N83236 is Crosswinds Aviation’s Piper Arrow. It has been upgraded with a GTN 650 GPS.
As a complex aircraft, N83236 is used for commercial instruction.
N83236
| Make | Piper | |
| Model | Arrow | |
| Year | 1981 | |
| Category | Normal | |
| Span / Length / Height | 35 ft. 5 in. / 27 ft. 0 in. / 8 ft. 3 in. | |
| Permitted Operations | Day and Night VFR and IFR | |
| Panel | Steam | |
| Engine | Lycoming IO-360-C1C6 (200hp @ 2700 RPM) | |
| Propeller Type | Constant Speed | |
| Gear Configuration | Retractible | |
| Body Construction | Sheet metal | |
| ADS-B | N/A |
| Model | Lycoming IO-360-C1C6 | |
| No. Cylinders | 4 | |
| Displacement | 361 cu. in. | |
| Output | 200hp @ 2700 RPM | |
| Fuel Delivery | Fuel Injection | |
| Propeller Type | Constant Speed | |
| Propeller Manufacturer | Hartzell |
| PFD / MFD | N/A | |
| GPS | Garmin GTN 650 | |
| Transponder | Bendix King KT76A | |
| Audio Panel | Bendix King KMA74 | |
| COM 1 | Garmin GTN 650 | |
| NAV 1 | Garmin GTN 650 | |
| COM 2 | Bendix King KX 165 | |
| NAV 2 | Bendix King KX 165 | |
| Autopilot | N/A |
| Total Fuel Capacity | 77 Gallons | |
| Usable Fuel Capacity | 72 Gallons | |
| Fuel Type | 100LL | |
| Oil Quantity | 8 Qts. |
| Max Ramp Weight | 2750 lbs. | |
| Max Takeoff Weight | 2750 lbs. | |
| Max Landing Weight | 2750 lbs. | |
| Aircraft Specific Basic Empty Weight & Arm | 1795.90 lbs. @ 87.42 in. | |
| Max Useful Load | 954.1 lbs. | |
| Useful Load w/ Full Usable Fuel | 522.1 lbs. | |
| Baggage Capacities | 200 lbs. |
| Climb Speeds | ||
| Cruise Climb | 104 KIAS | |
| Best Rate Climb – Flaps Up (VY) | Gear Up: 87 KIAS Gear Down: 76 KIAS |
|
| Best Angle Climb – Flaps Up (VX) | Gear Up: 77 KIAS Gear Down: 70 KIAS |
|
| Landing Speeds | ||
| Normal Landing | Flaps Up: 85 KIAS Flaps Full: 75 KIAS |
|
| Max Demonstrated Crosswind Component | 17 KTS | |
| Airspeed Limitations | ||
| Never Exceed Speed (VNE) | 190 KIAS | |
| Max Structural Cruising Speed (VNO) | 149 KIAS | |
| Maneuvering Speeds (VA) | 1863 lbs.: 96 KIAS 2750 lbs.: 121 KIAS |
|
| Flap Extended Speed (VFE) | 108 KIAS | |
| Landing Gear Extended Speed (VLE) | 130 KIAS | |
| Landing Gear Extension Speed | 130 KIAS | |
| Landing Gear Retraction Speed | 109 KIAS | |
| Clean Stall Speed (VS) | 59 KIAS | |
| Landing Stall Speed (VS0) | 53 KIAS | |
| Glide Ratio | 1.5 NM / 1000 ft. @ 79 KIAS | |
| Max Demonstrated Crosswind Component | 17 KTS | |
| Max Cruise Speed / Fuel Burn | 143 KTAS / 12.4 gph (75% Power -6,000 ft. @ 10c) | |
| Service Ceiling (100 ft./min climb) | 15,000 ft. @ Std. Temp. | |
| Sea Level Climb @ Max T/O Weight & 20c. | 810 fpm (Flaps Cruise, Gear Up @ 87 KIAS) | |
| Wing Loading | 16.18 lbs./sq. ft. (Max T/O Weight) | |
| Power Loading | 13.75 lbs./hp (Max T/O Weight) |
Information Manual (Please consult the manual specific to the aircraft for official information)
