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BEECHCRAFT KING AIR C-90A

BEECHCRAFT KING AIR C90A · Checklist

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Overview

This document is a checklist for the Beechcraft King Air C90A, detailing operational limitations, emergency procedures, and performance specifications. It serves as a quick reference for pilots to ensure safe operation of the aircraft.

  • Max Take-Off Weight: 10,100 lbs
  • Max Landing Weight: 9,600 lbs
  • Total Usable Fuel Capacity: 2,573 lbs
  • Max Cross Wind: 25 KIAS
  • Emergency Descent Airspeed: 182 KIAS
  • VYSE: 108 KIAS
  • VMO: 226 KIAS
  • MMO: 0.46 Mach

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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

Document

Source

Copy found at gob.cl. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Checklist
File size
·
18 KB
Copy found at
·
gob.cl
Language
·
es

Specifications & performance

Extracted from this document.

Specifications

Max landing weight (lb)
·
9,600
Max take off weight (lb)
·
10,100
Total usable fuel capacity (lb)
·
2,573

Performance

Mmo
·
0.46
Vmo kias
·
226
Vxse kias
·
100
Vyse kias
·
108
Vfe approach kias
·
184
Vfe full down kias
·
148
Emergency descent kias
·
182

V-speeds

VA_KIAS
·
169
VMCA_KIAS
·
90
VLE_EXTENSION_KIAS
·
182
VLE_RETRACTION_KIAS
·
163
VFLAPS_DOWN_1_ENG_KIAS
·
101
VFLAPS_UP_LANDING_KIAS
·
115

Weight & balance

Max zfw
·
No Limit
How rare is it?
1,952BEECHCRAFT KING AIR C90A registered worldwide · 1,939 active

Common. More common than 98% of the aircraft models we track.

Documentation completeness
2/7

Most owners only have the POH. Here's the essential set for the BEECHCRAFT KING AIR C90A.

More BEECHCRAFT KING AIR C90Amanuals & documents

In this document

Limitations

Details operational limitations including speeds and weights for the Beechcraft King Air C90A.

Emergency Procedures

Outlines steps to take in various emergency situations such as engine failure in flight and on the ground.

Starter Limitations

Specifies the operational limits for the starter, including on and off times.

Engine Failure Procedures

Describes procedures for handling engine failure during flight and ground operations.

Emergency Descent

Provides steps for conducting an emergency descent, including airspeed and configuration.

Weight and Balance

Lists maximum weights and limitations for safe operation of the aircraft.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Safety notes

  • Do not feather the propeller during a second engine flameout.
  • Maintain airspeed at VYSE during engine failure after lift-off.
  • Use fire extinguishers as required during engine fires.
  • Ensure power levers are idle during engine failure on ground roll.
  • Follow starter limitations to avoid damage.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Full document text

1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “BEECHCRAFT KING AIR C-90A” N149CM A.- Limitaciones de Operación 1.- Limitaciones (KIAS) 2.- Combustible Libras VA 169 Tipo a Utilizar JET A-1 VMO 226 Capacidad Total Usable 2.573 MMO (Mach) 0.46 VFE Approach 40% 184 VFE Full Down 100% 148 3.- Pesos (LBS) VMCA 90 Max. TAKE-OFF 10.100 VLE Extension 182 Max. LANDING 9.600 VLE Retraction 163 MAX ZFW No Limit. VXSE 100 VYSE 108 Emergency Descent 182 4.- Starter Limitations Max. Glide Speed 125 40 SEC ON 60 SEC OFF VFlaps Up Landing 115 40 SEC ON 60 SEC OFF VFlaps Down 1 Eng. 101 40 SEC ON 30 MIN OFF Max. Cross Wind 25 2 B.- Emergencies Procedures 1. ENGINE FAILURE IN FLIGHT OR FIRE IN FLIGHT a.- Affected engine: Condition Lever FUEL CUT- OFF Propeller Lever FEATHER Fuel FW Shutoff Valve CLOSE Fire Extinguisher ACTUATE (if required) 2. ENGINE FIRE ON GROUND a.- Affected engine: Condition Lever FUEL CUT- OFF Fuel FW Shutoff Valve CLOSE Starter Switch STARTER ONLY Boost Pump OFF Fire Extinguisher ACTUATE (As required) 3. ENGINE FAILURE DURING GROUND ROLL Power Levers IDLE Brakes AS REQUIRED a.- If insufficient runway remains for stopping: Condition Levers FUEL CUT- OFF Fuel FW Shutoff Valves CLOSE Master switch OFF (Gang bar down) Boost Pumps OFF 3 4. ENGINE FAILURE AFTER LIFT- OFF Maximum Continuous Power SET Airspeed MAINTAIN (VLOF or Above) Landing Gear UP Prop Lever (Inoperative Engine) FEATHER Airspeed VYSE 108 5. ENGINE FLAMEOUT (2ND ENGINE) Power Lever IDLE Prop Lever DO NOT FEATHER Condition Lever FUEL CUT- OFF Conduct Air Start Procedures in ABNORMAL PROCEDURES 6. EMERGENCY DESCENT Crew DONMASKS/CHECK O2 HANDLE ON Power Levers IDLE Propeller Control FULL FORWARD Flaps APPROACH Landing Gear DOWN Airspeed 182 KIAS MAXIMUM