![]() Left engine Lycoming IO-360-C1E6 fuel injected. Stabilator Incorporates an anti servo tab, improving longitudinal stability Wing Flaps Slotted/ mechanically operatedįuel Tanks 2 interconnected tanks form integral part of each wing Tire Size: Nose 6ply 600圆 - Mains 8ply 600圆įuselage Conventional Semi Monocoque structure ![]() THE FOLLOWING INFORMATION IS PROVIDED FOR TRAINING PURPOSES ONLY - THE OFFICIAL PILOT OPERATING HANDBOOK IS THE FINAL AUTHORITY FOR ALL SENECA I SYSTEMS INFORMATION AND LIMITATIONS. about Piper Seneca and we hope that this information is very valuable for you and thats all your Instructor wants you to know for your Flight Test.įor Flight test Guide, Click the following link below:įor weight and balance software contact us by clicking on this. After Going through Multi Engine POH and different books, we found out this valuable info.
0 Comments
Leave a Reply. |
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |