*****AIRCRAFT “Antonov - AN26”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position:  High wing

Engine position: (Front) Wing leading mounted

Tail configuration: Regular tail, high set

Landing gear: Tricycle retractable

Wing Span: 29.2 m

Length: 23.8 m

Height: 8.6 m

Power plant: 2 x 2.820 SHP Ivchenko AI 24VT turboprops with 4 blade

propellers and 1 x 8.83 kN RU 19-300 aux turbojet in starboard nacelle.

Accommodation: Crew of 5 (Pilot, Co-pilot,radio operator, navigator and flight engineer) and up to 40 troops or 24 patients.

Notes: Military tactical transport aircraft. In service since 1968. More powerful development of AN-24 with rear loading ramp and redesigned tail for military use. Chinese versions Y-7 and Y-7H. Civil version An-26S. In production from 1968 to 1985. Over 550 An-26s are in world wide civil service.
Alternative names:
ANTONOV An-26, XIAN Y-7H, Y-7H.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 24.000 kg

VMO - Maximum Operating Speed 235 KIAS

MMO - Maximum Operating Speed Mach nd Mach

Turbulent Air Penetration Speed   000 KIAS/.00 Mach

VLO - Maximum Gear Operating Speed   000 KIAS

VLE - Maximum Landing Gear Extension Speed   000 KIAS/.00 Mach

 

*****Maximum Flap Placard Speeds*****

Flaps degrees     KIAS

1           000

2           000

5           000

10          000

15          000

25          000

30          000

40          000

 

*****Take-off*****

WTC:        M

Distance:   1200 mt

V2 (IAS):   120 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        150 kt

ROC:        1500 ft/min

-(to FL150)

IAS:        200 kt

ROC:        1000 ft/min

-(to FL240)

IAS:        200 kt

ROC:        800 ft/min

-(mach)

mach:       na

ROC:        na ft/min

 

*****Cruise*****

TAS:        235 kt

MACh:       nd

Ceiling:    FL260

Range:      600 NM

 

*****Descent *****

- (to FL240)

mach:       nd

ROD:        nd ft/min

- (to FL100)

IAS:        240 kt

ROD:        1500 ft/min

 

*****Approach*****

IAS:        240 kt

MCS:        170 kt

ROD:        1500 ft/min

 

*****Landing*****

Vht (IAS):  105 kt

APC:        B

Distance:   700 mt