Search Results

Standard

BOLTS, SCREWS AND STUDS, SCREW THREAD REQUIREMENTS

1977-04-01

HISTORICAL

AS3062B

This standard establishes the rolled thread element tolerances for lead, half-angle, taper, and out-of-roundness for studs used in aerospace construction; it also establishes the requirements for lead threads and runout threads for these studs.

Standard

BOLTS, SCREWS AND STUDS, SCREW THREAD REQUIREMENTS

1974-08-01

HISTORICAL

AS3062A

Standard

DEFINITIONS, AIRCRAFT ENGINE

1941-11-01

HISTORICAL

AS20

Standard

DEFINITIONS, AIRCRAFT RECIPROCATING ENGINE PERFORMANCE

1950-04-15

HISTORICAL

AS20A

Standard

DEFINITIONS, AIRCRAFT RECIPROCATING ENGINE PERFORMANCE

1960-03-01

HISTORICAL

AS20B

Standard

Definitions, Aircraft Reciprocating Engine Performance

2018-06-20

CURRENT

AS20D

This document lists definitions that are commonly used in describing aircraft reciprocating engine performance.

Standard

Definitions, Aircraft Reciprocating Engine Performance

2012-11-01

HISTORICAL

AS20C

This document lists definitions that are commonly used in describing aircraft reciprocating engine performance.

Standard

Engines, Aircraft, Reciprocating, General Specification For

2018-06-18

CURRENT

AS25109A

This specification covers standard requirements for reciprocating aircraft engines.

Standard

Engines, Aircraft, Reciprocating, General Specification For

2012-11-01

HISTORICAL

AS25109

This specification covers standard requirements for reciprocating aircraft engines.

Standard

FINAL REPORT ON COLD STARTING OF AIRCRAFT ENGINES

1946-09-01

HISTORICAL

AIR13

Standard

GAGING PRACTICE AND GAGE REQUIREMENTS FOR MJ METRIC SCREW THREADS

1980-08-15

HISTORICAL

MA1566

The gaging practice established in this standard applies for final assessment of dimensional acceptability of the product complete thread (excluding the incomplete lead or runout thread). However, it is not the intent of this standard to preclude the use of other gaging systems or dimensional control systems provided they are properly correlated by the user and yield comparable results with respect to conformance with the requirements of ANSI B1.21M-1978, MJ metric screw threads.

Standard

GENERAL PRACTICES FOR USE OF LOCK WIRE, KEY WASHERS, AND COTTER PINS

1976-07-01

HISTORICAL

AS567E

This standard covers those devices whose primary function is locking, and excludes those devices which have integral locking features incorporated into the item being locked.

Standard

GENERAL PRACTICES FOR USE OF LOCK WIRE, KEY WASHERS, AND COTTER PINS

1980-01-01

HISTORICAL

AS567F

This standard covers those devices whose primary function is locking, and excludes those devices which have integral locking features incorporated into the item being locked.

Standard

GENERAL PRACTICES FOR USE OF LOCK WIRE, KEY WASHERS, AND COTTER PINS

1966-05-25

HISTORICAL

AS567C

This standard covers those devices whose primary function is locking, and excludes those devices which have integral locking features incorporated into the item being locked.

Standard

GENERAL PRACTICES FOR USE OF LOCK WIRE, KEY WASHERS, AND COTTER PINS

1969-08-15

HISTORICAL

AS567D

This standard covers those devices whose primary function is locking, and excludes those devices which have integral locking features incorporated into the item being locked.

Standard

HUB, FLANGED - SPLINE TYPE WOOD PROPELLER - #10, #20

2006-05-11

HISTORICAL

ARP381A

Standard

HUB, FLANGED - SPLINE TYPE WOOD PROPELLER - #10, #20

2013-02-05

CURRENT

ARP381B

Standard

HUB, FLANGED - SPLINE TYPE WOOD PROPELLER - #10, #20

1949-02-01

HISTORICAL

ARP381

Standard

Horsepower Correction Formulae

2018-08-09

CURRENT

ARP2C

This document discusses formulae considered applicable to aircraft engines having integral supercharging without aftercooling, and using gasoline introduced at the entrance to the supercharger or directly into the cylinders. Such engines are normally designated as single and two speed engines. Correction formulae for engines having two stage or exhaust turbo supercharging will not be discussed. Corrections for engines having a high degree of integral supercharging will be discussed in general terms only and no specific formulae will be presented. The correction formulae and methods listed are empirical and subject to error due to conditions beyond the scope of known corrections. Usage has indicated, however, that the correction formulae listed will provide a satisfactory approximation of power output under standard conditions.

Standard

Horsepower Correction Formulae

2012-11-02

HISTORICAL

ARP2B

This document discusses formulae considered applicable to aircraft engines having integral supercharging without aftercooling, and using gasoline introduced at the entrance to the supercharger or directly into the cylinders. Such engines are normally designated as single and two speed engines. Correction formulae for engines having two stage or exhaust turbo supercharging will not be discussed. Corrections for engines having a high degree of integral supercharging will be discussed in general terms only and no specific formulae will be presented. The correction formulae and methods listed are empirical and subject to error due to conditions beyond the scope of known corrections. Usage has indicated, however, that the correction formulae listed will provide a satisfactory approximation of power output under standard conditions.