HeavyLift International Airlines

Fleet Specifications

HeavyLift's A6-HLA and A6-HLB Aircraft
Aircraft Type:
DC8-63F
Engine Type:
JT3D-7
Aircraft Reg:
A6-HLA
A6-HLB
MSN:
46034
46035
Built:
February 1969
February 1969

Operational Data

Area Navigation:
BRNAV-RNP5
Reduced Vertical Separation Minimum:
RVSM Compliant
TCAS 7.0/ACASII:
Yes
TAWS Complaint:
Yes
FM Immune/8.33 MHz Spacing Complaint:
Yes
Navigation System:
GPS
Stage III Complaint:
Yes

Basic Operating Data

Engines:
Pratt & Whitney JT3D-7
Engine Thrust:
19,285 lbs
Number of Containers:
Eighteen 88 x 125 in (224 x 318 cm)

Aircraft Dimensions

Overall Length:
187 feet, 5 inches
Overall Height:
43 feet, 5 inches
Wingspan:
148 feet, 5 inches

Design Weights

Maximum Taxi Weight:
358,000 lbs (162,388 kg)
Maximum Take-Off Weight:
355,000 lbs (161,028 kg)
Maximum Zero Fuel Weight:
244,000 lbs (110,677 kg)
Maximum Landing Weight:
258,000 lbs (117,027 kg)
Dry Operating Weight (Typical):
150,505 lbs (68,269 kg)
Payload:
116,000 lbs (52,617.6 kg)
Fuel Capacity:
24,275 gals (91,891 liters)

Cargo Configuration Main Deck

Cargo Configuration Main Deck

Cargo Weight Limits

Cargo Weight Limits

Main Cargo Door Dimension

Main Cargo Door Dimension

Cargo Configuration Lower Deck

Cargo Configuration Lower Deck

Volume

Forward Cargo Compartment Aft Cargo Compartment Total Cargo
FT3 M3 FT3 M3 FT3 M3
1290 36.5 1210 34.3 2500 70.8