Douglas DC-9-30

Douglas · United States · first flew 1965 · airliner

The DC-9-30 is the first major stretch of the DC-9 family, extending the fuselage by 4.5m over the -10 series to seat up to 115 passengers, and became the most-produced variant of the original DC-9.

Recognition (WEFT)

W — WingsLow-mounted, swept
E — Engines2 × turbofan, tail-mounted
F — FuselageFuselage stretched to 36.4m by a 4.5m plug over the DC-9-10 (31.8m), making it the first significantly stretched DC-9 and the baseline for all subsequent variants
T — TailT-tail

WEFT is AircraftIQ's four-point recognition method — how it works.

Spot it by:

Longer fuselage than DC-9-10 (36.4m vs 31.8m); shorter than DC-9-50 (40.7m); all DC-9 variants share the distinctive T-tail and rear-engine arrangement; the -30 has a more balanced fuselage proportion than the compact -10.

Specifications

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

The DC-9-30 first flew in August 1965 and entered service with Eastern Air Lines in 1966. Douglas achieved the stretch rapidly by adding plugs fore and aft of the wing, simultaneously extending the wing span and adding leading-edge slats for improved performance. Over 620 were built, cementing the DC-9's commercial success.

Variants

Several sub-series existed including the -31, -32, -33 and -34, differing in fuel capacity and weight; the -30 series formed the structural basis for the later DC-9-40 and -50 as well.

Where you'll see it

Operated by virtually every US trunk airline; later examples flew with regional carriers and cargo operators; many were inherited by Northwest Airlines and eventually absorbed into the Delta fleet.

Related aircraft

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