TCA Aircraft Testing Department. Type 2 aircraft test report (v1.3) Date of Report: March 12, 1998 ----------------------------------------------------------------------- SECTION A: (Original FSFS aircraft details.) Aircraft name: TCA Hercules Cargo PJ-TJC ----------------------------------------------------------------------- SECTION B: (FS98 only aircraft file details.) File name: ----------------------------------------------------------------------- SECTION C: (Criteria Tested) 1) Endurance (range): 2800nm 2) Take-off distance: 1700m Landing distance: 1100m 3) Rotation speed (Vr): a) 140 KIAS b) 102 KIAS 4) Climb: Best climb speed: 200 KIAS = 2000fpm at Sea Level 1100fpm at 20000 feet 5) Overspeed clacker on at: Mach 0.60 6) Behavior under AP. a) Speed AP. OK b) Altitude AP. OK c) Heading AP. OK d) NAV1 AP. ? e) Back course AP. ? f) Approach AP. OK g) Autoland 7) Speed @ 80% N1, FL200. Mach 0.52 8) % N1 at recommended economic cruise speed: 80% @FL200 = Mach 0.52 9) Stall speed. a) 100% fuel: 105/78 KIAS b) 30% fuel: 94/72 KIAS 10) Approach speed at 30% fuel: 94 KIAS 11) Turns AP ON - realistic?: a) Level turns: 30° bank. b) Climbing turns. OK c) Descending turns. OK 12) Turns AP OFF - realistic?: a) Level turns. OK. b) Climbing turns. OK. c) Descending turns. OK. 13) Landing: a) 30% fuel: Aircraft is quite maneouverable. b) 15% fuel. Ditto. 14) Operation with some engines out of service: 1 engine out: yaw, slower 1 engine out on each side: no yaw, much slower. 3 engines out: yaw, gradually slows down, need to reduce altitude to maintain flight. ----------------------------------------------------------------------- SECTION D: NOTES/COMMENTS: 1) Notes on how to fly aircraft are good. 2) Rotation is stated as 125 to 135 KIAS depending on take-off weight etc. I have found that in this speed range a pitch up attitude of at least 15° is needed for lift off. Be careful of a stall.