TECHNICAL INFORMATION: ALL VARIANTS

‘STANDARD’ DC-8 SERIES 11-55

There was a great amount of evolution from the initial DC-8 Series 11 to the final Standard DC-8 Series 55. This was due to a combination of technological improvements that became available in the early 1960s plus Douglas’ efforts to meet the varied requirements of the world’s airlines. Most of these improvements are noted in the Remarks section of each Model Number.

Nearly all of the Standard DC-8s have been retired due to increasingly stringent noise standards throughout the world. However, there are still some DC-8F-54 and -55 Freighter Aircraft still flying due to special “hush kits” being installed on their engines which has reduced the noise they emit to right levels – in some parts of the world -primarily Africa and South America.

DELENGINEDIMENSIONSTYPICALCARGODATETOTALREMARKS
#MAKER, TYPE, & MODEL(FT) L=LENGTH W/S=WINGSPANPASSENGER CONFIGURATIONSCAPACITY IN CUBIC FEET (BELOW CABIN IN CARGO BINS UNLESS OTHERWISE NOTED)CERTIFIED BY FAA#
#,ALL FIRST (F)MADE
THRUST IN LBS.MIXED F/Y
ALL COACH (Y) - MAXIMUM Y* &
MW=MAXIMUMCARGO PALLETS** (IF APPLICABLE)
WEIGHTS (LBS) TAKEOFF/LANDING
11PWL=11613902179324INITIAL
DOMESTIC VERSIONTURBO-JET150.7ALL FVERSION; ENGINES WERE TURBOJET WITH WATER INJECTION
JT3C-6W/S= 139.7132 MIXED F/Y
13,500 LBS.MW=265,000/190,500144 - 179 ALL Y
12PWL=1161390220985ADDED EXTENDED WING TIP & LEADING EDGE SLOTS ENGINES WERE TURBOJET
DOMESTIC VERSIONTURBO-JET150.7ALL FWITH WATER INJECTION
JT3C-6W/S= 142.36132 MIXED F/Y
13,500 LBS.MW=273,000/193,000144 - 179 ALL Y
21PWL=11613902193434ENGINES
DOMESTIC VERSIONTURBO-JET150.7ALL FWERE NO LONGER WATER INJECTION FROM THIS VERSION FORWARD. EXTENDED
JT4A-3/-5W/S= 142.36132 MIXED F/YWING TIP & LEADING EDGE SLOTS WERE ADDED FROM THIS VERSION FORWARD.
15,800 LBS.MW=276,000/193,000144 - 179 ALL Y
-Or-
JT4A-9/-10 16.800 LBS.
-Or-
JT4A-11/-12 17,500 LBS.
31PWL=1161390220054FIRST
INTERCONTINENTAL VERSIONTURBO-JET JT4A-9/-10 16.800150.7ALL FINTERNATIONAL VERSION WITH LONGER RANGE
LBS.W/S=142.36132 MIXED F/Y
MW=300,000/196,500144 - 179 ALL Y
32PW TURBO-JET JT4A-9/-10 16.800L=11613902194743--
INTERCONTINENTAL VERSIONLBS.150.7ALL F
-or-JT4A-11/-12 17,500 LBS.W/S= 142.36132 MIXED F/Y
MW=310,000/199,500144 - 179 ALL Y
33PWL=11613902224810ADDED
INTERCONTINENTAL VERSIONTURBO-JET150.7ALL FFLAP MODIFICATION & LANDING GEAR STRENGTHENED
JT4A-11/-12 17,500 LBS.W/S= 142.36132 MIXED F/Y
MW=315,000/207,000144 - 179 ALL Y
41RRL=1161390219994SAME
INTERCONTINENTAL VERSIONLOW BYPASS FAN RCo.12150.7ALL FINTERNATIONAL VERSIONS AS THE SERIES 30s BUT WITH ROLLS-ROYCE CONWAY
17,500 LBS.W/S= 142.36132 MIXED F/Y(LOW) BYPASS ENGINES
MW=300,000/196,500144 - 179 ALL Y
42RRL=1161390220328THE
INTERCONTINENTAL VERSIONLOW BYPASS FAN RCo.12150.7ALL FROLLS-ROYCE CONWAY (LOW) BYPASS ENGINE WAS AN EARLY VERSION OF THE FANJET
17,500 LBS.W/S= 142.36132 MIXED F/Y
MW=310,000/199,500144 - 179 ALL Y
43RRL=11613902231320ADDED
INTERCONTINENTAL VERSIONLOW BYPASS FAN RCo.12150.7ALL F4% WING LEADING EDGE EXTENSION & LANDING GEAR STRENGTHENED
17,500 LBS.W/S= 142.36132 MIXED F/Y
MW=315,000/207,000144 - 179 ALL Y
51PWL=13213902256430FIRST
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-1/3 17,000/18,000150.7MIXED F/YTURBOFAN ENGINE VERSION
LBS.W/S= 142.36144 - 179 ALL Y
MW=276,000/199,500
52PWL=13213902240225ADDED
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-3B150.7MIXED F/Y4% WING LEADING EDGE EXTENSION & LANDING GEAR STRENGTHENED
18,000 LBS.W/S= 142.36144 - 179 ALL Y
MW=300,000/202,000 -or- 305,000/202,000
53PWL=13213902239923ADDED
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-3B150.7MIXED F/Y4% WING LEADING EDGE EXTENSION & LANDING GEAR STRENGTHENED
18,000 LBS.W/S= 142.36144 - 179 ALL Y
MW=315,000/207,000
53ABPWL=1321390223992DOUGLAS
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-3B150.7MIXED F/YDESIGNATED AS 'AB' FOR AFT BULKHEAD EXTENSION INCREASING PASSENGER CAPACITY
18,000 LBS.W/S= 142.36155 - 189 ALL YTO MAX. 189
MW=315,000/207,000
54JT/54CFPWL=13288102304015DOUGLAS
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-3B150.7MIXED F/YCABINDESIGNATED AS 'JT' FOR JET TRADER, LATER KNOWN AS 'CF' FOR COMBINATION
18,000 LBS.W/S= 142.36155 - 189 ALL Y -or-1390 CARGO BINS=PASSENGER/FREIGHTER
MW=315,000/240,0008 PALLETS CARGO + 63Y PSGRS -or-TOTAL OF 10,200
13 PALLETS CARGO
54JT/54AFPWL=1388102304015DOUGLAS
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-3B150.7PALLETS -CABINDESIGNATED AS 'JT' FOR JET TRADER, LATER KNOWN AS 'AF' FOR AIR FREIGHTER
18,000 LBS.W/S= 142.36ALL CARGO1390 CARGO BINS=- UNITED AIRLINES ONLY ordered THIS VERSION.
MW=315,000/240,000TOTAL OF 10,200
55JT/55CFPWL=13288102354724FURTHER
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-3B150.7MIXED F/YCABINSTRENGTHENED LANDING GEAR. DOUGLAS DESIGNATED AS 'JT' FOR JET TRADER,
18,000 LBS.W/S= 142.36155 - 189 ALL Y -or-1390 CARGO BINS=LATER KNOWN AS 'CF' FOR COMBINATION PASSENGER/FREIGHTER. DOUGLAS DID
MW=325,000/240,0008 PALLETS CARGO + 63Y PSGRS -or-TOTAL OF 10,200NOT MAKE THIS VERSION AS AN ALL FREIGHTER (AF), BUT SOME 55JT/55F WERE
13 PALLETS CARGOLATER CONVERTED INTO 55AFs.
55ABPWL=1321390238572FURTHER
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-3B150.7MIXED F/YSTRENGTHENED LANDING GEAR. DOUGLAS DESIGNATED AS 'AB' FOR AFT BULKHEAD
18,000 LBS.W/S= 142.36155 - 189 ALL YEXTENSION INCREASING PASSENGER CAPACITY TO MAX. 189
MW=325,000/240,000
55LPWL=1321390238576FURTHER
DOMESTIC & INTERCONTINENTAL VERSIONSTURBOFAN JT3D-3B150.7MIXED F/YSTRENGTHENED LANDING GEAR. DOUGLAS DESIGNATED AS 'L' FOR LESS AFT BULKHEAD
18,000 LBS.W/S= 142.36144 - 179 ALL YWHICH LEFT THE AFT BULKHEAD PLACEMENT THE SAME AS IN SERIES 30 VERSIONS
MW=325,000/240,000AND THUS MAX. PASSENGER CAPACITY REMAINED AT 179 (PER AIRLINE REQUESTS).
TOTAL'STANDARD'DC-8SERIES11MADE:294
- 55L

NOTES:

PW= PRATT & WHITNEY TURBO-JET OR TURBO-FAN ENGINES; RR= ROLLS-ROYCE CONWAY LOW BYPASS FAN ENGINES

1111111 *

ALL FIRST CLASS (F) CONFIGURATION BASED ON 5 ABREAST SEATING PLUS A LOUNGE IN THE FRONT AND THE REAR COMPARTMENTS.

1111111*

MIXED F/Y CONFIGURATION BASED ON 5 ABREAST SEATING IN FIRST CLASS & 6 ABREAST SEATING IN COACH PLUS A LOUNGE IN THE FRONT AND IN THE REAR COMPARTMENTS.

1111111*

MAXIMUM COACH/ECONOMY (Y) PASSENGER CONFIGURATION BASED ON HIGH DENSITY 6 ABREAST SEATING.

‘SUPER’

DC-8 SERIES 61-63

(All DC-8 Super 60 Series Aircraft were Domestic & Intercontinental Versions)

The DC-8 Super 60 Series Aircraft gave the DC-8 a “new lease on life” in the mid-1960s and has subsequently made it possible for the conversion to the Super 70s Series Aircraft – most which are still flying today (See Super 70s section below).

The DC-8-61 extended the DC-8-55 fuselage length by 36.5 feet (11.13 Meters) while retaining the original engines & wing of the DC-8-55. This dramatically increased the passenger capacity and was optimal for medium range flights such as New York – San Francisco or West Coast USA – Hawaii. The DC-8-62 combined a short extension
of the Series 55 fuselage of 80 Inches (2.03 Meters), along with a 36 inch (.91 Meter) extension of each wing tip (to reduce drag and increase fuel capacity), and with a new aerodynamically superior engine pod to create an -Ultra- Long Range Aircraft. The DC-8-62 enabled nonstop flights never before possible such as Europe to the USA’s West Coast with a full payload. The DC-8-63 combined the benefits of the longer stretched fuselage of the DC-8-61 and
the longer range refinements of the DC-8-62 plus more powerful engines to create a Long Range, High Capacity Airliner which was useful on many of the world’s long haul routes which need more passenger and cargo capacity. All DC-8 Super 60 Series Aircraft were equipped with Pratt & Whitney Turbo Fan Engines and were available in Passenger, Combination Passenger/Freight (CF) and All Freight (AF) Versions. In addition to the 110 Super 60s DC-8s which were converted into Super 70s Models, there are still quite a few Super 60s DC-8s which have had “hush kits” installed on their engines and thus enabling them to continue flying today – even with the more strict noise limitations in place.

SaintENGINEDIMENSIONSTYPICALCARGODATETOTALREMARKS
#MAKER & MODEL #, THRUST IN LBS.(FT) L=LENGTH W/S=WINGSPANPASSENGER CONFIGURATIONSCAPACITY IN CUBIC FEET (BELOW CABIN IN CARGO BINS UNLESS OTHERWISE NOTED)CERTIFIED BY FAA#
(ALL ARE TURBOFAN ENGINES)MIXED F/YMADE
ALL COACH (Y) - MAXIMUM Y* &
CARGO PALLETS**
MW=MAXIMUM(IF APPLICABLE)
WEIGHTS (LBS) TAKEOFF/LANDING
61PWL=200-21225002435178BASIC
JT3D-3B187.4MIXED F/YMEDIUM RANGE, HIGH CAPACITY JETLINER
18,000 LBS.W/S= 142.36251 - 269 ALL Y
MW=325,000/240,000
61CFPWL=200-212100352463410COMBO-PASSENGER
JT3D-3B187.4MIXED F/Y 251 - 269 ALL Y -or-CABIN&/OR FREIGHTER: LARGE CARGO DOOR INTO CABIN, ALL PASSENGER SERVICE
18,000 LBS.W/S= 142.364 CARGO PALLETS +2500 CARGO BINS=EQUIPMENT ON BOARD
MW=328,000/240,000189 PSGRS -or-TOTAL OF 12,535
18 CARGO PALLETS
61AFPWL=1810035246340DOUGLAS OFFERED THIS VERSION AS AN ALL FREIGHTER (AF), BUT NO ONE ORDERED
JT3D-3B187.4PALLETS -CABINIT NEW. However, SOME AIRLINES LATER CONVERTED -61s AND -61CFs INTO 61AFs.
18,000 LBS.W/S= 142.36ALL CARGO2500 CARGO BINS=
MW=328,000/240,000TOTAL OF 12,535
62PWL=142-16816152458931BASIC
JT3D-3B 18,000 LBS -or-157.4MIXED F/YULTRA LONG RANGE JETLINER (MAXIMUM PASSENGER CAPACITY IS LIMITED TO
PW JT3D-7 19,000 LBS.W/S= 148.36189 ALL Y189 DUE TO LIMITATIONS OF EMERGENCY EXITS)
MW=335,000/240,000
62HPWL=142-16816152458920H=HEAVY
JT3D-3B 18,000 LBS -or-157.4MIXED F/Y>> INCREASED GROSS TAKEOFF WEIGHT TO 350,000 LBS (FROM 335,000
PW JT3D-7 19,000 LBS.W/S= 148.36189 ALL YLBS)
MW=350,000/240,000
62CFPWL=142-16890502493710COUNT
JT3D-3B 18,000 LBS -or-157.4MIXED F/YCABININCLUDES 2 DC-8-62CF-H MODELS; COMBO-PASSENGER &/OR FREIGHTER: LARGE
PW JT3D-7 19,000 LBS.W/S= 148.36189 ALL Y -or-1615 CARGO BINS=CARGO DOOR INTO CABIN, ALL PASSENGER SERVICE EQUIPMENT ON BOARD
MW=350,000/240,0004 PALLETS + 106 PSGRS -or-TOTAL OF 10,665
14 CARGO PALLETS
62AFPWL=149050249376ALL
JT3D-3B 18,000 LBS -or-157.4PALLETS -CABINFREIGHTER: LARGE CARGO DOOR, ALL PASSENGER SERVICE EQUIPMENT REMOVED;
PW JT3D-7 19,000 LBS.W/S= 148.36ALL CARGO1615 CARGO BINS=PASSENGER WINDOWS PLUGGED; FREIGHT HANDLING EQUIPMENT INSTALLED IN CABIN.
MW=335,000/240,000TOTAL OF 10,665
63PWL=200-21225002465241BASIC
JT3D-7187.4MIXED F/YLONG RANGE, HIGH CAPACITY JETLINER
19,000 LBS.W/S= 148.36251 - 269 ALL Y
MW=350,000/245,000
63CFPWL=200-212100352499953COMBO-PASSENGER
JT3D-7187.4MIXED F/Y 251 - 269 ALL Y -or-CABIN&/OR FREIGHTER: LARGE CARGO DOOR INTO CABIN, ALL PASSENGER SERVICE
19,000 LBS.W/S= 148.364 CARGO2500 CARGO BINS=EQUIPMENT ON BOARD
MW=355,000/275,000PALLETS +TOTAL OF 12,535
189 PSGRS -or-
18 CARGO
PALLETS
63AFPWL=1810035249997ALL
JT3D-7187.4PALLETS -CABINFREIGHTER: LARGE CARGO DOOR, ALL PASSENGER SERVICE EQUIPMENT REMOVED;
19,000 LBS.W/S= 148.36ALL CARGO2500 CARGO BINS=PASSENGER WINDOWS PLUGGED; FREIGHT HANDLING EQUIPMENT INSTALLED IN CABIN.
MW=355,000/275,000TOTAL OF 12,535
63PFPWL=200-2122500249996PASSENGER
JT3D-7187.4MIXED F/YFREIGHTER: JETLINER BUILT WITH THE STRONGER FREIGHTER SPECIFICATIONS.
19,000 LBS.W/S= 148.36251 - 269 ALL YCOULD EASILY BE CONVERTED ALL FREIGHTER BY ADDING A LARGE CARGO DOOR
MW=355,000/275,000INTO CABIN & REMOVING PASSENGER EQUIPMENT. BUILT AT EASTERN AIRLINE'S
REQUEST.
TOTAL'SUPER'DC-8SERIES61MADE:262--
- 63PF
GRANDTOTALOFALLDC-8'sMADE:556--
NOTES:
NOTES:
PW= PRATT & WHITNEY TURBOFAN ENGINES
1111111 *
MIXED F/Y CONFIGURATION BASED ON 4 ABREAST SEATING IN FIRST CLASS & 6 ABREAST SEATING IN COACH.
1111111 *
MAXIMUM COACH/ECONOMY (Y) PASSENGER CONFIGURATION BASED ON HIGH DENSITY SIX ABREAST SEATING.
1111111 **
CARGO PALLETS ARE BASED ON A PALLET SIZE OF 88 INCHES X 108 INCHES AND USED ON ‘CF’ AND ‘AF’ DC-8 VERSIONS.

‘SUPER’ DC-8 SERIES 71-73

All DC-8 Super 70s Aircraft are versions of the Super 60s Aircraft which have been refitted with new General Electric/Snecma CFM56-2 High Bypass Turbo Fan Engines & New Pylons. The new engines burn less fuel, have more power to take-off on shorter runways & climb to higher initial cruise altitudes and have increased the DC-8’s Maximum Range. Most importantly, the new engines make substantially less noise (up to 70% less) than the older engines & thus have met the progressively more strict noise regulations which have gone into effect in the 1980s, 1990s and the New Millennium. Other Optional upgrades for the Super 70s DC-8s included a newer,
more efficient pressurization & air conditioning system; addition of an Auxiliary Power Unit on board to provide both electrical power and air supply for engine starting  (while all earlier DC-8 Versions require Ground Power & Air Supply Equipment);
Updated Avionics in the cockpit (to state-of-the-art “Glass Cockpits”) and an Updated Cabin Cabin Interior. All of these modifications and upgrades have enabled the DC-8 to remain in productive service to this day, and they
are expected to safely ‘soldier on’ until 2010 and later!
Please note that all DC-8-70 model subtypes match precisely to the DC-8-60 model subtypes which they were upgraded from DC-8-61 becomes DC-8-71, DC-8-62AF becomes DC-8-72AF, DC-8-63CF becomes DC-8-73CF, etc.
MODELENGINEDIMENSIONSTYPICALCARGODATETOTALREMARKS
#TYPE, MODEL #, THRUST IN LBS.(FT) L=LENGTH W/S=WINGSPANPASSENGER CONFIGURATIONSCAPACITY IN CUBIC FEET (BELOW CABIN IN CARGO BINS UNLESS OTHERWISE NOTED)CERTIFIED BY FAA#
(ALL ARE HIGH BYPASS RATIO FAN ENGINES)MIXED F/YCONVER-SIONS
ALL COACH (Y) - MAXIMUM Y* &
MW=MAXIMUMCARGO PALLETS** (IF APPLICABLE)
WEIGHTS (LBS) TAKEOFF/LANDING
71CFM56-2L=200-21225003005443MOST
22,000 LBS.187.4MIXED F/YOF THESE PASSENGER CONVERSIONS WERE LATER CONVERTED TO CF OR AF MODELS
W/S= 142.36251 - 269 ALL YFOR HAULING FREIGHT.
MW=325,000/240,000
71CFCFM56-2L=200-212100353005410COMBO-PASSENGER
22,000 LBS.187.4MIXED F/YCABIN&/OR FREIGHTER: LARGE CARGO DOOR INTO CABIN, ALL PASSENGER SERVICE
W/S= 142.36251 - 269 ALL Y -or-2500 CARGO BINS=EQUIPMENT ON BOARD.
MW=328,000/240,0004 CARGOTOTAL OF 12,535
PALLETS + 189 PSGRS -or-
18 CARGO
PALLETS
71AFCFM56-2L=1810035300540ALL
22,000 LBS.187.4PALLETS -CABINFREIGHTER: LARGE CARGO DOOR, ALL PASSENGER SERVICE EQUIPMENT REMOVED;
W/S= 142.36ALL CARGO2500 CARGO BINS=PASSENGER WINDOWS PLUGGED; FREIGHT HANDLING EQUIPMENT INSTALLED IN CABIN.
MW=328,000/240,000TOTAL OF 12,535
72CFM56-2L=142-1681615302110ULTRA
22,000 LBS.157.4MIXED F/YLONG RANGE JETLINER.
W/S= 148.36189 ALL Y
MW=335,000/240,000
72HCFM56-2L=142-16816153021143
22,000 LBS.157.4MIXED F/YWERE CONVERTED INTO CORPORATE/ PRIVATE JETLINERS; 1 WAS CONVERTED FOR
W/S= 148.36189 ALL YNASA FOR RESEARCH.
MW=350,000/240,000
72CFCFM56-2L=142-1689050302113COMBO-PASSENGER
22,000 LBS.157.4MIXED F/YCABIN&/OR FREIGHTER: LARGE CARGO DOOR INTO CABIN, ALL PASSENGER SERVICE
W/S= 148.36189 ALL Y -or-1615 CARGO BINS=EQUIPMENT ON BOARD; ALL 3 OF THESE AIRCRAFT WERE CONVERTED FOR THE
MW=350,000/240,0004 PALLETS + 106 PSGRS -or-TOTAL OF 10,665FRENCH AIR FORCE.
14 CARGO
PALLETS
72AFCFM56-2L=149050302110ALL
22,000 LBS.157.4PALLETS -CABINFREIGHTER: LARGE CARGO DOOR, ALL PASSENGER SERVICE EQUIPMENT REMOVED;
W/S= 148.36ALL CARGO1615 CARGO BINS=PASSENGER WINDOWS PLUGGED; FREIGHT HANDLING EQUIPMENT INSTALLED IN CABIN.
MW=335,000/240,000TOTAL OF 10,665
73CFM56-2L=200-2122500301251THIS
22,000 LBS.187.4MIXED F/YAIRCRAFT WAS LATER CONVERTED INTO A FREIGHTER
W/S= 148.36251 - 269 ALL Y
MW=350,000/245,000
73CFCFM56-2L=200-212100353012533COMBO-PASSENGER
22,000 LBS.187.4MIXED F/YCABIN&/OR FREIGHTER: LARGE CARGO DOOR INTO CABIN, ALL PASSENGER SERVICE
W/S= 148.36251 - 269 ALL Y -or-2500 CARGO BINS=EQUIPMENT ON BOARD
MW=355,000/275,0004 CARGOTOTAL OF 12,535
PALLETS + 189 PSGRS -or-
18 CARGO
PALLETS
73AFCFM56-2L=18100353012514ALL
22,000 LBS.187.4PALLETS -CABINFREIGHTER: LARGE CARGO DOOR, ALL PASSENGER SERVICE EQUIPMENT REMOVED;
W/S= 148.36ALL CARGO2500 CARGO BINS=PASSENGER WINDOWS PLUGGED; FREIGHT HANDLING EQUIPMENT INSTALLED IN CABIN.
MW=355,000/275,000TOTAL OF 12,535
73PFCFM56-2L=200-2122500301252BOTH
22,000 LBS.187.4MIXED F/YOF THESE AIRCRAFT WERE LATER CONVERTED INTO FREIGHTERS.
W/S= 148.36251 - 269 ALL Y
MW=355,000/275,000
TOTALOFDC-8-61CONVERTEDTO71-110--
- 63PF73
NOTES:
CFM-56-2 = GENERAL ELECTRIC/SNECMA
CFM56-2 HIGH BYPASS TURBOFAN ENGINES
1111111 *
MIXED F/Y CONFIGURATION BASED ON 4 ABREAST SEATING IN FIRST CLASS & 6 ABREAST SEATING IN COACH.
1111111 *
MAXIMUM COACH/ECONOMY (Y) PASSENGER CONFIGURATION BASED ON HIGH DENSITY SIX ABREAST SEATING.
1111111 **
CARGO PALLETS ARE BASED ON A PALLET SIZE OF 88 INCHES X 108 INCHES AND USED ON ‘CF’ AND ‘AF’ DC-8 VERSIONS.

TO SEE A MORE DETAILED HISTORY OF THE DC-8-70 CONVERSIONS BY INDIVIDUAL AIRCRAFT:

>>PLEASE CLICK HERE <<

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