SAE AS81366A
Current
The latest, up-to-date edition.
Boundary Layer Control System; Pressure
Hardcopy , PDF
English
02-07-2004
Important note : Users cannot be edited or removed once added to your Multi user PDF.
NOTICE
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY (NOT APPLICABLE)
6 NOTES
Covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.
| DocumentType |
Standard
|
| Pages |
7
|
| PublisherName |
SAE International
|
| Status |
Current
|
This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.
| MIL-B-81365 Base Document:1966 | BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.