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701/900 Aircraft Limitations – POH Chapter 3 (2026) – 214 Exam Questions – Weights, Speeds, Fuel & RVSM – Regional Jet Training

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This document contains 214 structured exam questions and answers covering Aircraft Limitations from POH Chapter 3 for the 701 and 900 series aircraft. It comprehensively reviews performance limitations, operating weights, airspeed limits (VFE, gear speeds, turbulence penetration), wind limitations, CAT II restrictions, braking action limits, RVSM requirements, engine operating limits, APU limitations, fuel system restrictions, anti-ice procedures, autopilot limitations, thrust reverser limitations, and emergency procedure memory items. The material is directly aligned with the Aircraft Pilot Operating Handbook (POH) Chapter 3 – Limitations, the Quick Reference Handbook (QRH), and associated Flight Operations Manual (FOM) procedures. It reflects operational standards for transport-category regional jets and emphasizes regulatory compliance, operational safety margins, and aircraft system limitations required for airline operations and recurrent training. This study guide is particularly suitable for: Airline First Officers (FO) and Captains operating 701/900 series aircraft Type rating candidates Initial and recurrent training students ATP candidates transitioning to regional jets Simulator checkride preparation Airline ground school students Aviation university transport-category jet students It is relevant for courses such as: Aircraft Systems and Limitations Transport Category Jet Performance Airline Ground School Regional Jet Type Rating Training Advanced Turbine Aircraft Operations RVSM Operations and Compliance Training The question-and-answer format makes this resource ideal for oral exam preparation, recurrent evaluations, simulator check preparation, upgrade training, and systems review. It includes detailed numeric limitations such as crosswind components, runway condition codes, differential pressures, weight limits, altitude limits, fuel imbalance tolerances, oil pressure limits, starter cycle limits, engine relight envelopes, braking limitations, and autopilot minimum engagement altitudes. Keywords: 701 Aircraft Limitations, 900 Aircraft Limitations, POH Chapter 3, Aircraft Limitations Study Guide, Regional Jet Limitations, Maximum Takeoff Weight, Maximum Landing Weight, VFE Speeds, Gear Extension Speed, Turbulence Penetration Speed, RVSM Requirements, Engine Operating Limits, APU Limitations, Fuel System Limitations, Anti-Ice Procedures, CAT II Restrictions, Crosswind Limits, Braking Action Codes, Autopilot Minimums, Thrust Reverser Limitations, Airline Ground School

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Aircraft Limitations POH
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Aircraft Limitations POH

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701 900 Aircraft Limitations
POH Chapter 3 2026 Exam
Questions and Answers | 100%
Solved



Maximum 90 degree crosswind for takeoff and landing - 🧠 ANSWER ✔✔27

knots

Maximum 90 degree crosswind for landing from a Category II Approach - 🧠

ANSWER ✔✔15 Knots

,Maximum headwind for landing from a Category II Approach - 🧠 ANSWER

✔✔16 Knots


Maximum direct tailwind for takeoff and landing (including Gusts) - 🧠

ANSWER ✔✔10 Knots


Minimum Runway Width - 🧠 ANSWER ✔✔100 ft


Maximum operating altitude <-701>, <-900> - 🧠 ANSWER ✔✔41,000 ft.


Max pressure altitude for takeoff and landing - 🧠 ANSWER ✔✔8,000 ft


Maximum ambient temperature for takeoff and landing - 🧠 ANSWER

✔✔ISA +35°C Limited to OAT of +51°C


Minimum ambient temperature approved for takeoff - 🧠 ANSWER ✔✔-40°C


Max peak wind value - 🧠 ANSWER ✔✔50 Kts


Flaps Retracted Load Limit Factors - 🧠 ANSWER ✔✔-1.0 to +2.5 G


Flaps Extended Load Limit Factors - 🧠 ANSWER ✔✔0.0 to +2.0 G


Maximum positive differential pressure - 🧠 ANSWER ✔✔8.7 psi


Maximum negative differential pressure - 🧠 ANSWER ✔✔-0.5 psi

, Maximum Pressure differential during ground maneuvering - 🧠 ANSWER

✔✔0.1 psi


Maximum Pressure differential during landing - 🧠 ANSWER ✔✔1.0 psi


Max altitude for single pack operation - 🧠 ANSWER ✔✔31,000


The use of the EMERG DEPRESS switch above _______ is prohibited - 🧠

ANSWER ✔✔15,000 ft


Maximum Taxi and Ramp Weight <701> - 🧠 ANSWER ✔✔75,250 lbs


Maximum Taxi and Ramp Weight <900> - 🧠 ANSWER ✔✔85,000 lbs


Maximum Takeoff Weight <701> - 🧠 ANSWER ✔✔75,000 lbs


Maximum Takeoff Weight <900> - 🧠 ANSWER ✔✔84,500 lbs


Maximum Landing Weight <701> - 🧠 ANSWER ✔✔67,000 lbs


Maximum Landing Weight <900> - 🧠 ANSWER ✔✔75,100 lbs


Maximum Zero Fuel Weight <701> - 🧠 ANSWER ✔✔62,300 lbs


Maximum Zero Fuel Weight <900> - 🧠 ANSWER ✔✔70,750 lbs




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