CIRRUS SR22 · IO-550-N · POH P/N 13772-006 (Serials 4433 & subs, Perspective+) · KIAS unless noted
AIRSPEED LIMITATIONS POH SECTION 2
| VNE | NEVER EXCEED | 205 | 208 CAS |
| VNO | MAX STRUCTURAL CRUISING | 176 | 179 CAS |
| VO | OPERATING MANEUVERING — at 3600 lb | 140 | 142 CAS |
| VFE | MAX FLAP EXTENDED — 50% | 150 | 152 CAS |
| VFE | MAX FLAP EXTENDED — 100% | 110 | 111 CAS |
| VPD | MAX DEMO CAPS DEPLOYMENT | 140 | 142 CAS |
AIRSPEED INDICATOR MARKINGS
176–205
YELLOW — SMOOTH AIR
| VS0 | STALL — LANDING CONFIG, 100% FLAPS | 64 | |
| VS1 | STALL — CLEAN, 3600 lb, FWD CG | 74 | |
EMERGENCY AIRSPEEDS POH SECTION 3
| VG | BEST GLIDE — ALL WEIGHTS (8.8:1) | 92 | |
| ENGINE-OUT LANDING — FLAPS UP | 90 | |
| ENGINE-OUT LANDING — FLAPS 50% | 85 | |
| ENGINE-OUT LANDING — FLAPS 100% | 80 | |
| EMERG DESCENT — 176 if turbulent | 205 | |
| PROP OVERSPEED — REDUCE TO | 90 | |
| NO ELEVATOR — TRIM, FLAPS 50% | 80 | |
TAKEOFF — 3600 LB, FLAPS 50% POH SECTION 5
| SPEED AT LIFTOFF | 76 | |
| SPEED OVER 50 FT OBSTACLE | 84 | |
NORMAL OPERATION — 3600 LB POH SECTION 4
| VR | ROTATION — NORMAL, FLAPS 50% | 73 | |
| ROTATION — OBSTACLE CLR, FLAPS 50% | 84 | |
| VY | BEST RATE OF CLIMB — SEA LEVEL | 108 | 99 @ 10K |
| VX | BEST ANGLE OF CLIMB — SEA LEVEL | 88 | 88 @ 10K |
| ENROUTE CLIMB — NORMAL, FLAPS UP | 110–120 | |
| APPROACH — FLAPS UP | 90–95 | |
| APPROACH — FLAPS 50% | 85–90 | |
| APPROACH — FLAPS 100% | 80–85 | |
| VREF | SHORT FIELD — FLAPS 100% | 79 | |
| GO-AROUND — FLAPS 50%, FULL POWER | 80 | |
TURBULENT AIR PENETRATION: 140 @ 3600 lb; 123 @ 2900 lb. MAX DEMO XWIND: 21 kt. NO VLE/VLO — fixed gear. FLAPS: takeoff UP or 50%; landing 0/50/100%. LOAD: +3.8/−1.9 g flaps up; +1.9/0 g flaps extended. MAX ALT: 17,500 MSL (takeoff 10,000). Known icing prohibited. Spins prohibited — deploy CAPS on departure from controlled flight.
Transcribed from Cirrus SR22 POH/AFM P/N 13772-006, Sections 2, 3, 4, 5 (Sec. 4 per TPOH 17-02, 27 Jul 2018). Reference aid only; does not supersede the FAA-approved AFM.
SR22 G6 QUICK REFERENCE
SIDE 2
DESCENT & GLIDEPATH
| 60-TO-1 | 1° ≈ 100 ft per NM → 3° = 300 ft/NM (everything below) |
| TOP OF DESCENT | (ft to lose ÷ 1000) × 3 = NM add 1–2 NM to slow |
| 3° DESCENT RATE | GS × 5 = fpm 150 kt → 750 · 120 kt → 600 · uses GROUND speed |
| CLIMB GRADIENT | ft/NM × GS ÷ 60 = fpm 200 ft/NM @ 120 kt = 400
Faster GS or tailwind = MORE fpm required |
| VDP (unpublished) | HAT ÷ 300 = NM before threshold
At MDA, past VDP, no runway → GO MISSED |
ENGINE LIMITS — CONTINENTAL IO-550-N POH SECTION 2
| CHT | 240–420 °F green · 420–460 caution · >460 warning |
| OIL TEMP | 100–240 °F green · >240 warning · 75 °F min for takeoff |
| OIL PRESSURE | 30–60 psi green · 60–100 caution · 10 min / 100 max |
| RPM · MAP · EGT | 2700 max · 15–29.5" green · 1000–1600 °F |
| FUEL | Flow green 0–25 gph (top of arc varies w/ alt) · totalizer FUEL QTY warn <9 gal · max imbalance 10 gal · 92 gal usable / 94.5 total |
| MAX PWR FUEL FLOW | SL 27.1 · 4K 23.6 · 8K 20.5 · 12K 18.4 · 16K 16.7 gph |
| BOOST PUMP | ON for takeoff, climb, landing, tank switching |
IMC FAILURE TRIAGE — PERSPECTIVE+ POH SECTION 3 / 3A
| ATTITUDE FAIL (AHRS) | Verify auto-switch to good AHRS · ADAHRS CB SET (one reset only) · be ready for standby |
| RED X ON ASI/ALT (ADC) | ADAHRS CB SET · revert to standby · land as soon as practicable (loses TAS & wind) |
| PFD BLANK | DISPLAY BACKUP — ACTIVATE · land as soon as practicable |
| STATIC BLOCKED | Pitot heat ON · ALT STATIC OPEN (console, right ankle) · apply Sec 5 correction |
| PITOT BLOCKED | Pitot heat ON · descend to warmer air · fly pitch + power, cross-check GPS GS |
| ALT 1 / ALT 2 FAIL | CB check & set · cycle ALT switch · if no reset: switch OFF, SHED LOADS (A/C, landing light, yaw servo) |
| ELEC FIRE / SMOKE | Masters OFF · in IMC turn ALT1, ALT2, BAT1 OFF — BAT 2 holds PFD ≈ 30 min · land as soon as possible |
IFR REGULATIONS
| ALTERNATE 1-2-3 | §91.169(b) — ETA ±1 hr: ceiling <2000 above arpt elev or vis <3 SM → alternate |
| ALTERNATE MINS | §91.169(c) — 600-2 precision · 800-2 nonprecision (planning mins at ETA; unless otherwise published) |
| FUEL | §91.167 — destination + alternate + 45 min at normal cruise |
| BELOW DA/MDA | §91.175(c) — normal descent rate · flight vis at/above mins · 1 of 10 visual references |
| IFR CURRENCY | §61.57(c) — 6 approaches + holding + intercept/track, 6 cal mo · 6 mo grace · then IPC |
| VOR CHECK | §91.171 — 30 days: ground ±4 · air ±6 · dual ±4 · VOT ±4 |
| INSPECTIONS | §91.411 / .413 — altimeter, static, transponder: 24 cal months |
| OXYGEN | §91.211 — 12,500–14,000 crew after 30 min · >14,000 crew · >15,000 pax offered |
| LOST COMM | §91.185 — Route A V E F · Altitude M E A (highest of) |
LIGHT GUN SIGNALS §91.125 · AIM 4-3-13
| SIGNAL | IN FLIGHT | ON GROUND |
| STEADY GRN | Cleared to land | Cleared for takeoff |
| FLASHING GRN | Return for landing | Cleared to taxi |
| STEADY RED | Give way, keep circling | STOP |
| FLASHING RED | Airport unsafe — do not land | Taxi clear of runway |
| FLASHING WHT | — | Return to starting point |
| ALT RED/GRN | Extreme caution | Extreme caution |
SQUAWK 7500 hijack · 7600 lost comm · 7700 emergency · 121.5 — hold COM transfer 2 sec to tune.
Engine limits and failure procedures from Cirrus SR22 POH/AFM P/N 13772-006, Sections 2, 3, 3A. Regulatory and light gun items summarized from 14 CFR Part 91 and the AIM — paraphrased for recall, not regulatory text. Reference aid only; does not supersede the FAA-approved AFM or current regulations.
About this card
- Every performance and limitation figure was read directly out of the POH for this airframe. Nothing was taken from a web summary — published SR22 speed lists are usually 3400 lb G3 or SR22T data, which is wrong here by as much as 10 knots.
- Download PDF gives you the colour card, two sides, half-letter. Print duplex, flip on short edge.
- Add to kneeboard on the resources page puts the black-and-white version straight onto your current briefing, so it prints with your legs and charts.
- Dark and light follow whatever you last set in the Kneeboard Pro app.