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Repair Apron & Trench Drain and Install Mooring Points
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McCONNELL AIR FORCE BASE, REPAIR APRON & TRENCH

SHEET INDEX to DRAWINGS

VICINITY MAPS

WICHITA KANSAS

LOCATION MAP

RE

PA

IR

A

PR

ON

T

RE

NC

H

SECURITY FORCES

(BUILDING 1115)

(BUILDING 948)

BASE CIVIL ENGINEER

BASE CONTRACTING

(BUILDING 732 AND/OR 1127)

(BUILDING 173)

MAIN GATE - PASS & ID

(BUILDING 60)

WEST COMMERCIAL GATE

McCONNELL AFB

WICHITA

US 54

DODGE CITY

McCONNELL AFB

OKLAHOMA

WICHITA

EMPORIA

PITTSBURG

HAYS

GOODLAND

SALINA

NEBRASKA

KANSAS CITY

TOPEKA

Previous Edition ObsoleteAMC 71FEB 01

FORM A

CB D

A CB D

C h i e f

E n g i n e e r i n g

C h i e f

C o n t r a c t s

C h i e f

O p e r a t i o n s

McCONNELL AIR FORCE BASE

ANNUAL CHANGE 12' EAST

MAG. DEC. 6 48'

SCALE IN FEET

1200 2400

FE G

P R

O J E

C T

T

I T

L E

L

A

H

F

S

P

R

O

E

E

N

S

S

I

O

L

A

B a s e

C i v i l

E n g i n e e r

U s i n g

A g e n c y

P r i n c i p a l

A

E

F i r m

D a t e

D a t e

D a t e

FE G

C h i e f

B i o

E n v i r o n m e n t a l

C h i e f

E n v i r o n m e n t a l

O t h e r

C h i e f

M a i n t

E n g i n e e r i n g

C h i e f

F i r e

P r o t e c t i o n

W i n g

S a f e t y

D a t e

D a t e

D a t e

D a t e

D a t e

D a t e

D a t e

D a t e

D a t e

H

C02 DETAILS

C03 DETAILS

C01 PHASING PLAN

DRAIN

DR

AI

N

- M

CC

ON

NE

LL

A

FB

McCONNELL AFB

SEE A

A

FWDUPPER DRAG STRUT

FORWARD LOCK LINK

LOWER DRAG STRUT

SHOCK STRUT

120 INCHES

(3048 mm)

30 ˚

TIE-DOWN

STRAP

DIMENSIONS ARE IN INCHES,

MILLIMETER ARE IN PARENTHESES

NOTE:____

2487192 S0000585612_V1

Nose Gear Tiedown Straps Figure 202/10-11-03-990-803

KC-46

AIRCRAFT MAINTENANCE MANUAL

10-11-03

D633T1C8 Mar 29/2016 BOEING COMMERCIAL PROPRIETARY INFORMATION - OMIT LICENSE RIGHTS. Use or disclosure is subject to the restriction(s) on the title page.

Copyright 2012 - All Rights Reserved - Unpublished Work. EXPORT CONTROLLED

EFFECTIVITY

ZRS ALL

UFC 3-260-01

17 NOVEMBER 2008

B11-5 AIR FORCE TIEDOWNS AND STATIC GROUNDS

B11-5.1 General. For the Air Force, tiedowns will be constructed in accordance with Figures B11-14 and B11-15 and may be used as a static ground provided they meet the requirements given in paragraph B11-5.4. For maximum flexibility, they may be installed in 4.6-meter (15-foot), 6.1-meter (20-foot), or 9.1-meter (30-foot) grids, or offset grids. At minimum, place tiedowns as indicated in aircraft Technical Orders or Facility Requirements Documents. Ideally, tiedowns will be centered in slabs, but, at minimum, shall not be located less than 914 millimeters (3 feet) from any joint.

B11-5.1.1 If tiedowns are intended to also be used as static grounds, soil conditions may require that a ground rod be installed. When a ground rod is included, bond it to the tiedown bar.

B11-5.1.2 Static grounding points will be installed using a minimum 3-meter (10-foot) rod with a closed eye. The 3-meter (10-foot) rod will have a diameter of not less than 19 millimeters (0.75 inch) and the top will be a closed forged eye or a shepherd's hook bend with clamped sleeve, having an inside diameter of not less than 40 millimeters (1.5 inches) (see Figure B11-12). The rod may be copper, copper-clad steel, galvanized steel, or copper-zinc-silicone alloy. The Air Force static ground is used only as a static ground, not an electrical ground, and is not designed to withstand the uplift forces imposed for mooring aircraft. On aprons, stencil the pavement near each static ground with the legend "Static Ground Only" in 102-millimeter (4- inch) block letters. Black lettering on a yellow background that extends a minimum of 51 mm (2 in) beyond the outermost edges of the letters is recommended.

B11-5.1.3 Inside hangars, Air Force activities may use the Army static ground fixture shown in Figure B11-9. All static ground fixtures inside hangars must be connected to the building ground and all grounds must be bonded.

B11-5.2 Layout. Static grounds and tiedowns will be configured and spaced in accordance with the requirements of the mission aircraft and will vary from aircraft to aircraft. An example of a multiple fixed-wing aircraft tiedown layout is shown in Figure B11-13.

Figure B11-12. Air Force Static Ground

19mm

19mm

5m m m m m m

[4

/2

A P

P R

O X

DETAIL OF EYE AND

SLEEVE ASSEMBLY 127mm [5"] DIA. MIN.

PAVEMENT

150mm [6"] MAX.

5m m

A A

B

B

APPROX. 80mm [3-1/4"] R.

ANCHOR

ANCHOR

EDGES ROUNDED

SECTION A

SECTION

B

DETAIL OF PAVEMENT RECESS

FOR CONCRETE

[3/4"] R

[3/4"] R

[1

[1

/2

[3

38 mm [1.5"]

THREADED OR

WELDED SCREW

ANCHOR FOR

FLEXIBLE PAVEMENT

SHEPHERDS HOOK

OR FORGED EYE

19mm [3/4"] MIN DIAMETER x 3,000mm [10'] COPPER, COPPER

CLAD STEEL, GALVANIZED

STEEL, OR

COPPER-ZINC-SILICONE ALLOY

COPPER COMPRESSION

SLEEVE FOR SHEPHERDS

HOOK STYLE ROD ENDS

NOTES

1. STATIC TIEDOWN GROUNDS ARE NOT INTENDED

AS AIRCRAFT TIEDOWNS OR THRUST ANCHORS.

2. THESE WILL BE USED AS EXTERIOR STATIC

GROUND POINTS FOR ARMY ROTARY WING

AIRCRAFT.

Figure B11-13. Example of Air Force Multiple Tiedown Layout for Fixed-Wing Aircraft

6m [20']

18m [60']

6m [20']

17m [56']

9m

3m [10']

B-1B BLAST DEFLECTOR

B-1B TIEDOWN

LOCATION

THIS IS AN EXAMPLE FOR ONE AIRCRAFT (B-1B).

FOR SPECIFIC AIRCRAFT DIMENSIONS REFERENCE

THE AIRCRAFT TECHNICAL ORDER (T.O.)

(AVAILABLE FROM MAINTENANCE ASSISTANCE

PROGRAM OFFICE).

[30']

C OF PARKING SPOTL C OF PARKING SPOTL

NOTE:

B11-5.3 Installation

B11-5.3.1 Static Grounds in Rigid Pavement. Where static grounds are to be installed in rigid pavement, the rods may be installed without bottom anchors. Static grounds should be offset a minimum of 600 millimeters (2 feet) from any pavement edge, joint, or tiedown point.

B11-5.3.2 Static Grounds in Flexible Pavements. Where flexible pavement is to be constructed, static grounding rods will be equipped with a screw-type bottom end having a wing diameter of not less than 127 millimeters (5 inches), as shown in Figure B11-12. The helical anchor may be welded to the rod or the rod may be threaded to permit attachment to the bottom anchor.

B11-5.3.3 Pavement Recess Design. The top of the static ground will be set at pavement grade or not more than 6 millimeters (0.25 inch) below grade. A smooth, rounded-edge recess 75 millimeters (3 inches) wide and not more than 150 millimeters (6 inches) long will be provided in the pavement around the eye for accessibility and attachment of grounding cables. This is shown in Figure B11-12.

Figure B11-14. Air Force Aircraft Tiedown, Profile

127mm [5"]

NOTES:

1. PLACE TIE DOWNS AS INDICATED IN AIRCRAFT TECHNICAL ORDER OR FACILITY REQUIREMENTS

DOCUMENT. IF THE TIEDOWN IS INTENDED TO ALSO BE USED AS A STATIC GROUND, SOIL

CONDITIONS MAY REQUIRE THAT A GROUND ROD BE INSTALLED. WHEN A GROUND ROD IS

INCLUDED, BOND IT TO THE TIEDOWN BAR.

2. MINIMUM DISTANCE FROM TIEDOWN CENTER POINT TO AN UNDOWELED JOINT IS 914 mm (3').

WHEN TIE DOWNS OCCUR 914mm [3 '] FROM A SINGLE JOINT, ORIENT BAR PARALLEL WITH THE JOINT. IF CENTER POINT OCCURS 914mm (3') FROM ADJACENT JOINTS, ORIENT BAR PARALLEL

WITH EITHER JOINT.

3. BAR WILL BE 32mm [1.25"] AISI 4130.

4. MINIMUM SLAB THICKNESS IS 254mm [10"].

5. PIER DIMENSIONS FOR ASPHALT PAVEMENTS MUST BE DESIGNED TO ACCOMMODATE

ANTICIPATED UPLIFT FORCES. FOR 17,100 kg (37,700 LBS) MINIMUM PIER DIMENSIONS ARE 1.83m x 1.83m x 2.13m (6' x 6' x 7').

6. FOR INSTALLATION IN PREEXISTING SLABS, INSTALL 1" Ø x 16" DOWEL RODS CENTERED AT HALF

SLAB DEPTH , ALL FOUR SIDES AS SHOWN IN THE PLAN VIEW. MINIMUM ANCHOR BLOCK

DIMENSIONS IN THIS CASE ARE 254mm [10"] x 1,067mm [42"] x 1,067mm [42"].

76mm [3"] R

146mm [5.75"]

914.4mm [36"]

254mm [10"] MINIMUM

92.25mm [3.75"]

178mm [7"] 127mm [5"] 152mm [6"]

#5 REBAR, FOUR

EACH WAY, TYP

114mm [4.5"]

DOWELS REQUIRED FOR

INSTALLATION IN PREEXISTING SLABS,

SEE NOTE 6

406mm [16"]

DOWEL

PRE-EXISTING

SLABS

Figure B11-15. Air Force Aircraft Tiedown, Plan

25mm [1"]

DOWELS

1,067mm [42"]

1,067mm [42"] 76mm [3"] MIN

305mm [12"] MIN

152mm 6"]

203 mm [8"]

203 mm [8"]

1m (3') MIN TO JOINT

1m (3') MIN TO JOINT

B11-5.4 Grounding Requirements. The maximum resistance of new static grounds, measured in accordance with IEEE Standard 81, should not exceed 10,000 ohms under normal dry conditions. If this resistance cannot be achieved, an alternative grounding system should be considered. Tiedowns that meet the above requirements may be used as static grounds.

B11-6 TIEDOWN MOORING EYES FOR NAVY AND MARINE CORPS.

Requirements, layout, and installation details for Navy and Marine Corps tiedown mooring eyes are found in Figure B11-16. Requirements, layout, and installation details for Navy and Marine Corps grounding arrangements are found in MIL-HDBK-274.

Atchmt04 RprApronAndTrenchDrains-InstallMoorPts UFC 3-260-01 TieDownMooringPtRqmts.pdf
FOREWORD
REVISION SUMMARY SHEET
CONTENTS
CHAPTER 1 GENERAL REQUIREMENTS
1-1 PURPOSE OF THIS MANUAL.
1-2 SCOPE.
1-2.1 Terminal Instrument Procedures (TERPS).
1-2.2 Objects Affecting Navigable Airspace.
1-2.3 Navigational Aids (NAVAIDS) and Lighting.
1-2.4 Vertical/Short Takeoff and Landing (V/STOL) Aircraft (V-22).
1-3 REFERENCES.
1-4 APPLICATION OF CRITERIA
1-4.1 Existing Facilities.
1-4.2 Modification of Existing Facilities.
1-4.3 New Construction.
1-4.4 Metric Application.
1-4.5 Military Activities on Civil Owned Airfields.
1-4.6 USAFE Installations.
1-5 SERVICE REQUIREMENTS.
1-6 THEATER OF OPERATIONS.
1-7 SECURITY CONSIDERATIONS FOR DESIGN.
1-7.1 Integration of Security Measures.
1-7.2 Security-Related Requirements.
1-8 WAIVERS TO CRITERIA.
1-9 USAF WORK ORDER COORDINATION AND AUTHORIZATION.
1-10 NEW RUNWAYS, EXTENDING EXISTING RUNWAYS, AND NOTICE OF CONSTRUCTION.
1-11 CONSTRUCTION PHASING PLAN.
1-12 ZONING.
1-13 ASSOCIATED DESIGN MANUALS.
Table 1-1. Associated Design Manuals
1-14 USE OF TERMS.
CHAPTER 2 AVIATION FACILITIES PLANNING
2-1 APPLICABILITY.
2-1.1 Manual Usage.
2-1.2 Terms.
2-1.3 Planning Process.
2-1.4 Planning Elements.
Figure 2-1. Aviation Facilities Planning Process
2-1.5 Guidance.
2-1.6 Additional Planning Factors.
2-1.7 Space Allowances.
2-2 JUSTIFICATION
2-2.1 Aviation Facilities Planning.
2-2.2 Number of Aircraft.
2-2.3 Joint Use Facilities.
2-3 GENERAL PLANNING CONSIDERATIONS
2-3.1 Goals and Objectives.
2-3.2 Functional Proponent.
2-3.3 Requirements.
2-3.4 Safety.
2-3.5 Design Aircraft.
2-3.6 Airspace and Land Area.
2-4 PLANNING STUDIES
2-4.1 Master Plan.
2-4.2 Land Use Studies.
2-4.3 Environmental Studies.
2-4.4 Aircraft Noise Studies.
2-4.5 Instrumented Runway Studies.
2-5 SITING AVIATION FACILITIES
2-5.1 Location.
2-5.2 Site Selection
2-5.3 Airspace Approval.
2-5.4 Airfield Safety Clearances
2-6 AIRSIDE AND LANDSIDE FACILITIES.
2-7 LANDING AND TAKEOFF AREA
2-7.1 Runways and Helipads.
2-7.2 Number of Runways.
2-7.3 Number of Helipads.
2-7.4 Runway Location.
2-7.5 Runway and Helipad Separation.
2-7.6 Runway Instrumentation.
2-8 AIRCRAFT GROUND MOVEMENT AND PARKING AREAS.
2-8.1 Taxiways.
2-8.2 Aircraft Parking Aprons.
2-9 AIRCRAFT MAINTENANCE AREA (OTHER THAN PAVEMENTS).
2-9.1 Aircraft Maintenance Facilities.
2-9.2 Aviation Maintenance Buildings (Air Force and Navy).
2-9.3 Aviation Maintenance Buildings (Army)
2-9.4 Maintenance Aprons.
2-9.5 Apron Lighting.
2-9.6 Security.
2-10 AVIATION OPERATIONS SUPPORT AREA
2-10.1 Aviation Operations Support Facilities.
2-10.2 Location.
2-10.3 Orientation of Facilities.
2-10.4 Multiple Supporting Facilities.
2-10.5 Transient Facilities.
2-10.6 Other Support Facilities.
2-10.7 Aircraft Fuel Storage and Dispensing
2-10.8 Roadways to Support Airfield Activities
2-10.9 Navy/Marine Corps Exemptions from Waivers.
CHAPTER 3 RUNWAYS (FIXED-WING) AND IMAGINARY SURFACES
3-1 CONTENTS.
3-2 REQUIREMENTS.
3-3 RUNWAY CLASSIFICATION.
3-3.1 Class A Runways.
3-3.2 Class B Runways.
3-3.3 Rotary-Wing and V/STOL Aircraft.
Table 3-1. Runway Classification by Aircraft Type
3-3.4 Landing Zones (formerly called Short Fields and Training Assault Landing Zones).
3-4 RUNWAY SYSTEMS.
3-4.1 Single Runway.
3-4.2 Parallel Runways.
3-4.3 Crosswind Runways.
Table 3-2. Runways
3-5 RUNWAY ORIENTATION/WIND DATA.
3-6 ADDITIONAL CONSIDERATIONS FOR RUNWAY ORIENTATION.
3-6.1 Obstructions.
3-6.2 Restricted Airspace.
3-6.3 Built-Up Areas.
3-6.4 Neighboring Airports.
3-6.5 Topography.
3-6.6 Soil Conditions.
3-6.7 Noise Analysis.
3-7 RUNWAY DESIGNATION.
3-8 RUNWAY DIMENSIONS.
3-8.1 Runway Dimension Criteria, Except Runway Length.
3-8.2 Runway Length Criteria
3-8.3 Layout.
Table 3-3. Army Class A Runway Lengths
Figure 3-1. Runway Transverse Sections and Primary Surface
Figure 3-2. Clear Zone Transverse Section Detail
Figure 3-3. Runway and Overrun Longitudinal Profile
Figure 3-4. Army Clear Zone and Accident Potential Zone Guidelines
Figure 3-5. Air Force Clear Zone and APZ Guidelines
Figure 3-6. Navy and Marine Corps Clear Zone and APZ Guidelines
Figure 3-7. Class A VFR Runway Primary Surface End Details
Figure 3-8. Class A VFR Runway Isometric Airspace Imaginary Surfaces
Figure 3-9. Class A VFR Runway Plan and Profile Airspace Imaginary Surfaces
Figure 3-10. Class A IFR Runway Primary Surface End Details
Figure 3-11. Class A IFR Runway Airspace Imaginary Surfaces
Figure 3-12. Class A IFR Runway Plan and Profile Airspace Imaginary Surfaces
Figure 3-13. Class B Army and Air Force Runway End and Clear Zone Details
Figure 3-14. Class B Army Runway Airspace Imaginary Surfaces
Figure 3-15. Class B Army and Air Force Runway Airspace Plan and Profile Runway Imaginary Surfaces
Figure 3-16. Class B Navy Runway Primary Surface End Details
Figure 3-17. Class B Air Force and Navy Runway Airspace Imaginary Surfaces
Figure 3-18. Class B Navy Runway Airspace Plan and Profile Runway Imaginary Surfaces
Figure 3-19. VFR and IFR Crosswind Runways Isometric Airspace Imaginary Surfaces
Figure 3-20. Plan, Single Runway, Navy Class A, and Basic Training Outlying Field
Figure 3-21. Plan, Single Runway, and Navy Class B
Figure 3-22. Typical Layout, Navy Dual Class B Runways
3-9 SHOULDERS.
3-9.1 Paved Shoulder Areas
3-9.2 Unpaved Shoulder Areas
3-10 RUNWAY OVERRUNS.
Table 3-4. Overruns
3-10.1 The Paved Portion of the Overrun
3-10.2 The Unpaved Portion of the Overrun
3-11 RUNWAY CLEAR ZONES.
3-11.1 Treatment of Clear Zones.
3-11.2 Clear Zone Mandatory Frangibility Zone (MFZ).
Table 3-5. Clear Zones
3-11.3 US Navy Clear Zones
3-12 ACCIDENT POTENTIAL ZONES (APZ).
3-13 AIRSPACE IMAGINARY SURFACES
3-13.1 Types of Airspace Imaginary Surfaces.
3-13.2 Imaginary Surfaces.
Table 3-6. Accident Potential Zones (APZs)
Table 3-7. Airspace Imaginary Surface
3-14 AIRSPACE FOR AIRFIELDS WITH TWO OR MORE RUNWAYS.
3-15 OBSTRUCTIONS TO AIR NAVIGATION.
3-15.1 Aircraft Movement Area.
3-15.2 Determining Obstructions.
3-15.3 Trees.
Table 3-8. Imaginary Surfaces Minimum Clearances over Highway, Railroad, Waterway, and Trees
3-16 AIRCRAFT ARRESTING SYSTEMS.
3-16.1 Navy and Marine Corps Requirements.
3-16.2 Installation Design and Repair Considerations.
3-16.3 Joint-Use Airfields.
3-16.4 Military Rights Agreements for Non-CONUS Locations.
CHAPTER 4 ROTARY-WING RUNWAYS, HELIPADS, LANDING LANES, AND HOVERPOINTS
4-1 CONTENTS.
4-2 LANDING AND TAKEOFF LAYOUT REQUIREMENTS.
4-3 ROTARY-WING RUNWAY.
4-3.1 Orientation and Designation.
4-3.2 Dimensions.
4-3.3 Layout.
Table 4-1. Rotary-Wing Runways
Figure 4-1. Helicopter VFR Runway
Figure 4-2. Helicopter IFR Runway
Figure 4-3. IFR Airspace Imaginary Surfaces: IFR Helicopter Runway and Helipad
4-4 HELIPADS.
4-4.1 Standard VFR Helipad.
4-4.2 Limited Use Helipad.
4-4.3 IFR Helipad.
4-4.4 Helipad Location.
4-4.5 Dimensional Criteria.
Table 4-2. Rotary-Wing Helipads and Hoverpoints
4-4.6 Layout Criteria.
4-5 SAME DIRECTION INGRESS/EGRESS.
4-5.1 Dimensions Criteria.
4-5.2 Layout Criteria.
4-6 HOVERPOINTS
4-6.1 General.
4-6.2 Hoverpoint Location.
4-6.3 Dimensions.
4-6.4 Layout.
4-7 ROTARY-WING LANDING LANES.
4-7.1 Requirements for a Landing Lane.
4-7.2 Landing Lane Location.
4-7.3 Touchdown Points.
4-7.4 Dimensions.
4-7.5 Layout.
Figure 4-4. Standard VFR Helipad for Army and Air Force
Figure 4-5. Standard VFR Helipad for Navy and Marine Corps and Limited Use VFR Helipad for Army and Air Force
Figure 4-6. Standard IFR Helipad
Figure 4-7. Army, Air Force, Navy, and Marine Corps VFR Helipad with Same Direction Ingress/Egress
Figure 4-8. Army and Air Force VFR Limited Use Helipad with Same Direction Ingress/Egress
Figure 4-9. Army and Air Force IFR Helipad with Same Direction Ingress/Egress
Figure 4-10. Helicopter Hoverpoint
Table 4-3. Rotary-Wing Landing Lanes
Figure 4-11. Rotary-Wing Landing Lane
4-8 AIR FORCE HELICOPTER SLIDE AREAS (OR “SKID PADS”).
4-9 SHOULDERS FOR ROTARY-WING FACILITIES.
Table 4-4. Shoulders for Rotary-Wing Facilities
4-10 OVERRUNS FOR ROTARY-WING RUNWAYS AND LANDING LANES.
Table 4-5. Overruns for Rotary-Wing Runways and Landing Lanes
4-11 CLEAR ZONE AND ACCIDENT POTENTIAL ZONE (APZ).
4-11.1 Clear Zone Land Use.
4-11.2 Accident Potential Zone (APZ).
4-11.3 Dimensions.
4-12 IMAGINARY SURFACES FOR ROTARY-WING RUNWAYS, HELIPADS, LANDING LANES, AND HOVERPOINTS.
Table 4-6. Rotary-Wing Runway and Landing Lane Clear Zone and APZ
Table 4-7. Rotary-Wing Imaginary Surface for VFR Approaches
Table 4-8. Rotary-Wing Imaginary Surfaces for IFR Approaches

4-13 OBSTRUCTIONS AND AIRFIELD AIRSPACE CRITERIA.

CHAPTER 5 TAXIWAYS
5-1 CONTENTS.
5-2 TAXIWAY REQUIREMENTS.
5-3 TAXIWAY SYSTEMS
5-3.1 Basic.
5-3.2 Parallel Taxiway.
5-3.3 High-Speed Taxiway Turnoff.
5-3.4 Additional Types of Taxiways.
5-3.5 Taxilanes.
5-3.6 USAF Taxitraks.
Figure 5-1. Common Taxiway Designations
5-4 TAXIWAY LAYOUT.
5-4.1 Efficiency.
5-4.2 Direct Access.
5-4.3 Simple Taxiing Routes.
5-4.4 Delay Prevention.
5-4.5 Runway Exit Criteria.
5-4.6 Taxiway Designation.
5-5 FIXED-WING TAXIWAY DIMENSIONS.
5-5.1 Criteria.
5-5.2 Transverse Cross-Section.
Figure 5-2. Spacing Requirements: Normal Taxiway Turnoffs
Table 5-1. Fixed-Wing Taxiways
Figure 5-3. Taxiway and Primary Surface Transverse Sections
5-6 ROTARY-WING TAXIWAY DIMENSIONS.
Table 5-2. Rotary-Wing Taxiways
5-7 TAXIWAYS AT DUAL USE (FIXED- AND ROTARY-WING) AIRFIELDS
5-7.1 Criteria.
5-7.2 Taxiway Shoulders.
Table 5-3. Rotary-Wing Taxiway Shoulders
5-8 TAXIWAY INTERSECTION CRITERIA.
5-8.1 Fillet-Only Dimensions.
5-8.2 Fillet and Lead-in to Fillet Dimensions.
Table 5-4. Runway/Taxiway Intersection Fillet Radii
Table 5-5. Taxiway/Taxiway Intersection and Taxiway Turns Fillet Radii
Figure 5-4. Runway/Taxiway Intersection Fillets
Figure 5-5. Taxiway/Taxiway Intersection Fillets
Figure 5-6. Intersection Geometry for Navy and Marine Corps FacilitiesServing Aircraft with Wingspan Greater than 33.5 m (110 ft)
5-9 HIGH-SPEED RUNWAY EXITS.
5-10 APRON ACCESS TAXIWAYS.
5-10.1 Parking Aprons.
5-10.2 Fighter Aircraft Aprons.
5-11 SHOULDERS.
5-11.1 Fixed-Wing Taxiways.
5-11.2 Rotary-Wing Taxiways.
5-12 TOWWAYS.
5-12.1 Dimensions.
5-12.2 Layout.
5-12.3 Existing Roadway.
5-13 HANGAR ACCESS.
Table 5-6. Towways
Figure 5-7. Towway Criteria
CHAPTER 6 APRONS AND OTHER PAVEMENTS
6-1 CONTENTS.
6-2 APRON REQUIREMENTS.
6-3 TYPES OF APRONS AND OTHER PAVEMENTS.
6-4 AIRCRAFT CHARACTERISTICS.
6-5 PARKING APRON FOR FIXED-WING AIRCRAFT.
6-5.1 Location.
6-5.2 Size.
6-5.3 Army Parking Apron Layout
6-5.4 Air Force Parking Apron Layout.
6-5.5 Layout for Combined Army and Air Force Parking Aprons.
6-5.6 Tactical/Fighter Parking Apron Layout.
Figure 6-1. Apron Nomenclature and Criteria
Figure 6-2. Army and Air Force Parking Plan
Figure 6-3. Apron with Diagonal Parking
6-5.7 Refueling Considerations.
6-5.8 Parking Dimensions.
Figure 6-4. Truck Refueling Safety Zone Example
Table 6-1. Fixed-Wing Aprons
6-6 TAXIING CHARACTERISTICS ON APRONS FOR FIXED-WINGAIRCRAFT
6-6.2 Turning Capabilities (Aircraft Turning and Maneuvering
6-6.3 Departure Sequencing.
6-6.4 Minimum Standoff Distances from Edge Pavements.
6-7 PARKING APRON FOR ROTARY-WING AIRCRAFT.
6-7.1 Location.
6-7.2 Apron Size.
6-7.3 Maneuverability.
6-7.4 Army Parking Apron Layout.
6-7.5 Air Force Parking Apron Layout.
6-7.6 Refueling Considerations.
6-7.7 Parking Dimensions.
Figure 6-5. Type 1 Parking for All Rotary-Wing Aircraft Except CH-47
Figure 6-6. Type 1 Parking for CH-47
Figure 6-7. Type 2 Parking for Skid Rotary-Wing Aircraft
Figure 6-8. Type 2 Parking for Wheeled Rotary-Wing Aircraft
Table 6-2. Rotary-Wing Aprons for Army Airfields
6-8 WARM-UP PADS.
6-8.1 Navy and Marine Corps.
6-8.2 Location
6-8.3 Siting Considerations
6-8.4 Warm-Up Pad Size.
6-8.5 Taxi-In/Taxi-Out Capabilities.
Figure 6-9. Warm-Up Pad at End of Parallel Taxiway
Figure 6-10. Warm-Up Pad Next to Parallel Taxiway
Figure 6-11. Warm-Up Pad Located in Clear Zone
Figure 6-12. Warm-Up Pad Located in Approach-Departure Clearance Surface
Figure 6-13. Warm-Up Pad/Localizer Critical Area
Figure 6-14. Air Force Warm-Up Pad/Glide Slope Critical Area
Figure 6-15. Warm-Up Pad/CAT II ILS Critical Area
Figure 6-16. Warm-Up Pad Taxiing and Wingtip Clearance Requirements
6-8.6 Parking Angle.
6-8.7 Turning Radius.
6-8.8 Taxilanes on Warm-Up Pads.
6-8.9 Tie-Downs and Grounding Points.
6-9 POWER CHECK PAD.
6-9.1 Location and Siting Considerations.
6-9.2 Unsuppressed Power Check Pad Layout.
6-9.3 Access Taxiway/Towway.
6-9.4 Grading.
6-9.5 Thrust Anchors/Mooring Points.
Figure 6-17. Geometry for Rectangular Power Check Pad
Figure 6-18. Geometry for Square Power Check Pad
Figure 6-19. Geometry for Circular Power Check Pad
6-9.6 Anchor Blocks.
6-9.7 Power Check Pad Facilities
6-9.8 Noise Considerations.
6-10 ARM/DISARM PADS.
6-10.1 Navy and Marine Corps Requirements.
6-10.2 Location.
6-10.3 Siting Considerations
6-10.4 Arm/Disarm Pad Size.
6-10.5 Taxi-In/Taxi-Out Capabilities.
6-10.6 Parking Angle.
6-10.7 Turning Radius.
6-10.8 Access Road.
6-10.9 Tie-downs and Grounding Points.
6-10.10 Ammunition and Explosives Safety Standards.
Figure 6-20. Arm-Disarm Pad for F-4 Fighter
Figure 6-21. Arm-Disarm Pad for F-15 Fighter
Figure 6-22. Arm-Disarm Pad for F-16 Fighter
Figure 6-23. Arm-Disarm Pad for F-22 Fighter
6-11 COMPASS CALIBRATION PAD (CCP).
6-11.1 Air Force.
6-11.2 Navy and Marine Corps.
6-11.3 Location.
6-11.4 Siting Consideration
6-11.5 Compass Calibration Pad (CCP) Size
Figure 6-24. Army and Air Force Compass Calibration Pad
6-11.6 Access Taxiway/Towway.
6-11.7 Grading.
6-11.8 Tie-Down/Mooring Points.
6-11.9 Embedded Material.
6-11.10 Control Points.
6-12 HAZARDOUS CARGO PADS.
6-12.1 Navy and Marine Corps Requirements.
6-12.2 Siting Criteria.
6-12.3 Hazardous Cargo Pad Size
6-12.4 Access Taxiway.
6-12.5 Tie-Down and Grounding Points.
6-12.6 Miscellaneous Considerations.
6-13 ALERT PAD.
Figure 6-25. Hazardous Cargo Pad Other than APOE/Ds
Figure 6-26. Typical Hazardous Cargo Pad for APOE/Ds
Figure 6-27. Typical Alert Apron for Bombers and Tanker Aircraft
Figure 6-28. Typical Alert Pad for Fighter Aircraft
6-13.1 Navy and Marine Corps Requirements.
6-13.2 Location.
6-13.3 Siting Criteria
6-13.4 Alert Pad Size
Table 6-3. Minimum Separation Distance on Bomber Alert Aprons from theCenterline of a Through Taxilane to a Parked Aircraft
6-13.5 Design Aircraft.
6-13.6 Alert Aircraft Parking Arrangements
6-13.7 Jet Blast Distance Requirements.
6-13.8 Taxi-In/Taxi-Out Capabilities.
6-13.9 Turning Radius.
Figure 6-29. Alert Apron Taxi-In/Taxi-Out Parking
Figure 6-30. Alert Apron Back-In Parking
6-13.10 Dedicated Access Taxiway.
6-13.11 Tie-Down and Grounding Points.
6-14 AIRCRAFT WASH RACKS.
6-14.1 Location.
6-14.2 Wash Rack Size.
Table 6-4. Wash Rack Clearances From Aircraft to Curb
6-14.3 Wash Rack Facilities.
6-14.4 Wash Rack Grading.
6-14.5 Tie-Down and Grounding Points.
6-14.6 Concrete Curbs.
6-14.7 Service Points
Figure 6-31. Wash Rack for Mixed Mission Facility
Figure 6-32. Heavy Bomber Wash Rack (B-52 or B-1)
Figure 6-33. Cargo Aircraft Wash Rack
Figure 6-34. Fighter Aircraft Wash Rack and Navy Type A Wash Rack
Figure 6-35. Navy Type B Wash Rack
Figure 6-36. Helicopter Wash Rack (Single Helicopter)
Figure 6-37. Utilities and In-Pavement Structures
6-14.8 Wastewater Collection.
6-14.9 Wastewater Treatment.
6-14.10 Utilities Control Building.
6-14.11 Utilities.
6-15 HANGAR ACCESS APRONS.
6-15.1 Dimensions.
6-15.2 Grades for Aircraft Fueling Ramps.
6-15.3 Grades for Aircraft Access into Hangars.
Table 6-5. Hangar Access Apron
6-16 TAXIING CHARACTERISTICS ON APRONS FOR ROTARY-WINGAIRCRAFT.
6-16.1 Hoverlane/Taxilane Width at Army Facilities.
6-16.2 Hoverlane/Taxilane Width at Air Force Facilities.
6-17 FIXED-WING AND ROTARY-WING GRADING STANDARDS
6-17.1 Fixed-Wing Aircraft.
6-17.2 Rotary-Wing Aircraft.
6-17.3 Grades for Aircraft Fueling Ramps.
6-18 SHOULDERS.
6-18.1 Paved Shoulder Areas
6-18.2 Unpaved Shoulder Areas
6-19 MISCELLANEOUS APRON DESIGN CONSIDERATIONS.
6-19.1 Jet Blast Deflectors.
6-19.2 Line Vehicle Parking.
6-19.3 Utilities.
6-20 CV-22 APRON CLEARANCES.
6-21 US NAVY AND MARINE CORPS AIRCRAFT BLOCK DIMENSIONS.
Figure 6-38. CV-22 Apron Clearance Requirements
Figure 6-39. Navy/Marine Corps, 45-Degree Aircraft Parking Configuration
Figure 6-40. Navy/Marine Corps, 90-Degree Aircraft Parking Configuration
Table 6-6. Navy/Marine Corps Aircraft Parking Spacing,Helicopter Aircraft, 90-Degree Parking
Table 6-7. Navy/Marine Corps Aircraft Parking Spacing,Propeller Aircraft, 90-Degree Parking
Table 6-8. Navy/Marine Corps Aircraft Parking Spacing,Jet Aircraft, 90-Degree Parking
Table 6-9. Navy/Marine Corps Aircraft Parking Spacing,Jet Aircraft, 45-Degree Parking
CHAPTER 7 LANDING ZONES FOR C-130 AND C-17
7-1 GENERAL INFORMATION.
7-1.1 Differences in Service Criteria.
7-1.2 Landing Zone Marking and Lighting Standards.
7-2 DEFINITIONS.
7-2.1 Accident Potential Zone–Landing Zone (APZ-LZ)
7-2.2 Clear Zone-LZ
7-2.3 Contingency Operations
7-2.4 Exclusion Area
7-2.5 Graded Area
7-2.6 Imaginary Surfaces-LZ
7-2.7 Infield Area
7-2.8 Landing Zone (LZ)
7-2.9 Maintained Area
7-2.10 Parking Maximum on Ground (MOG)
7-2.11 Paved Landing Zone (LZ)
7-2.12 Primary Surface-LZ
7-2.13 Runway End.
7-2.14 Semi-Prepared Landing Zone (LZ).
7-2.15 Turnaround (or Hammerhead)
7-3 ACRONYMS.
7-4 SITE PLANNING FOR LANDING ZONES (LZ).
7-4.1 Future Development (Land or Aircraft Technology).
7-4.2 Prohibited Land Uses.
7-4.3 APZs not on DOD Property.
7-5 SITING CONSIDERATIONS.
7-5.1 Training Landing Zones (LZs).
7.5.2 Siting Landing Zones (LZs).
7-5.3 FAA Requirements.
7-5.4 Siting LZs in Built-Up Areas.
7-6 GEOMETRIC CRITERIA FOR RUNWAYS AND OVERRUNS.
7-6.1 LZ Runway Lengths.
Table 7-1. C-17 LZ Runway Lengths
7-6.2 LZ Runway Widths.
Table 7-2. Runways for LZs
7-6.3 Operating Surface Gradient Allowances.
7-6.4 LZ Shoulders.
Table 7-3. Taxiways for LZs
Table 7-4. Aprons for LZs
Table 7-5. Overruns for LZs
7-6.5 Turnarounds.
7-7 IMAGINARY SURFACES AND LAND USE CONTROL AREAS.
Table 7-6. Runway End Clear Zone for LZs
Table 7-7. Imaginary Surfaces for LZs
Table 7-8. APZs and Exclusion Areas for LZs
Figure 7-1. LZ Primary Surface End Details
Figure 7-2. LZ Details
Figure 7-3. LZ with Contiguous Aprons and Turnarounds
Figure 7-4. LZ Apron Layout Details
Figure 7-5. LZ Runway Imaginary Surfaces
Figure 7-6. LZ Runway, Taxiway, and Apron Sections
Figure 7-7. Navy and Marine Corps LZ Primary Surface End Details
Figure 7-8. Navy and Marine Corps LZ Details
Figure 7-9. Navy and Marine Corps LZ with Contiguous Aprons and Turnarounds
Figure 7-10. Navy and Marine Corps LZ Apron Layout Details
Figure 7-11. Navy and Marine Corps LZ Runway Imaginary Surfaces
Figure 7-12. Navy LZ Runway, Taxiway, and Apron Sections
7-8 OPERATIONAL WAIVERS TO CRITERIA.
7-9 SEPARATION DISTANCES BETWEEN PERMANENTRUNWAYS/HELIPADS AND LZ RUNWAYS
7-9.1 Separation Distances between Permanent Runways/Helipads and LZRunways for Simultaneous Operations.
7-9.2 Separation between Permanent Class A or Class B Runways and LZRunways for Non-Simultaneous Operations.
7-10 SURFACE TYPES.
7-11 MARKING AND LIGHTING.
Table 7-9. Runway Separation for Simultaneous Operations
CHAPTER 8 AIRCRAFT HANGAR PAVEMENTS
8-1 GENERAL REQUIREMENTS.
8-2 AIRCRAFT MODULES SPACE.
Table 8-1. Aircraft Space Modules for Army Aviation Facilities
8-3 HANGAR AND SHELTER CLEARANCES.
8-4 HANGAR FLOOR DESIGN.
Table 8-2. Aircraft Clearances inside Hangars
GLOSSARY
APPENDIX A REFERENCES
APPENDIX B BEST PRACTICES
SECTION 1 WAIVER PROCESSING PROCEDURES
B1-1 ARMY
B1-1.1 Waiver Procedures
B1-1.2 Contents of Waiver Requests.
B1-1.3 Additional Requirements
B1-2 AIR FORCE
B1-2.1 Waivers to Criteria and Standards
B1-2.2 Waiver Processing Procedures.
B1-2.3 Waiver Authority.
B1-2.4 Effective Length of Waiver.
B1-2.5 Responsibilities.
B1-3 NAVY AND MARINE CORPS
B1-3.1 Applicability
B1-3.2 Approval.
B1-3.3 Obtaining Waiver.
B1-3.4 Exemptions from Waiver.
SECTION 2 ARMY LAND USE AND FACILITY SPACE -- ALLOWANCES
B2-1 APPLICABILITY
B2-1.1 Air Force.
B2-1.2 Navy and Marine Corps.
Table B2-1. Facility Class 1: Operational and Training Facilities, Category Group11: Airfields Pavement, General
SECTION 3 DOD AIR INSTALLATIONS COMPATIBLE USE ZONESSUGGESTED LAND USE COMPATIBILITY IN ACCIDENT POTENTIAL ZONES
B3-1 LEGEND.
B3-2 NOTES.
B3-3 REFERENCES.
B3-3.1 DOD.
B3-3.2 Air Force.
B3-3.3 Navy and Marine Corps.
SECTION 4 WIND COVERAGE STUDIES
B4-1 APPLICABILITY
B4-1.1 Army.
B4-1.2 Air Force.
B4-1.3 Navy and Marine Corps.
B4-2 OBJECTIVE.
B4-3 GENERAL.
B4-3.1 Basic Conditions.
B4-3.2 Meteorological Conditions.
B4-4 WIND VELOCITY AND DIRECTION.
B4-4.1 Composite Windrose.
B4-4.2 Terrain.
B4-4.3 Additional Weather Data.
B4-4.4 Wind Distribution.
B4-5 USE OF WINDROSE DIAGRAMS.
B4-5.1 Drawing the Windrose.
B4-5.2 Special Conditions.
Figure B4-1. Windrose Blank Showing Direction and Divisions(16-Sector [22.5°] Windrose)
Figure B4-2. Windrose Blank Showing Direction and Divisions(36-Sector [10°] Windrose)
Figure B4-3. Completed Windrose and Wind Velocity Equivalents(16-Sector [22.5°] Windrose)
B4-5.3 Desired Runway Orientation.
Figure B4-4. Windrose Analysis
B4-6 WIND COVERAGE REQUIREMENTS FOR RUNWAYS.
B4-6.1 Primary Runways.
B4-6.2 Secondary Runways.
B4-6.3 Maximum Allowable Crosswind Components (Navy Only) .
B4-6.4 Allowable Variations of Wind Direction.
Figure B4-5. Allowable Wind Variation for 19 Kilometer-per-Hour (10.4 Knot) and28 Kilometer-per-Hour (15 Knot) Beam Wind Components
SECTION 5 EXTRACT OF FEDERAL AVIATION REGULATION PART 77,OBJECTS AFFECTING NAVIGABLE AIRSPACE
SECTION 6 AIRCRAFT CHARACTERISTICS FORAIRFIELD-HELIPORT DESIGN AND EVALUATION
B6-1 GENERAL.
SECTION 7 JET BLAST EFFECTS
B7-1 CONTENTS.
B7-2 CONSIDERATIONS.
B7-2.1 Blast Temperatures.
B7-2.2 Blast Velocities.
B7-2.3 Minimum Clearances.
B7-2.4 Engine Blast Relationship.
B7-3 PROTECTION FROM JET BLAST EFFECTS.
B7-3.1 Blast Deflectors.
B7-3.2 Unprotected Areas.
B7-4 NOISE CONSIDERATIONS.
B7-5 JET BLAST REQUIREMENTS.
B7-5.1 Parked Aircraft.
B7-5.2 Taxiing Aircraft.
SECTION 8 JET BLAST DEFLECTOR
B8-1 OVERVIEW.
B8-1.1 Location.
B8-1.2 Size and Configuration.
B8-1.3 Paved Shoulders.
SECTION 9 EXPLOSIVES ON OR NEAR AIRFIELDS
B9-1 CONTENTS.
B9-2 SEPARATION DISTANCE REQUIREMENTS.
B9-3 PROHIBITED ZONES.
B9-4 HAZARDS OF ELECTROMAGNETIC RADIATION TO EED.
B9-5 LIGHTNING PROTECTION.
B9-6 GROUNDING OF AIRCRAFT.
B9-7 HOT REFUELING.
SECTION 10 COMPASS CALIBRATION PAD MAGNETIC SURVEY
B10-1 CONTENTS.
B10-2 AIR FORCE, NAVY, AND MARINE CORPS REQUIREMENTS.
B10-3 ACCURACY REQUIREMENTS.
B10-4 PRELIMINARY SURVEY REQUIREMENTS.
B10-4.1 Proton Magnetometer Method.
B10-4.2 Distant Object Method.
B10-4.3 Reciprocal Observation Method.
B10-5 MAGNETIC SURVEY REQUIREMENTS.
B10-6 MAGNETIC SURVEY PROCEDURES.
B10-6.1 Magnetic Field Survey (Variation Check).
Figure B10-1. Magnetic Field Survey Sheet
B10-6.2 Magnetic Direction Survey.
Figure B10-2. Layout of Compass Rose
B10-7 SITING CONSIDERATIONS.
B10-7.1 Separation Distances.
B10-7.2 Checking Site.
SECTION 11 TIEDOWNS, MOORING, AND GROUNDING POINTS
B11-1 TYPES OF EQUIPMENT
B11-1.1 Mooring and Grounding Point.
B11-1.2 Mooring Point.
B11-1.3 Static Grounding Point.
B11-1.4 Static Grounding Tiedown.
B11-1.5 Tiedown Mooring Eye.
B11-2 MOORING POINTS FOR ARMY FIXED- AND ROTARY-WING AIRCRAFT
B11-2.1 Type.
Figure B11-1. Army Mooring Point
B11-2.2 Design Load.
Figure B11-2. Army Load Testing of Mooring Points
B11-2.3 Layout.
Figure B11-3. Army Rotary-Wing Allowable Mooring Point Spacing
Figure B11-4. Army Rotary-Wing Mooring Points Layout
B11-2.4 Installation
Figure B11-5. Slab Reinforcement for Army Mooring Point
Figure B11-6. Mooring Point for Existing Rigid Pavement for Pavement ThicknessGreater Than 150 Millimeters (6 Inches)
Figure B11-7. Army Rotary-Wing Mooring Pad Detail
Figure B11-8. Army Mooring Point for Grassed Areas, Flexible Pavement, or RigidPavement - Thickness Less Than 150 millimeters (6 inches)
Table B11-1. Army Pier Length and Depths for Tiedowns
B11-3 EXISTING MOORING POINTS FOR ARMY.
B11-3.1 Evaluation of Existing Mooring Points for Structural Adequacy
B11-3.2 Evaluation of Existing Mooring Points for Resistance.
B11-4 STATIC GROUNDING POINTS FOR ARMY FIXED- AND ROTARY-WING FACILITIES
B11-4.1 Type.
Figure B11-9. Army Grounding Point Inside Aircraft Hangars
B11-4.2 Layout
B11-4.3 Installation.
B11-4.4 Grounding Requirements.
Figure B11-10. Mooring and Ground Point Layout for Rotary-Wing Parking Spac
Figure B11-11. Army Grounding Point for Turf Areas
B11-5 AIR FORCE TIEDOWNS AND STATIC GROUNDS
B11-5.1 General.
B11-5.2 Layout.
Figure B11-12. Air Force Static Ground
Figure B11-13. Example of Air Force Multiple Tiedown Layoutfor Fixed-Wing Aircraft
B11-5.3 Installation
Figure B11-14. Air Force Aircraft Tiedown, Profile
Figure B11-15. Air Force Aircraft Tiedown, Plan
B11-5.4 Grounding Requirements.
B11-6 TIEDOWN MOORING EYES FOR NAVY AND MARINE CORPS.
Figure B11-16. Navy and Marine Corps Mooring Eye/Tiedown Details
SECTION 12 FLIGHTLINE VEHICLE PARKING - NAVY AND MARINE CORPS
B12-1 CONTENTS.
B12-2 ARMY AND AIR FORCE CRITERIA.
B12-3 LOCATION.
B12-3.1 Area Required.
B12-3.2 Station-Assigned Vehicles.
B12-3.3 Squadron-Assigned Vehicles.
B12-3.4 Refueling Vehicles.
B12-4 SURFACING.
B12-5 SHELTER.
B12-6 LIGHTING.
Table B12-1. Vehicle Parking Area Requirements
Figure B12-1. Typical Site Plan - Vehicle Parking
Figure B12-2. Typical Line Vehicle Shelters
SECTION 13 DEVIATIONS FROM CRITERIA FOR AIR FORCE AIRFIELD SUPPORT FACILITIES
B13-1 WAIVERABLE AIRFIELD SUPPORT FACILITIES
B13-1.1 Contents.
B13-1.2 Army, Navy, and Marine Corps Requirements.
B13-1.3 Fixed Base Airport Surveillance Radar (ASR) or Fixed Base DigitalAirport Surveillance Radar (DASR).
B13-1.4 Airport Rotating Beacon.
B13-1.5 Nondirectional Radio Beacon Facilities.
B13-1.6 Rotating Beam Ceilometers.
B13-1.7 Laser Beam Ceilometers.
B13-1.8 Air Traffic Control Tower (ATCT).
B13-2 PERMISSABLE DEVIATIONS FROM DESIGN CRITERIA
B13-2.1 Contents.
B13-2.2 Frangibility Requirements.
B13-2.3 Visual Air Navigational Facilities.
B13-2.5 Emergency Generators, Maintenance and Personnel Facilities(Non-Frangible).
B13-2.6 Remote Microwave Link (Non-Frangible).
B13-2.7 PAR Reflectors (Frangible and Non-Frangible).
B13-2.8 Airborne Radar Approach Reflectors (Non-Frangible).
B13-2.9 Instrument Landing System (ILS).
B13-2.10 Microwave Landing System (MLS) and Mobile Microwave LandingSystem (MMLS) (Non-Frangible).
B13-2.11 Mobile Navigational Aids and Communication Facilities(Non-Frangible).
B13-2.12 Mobile Air Traffic Control Towers (MATCT) (Non-Frangible).
B13-2.13 Terminal Very High Frequency Omnirange (TVOR) Facility and Very HighFrequency Omnirange (VOR) Facility (Non-Frangible).
B13-2.14 Tactical Air Navigation (TACAN) Facility and Very High FrequencyOmnidirectional Radio Range (VORTAC) Facility (Non-Frangible).
B13-2.15 Runway Supervisory Unit (RSU) (Non-Frangible).
B13-2.16 Transmissometer Facilities (Non-Frangible).
B13-2.17 Wind Measuring Set (Non-Frangible).
B13-2.18 Temperature-Humidity Measuring Set (Non-Frangible).
B13-2.19 Wind Direction Indicators (Frangible and Non-Frangible).
B13-2.20 General Information for Operational and Maintenance Support Facilities.
SECTION 14 CONSTRUCTION PHASING PLAN AND OPERATIONAL SAFETYON AIRFIELDS DURING CONSTRUCTION
B14-1 CONTENTS.
B14-2 NAVY AND MARINE CORPS REQUIREMENTS.
B14-3 INFORMATION TO BE SHOWN ON THE CONSTRUCTION PHASINGPLAN. The
B14-3.1 Phasing.
B14-3.2 Aircraft Operational Areas.
B14-3.3 Additional Requirements.
B14-3.4 Temporary Displaced Thresholds.
B14-3.5 Access.
B14-3.6 Temporary Marking and Lighting.
B14-3.7 Safety Requirements and Procedures.
B14-3.8 FOD Checkpoints.
B14-4 OTHER ITEMS TO BE SHOWN IN THE CONTRACT DRAWINGS.
B14-4.1 Storage.
B14-4.2 Parking.
B14-4.3 Buildings.
B14-4.4 Designated Waste and Disposal Areas.
B14-5 MAXIMUM EQUIPMENT HEIGHT.
B14-6 OPERATIONAL SAFETY ON THE AIRFIELD DURING CONSTRUCTION.
B14-6.1 General Requirements.
B14-6.2 Formal Notification of Construction Activities.
B14-6.3 Safety Considerations.
B14-6.4 Examples of Hazardous and Marginal Conditions.
B14-6.5 Vehicles on the Airfield.
B14-6.6 Inspection.
B14-6.7 Special Safety Requirements during Construction.
B14-6.8 Construction Vehicle Traffic.
B14-6.9 Limitation on Construction.
B14-6.10 Marking and Lighting Closed or Hazardous Areas on Airports.
B14-6.11 Temporary Runway Threshold Displacement.
SECTION 15 AIRCRAFT TRIM PAD AND THRUST ANCHOR FOR UP TO 267KILONEWTONS (60,000 POUNDS) THRUST
Figure B15-1. Jet Blast Directed Away From Pavement on a Power Check Pad
Figure B15-2. Example of Square Aircraft Anchor Block and Cross Section
Figure B15-3. Example of Square Anchor Block, Cross Section A-A and B-B
Figure B15-4. Example of Octagonal Anchor Block
Figure B15-5. Example of Octagonal Anchor Block,Cross-Sections C-C, D-D, and E-E
SECTION 16 NAVIGATION AIDS DESIGN AND SUPPORT
B16-1 GENERAL.
Table B16-1. Navigational Aids (NAVAIDS) Design and Support
SECTION 17 AIR TRAFFIC CONTROL TOWER SITING CRITERIA
B17-1 GENERAL INFORMATION.
B17-2 SITING CRITERIA.
B17-2.1 Unobstructed View .
B17-2.2 Site Area Requirements
B17-2.3 Quantity Distance Criteria
B17-2.4 Obstruction Clearance
B17-2.5 Siting Effects on NAVAIDS
B17-2.6 Siting for Proper Depth Perception
B17-2.7 Compliance With Airfield Standards
B17-2.8 Orientation of the Cab
B17-2.9 Extraneous Lighting
B17-2.10 Weather Phenomena
B17-2.11 Exhaust Fumes and other Visibility Impairments
B17-2.12 Avoid Sources of Extraneous Noise
B17-2.13 Personnel Access Considerations
B17-2.14 Compliance With the Comprehensive Plan
B17-2.15 Consider the Effects on Meteorological and Communications Facilities
Figure B17-1. Runway Profile and New Control Tower
Figure B17-2. Minimum Eye-Level Determination
Figure B17-3. Minimum Eye-Level Measurement
B17-3 MINIMUM REQUIRED FLOOR LEVELS.
Figure B17-4. Minimum Tower Floors
B17-4 SITING PROCEDURES.
B17-4.1 Office Study by Siting Engineers.
B17-4.2 Field Study by Siting Engineers.
B17-4.3 TERPS Analysis.
B17-5 SITE RECOMMENDATIONS.
B17-6 SOI DISTRIBUTION.
B17-7 SAMPLE SOI
SECTION 18 GUIDELINES FOR ESTABLISHING BUILDINGRESTRICTION LINE AT AIR FORCE BASES
B18-1 OVERVIEW
B18-1.1 General Information.
B18-1.2 Purpose.
B18-2 ESTABLISHING THE BRL AT A BASE.
B18-3 STATUS OF EXISTING AND FUTURE FACILITIES ANDOBSTRUCTIONS WITHIN THE AREA.
B18-4 FUTURE DEVELOPMENT OF AREA WITHIN BRL CONTROL LINES
B18-4.1 Future Construction.
B18-4.2 Existing Facilities.
B18-5 DOCUMENTATION AND REPORTING.
B18-6 IMPLEMENTATION.
B18-7 FUTURE MODIFICATION TO BRL.
Figure B18-1. BRL – Plan View
Figure B18-2. BRL – Profile View

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