, 2026 · N408BA · Textrn 408 · Wing Main, Frame Structure
  > DURING PREFLIGHT, IT WAS DISCOVERED THAT THE RH UPPER WING STRUT MISSING PART OF METAL FAIRING. APPEARS THAT DURING MANUFACTURE THE SEAMS WERE OFFSET CAUSING A STRESS IN THE SKIN ALLOWING IT TO CRACK.
- [SDR FXTA20260628002](https://openairdocs.org/sdr/FXTA20260628002.md): Flex Drive · failed · Jun 28, 2026 · N409BA · Textrn 408 · Trailing Edge Flap Actuator
  > RT OUTBOARD FLAP FLEX SHAFT RUBBER CASE FAILING AT THE CRIMP UNDER STAINLESS STEEL OUTER WRAP. THIS SEPARATION ALLOWS THE OUTER CASE TO LENGTHEN AND THE INNER DRIVE SHAFT CAN SLIDE LEFT AND RIGHT TO THE POINT THE DRIVE COMES OUT OF THE JACKSCREW CAUSING THE FL
- [SDR FXTA20260628001](https://openairdocs.org/sdr/FXTA20260628001.md): Bolt · loose · Jun 28, 2026 · N409BA · Textrn 408 · Wing, Attach Fittings
  > FLAP ACTUATOR ATTACHMENT HARDWARE FOUND LOOSE
- [SDR FXTA20260626001](https://openairdocs.org/sdr/FXTA20260626001.md): Bolt · loose · Jun 26, 2026 · N701BA · Textrn 408 · Leading Edge Slat Actuator
  > FLAP ACTUATOR ATTACHMENT HARDWARE FOUND LOOSE
- [SDR COEA2026101314759](https://openairdocs.org/sdr/COEA2026101314759.md): Skin · damaged · Jun 19, 2026 · N759FX · Textrn 408 · Fuselage Main, Plate/Skin
  > PERMANENT REPAIR OF L/H NOSE SKIN AND L/H DOOR DRIP CAP DAMAGE. PERMANENT REPAIR COMPLETED IAW DQ51100M2.
- [SDR FXTA20260617001](https://openairdocs.org/sdr/FXTA20260617001.md): Flex Drive · failed · Jun 17, 2026 · N701BA · Textrn 408 · Leading Edge Slat Control System
  > LH AND RH OUTBOARD FLAP FLEX SHAFT RUBBER CASE FAILING AT THE CRIMP UNDER STAINLESS STEEL OUTER WRAP. THIS SEPARATION ALLOWS THE OUTER CASE TO LENGTHEN AND THE INNER DRIVE SHAFT CAN SLIDE LEFT AND RIGHT TO THE POINT THE DRIVE COMES OUT OF THE JACKSCREW CAUSING
- [SDR FXGA202606150001](https://openairdocs.org/sdr/FXGA202606150001.md): Drive Cable · deformed · Jun 12, 2026 · N418RE · Textrn 408 · Trailing Edge Flap Control System
  > FLAP FAIL CASS MESSAGE INDICATED WHEN FLAP DEPLOYED FROM FULL UP. UPON INVESTIGATION FOUND THE LT FLAP HAD A SLIGHT TWIST. THE OTBD ACTUATOR HAD NOT ENGAGED TO DRIVE THE FLAP AND THE INBD ACTUATOR DROVE THE INBOARD SIDE DOWN ABOUT 3 DEGREES BEFORE THE SYSTEM D
- [SDR MTNA2026061500002](https://openairdocs.org/sdr/MTNA2026061500002.md): Probe · false indication · Jun 12, 2026 · N714FX · Textrn 408 · Fuel Indicating System
  > ON JUNE 12, 2026, DURING DESCENT ON FLIGHT MTN8380 FROM MEM TO DHN, 714FX, EXPERIENCED INTERMITTENT FUEL LEVEL LO R AND FUEL LEVEL LO L AMBER CAS MESSAGES BEGINNING APPROX 15 MINS PRIOR TO LANDING WITH 3,210 LBS INDICATED FOB AT DEPARTURE. THE RIGHT TANK LEVE
- [SDR MTNA2026051900001](https://openairdocs.org/sdr/MTNA2026051900001.md): Probe · false indication · May 19, 2026 · N743FX · Textrn 408 · Fuel Indicating System
  > WHEN N743FX LANDED IN MCO LAST NIGHT WITH THE LOW FUEL LIGHT ON, WHEN THE PIC WAS PULLING INTO PARK, THEY HAD APPROXIMATELY 700 LBS AND THE NR 2 ENGINE SHUT OFF. THE RT SIDE NR 4 PROBE SEEMS TO BE WAY OFF PER 28-40-00.
- [SDR 2026FA0000312](https://openairdocs.org/sdr/2026FA0000312.md): Torque Tube · damaged · Apr 28, 2026 · N408TL · Textrn 408 · Elevator Structure
  > PERFORMED INSPECTION OF THE RUDDER HINGES INSTALLATION DUE TO THE CUSTOMER REQUEST. ALL FOUND SATISFACTORY. DURING THE INSPECTION TECHNICIAN TOUCH THE ELEVATORS LH & RH SIDE AND FEELS FREE PLAY. WITH THE INSPECTION MIRROR AND TORCH PERFORMED QUICK CHECK AND RE
- [SDR 2026FA0000310](https://openairdocs.org/sdr/2026FA0000310.md): Torque Tube · excess play · Apr 28, 2026 · N408TL · Textrn 408 · Flight Control System
  > PERFORMED INSPECTION OF THE RUDDER HINGES INSTALLATION DUE TO THE CUSTOMER REQUEST. ALL FOUND SATISFACTORY. DURING THE INSPECTION TECHNICIAN TOUCH THE ELEVATORS LH & RH SIDE AND FEELS FREE PLAY. WITH THE INSPECTION MIRROR AND TORCH PERFORMED QUICK CHECK AND RE
- [SDR MTNA2026061500001](https://openairdocs.org/sdr/MTNA2026061500001.md): Probe · false indication · Apr 23, 2026 · N758FX · Textrn 408 · Fuel Indicating System
  > DURING MTNA'S 800 HR INSPECTION ON 758FX IT WAS IDENTIFIED THAT: LEFT FUEL QTY FOUND TO BE INACURATE, WITH EMPTY LEFT SIDE IS 77OLB OF FUEL MX: SYSTEM T/S PERFORMED, DETERMINED #4 PROBE AT FAULT PER C408 MM CHAPT 28-40-00. REPLACED #4 LEFT FUEL QTY PROBE AND
- [SDR COEA2026041703781](https://openairdocs.org/sdr/COEA2026041703781.md): Brake · contaminated · Apr 16, 2026 · N781FX · Textrn 408 · Landing Gear Brake System
  > FLIGHT 8737, GEG - YKM R/H BRAKE PEDAL SOFT, LITTLE TO NO BRAKING EFFECTIVENESS DURING TAXI. SHUT DOWN AND THE AIRCRAFT WAS TOWED BACK TO THE RAMP. MAINTENANCE PERFORMED INSPECTIONS AND CLEANED DEICE FLUID FROM THE R/H BRAKE. ENGINE RUN AND TAXI CHECKS GO
- [SDR COEA2026010702708](https://openairdocs.org/sdr/COEA2026010702708.md): Pressure Switch · faulted · Jan 6, 2026 · N708FX · Textrn 408 · Airfoil Anti/De-ice System
  > FLIGHT 8737, ENROUTE GEG - YKM AIR TURNBACK, DURING CRUISE, THE STAB DE-ICE FAIL ILLUMINATED. DUE TO ICING CONDITIONS, THE PILOT DECLARED AN EMERGENCY AND RETURNED TO GEG WITHOUT INCIDENT. MAINTENANCE REMOVED THE EMPENNAGE PRESSURE SWITCH SV001 AND FOUND R
- [SDR COEA2026010601759](https://openairdocs.org/sdr/COEA2026010601759.md): Lead · faulted · Jan 5, 2026 · N759FX · Textrn 408 · Ice/Rain Protection System Wiring
  > FLIGHT 8658, ENROUTE: SMF - CEC AIR TURNBACK, RECURRING AMBER PROP HEAT L CAS MESSAGE MIDWAY TO CEC DURING ICING CONDITIONS. AIRCRAFT RETURNED TO SMF. NO EMERGENCY WAS DECLARED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT NR 3 PROP LEAD.
- [SDR 2026FA0000059](https://openairdocs.org/sdr/2026FA0000059.md): Tach Generator · loose · Dec 25, 2025 · N971LA · Textrn 408 · Propeller Indication System
  > ON 12/25/25, WE HAD AN INFLIGHT EMERGENCY DECLARED BY THE FLIGHT CREW FOR #1 ENGINE PROP SPEED ERRATIC. THE CREW REPORTED THE #1 ENGINE PROPELLER SPEED WAS JUMPING AROUND BETWEEN 1400 AND 1900 IN CLIMB SHORTLY AFTER TAKEOFF. THE CREW SAID ALL OTHER ENGINE INDI
- [SDR K2AA2026010900001](https://openairdocs.org/sdr/K2AA2026010900001.md): Fuel Filter · bypassing · Dec 11, 2025 · N408KA · Textrn 408 · Aircraft Fuel Distribution System
  > PILOT REPORTED FUEL BYPASS CAS MESSAGE ON LH ENGINE DURING FLIGHT.
- [SDR COEA2025110612738](https://openairdocs.org/sdr/COEA2025110612738.md): Panel · cracked · Nov 3, 2025 · N738FX · Textrn 408 · Nacelle/Pylon, Main Frame
  > NUMBER 2 ENGINE INBD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. STOP DRILLED CRACK AND COVERED WITH SPEED TAPE IAW DQ428170M2. REPLACED THE PLENUM PANEL IAW MM 6-40-50 REV. 5 AND IPC 54-10-25-01 REV. 10.
- [SDR COEA2025110611738](https://openairdocs.org/sdr/COEA2025110611738.md): Panel · cracked · Nov 3, 2025 · N738FX · Textrn 408 · Nacelle/Pylon, Main Frame
  > WO 272105 NR 6 MINOR REPAIR/DISCREPANCY: #1 ENGINE OUTBOARD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. STOP DRILLED CRACK AND COVERED WITH SPEED TAPE IAW DQ428170M2. REPLACED THE PLENUM PANEL IAW MM 6-40-50 REV. 5 AND IPC 54-10-25-01 REV. 10.
- [SDR COEA2025110610738](https://openairdocs.org/sdr/COEA2025110610738.md): Panel · cracked · Nov 3, 2025 · N738FX · Textrn 408 · Nacelle/Pylon, Main Frame
  > WO 272105 NR 5 MINOR: NR 1 ENGINE INBD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. REPLACED THE PLENUM PANEL IAW C408MM 6-40-50 REV.11
- [SDR COEA2025110616759](https://openairdocs.org/sdr/COEA2025110616759.md): Link · corroded · Oct 30, 2025 · N759FX · Textrn 408 · Nacelle/Pylon, Main Frame
  > WO 271980 NR 5 MINOR REPAIR/DISCREPANCY: RT ENGINE AFT DOOR LINK ASSY FRETTED AROUND CHAMBERED AREA. REPLACED RT AFT INERTIAL SEPERATOR DOOR LINK ASSY REF IPC 30-20-05 FIG 1-5.
- [SDR COEA2025110615759](https://openairdocs.org/sdr/COEA2025110615759.md): Link · corroded · Oct 30, 2025 · N759FX · Textrn 408 · Nacelle/Pylon, Main Frame
  > WO 271980 NR 3 MINOR REPAIR/DISCREPANCY: LT ENGINE AFT DOOR LINK ASSY FRETTED AROUND CHAMBERED AREA. CORRECTIVE ACTION: REPLACED L/H AFT INERTIAL SEPERATOR DOOR LINK ASSY. REF IPC 30-20-05 FIG 1-5.
- [SDR COEA2025110614759](https://openairdocs.org/sdr/COEA2025110614759.md): Link · cracked · Oct 30, 2025 · N759FX · Textrn 408 · Nacelle/Pylon, Main Frame
  > WO 271980 NR 2 MINOR REPAIR/DISCREPANCY: R/H ENGINE FWD DOOR LINK ASSY IS CRACKED. REPLACED FWD INERTIAL SEPERATOR DOOR LINK ASSY REF C408 IPC 30-20-05 FIG 1-5.
- [SDR FXTA20251029001](https://openairdocs.org/sdr/FXTA20251029001.md): Cylinder · leaking · Oct 29, 2025 · N409BA · Textrn 408 · Rudder Control System
  > PILOT FELT STRONG LEFT RUDDER PRESSURE ON TWO CONSECUTIVE TAKE OFFS
- [SDR FXTA20251106001](https://openairdocs.org/sdr/FXTA20251106001.md): Seal · broken · Oct 23, 2025 · N701BA · Textrn 408 · Main Landing Gear
  > RH MAIN LANDING SCRAPPER SEAL BROKEN AND HANGING FROM BOTTOM OF STRUT.
- [SDR FXTA2025111000001](https://openairdocs.org/sdr/FXTA2025111000001.md): Transducer · failed · Oct 20, 2025 · N703BA · Textrn 408 · Engine Indicating System
  > ON TAKE OFF RIGHT ENGINE LOSS TORQUE INDICATION.
- [SDR COEA2025110613778](https://openairdocs.org/sdr/COEA2025110613778.md): Mechanism · cracked · Oct 17, 2025 · N778FX · Textrn 408 · Nacelle/Pylon Structure
  > WO 271981 NR 5 MINOR REPAIR/DISCREPANCY: #1 AND #2 ENGINE SEPERATOR FWD DOOR LINK CRACKED. CORRECTIVE ACTION: REPLACED #1 AND #2 ENGINE INERTIAL SEPERATOR CONTROL MECHANISM ASSYS IAW C408 MM 30-20-16.
- [SDR COEA2025091109757](https://openairdocs.org/sdr/COEA2025091109757.md): Support · damaged · Sep 10, 2025 · N757FX · Textrn 408 · Engine Mount Section
  > LEFT ENGINE INBOARD AFT TRUSS SUPPORT DAMAGE. MAINTENANCE INSPECTED AND APPLIED SURFACE TREATMENT PER SRM.
- [SDR COEA2025091108757](https://openairdocs.org/sdr/COEA2025091108757.md): Bracket · gouged · Sep 10, 2025 · N757FX · Textrn 408 · Nacelle/Pylon, Main Frame
  > DAMAGE FOUND ON THE LEFT ENGINE INBOARD AFT FIREWALL BEHIND ICE VANE ACT REAR BRACKET ASSY. MAINTENANCE INSPECTED AND APPLIED SURFACE TREATMENT PER SRM.
- [SDR COEA2025091107757](https://openairdocs.org/sdr/COEA2025091107757.md): Rod End · sheared · Sep 10, 2025 · N757FX · Textrn 408 · Engine Anti-Icing System
  > LEFT ENGINE ICE VANE ACTUATOR AFT CLEVIS SHEARED OFF. REPLACED BROKEN ROD END AND RE-INSTALLED ICE VANE ACTUATOR IAW C408 MM 30-20-00.
- [SDR COEA2025082106759](https://openairdocs.org/sdr/COEA2025082106759.md): Seat · cracked · Aug 20, 2025 · N759FX · Textrn 408 · Flight Compartment Equipment
  > CAPTAIN SEAT BROKEN, FOAM UNDER CUSHION CRACKED. REPLACED WITH NEW CREW SEAT REF. MM 25-71-05.
- [SDR MTNA20250815001](https://openairdocs.org/sdr/MTNA20250815001.md): Access Panel · cracked · Aug 13, 2025 · N743FX · Textrn 408 · Nacelle/Pylon, Plate/Skin
  > CRACK FOUND ON RH ENGINE NACELLE..... PERFORMED TEMP REPAIR PER MAC EO # C408-54-0003 AND CESSNA 408 NACELLE CRACKING MINOR REPAIR LETTER DQ42817M3 DATED OCTOBER 16, 2024
- [SDR COEA2025081904734](https://openairdocs.org/sdr/COEA2025081904734.md): Support · cracked · Aug 11, 2025 · N734FX · Textrn 408 · Fuselage Miscellaneous Structure
  > CAPTAIN SEAT L/H BOTTOM SUPPORT CRACKED. REPLACED WITH NEW SEAT REF. C408 MM 25-10-05.
- [SDR COEA2025081903708](https://openairdocs.org/sdr/COEA2025081903708.md): Pan · cracked · Aug 11, 2025 · N708FX · Textrn 408 · Flight Compartment Equipment
  > CAPTAIN SEAT SUPPORT PAN CRACKED. MAINTENANCE REPLACED THE CREW SEAT IAW 408 MM 25-10-05.
- [SDR COEA2025080702708](https://openairdocs.org/sdr/COEA2025080702708.md): Fuel Filter · faulted · Aug 7, 2025 · N708FX · Textrn 408 · Aircraft Fuel Distribution System
  > FLT 8737 GEG-YKM AIR TURNBACK NO EMERGENCY DECLARED. FUEL BYPASS LIGHT TURNED ON DURING CLIMB. MAINTENANCE REPLACED BOTH FUEL HEATER FILTERS. LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR COEA2025081905738](https://openairdocs.org/sdr/COEA2025081905738.md): Seat · cracked · Aug 5, 2025 · N738FX · Textrn 408 · Flight Compartment Equipment
  > PILOT SEAT CRACKED. MAINTENANCE REPLACED THE PILOT SEAT.

Next page: https://openairdocs.org/model/textron-408/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 = '408'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/textron-408/reports

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