Annex C: APS UPRT Objective Maneuvering Quantification (FAA LOCART - August 2012) URT1 In-Flight UPRT Session: #1 (Introduction) ICATEE Training Matrix (Ver S12) AOA Targets (< CLmax, CLmax, > CLmax) Attitude Targets (degrees) G Targets (+ or - units) Suitable Platform Exercise Desciption Element(s) Maneuver Observed Margin (secs) Threat Pitch Roll Observed Margin Max Pitch/Roll Maneuver Observed G Margin Max G Normal, Utility or Aerobatic (25%) Familiarization Turns / Climbs / Descents Prevention (5b) <CL max <CL max NA, Does not Stall 20 deg 60 deg 80 deg roll NA, Target 30 deg pitch, 60 2.0 3 0.75 3.75 Normal, Utility or Aerobatic exceed CLmax does not deg roll exceed normal attitudes Primary Control Stategies (PCS) Power-Off Stall: Prevention & Recovery Awareness (3a,b,d,g,j), Prevention >CL max >CL max Recovery within Cross- 10 deg NU 30 deg 20 deg NU, 30 10 deg pitch, 30 deg pitch, 60 1 2 0.5 2.5 Normal, Utility or Aerobatic (3a,b,e, 5b), Recovery 3 sec or one controlled deg roll 30 deg roll deg roll (5a,b,c,d,f,k) spin rotation Stall, Incipient spin Power-On Stall: Prevention & Recovery Awareness (3a,b,d,g,j), Prevention >CL max >CL max Recovery within Cross- 20 deg NU 30 deg 20 deg NU, 30 10 deg pitch, 30 deg pitch, 60 1 2 0.5 2.5 Normal, Utility or Aerobatic (3a,b,e, 5b), Recovery (5a,b,c,d,f) 3 sec or one controlled deg roll 30 deg roll deg roll spin rotation Stall, Incipient spin All-Envelope Indoctrination: Awareness, Prevention & Recovery UPRT Falling Leaf (core exercise in stall/spin prevention Awareness (2b, 2c, 3c, 3d, 3f, 3g, >CLmax for >CLmax for Certified for Incipient spin, 10 Up, 45 ND 90 Degs 45 ND, 120 15 Degs Pitch (60 Down), 0.5 to 1.0 G - 1.0 G to -.25 G, -1.25 G to 3.75 Aerobatic (due to Roll and Pitch concepts - note that this exercise is not a traditional 3j), Prevention (2a, 2b, 3a, 3b, 3c, longer than 3 longer than 3 upright spins Developed deg roll Roll (135 Degs) 3.0 G .75 G G Attitudes, and Spin Threat) 'falling leaf' exercise sometime used in normal category 3e, 3h, 3i), Recovery (5a, 5b, 5d, sec sec Spin maneuvering) 5g, 5m, 5o, 6f) Zoom Maneuver: Stall Prevention & AOA SA Awareness (2b,d,h, 3a,f,m), <CL max >CLmax Recovery within Cross- 70 deg NU, 30 deg 75 deg NU, 30 10 deg pitch, 85 deg NU, 40 0.5 to 2.0 G - 1.0 G to -.25 G, .75 G -1.25 G to 3.75 Aerobatic (due to Pitch Attitude) Prevention (2a,d, 3a,j,n, 5b), 3 sec or one controlled 30 ND deg roll 10 deg roll deg roll 3.0 G G Recovery (5e, 6a,b,f,g,h,o,r) spin rotation Stall, Incipient spin All-Attitude Indoctrination All-Attitude Maneuver: Roll Awareness (2b, 2c, 3c, 3d, 3f, 3g, <CL max <CL max Demonstrated Upright or 20 deg NU, 360 roll 30 deg pitch, All Attitudes All Attitudes 0.5 to 2.0 G -1.0 G to 3.0 -.25 G, .75 G -1.25 G to 3.75 Aerobatic (due to roll attitude) 3j), Prevention (2a, 2b, 3a, 3b, 3c, recovery from Inverted Stall 10 deg ND 360 roll G G 3e, 3h, 3i), Recovery (2c, 5a, 5b, inverted stall 5d, 5g, 5m, 5o, 6e,f,h,q) All-Attitude Maneuver: Loop Awareness (2b,e,g,h, 3m), <CL max >CL max Recovery within Accelerated 360 deg 0 deg 360 deg pitch All Attitudes All Attitudes 0.5 to 3.0 G --1.0 G to -.25 G, 1.13 -1.25 G to 5.63 Aerobatic (due to Pitch Attitude Prevention (2a,d, 3n, 5b), 3 sec or one stall pitch 4.5 G G G and G) Recovery (2c, 6d,p) spin rotation All-Attitude Maneveur: Inverted Flight Awareness (2b,f,h, 3m), <CL max <CL max Demonstrated Inverted Stall 20 deg NU, 180 deg 180 deg All Attitudes All Attitudes 0.5 to 2.0 G -1.5 G to 2.0 -.38 G, .5 G -1.88 G to 2.25 Aerobatic (due to Roll, and G Prevention (2a,e, 3n, 5b,9), recovery from 10 deg ND G G Threat) Recovery (6c,f,o,q) inverted stall URT1 Aviation Performance Solutions Confidential Page 1 Annex C: APS UPRT Objective Maneuvering Quantification (FAA LOCART - August 2012) URT2 In-Flight UPRT Session: #2 (Advanced Stalls) ICATEE Training Matrix (Ver S12) AOA Targets (< CLmax, CLmax, > CLmax) Attitude Targets (degrees) G Targets (+ or - units) Suitable Platform Exercise Desciption Element(s) Maneuver Observed Margin (secs) Threat Pitch Roll Observed Margin Max Pitch/Roll Maneuver Observed Margin (25%) Max G Normal, Utility or Aerobatic Basic Stall (PCS) Review Awareness (3a,b,d,g,j), Prevention >CL max >CL max Recovery within Cross- 10 deg NU 30 deg 20 deg pitch & 10 deg pitch, 30 deg pitch, 60 1 0 to 2.0 G .5 G 2.5 G Normal, Utility or Aerobatic (3a,b,e, 5b), Recovery 3 sec or one Controlled 30 deg roll 30 deg roll deg roll (5a,b,c,d,f,k) spin rotation Stall, Incipient spin Stall Awareness & Prevention Exercises Negative Roll Damping Demonstration Awareness (3a,b,d,g,j), Prevention >CL max >CL max Certified for Cross- 30 deg NL 360 deg 30 deg NL & 30 deg pitch, 60 deg pitch, 360 1 .5 to 2.0G .75 G 2.75 G Aerobatic (due to Roll) (3a,b,e, 5b), Recovery (5a,b,c,d,f) upright spins Controlled 360 deg roll 360 deg roll deg roll Stall, Incipient spin, Fully- developed spin Steep Turns to Accelerated Stalls Awareness (2g, 3a,f,m), >CL max >CL max Recovery within Cross- 10 deg 60 deg 20 deg NL & 10 deg pitch, 20 deg pitch, 120 1 to 2.5G minus 1 to .75 G minus 1.75 G to Aerobatic (due to Roll & spin threat) Prevention (3a,b,h,n), Recovery 3 sec or one Controlled 90 deg AOB 30 deg roll deg roll 3.0G 3.75 G (5b,g,h,i,l, 6a,b,d) spin rotation Stall Slipping and Skidding Awareness Awareness (3i,k,l), Prevention (3k,l,m), Recovery (5g,h,i, 7d)<CL max <CL max NA, Does not NA, Does not 10 deg 30 deg 10 deg pitch & 10 deg pitch, 20 deg pitch, 40 1 1 .5 G 1.5 G Normal, Utility or Aerobatic exceed CLmax exceed CLmax 30 deg AOB 10 deg roll deg roll Advanced Primary Control Strategies (PCS) Slipping Turn Traffic Pattern Stall Awareness (2e,g,h, 3b,i,j,k), >CL max >CL max Certified for Cross- 10 deg 60 deg 180 deg pitch 180 deg 180 deg pitch & 1 to 2.5G minus 1 to .75 G minus 1.75 G to Aerobatic (due to Roll, Spin and G Prevention (3b,c,e,k,l, 5g) upright spins Controlled & 180 deg roll pitch & 180 360 deg roll 3.0G 3.75 G Threat) Stall, Incipient deg roll spin, Fully- developed spin Skidding Turn Stall Prevention & Diagnosis Awareness (1b, 2b,c,d, 3a,b,i), <CL max <CL max NA, Does not Cross- 10 deg 30 deg 10 deg pitch & 10 deg pitch, 20 deg pitch, 60 1 1 .5 G 1.5 G Normal, Utility or Aerobatic Prevention (1c, 2a,b,c, 3a,k,l, 5b), exceed CLmax Controlled 30 deg roll 30 deg roll deg roll Recovery (2a,b,d, 5c,h,i, 6f) Stall, Incipient spin, fully- developed spin Skidding Turn Traffic Pattern Stall Awareness (2e,g,h, 3a,b,c,i,j,k), >CL max >CL max Certified for Cross- 20 deg 80 deg 180 deg pitch 180 deg 180 deg pitch & .5 to 2.5G minus 1 to .75 G minus 1.75 G to Aerobatic (due to Roll, Pitch, Spin Prevention (2d, 3a,b,c,e,k,l), upright spins Controlled & 180 deg roll pitch & 180 360 deg roll 3.0G 3.75 G Threat, and G Threat) Recovery (2d, 5b,c,d,h,i, 6f,q) Stall, Incipient deg roll spin, fully- developed spin All-Attitude Awareness Exercises All-Attitude Maneuver: Split S Awareness (1b, 2e,h, 6h, 9), <CL max >CL max Recovery within Accelerated 180 deg 180 deg 180 deg pitch 180 deg 180 deg pitch & .5 to 3.5G .5 to 4.0G 1 G minus 1.5 G to Aerobatic (due to Roll, and G Prevention (2d, 3n, 5b, 9, 10b), 3 sec or one Stall & 180 roll pitch & 180 360 deg roll 5 G Threat) Recovery (2c, 5g,h, 6b,e,h,q,r) spin rotation deg roll All-Attitude Maneuver: Cuban 8 Awareness (2e,g,h), Prevention <CL max >CL max Recovery within Accelerated 230 deg 360 deg 250 deg pitch 20 deg pitch, 270 deg pitch, .5 to 3.5G minus 1 to 1 G minus 1.5 G to Aerobatic (due to Roll, and G (2d, 3n, 5b), Recovery (2c, 3 sec or one Stall & 360 deg roll 180 deg roll 360 deg roll 4.0G 5 G Threat) 6a,b,d,o,p,q,r) spin rotation System Component Failure - Power Plant (SCF-PP) Loss of Thrust in All Engines at Altitude Awareness (1b), Prevention (2a, <CL max <CL max NA, Does not Stall 20 deg 45 deg 60 deg AOB 10 deg pitch, 20 deg pitch, 60 1 1 .25 G 1.25 G Normal, Utility or Aerobatic 5b), Recovery (1e, 2c,d, 6r) exceed CLmax 10 deg roll deg roll Loss of Thrust in All Engines at Low Altitude Awareness (1b), Prevention (2a, <CL max <CL max NA, Does not Stall 20 deg 45 deg 60 deg AOB 10 deg pitch, 20 deg pitch, 60 1 1 .25 G 1.25 G Normal, Utility or Aerobatic 5b), Recovery (1e, 2c,d, 6r) exceed CLmax 10 deg roll deg roll URT2 Aviation Performance Solutions Confidential Page 2 In-Flight UPRT Session: #3 (Upsets and ACS)Annex C: APS UPRT Objective Maneuvering QuantificationICATEE Training Matrix (Ver S12) (FAA LOCART - August 2012) AOA Targets (< CLmax, CLmax, > CLmax) Attitude Targets (degrees) G Targets (+ or - units) Suitable Platform URT3 Exercise Desciption Element(s) Maneuver Observed Margin (secs) Threat Pitch Roll Observed Margin Max Avail Maneuver Observed Margin (25%) Max Avail G Normal, Utility or Aerobatic Pitch/Roll Needed Needed Advanced Stall Review: Prevention & Recovery Awareness (2d,e,g,h >CL max >CL max Certified for Cross- 20 deg 80 deg 180 deg pitch, 180 deg 180 deg pitch, .5 to 2.5G minus 1 to .75 G minus 1.75 G to Aerobatic (due to Roll, Pitch, G 3a,b,c,f,i,j,k,m), Prevention (2d, spins Controlled 180 deg roll pitch, 180 360 deg roll 3.0G 3.75 G Threat, and Spin Threat) 3a,b,c,e,h,i,j,k,l,n), Recovery (2d, Stall, Incipient deg roll 5b,c,d,g,h,i,l, 6a,b,d, f,q) spin, fully- developed spin Attitude Upsets: Prevention through Proportional Counter-Response and Recovery Spiral Dive Awareness (2g,h, 7f), Prevention <CL max >CL max Recovery within Accel Stall 30 deg NL 90 deg roll 30 deg pitch, 15 deg pitch, 45 deg pitch, 120 .5 to 2.5 G minus 1.5 to 1 G minus 2 to 5 Aerobatic (due to Roll, and G (4c, 5b, 7c), Recovery (2c,