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ICAO CIRCULAR 324 - GUIDELINES FOR LATERAL SEPARATION OF ARRIVING AND DEPARTING AIRCRAFT ON PUBLISHED ADJACENT INSTRUMENT FLIGHT PROCEDURES - FIRST EDITION Organization: ICAO
Date: 2010-01-01
Description: The material in this circular is limited to the application of: a) lateral separation minima for arriving and/or departing aircraft being separated on published IFPs; b) lateral separation minima between aircraft on published adjacent IFPs (SID, STAR, IAP, including holding patterns); and c) lateral separation minima for use primarily in terminal areas where procedural control is exercised.
FAA - FO JO 7110.316 - REDUCED WAKE TURBULENCE SEPARATION ON DEPARTURE FROM HEAVY/B757 AIRCRAFT DEPARTING PARALLEL RUNWAYS, SPACED LESS THAN 2,500 FEET, USING WAKE TURBULENCE MITIGATION FOR DEPARTURES (WTMD) Organization: FAA
Date: 2013-01-28
Description: This order describes equipment and conditions that allow aircraft departing from the upwind runway of a pair of Closely Spaced Parallel Runways (CSPR) to depart after a Heavy/B757 aircraft departing the downwind runway without applying wake turbulence separation standards specified in Federal Aviation Administration (FAA) Order JO 7110.65.
ESDU 93026 - VORTEX GENERATORS FOR CONTROL OF SHOCK-INDUCED SEPARATION. PART 3: EXAMPLES OF APPLICATIONS OF VORTEX GENERATORS TO AIRCRAFT. Organization: ESDU
Date: 1995-02-01
Description: The examples are the control of internal noise by the application of vortex generators on the forward cabin roof of a business aircraft (Gulfstream III), the control of separation associated with a three-shock pattern near the tip of a highly swept and tapered model wing in a wind-tunnel, and the improvement of the buffet manoeuvre boundary on a straight wing interceptor aircraft of the fifties (Avro Canada CF-100).
FAA - AD 96-CE-27 - SEPARATION OF THE STABILONS FROM THE AIRPLANE\BEECH AIRCRAFT\1900D\BEECH AIRCRAFT\1900D Organization: FAA
FAA - AD 98-02-07 - PREVENT COUNTERWEIGHT CLAMP BOLT FAILURE, WHICH CAN RESULT IN PROPELLER BLADE COUNTERWEIGHT SEPARATION AND DAMAGE TO THE PROPELLER AND AIRCRAFT\HARTZELL PROPELLER INC\HC-E4A-3 Organization: FAA
FAA - AD 98-02-08 - PREVENT CRANKSHAFT FAILURE, WHICH CAN RESULT IN ENGINE FAILURE, PROPELLER SEPARATION, FORCED LANDING, AND POSSIBLE DAMAGE TO THE AIRCRAFT\TEXTRON LYCOMING AVCO CORP\320 SERIES Organization: FAA
FAA - AD 95-CE-62 - SEPARATION OF THE EXHAUST SYSTEM ENDPIPE FROM THE MUFFLER\HOAC AUSTRIA (FORMERLY HOFFMANN AIRCRAFT)\DV-20 'KATANA' Organization: FAA
FAA - FO N JO 7110.685 - CHANGE TO FAA ORDER JO 7110.65. THE PROCEDURES IN THIS GENOT ESTABLISH INTERIM WAKE TURBULENCE SEPARATION CRITERIA FOR THE AIRBUS INDUSTRIES A400 AIRCRAFT AND SUPPLEMENT PROCEDURES CONTAINED IN FAA ORDER JO 7110.65 Organization: FAA
Date: 2015-03-26
NTIS AD887565 - SEPARATION CHARACTERISTICS OF THE PAVE STORM I AND II FROM THE F-4C AIRCRAFT AT MACH NUMBERS FROM 0.50 TO 0.95 Organization: NTIS
JAA LEAFLET 6 - GUIDANCE MATERIAL ON THE APPROVAL OF AIRCRAFT AND OPERATORS FOR FLIGHT IN AIRSPACE ABOVE FLIGHT LEVEL 290 WHERE A 300M (1,000 FT) VERTICAL SEPARATION MINIMUM IS APPLIED Organization: JAA
FAA - AD 97-NM-146 - PREVENT SEPARATION OF THE TAILPLANE (HORIZONTAL STABILIZER) FROM THE FIN, WHICH COULD LEAD TO REDUCED CONTROLLABILITY OF THE AIRPLANE\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101 Organization: FAA
FAA - FO N JO 7110.679 - SPECIAL VFR (SVFR) SEPARATION Organization: FAA
Date: 2014-10-01
Description: This notice clarifies separation standards to be used between Special VFR fixed wing aircraft, Special VFR Helicopters, and IFR aircraft.
FAA - FO N JO 7110.728 - SAME RUNWAY SEPARATION, WAKE TURBULENCE SEPARATION FOR INTERSECTION DEPARTURES, INTERSECTING RUNWAY/INTERSECTING FLIGHT PATH OPERATIONS, AND RADAR SEPARATION MINIMA Organization: FAA
Date: 2016-12-15
Description: This notice adds a parallel runway centerline separation requirement for small aircraft departing behind B757 aircraft to Federal Aviation Administration (FAA) Order JO 7110.65, Air Traffic Control, Paragraph 3-9-6, Same Runway Separation, and Paragraph 3-9-7, Wake Turbulence Separation for Intersection Departures; relocates the separation requirement for aircraft departing parallel runways separated by 2,500 feet or more from Paragraph 3-9-8 to Paragraph 3-9-6; makes editorial corrections to Paragraphs 3-9-6, 3-9-8, 3-9-9, and 3-9-10; and modifies the notes to Paragraph 5-5-4, Minima, Subparagraph g.3.
FAA - FO N JO 7110.666 - WAKE TURBULENCE SEPARATION FOR INTERSECTION DEPARTURES Organization: FAA
Date: 2014-04-24
Description: This notice amends FAA Order JO 7110.65, paragraph 3-9-7, Wake Turbulence Separation for Intersection Departures, by removing the requirement for controllers to ensure that visual separation/visual spacing exists between aircraft operating in a VFR tower pattern.
ICAO CIRCULAR 322 - GUIDELINES FOR THE IMPLEMENTATION OF GNSS LATERAL SEPARATION MINIMA BASED ON VOR SEPARATION MINIMA Organization: ICAO
Date: 2014-01-01
Description: It is aimed at a worldwide audience within the civil aviation authorities responsible for implementing this and other separation minima. As a result of the large number of aircraft equipped with instrument flight rules (IFR) GNSS equipment for navigation and its potential use for separation in the procedural environment, the Separation and Airspace Safety Panel (SASP) developed the separation minima detailed in this document for interim use in the transition period to widespread implementation of performance-based navigation (PBN).
ICAO CIRCULAR 334 - GUIDELINES FOR THE IMPLEMENTATION OF LATERAL SEPARATION MINIMA Organization: ICAO
Date: 2014-01-01
Description: This circular is limited to the application of lateral separation of aircraft operating on intersecting or nonintersecting tracks in a procedural control environment applying area navigation.
ICAO CIRCULAR 321 - GUIDELINES FOR THE IMPLEMENTATION OF GNSS LONGITUDINAL SEPARATION MINIMA Organization: ICAO
Date: 2010-01-01
Description:   It is aimed at a worldwide audience within the civil aviation authorities responsible for implementing these and other separation minima. As a result of the large number of aircraft equipped with instrument flight rules (IFR)- certified GNSS equipment for navigation and its potential use for separation in the procedural environment, the Separation and Airspace safety Panel (SASP) developed the separation minima detailed in this circular for interim use in the period of transition to a widespread implementation of performance-based navigation (PBN).
ICAO CIRCULAR 341 - GUIDELINES FOR THE IMPLEMENTATION OF LATERAL SEPARATION MINIMA Organization: ICAO
Date: 2015-01-01
Description: PURPOSE This circular provides guidance for the implementation of lateral separation minima intended for the separation of aircraft approved for performance-based navigation (PBN) and/or global navigation satellite system (GNSS) operations.
SAE ARP5108 - HUMAN INTERFACE CRITERIA FOR TERRAIN SEPARATION ASSURANCE DISPLAY TECHNOLOGY Organization: SAE
Date: 2012-06-01
Description: Although the system functionality assumed for this document exemplifies commercial aircraft implementation, the recommendations do not exclude other fixed wing aircraft implementation, the recommendations do not exclude other fixed wing aircraft types.
NASA-LLIS-1122 - LESSONS LEARNED – AERO-SPACE TECHNOLOGY/X-34 IN-FLIGHT SEPARATION FROM L-1011 CARRIER Organization: NASA
Date: 1999-02-01
Description: Description of Driving Event: Validation of Flight Software for X-34 and L-1011 Carrier Aircraft Flight Separation

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