Misc

Question 1

NATOPS

Answer 1

Naval Air Training and Operating Procedures Standardization

A positive approach toward improving combat readiness and achieving a substantial reduction in the aircraft mishap rate.

Question 2

Primary Missions

Answer 2

SUW, ASW, CC, NCO, EW

Question 3

NAMP Programs

Answer 3

Naval Oil Analysis Program (NOAP)
Tire and Wheel
Support Equipment Part Management (SE PMS)
Electrostatic Discharge (ESD)
HAZMAT
Aircraft Confined Space Program (ACSP)
Battery Safety
EWIS

310: FOD, Fuel Surveillance, PC

Question 4

General Preflight

Answer 4

FOD, corrosion, condition, and security

Question 5

Operational Necessity

Answer 5

A mission associated with war or peacetime operations in which the consequences of an action justify the loss of aircraft and crew.

Question 6

Maintainer Rates

Answer 6

AD: Aviation Machinist's Mate
AE: Aviation Electrician's Mate
AM: Aviation Structural Mechanic
AO: Aviation Ordnanceman
AT: Aviation Electronics Technician

AZ: Aviation Maintenance Administrationman
PR: Aircrew Survival Equipmentman

Question 7

Aircraft Tiedown Configurations

Answer 7

Initial: 4 total (2 on each main mount): prior to and after shipboard aircraft movement, during shipboard aircraft startup, and immediately after landing.

Permanent: 12 total (2 on each attachment point; mains, highs, tails): required aboard ship when not a flight quarters.

Heavy Weather: 18 total (3 on each attachment point; mains, highs, tails): required with surface winds reach average of 35 knots or greater and/or seas greater than 8 feet or when wind across the deck is in excess of 60 knots or with rolls greater than 12 and pitches greater than 4.

Question 8

HYD Leak Test Requirements and Lights

Answer 8

1. AC Power
2. WOW
3. Rotors Engaged
4. All Reservoirs Full
5. BACKUP HYD PUMP in AUTO

10 TOTAL: BACKUP PUMP ON, BACKUP RSVR LOW, SAS, BOOST SERVOS OFF, #2 RSVR LOW, #1 TR SERVO, #2 TR SERVO, #1 RSVR LOW, AFCS DEGRADED, MASTER CAUTION

Question 9

Automatic Preflight Test Requirements

Answer 9

1. WOW
2. Rotor Brake ON
3. TRQs below 10%
4. EGI Attitude Valid
5. SAS 1 PB on after AFCC on for 20 seconds

Question 10

Recommended Actions to Center the Cable

Answer 10

1. Use cyclic four way trim to command the aircraft in the corrective direction
2. Fly against lateral trim
3. Use trim release button, reposition
4. Fly against the longitudinal trim

A manual longitudinal correction against trim of 3% for 2 or more seconds will remove cable angle solution and requires 20 seconds for a new solution.

Question 11

Inputs to STAB

Answer 11

Collective position
Lateral acceleration
Airspeed
Pitch rate

Question 12

Flight Control Mixing

Answer 12

Collective to yaw
Collective to lateral
Collective to longitudinal
Yaw to longitudinal
Collective/Airspeed to Yaw (nose tries to yaw left with airspeed, compensation is provided by a trim input)

Question 13

Droops and Flaps

Answer 13

Droops go out at 70% and seat around 50%

Anti-flap restraints should go out at 35%

Question 14

ECS TRQ and Fuel Flows

Answer 14

ECS ON / FLOW NORM: TRQ reduced by 4% per engine and fuel increase of 8 lbs per hour per engine

TEMP in HOT below 15 C: TRQ reduced by 5% per engine

FLOW HIGH: TRW reduced by 7% per engine and fuel increase of 45 lbs per hour per engine

APU to power ECS: fuel flow increase of 150 lbs per hour

Question 15

Starter Disengagement

Answer 15

1. Pulling down on PCL
2. Pulling CB
3. Removing the air source

Question 16

Malfunctioning Engine AA/Start-Bleed Valve

Answer 16

1. Advisory on greater than 90% Ng or greater than 94% Ng with OAT 15 C or greater
2. No advisory with Ng less than 88%
3. No advisory with Engine AA switch ON
4. No rise in TGT with Engine AA switch ON

90 94 15 88 NANT

Normal TGT rise: 30 to 100 degrees C

Question 17

Secondary Missions

Answer 17

AMW, AW, HS, FS, INT, LOG, NSW