Editing Airbus A300 (section)

=== A300B4 ===
[[File:Continental Airlines Airbus A300 Durand.jpg|thumb|The A300B4-100 first took flight on 26 December 1974, kept the B2 length but featured a higher fuel capacity]]

==== A300B4-100 ====
The initial A300B4 variant, later named the A300B4-100, included a centre fuel tank for an increased fuel capacity of {{convert|47.5|t|lb}}, and had an increased MTOW of {{convert|157.5|t|lb|}}.<ref>{{cite magazine|last=Sweetman|first=Bill|title=Airbus Industrie spreads its wings|magazine=[[Flight International]]|date=4 September 1975|volume=108|issue=3469|pages=326|url=https://www.flightglobal.com/pdfarchive/view/1975/1975%20-%201721.html}}</ref><ref name="Gunston" />{{rp|38}} It also featured Krueger flaps and had a similar high-lift system to what was later fitted to the A300B2-200.<ref name="Gunston" />{{rp|74}} The variant made its maiden flight on 26 December 1974, was certified on 26 March 1975, and entered service with [[Bavaria Germanair]] in December 1975.<ref name="Endres99" />{{rp|32, 54}}<ref name="tcdsv3" />{{rp|16}}

==== A300B4-200 ====
The A300B4-200 had an increased MTOW of {{convert|165|t|lb}} and featured an additional optional fuel tank in the rear cargo hold, which would reduce the cargo capacity by two LD3 containers.<ref name="tcdsv3" />{{rp|19}}<ref name="Gunston" />{{rp|69}} The variant was certified on 26 April 1979.<ref name="tcdsv3" />{{rp|19}}

{| class="wikitable sortable"
! Variant
! Produced{{ref label|B4_produced|A|A}}
|-
| B4-100
| 47
|-
| B4-200
| 136
|-
! colspan=|Source:<ref name="Endres99" />{{rp|110}}
|}
{|
|{{note label|B4_produced|A|A}} Production figures are listed up to 1 January 1999.<ref name="Endres99" />{{rp|110}}
|-
|}

===== A300B4-200FFCC =====
It is the A300B4-200 without the flight engineer but analog flight instruments. Introduced by Garuda Indonesian Airways in 1982