15/05/95 LIMITATIONS 02−00−1 Table of Contents REV 61, Jun 29/06 CHAPTER 2 − LIMITATIONS TABLE OF CONTENTS Page TABLE OF CONTENTS 02−00−1 INTRODUCTION General 02−01−1 Kinds of Airplane Operation 02−01−1 STRUCTURAL WEIGHT Structural Weight Limitation 02−02−1 CENTRE OF GRAVITY Centre of Gravity Limits (MTOW 48,200 Lb) 02−03−1 Centre of Gravity Limits (MTOW 47,600 Lb) 02−03−3 OPERATING LIMITATIONS Altitude and Temperature Operating Limit 02−04−1 Operation in Icing Conditions 02−04−2 Cowl Anti-Ice System 02−04−2 Wing Anti-Ice System 02−04−3 Super-Cooled Large Droplet Icing 02−04−3 Cold Weather Operations 02−04−4 Runway Slopes 02−04−5 Tailwind Conditions 02−04−5 Minimum Flight Crew 02−04−5 Maximum Occupants 02−04−5 POWER PLANT Engines 02−05−1 Engine Indications 02−05−1 Engine Operating Limits 02−05−2 Engine Operating Limits Table 02−05−2 Airplane Cold Soak 02−05−2 Oil Temperature 02−05−3 Oil Pressure 02−05−3 Continuous Engine Ignition 02−05−3 Automatic Performance Reserve (APR) 02−05−3 Starter Cranking Limits (Ground and Air) 02−05−4 Engine Start 02−05−4 Associated Conditions 02−05−4 Dry Motoring Cycle 02−05−4 CL-604 Airplane Flight Manual DOT Approved PSP 604−1 (cid:1)(cid:2)(cid:3)(cid:4)(cid:2)(cid:3)(cid:5)(cid:2) LIMITATIONS 02−00−2 Table of Contents REV 57, Jul 19/05 Page POWER PLANT (CONT’D) Engine Relight 02−05−4 Fuel 02−05−6 Fuel Temperature 02−05−8 Fuel Grades 02−05−8 Fuel Additives 02−05−9 Fuel Transfer 02−05−10 Fuel Jettison 02−05−11 Oil Grades 02−05−11 Oil Consumption 02−05−11 Oil Replenishment System 02−05−11 Auxiliary Power Unit 02−05−11 Type 02−05−11 Maximum RPM 02−05−11 Maximum EGT 02−05−11 Starting 02−05−12 APU Bleed Air 02−05−13 APU Generator 02−05−13 APU Indications 02−05−13 OPERATING SPEEDS Maximum Operating Speed and Mach Number 02−06−1 RVSM Maximum Operating Speed 02−06−1 Design Maneuvering Speed 02−06−1 Flaps Extended Speed 02−06−1 Maximum Landing Gear Operating Speed 02−06−1 Maximum Landing Gear Extended Speed 02−06−1 Tire Limit Speed 02−06−4 Maximum Airspeed for ADG Operation 02−06−4 Turbulence Penetration Speed 02−06−4 Minimum Operating Limit Speed 02−06−4 CL-604 Airplane Flight Manual DOT Approved PSP 604−1 15/05/95 LIMITATIONS 02−00−1 Table of Contents REV 61, Jun 29/06 CHAPTER 2 − LIMITATIONS TABLE OF CONTENTS Page TABLE OF CONTENTS 02−00−1 INTRODUCTION General 02−01−1 Kinds of Airplane Operation 02−01−1 STRUCTURAL WEIGHT Structural Weight Limitation 02−02−1 CENTRE OF GRAVITY Centre of Gravity Limits (MTOW 48,200 Lb) 02−03−1 Centre of Gravity Limits (MTOW 47,600 Lb) 02−03−3 OPERATING LIMITATIONS Altitude and Temperature Operating Limit 02−04−1 Operation in Icing Conditions 02−04−2 Cowl Anti-Ice System 02−04−2 Wing Anti-Ice System 02−04−3 Super-Cooled Large Droplet Icing 02−04−3 Cold Weather Operations 02−04−4 Runway Slopes 02−04−5 Tailwind Conditions 02−04−5 Minimum Flight Crew 02−04−5 Maximum Occupants 02−04−5 Maximum Crosswind Component 02−04−5 POWER PLANT Engines 02−05−1 Engine Indications 02−05−1 Engine Operating Limits 02−05−2 Engine Operating Limits Table 02−05−2 Airplane Cold Soak 02−05−2 Oil Temperature 02−05−3 Oil Pressure 02−05−3 Continuous Engine Ignition 02−05−3 Automatic Performance Reserve (APR) 02−05−3 Starter Cranking Limits (Ground and Air) 02−05−4 Engine Start 02−05−4 Associated Conditions 02−05−4 Dry Motoring Cycle 02−05−4 CL-604 Airplane Flight Manual DOT Approved AR PSP 604−1 15/05/95 LIMITATIONS 02−00−2 Table of Contents REV 57, Jul 19/05 Page POWER PLANT (CONT’D) Engine Relight 02−05−4 Fuel 02−05−6 Fuel Temperature 02−05−8 Fuel Grades 02−05−8 Fuel Additives 02−05−9 Fuel Transfer 02−05−10 Fuel Jettison 02−05−11 Oil Grades 02−05−11 Oil Consumption 02−05−11 Oil Replenishment System 02−05−11 Auxiliary Power Unit 02−05−11 Type 02−05−11 Maximum RPM 02−05−11 Maximum EGT 02−05−11 Starting 02−05−12 APU Bleed Air 02−05−13 APU Generator 02−05−13 APU Indications 02−05−13 OPERATING SPEEDS Maximum Operating Speed and Mach Number 02−06−1 RVSM Maximum Operating Speed 02−06−1 Design Maneuvering Speed 02−06−1 Flaps Extended Speed 02−06−1 Maximum Landing Gear Operating Speed 02−06−1 Maximum Landing Gear Extended Speed 02−06−1 Tire Limit Speed 02−06−4 Maximum Airspeed for ADG Operation 02−06−4 Turbulence Penetration Speed 02−06−4 Minimum Operating Limit Speed 02−06−4 CL-604 Airplane Flight Manual DOT Approved PSP 604−1 (cid:1)(cid:2)(cid:3)(cid:4)(cid:2)(cid:3)(cid:5)(cid:2) LIMITATIONS 02−00−3 Table of Contents REV 58, Dec 05/05 Page MANEUVERING LOADS Maneuvering Limit Load Factors 02−07−1 Side Slip Maneuvers 02−07−1 SYSTEMS LIMITATIONS Air-Conditioning and Pressurization 02−08−1 Automatic Flight Control System 02−08−1 Bleed Air Systems 02−08−1 Electrical Systems 02−08−2 A/C Generators 02−08−2 Permissible Loads on AC System 02−08−2 Permissible Loads on DC Systems 02−08−2 Flight Controls - Lift/Drag Devices 02−08−2 Flaps 02−08−2 Flight Spoilers 02−08−2 Stall Protection System 02−08−2 Thrust Reversers 02−08−3 Taxi Lights 02−08−3 Wheel Brake Cooling Limitations 02−08−3 Traffic Alert and Collision Avoidance System (TCAS) 02−08−4 Configuration Deviation List 02−08−4 Electrical / Avionics Equipment 02−08−4 NAVIGATION SYSTEMS LIMITATIONS Flight Management System 02−09−1 Navigation Operational Approvals 02−09−5 Enhanced Ground Proximity Warning System (GPWS) 02−09−7 Airborne Flight Information System (AFIS) 02−09−7 CL-604 Airplane Flight Manual DOT Approved PSP 604−1 (cid:1)(cid:2)(cid:3)(cid:4)(cid:2)(cid:3)(cid:5)(cid:2) LIMITATIONS 02−00−4 Table of Contents REV 59, Jan 30/06 LIST OF ILLUSTRATIONS Page Figure 02−03−1 Centre of Gravity Limits (MTOW 48,200 lb) 02−03−1 Figure 02−03−2 Centre of Gravity Limits (MTOW 48,200 lb) Airplanes 5301 to 5547, 5549 and 5550 NOT incorporating SB 604−28−007 and airplanes 5301 to 5571 NOT incorporating SB 604−27−009 or 604−27−012 02−03−2 Figure 02−03−3 Centre of Gravity Limits (MTOW 47,600 lb) 02−03−3 Figure 02−03−4 Centre of Gravity Limits (MTOW 47,600 lb) Airplanes 5301 to 5547, 5549 and 5550 NOT incorporating SB 604−28−007 and airplanes 5301 to 5571 NOT incorporating SB 604−27−009 or 604−27−012 02−03−4 Figure 02−04−1 Altitude and Temperature Operating Limits 02−04−1 Figure 02−05−1 Engine Air Start Envelope (In Flight) 02−05−5 Figure 02−05−2 Auxiliary Tank Quantity / Tail Tank Quantity − Relation Versus Centre of Gravity 02−05−7 Figure 02−05−3 Manual Fuel Transfer - Auxiliary Tank Quantity vs Tail Tank Quantity 02−05−10 Figure 02−05−4 APU In-Flight Envelope 02−05−14 Figure 02−05−5 APU In-Flight Envelope Airplanes 5301 to 5630 NOT incorporating SB 604−49−006 or 604−49−009 02−05−15 Figure 02−06−1 Maximum Operating Speed and Mach Number 02−06−2 Figure 02−06−2 Design Maneuvering Speeds 02−06−3 CL-604 Airplane Flight Manual DOT Approved PSP 604−1 15/05/95 LIMITATIONS 02–01–1 Introduction REV 52, Jan 16/04 1. GENERAL The limitations included in this chapter contain items peculiar to the CL600, model 2B16, variant CL-604 Challenger airplane. Observance of these limitations is mandatory. 2. KINDS OF AIRPLANE OPERATION The airplane is certified for day and night operations, in the following conditions when the equipment and instruments required by the airworthiness and operating regulations are approved, installed and in an operable condition: (cid:1) Day and night (cid:1) VFR and IFR (cid:1) Flight in icing conditions The airplane is certified for ditching when the safety equipment specified by the applicable regulations is installed. On airplanes incorporating Canadair Service Bulletin 604–34–012: The airplane is certified capable of RVSM operations in accordance with FAA ”Interim guidance material on the approval of operations/aircraft for RVSM operations”, 91-RVSM, dated March 14, 1994. NOTE Compliance with the standard noted above does not constitute an operational approval. CL-604 Airplane Flight Manual DOT Approved PSP 604–1 15/05/95 LIMITATIONS 02–01–2 Introduction Sep 20/95 THIS PAGE INTENTIONALLY LEFT BLANK CL-604 Airplane Flight Manual DOT Approved PSP 604–1 (cid:1)(cid:2)(cid:3)(cid:4)(cid:2)(cid:3)(cid:5)(cid:2) LIMITATIONS 02−02−1 Structural Weight REV 58, Dec 05/05 1. STRUCTURAL WEIGHT LIMITATION Maximum taxi and ramp weight: 21,909 kg (48,300 lb) Maximum take-off weight: 21,863 kg (48,200 lb) Maximum landing weight: 17,237 kg (38,000 lb) Maximum zero fuel weight: 14,515 kg (32,000 lb) Minimum flight weight: 11,794 kg (26,000 lb) Minimum operating empty weight: 10,047 kg (22,150 lb) NOTE 1. The maximum take-off weight (MTOW) and/or maximum landing weight (MLW) may be further limited due to performance considerations. 2. The maximum landing weight (MLW) is further limited when landing at airport elevations above 10,000 feet (Refer to Chapter 7; SUPPLEMENT 3 − OPERATIONS AT AIRPORT ELEVATIONS UP TO 14,000 FEET). On airplanes 5301 to 5639 NOT incorporating Canadair Service Bulletin 604−11−001: Maximum taxi and ramp weight: 21,637 kg (47,700 lb) Maximum take-off weight: 21,591 kg (47,600 lb) Maximum landing weight: 17,237 kg (38,000 lb) Maximum zero fuel weight: 14,515 kg (32,000 lb) Minimum flight weight: 11,794 kg (26,000 lb) Minimum operating empty weight: 10,047 kg (22,150 lb) NOTE 1. The maximum take-off weight (MTOW) and/or maximum landing weight (MLW) may be further limited due to performance considerations. 2. The maximum landing weight (MLW) is further limited when landing at airport elevations above 10,000 feet (Refer to Chapter 7; SUPPLEMENT 3 − OPERATIONS AT AIRPORT ELEVATIONS UP TO 14,000 FEET). CL-604 Airplane Flight Manual DOT Approved PSP 604−1 15/05/95 LIMITATIONS 02–02–2 Structural Weight Sep 20/95 THIS PAGE INTENTIONALLY LEFT BLANK CL-604 Airplane Flight Manual DOT Approved PSP 604–1