Wing SOP 3710.7H /HSM-50 SOP 3710.1 Flashcards

1
Q

Flight Schedule procedures

A

a. The Squadron Duty Officer (SDO) is responsible for overseeing the execution of the daily flight schedule.

When changes to the flight schedule need to be made, those changes must be annotated on the master flight schedule and approved by the Commanding Officer (CO).

In the absence of the CO, the Executive Officer (XO), or in the absence of the XO, the Operations Officer may approve the changes. If none of the above personnel are available, the SDO is authorized to make the required change. When a change is made, the SDO shall ensure all requirements of reference (a), paragraph 4.6.1 have been met.

b. When conducting embarked detachment operations, changes to a published flight schedule shall be approved by the ship’s CO and the Detachment Officer-in-Charge (OIC).

(50) d. Snivel requests will be honored to the maximum extent practicable until the Wednesday prior to the following week. All snivel approvals will be at the discretion of the Operations Officer and all “short-fused” requests will require the individual to find a suitable replacement if necessary. The CO maintains the ultimate authority on recurring snivel requests.

Ref A: CNAF
4.6.1
WARPSWIM

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2
Q

Weather Criteria

A

a. In addition to weather criteria delineated in references (a), (b) and, (c) and local area course rules, the following minimums apply (ceiling/visibility):

(1) Shore or Ship Operations -500/1 *

*NOTE 1: If positive radar control and a Carrier Controlled Approach (CCA), Precision Approach Radar (PAR), or Instrument Landing System (ILS) is available for recovery, minimum launch weather minimums are 200-1/2.

Ref A: CNAF
Ref B: Naval SAR Program
Ref C: NATOPS

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3
Q

Crew Requirements: Personnel outside of command

A

Minimum crew requirements shall be followed per references (a) and (c).

The following additional guidance is provided:

a. COs may elect to recognize the qualifications (Helicopter Aircraft Commander (HAC), Weapons and Tactics Instructor, Night Systems Instructor, etc.) of specific H-60 series aircraft qualified Aircrew from outside their command and may also recognize the qualifications of any H-60 series aircraft qualified enlisted Aircrewmen. Qualification documentation shall be provided upon request. All visiting Aircrew shall comply with the reporting custodian’s Standard Operating Procedures (SOP)…

(50) and verify review of the HSM-50 R&I board.

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4
Q

Crew Requirements: Enlisted Aircrew

A

Minimum crew requirements shall be followed per references (a) and (c). The following additional guidance is provided:

b. Enlisted Aircrew should be utilized to the maximum extent practicable on all flights.

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5
Q

Crew Requirements: FCF Crew

A

Minimum crew requirements shall be followed per references (a) and (c). The following additional guidance is provided:

c. Functional Check Flight (FCF) checklist items shall only be conducted when the crew includes a designated Functional Check Pilot (FCP). COs shall designate minimum crew requirements for ground maintenance turns. Temporary Flight Orders personnel shall not be carried on FCFs for the sole purpose of accumulating flight time…

(50) Minimum crew for HSM-50 Non-FCF ground turns shall consist of at least 2 designated H2Ps

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6
Q

Crew Requirements: Tactical Training Events

A

Minimum crew requirements shall be followed per references (a) and (c). The following additional guidance is provided:

d. Minimum crew requirements for tactical training events unless otherwise specified are: HAC/L3, Pilot Qualified in Model, and Aircrewmen.

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7
Q

Currency Requirements: Pilot warm up flights and Check in Flights

A

a. In addition to minimum pilot and Aircrew currency requirements outlined in references (a), (c) and (g), and local course rules requirements, any pilot who has not flown in 45 days shall fly a warm-up flight with a current HAC. Warm-up flights should include autorotations and other FAM type maneuvers as determined by squadron COs.

(50) All pilots checking into the squadron shall fly a standardization flight with a Stan Board member and pass a course rules/SOP exam. Pilots returning from extended deployments over 90 days should complete a course rules/SOP exam and should complete an EP simulator.

(50) All Aircrewmen who have not flown in 45 days shall complete a flight with a current Aircrewman.

Ref a: CNAF
Ref c: NATOPS
Ref g: COMNAVAIRFORINST 3500.1 (HSM FCF Reqs)

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8
Q

Currency Requirements: Night currency

A

b. Pilots shall not fly at night as Pilot in Command (PIC) unless they are night current. To be considered night current, a Pilot shall have flown a minimum of2.0 night hours within the preceding 45 days. Between 45 and 60 days, the squadron CO may authorize a day into night transition to regain night currency. After 60 days, currency shall be regained by flying with a night current PIC.

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9
Q

Currency Requirements: LSO

A

c. All Pilots and Landing Safety Officers (LSOs) shall complete LSO qualification with a current LSO per references (c) and (f). For embarked detachments, qualified LSOs shall be designated in writing by the ship’s CO for deployment. When acting as LSO on a ship for a short duration evolution (e.g. Deck Landing Qualifications {DLQs), Integrated Ship Air Training Team (ISA TT)), the LSO does not need to be designated by the ship’s CO, but shall brief the ship’s CO or Officer of the Deck (OOD) prior to commencing DLQ evolutions.

Ref C: NATOPS
Ref F: ACS PQS

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10
Q

Currency Requirements: DLQs/Shipboard Ops

A

d. Shipboard Operations. In addition to the currency requirements in reference (c), the following standards are provided:

(I) Pilots whose night DLQ currency lapses while at the parent squadron’s home base shall conduct an Operational Flight Trainer or night Field Deck Landing Practice event within 30 days of scheduled DLQ requalification periods. During this event, Pilots shall complete no fewer than three evolutions (takeoff, downwind, approach and landing), emphasizing DLQ-specific communications and Crew Resource Management (CRM). When practical, these events should be conducted with the same Aircrew expected to participate in the scheduled DLQ requalification flight.

If the currency of all Pilots within a squadron or detachment lapses while deployed, the CO shall attempt to regain currency through use of an H-60-series current HAC from another unit. If the operational situation precludes compliance, a waiver to the unit’s Major Command ISIC (CVW or Type Wing) shall be submitted and a deliberate, risk mitigated approach shall be employed to allow non-current HACs to regain currency.

Ref c: NATOPS
Ref f: ACS PQS

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11
Q

Currency Requirements: Short ISATT

A

d. Shipboard Operations. In addition to the currency requirements in reference (c), the following standards are provided:

(2) If detachments experience an OIC change, ship Change of Command (Fleet-up XOs to COs are exempt), reassignment to a new ship, or more than 60 days elapse between embarked operations, the detachment shall conduct the following embarked training evolutions to reestablish readiness before resuming operations and continuing the work-up schedule. It is not required to have an ISA TT observer present during this warm-up period:

(a) Day and night landing evolutions

(b) Emergency flight quarters

(c) Crash on deck drill

(d) Hot refueling

(e) Straightening and traversing evolutions

(f) Emergency Low Visibility Approach (ELVA)/Self-contained Approach

(g) Lost Plane Homing

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12
Q

Currency Requirements: Pre-embarkation proficiency

A

To the maximum extent practicable, Pilots should fly a minimum of 9 hours within the 45 days preceding fly-on for an underway period. Pilots shall obtain night currency (2.0 hours within 45 days) and instrument currency (2.0 hours within 60 days) prior to the embarkation flight. During intervals of 45 days or less between embarked operations, Pilots should fly a minimum of six hours and achieve night and instrument currency prior to the next embarkation.

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13
Q

Currency Requirements: Night Coupler Currency

A

f. To be night coupler current per reference (b), the PIC shall have flown two windline rescue or Night/Instrument Meteorological Conditions (IMC) dip-to-dip patterns to automatic approaches to a coupled hover at night in the preceding 60 days. PICs failing to meet this requirement shall not be scheduled to fly night search and rescue (SAR) missions (to include Plane Guard).

Ref B: OPNAVINST 3130.6 (Navy SAR Manual)

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14
Q

Currency requirements: Instruments

A

To be considered instrument flight current, Pilots shall have flown a minimum of 2.0 hours of simulated or actual instrument time within-the preceding 60 days. Currency requirements may be satisfied in the aircraft or flight simulator. If currency lapses, it must be regained prior to flying any other missions in the aircraft as the PIC.

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15
Q

Currency Requirements: Illumination info

A

h. Night Environment. Deriving illumination information for planning and briefing night operations shall be done per reference (a). The Sun and Moon tool (SUMO), which is included in Joint Mission Planning Software, is also authorized for environmental planning.

Ref A: CNAF

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16
Q

Crew Rest: Ashore

A

a. Ashore, in addition to section 8.3 of reference (a), the following minimum crew rest policy is applicable:

(1) Aircrew shall not be scheduled to brief a flight event until 10 hours after completion of post-flight duties.

(50) (2) Aircrew should not report earlier than 12 hours prior to the scheduled completion of all flight and post-flight duties. Standard post flight duties are approximately one hour after scheduled land time and two hours after scheduled land time following a Gunnery Exercise (GUNNEX) for gun cleaning.

Ref A: CNAF

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17
Q

Crew Rest: At sea

A

b. At sea, Detachment OICs shall comply with and ensure ship COs are briefed on paragraph 8.3.2.1 and 8.3.2.2 ofreference (a).

Ref a: CNAF

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18
Q

Radius of action

A

The following radius of action ranges are maximum ranges. PICs shall give due consideration to paragraph 4.1.2.1 of reference ( d) prior to embarking on a mission. Particular attention must be paid during peacetime operations to environmental conditions (water temperature, sea state, winds, etc.) and availability of assets to conduct a SAR in a timely manner.

a. Shipboard radius of action is 150 Nautical Miles (NM) or maximum reliable navigation or communication range, whichever is less. Radius of action beyond 150 NM in support of specific operational or tactical training missions may be approved by assigned CVW Commander (or Type-Wing Commander when independently deployed), provided deliberate ORM has been conducted. Time spent beyond 150 NM shall be limited to the minimum required to accomplish mission objectives.

b. One-way flights ship-to-ship or shore-to-ship shall be limited to 150 NM (or 200 NM with a functioning AUX tank). Ship-to-shore range is 200 NM (or 250 NM with a functioning AUX tank)shore being defined as the nearest point at which a safe landing can be made.

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19
Q

Pax/Orientation/Indoc flights: embarkation of pax and minimum crew requirements

A

a. References (a) through (d) provide guidance on the embarkation of passengers and minimum crew requirements.

Ref a: CNAF
Ref b: OPNAVINST 3130.6 (Navy SAR Manual)
Ref c: NATOPS
Ref d: 80T-122

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20
Q

Pax/Orientation/Indoc flights: Pax Embarked/Orientation prohibited

A

b. Simulated emergencies, practice autorotation, intentional aircraft degradations and ordnance release shall not be performed with passengers embarked or during orientation flights (to include midshipman familiarization flights) .

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21
Q

Pax/Orientation/Indoc flights: Orientee requirements

A

c. Completion of Naval Aviation Survival Training Program (NASTP) is mandatory for all orientees unless waived in rare cases by designated approval authority per section 3.3 ofreference (a).

(1) Personnel participating in orientation flights shall receive appropriate screenings directed in section 3.3.4 of reference (a).

(2) Documentation of NASTP waivers shall be forwarded to CNAF N455 via the wing Safety Officer.

Ref A: CNAF

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22
Q

Low Level Flight Procedures

A

Unless dictated by operational requirements or as directed/required by controlling agencies, published restrictions, or approved training ranges, the following minimum Above-Ground Level (AGL) flight altitudes shall be observed:

a. Overland:
Populated Area: 1000’ AGL
Unpopulated Area: 500’ AGL

b. Overwater:
Day: 50’ AGL
Unaided Night: 150’ AGL
NVD: 100’ AGL

*NOTE: Flight operations down to 50’ over water during day conditions is intended for operational or tactical training flights where the altitude profiles support authorized mission or training objectives.

c. Coupled Hover: 70’ AGL*

*NOTE: Following establishment of a steady coupled hover at 70’, aircraft altitude may be reduced to no lower than 40’ to conduct live hoisting operations at the PIC’s discretion.

d. Terrain Flight (Low Level Routes): 200’ AGL (Only on approved low level routes and ranges).

e. SACT Training:
Day: 100’ AGL
Night: 500’ AGL

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23
Q

Checklists: Format

A

All checklists shall be verbally completed in the CHALLENGE-REPLY-REPLY format up to rotor engagement. After rotor engagement, checklists shall be in the CHALLENGE-REPLY format. When necessary to avoid interference with other cockpit duties and when safety of flight is a consideration, checklists may be performed silently by the Pilot Not At Controls (PNAC), except for items that require a response by another crewmember to ensure their completion.

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24
Q

Checklists: STAB AUTO MODE PBS not illuminated

A

a. If the STABILATOR AUTO MODE PBS is not illuminated when AC power is applied, stabilator lock pins shall be visually checked prior to flight.

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25
Q

Checklists: Rescue hoist op check

A

b. The Rescue Hoist Operational Check should be completed on the first flight of the day to ensure SAR capability.

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26
Q

Checklists: Callouts

A

c. Single engine airspeed and stabilator programming shall be called on the first takeoff of each flight and stabilator programming shall be called after reengaging the AUTO mode subsequent to a simulated or actual failure.

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27
Q

Checklists: Pad/runway transition

A

d. The landing checklist shall be accomplished when transitioning from pad to runway operations or vice versa.

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28
Q

Checklists: In Flt Msn Change

A

e. In-Flight Mission Change Checklist. Aircrew shall utilize the In-Flight Mission Change Checklist any time that the mission is altered from what was briefed.

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29
Q

Hot refueling/crew switch

A

a. Passengers shall not occupy the aircraft during hot refueling.

b. During crew switches, the helicopter shall be under the control of a designated helicopter Pilot and there shall be a PIC-to-PIC verbal turnover. The new crew shall begin with step 10 of the “Post Engagement Checks.”

c. Personnel shall not proceed aft of countermeasures dispensers, unless arming/de-arming the system, while rotors are turning.

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30
Q

Air Taxi

A

Aircraft shall ground taxi vice air taxi to the greatest extent possible whenever the possibility of damage from rotor wash exists.

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31
Q

Inter Squadron Ops

A

Flights such as DLQs, detachment fly-offs, and section/formation operations, where multiple squadrons may participate, require a joint brief between PI Cs. This brief may be face-to-face, PHONECON, VTC/GVS, message, email or per SOPs as applicable.

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32
Q

Use of Seat Belts

A

Seat and shoulder harnesses shall be utilized to the maximum extent possible per references (a) and (c). All occupants of the aircraft shall be in crash worthy seats with seat and shoulder harness secured with the exception of Aircrewman participating in

CVN launches or recoveries
hoist operations
troubleshooting
crew-served weapons operation
night formation flying
CAL/LZ flights
other mission-specific situations deemed necessary by the PIC.

The PIC must carefully weigh the risk of potential injury or death of crewmembers against the benefit of the mobility provided by Aircrew in gunner’s belts.

Ref A: CNAF
Ref C: NATOPS

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33
Q

Flight Demo Guidelines

A

The following guidance is provided for all flight demonstrations and flyovers:

a. Per reference (h), all flyovers should be:

( 1) Non-maneuvering, generally wings-level passes of one to two aircraft (waiverable to four).

(2) Restricted to a single pass over a fixed point at a specified time.

(3) Conducted no lower than 500’ AGL, with consideration given to the height of obstacles in the vicinity of the flyover location.

(4) Conducted no slower than 60 KIAS.

b. Any deviations to the above requirements, such as lower altitudes, obstacle clearance, airspeeds, multiple passes or other maneuvers must be specifically requested through Type Wing for TYCOM approval and will be considered on a case-by-case basis.

c. Flight demonstrations involving other than flyover profiles (Family Day/Tiger Cruise/Air Show/SAR Demonstration) are considered Aerial Demonstrations and requests must be submitted per reference (h).

Ref h: COMNAVAIRFORINST 3710.8

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34
Q

Det Concurrent Ops

A

a. Detachments operating on single-spot ships with two manned embarked helicopters utilizing the Rapid Securing Device (RSD) shall not conduct concurrent flight operations unless an emergency landing site (shore or ship) is available within 50 NM for the duration of the evolution.

b. The 50 NM alternate landing site requirement applies to missions where the parent ship is the intended point of landing for both aircraft, and does not apply to missions scheduled for termination at other than the parent ship. The 50 NM requirement does not apply to fly-ons for scheduled embarkations. For fly-ons, thorough prior mission planning shall be conducted and no-go criteria determined, which takes into consideration potential flight-deck/hangaring delays.

c. The 50 NM alternate landing site limitation does not apply for concurrent manned/unmanned flight operations.

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35
Q

Staged/Mission related photography

A

As per guidance set forth in reference (m).

Ref m: COMNAVAIRFORINST 5510.18

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36
Q

APU Ops

A

When the APU is required in-flight to support essential operations, per reference (c), it should be started on deck to the maximum extent possible.

Ref C: NATOPS

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37
Q

Vertrep Power Margin

A

When conducting vertical replenishment (VERTREP) training, a 10 percent power margin shall exist between Maximum Rated Power (MRP) and maximum power required when a load is lifted from the deck.

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38
Q

RADALT Discipline/Settings

A

a. During night overwater flight below 500 FT AGL, consideration should be given to setting the Decision Height (DH) no lower than 10 percent less than the current altitude. When operating in the shipboard landing pattern, each Pilot’s DH should be set to an altitude determined by the crew that best facilitates CRM. Each crewmember shall verbalize to the crew their DH settings and activation of warning tones.

b. In addition to night/IMC descent procedures in reference (c), all crewmembers should acknowledge when an altitude warning system aural tone is activated. This is not expected when operating in a traffic pattern.

Ref c: NATOPS

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39
Q

Dipping Sonar Ops: Steady Hover

A

a. NATOPS Dipping Sonar/Coupled Hover Procedures item 8 “Establish a steady coupled hover” shall be completed prior to “DOWN DOME”. PNAC should adjust LONG VEL and LAT VEL potentiometers to control drift and limit groundspeed to no greater than 2 kts (drift limits do not apply while in sonar cable angle mode).

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40
Q

Dipping Sonar Ops: Cable Angle

A

b. Cable angle hover mode shall be operable for all dipping sonar operations. Submerged Override shall not be used for routine operations.

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41
Q

Dipping Sonar Ops: Environmentals

A

c. Dipping sonar operations should not be conducted in seas with wave heights exceeding 10 feet during unit-level training or fleet-level exercises. Pre-flight deliberate ORM and in-flight time critical ORM assessments of forecasted or observed sea state conditions shall be accomplished prior to dipping sonar operations.

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42
Q

Dipping Sonar Ops: POCL

A

d. During dipping sonar training operations (with or without a submarine), Payed-Out Cable Length (POCL) shall be no more than half the ceiling up to 1,000 FT ceiling. When ceilings are above 1,000 FT, POCL shall be no more than 500 FT below ceiling. During operational ASW involving a submarine, under conditions that preclude a freestream recovery, then POCL need not be restricted. However, ORM shall be conducted to minimize the risk to the transducer assembly in the event of a malfunction.

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43
Q

Dipping Sonar Ops: AFCS

A

e. Dipping operations are prohibited with Automatic Flight Control System (AFCS) degradations affecting Automatic Approach, Coupled Hover, or Cable Angle hover functions.

44
Q

Dipping Sonar Ops: Code

A

f. With an 1177 fault (to include on MBIT), cease dipping operations until maintenance action is performed.

45
Q

Dipping Sonar Ops: Towing Limits

A

g. If transducer towing groundspeed limits are exceeded, cease dipping operations and document on a Maintenance Action Form (MAF).

46
Q

Dipping Sonar Ops: Level 2

A

H. While operating in a squadron’s local area for unit-level training, an ACTC Level II Sensor Operator shall be in the helicopter on any flight in which dipping is intended.

47
Q

Hung Dome Procedures

A

In the event of a hung dome, it is assumed the crew has exhausted all means of recovering the dome and all emergency procedures have been completed per references ( c) and (d). The following considerations/procedures apply:

a. If embarked, the Air Boss or HCO shall ensure all personnel are clear of the landing spot with the exception of the minimum number of maintenance personnel required (approximately four).

b. Consideration should be given to securing a mattress or padding to the deck either on or adjacent to the landing spot, POCL dependent, with tie down straps to provide a cushion onto which the dome could be lowered in order to minimize damage.

c. The aircraft should hover at an appropriate altitude to facilitate recovery. Maximum safe altitude will depend on POCL and environmental considerations. The Landing Signalman Enlisted (LSE) should be positioned in the best location to provide signals for placing the dome on the deck.

d. Conditions will dictate whether the cable will be sheared or the dome lowered to the deck. If lowered to the deck and sufficient POCL exists to allow maintenance personnel to disconnect the dome, they shall ensure the dome is grounded to prevent electrical shock and will then disconnect the dome from the cable. After the dome is detached, the aircraft will begin a descent and cable shall be walked with two-person integrity away from the landing spot. Ifthere is insufficient POCL to allow maintainers to safely work under the aircraft, the crew may opt to lower the dome onto the padding and then slide over to land. If at any time, a stable hover cannot be maintained during or after disconnecting the dome and during the descent, the crew shall execute the appropriate emergency procedure to facilitate safe recovery.

e. After landing and placement of chocks and chains, the cable should be placed in the aircraft cabin prior to aircraft shutdown.

Ref C: NATOPS
Ref D: 80T-122

48
Q

EKB Usage

A

Pilots and Aircrewmen are authorized to utilize electronic tablets as an Electronic Kneeboard (EKB) while airborne in accordance with reference (k). Prior to using an EKB in flight, all crewmembers shall be briefed on who is using a tablet, for what purpose, and any inflight duties shifting to other crewmembers while the tablet user is heads-down.

Ref k: interim flight clearance for EKBs

49
Q

PEDs

A

a. During the employment of classified systems or tactics non-Government-furnished PEDs and PPEDs not approved for use by an Authorizing Official are prohibited from being in the aircraft unless secured in a Faraday bag IAW reference (m).

Ref M: COMNAVAIRFORINST 5510.18

50
Q

Body Armor Usage

A

In the absence of theater commander’s guidance, hard body armor shall not be worn in the CMU-37/38 by Aircrew on missions over water. All Pilots and Aircrew shall be briefed on the risks and benefits of soft body armor. Use of soft body armor is at the individual’s discretion.

51
Q

Ordnance Safety: Hot refueling/seats w/ ordnance

A

a. Per reference (n), hot refueling aircraft with live ordnance loaded (Hellfire, loaded Digital Rocket Launcher [DRL], flares, and warshot torpedoes) is prohibited ashore. Hot refueling ashore with chaff or decoy flares may be subject to local directives that are more restrictive than NA VAIR 00-80T-103. Hellfire are authorized to be carried during hot seats ashore IA W the guidance set forth in reference (n). Hot and cold refueling with ordnance loaded is permitted at sea with approval from the ship’s CO.

Ref N: 80T-103

52
Q

Ordnance Safety: Shipboard approaches w/ ordnance

A

b. Aircrews are authorized to conduct multiple shipboard approaches and landings with missiles or rockets loaded with concurrence of the ship’s CO.

53
Q

Ordnance Safety: Straighten/Traversing w/ Hellfire

A

c. Shipboard straightening, maneuvering and traversing of the aircraft while loaded with Hellfire CATMs shall be limited to traverse qualified personnel. Straightening, maneuvering and traverse training with CATMs loaded is prohibited. Downloading warshot missiles shall be conducted prior to any of the above evolutions, except in an emergency with the specific authorization of the ship’s CO. Traversing at slow speed between the maintenance line and the flight position with warshot missiles loaded is authorized at the ship CO’s discretion with ISIC approval.

54
Q

Ordnance Safety: RNC Checks

A

d. The M-299 and Advanced Precision Kill Weapon System/DRL release and control checks shall only be conducted with the extended pylons in the ready for flight position.

55
Q

Ordnance Safety: Pax and Guns

A

e. Passengers shall not be embarked when the GAU-21 crew-served gun is installed. If a crewserved weapon is required during passenger transfer, the M240 shall be utilized. The M240 shall be kept in the stowed position when not in use, and ammo cans shall be secured to prevent missile hazards in the event of an emergency…

(50) During all flights in which M-240D swingarm is installed, aircrew shall ensure the M-240D mounting bracket hardware is installed correctly and verify that the bracket retaining pin is fully inserted.

56
Q

Ordnance Safety: Range Clearance

A

f. Crews conducting live Gunnery Exercise events shall be responsible for own range clearance to a minimum of 5 NM beyond maximum weapons employment envelopes for the GAU-21 and M240 crewserved weapons.

57
Q

Ordnance Safety: Side Arms

A

g. While embarked aboard ships at sea, issued side arms shall be carried in Condition 3 (chamber empty, magazine in gun, hammer down, safety on) or lower. Only when the force-protection scenario warrants (e.g., ditching in hostile territory) should the weapons condition be elevated to Condition 2 (round chambered, full magazine in gun, hammer down, safety on)…

(50) All sidearms carried by aircrew in the a/c shall remain at condition 4 (ammo not inserted) until required for use.

58
Q

Smoke Markers

A

a. Except in an emergency, smoke markers shall not be dropped closer than 10 NM from the coastline or in inland waterways, unless on a designated range or dip area

b. Smoke markers that cannot be de-armed shall be jettisoned outside of 1O NM from the coastline and prior to returning to home base and final landing.

59
Q

Ordnance Carriage

A

With the exception of sonobuoys and smoke markers, carrying live ordnance over populated areas shall be avoided. If a mission requires flight to a facility near a populated area, the most direct route that will minimize civilian exposure shall be used.

60
Q

Sonobuoy Launcher Requirements

A

a. Removal or replacement of the sonobuoy launcher cover should not be performed with the rotors engaged. If the cover is removed or replaced with rotors turning, two-person integrity shall be utilized.

b. The sonobuoy launcher cover shall be fastened with all possible attachment bolts, but no less than 11 total. Additionally, all corner bolts are required per enclosure (2). Missing bolts shall be documented on a MAF.

61
Q

Static Display of Aircraft

A

Paragraph 3.5 of reference (a), governs aircraft static display. In addition, the following safety precautions shall be taken:

a. Battery disconnected and appropriate circuit breakers pulled.

b. Sonobuoy launcher bottle pressure vented.

c. All intake plugs/covers installed.

d. Rotor brake lock on.

e. All doors/panels closed unless a crewmember is present.

f. Remove and properly store all Cryptographic Ignition Keys (CIKs).

g. No visitor shall enter the helicopter or display area unescorted. Visitor access to the aircraft interior shall be controlled and supervised by a crewmember. Non-crew members shall not be permitted access to the engine/transmission deck/tail pylon.

h. Following a static display, a preflight inspection is required, paying particular attention to both interior (switches, circuit breakers, etc.) and exterior areas (antennas, panels, fueling ports, pitot-static systems, etc.).

i. Live ordnance is prohibited during static displays.

Ref A: CNAF

62
Q

Flight Line Procedures: Night Signals

A

a. At night, crews shall utilize a blue light signal to communicate with flight deck/line personnel to reduce the likelihood of a miscommunication with the LSE/Plane Captain (PC).

63
Q

Flight Line Procedures: Eye/Hearing/Head Protection

A

b. All personnel shall use authorized eye, hearing and head protection in hangars and on,the flight line. Single hearing protection is required when within 200 FT of aircraft with rotors turning or within 50 FT of aircraft with only APU turning. Double hearing protection is required when within 30 FT of aircraft with rotors turning or APU running for extended periods of time. Double hearing protection is not required inside the aircraft.

64
Q

Flight Line Procedures: Rings

A

c. Rings shall not be worn while operating or working on aircraft or moving ground support equipment.

65
Q

Flight Line Procedures: Climbing On Aircraft

A

d. No one shall climb on top of aircraft unless both engines are secured (this does not include engine motoring with both fuel and ignition secured). If only the APU is operating, personnel may climb on top of an aircraft only with the permission of the PIC. In this case, the PIC shall ensure that one of the Aircrew visually checks the top of the aircraft for integrity and Foreign Object Debris (FOD) prior to continuing with the engine start.

66
Q

Flight Line Procedures: Climbing w/ helmet/cranial

A

e. All personnel shall wear a cranial or helmet with strap fastened whenever climbing on any part of the aircraft. This requirement may be relaxed only as long as required to perform maintenance or an inspection in which headgear restricts the proper accomplishment of the task.

67
Q

Flight Line Procedures: Entering/Exiting the rotor arc

A

f. All personnel shall enter and exit the rotor arc at the three and nine o’clock positions and only by direction of a Plane Captain (PC)/LSE and only after the PC has received clearance from the Pilot at Controls (PAC). In the absence of a PC, personnel entering and exiting the rotor arc shall receive clearance from the PAC. Personnel shall not enter or exit the rotor arc when Pilots are either entering or exiting the cockpit…

(50) n. Personnel shall not enter or exit the rotor arc while engines are online w/ the rotor brake on.

68
Q

Panel/Cover/Cowling Fasteners

A

The maximum numbers of unfastened, broken or missing fasteners is as follows:

Tail Gearbox Cowling
3 Total, 2 in a row

Intermediate Gearbox Cowling
3 Total
2 In a row

Vertical Tail Driveshaft Covers
2 Total
2 in a row

Other Tail Driveshaft Covers
1 total
1 in a row

NOTE: Flight with unfastened, broken, or missing corner fasteners is not recommended. Corner fasteners should be fixed as soon as practicable by qualified maintenance personnel. Tail Gearbox Cowling corner fasteners and required sonobuoy launcher cover fasteners are identified in enclosure (2).

69
Q

Maintenance Quals

A

M-4 MAINTENANCE OUALIFJCA TIONS. COs are authorized to accept maintenance qualifications from other commands per reference (i) as long as the technician is current and fully-qualified for the respective tasks by their current command. This gives COs latitude for joint evolutions conducted between multiple commands. Members must be loaded into the hosting squadron’s NALCOMIS/OOMA system to perform maintenance tasks and/or sign off discrepancies.

Ref I: Memo of understanding for mx

70
Q

Ship Firing Evolutions

A

a. Aircraft should be airborne or in the hangar during all ship weapons firing evolutions. When weapons firing evolutions are anticipated, detachments shall adhere to sections 7 .9 .1 of reference (d), and its associated cautions.

Ref D: 80T-122

71
Q

RAS evolutions

A

b. For RAS evolutions, consideration should be given to hangaring the aircraft, if not airborne, when shot lines are being fired from the replenishment ship in the vicinity of the flight deck.

72
Q

Deviation from Paint Scheme

A

a. Any deviation of the aircraft paint tactical paint scheme shall be approved by the Type Commander, via Type Wing, per reference (I).

b. Only the sonobuoy cover shall be approved for painting with a squadron CO-approved design.

Ref L: COMNAVAIRFORINST 4790

73
Q

Post Installation Mx Dips

A

Post-installation maintenance dips from shore shall be conducted in an area with no more than 2000 FT water depth to facilitate recovery efforts in the event of loss of transducer. For SOCAL operations, post-installation maintenance dips shall be conducted in Imperial Beach Dip Area Charlie.

74
Q

Blade Fold and Spread

A

To mitigate system damage arising from misuse of the bladefold test set (cheater box), the aircraft’s automatic blade-fold system shall be the primary means of folding or spreading the main rotor head while underway and ashore.

75
Q

EP Init/Prohib Maneuvers: Who initiates?

A

In addition to the prohibited maneuvers listed in paragraph 4.5.4 of reference (c), the following additional guidance is promulgated:

a. Simulated emergencies shall only be introduced in the aircraft under the cognizance of a designated HAC.

76
Q

EP Initiation/Prohib maneuvers: Compound EPs

A

In addition to the prohibited maneuvers listed in paragraph 4.5.4 of reference (c), the following additional guidance is promulgated:

b. Compound emergencies involving the degradation of two or more unrelated systems shall not be introduced, initiated or practiced.

77
Q

EP Init/Prohib Maneuvers: Circuit Breakers

A

In addition to the prohibited maneuvers listed in paragraph 4.5.4 of reference (c), the following additional guidance is promulgated:

c. No circuit breakers shall be pulled to initiate a simulated emergency. COs may authorize the following exceptions:

(1) CO’s may authorize HAC’s to pull the Batt Bus Panel circuit breaker in order to simulate failed backup attitude indicator for training during day VFR conditions only.

(2) ANI Aircrewmen and current qualified FRS Aircrew Instructors may pull circuit breakers necessary for simulating rescue hoist, cargo hook, RAST, Mission Power, RADAR, and Acoustic malfunctions.

78
Q

EP Init/Prohib Maneuvers: Practice Autos

A

In addition to the prohibited maneuvers listed in paragraph 4.5.4 of reference (c), the following additional guidance is promulgated:

d. Practice autorotations at night are prohibited.

e. Pilot and copilot radar altimeter indicators shall be operable for practice autos.

79
Q

EP Init/Prohib Maneuvers: OFT EPs

A

In addition to the prohibited maneuvers listed in paragraph 4.5.4 of reference (c), the following additional guidance is promulgated:

g. Dual engine malfunctions, tail rotor drive emergencies, total AC power failure, and in-flight emergency simulation that requires placement of an engine into Enhanced Digital Electronic Control Unit (EDECU) lockout shall only be accomplished in the OFT.

80
Q

EDECU Lockout Ops

A

In-flight training operations in EDECU LOCKOUT, with the exception of scheduled FCF training flights while conducting FCF checklist steps in accordance with reference (c) under the cognizance of a qualified FCP, are prohibited. The use of EDECU LOCKOUT as part of an in-flight engine malfunction troubleshooting procedure not specifically promulgated in the MH-60R NA TOPS, FCF checklist, or approved NA VAIR maintenance troubleshooting procedure is prohibited.

Ref C: NATOPS

81
Q

H2P/H2P Flights

A

Simulated emergencies, movement of PCLs from the FLY position (other than in an actual emergency), night Coupled approaches and 180-degree practice autorotations are prohibited on H2P/H2P flights.

Shipboard H2P/H2P flights may be scheduled by OICs with the permission of squadron and ship COs and shall be conducted as day, VMC, non-tactical training flights only.

82
Q

CAL/LZ

A

CAL/LZ training shall be conducted on approved ranges or airfields per their governing directives.

Pre-mission planning shall be conducted to calculate power available and power required given expected conditions at the CAL/LZ site.

A “power available” check shall be conducted at the planned landing altitude before commencing the approach.

The MRP available versus maximum power required shall be 10% or greater to proceed with the approach.

Operational CAL/LZ flights other than those of operational necessity shall also adhere to this power margin…

(50) Practice CAL/LZ ops shall only be conducted when annotated on the flight schedule.

(50) Practice unaided CAL ops are prohibited after EENT.

83
Q

ELRF Training Guidance

A

The ELRF may be used for mission training purposes outside of an approved laser range, but shall not be used on personnel or wildlife. Crew acknowledgement is required when selecting ELRF from the FLIR menu. The ELRF shall not be fired unless crew concurrence has been received following the “ARM ELRF” prompt. This concurrence shall acknowledge “ELRF” is indicated on the lower left portion of the FLIR Attack Page.

84
Q

NVD NITE Lab Periodicity

A

The currency for NVD NITE Lab training for Pilots and Aircrewmen shall be 48 months from the last day of the month in which the training is received. NVD NITE Lab training may be accomplished within 60 days preceding expiration of the current training and is valid for 48 months from the last day of the month in which the current training expires. Pilots and Aircrewmen shall not fly NVD-aided events unless they are NVD NITE Lab training current.

85
Q

Dipping Sonar Ops: MBIT

A

(50) If ALFS is installed and dipping operations are scheduled, an MBIT shall be completed on the first flight of the day and should be completed prior to any dome deployment.

If the MBIT fails, the aircraft may be flown on a non-dipping flight as long as there is a DOME SEATED indication and the UTILITY HYD PUMP switch remains OFF for the duration of the flight.

MBITs should be performed on deck to the maximum extent practicable. Crews may perform in-air MBlTs as required by NATOPS troubleshooting procedure, however. careful consideration shall be given to the possibility of dome loss or damage.

86
Q

Night Transits to AUTEC

A

(50) a. Squadron aircraft flying to AUTEC from the Continental United States should launch in time to land at AUTEC prior to sunset.

b. Due to the risks associated with nighttime fly-offs and recoveries, these evolutions shall be planned for daytime take off and recovery to the maximum extent practical. The Squadron CO may approve day launch with nighttime recovery on a case-by-case basis, after a thorough ORM assessment.

87
Q

Performance Calcs

A

(50) At a minimum, crews shall brief the following performance calculations prior to every flight:

a. HIGE/HOGE Torque
b. Fly Away Torque
c. Dual Engine Intermediate Power
d. Single Engine Contingency Power
e. Single Engine Airspeed
f. Airspeed for Onset of Retreating Blade Stall for the anticipated flight regimes.

88
Q

Debrief Requirement

A

(50) A face-to-face debrief shall be conducted post flight with all members of the crew. This debrief should be conducted outside of the aircraft to the maximum extent practical and in accordance with reference (c) and the SEAWOLF manual.

Ref C: NATOPS

89
Q

Ordnance Safety: Mx w/ weapons loaded

A

(50) Maintenance requiring the application of electrical power to armament or weapons circuitry shall not be performed with weapons loaded or during loading/downloading evolutions.

90
Q

Hangaring A/C w/ Ordnance

A

(50) All Marine Location Markers. MK-17 (BRU), M55 (BRU). CCU-107 (CMDS). cartridges and ALE-47 ECM Dispensers shall be removed from aircraft prior to entering hangar.

91
Q

Flight Line Procedures: Life Vests

A

(50) f. At sea, all personnel on the flight deck at night shall wear an inflatable life vest with functional strobe light and proper preventative maintenance conducted.

92
Q

Flight Line Procedures: Cell Phones

A

(50) g. Cell phone use is prohibited in the hangar or on the flight line ashore, with the exception of Aircrew designated on the flight schedule carrying out official duties.

93
Q

Flight Line Procedures: L5

A

(50) h. All maintenance personnel shall clear the flight line when lightning within five miles (L5) is set. If the PIC determines that a shutdown is required, the shutdown may be conducted unassisted. If the aircraft cannot be turned over in accordance with reference (L) (engines running with both PICs in the aircraft) the aircraft shall be shutdown and a Turnaround inspection shall be performed.

Ref L: COMNAVARIFORINST 4790

94
Q

Flight Line Procedures: Wash Rack

A

(50) i. Unless otherwise directed by Maintenance Control, all aircraft should be taxied through the wash rack prior to final shutdown and prior to hot seat evolutions following over-water hovers or shipboard operations. Aircraft shall not be taxied through the wash rack with externally loaded ordnance and/or M299 launcher.

95
Q

Flight Line Procedures: Dog House Cover

A

(50) j. Positive control of the doghouse cover shall be maintained anytime the doghouse latches are released. This requirement is relaxed when the aircraft is in the hangar. The hydraulics bay safety straps shall be used any time the hydraulics bay is opened in the shipboard environment.

96
Q

Flight Line Procedures: Aircrew and move evolutions

A

(50) k. Aircrewmen shall not occupy the cabin during move evolutions unless performing preflight duties with safety harness secured at the Sensor Operator (SO) console.

97
Q

Flight Line Procedures: TA Requirement

A

(50) l. If an aircraft is shut down between consecutive flights due to an unexpected delay, Maintenance Control, the oncoming PIC, and the SDO (or OIC embarked) shall confer to determine if the aircraft can be relaunched in accordance with reference (I). A turnaround inspection shall be performed if the anticipated delay is long enough and the opportunity exists, based on the judgment of the Squadron MO (or OIC embarked). HAC-to-HAC startups are not authorized.

Ref L: COMNAVAIRFORINST 4790

98
Q

Flight Line Procedures: Jewelry

A

(50) m. Jewelry shall not be worn on the flight line with the exception of watches. Watches shall not have a case or protective enclosure that can be removed while the watch is being worn.

99
Q

Turnaround Expiration

A

(50) TA Inspection expiration time should no be flown through for training flights

100
Q

Det Patch Guidance

A

(50) Det name, logo, and patches shall be approved by the squadron CO.

101
Q

EP Init/Prohib Maneuvers: Shipboard environment

A

(50) Simulated aircraft emergencies requiring intentional degradations while in the shipboard environment are prohibited, with the exception of

day VMC practice Stabilator Auto Mode Failure

day VMC practice AFCC I/O and AFCS DEGRADED flight

day VMC PAS Malfunction flight

provided there is no intent to land.

102
Q

EP Init/Prohib Maneuvers: Simulated Dome EPs

A

(50) i. When conducting simulated dome emergencies. manual or automatic hydraulic mode shall be reengaged prior to 100 feet of POCL when recovering the TA.

103
Q

EP Init/Prohib Maneuvers: Weight Restrictions

A

(50) j. There is no weight restriction for power recovery autorotations. however, the PIC shall consider and discuss environmental and weight factors before conducting.

104
Q

EP Init/Prohib Manevers: Actual Degradations at Night

A

In addition to the prohibited maneuvers listed in paragraph 4.5.4 of reference (c), the following additional guidance is promulgated:

D. …Simulated emergencies requiring the actual degradation of aircraft systems at night are prohibited with the following exceptions:

(1) Single-engine approaches and landings to a prepared surface with adequate overrun and underrun to allow for safe execution.

(2) Single-engine running landings

(3) Boost-off and failed SAS/AFCS

(4) Simulated lost ICS

(5) STAB auto mode failure

105
Q

EP Init/Prohib Maneuvers: Single Engine Training

A

In addition to the prohibited maneuvers listed in paragraph 4.5.4 of reference (c), the following additional guidance is promulgated:

f. Simulated single engine failures from a hover out of ground effect (e.g., 70 FT Coupled Hover) shall only be initiated over a surface where a run-on landing can be made.

(50) k. If a PIC elects to conduct Single Engine to a spot training with both PCLs in FLY. they shall establish a simulated power available torque limit prior to the approach. taking into consideration weight. environment and torque available in a single engine configuration. PICs may consider utilizing dual engine HIGE torque minus 5 to 10 percent on each engine based on current environmental conditions.

106
Q

Hot Refueling w/ failed precheck valves

A

(50) d. Refueling operations ashore should not be continued following the failure of a pre-check valve in accordance with applicable (IETM). Embarked det OICs shall give due consideration to operational impacts, risk mitigation and all governing directives (NATOPS, IETMS, ref O) prior to refueling an aircraft with one or two failed pre-check valves. Fueling with two inoperable pre-check valves should be conducted as a last resort and fuel flow stopped well short of a full fuel load to avoid cell rupture or fuel spill.

Ref O: 80T-109