Aircraft MD-83 YOM 1990, 165 Pax configuration

Technical specification 
28.10 2015
                   
Aircraft Description DC-9-83 (MD-83)
Manufacture date 19. oktober 1990
Total flight hours 59 453 Hours
Total flight cycles 28 760 Cycles
Configuration 165 pax
                   
Design Weights
Date of last weighing 13. Mar 2015
Empty weight   84 205 lb
CG(inch)     942,93 in
MTOM     72575 kg
MZFM     55.338    kg
                   
Engines TBO: OC Hrs OH OC Hrs HSI
ENGINE LH ENGINE RH
Type JT8D-219   Type JT8D-219  
S/N 717886   S/N 725918  
TSN 49 051 Hrs TSN 46 429 Hrs
CSN 29 294 Cyc CSN 24 128 Cyc
TSO 5 155 Hrs TSO 218 Hrs
Most limited LLP 1 651 Cyc Most limited LLP 2 734 Cyc
33 147        
APU OC  Hrs
P/N:  381276-1
S/N: P-1079
Type GTCP85-98DHF
TSN 34 655 FH 
Date last inspection 07. Mar. 2008
Time since last Insp.   15 585 Hrs
Cycles since last Insp.  17 915 Hrs
                   
Landing gear CBO: 20 000 Cyc. 10 YE
Left body Right body Nose
P/N 5930999-5001 5930999-5002 5940337-5001
S/N CPT1129 CPT0575 CPI569
CSO          (Cycles) 384 4 031 5 266
Date of last OH 21. august 2014 10. juni 2009 7. juli 2006
Date of next OH 18. august 2024 8. juni 2019 4. juli 2016
REMAINING Cycles 19 616 15 969 14 734
                   
Equipment:
Avionic type Manufactor Model Qty
Autoflight CAT III              
Digital Flight Guidence Computer HONEYWELL 4034241-971 1 ea
FLIGHT MODE ANNUNCIATOR HONEYWELL 4034234-902 1 ea  
                 
Navigation Systems      
Air Data Computer   ADC HONEYWELL HG280D80 2 ea
ADF System Bendix/King 2041168-7501 2 ea
ATC COLLINS XS-950 2 ea
DME COLLINS 622-7309-101 2ea
EGPWS/TAWS HONEYWELL MK VII 1 ea
EFIS Computer SGU HONEYWELL 965-0449-002 2ea
EFIS DISPLAY HONEYWELL 4056510-903 4 ea
FMS COMP Canadian Marconi 100-601900-202 2 ea
FMS MCDU Canadian Marconi 100601-702-002  2 ea
GPS Receiver     Canadian Marconi CMA-900 2 ea
Marker Receiver          Bendix/King   MKA-28C 1 ea
RADIO ALTIMETER  T/R COLLINS 622-3890-014 2 ea
TCAS COLLINS TTR-920 1 ea
TCAS PROCESSOR Allied Signal 066-50000-2120 1 ea
VHF NAV HONEYWELL RNA-34A 2 ea
Weather Radar System Bendix RTA-4A 1 ea
Windshear HONEYWELL 4059845-911 1 ea
Communication Systems      
VHF COM Allied Signal RTA-83A 2 ea
HF COM # 1     COLLINS 622-3371-001 1 ea
HF COM # 2     COLLINS 522-1501-000 1 ea
VHF Audio Control Panel GABLES G7406-12 4 ea
P.A. AMPLIFIER COLLINS 622-4096-001 2 ea
INDICATING/RECORDING      
CVR       L-3 COMM 93-A100-80 1 ea
SDFDR Allied Signal 980-4100-DXUN 1 ea
QUICK ACCESS RECORDER L-3 COMM ATL0000-10 1 ea
FDAU       HAMILTON STANDARD ED742951-9 1 ea
ELT KANNAD 406AS   2ea
 Hours Cycles Month
MAJOR CHECKS Performed Next due Remaining Performed Next due Remaining Performed Next due Remaining days
A-check 59 370 60 020 567       14.8 2015 10.2 2016 105
2A-check 59 370 60 670 1 217       14.8 2015 13.8 2016 290
4A-check 58 130 60 730 1 277       19.9 2013 19.9 2015 -39
                   
C-check 58 130 60 730 1 277       19.9 2013 19.9 2015 -39
2C-check 56 223 61 423 1 970       9.3 2012 8.3 2016 132
3C-check 53 549 61 349 1 896       11.10 2009 10.10 2015 -18
4C-check 53 549 63 949 4 496       11.10 2009 9.10 2017 712
5C-check 53 549 66 549 7 096       11.10 2009 9.10 2019 1442
6C-check 53 549 69 149 9 696       11.10 2009 8.10 2021 2172
8C-check 53 549 74 349 14 896       11.10 2009 7.10 2025 3632
                   
3YE-check             9.11 2012 9.11 2015 12
4YE-check             1.9 2013 31.8 2017 673
5YE-check             1.9 2013 31.8 2018 1038
6YE-check             11.10 2009 10.10 2015 -18
8YE-check             10.11 2009 8.11 2017 742
10YE-check             11.10 2009 9.10 2019 1442
Implemented Supplemental Type Certificates OY-RUE MSN 49936:
L3 Communication Quick access recorder (QAR) Minor STC: ATL MOD-11062-001
Geven seats Minor STC: AERO TECHNICS DESIGN ATD0434
Lufthansa Guideline floor path marking system STC: EASA.A.S.01647
Honeywell TICAS II STC: EASA.IM.A.S.01625
Honeywell solid state flight data recorder STC: EASA.IM.A.S.02013
JET Engineering Turbine exhaust cone mixer STC: EASA.IM.E.S.01012
JET Engineering Advanced jet nozzle STC: EASA.IM.A.S.02331
Alliedsignal (Honeywell) EGPWS STC: EASA.IM.A.S.01776
The Mexmill Company Insulation blankets STC: ST01052LA
The Mexmill Company RTA-83A VHF COMM System STC: ST01828AT
C&D Zodiac Reinforced cockpit door STC: CAA.21NE1.00014
EJM Aerospace Services Dual Marconi CMA-900 FMS STC: ST01532AT
NavAero T-bag C2 Electronic flight bag STC: EASA.IM.A.S. 03005
General aircraft description:
Aircraft for pax only
Interior:
Seats: Geven DIVA model seats
Galleys: 3 ea FWD: G1, G2, G5
Lavatories: 3 ea FWD: L1 AFT: L2, L3 
Other aircraft data:
Wing span: 108 ft / 32,85 m
Length: 130 ft / 36,30 m
Height:   30 ft /   9,36 m
Max pay load: 165 Y seats hand luggage 5 kg check in 20 kg
Range at max payload: 4.395 km / 2.373 NM
Cruising speed: 811 kph / 437 kts/ 815 kmt/ 504 mph
MAX Altitude 10.668 m / 35.000 ft
Cargo FWD door 1.32 m x 1.34 m Hold: 4.80 L x 0.96 H x 2,0 B
Cargo MID door 1.32 m x 1.34 m Hold: 6.56 L x 0.96 H x 2,0 B
Cargo AFT door 1.29 m x 0.91 m Hold: 5.53 L x 0.96 H x 2,0 B
Volume cargo : 32,43 m³
Main door FWD dim: 0,88 m x 1,82 m
Pax door aft: 0.70 m x 1,82 m
  NOISE CERTIFICATION STANDARD        
Stage 4
         Lateral / Full-Power   Approach   Flyover  
Noise Level (EPNdb)   94.9   93.3   86.4  
Noise Limit (EPNdb)   96.4   100.2   91.0  
Margin       (EPNdb)   1.5   6.9   4.6  
Cumulative Margin (EPNdb) 13.0  
  ENGINE EXHAUST EMISSIONS        
ENGINE IDENTIFICATION: JT8D-219
MODE POWER SETTING  TIME         minuttes FUEL FLOW  kg/s EMISSIONS INDICES g/kg SMOKE NUMBER
        HC CO Nox  
TAKE-OFF 100 0.7 1 354 0 0.42 18.72 6.9
CLIMB OUT 85 2.2 1 085 0 0.46 13.73 -
APPROACH 30 4.0 0.3817 0 3.57 7.65 -
IDLE 7 26.0 0.1344 0 17.19  4.16 -
LTO TOTAL FUEL (kg) OR EMISSIONS (g) 501 0 4021 4604 -

 

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Пн 07.12.2015 8:20