ENGINE MAINTENANCE CONDITIONS Clause Samples
ENGINE MAINTENANCE CONDITIONS. The Operator shall operate and maintain the Engines and components in accordance with the Aircraft Flight Manual, Pilot’s Operating Handbook, the applicable Engine Maintenance Manual, recommended Service Bulletins, the terms and conditions of this Agreement, and any other instructions and recommendations issued by P&WC or the aircraft manufacturer. In addition, the following maintenance tasks are or will be performed at the indicated intervals for each such Engine and the Operator shall transfer the recommended tasks\intervals into its approved maintenance program within ninety (90) days following the signature of this Agreement.
Note 1: The tasks and intervals below may be supplemented, adjusted, or removed at any time at P&WC’s discretion, based on experience or on review of Engine samples.
Note 2: Unless otherwise specified below, all Engine maintenance tasks and intervals listed in the applicable aircraft and Engine Maintenance Manual are to be performed. 1 Gas generator — Overhaul GGV1 =12,000 cycles Power section — overhaul GGV2 = 24,000 cycles (Ref: SB 14003R10 — Option C) PSV1 = 7,500 cycles PSV2 = 15,000 cycles 2 Hot Section Inspection interval 6000 cycles or based on ECTM® and borescope inspection 1 Fuel nozzle inspection* 600 hrs* 2 Fuel pump filters replacement 600 hrs 3 If Sundstrand pump is installed - inspect for corrosion & fretting 600 hrs 4 Clean gas generator. Case drain valves At fuel nozzle inspection * P&WC shall have the right to adjust, in consultation with Operator, this Interval should hot section condition trends show evidence that the fuel nozzles and flow divider have been run beyond the optimum removal interval. The disclosure of this document is subject to the restrictions of Article 14 contained herein 3▇ ▇▇▇▇-▇▇▇ TCP® Agreement # 06-2454 Dated: March 1, 2007 BOROSCOPE INSPECTION (by qualified personnel) 1 Hot section (CC Liner, CT Stator Assembly, CT Blades and Shroud Segments At fuel nozzle inspection 2 Comprressor inlet At fuel nozzle inspection 3 Oil scavenge pump, Inlet screen 1,000 hrs 1 WebECTM® (latest version) Automated Daily data collection 2 Trend alert D ITT = 15°C, D Ng = 1% (D : Delta)
ENGINE MAINTENANCE CONDITIONS. The Customer shall operate and maintain the Engines and components in accordance with the Aircraft Flight Manual, Pilot’s Operating Handbook, the applicable Engine Maintenance Manual, recommended Service Bulletins, the terms and conditions of this Agreement and any other instructions and recommendations issued by P&WC or the aircraft manufacturer. In addition, the following maintenance tasks are or will be performed at the indicated intervals for each such Engine and the Customer shall transfer the recommended tasks\intervals into its approved maintenance program within the next ninety (90) days:
Note 1: The tasks and intervals below may be supplemented, adjusted, or removed at any time at P&WC’s discretion, based on review of Engine samples.
Note 2: Unless otherwise specified below, all Engine maintenance tasks and intervals listed in the applicable aircraft and Engine Maintenance Manual are to be performed.
ENGINE MAINTENANCE CONDITIONS. The Customer shall operate and maintain the Engines and components in accordance with the Aircraft Flight Manual, Pilot’s Operating Handbook, the applicable Engine Maintenance Manual, recommended Service Bulletins, and any other instructions and recommendations issued by P&WC. In addition, the following maintenance tasks are or will be performed at the indicated intervals for each such Engine (it being understood, however, that the Overhaul intervals set forth below shall not be applicable for an Engine subject to the Transition Plan until the initial Overhaul under the Transition Plan is completed:
Note 1: The tasks and intervals below may be supplemented, adjusted, or removed at any time at the CFR or P&WC’s discretion to improve engine reliability or cost control.
Note 2: Unless otherwise specified below, all Engine maintenance tasks and intervals listed in the applicable aircraft and Engine Maintenance Manual are to be performed.