STANAG 3218 : 86 AMD 2
Withdrawn
Withdrawn
LOCATION, ACTUATION AND SHAPE OF ENGINE CONTROLS AND SWITCHES
Published date
01-12-2013
Publisher
Withdrawn date
06-21-1999
Sorry this product is not available in your region.
Standardizes the location, actuation and shape of all engine controls and switches in fixed and rotary-wing aircraft.
| DocumentType |
Standard
|
| PublisherName |
NATO
|
| Status |
Withdrawn
|
| DEFSTAN 00-970(PT7)SEC1/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 1: GENERAL AND OPERATIONAL REQUIREMENTS |
| DEFSTAN 00-970(PT0)/3(2003) : 2003 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT7)SEC1/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 1: GENERAL AND OPERATIONAL REQUIREMENTS |
| DEFSTAN 00-970(PT7)SEC1/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 1: GENERAL AND OPERATIONAL REQUIREMENTS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT7)SEC2/SUPPD/4(2014) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT D: DESIGN AND CONSTRUCTION (SUBPART D) |
| STANAG 3705 : 0 | HUMAN ENGINEERING DESIGN CRITERIA FOR CONTROLS AND DISPLAYS IN AIRCREW STATIONS |
| DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
| STANAG 7096 : 0 | LOCATION, ACTUATION AND SHAPE OF AIRFRAME CONTROLS |
| STANAG 3692 : 76 AMD 4 | LOCATION AND ACTUATION OF THRUST VECTOR CONTROLS FOR VSTOL AIRCRAFT OTHER THAN ROTARY WING AIRCRAFT |
| DEFSTAN 16-24/1(1983) : 1983 | SHAPES OF AIRFRAME AND ENGINE CONTROL HANDLES AND KNOBS IN FIXED WING AIRCRAFT |
| STANAG 3217 : 2006 | OPERATION OF CONTROLS AND SWITCHES AT AIRCREW STATIONS |
| STANAG 3341 : 72 AMD 6 | EMERGENCY CONTROL COLOUR SCHEMES |
| STANAG 3593 : 1997 | NUMBERING OF ENGINES AND THEIR ASSOCIATED CONTROLS AND DISPLAYS IN AIRCRAFT |
| STANAG 3219 : 0 | LOCATION AND GROUPING OF ELECTRICAL SWITCHES IN AIRCRAFT |
Summarise
Sorry this product is not available in your region.