Rockwell Collins Electromechanical Systems - Alphabetical Listing of Products

1-inch Lavatory Rinse and Fill Ball Valve

Fits existing lavatory service panels

Ball valves have demonstrated superior performance against leakage in aircraft lavatory systems

Dual seal eliminates leakage

No exposed seals

No separate lever-lock mechanisms required

Optional heater element available

4-inch In-Line Waste Drain Valve

The most reliable ball valve for aircraft lavatory systems

Solves the Blue Ice problem

Fully operable during sub-zero conditions

No exposed seals

All stainless steel construction

Dual energized seal design eliminates leakage

Applicable to all aircraft waste systems

Ball Valve Kits available for retrofit

FAA/AD approval on multiple aircraft for 5000 hour leak check interval

Available in multiple design configuration

4-inch Lavatory Service Panel Ball Valve

4000 flight hour leak check interval

Dual energized seals

No lever lock caps

Flow-through design with no obstruction

Stainless steel construction

Eliminates ramp spillage

No exposed seals

PMA certified

Ramp seal replacement

Additional Rocket Motor Hardware

Rollmet manufactures various components as part of the rocket motor hardware package--including closures, attachments, etc.

Aft Closures

Aft Closures

Aft closures -- for rocket motors which house the nozzle components or thrust actuation controls.

Alenia C-27J Pedestal Assembly

Alenia C-27J Throttle Control

Alenia C27J Throttle

Ergonomically designed Pilot Interface (adjustable friction feel characteristics)

Dual resolver position feedback to EEC (FADEC)

Ground idle and maximum continuous detent mechanisms

NVG compatible light panel

Integrated Gustlock Lever & Lockout Mechanism

Integrated adjustable switchbanks

Alenia C27J Pedestal

Fabricated CNC machined and riveted structure

Standardized three bay design to incorporate modules (throttle quadrant, flap control lever, avionics equipment)

Removable access covers

Aluminum Lavatory Wye Drain Coupling

The Lavatory Wye Drain Coupling provides the means to remove the lavatory drain plug or "donut" from the aircraft lavatory drain nipple, allowing the waste to drain into the lavatory service truck without spillage or leakage.

Industry standard for over thirty years

Eliminates ramp spillage and waste contact with servicing personnel

Leakproof connection to all standard lavatory 4" service panel drain nipples

Aluminum body and collar for long-lasting service life

Full-flow waste drainage for fast servicing

Stainless steel control shaft for easy plug removal and reinstallation

Hose bib end for 4" ground servicing hose/clamp connection (Part Number M2651-133-11)

Outlet nipple adapter for quick-change operation (Part Number M2651-133-13)

CMM 38-30-08 for operation and maintenance instructions

AMRAAM Rocket Motor Case

This is the solid rocket motor case for the "Advanced Medium Range Air-to-Air Missile" carried by most U.S. and Allied fighter aircraft.

ARJ-21 HSTA

ARJ-21 Throttle Control

BAe A-10 Control Grips / Panels

Bleed Air Ground Connector & Check Valve

Over 30 years of proven service

OEM on Boeing, Gulfstream, Airbus, Bombadier, and Aerospatiale Aircraft

Low pressure drop

Air start check valve connection

Versatile mounting configurations

Rugged stainless steel contruction

Preferred durable choice for commercial and military aircraft

Conforms to highest commercial and military quality standards

Blue Ice Tester (BLISTER)

Boeing and FAA approved

Self-test capability

Easy to use and easy to transport

No electricity needed

Uses available air pressure

Fits all drain valves

Boeing 787 FBW Primary Cockpit Controls Systems

Boeing 787 Flap Lever Module

Boeing 787 Pedestal Assembly

Boeing 787 Speedbrake / Spoiler Lever Module

Boeing 787 Throttle Control

Boeing B-2 (FBW) Throttle Quadrant

Fly-by-Wire

Power Levers

Edgelight Panel

LRU Grips with Integrated Speed Brake and Communication Switches

Boeing B-2 Nose Wheel Steering Gearbox

The B-2 Nosewheel Steering Gearbox is a lightweight, ultra strong unit that utilizes planetary gear technology enclosed in a high strength aluminum housing

The unit is designed to transmit a limit load of 115,530 inch pounds of torque at the pinion gear

Fully qualified

Hydraulically operated

Two simple planetary (19.4:1)

Anti-backlash gear train

Max operating: 59,470 inch pounds

Boeing C-17 HSTA

Boeing F-117 Throttle Quadrant

Interfaces with FBW sensors

Ties into weapons displays

Integrated function switches

Boeing F-14 Throttle Quadrant

Boeing F-22 Arresting Gear System Actuator

The F-22 Arresting Gear System utilizes two 28 VDC brushless motors and built-in-test (BIT) electronics. The uplock actuator incorporates:

A Rockwell Collins Electromechanical Systems-designed uplock actuator

A gas-over-hydraulic hamper assembly

Two cable assemblies

A hydraulic retract actuator

Boeing Space Station Heat Rejection Array Actuator

Fully Qualified

Max Operating: 8500 inch pounds

Simple Offset Gearing + Simple Planetary + Differential Planetary (1330:1)

All Stainless Gears

Worm Gear Manual Back-up

Temperature: -140°F to +/- 140°F

Dry Lubrication (No Grease)

30 Years Life in Orbit

Bombardier Learjet 45 HSTS

Breakaway Coupling

The Breakaway Coupling prevents costly damage to the aircraft service panel by separating or "breaking away" should servicing personnel inadvertently drive away from the aircraft prior to disconnecting the service hose. The patented Breakaway Coupling is spliced into the 3/4" Potable Water Fill and 1" Lavatory Rinse/Fill service hoses between the servicing truck and the aircraft connecting coupling. Upon a pull force of approximately 100 pounds, the tabs of the internal Shear Ring break, thus allowing the coupling to separate.

Spliced and clamped into ground servicing 1" lavatory rinse/fill supply hose and 3/4" potable water fill supply hose

Lightweight anodized aluminum construction for easy handling

Coupling nipple and housing separate with a pull force of 100 pounds; other pull forces available upon request

Field-replaceable Shear Ring after separation has occurred: Part number 2145-0155

Breakaway Coupling for 1" Lavatory rinse/Fill System: Part number 0030-0087

Breakaway Coupling for 3/4" Potable Water Fill System: Part Number 0030-0090-1

Buddy Combo

The Buddy Combo is comprised of:

Buddy Start System

De-Icing Nozzle

See the De-icing Demo.

Buddy Start™

The Lightweight Buddy Start™ System is ideal for use in remote areas where an Air Start Cart is not available. The Buddy Start utilizes APU or engine bleed air from one air craft (donor) to start another aircraft (receiver). Its lightweight, compact design allows for easy storage and transporation.

Proprietary hose design utilizes lightweight, durable materials for ease of handling and transporation

Meets standard ground start temperature requirements without the excessive weight

Packaged in a compact bag for easy storage

Fits standard air start nipples

Hose available in 2 ply or 4 ply construction

Utilizes a lightweight, quick disconnect aluminum coupling

Can be used on most aircraft with air start capabilites

Enables aircraft to avoid costly down time due to unavailability of an airstart cart

Based on a proven U.S. Army and USAF design. Adopted by the U.S. Military for the H-60, AH-64, C-130, and C-17.

See also Buddy Start™.

Embraer 170/190 Throttle Module

Illuminated panel for function definition and indication

Full autothrottle capability with resident control software certified to RTCA/DO-178B requirements

Autothrottle function interfaces with A/C via ARINC 429 bus for input and output communications

Ergonomically designed linear throttle with trigger release into thrust reverse range

TOP mounted LRU with 10 captive attachment points for easy installation and removal

Dual redundant output signal per lever for engine control commands to FADEC (full authority digital engine control)

TOGA, A/T disconnect, and A/T engage disengage push button switches with large knobs for easy access and comfortable actuation

Embraer ERJ 170 HSTA

The ERJ170/190 HSTA is a linear electro-mechanical ball screw actuator that utilizes brushless DC motor technology

FAR 25 certification

Dual structural load path

Innovative spring energized, triggered locked, secondary split nut with in-situ inspection feature

Fail locked safety rod design

Dual skewed roller no-back brake

Dual brushless 28Vdc motors with resolver commutation

Integrated dual position feedback sensors

Integrated skewed roller inertia dump clutch for overload protection

The unit is designed to transmit maximum operating loads of 2300 pounds at .70 inches per second

Embraer ERJ 190 HSTA

The ERJ170/190 HSTA is a linear electro-mechanical ball screw actuator that utilizes brushless DC motor technology

FAR 25 certification

Dual structural load path

Innovative spring energized, triggered locked, secondary split nut with in-situ inspection feature

Fail locked safety rod design

Dual skewed roller no-back brake

Dual brushless 28Vdc motors with resolver commutation

Integrated dual position feedback sensors

Integrated skewed roller inertia dump clutch for overload protection

The unit is designed to transmit maximum operating loads of 2300 pounds at .70 inches per second

EMS ISO 9001 Employee Training Reference Booklet

PREVIOUS

September 2000

What is the Quality Policy?

The Quality Policy is a document that defines RCEMS's organizational goals and expectations of its internal & external customers. As such, it is a key element of management responsibility.

The Quality Policy should be understood by all personnel and within all levels of the company.

Find the provided OP 1.0, Rockwell Collins ElectroMechanical Systems's Quality Policy for Total Quality Management below.

RCEMS Quality Policy, OP 1.0
The people of Rockwell Collins ElectroMechanical Systems will provide products and services to our internal and external customers that meet or exceed expectations every time. We will have an environment that encourages continuous improvement, data-driven decisions, lean manufacturing, and team achievement. The Leadership Team of Rockwell Collins ElectroMechanical Systems supports this policy 100% of the time.

RCEMS's ISO Quality System Elements
In ISO 9001, there are 20 different requirements that we address in our quality system.

Management Responsibility
Quality System
Contract Review
Design Control
Document and Data Control
Purchasing
Control of Customer Supplied Product
Product Identification and Traceability
Process Control
Inspection and Testing
Control of Inspection, Measuring and Test Equipment
Inspection and Test Status
Control of Nonconforming Product
Corrective and preventive Action
Handling, Storage, Packaging and Delivery
Quality Records
Internal Quality Audits
Training
Servicing
Statistical Techniques

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Expander Valve

Low profile design

Easy retrofit mounting

Patented cap assembly

Lightweight construction

Guaranteed flapper actuation

Rugged stainless steel material

100,000 HR MTBUR tested

Eliminate lavatory plug loss

FAA design approval and PMA

Easy shop/line maintenance capability

One-piece and two-piece configurations

Expandable plug to prevent in-service leakage

First Article Inspection Product Accountability-Raw Material, Special Process, Functional Testing

Flexible Drive Shafts

Bi-directional steel inner core

Durable phosphor bronze liner for wear resistance

Abrasion resistant stainless steel braided outer case

O-Ring sealed end fittings to protect against moisture intrusion

4000 RPM operation

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Fuel Level Measuring Stick

The Magna-Stick® and the Flexi-Stick™ offer direct reading of aircraft fuel tanks:

Quick, clean, and accurate

Calibrated in choice of units

Fits commercial aircraft. Made for either underwing or overwing mounting

Fulfills FAA and international industry standards (PMA)

Offers direct reading of aircraft fuel tank quantity in a variety of measurements (kg., lb., in., gal., ltr.)

Available with two floats for stacked tanks or tanks with two compartments

Maximum safety for measuring the level of flammable, corrosive or volatile liquids

Versatile mounting configurations

Operating temperature range: -65°F to 165°F

Installation angles up to 15°F

Durable Flexi-Stick™ provides longer life

Gulfstream 350/450/500/550 Flap Lever Module

Gulfstream 350/450/500/550 Pedestal Assembly

Gulfstream 350/450/500/550 Speedbrake / Spolier Lever Module

Gulfstream 350/450/500/550 Throttle Control

Gulfstream G-IV Pedestal Assembly

Gulfstream G-IV Throttle Control

FAR 25 certified

Fully qualified

Esthetic ergonomic pilot interface

Modular Design

Throttle quadrant with piggyback thrust reverser control

Trim wheels

Flap lever

Fuel cock switches

Speed brake lever

Gustlock lever

H.A.M.S. (Hot Air Management System)

Complete kit contains:

De-Icing Nozzle

60' Light Weight Airstart Hose

Aircraft coupling assembly

Convenient carrying bag

Multiple Applications or Uses:

De-Icing wing edges or rotor blades

Cooling brake surfaces

De-Icing virtually anything in proximity to an aircraft

Advantages to the Kaiser H.A.M.S.:

Everything you need to use the De-Icing Nozzle

Perfect for carrying to remote airports

Compact, light weight (55 lbs.), and easy to transport

Harpoon Launch Canister

Hawker 4000 Engine and Trim Switch Panel Module

Illuminated panel for function definition and indication

Left and Right engine start indication switches

Left and Right Engine Fuel Shut Off indication switches

Rudder, Aileron, Stand-by Pitch Trim Disconnect indication switches

Rudder, Aileron, Stand-by Trim Switches with distinct snap action feel

All indication switches are flush mounted for sleek and high tech look and comply with the dark cockpit concept

Top mounted LRU with four attachment points with captive hardware

Hawker 4000 Flap Actuation System

Outboard Actuator Design Features

Inboard Actuator Design Features

Power Drive Unit Features

Wing Tip Asymmetry Brake

Flexible Drive Shafts

Hawker 4000 Pedestal Assembly

Pedestal Assembly contains . . .

Throttle Module

Flap Control Module

Speed Brake Control Module

Trim Switch Panel Module

Parking Brake Control

Gust Lock Control

Mounting Provisions for two MCDUs

Provisions for Side cover installation with matching color schemes

Features:

The Throttle, Flap, Speed Brake, and Trim Switch Modules are state of the art fly-by wire equipment

Each module is designed as a stand alone LRU (Line Replacement Unit)

Each LRU can be removed and replaced easily

Complies with RAC dark cockpit philosophy

LRUs designed with flush mounted components for sleek, uncluttered, high tech appearance

LRUs are provided with below surface FOD covers for aesthetics and FOD prevention

Entire assembly designed and modeled in 3-D solid UniGraphics CAD Software

The Pedestal structure is designed as an LRU with six attachment points to the aircraft

Pedestal structure designed as one piece casting for clean look and aesthetics

Structure is sculpted at the aft section to allow easy entrance and egress into and out of the cockpit seats

Hawker 4000 Pedestal Assembly

Pedestal Assembly contains . . .

Throttle Module

Flap Control Module

Speed Brake Control Module

Trim Switch Panel Module

Parking Brake Control

Gust Lock Control

Mounting Provisions for two MCDUs

Provisions for Side cover installation with matching color schemes

Features:

The Throttle, Flap, Speed Brake, and Trim Switch Modules are state of the art fly-by wire equipment

Each module is designed as a stand alone LRU (Line Replacement Unit)

Each LRU can be removed and replaced easily

Complies with RAC dark cockpit philosophy

LRUs designed with flush mounted components for sleek, uncluttered, high tech appearance

LRUs are provided with below surface FOD covers for aesthetics and FOD prevention

Entire assembly designed and modeled in 3-D solid UniGraphics CAD Software

The Pedestal structure is designed as an LRU with six attachment points to the aircraft

Pedestal structure designed as one piece casting for clean look and aesthetics

Structure is sculpted at the aft section to allow easy entrance and egress into and out of the cockpit seats

Hawker 4000 Speed Brake Module

Illuminated panel for function definition and indication

Four redundant electrical output signal for reliable operation

Feature Ground Spoiler arming indicator switch in accordance with RAC dark cockpit concept

Top mounted LRU with six attachment points with captive hardware

Continuous position lever (from Retract to Extend) for speed brake panels deployment

Retract position feature a pilot feel detent

Large size knob for easy gripping and use as hand rest when operating pilot side MCDU

Hawker 4000 Throttle Control

Illuminated panel for function definition and indication

Full autothrottle capability with resident control software certified to RTCA/DO-178B requirements

Autothrottle function interfaces with A/C via ARINC 429 bus for input and output communications

Ergronomically designed throttle and thrust reverse levers

TOP mounted LRU with 10 captive attachment points for easy installation and removal

Dual redundant output signal per lever for engine control commands to FADEC (full authority digital engine control)

TOGA, A/T disconnect and A/T engage disengage push button switches with large knobs for easy access and comfortable actuation

HCW Pipe & Tube/Seam-Free™

HCW (Heavily Cold Worked)
HCW New Method of Manufacturing in ASTM A 312 Specification
300 Series Stainless Steel
Cold Worked/Annealed Manufactured Pipe Process
Metallurgical Equivalent of Seamless
Lower Cost than Seamless
Sizes 6" to 12" Schedule 20, 10, and 5 (s)
ASME B31 and Section VIII Code Cases
Produced from Low Cost Welded Starting Material
Weld and Heat Affected (HAZ) Eliminated via Kaiser's Patented Cold Extrusion Process and Subsequent Annealing
Exceptional Diameter and Wall Thickness Control
Enhanced Corrosion Resistance

Corrosion Tested by ASTM 249 - Former Weld/Parent Metal Decay Ratios of Less than 1.0
Corrosion Tested to ASTM 262 Practice A, B, C, E, and F - All Acceptable

DIMENSIONS OF SEAM-FREE™ HCW TUBE* **

TUBE SIZE DIAMETER WALLS WALLS WALLS WALLS

6" 6.00 .065 .083 .109 .120

8" 8.00 .065 .083 .109 .120

10" 10.00 .109 .120 .188

12" 12.00 .109 .120 .188
*To thousandths of an inch. **Most diameter and light wall combinations of seamless tubes can be manufactured by Rockwell Collins Rollmet Products.

DIMENSIONS OF SEAM-FREE™ HCW PIPE*

PIPE SIZES OUTSIDE DIAMETERS 5S 10S 10 20

6" 6.625 .109 .134 .134

8" 8.625 .109 .148 .148

10" 10.750 .134 .165 .165 .250

12" 12.750 .156 .180 .180 .250
*To thousandths of an inch.

Hybrid Rocket Case

Hybrid cases are being developed to accommodate innovative methods of propulsion for future missile, launch vehicles, etc.

Inboard Actuator Design Features

Dual structural load path and wing tructure

Recirculating ball screw design with ice scraper

Skewed roller no-back brake to prevent actuator from backdriving under aerodynamic loading

Ball cam enegerized torque limiter to limit actuator output force in case of flap jam

Maximum operating output load: 6404 lbs.

4000 RPM input shaft speed

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Lavatory Rinse/Fill Coupling

The Lavatory Rinse/Fill Coupling attaches to the aircraft lavatory 1" rinse/fill nipple at the service panel by a quarter-turn action and provides the connection between the ground service vehicle and the aircraft lavatory system during servicing of the lavatory.

Positive leakproof sealing on all aircraft 1" rinse/fill nipples

Lightweight anodized aluminum construction

Open end, quarter-turn to lock and release

Knurled body for easy handling

Hose bib end for 1" ground servicing hose/clamp connection

High operating pressure rating with low pressure drop

CMM 38-00-01 for operating and maintenance instructions

Levels of Service: Repair, Overhaul, and Rebuild -- FAA Certificate YF3R995L

Rockwell Collins Electromechanical Systems (RCEMS) offers three levels of service at its service centers:

Repair - The repair, per the Component Maintenance Manual (CMM), of a specific discrepancy identified by the customer and then returned in a flight worthy condition with supporting documentation and warranty. If a part is sent to RCEMS which is beyond economical repair, RCEMS will inform the customer. The customer may then elect to have the part overhauled, scrapped, or returned to them.(See Teardown Charges.)

Overhaul - The rework of an aircraft component removed from normal service per the applicable Component Maintenance Manual (CMM) and then returned in a flight worthy condition with supporting documentation and warranty. If a part is sent to RCEMS which we are not able to overhaul due to its poor condition, RCEMS will inform the customer. The customer may then elect to have the part rebuilt, scrapped, or returned to them.(See Teardown Charges.)

Rebuild - The refurbishment of an aircraft component originally manufactured by RCEMS, returned from normal service to new part tolerances, condition and performance, and returned in an "as new" flightworthy condition with supporting documentation and warranty. Parts originally manufactured by RCEMS will be upgraded to the current revision when the core allows.

For brochures on our Repair and Overhaul, click here.

Lever Ball Lock

There are three types of lever ball locks:

Lever Cap - a flip-over cap closing mechanism is attached to the panel.

Lever Ball Lock Cap - a cap is attached to the panel by a lanyard. Its opening and closing mechanism is engaged with a flip-up top.

Quarter Turn Ball Lock Cap - a cap is attached to the panel by a lanyard. The operating mechanism is engaged with a quarter turn of the cap.
Lever Lock Cap

Expandable convoluted plug prevents in-service leakage

Redundant sealing design provides the highest reliability

Fits on existing lavatory service panels

Optional heater element available

PMA certified
Lightweight Air Start Wye Coupling

Available with strainers and check valves

Ultra low "pressure drop"

Experience-proven coupling

All-aluminum cast body

Stainless steel nipples

Requested by numerous Ground Support Equipment Operators
Liquid Level Measuring System (LLMS)

Rockwell Collins Electromechanical Systems has developed a completely new, non-intrusive system of sensors that continuously detect the lavatory waste tank level. The LLMS is a system of small sensors that determine the weight of a waste tank, and consequently the relative fullness of the tank. This system consists of forward and aft load cell brackets and a Logic Control Module (LCM).

Non-intrusive system provides high reliability

Prevents human contact with waste

Decreases aircraft turnaround time by eliminating unnecessary waste tank servicing

Load Cell brackets directly replace existing tank mounting brackets
Load Cells

Non-intrusive system provides high reliability MTBF (50,000 flight hours per tank assembly)

Eliminates health concerns--non-intrusive system prevents contact with waste

Low weight: provides considerable weight savings over alternate systems

Low cost: lower acquisition and operating costs over alternate systems

Redundancy in load cell arrangement replaces the need for two separate sensing systems

Low maintenance costs: no sensor cleaning or inspection require (no schedule maintenance)

Eliminates unnecessary tank inspection and cleaning--tank "build-up" can be identified
Lockheed C-130J Throttle Control

FAR 25 certified

Fully qualified

Fly-by-Wire with backdriven four lever autothrottle

Integrated closed rate loop motor control electronics

Ergonomically designed Pilot Interface (friction feel characteristics)

Power levers with propeller position switches

Dual redundant resolvers per lever

Night vision switches to control ground speed module

Modularized servo drive, electronics module and clutch pack

Brushless motor

Night vision edgelight panel
Mitsubishi MRJ Flap Lever Module

Mitsubishi MRJ Pedestal Assembly

Mitsubishi MRJ Primary Pilot Controls System

Mitsubishi MRJ Speedbrake /Spoiler Lever Module

Mitsubishi MRJ Throttle Control

MK104 Mod 2 / Mod 3 Rocket Motor Case

The Navy's Dual Thrust Rocket Motor Case for Standard Missile. The Mod 2 is for the medium range and the Mod 3 is for extended range using the MK72 Booster.
MK72 Aegis Booster Case

Solid rocket booster case designed to boost the Navy's Standard Missile from the vertical launch system plus giving extended range for intercept of Aircraft and/or long range missiles.
More Information

Teardown Charges

Warranties

Turn Around Time

Shipping Charges

Repair Station Certificate No. YF3R995L

Drug Testing Policy

Quality Approvals

Audit

Overhaul and Rebuild Capabilities
Teardown Charges - A component sent to a Rockwell Collins ElectroMechanical Service Center for repair of overhaul which due to its poor condition is not able to be repaired or overhauled and which subsequently the customer elects to have scrapped or returned will be subject to teardown charge. If the customer elects to have the part rebuilt, then no separate teardown charges will apply.
Warranties
Repair and Overhaul Warranty - Rockwell Collins ElectroMechanical Systems ("RCEMS") warrants that the products which RCEMS rebuilds ("Products") shall be free from defects in material, workmanship; conform to the specifications; and be suitable for their inteded use for 1000 hours or 12 months after shipment, whichever occurs first. This warranty does not cover the Products unless they are installed and maintained in accordance with instructions and manuals of RCEMS or the aircraft manufacturers and unless they are used under normal operating conditions. For further information, email questions to Warranty Information.
Rebuilt Components and Assemblies Warranty - Rockwell Collins Electromechanical Systems ("RCEMS") warrants that the products which RCEMS rebuilds ("Products") shall be free from defects in material, workmanship; and be suitable for their intended use for 3000 hours or 36 months after shipment, whichever comes first. This warranty does not cover the Products unless they are installed and maintained in accordance with instructions and manuals of RCEMS and unless they are used under normal operating conditions. For further information, email questions to Warranty Information.
Turn Around Time

Level of Service Turn Around Time

Repair 7 Days ARO

Overhaul 14 Days ARO

Rebuild 21 Days ARO

Shipping Charges - All repair, overhaul, and rebuild prices are quoted F.O.B. service Center. Shipping charges can be included on a case by case basis.
Repair Station Certificate - RCEMS is an authorized FAA FAR Part 145 Repair Station REF Certification No. YF3R995L. RCEMS also has JAA JAR 145 approval in supplement to FAA Repair Station Certificate YF3R995L, REF JAA Certification JAA.4600.
Drug Testing Policy - The RCEMS drug testing policy has been fully accepted by the FAA, Plan Identification No. E-14P-00045-U.
Quality Approvals - RCEMS has received the following quality approvals from various companies:

AS9000 . . . Honeywell Compliant

D1-9000 . . . Boeing Approved to Rev. "A"

ISO9001: 1994 . . . Certified

MIL-Q-9858A . . . Compliant

MIL-I-45208A . . . Compliant
Audit - Our customers are invited to visit any of our Service Centers to audit our non-proprietary facilities.
Overhaul and Rebuild Capabilities - A list of our current repair overhaul and rebuild capabilites with a fixed price quote for overhaul and rebuild is available via email. In addition, RCEMS is enthusiastic to work with customers to expand our part number offerings.
For brochures on our Repair and Overhaul, click here.
Nipple Check Valve

Eliminates kinks in Air Start hoses

Rugged stainless steel construction

Allows 360° rotation of Air Start hoses

Precision ball bearing

Temperature ranging from -40°F to 600°F

Offered in a 45° angle variation which allows more installation options

Made to fit standard ground Air Start supply
Northrop E-2C Pedestal Assembly

Northrop Grumman E-2C

Power levers

Landing gear

Windshield wiper

Flap lever

Catapult grip

Arresting hook

Parking brake

Wing fold
Northrop E-2C Throttle Control

Power levers

Landing gear

Windshield wiper

Flap lever

Catapult grip

Arresting hook

Parking brake

Wing fold
Northrop E-2D Pedestal Assembly

Northrop Grumman E-2D Throttle Controls

Nozzle Bodies

The nozzle bodies are the metal, machined aft end of the rocket motor which when assembled controls the motor's thrust.
Orion P-3C Wing Flap Actuator

Wing Flap Actuator and Brake Assemblies

Fully Qualified

Telescopic Ball Screw + Zero Level Gear

Max Operating: 3600 pounds

Full Stroke: 37 inches

SRP, SPL and Electra

Full Spare parts Availability

Full Overhaul/Repair Capability

Linear Telescoping Ball Screw

Electrically Operated Solenoid Brake
Outboard Actuator Design Features

Dual structural load path and wing structure

Recirculating ball screw design with ice scraper

Skewed roller no-back brake to prevent actuator from backdriving under aerodynamic loading

Ball cam energized torque limiter to limit actuator output force in case of flap jam

Maximum operating output: 5155 lbs.

4000 RPM input shaft speed
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Overhaul and Rebuild Capabilities

For brochures on our Repair and Overhaul or to download our Capabilities document, click here.

Boeing 737

Boeing 747 HSTA

Boeing 757 HSTA

Boeing 767 HSTA

Boeing 777 HSTA (coming soon)

DC-8 CFM56 Engine Right Angle Gearbox

C-130 Throttle Quadrant

E-2C Throttle Quadrant/Pedestal

Fuel Sticks

Lavatory In-Line Ball Valves

Lavatory Drain Valves

Potable Water Tank Level Sensors

Ground Support Equipment

De Havilland Reservoirs

Waste Tank Sensors

Overview of Quality Assurance and Control

The quality system documentation and processes are structured in alignment with all 20 elements of ISO9001 & AS9100. Titles of polices/procedures are on file for review by interested parties.
The quality system meets the requirements of MIL-Q-9858A and Federal Air Regulations part 21, Part 43 and part 145. The figure below pictorially shows the documentation levels in the Rockwell Collins system. Level I documents are Operations Policies that outline the quality system structure, define the major elements of the system, and describe the quality system principles. Level II documents are Standard Operating Procedures that define the major activities of functional departments and general guidelines for those activities. Level III documents are specific Work Instructions that define, in detail, the specific tasks necessary to implement the Standard Operating Procedures. Level IV entails records established in Level I, II and III documents.

Oxygen Check Valve

Meets all oxygen check valve requirements

Different configurations

OEM on Boeing, Gulfstream, and Bombardier (among others)
Patriot Rocket Motor Case

Solid rocket motor case for the Army's Patriot or PAC-2 ground-to-air defense system.
Potable Water Fill Couplings

The quarter-turn Potable Water Fill Coupling is attached to the aircraft 3/4" water-fill nipple at the service panel and provides the connection between the ground service vehicle and the aircraft potable water fill system during servicing.

Positive leak-proof sealing on all aircraft 3/4" potable water-fill service panel nipples

Open-end, quarter-turn to lock and release

Lightweight anodized aluminum construction

Knurled body for easy handling

Hose bib end for 3/4" ground servicing hose/clamp connection

High operating pressure rating with low pressure drop

FDA approved o-ring material

CMM 38-00-01 for operating and maintenance instructions
Power Drive Unit Features

270 VDC brushless motor with integral failsafe 28 VDC electro-mechanical brake

Protection circuit to protect the hall - effect sensors

16,000 RPM motor operating speed

Skewed roller inertia dump clutch to protect the flap system from moto inertia in case of flap jam

4000 RPM operational output shaft speed

One stage spur gear with oil/grease lubrication
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Pre-Conditioned Air Adapters

Ultra lightweight

Durable construction prolongs life

Easy to couple handles
Pressure Reoiling Assemblies

Visual locking verification

Small, lightweight

Two-way flow

Qualified to MIL-A-25676 and MIL-N-25677

Mating pressure caps and plugs or dust caps and plugs are available

Minimum number of parts consistent with Reliability & Maintainability requirements

Compatible with aircraft turbine engine lubricating and preservative oils conforming to MIL-L-7808, MIL-C-8188, and MIL-L-23699

End fittings also available in custom design or to customer specifications
Quality Manual Contents

OPERATIONS MANUAL (RC-EMS Quality Assurance Manual)

TABLE OF CONTENTS

POLICY NUMBER TITLE (REVISION)/DATE

OP 1.0 Rockwell Collins ElectroMechanical Systems POLICY FOR TOTAL QUALITY MANAGEMENT (B) 07/18/00

OP 1.1 MANAGEMENT RESPONSIBILITY (E) 04/02/01

OP 1.2 QUALITY SYSTEM (B) 03/01/01

OP 1.3 CONTRACT REVIEW (A) 03/01/01

OP 1.4 DESIGN CONTROL (B) 03/01/01

OP 1.5 DOCUMENT AND DATA CONTROL (B) 03/01/01

OP 1.6 PURCHASING (B) 03/01/01

OP 1.7 CONTROL OF CUSTOMER SUPPLIED PRODUCT (A) 03/01/01

OP 1.8 PRODUCT IDENTIFICATION AND TRACEABILITY (B) 03/01/01

OP 1.9 PROCESS CONTROL (C) 03/01/01

OP 1.10 INSPECTION AND TESTING (B) 03/01/01

OP 1.11 CONTROL OF INSPECTION, MEASURING AND TEST EQUIPMENT (A) 03/01/01

OP 1.12 INSPECTION AND TEST STATUS (B) 03/01/01

OP 1.13 CONTROL OF NONCONFORMING PRODUCT (A) 03/01/01

OP 1.14 CORRECTIVE AND PREVENTIVE ACTION (B) 03/01/01

OP 1.15 HANDLING, STORAGE, PACKAGING, PRESERVATION AND DELIVERY (B) 03/01/01

OP 1.16 CONTROL OF QUALITY RECORDS (B) 03/01/01

OP 1.17 INTERNAL QUALITY AUDITS (A) 03/01/01

OP 1.18 TRAINING (B) 03/01/01

OP 1.19 SERVICING (C) 03/01/01

OP 1.20 STATISTICAL TECHNIQUES (B) 03/01/01

OP 1.30 COST OF QUALITY (B) 07/06/01

OP 1.40 SAFETY (A) 04/03/01

Quality Policy for Total Quality Management

The people of Rockwell Collins ElectroMechanical Systems will provide products and services to our internal and external customers that meet or exceed expectations every time. We will have an environment that encourages continuous improvement, data-driven decisions, lean manufacturing and team achievement. The Leadership Team of Rockwell Collins ElectroMechanical Systems supports this policy 100% of the time.
Resealable Breakaway Nipple

The world's first fully Resealable Breakaway Nippple is designed to pull off if the lavatory service truck inadvertently drives off with the hose still attached.

Pull off load 300 lb. nominal

Minimizes risk of damage to aircraft service panel

Unlike competitive products, our design will reseal after breakaway without nipple replacement, thus allowing aircraft dispatch

Fast easy threaded replacement of complete nipple assembly

No dispatch delay--replacement at maintenance crew convenience

Lever lock redundant "taper seal" for high reliability against leakage

Expandable convoluted plug design eliminates unnecessary components

Existing lever lock cap assembly can easily be converted with frangible kit

Ultimate solution for all FAA-AD's applicable to Blue Ice.
Roll Extrusion (Commercial)

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Roll Extrusion Methods

Roll Extrusion, as a net process, achieves final pipe dimensions through metal displacement.
Rockwell Collins Rollmet manufactures seamless pipe using two methods of Roll Extrusion:

External Roll Extrusion: External roll extrusion utilizes a mandrel over which the hollow is placed. Two annular die rings are brought into position on the hollow. The mandrel and hollow are rotated while the die rings progress axially through a series of passes. This simultaneously reduces wall thickness and O.D. while the hollow grows in length. The I.D. remains constant.
EXAMPLES OF TOLERANCES HELD*

O.D. TOL ± WALL TOL ±

6.000" .002 .050 .001

12.555" .010 .007 .003

15.250" .030 .188 .010

16.000" .031 .250 .010

20.965" .005 .220 .005

*To thousandths of an inch.

Quality assurance program to ISO 9001

Superior precision manufacturing and quality for your commercial seamless pipe and tube requirements

Fast turnaround on your delivery needs

300 foot minimum order - 6" through 12" pipe size (dependent on size)

Smaller quantities available from stocking distributors

40 to 80 foot minimum order - 14" through 26" pipe size (dependent on size)

Single random lengths - ASTM allowables

Fine grain size for stainless grades runs 6 to 8 typical

Wall tolerances better than ASTM allowables
Other Order Specifications Achieved

60 RA or better - I.D. finish

Straightness .040" per 7 feet

Roundness to .060"

Cylindricity within .040" in 240
For more information, email Rollmet Commercial Info.
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SAAB 2000 Pedestal Assembly

Fly-by-Wire

JAR/FAR 25 certified

Go-around switch

Edgelight panel

Lightweight (14 lbs)

Throttle module with dual position feedback sensors

Ground range lockout mechanism lever

Gustlock lever with throttle interlock mechanism

Fuel condition levers

Flap lever control

Lighted panel
Saab 2000 Throttle Control

Fly-by-Wire

JAR/FAR 25 certified

Go-around switch

Edgelight panel

Lightweight (14 lbs)
Esthetic and ergonomic modular design includes:

Throttle module with dual position feedback sensors

Ground range lockout mechanism lever

Gustlock lever with throttle interlock mechanism

Fuel condition levers

Flap lever control

Lighted panel
Sikorsky Blackhawk Helicopter APU Start Accumulator

Flight Critical Component for Engine Start-Up

Oil is discharged from Accumulator to start the auxiliary power unit (APU).

Helicopter engine is then started using power from the APU

Light-weight, compact, high performance oil and gas accumulator.

Accumulator is "self-displacing": discharged oil re-enters accumulator immediately after starting of APU. High energy output.

Easy to install. Fully corrosion protected. Very high reliability product.

Over 1500 units in service since initial production in 1985.
Sounding Rocket Motor Case

Rollmet has made various versions of sounding rocket motor cases in differing configurations and materials. These rockets are used to conduct high attitude studies related to the environment, weightlessness, medical, geological, etc..
Space Products (part 2 of 2)

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Roll Extrusion Methods

Roll Extrusion, as a net process, achieves final pipe dimensions through metal displacement.
Rockwell Collins Rollmet manufactures seamless pipe using two methods of Roll Extrusion:

Quality assurance program to ISO 9001

Aerospace manufacturing precision and quality for your commercial seamless pipe and tube requirements

Fast turnaround on your delivery needs

100 foot minimum order - 6" through 12" pipe size (dependent on size)

Single random lengths - ASTM allowables

Grain size for stainless grades run 60 to 8 normally

Wall tolerances better than ASTM allowables
Other Order Specifications Achieved

60 RA or better - I.D. finish

Straightness .040" per 7 feet

Roundness to .060"

Cylindricity within .040 in 232
For more information, email Roll Extrusion Info Request.
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Stinger Kit (Airflow Limiting Adapter Kit)

The Stinger Kit (Airflow Limiting Adapter Kit) is used for ground checking the Anti-Ice System (Leading Edge) on the listed aircraft.
Ultra-lightweight system
Pre-packaged for easy transport
Everything required is packed in a sturdy case, including:
100 feet of "Spooled" Thermocouple lead
Readout Handset
All electrical connectors
Tomahawk Booster Case

Solid rocket booster case designed to boost the Tomahawk cruise missile from the vertical launch systems used on Navy ships.
Tomahawk Launch Canister

This canister is used to transport and launch the Tomahawk cruise missile and booster from the vertical alunch system on Navy ships.
Vertical Launch ASROC Case

VLA is an anti-submarine weapon system whereby the rocket motor is attached to a torpedo that is launched from a surface ship. The motor drops off upon entering the water and the torpedo proceeds to the target.
Water Quantity Transmitter

Magnetic float and reed switch mechanism indicates potable water tank level.
Wing Tip Asymmetry Brake

Dual friction disk surfaces for high holding capacity

Failsafe electro-mechanical design

Seal connector
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