CR4J 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-4 LIMITATIONS INTRODUCTION The [imitations included in this chapter contain items that are applicable to the CL600-2C10 (CRI700) airplane. Observance of these limitations is mandatory. ‘The information presented in this chapter contains limitations that have been extracted from the Aircraft Flight Manual (AFM) and Flight Crew Operating Manual (FCOM). The limitations in this chapter are not all inclusive. In addition, SOP limitations do not represent all aircraft configurations, For a specific aircraft configuration consult the AFM or applicable airline manual, BLL i in erat ‘The airplane is certified in the transport category 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: «© VFR and IFR * Flight in icing conditions The airplane Is certified for ditching when the safety equipment specified by the applicable regulations is Installed. ‘The alrplane is certified capable of RVSM operations in accordance with the FAA “Interim guidance material on the approval of operations/aircraft for RVSM operations.”, 91-RVSM, datad June 30, 1999 and with the JAA Temporary Guidance Leaflet, TGL No. 6, Revision 1, RVSM. Note: Compliance with the standard noted above does not constitute an operational approval RVSM operations must not be commenced or continued unless all of the required équipment specified below is operational, RVSM REQUIRED EQUIPMENT LIST EQUIPMENT REQUIRE! AUTOPILOT (1) MUST BE OPERATIONAL, FOR RVSM ALTITUDE ALERTING SYSTEM MUST BE OPERATIONAL ALTITUDE REPORTING TRANSPONDER (2) | ONE (1) MUST BE OPERATIONAL TWO (2) MUST BE OPERATIONAL AIR DATA COMPUTERS (2) Rev: 18 7 Section: 3 ffs Oorzaro9 GoJdet Pages 4CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS. Procedures Manual 3-2 STRUCTURAL WEIGHT LIMITATIONS. The following information is provided for the extended range (ER) version of the CRJ700 aircraft. : Weights “Maximum Taxi and Ramp Weight | __75,250 lbs Maximum Takeoff Weight 75,000 tbs, Maximum Landing Weight 67,000 Ibs, Maximum Zero Fuel Weight 62,300 tbs. Minimum Flight Weight 42,000 tbs. | _ Minimum Operating Empty Weight 39,835 lbs. | ‘The maximum takeoff weight (MTOW) and/or maximum landing weight (MLW) bay be further timited due to performance considerations. Rov. 1 - Section: 3 Eff: 08/31/05 Gotet Eeerw es eeeCRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS. Procedures Manual 3-3 CENTER-OF-GRAVITY LIMITS ‘The CRJ700 (ER) maximum permissible center-of-gravity (CG) range with landing gear extended Is shown in the figure below. The effect of landing gear retraction on CG position is negligible, For other weight variants, refer to the AFM, & Weight (1000 ka) Weight (1000 Ibs) a Enroute Unit 36757 20 ‘Longitudinal CG Envelope Optional 35 I 15 5 10 41s 20 25 30 35 40 ce (MAG) Section; 3 Rev.: 1 | Pase 3 Eff: 08/31/05,CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-4 ALTITUDE AND TEMPERATURE OPERATING LIMITS ‘Maximum airport pressure altitude for takeoff and landing is 8,000 feet. Maximum operating altitude is 41,000 feet. ‘The maximum ambient air temperature approved for takeoff and landing is ISA +35°C. The minimum ambient temperature approved for takeoff is ~40°C (-40°F), 3-5 OPERATION IN ICING CONDITIONS. 3-5.1 Cowl Anti-Ice System 3-5.1.1 Ground Operations Cowl anti-ice system must be ON when the OAT is 10°C (50°F) or below: + and visible moisture in any form is present (such as fog with visibility of 1,500 meters [1 mile] or less, rain, snow, sleet and ice crystals) ‘+ when operating on runways, ramps or taxiways where surface snow, ice, standing water, or slush is Present 3-5.1.3 Flight Operations Note: Icing conditions exist in-flight at a TAT of 10°C (50°F) or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet or ice crystals), except when the SAT is -40°C (-40°F) or below. The engine cowl anti-ice system must be ON when: + in icing conditions, or ‘+ ICE is annunciated by the ice detection system 3-5.3 Wing Anti-Ice System 3-5.3.1_ Ground Operations ‘Wing anti-ice system must be ON for takeoff when the OAT is 5°C (41°F) or below and: + visible moisture in any form is present (such as fog with visibility of 1,500 meters [1 mite] or less, rain ,snow, sleet and ice crystals) © the runway contaminated with surface snow, slush or standing water When Type I! or Type IV anti-icing fluids have been applied: ‘* wing anti-ice system must only be selected ON, if required, just prior to thrust increase for takeoff of a Section: 3 08/31/05 GoJset ote ATR CTR ESSOP — CRJ 700 Standard Operating Procedures Manual Pete na tee ee renon Tee 3-5.3.3 Flight Operations Note: Icing conditions exist in-flight at a TAT of 10°C (50°F) or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet or ice crystals), except when the SAT is ~40°C (-40°F) or below, ‘The wing anti-ice system must be ON when: + ICE is annundiated by the ice detection system, or ‘+ in icing conditions and the airspeed Is less than 230 KIAS Note: Do not hold in icing conditions with Slats/Flaps extended, 3-5.5 Supercooled Large Droplet Icing Continued operation in areas where supercooled large droplet (SLD) icing conditions exist is prohibited, SLD Icing conditions are indicated by ice accretion on the flight deck side windows, ‘+ wing and cowl anti-cing systems must be ON in SLD Icing conditions + leave icing conditions when side window icing occurs, 3-6 COLD WEATHER OPERATIONS Take-off Is prohibited with frost, ice, snow or slush adhering to any critical areas (wings, upper fuselage, horizontal stabilizer, vertical stabilizer, control surfaces, and engine inlets, WARNING: Even small amounts of frost, Ice, snow or slush on the wing leading edges and forward upper wing surface may adversely change the stall speeds, stall characteristics and the protection provided by the stall protection system, which may result in loss of control on take-off. Note: Takeoff is permitted with frost adhering to: ‘+The upper surface of the fuselage if and/or is possible to distinguish surface features. See WOP 2.13.1; (3.0 mm) layer of frost on the underside of the wing that is caused by cold soaked ‘Comprehensive procedures for operating in cold weather are provided in the GoJet Winter Operations Ground Icing Program. Rev. 17 ec Section: 04/30/09 Godse cede aud See Poge: 5SOP — CRI 700 Standard Operating Procedures Manual LIMITATIONS & MEMORY ITEMS 37 RUNWAY SLOPES ‘The maximum runway slopes approved for takeoff and landing are: + +2% (uphill) *-2% (downhill) 3-8 ‘TAILWIND CONDITIONS ‘The maximum tailwind component approved for takeoff and landing is 10 knots. 39 MINIMUM FLIGHT CREW ‘The minimum flight crew is one pilot and one copilot, 3-10 FLIGHT DECK DOOR The flight deck door must be kept closed and locked at all times during fight except to permit access and egress in accordance with the approved procedures for opening, closing and locking the door. Any time the flight deck door is opened in-flight, a challenge and response closing and locking verification must be used to verify that the door is dosed and locked. Any time one of the required flight crew leaves the flight deck another crew member must be present In the flight deck to ensure that the required crew member is not locked out of the flight deck, BAL CARGO Flight must be within 60 minutes of a suitable airport, if cargo is carried in either cargo compartment. 3-12 OZONE CONCENTRATION Airplane operations are prohibited on routes where ozone concentrations will exceed the following limits: ‘* 0.25 parts per million by volume, sea level equivalent, at any time above flight level 320, and + 0.1 parts per million by volume, sea level equivalent, time-weighted average during any 3 hour interval above flight level 270 Note: ‘Sea level equivalent’ refers to conditions of 25°C and 760 millimeters of mercury pressure, Data to determine flight altitudes and/or duration at altitude in compliance with these requirements are given in Flight Planning and Cruise Control Manual, Chapter 6, SPECIAL OPERATIONS, Maximum Allowable Cabin Ozone Concentration. Flight crews may utilize SOP 3-28.3, Maximum Flight Duration at Altitude Due to Cabin Ozone Concentration, for determining flight duration at altitudes higher than originally planned by Dispatch. 30 G oJet Section; 7 ogts/12 Cee Page:CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-13 ENGINES 3-13.1. Engine Indications The CRJ700 aircraft uses two General Electric CF34-8C5B1 engines, The engine limit display markings on EICAS must be used to determine compliance with the maximum/minimum limits and precautionary ranges. If EICAS markings show more conservative limits than those specified below, the limit markings on the EICAS must be used. Note: Red - Maximum and minimum limitations. Amber - Caution range. Green - Normal operating range. a CF34-8C5B1 [CF34-8C1] (CRJ700) Engines Indication Red ‘Amber Green Nem | 99.5 : 0t0 99.4 N; rpm 99.4 seeeeeteaeeca |e 0t0 99.3 mc Variable ais Variable oil Temp *C 164 15610163 | -40 to 155 Oil Press psi Otom | Variable Variable 3-13.2 Powerplant Intermix Powerplant intermix operations are prohibited, 3-13.3 Engine Warm-up ‘The engine must remain at IDLE until oil pressure reaches normal operating range. During all starts, do not exceed 75% N; for 2 minutes after start, or until all operating indications are in the normal range, whichever is longer. 3-13.4 Thrust Management Data With the engines running and bleeds configured for take-off, the crew must verify that the target Ny values correspond to the data presented in the thrust setting charts ( 1.0%). Refer to PERFORMANCE THRUST SETTINGS. With the thrust levers set for take-off, target and actual N; values should match. 3-13.5 Engines High-Power Schedule Switchlight Use of the ENGINES HIGH PWR SCHEDULE switchtight is prohibited. 8 . Section: 3 11/24/06 GoJet tee 7RJ 700 Standard Operating Procedures Manual LIMITATIONS & MEMORY ITEMS 3-13.7 Engine Operating Limits CFSeaCsBt ASSISTED NORMAL | _APR(2] GROUND WINDMILL MaxiMUM uM AIR START LE TAKEOFF | (WAX sranrisy | ARSTART | stant F _[eowmuows | Tsai | power Ni - 5 5 20.25% 005% 995% | 905% : : : : ere | 1006" mn aso | aise were s60°c Panic ary : ‘ : : uso | src (min) | Gain) Ne 045% | 045% : wan | 980% cea [900% 0c we | 16rC OMTEMP | (rintum) 155° | casminy | (15min) sy | 260rsit6] teopsi | te2psiy | t82psie7 ; OIL Press ee ae : eet "| asses: | 595s | 5950s eee (ater 10m | (afer te) | (ater tommy | Pome | IIE a me minimum | At oiLtevel | | wi affected | - zi : : : : FORA | ern slated {1} Nera takot power and maxima power two engines is lied oS minutes, [2]_ APR power (ane engine) is ited 6 10 minutos. [3] _ITT must be below 120°C beloe atianpting to ground stat engine, [4] ITT must be below 60°O beloreatlenping oa start engine. {5]__ Maximum ol pressures ried o 168 pheno trporatrovansontie ea than 60°C. [6] _Oilpresues (shove IDLE betwen 25 and 45 pl raquo empeaure mono [7] Ollpressures should show postive value during start and may peak beyond 182 pi (max display value). Ol pressures above 182 pela splayed 2 ember dashes. (pressure may bo greater han 95 psi fora maximum of 10 minutes. {6} _Fortuther dea, reler tothe Fig Crew Operating Marual, Vol. 1, OSP E013 - POWERPLANT -OlL SYSTEM. Rev.: 2 Eff. 02/03/06 GoJvet Section: Page:CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-13.9 Airplane Cold Soak prone the fist flight of a day, when the airplane is cold-soaked at an ambient temperature of 30°C ( 22°F) or below for more than 8 hours: + the engines must be motored for 60 seconds and the fan rotation must be verified before an engine start is initiated * thrust reversers must be actuated until the deploy and stow cycles are 2 seconds of less 3-13.11 Continuous Engine Ignition Continuous engine ignition must be used during the following: ‘+ takeoffs and landings on contaminated runways ‘+ flight through moderate or heavier intensity rain + flight through moderate or heavier intensity turbulence + flight in the vicinity of thunderstorms 3-13.13 Starter Cranking Limits 3-13.13.1 Associated Conditions The starter must not be used if indicated Ne rpm exceeds 45%, At initiation of thrust lever movement from SHUT OFF to IDLE: + ITT must be 120°C or less for all ground starts + TT must be 90°C or tess for ail air starts 3-13,13.3 CRJ700 ENGINE START (GROUND) ee START __ MAXIMUM TIME ON FOLLOWED BY “182 Wseconds | 10 seconds coal down 3 through 5 ~___8089cands “_S minutes cool down ree ENGINE START OR MOTORING (FLIGHT) STARTIMOTORING | MAXIMUM TIME ON ____ FOLLOWED BY [ 1 [120 seconds 10 seconds coo! down 2 through § ‘60 seconds E ‘minutes cool down ______ MOTORING (GROUND) iat i. _ TMOTORING MAXIMUM TIME ON FOLLOWED BY tien seconds ____Siminutes cool dow 2 through & ae - ‘minutes coot down Rev: 10 £ Section: 3 Er: 02/25/07 Godse Page: "9CRJ 700 Standard Operating Procedures Manual LIMITATIONS & MEMORY ITEMS. eS ee ee eee eee ery 3-13.13.5 Engine Relight Limitations Relight Type Relight Envelope (see figure below) Windmilting Windmilling Altitude from 21,000 to 10,000 feet: Speed 290 KIAS to Vig and 7.2% No minimum Altitude from 10,000 feet to sea level: Speed 250 KIAS to Vg and 7.2% No minimum Starter Assisted All-Engine-Out Rapid Retight Altitude from 21,000 feet to sea level: ‘Speed from Vser Up to Vino and from 0 to 45% Nz. Altitude from 10,000 feet to sea level: FADEC rapid relight capability has been demonstrated at 200 KIAS for up to 15-second fuel interruptions, Engine starting in-flight is only permitted within the envelope defined below. 3-13.13.5.1. Engine Start Envelope Figure Note 1: Special All-Engine-Out rapid relight envelope is from 10,000 feet to SL and 200 to 250 KIAS. Efr.: 06/02/08 a oJset sear: = oe Page:CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS 1 Procedures Manual 3-14 ENGINE OPERATING LIMITS DUE TO WIND DIRECTION Wind and fan speed limitations listed below must be observed, a\ 20 He ag Faraeani SHOE] ‘See NOTE 3) t | Wind Condition Limitation NOTE 1 Within 30° on elther direction of the airplane nose; no | No limitations TOGA thrust may | windspeed limit. be applied before brakes “OR: released, 30° in either direction of the airplane nose; < 5 knots windspeed. | NOTE 2 | >30° in either direction of the airplane nose; between 5 Apply maximum of 75% Ny before and 30 knots windspeed. brakes released, then TOGA thrust. NOTE 3) >30° in either direction of the airplane nose; >30 knots | Apply maximum of idle/taxi windspeed. thrust before brakes released, then TOGA thrust. Rev. 1 vm Section: 3 Eff.) 08/31/05 Godse [PeeEro dou erandeld Operating LIMITATIONS & MEMORY ITEMS Procedures Manual D 3-15 FUEL 1 3-15.1 Fuel Quantities Center tank fuel quantity must be monitored throughout the flight. ‘The maximum permissible fuel imbalance between the contents of the left wing tank and the right wing tank are given below: + during takeoff: 300 tbs (136 kg) + all other phases of flight: 800 Ibs (363 kg) Fuel remaining In a tank when the appropriate fuel quantity Indicator reads zero is not usable. Fuel quantities are based on 6.75 Ibs per U.S. gal and 2.2046 lbs per kg conversion factors, ‘The maximum usable fuel load for each fuel tank is given below. iz Pressure Refueling Gravity Refueling Left wing tank 7,492 lbs 7,290 lbs Right wing tank 7,492 Ibs 7,290 ios Ha | Center tank 4,610 Ibs - Total _ 19,594 Ibs 14,580 lbs ‘Takeoff with a fuel load in excess of 500 Ibs in the center tank is not permitted unless: ‘+ each main wing tank is above 4,400 Ibs, ot + iffeach main wing tank is fess than 4,400 lbs consult the Aircraft Flight Manual’s Limitations section for additional requirements ‘The minimum fuel quantity for go-around is 600 Ibs per wing tank (with the airplane level) and assuming a maximum airplane climb altitude of 10° nose up. Rev: 18 - Section; 3 Eff: 09/24/09 GoJet ae AT RETR ES eeeCRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-15.3 Fuel Temperature Takeoff with engine fuel temperature indications below 5°C (41°F) Is prohibited. Takeoff with bulk fuel temperature indications below the limits stated is prohibited During fight, bulk fuel temperature must remain above the applicable bulk fue! freezing point, 1. Russian/CIS RT fuel ‘Fuel Type Bulk Fuel Takeoff Limit | Bulk Fuel Freezing Point cf Minimum Temperature i ASTM D 1655 (JET A) "30°C | -40°C ASTMD 1655GET AI) | 37°C “PC MIL DTL-5624 (0P-5) 36 °C MIL DTL-83133 (3P-8) are “47°C GB6537-94No.3Jet_ | 37C ae “47°C cis RT 40°C | See NOTE NOTE ith 2 freezing point of not higher than -50°C are approved for use wherein the ground level OAT is not below ~30°C duting the 24 hours before departure. 2, Russian/CIs fuel with a freezing pointy of not higher than -55°C (RT) for use in low temperature fegions are available at the operator's request. 3-15.4 Fuel Grades * For approved grades ar ind mixing of fuels consult the Airplane Flight Manual See also GOM 2-4.4, Fuel Specifications, Rew: 18 Eff: 09/24/09 ie tion: 3 GoJet Pea! ‘CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS, Procedures Manual 3-15.5 Fuel Additives Fuel System Icing Inhibitors (FSII) Fluid 1 or Fluid 1-M should not be used continuously. For approved additives and their concentrations, consult the Aircraft Flight Manual’s Limitations section. For approved biocide additives and their concentration, consult the Aircraft Flight Manual’s Limitations section, For approved anti-static additive and its concentration, consult the Aircraft Flight Manual’s Limitations section. For approved fuel conductivity additive and its concentration, consult the Aircraft Flight ‘Manual’s Limitations section, For approved corrosion inhibitors and their concentr: Limitations section. , consult the Aircraft Flight Manual’s Powered crossflow and gravity crossflow must be OFF for takeoff. Rev. Ef 5 é section: 3 06/02/08 GoJet Page: 14CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-16 OL 3-161. Oil Consumption faximum oll consumption on each engine is 189 cubic centiliters per hour (6.4 U.S. ounces per hour/0.05 U.S. galtons per hour). 3-16.2 Oil Grades Note: Mixing of different types of oils is prohibited. | COMPONENT erYeE ME yee CASTROL 4000 Engines wie v yo Air Turbine Starter v cui ae | integrated Drive Generator v | v v Auxiliary Power Unit anny eae va ‘| 3-16.3 Engine Oil Level Engine ofl levels must be checked as follows: + the maximum duration without engine oil servicing is 36 operating hours * for airplane operations in excess of 36 operating hours (without engine oil tank servicing), the ‘engine oll level must be checked within 3 minutes to 2 hours after every engine shutdown 3-16.5 Oil Replenishment System If use of the oil replenishment system is requited, then the engine(s) should be replenished within 15 minutes to 2 hours after engine shutdown, Maximum refill allowable is 2 U.S. quarts without dry-motoring the engine. If the oi system has to be replenished to maximum capacity and the replenishment period has been exceeded, the engine(s) must be dry- motored, Note: Mixing of different types of oils is prohibited, Rev: 15 Eft: 06/02/08 Section: Page:i i i | | | CRY 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-17 AUXILIARY POWER UNIT Allied Signal RE 220 (RJ) 3-17.14 Starting Minimum ambient temperature for starting a cold-soaked APU on the ground is -40°C (-40°F). Maximum EGT (dependant upon altitude and temperature) * 0 to 100 % RPM 692°C to 1038°C The APU starter motor duty cycle is timited to not more than 3 starts/start attempts in 1 hour. Note: A two minute delay must be observed between cranking attempts to allow for cooling of starter and starter contactor and APU fuel drainage. 317.3 Operating Range Maximum RPM: 106% ‘Maximum EGT: 1038°C (do not exceed under any operating condition). APU starting and operation is permitted within the following operating envelope: ‘+ Start and operating limits refer to 3-17.13, + Altitude and airspeed refer to 3-17.14 3-17.5 APU Bleed Aj ‘APU Bleed Air Limitations System/Condition Limitation Bleed air extraction | APU bleed air extraction is not permitted above 25,000 feet. Engine start during ground operations | No bleed air extraction limitation. Each engine may be started using the APU as a bleed air source. Rey. eft. 15, * Section: 3 2602/08 Gowet rs Page:CRI 700 Standard Operating LIMITATIONS & MEMORY ITEMS ' Procedures Manual 3-17.7 APU Generator ‘The maximum permissible load on the APU generator is 40 kVA. 3-17.9 APU Indications The APU limit display markings on the EICAS must be used to determine compliance with the maximum timit and precautionary ranges. If EICAS markings show more conservative limits than those specified betow, the limit markings on the EICAS should be used, Note: Red - Maximum Limitations Green - Normal Operating Range E ~ Indication Red Green APU EGT "Cc 807 0 t0 806 APU RPM % 107 Oto 106 5 ae Section: 3 06/02/08 GoJte Pages 17CRJ 700 Standard Operating "ATIONS & MEMORY ITEMS Procedures Manual sie on 3-17.13 APU Start and Operating Limits Enyelope PB. EEPEEEEGE Rev: 15 Eff: 06/02/08CRJ 700 Standard Operating TONS. ORY ITEM: Procedures Manual ae ‘in s 3-18 MAXIMUM OPERATING SPEED AND MACH NUMBER: ‘Maximum operating limit speeds must not be deliberately exceeded in any regime of flight unless a higher speed is specifically authorized for flight test or training operations. The Maximum cruise Mach number during flight in RVSM airspace is 0.83. ° 250 260 270 280 290 300 310 ae0 390 340 350 90 Indicated Airspeed (KIAS) 5 ee Section: 3. 05/02/08 Godte Page: 19CRJ 700 Standard Operating Procedures Manual LIMITATIONS & MEMORY ITEMS 3-19 DESIGN MANEUVERING SPEED Full application of rudder and aileron controls, as well as maneuvers that involve angles-of-attack near the stall, must be confined to speeds below VA. Values of VA are given in the following figure for varying pressure altitudes and aircraft weights. 310 300 290 200 260 8 g 220 210 DESIGN MANEUVRING SPEED (KiAS) & 200: 190 180 170 160 150 los 40 42 44 46 48 50 2 54 56 58 60 62 64 G6 G8 70 72 74 76 78 AIRCRAFT WEIGHT (1000 UB) auTiOn Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, rolt, or yaw (.g., large side slip angles) as they may cause structural failure at any speed, including below Vs. 5 Section: 3 06/02/68 GoJet 0CRJ 700 Standard Operating LIMITATIONS & MEMORY, ITEMS Procedures Manual 3-20 FLAPS EXTENDED SPEEDS ‘The maximum speeds at which the flaps may be extended are: Flap Position Vee | ____ Flaps 1 "230 KIAS : Flaps @ B30 KIA Flaps20 230 KIAS - ~ Flaps 30 185 KIAS Flaps 45 tT KIAS 3-21 MAXIMUM LANDING GEAR OPERATING SPEEDS Gear Position ‘Maximum Operating Speed | _Extension 220 KIS _____ Down and Locked RO KIAS Retractio ae 200 KIAS 3-22. TIRE LIMIT SPEED Maximum tire limit speed is 182 knots (210 mph) ground speed. 3-23 MAXIMUM AIRSPEED FOR ADG OPERATION The maximum speed for ADG operation is VMO/MMO. 3-24 TURBULENCE PENETRATION SPEED ‘Maximum airspeed for turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower. 3-25 MINIMUM OPERATING SPEED LIMIT. Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited unless a lower speed Is specifically authorized for flight test or training operations. Rev. 15, i Section: 3 Fee 6/02/08 Godet PoresCRJ 700 Standard Operating LIMITATIONS && MEMORY ITEMS. Procedures Manual 3-26 WINDSHIELD WIPER OPERATION | The windshield wiper must not be operated above 250 KIAS. if the windshield wiper has failed in a non-parked position, the airplane speed must not exceed 250 KIAS. 3-27 MANEUVERING LIMIT LOAD FACTORS Phase of Operation ‘Maximum “G” Loading Flaps Retracted 1.0 t02.56 Flaps Extended 0.0 to 2.06 Avoid unnecessary and large side-slip maneuvers during low speed high altitude cruise. 3-28 AIR-CONDITIONING AND PRESSURIZATION The maximutn relief differential pressure is 8.7 psi. The maximum negative differential pressure is -0.5 psi. During taxi, takeoff and landing, the pressure differential must not exceed 0.1 psi. The airplane must be completely depressurized prior to opening any of the airplane doors. To preclude possible crew and/or passenger ear damage, use of the EMERG DEPRESS switch above 15,000 feet is prohibited. 3-28.1 Single Pack Operation ‘The maximum altitude for single pack operation is 31,000 feet. 7 sexton 3 Sorenr08 GoJset tehSOP — CRI 700 Standard Operating Procedures Manual LIMITATIONS & MEMORY ITEMS 3-28.3 ximum Flight Duration at Altitude Due to Cabit tio 14CFR 25.832(a)(2) ‘The maximum allowable flight duration at altitude in accordance with 14CFR 25.832 (a)(2) is presented in the QRH Volume 1, Planning tab. The charts referenced in the QRH separate conditfons for Eastem and Western North America. For all operations above FL350, two checks are required to determine the cabin ozone concentration flight profile limitation. The first check is the Eastern, or Western North America Maximum Altitude chart, This chart must be referenced to determine the maximum altitude during a specific month, at a specific latitude. It is permitted to interpolate linearly between months, latitudes, or altitudes. “The second check is for maximum duration (hours) during a specific month, at a specific latitude and longitude. Longitude line 100 degrees West is the dividing line between Eastern and Western North America. In a scenario where a flight will be traversing the 100 degree West longitude axis, a modification of the maximum flight duration will be required. Consideration between the time spent on both sides of the axis must be taken for any flight crossing the 100 degree West axis, Below is an example: Ex, KORD-KBOI, FL 350 in March, ETE 3hom Origin Lat/Long: N41 583.9 WO87 54.4 Destination Lat/Long: N43 33.9 W116 13.5 Max duration Eastern North America (East of Long 100 West): 3,20 Hours Max duration Western North America (West of Long 100 West): 6.00 Hours KORD-100 degree West Long ETE: 1h20m (1/3 ETE) 100 degree West-KORD: 2h40min (2/3 ETE) YS of 3.20n = 1.06h 2/3 of 6.00h = 2.00h Together = = 3.06h Total allowable time at FL350 = 3,06h 30 ce Section: 3 ogisyiz Gaote Page: 23 TeteSOP — CRJ 700 Standard Operating Procedures Manual eee even atene 3-29 AUTOMATIC FLIGHT CONTROL SYSTEM. The following table identifies the approved CRJ700 autopilot minimum use heights as a function of flight phase and glidepath (glidestope) angle. ‘Airport Elevation ‘Minimum Use Final Phe Glide te i zee asa jepath Angle |= 4,000 feet > 4,000 feet Height |___ Takeoff - - a 600 feet AGL__| Non-Precision ~ 1 “Approach : Approved Approved 400 feet AGL Precision $3.5° Approved Approved 80 feet AGL ‘Approach > 3.5", < 4.0" Approved Prohibited 120 feet AGL ‘+ The ADC Source coupled to the active autopilot must be the same as that coupled to the ATC Transponder during flight in RVSM airspace. 3-30 ELECTRICAL SYSTEMS 3-301 ible AC Electrical m Loads Individual AC generator loading must not exceed the following values: Altitude Load Limitation ‘Main Generator (each) ‘APU Generator 0 to 41,000 feet 40 kVA “40 kVA 3-30.3 Permissible DC Electrical System Loads In-flight: * maximum permissible continuous load on each TRU is 120 amps Ground Operation: ‘+ to protect the CRT displays, the maximum permissible time for ground operations with DC power is 5 minutes, 3-305 Circuit Breaker Reset (In Flight) A circuit breaker must not be reset or cycled (i.e., opened or closed) untess doing so is consistent with explicit procedures specified in the Airplane Flight Manual or unless, in the judgment of the Pilot in ‘Command, that resetting or cycling of the circuit breaker is necessary for the safe completion of the flight. Section: 3 Page: 24CRJ 700 Standard Operating pigeuadras Mental LIMITATIONS & MEMORY ITEMS 3-31 FLIGHT CONTROLS - LIFT/DRAG DEVICES 3:31.14 Slats/Flaps Enroute use of Slats/Flaps is prohibited. Flight with Slats/Flaps extended at altitudes above 15,000 feet is prohibited. 3-31.3 Flight Spoilers Flight spoilers must not be extended in-flight below an altitude of 300 feet AGL. To ensure adequate maneuver margins, flight spoilers must not be extended in-flight airspeeds below the recommended approach speed plus 10 KIAS. 3-31.53. Stall Protection Both stall protection system switches must remain on for all phases of flight. 3-32 THRUST REVERSERS. Thrust reversers are approved for ground use only, activation of the reverse thrust levers fs prohibited in-flight. The thrust reversers are intended for use during full stop landings. Do not attempt a go-around maneuver after deployment of the thrust reversers. ‘Takeoff with any thrust reverser icons or EICAS warning and/or caution messages displayed is prohibited, The allowable use of thrust reversers during landing is defined in the Figure below. Backing-up using thrust reversers is prohibited. Backing-up.using thrust reversers is prohibited, TOUCHDOWN SPEED Section: 3 Page: 25CRJ 700 Standard Operating Cpseaaiess Manat LIMITATIONS & MEMORY ITEMS 3-33 TAXI LIGHTS: The taxi lights must be switched OFF whenever the airplane is stationary in excess of 10 minutes. 3-34 WHEEL BRAKE COOLING LIMITATIONS Brake cooling times must be observed between a landing or rejected takeoff (RTO) and a subsequent takeoff to ensure that sufficient brake energy is available to bring the airplane to @ complete stop, if the subsequent takeoff is rejected. (refer to QRH Volume 1) 3-35 MISCELLANEOUS LIMITATIONS. 3-35.1 Nose Wheel Steering System ‘Towbarless towing is prohibited, unless the operation is performed in compliance with the Airplane Maintenance Manual towbariess towing requirements. 3-35.3 Minimum Descent Altitude When setting the MDA marker on the barometric altimeter using the DH/MDA knob on the altitude reference panel, the next highest 10-foot increment must be selected if the altitude Is not at a 10-foot increment. 3-355 Traffic Alert and Collision Avoidance System (TCAS) Pilots are authorized to deviate from their Air Traffic Control (ATC) clearance In order to comply with a TCAS resolution advisory (RA) command. 6.5. Pilots shall notify Dispatch after compliance with a TCAS RA, as defined in GOM 1. 3-35.7 Configuration Deviation List If the aircraft is to be operated with certain secondary airframe and/or any nacelle parts missing, ‘operation must be in accordance with the limitations specified In the basic Airplane Flight Manual, and as amended by the Configuration Deviation List. Section: 3 Page: 26 Rev.: 24 Eff: 05/12/10CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-36 AVIONICS 3-36.1 Integrated Standby Instrument (1ST) When NAV 1 Is tuned to a valid ILS frequency, the ISI will display localizer and glidestope deviation while ‘on the backcourse approach. Use of the IST localizer and backcourse Information is prohibited during backcourse approaches. 3-36.3 Enhanced Ground Proximity Warning System (EGPWS) ‘* Airplane navigation must not be predicated upon the use of the terrain display. * To avold giving unwanted alerts, the terrain awareness alerting and display functions must be inhibited on takeoff, approach or fanding within 15 nm of an airport not contained in the EGPWS elrport database, The terrain database, terrain displays and alerting system do not account for man-made obstructions, except for all known man-made obstructions in Canada, the United States and Mexico, ‘+ If GPS Is Inoperative (Identified by NO GPS RAIM, GPS NOT AVAILABLE or GPS-FMS DISAGREE message on the FMS CDU) «The terrain awareness alerting and display functions must be Inhibited during QFE (atmospheric pressure at alrport elevation) operations [cauTzo1 ‘The EGPWS may fall to alert when a terrain threat exists, during ambient surface temperatures below ISA, during non-standard temperature fapse rates or if incorrect barometric settings are set on the altimeter, ‘ens section: 3 fee Broa GoJet fae 7‘CRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-36.5 Alrcra ‘The ACARS is approved for the transmission and receipt of messages that will not create an unsafe condition if the message is improperly received. An unsafe condition may exist + The message or part of the message Is delayed or not received, + The message is delivered to the wrong recipient, or ‘+ The message content is corrupted. Crew actions based on messages such as pre-departure clearance, digital automatic terminal information service, Weight and balance, take-off data (speeds, trim settings, runway distances), are prohibited, unless approved operational procedures are used to verify that the message is received by the Intended recipient, that the message is valid and that the content is not corrupted, pry FH Section: 3 06/02/11 GoJet ue STR ee reeSOP — CRJ 700 Standard Operating Procedures Manual rastrtia Vi ech trtleeaettccd 3-36.7 Flight Management System (FMS) 3-36.71 Operating Data +The Flight Management System (FMS) must be operated in accordance with the latest edition of the following: Airplane Flight Manual, and + Flight Management System Pilot Guide: consult the Aircraft Flight Manual for the Guide's Publication Number. 3-36.7.3 _ EMS-4200 Operating Limitations For the approved Software Program Version, consult the Aircraft Flight Manual. ‘The FMS meets the enroute, terminal, and non-precision approach lateral performance/accuracy criteria of ‘AC20-130A, When equipped with an operating FMS and GPS the aircraft meets the functional and the -+1 nm accuracy requirements of AC 90-1004, US Terminal and Enroute Area Navigation (RNAV) Operations, ‘+ AC 90-100A operations must not be conducted with any of the following messages displayed: + NO GPS RAIM ‘+ GPS NOT AVAILABLE GPS DISABLED ‘+ GPS-FMS DISAGREE © FMS-FMS DISAGREE Refer to 2-18.9 GPS-FMS (CDU/PFD) Messages for descriptions, ‘+ The GPS availability and integrity (RAIM) is confirmed for the intended flight (route and time), using an appropriate RAIM availability prediction program, Refer to 1-11 for RAIM Prediction Note: Compliance with the standard noted above does not constitute an operational approval. For approved PRNAV Operations conducted in designated European airspace, consult the Aircraft Flight Manual. keys Section: 3 Bee Gevouts Govet Poe: 29SOP — CRJ 700 Standard Operating Procedures Manual LIMITATIONS & MEMORY ITEMS Precision RNAV operations must not be conducted unless: 1. Allof the required equipment specified below is operational. PRNAV REQUIRED EQUIPMENT LIST ______ EQUIPMENT REQUIREMENTS FOR PRNAV Flight management computer (1 or 2 as installed) | One must be operational FMS control display unit (1 or 2 as installed) (One must be operational VHF NAV, DME, GPS (One VHF NAV and one DME, or one GPS must be operational 2. The following messages are not displayed on any PFD or CDU: + FMSDR + IRSONLY VOR/DME ONLY or V/D ONLY + VOR/DME DIST >40. NM 3. For procedures that specifically require GPS, or when GPS is the only available sensor, none of the following messages are posted on the CDU: ‘© GPS NOT AVAILABLE © GPS-FMS DISAGREE ILS, LOC, LDA, SDF and MLS approaches using the FMS are prohibited. The FMS does not provide automatic transition to the ILS. ‘The FMS is approved for use only during enroute, terminal and non-precision approach phases of flight. FMS range, fuel management, and altitude/speed capability information is advisory only. IFR enroute and terminal navigation is prohibited unless the plot verifles the currency of the database and verifies waypoints for accuracy by reference to current publications. Instrument approaches must be accomplished with instrument approach procedures that are retrieved from the FMS database. The FMS must incorporate the current update cycle, The pilot must verify approach waypoints for accuracy by reference to current publications. ‘The approach must not be continued past the final approach fix if an FMS "NO APPR” message Is displayed on the PFD. ‘The VNAV system information is not temperature compensated. FMS generated altitudes and V- paths are not corrected for non-ISA conditions. Operations with a VNAV final approach glidepath angle that exceeds 4.0 degrees are prohibited, 29 Z os/toyi2 GoJetCRJ 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-36.9 Multifunction Displays Flickers may ocour on the MFD with a large number of FMS symbols selected, To manually declutter the MFD: + Reduce range selected + Deselect TCAS overlay + Deselect radar/terrain overlay + Deselect some of the FMS symbology 3-37 GLOBAL POSITIONING SYSTEM 3-37.1 General Other approved navigation equipment appropriate to the route of flight (enroute and terminal) must be installed and operating. When an altemate alrport Is required by applicable operating rules, the following concitions apaly: + the alternate aerodrome must be served by an approach based on other than GPS navigation + the airplane must have operational equipment capable of using that navigation ald, and + the required navigation ald must be operational The area navigation system used for IFR Class 1 navigation meets the performance/accuracy criteria of AC 20-1304 for enroute, terminal area navigation and non-precision approach operaticns (Including "GPS" and “RNAV” approaches). 3-37.3 RNP-10 Operations ‘The duel GPS installation, when used In conjunction with the Prediction Program 832-3443-005 and with two operational FMS-4200 systems, has been found to comply with the requlrements of MNPS operations and as a primary means of navigation in oceanic and remote airspace operations. Likewise, this compliance is considered as meeting RNP-10 requirements, without time limitations. Note: The demonstration of performance with the above criterla does not constitute approval to conduct MNPS, oceanic/remote alrspace or RNP-10 operations, uw Govet Sect: 3 osroarta Page:| | CR 700 Standard Operating LIMITATIONS & MEMORY ITEMS Procedures Manual 3-38 MEMORY ITEMS 3-38.1 Immediate Action Checklist This section contains the Immediate Action Checklist. for general reference and training purposes. Two copies of this Checklist are to be carried onboard Golet aircraft at all times. One checklist should be immediately accessible to each pilot while on duty In the flight deck. Normally one copy will be stowed in the side pocket adjacent to each seat. These Immediate Action Items in no way supersede current procedures In the Quick Reference Handbook or the approved Alrplane Flight Manual and any revisions thereto. In case of conflict, the Airplane Flight ‘Manual takes precedence. Items surrounded by a dashed box are considered critical and are therefore considered memory items. ‘These boxed Items are to be performed from memory prior to pulling out the Immediate Action Checklist. Upon completing an Immediate Action Checklist section, proceed to the QRH page indicated for adcitional procedures. If, In the additional procedures, you are guided to another QRH Checklist, that checkist may be completed using the QRH. It is not necessary to retum to the Immediate Action Checklist unless there is a situation not related to the original message or event, Rev.: 24 zs Section: 3 ere O6ns44 Godet Page: 32