An Acorn Growth Company
Document Title | Doc. # | Description |
Nacelle Wing Lockers | SL-16-BC-03 | Upgrade of hatch gas spring for Lockers equipped with P/N 85-352-077 gas spring |
C90A equipped with Raisbeck/Hartzell Swept Blade or Quiet Turbofan Propellers: Gross Weight Increase to 10,500 lbs | SL-16-BC-02 | Rescindment of the requirement of Wing Ballast Weights for the optional Gross Weight Increase (GWI) to an MTOW of 10,500 lbs |
Optional Hinge and Latch Mechanism (90 Series/F90/A100/200 Series) | SL-04 | Nacelle Stowage Wing Lockers – 90 Series/F90/A100/200 Series |
Elimination of Electromagnetic Interference with Aircraft Avionics (200 Series) | SL-05 | Enhanced Performance Leading Edge – 200 Series |
Non-chafing Silicone Gaskets for Stainless Steel Exhaust Stack Fairings | SL-06 | Stainless Steel Stack Fairings – All Models |
Automatic Gas Springs Installation | SL-08 | Nacelle Wing Lockers – 90 Series/F90/200 Series |
Gross Weight Increase to 10,500 pounds | SL-08-BC-1 | C90/C90A Gross Weight Increase to 10,500 lbs |
Topcoat Application Process | SL-08-BC-36 | 200/200C/200T/200CT/A200/ A200C/A200CT/B200C/B200T/ B200CT with Enhanced Performance Leading Edge |
Swept Turbofan Propeller System — HC-D3A/D9515K Elevator Trim Placard Installation | SL-13-BC-02 | King Air 200/A200/B200/B200GT aircraft equipped with Raisbeck Engineering Swept Turbofan Propeller System under STC SA2698NM-S |
Water Leakage into Stowage Compartment through Bayonet Latch Pocket | SL-18 | Nacelle Wing Lockers – All Models |
Mark VI – 200 Series | SL-20 | Removal of Mark VI Aileron Seals |
Quiet Turbofan Propellers and Ram Air Recovery System | SL-31 | Creation of Flight Manual Supplement 99-117 for Quiet Turbofan Propeller and Ram Air Recovery System combination |
B200 equipped with Dual Aft Body Strakes, Enhanced Performance Leading Edges, Ram Air Recovery System and High Floatation Gear Doors (when HFG equipped) | SL-32 | Update to flight manual supplement 99-126 |
Revised Topcoat Assembly | SL-34 | Nacelle Wing Lockers |