388 
SAAB AIRCRAFT COMPANY 
^фоф^ 
LINKÖPING, SWEDEN 
SAAB 91 C 'SAUK** 
Purpose: Aerial mapping (and prospecting) 
Size: Two—Three persons plus camera equipment 
Max. weight 1215 kg (2680 lbs) 
Disposable load 475 kg (1050 lbs) 
Normal speed range: 130 to 250 km/h (80 to 155 mph) 
Operating time: Up to 7 hours 
Construction, and function: Single-engine all-metal aircraft of 
sturdy design. Built for simple maintenance and reliability 
in operation. Pilot and photographer in front seats. Camera 
(plus photographer if small camera) in rear of cabin. 
Use: The Safir offers extraordinary economy for aerial mapping at altitudes up to 5000 m (16000 ft) 
Stability and good flight characteristics give small deviations from vertical direction and small 
variation in altitude. 
Fittings: Any modern camera can be installed. 
Service: Special service departm. offers all-world service. Safir now operating in 17 countries. 
Price: Quotations from Saab upon request. (Depending on camera type, equipment requirements etc. 
PH0T0GRAMMETRIC EQUIPMENT 
JENA made 
Mirror Stereoscope 
Illumination Device for Mirror 
Stereoscope 
Stereopantometer 
Phototheodolite Equipment 
Stereocomparator 
Stereoautograph 
Stereoplanigraph 
Sketch-master 
Rectifier 
Precision Coordinatograph 
Multiplex 
Levels Theodolites Tacheometers 
VEB CARL ZEISS JENA 
Representatives in all parts of the world