Landing Gear. (i) The Landing Gear shall ***** In the event that Lessee must replace the Landing Gear in order to meet these requirements, Lessee agrees that such replacement landing gear will have at least the same remaining life as such Landing Gear’s full allotment of time remaining to operate until overhaul.
Landing Gear. (a) Outer cylinder.
Landing Gear. (1) The landing gear and wheel wxxxx will be clean, free of leaks and repaired as necessary.
Landing Gear. All Landing Gear installed on the Aircraft will be serviceable and in compliance with the Manufacturer’s maintenance program. Upon return to Lessor all landing gear components shall individually have the same or greater time remaining to the next-due overhaul or limiter as the Aircraft at the Closing Date;
Landing Gear. (a) Approved Release to Service Certification for each fully built gear assembly, or major assemblies on each gear, as applicable, including either FAA 8130-3 or JAA/EASA Form 1;
Landing Gear. The Aircraft undercarriage is composed of one steerable nose landing gear (NLG) and two trailing-link type main landing gear units (MLG). Each nose and main gear assembly has twin wheels and tires. The main wheels are fitted with hydraulically powered and electrically actuated carbon brakes. Anti-skid protection and automatic braking is also provided. The landing gear is of the tricycle type. The two MLG assemblies, one located on the inboard portion of each wing, retract inboard each into the MLG bay located in the central fuselage. The NLG assembly is located beneath the cockpit and retracts forward into the nose section of the fuselage. Normal extension and retraction is electrically controlled and hydraulically operated by the cockpit landing gear control handle located in the center console. Landing gear position and status is visually displayed on EICAS and aurally annunciated in the cockpit. The anti-skid, brake control, nose wheel steering indications and status are also displayed on EICAS and interface with the central maintenance system for failure detection. The Aircraft has four braked main wheels (two per main gear), and two free rolling nose wheels. The main wheels and nose wheel are fitted with tubeless tires incorporating fusible plugs for over temperature protection and metallic diaphragm plugs for over pressure protection. Brake temperature is monitored with a system consisting of four sensors each mounted in a brake housing and a brake temperature-monitoring unit. Independent brake temperature is indicated in the cockpit on the EICAS. The brake/anti-skid control system interfaces with a dual integrated digital electronic controller with autobrake capability. The control unit provides brake control with independent wheel anti-skid protection, locked wheel crossover protection, touchdown protection, gear retract braking and Built-In-Test-Equipment (BITE). The steering system is comprised of an electronically controlled and hydraulically powered actuation of the nose landing gear steering actuators for taxi, take-off and landing operations. When the steering is not active due to pilot selection or failure conditions, the system continues to provide effective shimmy damping to ensure dynamic stability of the nose wheel. Steering commands are input to the Electronic Control Unit (ECU) through the pilot’s hand wheel (full authority) and/or rudder pedals (limited authority). Landing gear retracted, in travel, not safe or down-and-locked as well...
Landing Gear. The Landing Gear shall be serviceable and have a status as detailed in Schedule 1 Part 1. The Landing Gear, components and associated actuators shall have at least 3 months and 375 Flight Cycles remaining until the next 6 month, 750 Flight Hour, 750 Cycle inspection (or such inspection shall be performed by Lessor prior to Delivery). Wheels and brakes shall be serviceable. APU: The APU shall be Serviceable and have a model and status as detailed in Schedule 1 Part 1. ALA MSN 2830 – Global Crossing Airlines
Landing Gear. If the Landing Gear undergoes a Landing Gear Overhaul, performed by an Approved Maintenance Performer, Lessor will reimburse Lessee, from the then-existing Landing Gear Payments, for the actual costs incurred by Lessee for such Landing Gear Overhaul.”
Landing Gear. If the Landing Gear undergoes a major overhaul pursuant to Lessee's Maintenance Program performed by an Approved Maintenance Performer which results in full overhaul of the main landing gear or nose gear, subject to the last sentence of this clause (E), Lessor will reimburse Lessee, from the Landing Gear Payments paid to Lessor by Lessee as of the date such major overhaul is completed, for the actual cost incurred by Lessee for the major overhaul of the Landing Gear. Lessor will make such Landing Gear Payments available to Lessee for the cost of such major overhaul of the removed Landing Gear: (x) when Lessee reinstalls such Landing Gear in the Airframe following such major overhaul or (y) when Lessee replaces such Landing Gear with a landing gear that meets the requirements of this Lease, including Article 6 hereof (determined immediately after such major overhaul of the removed Landing Gear and on the assumption that the removed Landing Gear had been reinstalled in the Airframe).
Landing Gear. If the Landing Gear undergoes an overhaul as defined in Manufacturer’s component maintenance manual, or equivalent, which results in full refurbishment of the Landing Gear, subject to the penultimate sentence of this clause (vi), Lessor will pay Lessee the Landing Gear Payments referred to in paragraph 9(vi) of Schedule “1” hereto. Any cost in excess of such amount to be paid by Lessor pursuant to the preceding sentence shall be Lessee’s sole responsibility and shall be promptly paid by Lessee. Lessor will pay the Landing Gear Payments to Lessee for the cost of such overhaul of the removed Landing Gear: (x) when Lessee reinstalls such Landing Gear in the Airframe following such overhaul or (y) when Lessee replaces such Landing Gear with a freshly overhauled landing gear that meets the requirements of this Lease, including Article 6 hereof (determined immediately after giving effect to such overhaul of the removed Landing Gear and on the assumption that the removed Landing Gear had been reinstalled in the Airframe). Lessee agrees to provide Lessor with a copy of the warranties for the overhaul for approval by Lessor (which warranties shall expressly be assignable to Lessor), which approval will not be unreasonably withheld.
