McDonnell Douglas DC-10-30LR
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4 months ago
Auto Credit Based on onelast747's DC-10-30
What If This Was DC-10's Last Variant?
Sample
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Information
The McDonnell Douglas DC-10-30LR is the long-range variant of the original DC-10-30. It Made Its First Flight In The Early 2000s 2 Years And 10 Months Ago When McDonnell Douglas Went Defunct
Specs (by me)
Powerplant: 2x RR RB11, 1x GE CF6-50C
Range: 7000nmi
First Flight: May 16th 2000
Introduction: December 17th 2000, With Martinair
Status: In Production, In Service
Producted: 2000-Present
Minimum Runway Length: 6000ft Free
Primary Users: Martinair, KLM, Lufthansa, American Airlines
Number Built: 140
MTOW: 700000kg
MLOW: 200000kg
Retired: Didn't Retire Yet
Variants: KC-10LR, KDC-10LR, DC-10-30XLR
Controls
AG1: Door L1
AG2 - AG8: None
Brakes: Reverse Thrust, Mimium Speed 30Knots
Fun Facts For the DC-10-30LR
- The DC-10-30LR Was The First Ultra-Long Range Trijet In The 2000s
- This Is the Only Plane To Have 2 Engines In Just 1 Variant
- This Was The Only plane To Make its first Flight When A Company Was Defunct, McDonnell Douglas Was Defunct In 1997 After It Merged With Boeing
Specifications
General Characteristics
- Predecessor DC-10-30
- Created On Mac
- Wingspan 168.2ft (51.3m)
- Length 184.7ft (56.3m)
- Height 60.1ft (18.3m)
- Empty Weight 109,298lbs (49,576kg)
- Loaded Weight 164,967lbs (74,828kg)
Performance
- Power/Weight Ratio 0.367
- Horse Power/Weight Ratio 0.097
- Wing Loading 43.9lbs/ft2 (214.4kg/m2)
- Wing Area 3,756.5ft2 (349.0m2)
- Drag Points 31081
Parts
- Number of Parts 743
- Control Surfaces 1
- Performance Cost 3,559