ATR 72-212A Aircraft Flight Manual (AFM) – 600 Version PDF Download
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Complete ATR 72-212A “600” version Aircraft Flight Manual (AFM) covering limitations, normal procedures, emergency procedures, performance charts, and appendices. EASA-approved REV15, February 2012, 416 pages.
Description
ATR 72-212A Aircraft Flight Manual (AFM) β 600 Version
This is the complete Aircraft Flight Manual (AFM) for the ATR 72-212A aircraft, specifically the “600” version equipped with the new avionics suite. The document is approved by EASA on behalf of the AgΓͺncia Nacional de AviaΓ§Γ£o Civil (ANAC) for Brazilian registered aircraft, and represents the full operational and technical reference required for flight crews, maintenance engineers, and training departments. The ATR 72-212A Aircraft Flight Manual AFM PDF covers every chapter from general information and limitations through to performance charts and appendices, giving you the authoritative source for operating this regional turboprop safely and within certified limits.
File Details
- Manual Type: Aircraft Flight Manual (AFM)
- Brand: ATR β Avions de Transport Regional
- Model: ATR 72-212A (“600” version)
- Language: English
- Page Count: 416
- File Format: PDF
- Revision: REV15, February 2012 (FEB 12)
- Approval: EASA approved on behalf of ANAC, June 29th 2011
- Manufacturer: Avions de Transport Regional, Direction Support Exploitation, 1 AllΓ©e Pierre NADOT, 31712 BLAGNAC Cedex, FRANCE
Chapters Covered
- 1 β General: Introduction, Particular Explanations, Unit Conversion, Glossary of Standard Nomenclature, 3-View Drawing
- 2 β Limitations: General Introduction, Kinds of Operation, Minimum Flight Crew, Performance Configuration, Maximum Operating Altitude, Maneuvering Limit Load Factors, Configuration Deviation List, Noise Characteristics, Maximum Number of Passenger Seats, Weight and Loading, Center of Gravity Envelope, Airspeed and Operational Parameters, Power Plant (Engines, Propellers, Oil System, Starter, Fuel System), Systems (Air/Pressurization, Hydraulic System, Landing Gear, Flaps, AFCS, Instruments Marking, Cargo Door Operation, Electrical, MFC, Communications, TCAS, FMS, Cabin Lighting, TAWS, Airport Navigation Function), Icing Conditions, Temporary Limitations
- 3 β Normal Procedures: Cockpit Preparation Checks, Daily Checks, Take Off, Flight Conditions (Icing Conditions, Severe Turbulence), Approach and Landing, Container Transportation, TAWS
- 4 β Emergency Procedures: Introduction, Power Plant (ENG 1(2) Fire or Severe Mechanical Damage In Flight, On Ground, At Take Off, Both Engines Flame Out), Smoke (Electrical, Air Conditioning, FWD, AFT, AUX AFT Compartment), Electrical System (Dual DC Gen Loss), Miscellaneous (Emergency Descent, Ditching, Forced Landing, On Ground Emergency Evacuation, Severe Icing, Recovery After Stall or Uncommanded Roll Control, Unreliable Airspeed Indication)
- 5 β Procedures Following Failure: Introduction, Engine (ENG 1(2) Flame Out In Flight, ENG 1(2) Oil Lo Pr, One EEC Fault, ENG Relight Envelope, ENG Restart In Flight, NAC OVHT), Flying With One Engine Inoperative (Take Off, Approach and Landing, Missed Approach), Systems (Fuel, Electrical System, Hydraulic System, Flight Controls, Landing Gear, Air, Ice and Rain Protection, MFC, Autopilot, Propeller Control, Miscellaneous)
- 6 β Performance: General (Introduction, Stall Speeds β VSR, Airplane Configuration, Crosswind, Determination of Wind Components, Calibration Speed and Altitude), Engine Management, Take Off (Definition, Performance Determination, Maximum Take Off Weight, Performance Charts, AltitudeβSpeedβBank AngleβTurn Radius Relationships), Single Engine Cruise, Landing, Atmospheric Icing Conditions
- 7 β Appendices and Supplements: External Noise, Configuration Deviation List, CAT II Operation, TCAS, Steep Slope Approach, Cargo/Cargo+Pax Configuration, ETOPS, Operations on Narrow Runways, Runway Slope Beyond 2%, Take-Off After Use of Fluids Type II or IV, Cockpit Door Locking System, Corporate Lounge, Aircraft Performance Monitoring (APM), SSR Mode S Enhanced Surveillance, ACARS, High Latitudes Operations, Dry Unpaved Runways, Take Off at 100% Torque, 20 kt Tailwind Take Off, Supplements (Dispatch with one ACW generator channel inoperative, spoilers control system inoperative, flaps retracted, one wheel brake deactivated, anti-skid system inoperative, autofeather system inoperative, one EEC OFF, one AFU inoperative, one TQ indicator inoperative, ATPCS OFF, landing gear down, ferry flight with pitch elevators disconnected), Advisory Materials (Non Dry Runways β General, Take Off, Landing), LBA Supplement, Operations in CIS Countries, ANAC Supplement
The ATR 72-212A Aircraft Flight Manual AFM is the single-source reference that ties together every operational domain of the aircraft. Limitations chapter sets the hard boundaries β VMO 250 kt CAS, MMO 0.55, maximum operating altitude 25,000 ft, maneuvering load factors +2.5 to -1 g clean and +2 to 0 g with gear/flaps extended, maximum weights (RAMP 23,170 kg, TAKE-OFF 23,000 kg, LANDING 22,350 kg, ZERO FUEL 21,000 kg), crosswind limits, icing envelope, and temporary limitations applicable to the “600” version. Normal Procedures gives you the exact checklist flows for cockpit preparation, daily checks, ATPCS test, stick pusher/shaker test, engine boost test, take-off, icing conditions, severe turbulence, approach and landing, missed approach, and TAWS operation. Emergency Procedures covers memory-item drills and expanded procedures for engine fire, dual DC gen loss, smoke of every origin, emergency descent, ditching, forced landing, ground evacuation, severe icing, recovery after stall or uncommanded roll control, and unreliable airspeed indication. Procedures Following Failure gives you the non-emergency failure handling for engine flame-out, oil low pressure, EEC faults, fuel leaks, electrical faults, hydraulic faults, flight control jams and disconnects, landing gear anomalies, air bleed faults, ice and rain protection faults, MFC module failures, autopilot mistrims, propeller control faults, and miscellaneous avionics degradations. Performance gives you the take-off, single-engine cruise, landing, and icing-condition performance data, including V1 limited by VMCG, VMCA, VR, V2, TOR, TOD, ASD, obstacle clearance flight paths, and the corrections for tailwind, slope, air conditioning, and engine bleed. The Appendices and Supplements close the loop with configuration deviation list, CAT II operations, TCAS, ETOPS, narrow runways, runway slope beyond 2%, fluid type II/IV take-off, APM, SSR Mode S Enhanced Surveillance, ACARS, high latitude operations, and all MMEL dispatch supplements.
This ATR 72-212A Aircraft Flight Manual AFM PDF is the reference flight crews, dispatchers, and maintenance personnel rely on to verify every limit, every procedure, and every performance number before flight. It is the document that keeps the operation within certified boundaries and gives you the approved data to plan take-off, en-route, approach, and landing safely. Whether you are preparing for a line check, building a training syllabus, or verifying a specific limitation on the “600” version, having the complete AFM at hand means you are working from the approved source rather than from memory or third-party summaries.
Complete Bookmarks
The complete bookmarks in the βATR 72-212A Aircraft Flight Manual (AFM) – 600 Version PDF Downloadβ are as follows:
IMAGES PREVIEW
With this ATR 72-212A Aircraft Flight Manual AFM you can perform the full range of tasks the aircraft demands β pre-flight limitation checks, performance planning against the approved charts, emergency procedure review, failure handling for systems and powerplant, icing condition assessment, and configuration deviation dispatch decisions. The value lies in the precision: correct V-speeds, correct torque and ITT limits, correct emergency memory items, and correct performance corrections for the actual conditions. Getting these wrong is not an option in commercial operations, and this manual removes the guesswork. Delivered as an instant PDF download after payment, no shipping, no waiting. Read it on any device β laptop, tablet, or phone β and print the pages you need for the cockpit or the hangar. The file is the complete 416-page document, exactly as approved by EASA.
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