PRECEDENCE: ROUTINE
FROM: UKRAINE
TO: ALL STATES PARTIES
INFO:
SUBJECT: DESIGNATION/ADDITION OF AN OBSERVATION AIRCRAFT TYPE OR MODEL AND ITS INSTALLED SENSORS (ONE MESSAGE PER AIRCRAFT TYPE OR MODEL)
1. OS MESSAGE NUMBER: OS/UA/02/009/F08/0
2. OS MESSAGE DATE AND TIME: 281200ZFEB02
3. TREATY REFERENCE: ARTICLE V, PARAGRAPH 2; ANNEX C
4. MESSAGE REFERENCE: OS/UA/02/004/F08/0
5. CONTENT
A. IS THIS AN INITIAL DESIGNATION OR A CHANGE TO A DESIGNATION? (INITIAL/CHANGE) (IF IT IS A CHANGE, EXPLAIN THE CHANGE BRIEFLY IN THE REMARKS SECTION): INITIAL
(1) OS FORMATS 3, 4, 5, AND 6, AS APPLICABLE, HAVE BEEN COMPLETED AND SENT? (YES/NO): YES OS/UA/02/003/F03/0
B. INFORMATION ON DESIGNATED/ADDITIONAL OBSERVATION AIRCRAFT
(1) AIRCRAFT TYPE AND MODEL: AN-30B
C. MISSION PLAN DATA FOR EACH SENSOR CONFIGURATION
(1) FOR SENSORS WHOSE RESOLUTION IS DEPENDENT UPON ALTITUDE
SENSOR CONFIGURATION NUMBER
HEIGHT ABOVE GROUND LEVEL IN METRES AT WHICH AGREED GROUND RESOLUTION IS ACHIEVED
OPTIMUM CRUISING SPEED (TRUE AIR SPEED THAT PROVIDES MAXIMUM FLYING RANGE) AT ALTITUDE SPECIFIED ABOVE, IN KILOMETRES PER HOUR
FUEL CONSUMPTION AT OPTIMUM CRUISING SPEED AT ALTITUDE SPECIFIED ABOVE, IN KILOGRAMS PER HOUR
1073
385
995kg/godz
UA-OFBI-111V
2308
405
970kg/godz
D. NAVIGATION, COMMUNICATIONS, AND LANDING AIDS
(1) NAVIGATION EQUIPMENT INSTALLED, INCLUDING POSITIONAL ACCURACY
(a) TYPE OF EQUIPMENT: KS-6K
(i) POSITIONAL ACCURACY IN METRES: N/A
(b) TYPE OF EQUIPMENT: AP-28L1F
PITCH STABILITY IN DEGREES: 0.5
(i) POSITIONAL ACCURACY IN METRES: 20 (ALTITUDE)
(c) TYPE OF EQUIPMENT: ARK-11
HEADING ERROR IN DEGREES: 3
(d) TYPE OF EQUIPMENT: DISS-013-24FK
GROUNDSPEED ACCURACY IN PER CENT: 0.4
DRIFT ANGLE ACCURACY IN MINUTES: 20
(e) TYPE OF EQUIPMENT: “GROZA” M-30
SURVEILLANCE RANGE: 100-150 KM
(i) RANGING ERROR IN METRES: N/A
(f) TYPE OF EQUIPMENT: SO-72 + VEM – 72FG
(i) POSITIONAL ACCURACY IN METRES: 30
(g) TYPE OF EQUIPMENT: RV-18Zh
(i) POSITIONAL ACCURACY IN METRES:
25+0.02 (DIAL READOUT)
5 (DIGITAL READOUT)
(h) TYPE OF EQUIPMENT: RV-5M
(i) POSITIONAL ACCURACY IN METRES: 0.08
(i) TYPE OF EQUIPMENT: “VEYER – M”
(i) ALTITUDE-MEASURING ERROR IN METRES: 250±0.05%D
(MEASURING DISTANCE)
(j) TYPE OF EQUIPMENT: SD-75
200 (FROM 0 TO 20 KM)
400 (FROM 0 TO 569 KM)
(k) TYPE OF EQUIPMENT: GPS “GARMIN” 155
(i) POSITIONAL ACCURACY IN METRES: 5
(2) RADIO COMMUNICATIONS EQUIPMENT INSTALLED
(a) TYPE OF EQUIPMENT: R-863 (2 SETS)
(b) TYPE OF EQUIPMENT: “MIKRON”
(c) TYPE OF EQUIPMENT: SPU-7
(d) TYPE OF EQUIPMENT: SPU-8
(3) APPROACH AND LANDING EQUIPMENT INSTALLED
(a) TYPE OF EQUIPMENT: KURS-MP 70
(b) TYPE OF EQUIPMENT: VEM-72 FG
(c) TYPE OF EQUIPMENT: VMF-50 KG
(d) TYPE OF EQUIPMENT: VM-15 K
E. GROUND HANDLING
(1) DIMENSIONS OF THE AIRCRAFT IN METRES
(a) LENGTH: 24.26
(b) WINGSPAN: 29.2
(c) MAXIMUM HEIGHT: 8.32
(d) WHEEL BASE/TRACK WIDTH: 7.90/8.48
(e) TURNING RADIUS: 13
(2) WEIGHT OF THE AIRCRAFT IN KILOGRAMS
(a) MAXIMUM TAKE‑OFF WEIGHT: 23,000
(b) MAXIMUM LANDING WEIGHT: 23,000
(3) AIRFIELD RUNWAY LENGTH AND PAVEMENT STRENGTH REQUIRED AT MAXIMUM TAKE‑OFF AND LANDING WEIGHTS INCLUDING ANY CAPABILITY FOR LANDING ON UNPAVED STRIPS
(a) AIRFIELD RUNWAY LENGTH IN METRES REQUIRED AT
(i) MAXIMUM TAKEOFF WEIGHT: 1800
(ii) MAXIMUM LANDING WEIGHT: 1500
(b) PAVEMENT STRENGTH
(i) UNITS OF MEASUREMENT: kgf/cm²
(ii) REQUIRED AT MAXIMUM TAKEOFF WEIGHT: >0.8
(iii) REQUIRED AT MAXIMUM LANDING WEIGHT: >0.8
(c) CAPABLE OF LANDING ON UNPAVED STRIPS (YES/NO): YES
(4) CAPACITY AND TYPE OF
(a) FUEL:
(i) CAPACITY IN LITRES, IMPERIAL OR US GALLONS: 7100 L
(aa) TYPE OF FUEL: TS-1
(i) DENSITY OF FUEL IN WEIGHT PER VOLUME: 0.78 kg/L
(bb) TYPE OF FUEL: T-2
(cc) TYPE OF FUEL: T-1
(dd) TYPE OF FUEL: JET-A
(ee) TYPE OF FUEL: JET A-1
(b) OILS:
(i) CAPACITY IN LITRES: 124 (FOR TWO ENGINES)
(aa) TYPE OF OIL: 75% МК-8 (MK-8P) + 25% МS-20
(bb) TYPE OF OIL: 75% 1010 (TURBOOIL-3) + 25% 1100 (V/O)
(cc) TYPE OF OIL: 100% MN-7, 5U
(ii) CAPACITY IN LITRES: 6.5
(aa) TYPE OF OIL: МК-8 (MK-8P)
(bb) TYPE OF OIL: AEROSHELL
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