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Airplane Flight Manual

Cessna 340 · Flight Manual

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Overview

This Airplane Flight Manual (AFM) provides essential information for the operation of the Cessna 340. It is designed for pilots and aviation enthusiasts who require detailed knowledge of the aircraft's performance, systems, and operational procedures. The manual includes critical data on weight and balance, performance charts, limitations, and emergency procedures, ensuring safe and efficient flight operations. The Cessna 340 is a twin-engine aircraft known for its reliability and performance, making this manual a vital resource for both training and reference.

  • Maximum takeoff weight: 5,400 lbs (2,449 kg)
  • Cruise speed: approximately 200 knots
  • Range: about 1,200 nautical miles
  • Takeoff distance at sea level: approximately 1,800 feet
  • Maximum altitude: 25,000 feet

Document

Source

Originally published by acethermalsystems.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Flight Manual
Pages
30
File size
824 KB
Publisher
acethermalsystems.com
How rare is it?
206Cessna 340 registered worldwide · 182 active

Common. Rarer than 1% of the aircraft models we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the Cessna 340.

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In this document

Aircraft Specifications

The Cessna 340 is a twin-engine aircraft with a maximum takeoff weight of 5,400 lbs (2,449 kg). It features a cruise speed of approximately 200 knots and a range of about 1,200 nautical miles. The aircraft is powered by two Continental TSIO-520-U engines, each producing 300 horsepower.

Performance Data

The performance section includes takeoff and landing distances at various weights and altitudes. For example, at sea level and a weight of 5,400 lbs, the takeoff distance is approximately 1,800 feet. The landing distance under similar conditions is about 1,600 feet.

Weight and Balance

Proper weight and balance calculations are crucial for safe flight operations. The maximum useful load for the Cessna 340 is 1,200 lbs (544 kg). Pilots must ensure that the center of gravity remains within specified limits for safe handling.

Emergency Procedures

This section outlines critical emergency procedures, including engine failure, electrical failure, and cabin depressurization. Pilots are advised to follow the checklist for each scenario to ensure safety.

Limitations

The manual specifies operational limitations, including maximum altitude of 25,000 feet and maximum airspeed of 200 knots. Pilots must adhere to these limitations to maintain safety and compliance.

Safety notes

  • Always perform weight and balance calculations before flight.
  • Adhere to operational limitations to ensure safety.
  • Follow emergency procedures as outlined in the manual.

Full document text

Keith Environmental Systems INSTALLATION INSTRUCTION AND SERVICE MANUAL FOR INSTALLATION OF AIRCONDITIONING KITS MODEL CESSNA 340/340A REPORT NO. 34-010-59M REPORT DATE: October 19, 1977 PREPARED BY: CHECKED BY: APPROVED BY: J.R. Sattler PREPARED BY: CHECKED BY: DATE: REV 10-22-84 B REV. DATE TITLE Keith Environmental Systems Keith Products, Inc. 4864 Claire Chennault Dallas, TX 75248 Phone (214) 407-1234 Fax (214) 407-1571 PAGE NO INSTALLATION INSTRUCTIONS DESCRIPTION OF REVISION REPORT NO. 34-010-59 MODEL NO. 340/340A BY APPROVAL 8-11-81 Last revision was 10-19-77. No record of previous revisions. Updated to Parker Format. KR A 10-22-84 Kit List raised to Rev E. KS Kit List Rev E removed from Install Instructions. Added Table of Contents to Install Instruction. Added "Item" pages I, II, III. джу Added STC, Weight & Balance, FMS to III Aircraft Documents section. B 1-11-88 Revised to ADD required publications section for new format ECN287-59. REH Rett C 4/3/92 Deleted warranty information KS ; TABLE OF CONTENTS ITEM I. II. III. IV. INSTALLATION INSTRUCTIONS REQUIRED PUBLICATIONS SERVICE AND MAINTENANCE MANUAL AIRCRAFT DOCUMENTS STC # SA16RM Weight & Balance Data Flight Manual Supplement SECTION I INSTALLATION INSTRUCTIONS INSTALLATION INSTRUCTIONS CESSNA MODEL 340/340A 1. PREPARATION FOR INSTALLATION a. Remove pilot's seat and all passenger seats on left hand side of aircraft. b. Remove console on left hand side of aircraft housing switch and circuit breaker panels. c. Remove left forward baggage compartment floors. 2. PLUMBING AND WIRING INSTALLATION (Reference Drawings 34-010 and-050) a. Install switches and circuit breakers in appropriate panels on a "space available" basis and route wiring. b. Install pressure grommet mounting holes and grommets as shown on 34-010 and 34-050 drawing in the forward and aft pressure bulkheads; install drain valve solenoid. c. Route plumbing as indicated. d. Seal pressure grommets with silicone sealer, assuring adequate lengths of hoses are present to make connections. CAUTION: Before starting installation, assertain exactly which installation kit is being installed. 3. COMPRESSOR/MOTOR PALLET INSTALLATION (Reference Drawings 34-050) a. Install Z section supports at stations 77 and 91.5 as indicated. b. Install compressor pallet assembly per drawing. c. Connect freon lines and electrical wiring. 4. PROVISIONS FOR THE CONDENSER FAN INSTALLATION (Reference Drawing 34-050) ; a. Position skin doubler as indicated and scribe cut out of the skin; remove doubler and complete cutout; deburring and smoothing edge. b. Install doubler, drilling through the skin using the pilot holes in the doubler as a pattern. Rivet in place. c. Position the fan in position as shown, assuring clearance from compressor pallet assembly; mark attach holes on doubler, remove fan assembly and drill through. INSTALLATION INSTRUCTIONS CESSNA MODEL 340/340A Page 2 - 4. PROVISIONS FOR THE CONDENSER FAN INSTALLATION cont'd d. Install deflector from the inside%3B hold in position and drill through flange from front two holes installed in Step C previously; set aside until later. 5. INSTALLATION OF AIR INLET DEFLECTOR (Reference Drawing 34-050) a. Position the skin doubler as shown externally and scribe cutout in skin; and using pilot holes as a pattern, drill all holes; remove and complete cutout%3B deburr and smooth edge of cutout. b. Position doubler on the inside and rivet in place. c. Position inlet deflector on inside over cutout and drill holes thruskin, doubler and flanges. Install mounting hardware. d. Position screen and secure as shown. 6. INSTALLATION OF CONDENSER (Reference Drawing 34-050) a. Install forward lateral floorboard angle to station 62.0 structure as indicated. b. Mount the condenser to the forward floor panel to clear structure as indicated. c. Notch the legs of the angles on the aft edge of forward panel and the forward edge of the aft panel to provide clearance for the upper inboard freon hose. d. Install the forward floor panel with condenser and freon lines attached by positioning both floors before installing rivnuts to assure correct location. 7. INSTALLATION OF CONDENSER FAN a. Using washers as shims to match contours, install the fan with provided hardware thru the previously installed doubler. (Install screen and negative scoop at the same time.) b. Install ducting between condenser and condenser fan. c. Make electrical connections. INSTALLATION INSTRUCTIONS CESSNA MODEL 340/340A Page 3 - - 8. INSTALLATION OF EVAPORATOR ASSEMBLY (Reference Drawing 34-010) a. Floor-Mounted Alternate 1) Remove carpeting and bulkhead upholstery panel. 2) Locate evaporator box and wooden cover box in right rear corner. Locate clips to hold down evaporator per drawing. Locate clips to hold evaporator cabinet in place. Locate drain tube outlet and install in bottom of evaporator. Drill clearance hole in floor panel for drain and hose locations. Add duct clip to top of box. 3) Attach hoses and drain tube and secure evaporator box. Secure evaporator cabinet over it. 4) Attach the duct assembly. b. Aft Overhead Centerline Mounting 1) Locate the ZEEs under headliner and clip into frames at stations 232 and 242. 2) With the evaporator plastic cover removed match drill mounting panel in conjunction with the ZEES and attach nut- plates in the ZEEs. 3) Attach the evaporator using provided screws. 4) Hook up plumbing connections and drain hose to drain valve in lower skin, penetrating bulkhead. 5) Install plastic evaporator cover. 6) Install forward overhead centerline distribution duct or free-blow outlet, which ever is applicable. 9. CHARGING AND TESTING a. Charge and test system in accordance with Service data. b. Install aft nose compartment floor. 10. WEIGHT AND BALANCE a. Forward Installation 58 lb at Station 79 b. Aft Installation (Top) 15 lb at Station 280 ; INSTALLATION INSTRUCTIONS CESSNA MODEL 340/340A Page 4 10. WEIGHT AND BALANCE cont'd c. Alternate Aft Installation (Floor)

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14.8 lb at Station 244.6 d. Alternate Aft Installation (Ceiling Evaporator) 15.0 lb at Station 242.0 Alternate Aft Installation (Ceiling Duct) 6.0 lb at Station 183.0 SECTION III SERVICE AND MAINTENANCE MANUAL II. REQUIRED PUBLICATIONS TO INSTALL34-010-59 AIRCONDITIONER KIT INSTALLATION DRAWINGS: 34-010 (SHTS. 1, 2, & 4) GENERAL ARRANGEMENT AND INSTALLATION 34-050 (SHTS. 1 4) INSTALLATION COMPRESSOR/CONDENSER INSTALLATION MANUALS: 34-010-59 P/L COMPUTERIZED PARTS LIST 34-010-59M INSTALLATION INSTRUCTIONS (THIS DOCUMENT) SERVICE DOCUMENTS: TR128 AIRCONDITIONING SERVICE MANUAL DESCRIPTION - AIRCONDITIONING SYSTEM The KEITH Airconditioning unit is composed to two major 1) the equipment package and 2) the evaporator component installations: package. The Equipment Package comprises the compressor, drive motor, condenser fan, coil, and receiver drier. The Evaporator Package consists of the evaporator coil, blower, blower drive motor, and the expansion valve. The control for the system is located on the pilot's switch panel and consists of a simple on-off switch; some units carry a fan only position. When the switch is placed in the ON position, the compressor, driven by an electric motor, compresses the Freon gas to a high pressure and high temperature. This gas is routed to the condenser where cooling from the fan removes heat from the gas, condensing it to a liquid. The liquid is then stored in the receiver drier, adjacent to the compressor, until it is used. The Freon is metered to the evaporator through the expansion valve at a rate to allow all the liquid to evaporate and return to the compressor at a reduced pressure. The cabin heat is absorbed from air passing over the evaporator cooling fins. See Figure No. 1. CAUTION WHEN THE AIRCONDITIONER IS TURNED OFF, IT IS RECOMMENDED THAT A MINIMUM OF THREE MINUTES ELAPSE BEFORE IT IS TURNED ON AGAIN: THIS ALLOWS THE COMPRESSOR HEAD PRESSURE TO BLEED OFF AND BRING THE STARTING LOAD TO NORMAL. TROUBLE SHOOTING THE AIRCONDITIONING SYSTEM TROUBLE Insufficient or no cooling (Low side gauge reads High, High side gauge reads Low) (Low side gauge reads High, High side gauge reads High) (Low side gauge reads High, High side gauge reads High) (Low side gauge reads Low, High side gauge reads Low) Insufficient or no cooling (Gauges read pressure as normal) PROBABLE CAUSE Inoperative evaporator blower Complete loss of Freon charge Partial loss of Freon charge (continual foam in sight glass after turning system on). Compressor malfunction Head gasket failure or valves not seating Condenser malfunction Condenser Fan malfunction Condenser blocked Expansion Valve mal- function Expansion Valve mal- function Compressor belts broken Expansion valve in- operative, stays open or closed Moisture or air in system Inoperative compressor motor CORRECTION Check wiring, circui breaker, repair or r place blower Evacuate system. Recharge system and check for leaks. Recharge system and check for leaks. Replace compressor a) Check fan circuit to verify correct functioning. b) Blow out condens c) Replace condenser Purge system, re- place valve, evacuat and recharge. Purge system, re- place valve, evacuato and recharge. Service valves im- properly set (should be maximum counter clockwise). Replace belts. (Tension to 30 lbs.) Replace expansion valve. Evacuate system and re-charge (per charg procedure). Inspect wiring, circ breakers. Repair or replace compressor n 2. i TROUBLE SHOOTING THE AIRCONDITIONING SYSTEM (Cont'd) TROUBLE Noisy Compressor Noisy Fan PROBABLE CAUSE Loose, torn or mis- aligned belt Foreign material or damaged port in com- pressor Compressor loose on bracket Fan striking housing Fan shaft bearings out EVACUATION AND CHARGING PROCEDURES CORRECTION Align or replace belt. Remove and replace compressor. Tighten compressor. Check fan travel. Replace bearings. The evacuation and charging procedures given are factory recommended. If followed, these procedures will give optimum results. The following equipment must be available to properly service the air- conditioning system. a) Charging manifold and hoses b) Refrigerant can adapter c) R-12 refrigerant cans or R-12 cylinder d) Vacuum pump capable or operating at least 28 to 29 inches Hg e) 1/4" open end wrench CONNECTING THE MANIFOLD AND HOSE a) Remove caps from service ports on compressor b) Connect compound gauge (low pressure) hose to suction port c) Connect high pressure gauge hose to discharge port d) Close valves on the charging manifold (turn clockwise) 3 RECHARGING THE SYSTEM Whenever it becomes necessary to replace any of the refrigerant. components or lines, the refrigerant pressure must be discharged. Open oil filler plug in compressor until seal is broken and Freon escapes slowly. CAUTION EXERCISE CARE WHEN RELEASING REFRIGERANT GAS. THIS IS A HIGH PRESSURE SYSTEM: GOGGLES AND GLOVES SHOULD BE WORN FOR PROTECTION. EVACUATION OF THE REFRIGERANT SYSTEM a) Connect manifold and hose in accordance with Connecting Procedures. b) Connect center hose from charging manifold to vacuum pump and turn pump on. c) Open service valves halfway (turn counter clockwise) on compound gauge (low pressure). d) Continue to pull a vacuum on the system for 30 minutes after compound gauge reaches 28 inches or more on vacuum gauge. e) Periodically check for leaks by closing valves and verify- ing that system is holding vacuum. NOTE IN THE EVACUATING PROCEDURES GIVEN, THE SPECIFICATION FIGURE, 28 INCHES OF MERCURY OR MORE IS USED. THIS FIGURE IS ONLY ATTAINABLE AT OR NEAR SEA LEVEL. FOR EACH 1000 FEET OF FIELD ELEVATION WHERE THIS OPERATION IS BEING PERFORMED, LOWER THE SPECIFICATION FIGURE ONE- (1) INCH. f) Close hand valve (clockwise) on compound gauge. g) Turn off vacuum pump and disconnect from charging hose. CHARGING THE REFRIGERANT SYSTEM a) Connect manifold and hose in accordance with Connecting Procedures. CAUTION USE ONLY R-12 IN THIS SYSTEM b) Connect center manifold hose to R-12 can, using can ad- apter or R-12 cylinder. Open valve on can adapter or cylinder. c) Slightly loosen connect of center hose at manifold to purge any air trapped in hose. (This should take ap- proximately one second.) Tighten center hose connection. d) Open low side valve and do not exceed 40 PSI on low side gauge. NOTE MOST OF THE FIRST CAN WILL BE PULLED INTO UNIT SYSTEM BY VACUUM. e) Connect APU or start engines and turn on airconditioning system, refrigerant will begin to be pumped from the can into the condensing unit. f) Charge to a High Pressure Reading as follows: Ambient Temperature 80 F 90 F 95 F 100 F 105 F High Side Pressure 150 - 170 psi. 175 195 psi. ; 185 - 205 psi. 210 - 230 psi. 230 - 250 psi. - 40 psi.) (Low side reading should be 20 CHARGE ONLY UNTIL THE SIGHT GLASS IN THE RECEIVER DRIER IS CLEAR OF BUBBLES. g) Close hand valve (clockwise) on compound gauge and close valve on can adapter or cylinder. h) Disconnect charging hoses from high side unit. (Some re- frigerant trapped in the hoses will be expelled at this time and sound as though the system is leaking. This is normal.) i) Back seat service valves (fully counter clockwise); replace caps on suction and discharge ports. 5.

Type certificate, explained

What's in the Cessna 340 TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS 3A25Rev 25· Issued 1994
Read the full TCDS

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