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Archive / FAA Parachute Rigger Handbook / FAA Parachute Rigger Handbook: Chapter 8

Chapter 8

Chapter 8 — Part 2

FAA-H-8083-17 (2015 Change 1)

Figure 2-22. Type 2 deployment—Lo-Po Reserve.

Figure 2-23. Type 3 deployment—Phantom canopy.

Figure 2-24. Type 4 deployment—Preserve diaper.

Figure 2-26. Type 6 deployment—Sleeve.

Figure 2-25. A) Type 5 deployment—Freebag and B) Type 5

deployment—Speedbag.

Type 3: Ascuitto or Piglet-Style Flat Diaper

This deployment features a full diaper with all lines stowed

left to right or perpendicular to the radial seam. Examples

of this method are the Piglet, Phantom, and Security Aero

Conical (SAC) canopies. [Figure 2-23]

Type 4: Handbury or Preserve Full Diaper

This features a choker-type diaper that wraps around the

canopy skirt. It is locked with three stows and all lines are

stowed on the diaper parallel to the radial seam. Examples of

this method are the Preserve series canopies, Strong Lo-Po

Lite, and the Hobbit square reserve. [Figure 2-24] The military

quarter bag is basically a version of the Type 4 method.

Type 5: Free Bag

With a free bag, the canopy is stowed in the bag, and lines are

either stowed on or in the bag. They were originally used on

the Safety Flyer reserve. This is the dominant and preferred

method for virtually all modern square reserves. [Figure 2-25]

Type 6: Sleeves

The sleeve type includes a fabric tube that encloses the

full length of the folded canopy. Lines are stowed on the

sleeve. They were originally used on early sport canopies,

particularly the Para-Commander. [Figure 2-26] A modern

version, known as a “slag,” is used on some ram-air canopies.

An additional deployment method is the “tail pocket.” This is

a fabric pocket sewn on the tail of a ram-air canopy in which

the lines are stowed. [Figure 2-27]

Figure 2-30. Safety Stow®.

Figure 2-28. Hesitator loops.

Figure 2-29. Para-Flite O-rings.

Figure 2-27. Tail pocket.

Securing the Deployment Device

With all deployment methods, it is necessary to properly

fold or stow the canopy and secure the deployment device

with the lines. The early parachutes utilized hesitator loops

to secure the lines. [Figure 2-28] This method is still used

today in many military systems.

In modern designs that utilize types 1 through 4 and 6,

the preferred method of locking the deployment device is

rubber bands. The specification for standard rubber bands

is MIL-R-1832. Type 1 are made of natural rubber and are

1⁄2" × 2". These were designed for use with the thicker Type

III nylon lines such as on the 28' C-9 canopy. Many of the

newer lightweight, round canopies use smaller diameter and

fewer lines. Consequently, the standard rubber bands do not

work well. Some manufacturers supply smaller, 1¼" diameter

rubber bands to be used with their canopies. It is extremely

important to utilize the correct size rubber bands.

With the introduction of the free bag system in 1977, Para-

Flite, Inc., used a BUNA-N “O” ring to secure the locking

stows. [Figure 2-29] During testing of the free bag system,

they found inconsistent holding and breaking strengths of

rubber bands. They wanted the locking stows to release at a

consistent force to prevent bag lock. The “O” rings provided

this. A couple of years later, the “O” rings were upgraded to

a thicker diameter model. In 1983, Para-Flite, Inc. replaced

the “O” rings with the Safety Stow ®. The Safety Stow® is

a continuous loop of elastic shock cord that runs through a

webbing channel and through two grommets to secure the

first two locking stows. [Figure 2-30] In the event of any

restriction on the locking stow, as the loop stretches, it allows

first one side to release and then the opposite side.

It is important to maintain the rubber bands or Safety Stow®.

Rubber bands are susceptible to heat degradation and may dry

out. If they break prematurely during use, the parachute may

malfunction. Non-mil. specification rubber bands may react to

natural brass grommets and may become gummy and sticky,

causing the lines to stick to the diaper or bag. Rubber bands

should be replaced during routine Inspection and Repack.

[Figure 2-31A and B] The BUNA-N “O” rings should be

replaced with the Safety Stow ®. The Safety Stow ® should

be inspected for broken stitching or internal rubber strands.

[Figure 2-32]

In response to occasional violent openings on ram-air

canopies, Parachute Labs (Jump Shack) in 2003 introduced

the “speed bag” to eliminate “line dump” (line strip). The

lines are retained in rubber bands 25 percent in from the edge

of the bag. This balances the mass of the stows between the

Change 1 (December 2015)

Figure 2-32. Bad Safety Stow®.

Figure 2-31. A) Old rubber bands and B) new rubber bands. They come in 3 sizes: 3⁄8" wide × 1¼" diameter, 3⁄8" wide × 2" diameter

and ¾" wide × 2" diameter.

Figure 2-34. Hand tack floating bridle loop.

Figure 2-33. Pre-sewn round bridles.

bights and center span of the stow. The bag has an additional

flap on the top side that has slots for the rubber bands mounted

on the bottom flap. These two flaps overlap closing the bag

over the canopy. The design was used on main canopies

only for the first three years. Its success led to the release as

a reserve bag in 2006.

Bridles

The bridle is a cord or webbing strap that is used to connect

the pilot chute to the canopy or deployment device. Main

and reserve bridles, while sharing the same function,

operate differently.

Early bridles were simply a length of suspension line tied off

to the two components. It was soon learned that the length

of the bridle affected the function of the pilot chute and

the opening characteristics of the canopy. On most round

emergency and reserve parachute assemblies, the length and

type of the bridle is fixed for optimum performance. The

rigger cannot change the configuration of the bridle without

approval of the manufacturer.

There are two basic types of round canopy bridles. The first

is a tubular nylon bridle that is tied on. The second is a pre-

sewn bridle with loops at each end. The loop of one end is

passed through the attach point on the pilot chute and then

back through itself forming a lark’s head knot. The other

loop of the bridle is then similarly attached to the canopy

apex. [Figure 2-33] With this type, it is essential for the

loop to remain loose to ensure the bridle is free floating and

self-centering around the apex lines. Hand tack the loop to

ensure this. [Figure 2-34]

Square reserve bridles are generally built into the free bag. The

bridle material is usually 2 feet wide or more for high drag. The

original concept of the free bag is to allow the square reserve

Figure 2-36. Bungee collapsible bridle.

Figure 2-37. Kill-line collapsible bridle.

Figure 2-38. Kill-line eye or window.

Figure 2-35. Freebag assistor pocket.

to deploy if the reserve pilot chute is captured resulting in a

horseshoe-type malfunction. The high-drag bridle would then

pull the reserve bag off the parachutist’s back and allow the

canopy to deploy free from the bag. In the late 1980s, assistor

pockets were added to some bridles for additional drag as

square reserves became bigger and heavier. [Figure 2-35]

Early main bridles were simply longer versions of the reserve

bridles. This was necessary to compensate for the “burble”

created in free fall by the parachutist. In the mid 1970s and

with the advent of the hand deploy pilot chute, the length of

the bridle was critical in order to allow proper extraction of

the locking pin that secured the pack closed.

In recent years and with the almost total use of ram-air

parachutes, the need for collapsible main pilot chutes has

become widespread. As the main canopies have become

smaller and faster, the drag of the inflated main pilot

chute after opening can have an adverse effect on canopy

performance. This problem has been solved through the

use of a collapsible pilot chute/bridle system. There are two

primary designs used to accomplish this.

The first is the “ bungee” collapsible configuration. This

consists of a length of elastic shock cord inside a tape sheath

on the bridle near the pilot chute end. [Figure 2-36] When

relaxed, it holds the apex of the pilot chute collapsed. When the

pilot chute is deployed into the airstream, the airflow inflates

the pilot chute, which deploys the canopy. After opening, the

elastic pulls the apex down again and collapses the pilot chute,

reducing the drag. While this system works, its main drawback

is that certain airspeeds are needed to inflate the pilot chute.

Remember, the primary function of the pilot chute is to initiate

deployment. Collapsing the pilot chute is secondary.

The second type is the “kill-line collapsible” configuration. This

consists of a bridle with a full length channel through which

passes a line of Kevlar® or Spectra®. [Figure 2-37] The bridle

is “cocked” and the lower end of the bridle is collapsed during

packing. This allows the pilot chute to inflate immediately.

During the deployment sequence, as the canopy inflates, the

lower end is stretched to length and the centerline pulls the apex

of the pilot chute down and collapses it. This configuration

has become almost universal in use for skydiving today. The

only drawback is if the user forgets to cock the bridle during

packing. This results in a collapsed pilot chute and a pilot chute

in tow. In the early days of use of the kill-line bridle, this was

a problem but has become less frequent today. Some bridles

have a colored “eye” at the locking pin location to show if it

is cocked and the centerline is set correctly. [Figure 2-38]

The kill-line configuration is used almost exclusively on

tandem systems due to the high speeds involved and the size

of the drogue pilot chutes. Some bridles are made from 2"

Figure 2-39. Tandem main collapsible bridle.

Kevlar® tape and have tubular nylon centerlines. Others are

made from Type 4 square weave with a Spectra centerline.

The advantage of the latter is that it can be cut with a hook

knife in the event of an on-person malfunction. [Figure 2-39]

Another method of collapsing the pilot chute is to install a No.

8 grommet in the deployment bag and allow the bag to float

on the bridle. After the canopy deploys, the bag slides up the

bridle, inverts, and covers the pilot chute. This is commonly

called the “poor man’s collapsible pilot chute system.” The

drawback to this design is the high wear on the bridle and

pilot chute mesh.

Pilot Chutes

A pilot chute is a small parachute that is used to deploy the

main or reserve parachute. In the earliest uses of parachutes,

the parachute was static line deployed. With the advent of

manually operated or “free fall” parachutes, the need for a

pilot chute was quickly recognized.

There are two basic types of pilot chutes. The first is the

spring-loaded design. This uses a collapsible spring, which

is compressed in the parachute container and held closed

with the ripcord. When the ripcord is pulled, the pack opens

and the pilot chute launches into the airstream. The pilot

chute provides drag and pulls the canopy from the pack as

the parachutist or load falls away. During this process, the

pilot chute also provides tension on the lines of the deploying

canopy and helps the opening sequence. Spring-loaded

pilot chutes are used primarily for emergency and reserve

parachutes. In addition, they are used in military free fall and

training systems for the main parachute.

The second type of pilot chute is the “hand deploy” design.

This type consists of the pilot chute canopy but does not have

a spring to launch it. Instead, the parachutist extracts the

folded pilot chute from a pouch or the container and launches

it into the airstream. The pack is held closed by a locking pin

attached to the bridle of the pilot chute. As the pilot chute

inflates, it extracts the pin from the locking loop and pulls

the parachute from the pack. The rest of the opening process

is similar to the spring-loaded pilot chute. This configuration

came into popularity in the mid 1970s and is now the primary

method of deployment in skydiving.

Spring-Loaded Pilot Chutes

Spring-loaded pilot chutes date from the 1920s. However,

it was not until 1940 that the spiral vane pilot chute was

invented. This design used a spiral spring that is easy to

collapse and pack. The most common type of spiral vane pilot

chute used today is the MA-1 model. [Figure 2-40A and B]

This is used in several military parachute assemblies. In the

early days of skydiving, military pilot chutes, such as the

MA-1 and others were popular. Soon commercial designs

were introduced that improved on the MA-1 with better

launch and drag characteristics. These included the Grabber®

and Hot Dog® pilot chutes. Both of these were primarily for

use with main parachutes.

With the advent of the hand deploy pilot chute for the main,

most of the improvement in spring-loaded pilot chute design

has focused on its use in the reserve or emergency parachutes.

This has paralleled the improvements in container design and

the increased use of AADs. Both of these require better pilot

chutes than in the past.

One example for reserve use is the Magnum® pilot chute

designed by National Parachute Industries. [Figure 2-41]

With its unique shape, it provides maximum drag at low

speeds, such as are experienced during cutaways. Its design

has been licensed by other manufacturers for use in their

assemblies. Additional designs include the Vector II reserve

pilot chute and the Stealth pilot chute. The Vector II design is

a “ballute” configuration that eliminates the use of mesh. In

the event of an unstable launch on its side, the mass of fabric

is sufficient to lift the pilot chute and deploy the parachute.

The Stealth pilot chute uses a conventional mesh design but

has a unique spring/cap configuration that allows the pilot

chute to virtually disappear when packed, hence the name.

The MA-1 spring with mesh in place of the vanes, and a

closed canopy instead of the scalloped canopy provides the

best of both worlds: a spring that does not lock up on itself

and high drag without the possibility of snag.

Hand Deploy Pilot Chutes

The hand deploy pilot chute was introduced in 1976. There

are two types of hand deploy designs. One is the throw-out

pilot chute (TOP) configuration. This is the type where

the pilot chute pulls the locking pin located on the bridle.

[Figure 2-42] The original design had the pilot chute pouch

Figure 2-40. A) MA-1 pilot chute and B) high-drag pilot chute with large hole mesh.

mounted on the belly band. Today, the primary location is an

elastic/Spandex® pocket mounted on the bottom of the main

container (BOC). [Figure 2-43] Most of the difficulties of this

design have to do with pilot chute in tow due to misrouting

of the bridle or failure of the pin to extract.

The second type is the pull-out pilot chute (POP) configuration.

This design has the pilot chute packed in the container, which

is locked with a straight locking pin attached to a short lanyard

and handle. [Figure 2-44A and B] This handle is usually

mounted on the bottom corner of the main container. The

parachutist grasps the handle and pulls the locking pin from

the locking loop and puts the pilot chute into the airstream. The

handle is usually attached to the bottom of the pilot chute and

as the chute enters the airstream, the jumper loosens his grip

on the handle allowing it to be pulled from his or her hand.

This makes for a positive deployment. The main drawback to

this system is losing the handle due to it being dislodged while

moving around in the aircraft or in the air. Fortunately, the

handle does not go far and is easy to obtain because it is on a

short lanyard that is tucked up under the side flap. .

Automatic Activation Devices (AADs) and

Reserve Static Lines (RSLs)

Safety considerations have led to the development of AADs

and reserve static line (RSL) systems. These devices allow

for automatic deployment of the main or reserve parachutes

in the event of an emergency.

Automatic Activation Devices

AADs are devices that activate the parachute automatically.

Modern systems combine a barometric sensor with a rate

of descent sensor so that the system is fully automatic once

turned on and calibrated. The activation may be by either

pulling the ripcord pin(s) or cutting the locking loop(s),

Figure 2-41. Magnum pilot chute.

Figure 2-42. TOP bridle/pin configuration.

Figure 2-43. BOC pocket location.

causing the pilot chute to release. Most older models use

a mechanical or pyrotechnic pin pulling technique. Newer

models use a pyrotechnic loop cutting design.

For many years, AADs were primarily used by the

military and student parachutists. The designs were bulky,

expensive, and, to a degree, inconsistent. The installations

themselves were cumbersome and awkward. In the early

1990s, a new generation of AADs became available. The

CYbernetic Parachute RElease System (CYPRES ®) uses

modern parachute release technology. It is small, reliable,

computer based, and uses a pyrotechnic loop cutter. It has

an auto-off feature that turns the unit off after 14 hours

of operation to conserve power. It also has the ability to

calibrate the unit for operation at altitudes other than the

calibrating ground level. Based on these concepts, other

companies have developed similar systems and as a result,

changed the approach to the design and use of AADs.

Today, a good many sport parachutists use an AAD and

some countries (rightly or wrongly), mandate their use by

all parachutists.

The following describes the operation and installation

requirements of the CYPRES ® model AA. Other designs,

such as the Vigil ®, are compatible with these installation

requirements.

Operation

The CYPRES ® system is a barometrically controlled

microprocessor that activates a pyrotechnic cutter that cuts

the container locking loop. When calibrated to ground

level, the barometric sensor activates the unit firing the

cutter when the descending parachutist reaches an altitude

of approximately 750 feet above ground level (AGL) and

exceeds a rate of descent of 115 feet per second (fps).

The CYPRES® consists of three parts:

1. Battery and processing unit

2. Control unit

3. Cutter [Figure 2-45]

Figure 2-45. CYPRES® AAD.

Figure 2-44. A) POP handle with pilot chute and B) POP handle and lanyard.

Figure 2-46. CYPRES® container pouch.

Figure 2-47. CYPRES® control unit vinyl pocket.

Figure 2-48. CYPRES® cutter location.

The processing unit is generally located in a stowage pouch

installed in the reserve container of the parachute system.

[Figure 2-46] The control unit is contained in a vinyl pocket

located either under the pin protector flap or in the upper back

pad area. [Figure 2-47]

The cutter(s) may be located at the base of the pilot chute

or on a flap over the pilot chute. [Figure 2-48] Each

parachute system has its own particular requirements, and

it is imperative that the rigger have the appropriate manuals

for installation.

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