MCDONNELL DOUGLAS CORPORATION
DOUGLAS AIRCRAFT COMPANY
DC/MD-10
AIRPLANE
CHARACTERISTICS FOR
AIRPORT PLANNING
DAC-67803A REPRINTED JANUARY 1991
REVISION A APRIL 2004
DC/MD-10 AIRPLANE CHARACTERISTICS LIST OF REVISIONS
Page Date Page Date Page Date
Original 1 to 190 January 1991
Rev A April 2004
Title Page April 2004 iv April 2004 v April 2004 vi April 2004 2 April 2004 5 April 2004
135 April 2004 136 April 2004 137 April 2004 138 April 2004
140-A April 2004 141-A April 2004 163-A April 2004 164-A April 2004 165-A April 2004 166-A April 2004 167-A April 2004 168-A April 2004
APRIL 2004 iv
CONTENTS
Page
1.0 SCOPE ............................................................................................................................. 1 1.1 Purpose ................................................................................................................... 1 1.2 Introduction ............................................................................................................ 2 1.3 Inclusion of MD-10-10F/-30F Information ........................................................... 2 2.0 AIRPLANE DESCRIPTION ........................................................................................... 3 2.1 General Airplane Characteristics ........................................................................... 3 2.2 General Airplane Dimensions ................................................................................ 6 2.3 Ground Clearances ................................................................................................. 12 2.4 Interior Arrangements ............................................................................................ 14 2.5 Passenger Cabin Cross Section .............................................................................. 18 2.6 Lower Compartment Containers ............................................................................ 25 2.7 Door Clearances ..................................................................................................... 29 2.7.1 Passenger Loading Doors ............................................................................. 30 2.7.2 Cargo Loading Doors ................................................................................... 34 2.7.3 Critical Interference Path Door/Sill Wing Clearance ................................... 41 3.0 AIRPLANE PERFORMANCE ....................................................................................... 43 3.1 General Information ............................................................................................... 43 3.2 Payload/Range ....................................................................................................... 44 3.2.1 Payload/Range .............................................................................................. 44 3.2.2 Payload/Range (Metric) ............................................................................... 52 3.3 FAR Takeoff Runway Length Requirements ........................................................ 60 3.4 FAR Landing Runway Length Requirements ........................................................ 64 3.5 Approach Speed (Threshold) ................................................................................. 67 4.0 GROUND MANEUVERING .......................................................................................... 69 4.1 General Information ............................................................................................... 69 4.2 Turning Radii, No Slip Angle ................................................................................ 70 4.3 Minimum Turning Radii ........................................................................................ 72 4.4 Visibility From Cockpit in Static Position ............................................................. 74 4.5 Runway and Taxiway Turn Paths .......................................................................... 75 4.5.1 More than 90º Turn – Runway to Taxiway .................................................. 75 4.5.2 90º Turn – Runway to Taxiway ................................................................... 77 4.5.3 90º Turn – Taxiway to Taxiway ................................................................... 79 4.5.4 90º Turn – Taxiway to Taxiway ................................................................... 81 4.6 Runway Holding Bay Apron .................................................................................. 83 4.7 Minimum Parking Space Requirements ................................................................ 85 4.7.1 Minimum Parking Space Requirements (Feet) ............................................ 85 4.7.2 Minimum Parking Space Requirements (Meters) ........................................ 88 5.0 TERMINAL SERVICING .............................................................................................. 91 5.1 Airplane Servicing Arrangement (Typical) ........................................................... 91 5.2 Terminal Operations, Turnaround Station ............................................................. 93 5.3 Terminal Operations, Enroute Station ................................................................... 99 5.4 Ground Service Connections ................................................................................. 105 5.5 Engine Starting Pneumatic Requirements .............................................................. 113 5.6 Ground Pneumatic Power Requirements ............................................................... 116 5.7 Preconditioned Airflow Requirements ................................................................... 117 5.8 Ground Towing Requirements ............................................................................... 118
APRIL 2004 v
CONTENTS
Page
APRIL 2004 vi
6.0 OPERATING CONDITIONS ......................................................................................... 121 6.1 Jet Engine Exhaust Velocities and Temperatures .................................................. 121 6.1.1 Jet Engine Exhaust Velocity Contours, Breakaway Power .......................... 122 6.1.2 Jet Engine Exhaust Velocity Contours, Takeoff Power ............................... 124 6.1.3 Jet Engine Exhaust Velocity Contours, Idle Power ..................................... 127 6.1.4 Jet Engine Exhaust Temperature .................................................................. 130 6.2 Airport and Community Noise ............................................................................... 131 7.0 PAVEMENT DATA ....................................................................................................... 133 7.1 General Information ............................................................................................... 133 7.2 Footprint ................................................................................................................. 135 7.3 Maximum Pavement Loads ................................................................................... 137 7.4 Landing Gear Loading on Pavement ..................................................................... 139 7.4.1 Loads on Main Landing Gear Group ........................................................... 139 7.4.2 Center Gear and Wing Gear Loading on Pavement ..................................... 141 7.5 Flexible Pavement Requirements, U.S. Army Corps of Engineers Design Method S-77-1 ........................................................................................... 144 7.6 Flexible Pavement Requirements, LCN Conversion ............................................. 148 7.7 Rigid Pavement Requirements, Portland Cement Association Design Method .... 152 7.8 Rigid Pavement Requirements, LCN Conversion ................................................. 156 7.9 ACN-PCN Reporting System ................................................................................ 162 7.9.1 Aircraft Classification Numbers (ACNs) ..................................................... 162 7.9.2 ACN-PCN System Background ................................................................... 169 8.0 POSSIBLE DC-10/MD-10 DERIVATIVE AIRPLANES .............................................. 173 9.0 SCALE DRAWINGS ...................................................................................................... 175
1.0 SCOPE 1.1 Purpose 1.2 Introduction 1.3 Inclusion of MD-10-10F/-30F Information
1.0 SCOPE
1.1 Purpose
This document provides, in a standardized format, the recommended minimum airplane characteristics data that are needed for general airport planning information. The DC-10 data in this document are for each series considering airport operations. Since operational practices vary among airlines, specific data should be coordinated with the using airlines prior to facility design. The Douglas Aircraft Company should be contacted for any additional information required.
Content of the document reflects the results of a coordinated effort by representatives from
the following organizations:
Aerospace Industries Association Airport Operators’ Council International Air Transport Association of America International Air Transport Association
APRIL 2004 1
APRIL 2004 2
1.2 Introduction
This document is completely updated to conform to NAS 3601 as revised November 1976. All previous revisions are incorporated in this edition. It provides Douglas Model DC-10 characteristics for airport operators, airlines and engineering consultant organizations. Since airplane changes and available options may alter the information, the data presented herein must be regarded as subject to change. Similarly, for airplanes not yet certified, changes can be expected to occur.
For further information, contact: Boeing Commercial Airplanes Airport Technology, M/C 67-KR P.O. Box 3707 Seattle, WA 98124-2207 USA Telephone: 425-237-0126 Fax: 425-237-8281 Email: [email protected] Website: www.boeing.com/airports
1.3 Inclusion of MD-10-10F/-30F Freighter Information
This document has been partially revised to incorporate key information for the MD-10-10F and MD-10-30F Freighters. The main change was the incorporation of the MD-11 landing gear tires and carbon brakes onto the MD-10-10F and MD-10-30F Freighters. The general airplane characteristics table and select pages from section 7 of the document pertaining to pavement data were the only pages revised. All existing charts and diagrams for the DC-10 that were not revised can still be considered valid for the MD-10-10F and MD-10-30F Freighters.
April 2004
5
SERIES 10CF 30CF 40CF MD-10-10F MD-10-30F
MODE PSGR CARGO PSGR CARGO PSGR CARGO CARGO CARGO
ENGINE CF6-6D CF6-50C JT9D-59A* CF6-6D CF6-50C
MAXIMUM RAMP WEIGHT POUNDS
KILOGRAMS
443,000
200,942
443,000
200,942
558,000
253,105
558,000
253,105
558,000
253,105
558,000
253,105
443,000
200,942
583,000
264,444
MAXIMUM LANDING WEIGHT POUNDS
KILOGRAMS
363,500
164,881
363,500
164,881
411,000
186,427
411,000
186,427
411,000
186,427
411,000
186,427
375,000
170,097
436,000
197,766
MAXIMUM TAKEOFF WEIGHT POUNDS
KILOGRAMS
440,000
199,581
440,000
199,581
555,000
251,744
555,000
251,744
555,000
251,744
555,000
251,744
440,000
199,581
580,000
263,084
OPERATING WEIGHT EMPTY POUNDS
KILOGRAMS
243,750
110,563
215,444
97,724
268,751
121,904
238,036
107,971
272,773
123,728
242,058
109,796
216,000
97,976
236,500
107,275
MAXIMUM ZERO FUEL WEIGHT
POUNDS
KILOGRAMS
335,000
151,954
335,000
151,954
391,000
177,355
391,000
177,355
391,000
177,355
391,000
177,355
355,000
161,025
414,000
187,787 MAXIMUM STRUCTURAL
PAYLOAD (WEIGHT LIMITED)
POUNDS
KILOGRAMS
91,250
41,390
119,556
54,230
122,249
55,451
152,964
69,383
118,227
53,627
148,942
67,559
139,000
63,049
177,500
80,512
MAXIMUM CARGO VOLUME CUBIC FEET
CUBIC METERS
4,597
130.17
16,845
477.05
4,618
130.77
16,866
477.65
4,618
130.77
16,866
477.65
14,200
402.1
14,200
402.1
SEATING CAPACITY (STD/MAX)
STANDARD
MAXIMUM
255
399
0
0
255
399
0
0
255
399
0
0
0
0
0
0
USABLE FUEL CAPACITY U.S. GALLONS
LITERS
21,762***
82,376
21,762***
82,376
36,652
137,509
36,652
137,509
36,652
137,509
36,652
137,509
21,762
82,376
36,652
137,509 * FOR JT9D-20 ENGINE VERSION, SUBTRACT 515 POUNDS FROM OWE ** FOR NONEXTENDED CTR CARGO COMPARTMENT, REDUCE VOLUME 21 CU FT (SEE PAGE 27) ***FUEL CAPACITY WITH AUXILIARY CENTER WING TANK, 26,647 GALLONS FOR 572,000 POUND MTOGW: • ADD 379 POUNDS TO OWE AND SUBTRACT 379 POUNDS FROM MAXIMUM STRUCTURAL PAYLOAD • INCREASE LANDING WEIGHT TO 421,000 POUNDS
2.1 GENERAL AIRPLANE CHARACTERISTICS MODEL DC-10 SERIES 10CF, 30CF, 40CF,
AND MD-10 SERIES 10F AND 30F
THIS PAGE LET BLANK INTENTIONALLY
68
April 2004 135
54 IN (137 CM)(TYPICAL)
64 IN (163 CM)(TYPICAL)
72 FT 4.6 IN (22.06 M)
(10.67 M)
24 IN(61 CM)
35 FT
41 FT 3 IN(12.57 M)
UNITS SERIES 10 AND 10CF MD-10-10F MAXIMUM DESIGN TAXI
WEIGHT LB KG
458,000 207,746
443,000 200,941
PERCENT OF WEIGHT ON MAIN GEAR % SEE SECTION 7.4
NOSE GEAR TIRE SIZE IN. 37 x 14 - 14 37 x 14 - 14
NOSE GEAR TIRE PRESSURE
PSI KG/CM2
165 11.60
165 11.60
MAIN GEAR TIRE SIZE IN. 50 X 20 - 20 H54 X 21 - 24
MAIN GEAR TIRE PRESSURE
PSI KG/CM2
195 13.71
155 10.90
7.2.1 FOOTPRINT MODEL DC-10 SERIES 10, 10CF AND
MD-10 SERIES 10F
April 2004 136
25 IN(64 CM)
54 IN (137 CM)(TYPICAL)
64 IN (163 CM)(TYPICAL)
72 FT 4.6 IN (22.06 M)
30 IN. 37.5 IN.
35 FT
(76 CM) (95 CM)
(10.67 M)
41 FT 3 IN(12.57 M)
UNITS SERIES 30, 30CF, 40, 40CF MD-10-30F
MAXIMUM DESIGN TAXI WEIGHT
LB KG
583,000 264,445
583,000 264,445
PERCENT OF WEIGHT ON MAIN
GEAR % SEE SECTION 7.4
NOSE GEAR TIRE SIZE IN. 40 x 15.5 - 16 40 x 15.5 - 16
NOSE GEAR TIRE PRESSURE
PSI KG/CM2
185 13.01
185 13.01
WING AND CENTER GEAR TIRE SIZE IN. 52 X 20.5 - 23 H54 X 21 - 24
WING GEAR TIRE PRESSURE
PSI KG/CM2
177 12.45
175 12.30
CENTER GEAR TIRE PRESSURE
PSI KG/CM2
153 10.76
145 10.19
7.2 .2 FOOTPRINT
MODEL DC-10 SERIES 30, 30CF, 40, 40CF AND
MD-10 SERIES 30F
April 2004 137
V N = MAXIMUM VERTICAL NOSE GEAR GROUND LOAD PER STRUT AT MOST FORWARD
CENTER OF GRAVITY
V W = MAXIMUM VERTICAL WING GEAR GROUND LOAD PER STRUT AT MOST AFT
CENTER OF GRAVITY Hw = MAXIMUM HORIZONTAL GROUND LOAD PER STRUT FROM BRAKING NOTE: ALL LOADS CALCULATED USING AIRPLANE MAXIMUM DESIGN TAXI WEIGHT
NOSE GEAR VN
WING GEAR Vw
Hw PER STRUT
MAX STATIC STATIC + MAX STEADY AT AIRPLANE UNITS DESIGN AT BRAKING LOAD AT BRAKING INSTANTANEOUS
MODEL TAXI MOST 10 FT/SEC2 STATIC 10 FT/SEC2 BRAKING WEIGHT FWD C.G. DECEL AFT C.G. DECEL (m = 0.8)
SERIES 10, 10CF LB 458,000 50,243 84,959 213,680 71,501 170,944
KG 207,746 22,790 38,537 96,923 32,433 77,538 MD-10- 10F LB 443,000 47,454 80,705 207,123 68,798 165,698 FREIGHTER KG 200,941 21,525 36,607 93,949 31,206 75,159
7.3.1 MAXIMUM PAVEMENT LOADS MODEL DC-10 SERIES 10, 10CF AND
MD-10 SERIES 10F
April 2004 138
V N = MAXIMUM VERTICAL NOSE GEAR GROUND LOAD PER STRUT AT MOST FORWARD CENTER
OF GRAVITY V W = MAXIMUM VERTICAL WING GEAR GROUND LOAD PER STRUT AT MOST AFT CENTER OF GRAVITY V C = MAXIMUM VERTICAL CENTER GEAR GROUND LOAD PER STRUT AT MOST AFT CENTER OF GRAVITY H W = MAXIMUM HORIZONTAL WING GEAR GROUND LOAD PER STRUT FROM BRAKING H C = MAXIMUM HORIZONTAL CENTER GEAR GROUND LOAD PER STRUT FROM BRAKING NOTE: ALL LOADS CALCULATED USING AIRPLANE MAXIMUM DESIGN TAXI WEIGHT
NOSE GEAR WING GEAR CENTER GEAR VN VN Vw Hw Vc Hc
AIRPLANE MODEL UNITS
MAX DESIGN
TAXI WT
STATIC AT
FWD C.G.
STATIC + BRAKING
10 FT/SEC^2
STATIC AT AFT
C.G.
STEADY BRAKING
10 FT/SEC^2
INST BRAKING (M=0.8)
STATIC AT AFT
C.G.
STEADY BRAKING
10 FT/SEC^2
INST BRAKING (M=0.8)
LB 583,000 72,234 112,229 218,767 74,278 175,014 94,746 32,170 75,797 SERIES 30, 30CF, 40,
40CF KG 264,445 32,965 50,906 99,231 33,692 67,454 42,976 14,952 29,215
LB 583,000 71,060 111,375 221,432 74,424 177,145 96,102 32,300 76,882 MD-10- 30F FREIGHTER
KG 264,445 32,232 50,518 100,440 33,758 80,352 43,591 14,651 34,873
7.3.2 MAXIMUM PAVEMENT LOADS MODEL DC-10 SERIES 30, 30CF, 40, 40CF AND
MD-10 SERIES 30F
April 2004 140-A
80 85 90 95 100200
240
280
320
100
120
10 15 20 25 30
% MAC
MAXIMUM RAMP WEIGHT 443,000 LB
C.G. FOR ACNCALCULATIONS
360
200
240
280
320
360
440
400400
440
480
140
160
180
200
AIRPLANEGROSSWEIGHT(1000 KG)
AIRPLANEGROSSWEIGHT(1000 LB)
WEIGHTON MAINLANDINGGEARS(1000 LB)
7.4.1-A LANDING GEAR LOADING ON PAVEMENT MODEL MD-10 SERIES 10F
April 2004 141-A
80
PERCENT OF WEIGHT ON MAIN GEAR
85 90 95 100250
300
350
400
120
140
10 15 20 25 30
% MAC
MAXIMUM RAMP WEIGHT 583,000 LB
C.G. FOR ACNCALCULATIONS
450
250
300
350
400
450
550
500500
550
600
160
180
200
220
AIRPLANEGROSSWEIGHT(1000 KG)
AIRPLANEGROSSWEIGHT(1000 LB)
WEIGHTON MAINLANDINGGEARS(1000 LB)
240
260
7.4.2-A LANDING GEAR LOADING ON PAVEMENT MODEL MD-10 SERIES 30F
April 2004
163-A
100 150 200 250 300 350 400 450 5000
20
40
60
80
100
(1,000 LB)
60(1,000 KG)
CODE D - CBR 3 (ULTRA LOW)CODE C - CBR 6 (LOW)CODE B - CBR 10 (MEDIUM)CODE A - CBR 15 (HIGH)
H54 X 21-24 36 PR TIRES PRESSURE CONSTANT AT 155PSI
AIRCRAFT
AIRCRAFT GROSS WEIGHT
80 100 120 140 160 180 200 220
CG AT MOST AFT POSITION FOR MAXIMUM RAMP WEIGHT
CLASSIFICATIONNUMBER(ACN)
7.9.1-A AIRCRAFT CLASSIFICATION NUMBER - FLEXIBLE PAVEMENT
MODEL MD-10 SERIES 10F
April 2004
164-A
200 250 300 350 400 450 500 550 60020
60
(1,000 LB)
100(1,000 KG)
CODE D - CBR 3 (ULTRA LOW)CODE C - CBR 6 (LOW)CODE B - CBR 10 (MEDIUM)CODE A - CBR 15 (HIGH)
H54 X 21-24 36 PR TIRESPRESSURE CONSTANT AT 175PSI
AIRCRAFT GROSS WEIGHT
120 140 160 180 200 220 240 260
CG AT MOST AFT POSITION FOR MAXIMUM RAMP WEIGHT
AIRCRAFTCLASSIFICATIONNUMBER(ACN)
7.9.2-A AIRCRAFT CLASSIFICATION NUMBER - FLEXIBLE PAVEMENT MODEL MD-10 SERIES 30F
WING GEAR
April 2004
165-A
200 250 300 350 400 450 500 550 60020
40
60
80
100
120
(1,000 LB)
100(1,000 KG)
CODE D - CBR 3 (ULTRA LOW)CODE C - CBR 6 (LOW)CODE B - CBR 10 (MEDIUM)CODE A - CBR 15 (HIGH)
H54 X 21-24 36 PR TIRES PRESSURE CONSTANT AT 145PSI
AIRCRAFT GROSS WEIGHT
120 140 160 180 200 240 260 280
CG AT MOST AFT POSITION FOR MAXIMUM RAMP WEIGHT
AIRCRAFTCLASSIFICATIONNUMBER(ACN)
7.9.3-A AIRCRAFT CLASSIFICATION NUMBER - FLEXIBLE PAVEMENT
MODEL MD-10 SERIES 30F CENTER GEAR
April 2004
166-A
100 150 200 250 300 350 400 450 500
(1,000 LB)
60(1,000 KG)
CODE D - k=75 (ULTRA LOW)CODE C - k=150 (LOW)CODE B - k=300 (MEDIUM)CODE A - k=550 (HIGH)
H54 X 21-24 36 PR TIRES PRESSURE CONSTANT AT 155PSI
AIRCRAFT GROSS WEIGHT80 100 120 140 160 180 200 220
CG AT MOST AFT POSITION FOR MAXIMUM RAMP WEIGHT
AIRCRAFTCLASSIFICATIONNUMBER(ACN)
7.9.4-A AIRCRAFT CLASSIFICATION NUMBER - RIGID PAVEMENT
MODEL MD-10 SERIES 10F
April 2004
167-A
200 250 300 350 400 450 500 550 60020
40
60
80
100
120
(1,000 LB)
100(1,000 KG)
CODE D - k=75 (ULTRA LOW)CODE C - k=150 (LOW)CODE B - k=300 (MEDIUM)CODE A - k=550 (HIGH)
H54 X 21-24 36 PR TIRES PRESSURE CONSTANT AT 175PSI
AIRCRAFT GROSS WEIGHT
120 140 160 180 200 220 240 260
CG AT MOST AFT POSITION FOR MAXIMUM RAMP WEIGHT
AIRCRAFTCLASSIFICATIONNUMBER(ACN)
7.9.5-A AIRCRAFT CLASSIFICATION NUMBER - RIGID PAVEMENT
MODEL MD-10 SERIES 30F WING GEAR
April 2004
168-A
200 250 300 350 400 450 500 550 60020
40
60
80
100
120
(1,000 LB)
100(1,000 KG)
CODE D - k=75 (ULTRA LOW)CODE C - k=150(LOW)CODE B - k=300 (MEDIUM)CODE A - k=550 (HIGH)
H54 X 21-24 36 PR TIRES PRESSURE CONSTANT AT 145PSI
AIRCRAFT GROSS WEIGHT
120 140 160 180 200 220 240 260
CG AT MOST AFT POSITION FOR MAXIMUM RAMP WEIGHT
AIRCRAFTCLASSIFICATIONNUMBER(ACN)
7.9.6- A AIRCRAFT CLASSIFICATION NUMBER - RIGID PAVEMENT MODEL MD-10 SERIES 30F
CENTER GEAR
8.0 POSSIBLE DC-10/MD-10 DERIVATIVE AIRPLANES
8.0 POSSIBLE DC-10/MD-10 DERIVATIVE AIRPLANES
No additional versions of the DC-10/MD-10 series aircraft are currently planned.
APRIL 2004 173
APRIL 2004 174
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