The basic stability modes are available for use from liftoff to landing. They provide a high level of aircraft stability, both transparent and visible, to the pilot. These modes provide a much more stable aircraft and allow a much lower pilot workload while increasing the ability for precise maneuvering.
The stability Augmentation is performed through dedicated in-line actuators whose high speed, high bandwidth and high accuracy provide rapid and precise reactions to any instability and perturbation including wind gusts, rough air and turbulence. The unrivaled responsiveness of the stability augmentation system contributes to an unmatched ride quality for pilots and passengers
ATRM mode provides basic heading hold and turn coordination on the yaw axis. When below 50kts, or when the roll angle is less than 4 degrees, the AutoPilot will utilize yaw inputs to maintain the heading. When the roll angle exceeds 4 degrees above 50kts the AutoPilot will automatically control pedal position as required to maintain coordinated flight. This allows the pilot to easily perform coordinated turns with simple cyclic inputs while keeping their feet on the floor. Additionally, the manual pedal input normally required with large collective changes is managed automatically by the ATRM function.
The basic flight director AutoPilot modes are available to the pilot to allow true hands-off flight. The modes may be combined such as engaging Heading, Altitude, and Airspeed holding simultaneously or individually as the pilot may desire.
The heading mode enables the AutoPilot to select, capture and track a desired aircraft heading. The heading hold mode is engaged by pressing the HDG button on the control panel. When the mode is engaged, the aircraft will turn to and follow the HSI heading bug.
The IAS mode enables the AutoPilot to capture, maintain and adjust a desired indicated airspeed. The pilot may adjust the speed target by pressing the forward or aft cyclic beep trim switch and releasing when the new desired speed is attained. Should the current airspeed lie outside of the normal operating envelope the AutoPilot will bring the new target back into limits
The ALT mode enables the AutoPilot to capture, maintain and adjust a desired barometric altitude. The pilot may adjust the altitude target by pressing the beep trim switch and releasing when the new desired altitude is attained or using the collective Force Trim Release button for larger changes of the altitude reference.
The VS mode enables the AutoPilot to capture, maintain, and adjust a desired rate of climb or descent speed. The pilot may adjust the vertical speed target by holding the beep trim switch and releasing when the new desired vertical speed is attained or by using the force trim release switch for larger changes.
The RHT mode enables the AutoPilot to capture, maintain, and adjust a desired Radio Altimeter height. The pilot may adjust the height target by pressing the collective beep trim switch or holding the collective force trim switch and releasing when the desired height is attained. The RHT mode is performed by AutoPilot inputs on the collective axis control and may be simultaneously engaged with pitch and roll modes.
The Hover mode enables the AutoPilot to capture, maintain, and adjust a desired ground referenced velocity or a stationary position. When a stationary hover is commanded, the AutoPilot will make the corrections necessary to hold the position regardless of changes in wind speed and direction. The heading of the helicopter will be held automatically and can be adjusted by providing pedal inputs or inputs on the collective beeper.
The Go Around mode enables the AutoPilot to perform a fully hands off wings-level climb at the best rate of climb speed with a single button push. The mode is available for use when airspeed is greater than 50kts. It may be used to terminate an approach procedure, during a departure, or any time the pilot desires to automatically transition to a Vy wings level climb, such as recovery from spatial disorientation or inadvertent IMC encounter. The GA mode is performed by AutoPilot inputs on the pitch, roll, yaw, and collective controls.
The departure mode enables the AutoPilot to perform a straight, steady acceleration and climb from low speed (<50kt) and hover flight conditions with a single button push. This mode is very valuable for automatic recovery from inadvertent loss of visual reference conditions such as white-out and brown-out in hover. It is activated using the same button as Go Around.
This mode provides capture and tracking of the lateral guidance from a GPS/FMS system that is selected as the navigation source by the avionics system. This mode is used to provide a full hands-off following of any route defined in the FMS/GPS.
The AutoPilot provides full hands-off guidance on Localizer, ILS, LP, and LPV approaches. Both the lateral and vertical guidance will be tracked down the approach. When the GS mode is engaged and a valid RadAlt signal is available, the AutoPilot will perform an automatic level off at 50 feet height and continue flying down the runway centerline. Automatic tracking of the approach centerline is performed with roll control inputs, and the glideslope is tracked with inputs to the collective axis. The airspeed hold mode (IAS) may also be engaged during these approaches for a fully hands-off automatic approach to the runway.
When the AutoPilot is engaged in APPR & GS modes on an ILS or LPV approach and the DCEL mode is armed, it will automatically engage during the approach profile to provide a smooth deceleration from any initial approach speed to 70KIAS at approximately 200ft AGL (for ILS) or 300ft AGL (for LPV). The pilot may use the airspeed hold (IAS) mode to fly the initial portion of the approach, then let the AutoPilot automatically engage DECEL and perform a comfortable deceleration to the approach minimums altitude.
The AutoPilot is able to perform a fully hands-off approach from initial approach conditions to a stationary hover at specific RadAlt height. The ATH mode is intended to provide an automatic, hands-off, predictable profile descent & deceleration to hover. The ATH mode is based on a capture and hold a line principle so that the aircraft decelerates in level flight (if necessary, to join the descent profile) and then descends & decelerates using a constant slope relative to the ground. This constant angle approach enables the pilot to easily predict the final hover point. Once the hover targets are reached, the HOV & RHT modes are automatically engaged allowing for a fully hands-off hover. At the end of the description add: The pilot can adjust the descent slope and heading with the collective beep trim switch to precisely direct the aircraft to the desired hover point.
When coupled, the system can automatically limit upward collective movement to ensure engine power limits are not exceeded, or to automatically limit downward collective movement to prevent the helicopter from entering autorotation and high rotor RPM.
The TAWS mode reduces CFIT hazards by automatically commanding an avoidance maneuver upon receipt of an alert from a separately installed Terrain Warning System and when no evasive action is performed by the pilot. TAWS mode is available while the helicopter is in cruise conditions.
StableLight: The TRUE AutoPilot retrofit that helps AS350/H125 operators get the job done faster and safer!
On this video series, the StableLight development team provides valuable insight into the unique capabilities, features, and 4-axis technology that only a transport category AutoPilot can bring to your AS350/H125 aircraft operations.
Enter the new era of safety and performance for light helicopters. Lift-off!
These Standard Terms and Conditions of Sale for Services (“Terms and Conditions” or “Terms”), together with the terms of sale of the services (“Services”) as set forth in StandardAero’s catalog, quotation document, or other StandardAero communicated offer document (to be known herein as “Quote” or “Offer”) will comprise the entire agreement (“Agreement”) between the Parties for Services on Customer’s components or accessories (collectively “Components”). In this Agreement, “Customer” refers to the entity listed on StandardAero’s Quote. StandardAero and Customer may be individually referred to as a “Party” or collectively as “Parties”.
Asian Surface Technologies Pte Ltd
EB Airfoils, LLC
Jet Aviation Specialists, LLC
PAS Technologies Inc
PAS Technologies Romania SRL and
SAComponent Services (Ireland) Ltd
Accel Aviation Accessories, LLC
International Governor Services, LLC
Each Offer shall be deemed a separate contract between the Parties named therein. The Parties acknowledge and agree that any one StandardAero entity shall have no liability nor incur any obligation or be responsible for any failure of any other StandardAero entity to perform its obligations.
Paragraph (a) – Inspection/Acceptance is Reserved. Paragraph (f) – Excusable Delays is replaced with Clause 13 herein. Paragraph (h) – Patent Indemnity is modified as follows: The Contractor shall indemnify the Government and its officers, employees and agents against liability, including costs, for actual or alleged direct or contributory infringement of, or inducement to infringe, any United States or foreign patent, trademark or copyright, arising out of the performance of this contract, provided the Contractor is reasonably notified of such claims and proceedings. The Contractor shall not be liable for breaches or Patent Infringement caused by the OEM. Paragraph (I) – Risk of Loss is replaced with Clause 25 herein. Paragraph (o) – Warranty is replaced with Clause 15 herein. Paragraph (p) – Limitation of Liability is replaced with Clause 18 herein. Clause 26 – Risk of Repair and Clause 19 – Waiver of Claims are to apply to any US Government Orders. In the event FAR 52.212-4 is not applicable, in any event, StandardAero shall apply the above modifications to any like terms within such contract or award.
StandardAero will Redeliver the Components to Customer ExWorks (“EXW” Incoterms 2020) at StandardAero’s facility dock. Customer is responsible for any and all shipping costs (including any import/export duties, import/ export clearance costs, tariffs, applicable taxes, and insurance) to deliver Components from StandardAero’s facility dock to Customer’s facility.
If StandardAero agrees in writing to act as IOR, at its so election and discretion, which can be withheld for any reason, StandardAero may utilize a variety of measures to import the goods. All shipping instructions must be agreed to in writing prior to the inbound shipment. Depending on the transaction, the follow instructions may apply:
To facilitate shipments, Customer shall provide a commercial invoice, or the documentation acceptable in place of a commercial invoice, with the entry and before release of the goods is authorized. The commercial invoice or other acceptable documentation shall contain: 1) an adequate description of the Component(s) including, at a minimum, the part number, serial number, and correct country of origin; 2) the quantity of Component(s) sent, 3) the value or approximate value of the Component or Accessory being sent (e.g. depreciated book value or inventory value), 4) the appropriate eight-digit subheading from the Harmonized Tariff Schedule as per the International Convention on the Harmonized Commodity Description and Coding System done at Brussels on 14 June 1983 and its amendments. Additionally, Customer shall obtain a Certificate of Origin or Certificate of Airworthiness (if applicable) from the OEM and provide it to StandardAero.
Notwithstanding any Incoterms stated herein, in the event that Customer provides a faulty shipping container and StandardAero repairs such container to return the Component, or Customer requires StandardAero to use a shipping container that has been found to not meet StandardAero’s packing specifications, Customer accepts all liability for any loss or damage in transit including for packaging of the Component.
Subject to paragraph (b) below, any Dispute that cannot be amicably settled by the Parties shall be finally settled under the Commercial Arbitration Rules of the American Arbitration Association (the “AAA Rules”), commencing with the filing of a notice of demand for arbitration by either Party following the conclusion of the thirty (30) calendar day period referenced in the paragraph above. Any arbitration will be conducted in accordance with the following: (i) if the Dispute involves a claim for damages totaling at least $5 million (combined with damages alleged in any counterclaim, cross-claim or third-party claim but not including attorneys’ fees or other costs associated with the resolution of the dispute), the Dispute is to be decided by three arbitrators appointed in accordance with the AAA Rules – all other claims are to be decided by one arbitrator appointed in accordance with the AAA Rules; (ii) the arbitrator has no authority to award punitive or other damages beyond the prevailing Party’s actual direct damages and may not, in any event, make any ruling, finding, or award that does not conform to the terms and conditions of the Agreement; (iii) the arbitration award is to be in writing and is to specify the factual and legal basis for the award; (iv) the Parties are to share all fees and expenses of the arbitration equally, with the exception that each Party bears the expense of its own counsel, experts, witnesses, and preparation and presentation of submissions; (v) the arbitration is to be conducted in Phoenix, Arizona unless all Parties agree to a different location; and (vi) the arbitration is to be final and binding and may be entered in any court of competent jurisdiction. A Party’s failure to make a timely demand for arbitration results in the forfeiture of all of the claims and issues that the Party identified in its Dispute Notice.
This Catalog Confidentiality Agreement (“Agreement”) establishes the terms of use, handling, protection, and safeguarding by Customer (“Customer” shall mean the person requesting access to the Catalog and their employer) required for access StandardAero’s prices (“Catalog”) to procure repair and overhaul services (“Services”) from StandardAero (hereinafter the “Purpose”).
