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SUDAN AIRWAYS CO.

MAINTENANCE & ENGINEERING

PLANNING & ENGG. SERVICES

TECHN. RECORDS SECTION

DATE: 08-07-2015

SUBJ.: A/C ST-ASF

A/C SPECIFICATIONS

1/ A/C TYPE : F25 MK 050

A/C REG. : ST-ASF

DATE OF MANUF.: 24/04/1989

A/C S/NO. “MSN” : 20155

ENG. TYPE : P & W 125B

PROP. TYPE : R352/6-123/F/2

2/ A/F DATA:-

TOTAL A/F HRS SINCE NEW : 26177

TOTAL CYCLES SINCE NEW : 26656

C OF A EXPIRED

RAD.LIC. EXPIRED

COMPASS SW. EXPIRED

W&P EXPIRED .

3/ A/C CHECK CYCLES:-

A. INSP. EVERY 200 FH ( UP TO A19 )

CKK.C. EVERY 4000 FH ( UP TO C3 )

D1. EVERY 6 YRS

D2. EVERY 12 YRS. (MAJOR)

4/ LAST CHECKS ACCOMPLISHED:-

A/ A/C UNDER CHK. A3+C3+CHK.D2 (MAJOR CHK.)

B/ LAST D1. CHK C/OUT ON 16/11/05 .

C/ LAST D2. CHK. C/OUT ON 05/05/01/ NXT.D2 DUE ON 04/05/013 (expired).

5/ MLG & NLG STATUS

DESC. / P/N. / S/NO. / POS / REM.LIFE / REMARKS
MLG LEG / 201020001 / TO BE ADVISED
MLG LEG / 201020001 / TO BE ADVISED
NLG / 201013001 / TO BE ADVISED

6/ ENGINE DATA:-

TBO : C/M

ENG. S/NO. /

POS

/ E. T. T. &
E. T. C. / T. S. O. &
C. S. O. / T. S. H. S. I. &
C. S. H. S. I. / FIRST LIMIT REM.
TO BE ADVISED / L/H
TO BE ADVISED / R/H

7/ PROP. DATA:-

O/H EVERY : 7500 FH

PROP S/№ / POS / T.T.S.N. / T.T.S.O.
TO BE ADVISED
TO BE ADVISED

8/ A/C AVIONICS

ATA Description QTY Manufacturer Model Part number

22 AUTO FLIGHT

22-22 Stabilizer Augmentation Computer 1 Honeywell/Sperry SZ-601700-4 187-903

23 COMMUNICATIONS

23-11 HF Communication 1 full provisions for

23-12 VHF Communication 2 Collins VHF-22C 822-1113-001

23-31 Audio Accessory Unit 1 Fokker F7941-024-417

23-31 Passenger Address System 1 Collins 346D-2B 622-4096-001

23-71 Cockpit Voice Recorder (+ ULB) 1 Fairchild 93A100-80

24 ELECTRICAL POWER

24-22 Generator Control Unit 2 Sundstrand 737854D

24-40 Ground Power Control Unit 1 Sundstrand 738061

25 ELT 1 Elta ADT406AP 01N65910

31 INDICATING/RECORDING

31-31 Flight Data Acquisition Unit 1 Teledyne 70-251J222-9765-2-C1

31-31 Digital Flight Data Recorder (+ ULB) 1 Fairchild 980-4100-DXUN

31-35 Integrated Alerting Unit 1 Grimes 80-0590-3-5

32 LANDING GEAR

32-42 Skid Control Box 1 ABS 6004125-2

33 LIGHTS

33-10 Overhead Dimming Unit 1 Fokker EAODS8416-412

34 NAVIGATION

34-00 GNS/XLS System 1 AlliedSignal 17960-0102-0012

34-12 Air Data Computer 1 Honeywell/SperryAZ-8007000700-933

34-20 Attitude and Heading Reference System 2 LittonLTR-81-01 460800-33-31

34-22 EFIS – Symbol Generator 2 Honeywell-Sperry SG-806701-3788-808/807

34-23 Standby Magnetic Compass 1 Smiths Industries KCA0106W

34-25 Flight Director Computer 2 Honeywell/Sperry FZ-5004018369-905

34-26 EFIS – Control Panel 2 Sperry Primus 7012977-757

34-26 Flight Mode Panel 1 Sperry Primus 7009750-913

34-43 Weather Radar System 1 Sperry Primus P6507008470-812

34-46 EGPWS 1 Honeywell MKVIII 965-1216-008

34-46 TCAS Computer 1 Honeywell 7517900-55003

34-46 TCAS Mode S Transponder 2 Honeywell 7510700-850

34-51 VHF Navigation 2 Bendix/King VN-411B066-1101-31

34-55 Distance Measuring Equipment 2 Bendix/King DM-411B066-1107-00

34-57 Automatic Direction Finder 2 Bendix/King DF-431066-1105-00

34-60 Instrument Switching Unit 1 Fokker F7981-108-433

BASHIR YAGOUB

HEAD OF TECHN. RECORDS