H-53E Att 09 Fac and AF Req 2019-12-13.docx

DOCX document 24 KB Posted

Attached to
H-53E Aircraft Maintenance and Repair Services
Solicitation number
N6264920R0003
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About this file

This document contains a draft request for proposal and associated attachments for H-53 aircraft maintenance and repair services. The solicitation is for depot-level maintenance, repair, and overhaul products and services in support of United States Navy and Marine Corps H-53 aircraft to be conducted by Fleet Readiness Center Western Pacific and NAVSUP Fleet Logistics Center Yokosuka. The draft RFP and attachments provide interested offerors with requirements for facility space, equipment, airfield support, transport aircraft characteristics, and H-53 aircraft specifications to request industry feedback before finalizing the solicitation. Feedback should be directed to the identified Navy contacts by the specified deadline. The Government will distribute the full specification to prospective offerors who sign a non-disclosure agreement and identify the email for receipt.

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N6264920R0003 Attachment (9) 25 September 2019

ATTACHMENT (9): Facility and Airfield Requirements For H-53E Integrated Maintenance Plan (IMP) Planned Maintenance Interval Depot (PMID)

Facility Requirements

· The Contractor shall allow drop-off and departure of PMI aircraft at its facility from 0700 to 1630, Monday through Friday.[footnoteRef:1] [1: The Contractor shall allow drop off and departure of PMI aircraft outside these hours when notified at least 24 hours in advance by the ACO. ]

· The Contractor’s shall use a strip and paint facility that meets all requirements for performing H-53 strip and paint according to the H-53E PMID Specification.

· The Contractor shall provide all necessary common hand-tools, Personnel Protective Equipment (PPE) and Confined Space detection equipment in order to comply with H-53E PMID Specification.

· The Contractor shall provide office spaces for Government personnel (DCMA and FRCWP) performing Contract Administration Services (CAS) and supply at its aircraft maintenance facility. The spaces provided for the Government personnel should be large enough that personnel are able to enter, exit, and work in the space comfortably, and be arranged to provide a collaborative environment for Government personnel. The contractor-provided spaces shall meet the following criteria:

· Located inside the Contractor's H-53E PMI facility, minimum of 1,000 square feet of floor space, fully segregated from any Contractor work spaces;

· Securable using a Contractor-provided cipher lock system, with access by Government personnel 24 hours per day, 7 days per week;

· Environmentally controlled (air conditioning and heating);

· Access to adequate restroom facilities and potable water;

· Custodial services (trash removal, dusting and floor cleaning/maintenance) coinciding with the Contractor's schedule for similar services;

· Minimum of ten (10) work stations equipped with power outlets capable of supporting at least two (2) 90W AC power adapters;

· Each work station provided with hard-wired access to a local commercial Internet Service Provider (ISP) at each workstation;

· Local ISP capable of supporting unrestricted access to Virtual Private Network (VPN) in the United States;

· Each work station provided with access to commercial telephone networks[footnoteRef:2]; [2: The Government will procure telecommunications and internet hardware, installation and services for the office spaces under separate contracts.]

· Telephones with access to the Defense Switch Network (DSN), if the capability exists

· The Contractor shall formally request changes to the Government’s workspaces to the PCO via DCMA. Such requests shall provide details of the requested facility changes required to accommodate the Government personnel, to include a cost estimate. The Contractor shall receive written approval from the PCO before incurring any costs associated with such workspace alterations, modifications or changes.

· When required, the Contractor shall provide temporary work space accommodations for up to 15 government personnel for meetings, FCF crew, etc.

Airfield Requirements The Contractor’s airfield and associated services shall meet the following minimum requirements:

· The Contractor shall provide access to an annually certified compass rose.

· Support all aircraft arrivals and departures performed in connection with this contract.

· Support all C-5, AN-124, C-17 and equivalent transport aircraft arrivals and departures in connection with this contract.[footnoteRef:3] [3: The Contractor shall ensure that AN-124 aircrew (Government or commercial) are cleared through Host Nation Customs and Immigration upon arrival to the Contractor’s facility.]

· Support all aircraft arrivals and departures (whether Government or commercial) for transporting passengers, cargo and parts in connection with this contract.

· The Contractor shall provide heavy equipment and qualified operators to support aircraft loading and offloading operations in connection with this contract.[footnoteRef:4] [4: The Contractor shall charge heavy equipment support for loading/off-loading as Over and Above. ]

· The Contractor shall provide airfield services (defueling/storage/fueling, towing, etc.) of all aircraft used to support this contract.[footnoteRef:5] [5: The Contractor shall charge airfield services as Over and Above. ]

· The Contractor shall provide towing services and hangar space for the Government’s emergency repairs of all aircraft used to support this contact.[footnoteRef:6] [6: The Contractor shall charge emergency towing and hangar space use as Over and Above.]

· The Contractor’s airfield shall allow unlimited access and use by FCF aircraft under this contract.

· The Contractor’s airfield shall allow unlimited access and use by transport aircraft under this contract.

The following tables provide general characteristic of aircraft that the Government may use to deliver H-53’s to the Contractor’s facility:

Transport aircraft general characteristics (C-5B/C-5M)

Length
247 ft 10 in
75.54 m
Height at tail
65 ft 1 in
19.85 m
Max. takeoff weight
837,000 lb
379,657 kg
Takeoff distance (fully loaded)
12,200 ft
3,720 m
Landing distance
4,900 ft
1,494 m
Wingspan
222 ft 9 in
67.88 m
Wingarea
6,200 sq ft
575.98 sq m
Cargo compartment height
13 ft 6 in
4.1 m
Cargo width
19 ft
5.76 m
Crew
Six(Pilot, Co-pilot, (2) Flight Engineers (2) Loadmasters)
Engines
4 General Electric TF39-GE-1C high-bypass turbofan (C-5B) 4 General Electric CF-80C2 turbofan (C-5M)

Transport aircraft general characteristics (C-17)

Length
174 ft
53 m
Height at tail
55 ft 1 in
16.8 m
Max. takeoff weight
585,000 lb
265,350 kg
Takeoff distance (fully loaded)
7,600 ft
2,316 m
Landing distance
3,500 ft
1,060 m
Wingspan
169 ft 8 in
51.75 m
Wingarea
3,800 sq ft
353 sq m

Cargo compartment height (fwd of wing)

12 ft 3 in
3.76 m

Cargo compartment height (aft of wing)

14 ft 8 in
4.5 m
Cargo floor length
68.2 ft
20.78 m
Cargo width
18 ft
5.49 m
Crew
three(Pilot, Co-pilot, and (1) Loadmaster)
Engines
4 Pratt & Whitney F117-PW-100 turbofans

Transport aircraft general characteristics (AN-124)

Length
226 ft 3 in
68.96 m
Height at tail
68 ft 2 in
20.78 m
Max. takeoff weight
893,000 lb
405,000 kg
Takeoff distance (fully loaded)
9,843 ft
3,000 m
Landing distance
2,953 ft
900 m
Wingspan
240 ft 5 in
73.3 m
Wingarea
6,760 sq ft
628 sq m
Cargo compartment height
14 ft 4 in
4.4 m
Cargo width
21 ft
6.4 m
Cargo floor length
119.7 ft
36.5 m
Crew
Six(Pilot, Co-pilot, (2) Flight Engineers (2) Loadmasters)
Engines
4A-Lotarev D-18T Turbofans

CH-53E

Length:
99 ft 1/2 in /
30.2 m
Length Folded: Rotors and Pylon
60 ft 6 in
Rotor diameter:
79 ft
24 m
Height:
29 ft 5 in
Height: Folded
18 ft 7 in
Empty weight:
33,226 lb
15,071 kg
Max takeoff weight:
73,500 lb
33,300 kg
Width (fuselage):
15 ft 5 in
Width (stub wings):
28 ft 4 in
8.64 m

Rotor systems: 7 blades on main rotor, 4 blades on anti-torque tail rotor

Ref: NAVAIR 00-110AH53-6

MH-53E

Length:
99 ft 1/2 in
30.2 m
Length Folded: Rotors and Pylon
60 ft 6 in
Rotor diameter:
79 ft
24 m
Height:
29 ft 5 in
8.46 m
Height: Folded
18 ft 7 in
Empty weight:
36147 lb
Max takeoff weight:
73,500 lb
33,300 kg
Width (stub wings):
28 ft 3 in
Width (fuselage):
15 ft 5 in

Rotor systems: 7 blades on main rotor, 4 blades on anti-torque tail rotor

Ref: NAVAIR 00-110AH53-5

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