Turbine Aircraft Chocks
Item #:CK TURBINE
MPN #:W88-YRC36
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10+ Quick Facts:
Heavy-Duty Design: Each chock measures 24" x 7" x 5.5", weighs 26 lbs. (52 lbs. per pair), and is built from industrial-grade rubber to withstand the force of turbine-powered aircraft.
Reliable Stability: Angled to fit aircraft tires and connected by a 36" heavy-duty rope for secure positioning and easy handling.
Built for Harsh Conditions: Resists shifting, weather, fuel, and wear—ideal for flight lines, hangars, and busy Air Operations Areas (AOA).
- In Stock - Ships Tomorrow
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Quantity
1-4Quantity
5-9Quantity
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$101.95
$91.75![regular price]()
$96.85
$91.75$91.75
ShareAircraft Rubber Wheel Chocks – Heavy-Duty, Turbine-Grade Security
When it comes to securing turbine-powered aircraft, compromise is not an option. Our premium Aircraft Rubber Wheel Chocks are engineered for maximum reliability, durability, and performance—built specifically for the unique demands of jet and turboprop operations.
Each chock measures 24" long x 7" wide x 5.5" tall and weighs a solid 26 lbs (52 lbs per pair), offering a heavy, grounded presence that resists shifting under the powerful thrust of turbine engines. Molded from ultra-dense, industrial-grade rubber, these chocks grip the tarmac with confidence, even in extreme weather conditions.
The set is connected by a 36" heavy-duty rope, ensuring consistent spacing and easy handling during deployment and removal. The angled design perfectly contours to aircraft tires, preventing rolling or movement during fueling, loading, or extended parking.
Whether you're operating on the flight line, in a hangar, or at a remote airstrip, these chocks deliver the steadfast protection your aircraft demands. Engineered for aviation professionals, trusted in every takeoff and touchdown.
Key Features:
Designed for turbine-powered aircraft
Massive 26 lb. weight per chock (52 lbs. per pair) for superior holding power
Heavy-duty 24" x 7" x 5.5" dimensions
Durable 36" connecting rope for stability and convenience
Industrial-grade rubber resists weather, fuel, and wear
Protect your aircraft. Secure your investment. Trust the chocks built for the jet age.
(PDF) Aircraft Wheel Chock Selection Guide
| Aircraft Model | Wheel Diameter (in) | Minimum Recommended Chock Height (in) |
|---|---|---|
| Gulfstream GII/GIII/GIV | 34.0 | 8.5 |
| Learjet 31/35 | 17.5 | 4.4 |
| Learjet 45 | 18.0 | 4.5 |
| King Air 200/350 | 22.0 | 5.5 |
| Dash 8 Q400 | 32.0 | 8.0 |
| Cessna 208 Caravan | 29.0 | 7.2 |
| Pilatus PC-12 | 26.0 | 6.5 |
| HondaJet HA-420 | 17.0 | 4.2 |
| Embraer Phenom 100 | 18.0 | 4.5 |
| Embraer Phenom 300 | 19.0 | 4.8 |
| Cessna Citation CJ3 | 18.0 | 4.5 |
| Cessna Citation XLS+ | 22.0 | 5.5 |
| Cessna Citation Latitude | 24.0 | 6.0 |
| Dassault Falcon 2000 | 30.0 | 7.5 |
| Dassault Falcon 900 | 32.0 | 8.0 |
| Bombardier Challenger 300 | 30.0 | 7.5 |
| Bombardier Global 6000 | 34.0 | 8.5 |
| Dassault Falcon 7X | 32.0 | 8.0 |
| Dassault Falcon 8X | 32.0 | 8.0 |
| Bombardier Challenger 650 | 30.0 | 7.5 |
| Bombardier Global 7500 | 34.0 | 8.5 |
| Embraer Legacy 450/500 | 30.0 | 7.5 |
| Embraer Praetor 500/600 | 30.0 | 7.5 |
| Beechcraft Denali | 24.0 | 6.0 |
| Piaggio P.180 Avanti | 22.0 | 5.5 |
| Cessna Citation M2 | 17.0 | 4.2 |
| Cessna Citation Mustang | 17.0 | 4.2 |
| Cessna 172 Skyhawk | 15.0 | 3.8 |
| Cessna 182 Skylane | 16.0 | 4.0 |
| Cessna 206 Stationair | 17.0 | 4.2 |
| Piper PA-28 Cherokee | 15.0 | 3.8 |
| Piper PA-32 Saratoga | 16.0 | 4.0 |
| Beechcraft Bonanza | 16.0 | 4.0 |
| Mooney M20 | 14.0 | 3.5 |
| Cirrus SR20 | 14.0 | 3.5 |
| Cirrus SR22 | 14.0 | 3.5 |
| Diamond DA40 | 14.0 | 3.5 |
| Diamond DA42 | 15.0 | 3.8 |
* General industry guidelines suggest that the height of a wheel chock should be approximately 25% of the tire's diameter. Consult your aircraft's Pilot's Operating Handbook (POH) to confirm the correct size for your aircraft. Disclaimer:The information presented in this chart is provided for informational purposes only. While we strive for accuracy, we make no representations or warranties, express or implied, regarding the completeness, accuracy, reliability, or suitability of the information contained herein. By viewing or using this chart, the user acknowledges and agrees that they assume all risk associated with its use. We expressly disclaim any and all liability for any loss or damage arising from reliance on the information presented. | ||
