| Manufacturer |
Boeing |
| First flight |
September 26, 1981 |
| Introduction |
September 8, 1982, with United Airlines |
| Role |
Wide-body airliner |
| Produced |
1981–present |
| National origin |
United States |
|
|
| Primary users |
- Delta Air Lines
- FedEx Express
- UPS Airlines
- United Airlines
|
| Cockpit crew |
Two |
| 3-class seats |
- 174 (15F, 40J, 119Y) – 767-200, 767-200ER
- 210 (18F, 42J, 150Y) – 767-300, 767-300ER/F
- 243 (16F, 38J, 189Y) – 767-400ER
|
| 2-class seats |
- 214 (18J, 196Y) – 767-200, 767-200ER
- 261 (24J, 237Y) – 767-300, 767-300ER/F
- 296 (24J, 272Y) – 767-400ER
|
| 1-class (limit) |
- 245Y (290) – 767-200, 767-200ER
- 290Y (351)- 767-300, 767-300ER/F
- 409Y (375) – 767-400ER
|
| Length |
- 159 ft 2 in / 48.51 m – 767-200, 767-200ER
- 180 ft 3 in / 54.94 m – 767-300, 767-300ER/F
- 201 ft 4 in / 61.37 m – 767-400ER
|
| Cargo |
- 3,070 ft3 / 86.9 m3 – 767-200, 767-200ER
- 4,030 ft3 / 114.1 m3 – 767-300, 767-300ER/F
- 4,905 ft3 / 138.9 m3 – 767-400ER
|
| Fuselage |
Exterior: 17 ft 9 in / 5.41 m height, 16 ft 6 in / 5.03 m width; Cabin width: 186 in/ 4.72 m |
| Unit load device |
- 22 LD2s – 767-200, 767-200ER
- 30 LD2s – 767-300, 767-300ER/F
- 38 LD2s – 767-400ER
|
| Wing |
- 3,050 ft2 / 283.3 m2, 31.5° sweepback – 767-200, 767-200ER, 767-300, 767-300ER/F
- 3,130 ft2 / 290.7 m2 – 767-400ER
|
| Wingspan |
- 156 ft 1 in / 47.57 m – 767-200, 767-200ER, 767-300, 767-300ER/F
- 170 ft 4 in / 51.92 m – 767-400ER
|
| Max. payload |
- 73,350 lb (33.3 t) – 767-200
- 78,390 lb (35.6 t)– 767-200ER
- 88,250 lb (40.0 t)– 767-300
- 96,560 lb (43.8 t)– 767-300ER/F
- 101,000 lb (45.8 t) – 767-400ER
|
| MTOW |
- 315,000 lb / 142.9 t – 767-200
- 395,000 lb / 179.2 t – 767-200ER
- 350,000 lb / 158.8 t – 767-300
- 412,000 lb / 186.9 t – 767-300ER/F
- 450,000 lb / 204.1 t – 767-400ER
|
| Range |
- 3,900 nmi
7,200 km – 767-200
- 6,590 nmi
12,200 km – 767-200ER
- 3,900 nmi
7,200 km – 767-300
- 5,980 nmi
11,070 km)– 767-300ER/F
- 5,625 nmi
10,415 km – 767-400ER
|
| Fuel capacity |
std-ER: 16,700-24,140 US gal / 63.2-91.4 m3 (111,890-161,740 lb / 50.8-73.4 t ) |
| Ceiling |
43,100 ft (13,100 m) |
| Cruise speed |
Long range-Maximum: 459–486 kn (850–900 km/h) at altitude of 39,000 ft (12,000 m) |
| Engines (×2) |
- JT9D / PW4000 / CF6 – 767-200
- JT9D / PW4000 / CF6 / RB211– 767-200ER, 767-300
- PW4000 / CF6 / RB211– 767-300ER/F
- CF6 / PW4000 – 767-400ER
|
| Thrust (×2) |
- 48,000–52,500 lbf
214–234 kN – 767-200
- 48,000–60,600 lbf
214–270 kN– 767-200ER
- 48,000–60,600 lbf
214–270 kN– 767-300
- 56,750–61,500 lbf
252–274 kN– 767-300ER/F
- 60,600 lbf
270 kN – 767-400ER
|
| Takeoff |
-
- 6,300 ft (1,900 m) – 767-200
- 2,480 m / 8,150 ft– 767-200ER
-
- 9,200 ft (2,800 m) – 767-300
- 2,650 m / 8,700 ft – 767-300ER/F
- 3,290 m / 10,800 ft – 767-400ER
|