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Maximum takeoff weight and McDonnell Douglas F-4 Phantom II

Shortcuts: Differences, Similarities, Jaccard Similarity Coefficient, References.

Difference between Maximum takeoff weight and McDonnell Douglas F-4 Phantom II

Maximum takeoff weight vs. McDonnell Douglas F-4 Phantom II

The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits. The McDonnell Douglas F-4 Phantom II is a tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber originally developed for the United States Navy by McDonnell Aircraft.

Similarities between Maximum takeoff weight and McDonnell Douglas F-4 Phantom II

Maximum takeoff weight and McDonnell Douglas F-4 Phantom II have 0 things in common (in Unionpedia).

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Maximum takeoff weight and McDonnell Douglas F-4 Phantom II Comparison

Maximum takeoff weight has 13 relations, while McDonnell Douglas F-4 Phantom II has 286. As they have in common 0, the Jaccard index is 0.00% = 0 / (13 + 286).

References

This article shows the relationship between Maximum takeoff weight and McDonnell Douglas F-4 Phantom II. To access each article from which the information was extracted, please visit:

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