Standard
FERRULE-HIGH ALTITUDE SPARK PLUG LEADS
1992-12-01
CURRENT
ARP457A
Search Results
Standard
TERMINAL WELL, LOW VOLTAGE IGNITER PLUG
1992-12-01
CURRENT
ARP295
Standard
Spark Plugs, Aircraft Engine - 18mm Short Reach Shielded
1992-12-01
CURRENT
AS299
Standard
Terminal, High Altitude, Socket Contact
2002-07-23
CURRENT
ARP296
Standard
Magnetos, Aircraft, Mountings For
1997-04-01
CURRENT
AS12
This specification covers three types of flanges for magneto mountings as follows: 1. Two-bolt Flange, 2. Three-bolt Flange, and 3. Four-bolt Flange.
Standard
Magnetos, Aircraft, Installation Of
1991-07-01
CURRENT
AS14
This Aerospace Standard establishes the diameter - pitch combinations of ISO metric 60 screw threads recommended for use in the aerospace industry for metric module shaft of bearing retaining screw threads.
Standard
GASKET - 18MM FOLDED STEEL AIRCRAFT
1960-08-01
HISTORICAL
AS678
Standard
GASKET - 18 MM FOLDED STEEL AIRCRAFT
1963-04-01
HISTORICAL
AS678A
Standard
GASKET-18MM FOLDED STEEL AIRCRAFT
1981-03-01
HISTORICAL
AS678B
Standard
HIGH TENSION EXCITER OUTPUT VOLTAGE MEASUREMENT USING CATHODE-RAY OSCILLOSCOPE
1994-06-01
CURRENT
AIR1092
Standard
LOW TENSION SPARK IGNITER SPARKING VOLTAGE TEST
1992-11-01
CURRENT
ARP846
These specifications contain general information pertaining to the sparking voltage parameter of shunted surface gap spark igniters; test equipment circuitry; bill of materials for test equipment; test equipment operation.
Standard
LEADS, SHIELDED, HIGH TENSION, DETACHABLE SPARK PLUG
1992-12-01
CURRENT
ARP489A
This specification establishes the requirements for shielded, detachable high tension spark plug leads for reciprocating engines.
Standard
IGNITION SYSTEM TESTING - METERING AND POWER SUPPLIES
1976-11-15
HISTORICAL
ARP504B
This procedure establishes the ignition system power supply design parameters for aeronautical engine ignition system testing.
Standard
IGNITION SYSTEM TESTING - METERING AND POWER SUPPLY REGULATION
1971-06-15
HISTORICAL
ARP504A
This specification establishes the ignition system power supply design parameters for aeronautical engine ignition systems.
Standard
IGNITION SYSTEM TESTING - METERING AND POWER SUPPLIES
1994-07-01
CURRENT
ARP504C
This procedure establishes the ignition system power supply design parameters for aeronautical engine ignition system testing.
Standard
GAP SETTINGS FOR AIRCRAFT PISTON ENGINE SPARK PLUGS
1981-03-01
HISTORICAL
ARP716B
Standard
GAP SETTINGS FOR AIRCRAFT PISTON ENGINE SPARK PLUGS
1994-07-01
CURRENT
ARP716C
Standard
GAP SETTINGS FOR AIRCRAFT PISTON ENGINE SPARK PLUGS
1962-06-30
HISTORICAL
ARP716
Standard
GAP SETTINGS FOR AIRCRAFT PISTON ENGINE SPARK PLUGS
1963-08-01
HISTORICAL
ARP716A
Standard
LEADS, FLEXIBLE, SHIELDED, HIGH ENERGY IGNITION
1994-07-01
CURRENT
ARP841A
This specification establishes the requirements for shielded, flexible, high energy ignition leads for gas turbine engines.
