Balked Landing; Balked Landing Climb Gradient - Cirrus SR22 Pilot Operating Handbook

S 5: P
ECTION ERFORMANCE
B L
ALKED ANDING

Balked Landing

Balked Landing Climb Gradient

Conditions:
• Power ........................................................................................Full Throttle
• Mixture.................................................................................Set per Placard
• Flaps ............................................................................................ 100% (DN)
• Airspeed ................................................................................................ V
Balked Landing Climb Gradients shown are the gain in altitude
for the horizontal distance traversed expressed as Feet per
For operation in air colder than this table provides, use coldest
For operation in air warmer than this table provides, use caution.
Weight Press Alt
LB FT
3600 SL
2000
4000
6000
8000
10000
2900 SL
2000
4000
6000
8000
10000
5-38
D
ATA
Nautical Mile.
data shown.
Climb CLIMB GRADIENT - Feet per Nautical Mile
Speed
KIAS -20
79 860
79 732
79 611
79 497
79 391
79 291
79 1196
79 1033
79 880
79 737
79 603
79 478
• N •
OTE
TEMPERATURE ~°C
0 20
808 756
682 633
564 518
453 410
349 308
251 213
1129 1063
970 908
821 763
681 627
551 500
429 381
C
IRRUS
40 50
706 681
586 563
474 452
368 348
269 250
177 159
1000 969
849 820
707 680
575 550
451 428
336 314
P/N 13772-006
Reissue A
D
ESIGN
SR22
REF
ISA
769
655
548
446
351
261
1080
936
800
673
553
441