|
10-5 |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-17 |
Pull-type master cylinders are a great choice when the aircraft’s linkage is not set up for a push-type master cylinder due to cockpit design constraints or the air framer’s preference. Cleveland’s pull-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-19 |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-22 |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-23A |
Pull-type master cylinders are a great choice when the aircraft’s linkage is not set up for a push-type master cylinder due to cockpit design constraints or the air framer’s preference. Cleveland’s pull-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-24D |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-30 |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-30C |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-35 |
Pull-type Reservoir master cylinders incorporate the reservoir into the body of the valve to eliminate the need for an additional reservoir and the associated plumbing. Our master cylinders utilize hardened steel rods, aluminum housings, and pistons that have low seal friction, which means they are designed for long, reliable service life. |
|
10-54 |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-55A |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-55B |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-69 |
Pull-type Reservoir master cylinders incorporate the reservoir into the body of the valve to eliminate the need for an additional reservoir and the associated plumbing. Our master cylinders utilize hardened steel rods, aluminum housings, and pistons that have low seal friction, which means they are designed for long, reliable service life. |
|
10-73 |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-75 |
Pull-type master cylinders are a great choice when the aircraft’s linkage is not set up for a push-type master cylinder due to cockpit design constraints or the air framer’s preference. Cleveland’s pull-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
10-100 |
Pull-type master cylinders are a great choice when the aircraft’s linkage is not set up for a push-type master cylinder due to cockpit design constraints or the air framer’s preference. Cleveland’s pull-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
010-05101 |
Push-type master cylinders are the most common type of master cylinder. The aircraft’s brake pedal linkage is set up to push the rod of the master cylinder to engage the brake discs. Cleveland’s push-type master cylinders have been designed with hardened steel rods, aluminum housings, and pistons that have low seal friction for a long, reliable service life. |
|
11-16 |
Utility actuators are used for the movement of structures that do not require precise mid-position control, while still providing reliability and safety features. |
|
11-17 |
Utility actuators are used for the movement of structures that do not require precise mid-position control, while still providing reliability and safety features. |
|
11-22 |
Utility actuators are used for the movement of structures that do not require precise mid-position control, while still providing reliability and safety features. |
|
15-8 |
Shimmy damper is a hydraulic fluid-filled cylinder that prevents rapid movement of the nose or main landing gear without interfering with slower operations. |
|
15-9 |
Shimmy damper is a hydraulic fluid-filled cylinder that prevents rapid movement of the nose or main landing gear without interfering with slower operations. |
|
15-10 |
Shimmy damper is a hydraulic fluid-filled cylinder that prevents rapid movement of the nose or main landing gear without interfering with slower operations. |
|
015-00100 |
Shimmy damper is a hydraulic fluid-filled cylinder that prevents rapid movement of the nose or main landing gear without interfering with slower operations. |
|
30-6 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-9 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-9C |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-9D |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-9E |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-18 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-19 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-19A |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-23 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-23B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-23C |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-23D |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-28B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-28C |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-28D |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-30 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-31 |
The Internal Dual Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-32B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-32C |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-32E |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-40 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-41B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-51A |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-51B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52A |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52AA LH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52AA RH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52AB |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52AC LH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52AC RH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52E |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52F |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52H LH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52H RH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52K |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52L |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52M |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52N |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52P |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52Q |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52T |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52U |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52V LH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52V RH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52W |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52Z LH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-52Z RH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-53A LH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-53A RH |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-54 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-54A |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-54B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-54C |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-55 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-55B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-56A |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-56B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-56D |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-56F |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-59 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-59A |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-59D |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-59E |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-60A |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-60B |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-61 |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-61D |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-61E |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-63A |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-63E |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-63J |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-63K |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-63M |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
|
30-63P |
The External Single Caliper brake assembly and disc combination are designed, and qualification tested to decelerate the aircraft properly and safely during landing. The brake assembly consists of one or more pistons depending upon the aircraft requirements. |
