H-60S Plane Captain

Front 1

Acceptable Fuel for 60S

Back 1

JP-5

JP-8

A++

Front 2

Nato Code for JP-5

Back 2

F-44

Front 3

Nato Code for JP-8

Back 3

F-34

Front 4

Nato Code for A++

Back 4

F-24

Front 5

Restricted Fuel for 60S

Back 5

Jet A-1

Jet A

Jet B

JP-4

Front 6

Nato Code for Jet A-1

Back 6

F-35

Front 7

Nato Code for Jet A

Back 7

None

Front 8

Nato Code for Jet B

Back 8

None

Front 9

Nato Code for Jet-4

Back 9

F-40

Front 10

Servicing Engines

Back 10

MIL-PRF-23699; Alternative MIL-PRF-7808

Front 11

Servicing Main Gear Box

Back 11

MIL-PRF-85734; Alternative MIL-PRF 7808

Front 12

Servicing Intermediate Gear Box

Back 12

MIL-PRF-85734; Alternative MIL-PRF-7808

Front 13

Servicing Tail Gear Box

Back 13

MIL-PRF-85734; Alternative MIL-PRF-7808

Front 14

Servicing Hydraulic Reservoir

Back 14

MIL-PRF- 83282; Alternative MIL-PRF-5606

Front 15

Servicing Auxiliary Power Unit

Back 15

MIL-PRF-23699; Alternative MIL-PRF-7808

Front 16

PC directly responsible to...

Back 16

CO

Front 17

Primary job of PC

Back 17

Safety

Front 18

Main fuel cell totality

Back 18

two separate tanks each holds 180 gallons equaling 360 gallons

Front 19

ERFS

Back 19

Extended Range Fuel System; Holds 200 gallons

Front 20

Wait time for fuel samples after move or fueling

Back 20

2 hours, or as long as flight schedule permits

Front 21

Fuel Contaminants

Back 21

Particles (sand, dirt, iron and rust) - Black/Brown

Water/Air - Bubbles

Microorganisms - Green

Fuel Cell lining/sealent - Purple

Alconox - White

Front 22

# of people for fuel sample

Back 22

2

Front 23

How much to drain for sample

Back 23

1 pint

Front 24

Chemical to clean jars with

Back 24

Alconox

Front 25

Precautions before sampling Internal Auxilary

Back 25

Secure power to bird and disconnect battery

Front 26

Rotor Brake Pressure

Back 26

450-690 PSI

Front 27

APU accumulator pressure

Back 27

2700-3100 PSI

Front 28

How do you ground an aircraft in the hangar

Back 28

From ground to aircraft and remove aircraft then ground

Front 29

Cut limit on MLG and location of info

Back 29

4/32nd of an inch; found on sidewall of tire pub (04-10-506)

Front 30

Cut limit on TLG and location of info

Back 30

5/32nd of an inch; found on sidewall or tire pub (04-10-506)

Front 31

Limits for tire pressure on MLG and TLG

Back 31

MLG 130-140 PSI and TLG 100-110 PSI

Front 32

What is the slip mark and what are the limits

Back 32

red dot on the tire in line with the valve stem to indicate rotating on rim; tire can only rotate 1/4 of an inch before valve stem blows tire

Front 33

How many Flex/Thomas Couplings and limit gaps

Back 33

11; space between couplings up to .030 of a inch

Front 34

Inspecting Viscous Dampers and Limits

Back 34

To inspect, look for air bubbles with limits less than 1 inch good, 1 to 2 inches serviceable, and over 2 inches over serviced

Front 35

How to test brakes on 60S

Back 35

By pressing the war indication pin, if goes flush then brakes are bad and need to be replaced

Front 36

Locations of primary and backup computers on A/C

Back 36

Primary: located in the T-Section

Backup: located in the nose

Front 37

What is added to windshield wiper reservoir in freezing weather

Back 37

Isopropyl Alcohol 50/50 and water

Front 38

When you clamp and tie down the blade to secure the bird how far should the blade deflect

Back 38

6-12 inches

Front 39

When can you not enter the rotor arc (5)

Back 39

Engage/disengaging rotors

During engine start up and shut down

When pilots are switching seats

During a hit check

Engine burnout

Front 40

Positions to enter and exit the rotor arc

Back 40

3 and 9 o'clock

Front 41

How long does a daily take

Back 41

As long as it takes. You cannot rush maintenance

Front 42

"Hot" DTA and maintenance needs to be done quickly

Back 42

Ask for more PCs to help

Front 43

Publications to wash a bird

Back 43

IETMs Plane Captains Manuel, MRC-350 and 01-1A-509 Vol II

Front 44

Soap to water ratio for wash jobs

Back 44

1:1 is a heavy wash

1:4 is a normal wash

1:9 is a light wash

Front 45

Job of ECS

Back 45

Environmental Control System; Primarily cool avionics. Secondarily cool cabin and cockpit

Front 46

First step to conducting a bird move

Back 46

Make a move sheet and hold a move brief in maintenance control

Front 47

Type of towbar used for moving MH-60S

Back 47

24 ALBAR

Front 48

How and Why slew stab prior to move

Back 48

You slew the stab to 0 by connecting external power, with all 5 stab CB open, to maximize the tow tractors view of the PC

Front 49

# of people for a move and positions

Back 49

6; Brake rider, PC, Tow Tractor, Safety Observer, and 2 wing walkers

Front 50

Max towing speed of A/C on flight line

Back 50

5 MPH or as fast as slowest wing walker

Front 51

How far will A/C travel at 5 MPH

Back 51

Aprox. 7.3 feet

Front 52

How far will A/C move after unexpected stop on a move

Back 52

6-9 feet

Front 53

Who can authorize move without brake

Back 53

The MO

Front 54

# of people for move without brakes

Back 54

7; PC, Tow Tractor, Safety Observer, 2 wing walkers and 2 chock walkers

Front 55

Pubs for move procedures

Back 55

00-80T-96

17-1-537

GAI-010 Tow and Park Helicopter

Front 56

If you strike something during a move

Back 56

Stop the bird, chock the bird, and alert maintenance control and QA; Do not move the bird

Front 57

PDIs

Back 57

Pressure Differential Indicators; 14; 2 on each engine and hyrdaulic pump, one on the PAM (Pilot Assist Module) and the MGB oil filter; located on a filter

Front 58

Elastomeric bearings

Back 58

22; 2 on each PCR (Pitch Control Rod), 2 on each PCL (Pitch Control Link), one on each spindle and 2 on the stab (Port)

Front 59

CADs on A/C with BRUs installed

Back 59

Cartridge Actuated Device; Bomb Rack Unit;10; 2 on each fire bottle, 2 on each BRU (port and starboard) 1 on the cargo hook and 1 on rescue hoist

Front 60

ADB

Back 60

Aircraft Discrepancy Book

Front 61

Chip Detectors

Back 61

9 total; one in each input module, accessory box and engine, and MGB, IGB, and TGB; Gearboxes contain an igniter to burn off particles it collects.

Front 62

PUB for Daily, how long it suppose to take and how long is it good for

Back 62

MRC-300; 30 min at the least unless split amongst PCs and 72 hours

Front 63

PUB for Turnaround

Back 63

MRC-100 and 24 hours

Front 64

First thing to do before starting daily

Back 64

Screen the open work orders on ADB to avoid duplicate MAFs

Front 65

# of drive shafts and the longest one

Back 65

6 total with the sixth one as the longest

Front 66

# of hydraulics pumps

Back 66

4 total; 3 in hyds bay and the utility pump is the on the MGB with the reservoir located in the oil cooler section

Front 67

DEMOT

Back 67

System used by pilot to call troubleshooter each letter indicated a different rate;

T1- AD

T2- AE

T3- AM

T4-AO

T5-AT

T6-QA

T7/Scissors- PR

Front 68

2 mandatory hand signals

Back 68

Hold and Wave-Off

Front 69

Wind restrictions for folding tail/blades

Back 69

45 knots

Front 70

# of people to fold tail

Back 70

5; 3 on fold pole, 1 on stab and 1 on wrench/stab brick

Front 71

Why turn on battery while folding tail

Back 71

to engage the tail rotor indexer

Front 72

When spreading bird from completely folded which is first and why

Back 72

Tail first; if restraints are removed first trim tab on black blade may be damaged

Front 73

Correct order to remove restraint gear from blades before spreading

Back 73

Forward to aft; Yellow, Blue, Black, Red; allowing no blade to come in contact with one another

Front 74

When folding bird from a completely spread position what do you fold first

Back 74

fold blades first then tail; if you fold the tail first the blades will be damaged by crashing into the tail

Front 75

Correct order to install restraints blades after folding

Back 75

Aft to Forward; Red, Black, Blue, Yellow; this way keeps blades from coming in contact with one another

Front 76

Can you check servicing on IGB/TGB if tail is serviced

Back 76

No. Tail being folded will give an incorrect reading

Front 77

Leak limit for hydraulic swivel and why

Back 77

1 drop every 24 hrs; hydraulic swivel holds all hyds fluid leading to tail rotor and if leaking results in lose of all flight controls in tail

Front 78

Colors on a hydraulic pump

Back 78

Red, Green and Blue

Front 79

How far over serviced can hydraulic pump be

Back 79

3/8th of an inch

Front 80

4 things to look for on a head check

Back 80

Lockpin pullers fully retraced

Blade lockpins fully inserted

main rotor indexer retracted (gust lock free)

Tail rotor indexer retracted

Front 81

What does BIM stand for and what is being tested when you check it

Back 81

Blade Inspection Method; Checking BIM to see if it works, 3 black stripes should appear within 30 sec in BIM is working correctly. BIM appears black if there is a nitrogen leak in spar

Front 82

Oil capacity for MGB

Back 82

7.5 gallons

Front 83

Oil capacity for TGB and IGB and where can information be found

Back 83

2.75 quarts; NATOPS Ch. 3

Front 84

Oil capacity of each engine

Back 84

7.3 quarts

Front 85

Capacity of Hydraulic Reservoir (coffee can)

Back 85

1.3 quarts

Front 86

Popped Fastener Rule

Back 86

3,2,1; No 3 on a single panel/cowling, no 2 in a row, and no 1 in a corner

Front 87

Where can you find the limits for the MRH (Main Rotor Head) accumulator and why is this important

Back 87

In IETMs, Air Vehicle, General Aircraft Information, Servicing in figures 8 and 10; A1-H60CA/SA-GAI-000, WP 007; It's important to know where to find the charts because the nitrogen is temperature dependent

Front 88

Hazard associated with copper beryllium

Back 88

If copper beryllium dust in inhaled or ingested it will give you CANCER

Front 89

Components made of copper beryllium on 60S

Back 89

Droop Stops, Pitch Lock Housing and Lockpin Pullers

Front 90

How much play allowed in Lockpin Pullers

Back 90

1/4 rotation

Front 91

How do you check the pressure gage on the Fire Bottles

Back 91

Read temperature chart on the side of the bottles

Front 92

Can you turn on hydraulics while someone is on the head

Back 92

Yes, with a safety observer

Front 93

How do you perform a teeter test and what are you testing

Back 93

Pull back and move forward on paddle 3-4inchs and verify little to no movement on the opposing paddle. A teeter test is testing the outboard retention plate

Front 94

How to check oil filler cap for security on TGB an IGB

Back 94

Pull on cap with three fingers in an upward motion

Front 95

What components do we log oil consumption

Back 95

Engines, IGB and TGB; Fill out the oil consumption table in the hard copy ADB in maintenance control

Front 96

Acceptable oil consumption rate for engines

Back 96

4.5 ounces per flight hour

Front 97

What are primary servos and where are they located

Back 97

Primary flight controls, Forward, Aft and Lateral Aft of work platform in hyds bay

Front 98

What are secondary servos, location, and which are trim and boost servos

Back 98

Yaw/Boost w/ Power Pistons

Roll/Trim

Pitch/Trim

Collective/Boost w/ Power Pistons

Forward of work platform in hyds bay

Front 99

Proper Flight Deck PPE

Back 99

Long Sleeve Jersey

Flight Deck Pants

Steel Toed Flight Deck Boots

Cranial

Leather Gloves

Front 100

Tiedown requirement for 60S

Back 100

Initial - 4 chains

Intermediate - 8 chains

Permanent - 12 chains

Heavy Weather - 16 or as many as can fit

Front 101

type of chain used for tie downs

Back 101

TD1-B

Front 102

How many tiedown points are on the A/C

Back 102

6; 1 at each main mount, one above each main mount and on eon either side above the tail land gear; HOIST POINT ARE NOT TIEDOWN POINT EXCEPT IN EMERGENCY SITUATIONS

Front 103

Difference in 7 and 14 day afloat compared to ashore

Back 103

7 day out to sea is a wash job and a 14 day is for circuit breakers

Front 104

When are doghouse straps required

Back 104

Anytime out to sea and anytime wind is grater than 10 knots

Front 105

Special precautions taken when brake riding from EL (elevator) to the flight deck

Back 105

Removal of CO2 cartridge in float coat to prevent auto inflation

Front 106

Must be removed from A/C before being moved into the hanger bay

Back 106

Smokes (flairs); considered live ordinance thus cant be in helo while riding EL

Front 107

Who does LSE ask for permission for all helo evolutions

Back 107

Primary

Front 108

When does LSE talk to dog

Back 108

Start of APU and spreading the A/C

Front 109

Difference is landing helo on spot 2-8 and 1 and 9

Back 109

2 through 8 - you stand directly on number

1 and 9 - you land helo directly on the number

Front 110

Jet ops while trying to land helo on spot 7

Back 110

first make sure no fixed wing A/C are in final approach, if so hold the pilots in a hover off the deck until the fixed wing lands and then bring them over the deck for their landing

Front 111

When do you ask primary for permission to start engines

Back 111

As soon at position lights begin to flash

Front 112

When do you ask primary for permission to brake and hold

Back 112

When position lights go steady

Front 113

Rotary beacon color indications for helo

Back 113

Green - Clear to land/lift

Red - Clear start/shut down

Amber - Clear to engage/disengage rotors

Front 114

Authorization of bird move without brakes while afloat

Back 114

The Handler

Front 115

PUB for Special Inspections

Back 115

MRC-350

Front 116

PUB for Conditional

Back 116

MRC-390

Front 117

ORM

Back 117

I - Identifying Hazards

A - Assessing Hazards

M - Making Risk Decisions

I - Implementing Controls

S - Supervising

Front 118

Define Warning

Back 118

Operating procedure or practice that could result in injury or death; highlighted in red in IETM

Front 119

Define Caution

Back 119

Operating procedure or practice that could result in damage or destruction of equipment; highlighted in yellow in IETM

Front 120

Define Note

Back 120

Operating procedure or condition that requires emphasis

Front 121

3 ways to start engine

Back 121

Ground Pneumatic Source

APU

Engine Cross Bleed

Front 122

HERO

Back 122

Hazards of Electromagnetic Radiation, to Ordinance; safe, unsafe, and suspendable

Front 123

Over serviced TGB

Back 123

Write MAF for AD CDI to inspect; possible contamination

Front 124

Corrosion of Aluminum

Back 124

White or gray powder

Front 125

Corrosion of Magnesium

Back 125

White powdery snow-like mounds and white spots on surface

Front 126

Corrosion of copper beryllium

Back 126

Blue or blue green powdery substance

Front 127

Time after shutdown when engine oil can be checked

Back 127

20 min

Front 128

Engine Model for H-60S

Back 128

T700GE-401C (General Electric)

Front 129

Responsible to brief pilot of A/C material readiness

Back 129

Plane Captian

Front 130

Plane Captain Manual Pub

Back 130

GAI-010

Front 131

General Aircraft Pub

Back 131

GAI-000

Front 132

Aircraft Fueling Pub

Back 132

00-80T-109; NATOPS

Front 133

Basic Support Equipment Handling and Safety

Back 133

000-80T-96

Front 134

Aircraft Signals Pub

Back 134

00-80T-113; NATOPS

Front 135

Aircraft Securing and Handling Pub

Back 135

17-1-537

Front 136

Cleaning and Corrosion Manual

Back 136

01-1A-509 VOL I-V

Front 137

DTA Paperwork

Back 137

4790/58

Front 138

Acceptance Sheet Paperwork

Back 138

4790/141

Front 139

Pre-Op Card

Back 139

4790/52

Front 140

MAF Form

Back 140

Maintenance Action Form; 4790/60

Front 141

Safe distance for refueling from another aircraft or structure and radar

Back 141

50 feet from aircraft/structure and 75 from radar

Front 142

Red and Blue meaning in ADB

Back 142

Red: down

Blue: Partially Mission Capable

Front 143

Max pressure on refueling

Back 143

55 psi

Front 144

Pressure for refueling

Back 144

-3 or 2 psi

Front 145

Can APU be started with someone on head and/or tail

Back 145

No Head

Yes Tail

Front 146

Difference in JP-5 and JP-8

Back 146

JP-5 Shipboard and land use

JP-8 Not authorized for shipboard use

Front 147

What does SDS stand for

Back 147

Safety Data Sheet; has all hazmat information