Showing posts with label MD-80. Show all posts
Showing posts with label MD-80. Show all posts

BOEING AND AIRBUS WHEELS AND BRAKES FOR SALE - BIG SAVINGS


Monday, September 8, 2014


NEW GEN BOEING AIRCRAFT 737NG 767-WHEELS & BRAKES FOR SALE -AIRCRAFT ENGINE SPARES IN REPAIRED CONDITION WITH 8130-3 AND FULL TRACE DOCS -  CFM56-V2500 - PW4000 ENGINE MATERIAL FOR SALE 

3C AERO LLC SEPTEMBER SALES-NEXT GEN SPARES-ENGINE SPARES

737 WHEELS & BRAKES
C20637000  NOSE WHEELS QTY 2 EA OH 737NG MESSIER TAGS
2-1474-7     BRAKES 2 EA FRESH OH STOCK
3-1438         NOSE WHEELS QTY 6 EA AR
3-1438-1      NOSE WHEELS QTY 2 EA SV
AHA1290     NOSE WHEELS QTY 6 EA AR
2607825-2   NOSE WHEELS QTY 8 EA OH
2606671-2   MAIN WHEELS QTY 6 EA SV (HPT INSTALLED)
2612311-1   MAIN WHEELS QTY 7 EA AR COND
3-1559         NOSE WHEELS QTY 2 EA OH
2-1587-1      BRAKES QTY 4 EA AR COND

767 WHEELS & BRAKES
PN: 2608811-5 MAIN WHEELS QTY 50 EA AR COND
PN:2612412-1 BRAKES 60% LIFE AND BETTER


STOCK ON THE FOLLOWING BRAKE PARTS
357257                  661 ea   $37.00 ea                          
357286                  43 ea   $40.00 ea                              
357393                  169 ea $42.00 ea                             
357501                  56  ea  $49.00 ea                   
357503                  20 ea   $45.00.ea             
357505                  56 ea  $77.00 ea            


CFM56-V2500-PW4000-9D ENGINE MATERIAL FOR SALE

Engine ModelConditionMaterial PNMaterial DescriptionQTY
9DPW_UNSERV782714CHAMBER-COMBUSTION,O1
9DPW_NEW741055LOCK-NOZZLE STATOR19
9DPW_NEW746723P4PIN-SHOULDER,HEADLES1
9DPW_NEW770006SHIELD-HEAT,COMBUSTI1
9DPW_NEW802706GUIDE-NOZZLE STATOR1
9DPW_NEW802706GUIDE-NOZZLE STATOR1
9DPW_NEW808832LINER-CC,ASSY OF1
CFM56Overhauled1277M90G01SEAL-HPC STTR STG 38
CFM56Overhauled1285M67G03SEAL-STATIONA HPT INR1
CFM56Overhauled1476M26G01VANE ASSY-SECTOR STG63
CFM56Overhauled1476M26G02VANE ASSY-SECTOR STG62
CFM56Overhauled1476M26G04VANE ASSY-SECTOR STG62
CFM56Overhauled1476M27G01VANE ASSY-SECTOR STG75
CFM56Overhauled1476M27G02VANE ASSY-SECTOR STG72
CFM56Overhauled1476M27G03VANE ASSY-SECTOR STG71
CFM56Overhauled1476M28G01VANE ASSY-SECTOR STG86
CFM56Overhauled1476M28G03VANE ASSY-SECTOR STG81
CFM56Overhauled335-040-606-0SEAL-LPT STA AIR STG 42
CFM56Overhauled338-112-708-0Stg.2 LPT Seal Segment2
CFM56Overhauled338-112-709-0Stg.2 LPT Seal Segment1
CFM56Overhauled9526M64G17VANE ASSY-SECTOR STG43
CFM56Overhauled9526M65G18VANE ASSY-SECTOR STG51
CFM56Overhauled9526M65G20VANE ASSY-SECTOR STG53
CFM56OverhauledP201P15VANE-CPRSR STTR STG 11
CFM56OverhauledP223P02VANE-CPRSR STTR STG 31
CFM56OverhauledP223P04VANE-CPRSR STTR STG 32
CFM56OverhauledP246G04VANE-SECT HPC6-BOR1
CFM56OverhauledP247G03VANE-SECT HPC72
CFM56OverhauledP247G09VANE SECTOR-CPRSR STTR STG 72
CFM56OverhauledP258G03VANE ASSY-SECTOR STG81
CFM56PW_OVHL1316M84G01NUT2
CFM56PW_OVHL1316M84G01NUT2
CFM56PW_OVHL9945M19G03NUT-CCHMBR1
CFM56PW_NEW1275M27P04NOZZLE-SWIRL PRIMARY28
CFM56PW_NEW1275M27P04NOZZLE-SWIRL PRIMARY9
CFM56PW_NEW1275M27P04NOZZLE-SWIRL PRIMARY18
CFM56PW_NEW1275M27P04NOZZLE-SWIRL PRIMARY24
CFM56PW_NEW1275M27P09Nozzle, Swirl5
CFM56PW_NEW1275M27P09Nozzle, Swirl4
CFM56PW_NEW1561M47P02NUT49
CFM56PW_NEW1602M69G04LINER-OUTER COMB CHA0
CFM56PW_NEW1602M73P04LINER1
CFM56PW_NEW1755M32P01FLANGE7
CFM56PW_NEW1862M98P01DEFLECTOR20
CFM56PW_NEW1862M99P01SLEEVE23
CFM56PW_NEW1968M42G02LUG RING, OUTER LINE2
CFM56PW_NEW1968M50P02NOZZLE7
CFM56PW_NEW1968M50P02NOZZLE5
CFM56PW_NEW1968M51P01NOZZLE1
CFM56PW_NEW1968M51P01NOZZLE3
CFM56PW_NEW1968M51P01NOZZLE16
CFM56PW_NEW1968M59G01COWL-OUTER COMB1
CFM56PW_NEW2253M93P01NOZZLE1
CFM56PW_NEW2253M93P01NOZZLE40
CFM56PW_NEW2439M79P01Liner, Segment Combu0
CFM56PW_NEW9528M74P01RETAINER4
CFM56PW_NEW9528M75P01RETAINER4
CFM56PW_NEW9528M76P01SLEEVE2
CFM56PW_NEW9531M11G02COWL-INNER COMB3
CFM56PW_NEW9945M19G03NUT-CCHMBR5
CFM56PW_NEW9946M69P03RET-CCHMBR39
CFM56PW_NEW9968M26P02FERRULE2
CFM56PW_NEW9968M26P02FERRULE4
CFM56PW_NEW9968M26P02FERRULE2
CFM56PW_NEW9968M26P02FERRULE2
CFM56PW_NEWJ1051P03NUT-COMBCH27
CFM56PW_NEWJ643P05ABOLT ,MACHINE1
CFM56PW_NEWJ643P05ABOLT ,MACHINE32
CFM56PW_NEWJ643P05ABOLT ,MACHINE100
CFM56PW_NEWJA1275M27P04NOZZLE-SWIRL PRIMARY2
CFM56PW_OVHL1882M60G04MANIFOLD-FUEL INNER1
CFM56PW_OVHL1882M61G04Fuel Manifold (SAC)1
CFM56PW_OVHL1882M62G04MANIFOLD-FUEL OUTER1
CFM56PW_OVHL1882M63G04MANIFOLD-FUEL OUTER1
CFM56PW_OVHL1971M63G01MANIFOLD, FUEL1
CFM56PW_OVHL1971M63G02MANIFOLD, FUEL1
CFM56PW_OVHL337-116-101-0TUBE1
CFM56PW_OVHL338-118-602-0MANIFOLD-AIR1
CFM56PW_OVHL340-027-506-0MANIFOLD-LPT COOLING RH1
CFM56PW_OVHL340-027-507-0MANIFOLD-LPT COOLING RH1
CFM56PW_OVHL340-027-557-0MANIFOLD-LPT COOLING LH1
CFM56PW_OVHL340-027-603-0MANIFOLD-AIR1
CFM56-3PW_OVHL6840023M9NOZZLE-FUEL LARGE TI1
CFM56-3PW_OVHL6840023M9NOZZLE-FUEL LARGE TI1
CFM56-3PW_OVHL6840023M9NOZZLE-FUEL LARGE TI1
CFM56-3PW_OVHL6840023M9NOZZLE-FUEL LARGE TI1
CFM56-3PW_OVHL6840023M9NOZZLE-FUEL LARGE TI1
CFM56-3PW_OVHL6840023M9NOZZLE-FUEL LARGE TI1
CFM56-3PW_OVHL6840023M9NOZZLE-FUEL LARGE TI1
CFM56-3/-5PW_OVHL6840023E17NOZZLE-FUEL LARGE TI4
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI1
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI3
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI1
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI3
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI1
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI4
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI2
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI1
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI4
CFM56-3/-5/-7PW_OVHL6840023M1NOZZLE-FUEL LARGE TI2
CFM56-5/-7PW_OVHL6840023E18NOZZLE-FUEL LARGE TI1
CFM56-5/-7PW_OVHL6840023E18NOZZLE-FUEL LARGE TI1
CFM56-5/-7PW_OVHL6840023E18NOZZLE-FUEL LARGE TI1
CFM56-5/-7PW_OVHL6840023E18NOZZLE-FUEL LARGE TI1
CFM56-5/-7PW_OVHL6840023E18NOZZLE-FUEL LARGE TI13
JT8D-200PW_OVHL803619TUBE-#41/2&6BRG,ASSY OF1
JT8D-200PW_OVHL803619TUBE-#41/2&6BRG,ASSY OF1
JT9D-7R4E1PW_OVHL5006809-01TUBE-SENSING,VALVE,ASSY OF1
JT9D-7R4E1PW_OVHL5006811-01TUBE-SENSING,VALVE,ASSY OF1
JT9D-7R4E1PW_OVHL5007025-01TUBE-PS4,BL VAL CONT,ASSY OF1
JT9D-7R4E1PW_OVHL5007026-01TUBE-OIL,CSD COOLER,ASSY OF1
JT9D-7R4E1PW_OVHL655855TUBE-PRESSURE,ANGLE GEARBOX,ASSY OF1
JT9D-7R4E1PW_OVHL762623MANIFOLD-FUEL,PRIMARY,RIGHT,ASSY O1
JT9D-7R4E1PW_OVHL773842TUBE-FUEL SIGNAL,BLEED CYLINDER VA1
JT9D-7R4E1PW_OVHL791879HOSE & TUBE-AIR,TCC,ASSY OF1
P&WOverhauled733812JT9D RING-AIR SEALING,COMPRESSOR,5STAGE1
P&WOverhauled743485JT9D DUCT-COMPRESSOR,6STAGE,ASSY OF1
P&WOverhauled748717JT9D RING-AIR SEALING,COMPR,7STAGE,ASSY1
P&WOverhauled788281COMPRESSOR STATOR-11S,ASSY OF1
P&WOverhauled788282COMPRESSOR STATOR-12S,ASSY OF1
P&WOverhauled788284COMPRESSOR STATOR-14S,ASSY OF1
P&WOverhauled804883COMPRESSOR STATOR-13STG,ASSY OF1
P&WOverhauled807807JT9D DUCT-HPC,14STG,ASSY OF1
P&WOverhauled808155JT9D RING-AIR SEALING,HPC,6STG1
P&WOverhauled5005174-021JT9D, COMPRESSOR STATOR-14STG,ASSY OF1
P&WOverhauled807795M20JT9D DUCT-HPC,11STG,ASSY OF1
P&WOverhauled807797M20JT9D DUCT-HPC,13STG,ASSY OF1
P&WOverhauled807805M20JT9D-3/7, DUCT, C151
P&WOverhauled807807M20JT9D DUCT-HPC,14STG,ASSY OF1
P&WOverhauled809334STATJT9D-7Q HPT Compressor Stators Kit2
P&WOverhauled50B770SUPPORT-#1BRG SEAL,ASSY OF1
P&WOverhauled51D380BASE&VANE-FAN EXIT,ASSY OF11
P&WOverhauled51D390BASE & VANE ASSY OF-FAN EXIT2
P&WOverhauled51D766SUPPORT-#2BRG,ASSY OF2
P&WOverhauled54D280BASE&VANE ASSY OF-FAN EXIT6
P&WOverhauled54D380BASE & VANE ASSY OF-FAN EXIT1
P&WOverhauled54D390BASE&VANE ASSY OF-FAN EXIT5
P&WOverhauled54D910BASE&VANE ASSY OF-FAN EXIT1
P&WOverhauled50S157VANE-HIGH PRESSURE COMPRESSOR,7 STAGE25
PW2000PW_OVHL1A5345-01MANIFOLD-HYDRAULIC,AIR SOV,ASSY OF1
PW2000PW_OVHL1A7331-01MANIFOLD-CLG,#4BRG,ASSY OF1
PW2000PW_OVHL1A7356-01TUBE-RETURN,FUEL PUMP INLET,ASSY OF1
PW2000PW_OVHL1A7612-01MANIFOLD-SPY,FUEL NOZZLE,ASSY OF1
PW2000PW_OVHL1A7615-01MANIFOLD-SPY,FUEL NOZZLE,ASSY OF1
PW2000PW_OVHL1A7617-01MANIFOLD-SPY,FUEL NOZZLE,ASSY OF1
PW2000PW_OVHL1A7617-01MANIFOLD-SPY,FUEL NOZZLE,ASSY OF1
PW2000PW_OVHL1A8267-01MANIFOLD-HYDRAULIC,COMPR STATOR CYL,OPEN1
PW2000PW_OVHL1A9395-01TUBE-HYDRAULIC,AIR SOV,ASSY OF1
PW2000PW_OVHL1B0079-01TUBE-OIL AIR COOLER,ASSY OF1
PW2000PW_OVHL1B0109-01TUBE-PB,EEC,ASSY OF1
PW2000PW_OVHL1B0111-01TUBE-PT4.9,EEC,ASSY OF1
PW2000PW_OVHL1B0953-01MANIFOLD-HYDRAULIC BL VAL CYL,ASSY OF1
PW2000PW_OVHL1B1351-01TUBE-CLG,#4BRG,ASSY OF1
PW2000PW_OVHL1B1413-01TUBE-BL VAL CYL RETURN,ASSY OF1
PW2000PW_OVHL1B1605-01TUBE-SPY,#4&5BRG SCAV VAL,ASSY OF1
PW2000PW_OVHL1B1723-01MANIFOLD-PT4.9,ASSY OF1
PW2000PW_OVHL1B1936-01TUBE-CL OIL,IDGS AIR COOLER,ASSY OF1
PW2000PW_OVHL1B2147-01TUBE-BRTH,OIL TANK,ASSY OF1
PW2000PW_OVHL1B2147-01TUBE-BRTH,OIL TANK,ASSY OF1
PW2000PW_OVHL1B2231-01TUBE-FUEL OIL COOLER OUTLET,ASSY OF1
PW2000PW_OVHL1B2232-01MANIFOLD-FUEL OIL COOLER OUTLET, ASSY OF1
PW2000PW_OVHL1B2239-01TUBE-HYDRAULIC,AIR SOV,ASSY OF1
PW2000PW_OVHL1B2240-01TUBE-SPY,BL VAL,ASSY OF1
PW2000PW_OVHL1B2241-01TUBE-HYDRAULIC,AIR SOV,ASSY OF1
PW2000PW_OVHL1B2942-01TUBE-HYDRAULIC BL VAL CYL,ASSY OF1
PW2000PW_OVHL1B2964-01MANIFOLD-SCAV,#4BRG,ASSY OF1
PW2000PW_OVHL1B5433-01TUBE-COOLING,TCC ACTUATOR,ASSY OF1
PW4000PW_NEW_VEN221-0827-503Elbow AY-Regulated Pressure, ECS1
PW4000PW_OVHL221-4950-867TUBE (E1/PP)1
PW4000PW_OVHL50J959-01MANIFOLD ASSY OF-SPY,FUEL NOZZLE, FS01-F1
PW4000PW_OVHL50J959-01MANIFOLD ASSY OF-SPY,FUEL NOZZLE, FS01-F1
PW4000PW_OVHL50J959-01MANIFOLD ASSY OF-SPY,FUEL NOZZLE, FS01-F1
PW4000PW_OVHL50J959-01MANIFOLD ASSY OF-SPY,FUEL NOZZLE, FS01-F1
PW4000PW_OVHL50J959-01MANIFOLD ASSY OF-SPY,FUEL NOZZLE, FS01-F1
PW4000PW_OVHL50J959-01MANIFOLD ASSY OF-SPY,FUEL NOZZLE, FS01-F1
PW4000PW_OVHL50M154TUBE-A/O, OIL FEED, ELBOW1
PW4000PW_OVHL50T094MANIFOLD-CLG,TURB CASE,ASSY OF1
PW4000PW_OVHL50T095MANIFOLD-CLG,TURB CASE,ASSY OF1
PW4000PW_OVHL50U234-01TUBE ASSY OF-SENSING,EBU,AA861
PW4000PW_OVHL51T478MANIFOLD-HYDRAULIC1
PW4000PW_OVHL51T818TUBE-PB,EEC,ASSY OF1
PW4000PW_OVHL51U334-01TUBE ASSY OF-OIL COOLING,OUTLET (LS03)1
PW4000PW_OVHL51U350-01TUBE ASSY OF-SENSING,PT4.95 (AS66)1
PW4000PW_OVHL51U350-01TUBE ASSY OF-SENSING,PT4.95 (AS66)1
PW4000PW_OVHL51U930-01HOSE AND TUBE-SUPPLY,GRBX(CR10)1
PW4000PW_OVHL51U955-01BRACKET ASSY OF-HYDRAULIC FILTER1
PW4000PW_OVHL52T576-01TUBE-CLG,#3BRG,ASSY OF1
PW4000PW_OVHL52T622-01TUBE-SPY,BL VAL,ASSY OF1
PW4000PW_OVHL52T636-01TUBE-SIG,HPC DRUM AIR VAL,ASSY OF1
PW4000PW_OVHL52T783-01BRACKET-LOOP CLAMP,ASSY OF1
PW4000PW_OVHL53T003-01MANIFOLD-SPY,BL VAL,ASSY OF1
PW4000PW_OVHL53T194-01TUBE-SIG,HPC DRUM AIR VAL,ASSY OF1
PW4000PW_OVHL53T194-01TUBE-SIG,HPC DRUM AIR VAL,ASSY OF1
PW4000PW_OVHL56H104-101TUBE ASSY OF-BLEED,HPC,9STAGE24
PW4000PW_OVHL56T105-01MANIFOLD-COOLING,PMA,ASSY OF1
PW4000PW_OVHL56T647-01MANIFOLD-BRTHR,OIL TANK,ASSY OF1
PW4000PW_OVHL57T253-01TUBE-A/O,SENSING, EBU (AS121)1
PW4000PW_OVHL57T253-01TUBE-A/O,SENSING, EBU (AS121)1
PW4000PW_OVHL57T982-01MANIFOLD-PB,EEC,ASSY OF1
PW4000PW_OVHL58T270-01TUBE-SEN,PRESS REGULATING VAL,ASYO1
PW4000PW_OVHL58T687-01TUBE-SENSING,EBU,ASSY OF1
PW4000PW_OVHL58T850-001TUBE-SCAV,#4BRG,ASSY OF1
PW4000PW_OVHL59T071-01TUBE ASSY OF-DRAIN,DR561
PW4000PW_OVHL59T309-01TUBE ASSY OF-DRAIN,PMA,DR031
PW4000PW_OVHL59T326-01TUBE ASSY OF-SENSING,PB,AS931
PW4000PW_OVHL59T333-01TUBE ASSY OF-PRESSURE,IDG OIL,LS041
PW4000PW_OVHL59T806-01TUBE-SEN,HIGH PRESS SOV,ASSY OF1
PW4000PW_OVHL59T906-01MANIFOLD ASSY OF-SPY,TURB CLG AIR,AA401
PW4000PW_OVHL59T919-01BRACKET ASSY OF-LOOP CLAMP1
PW4000PW_NEW_VENAE2463533H0590HOSE ASSY-HYD (QPA-4)2
PW4000PW_OVHL51U969HOSE&TUBE-SCAVENGE,#4BRG,LUBE (LR05)1
PW4000PW_OVHL58T589HOSE-METAL,.5625-18X12.000,45&901
PW4000PW_OVHL59T180HOSE&TUBE-FUEL PUMP INLET,FM111
PW4000PW_OVHL59T484HOSE&TUBE-SCAVENGE,#4BRG,LR051
PW4000 94"PW_OVHL50K184SUPPORT ASSY-HPT,1ST1
PW4000 94"PW_NEW58H590BOLT-HIGH PRESSURE C9
PW4000 94"PW_NEWSR50K213-01CHAMBER ASSY OF-COMB1
V2500PW_OVHL2A1637-001NOZZLE&SUPPORT ASSY-1
V2500PW_OVHL2A2250NOZZLE&SUPPORT ASSY-1
V2500PW_OVHL2A2250NOZZLE&SUPPORT ASSY-6
V2500PW_OVHL2A3341GUIDE-FUEL NOZZLE4
V2500PW_OVHL2A3448NOZZLE&SUPPORT ASSY-1
V2500PW_OVHL2A3448NOZZLE&SUPPORT ASSY-1
V2500PW_OVHL2A3448NOZZLE&SUPPORT ASSY-1
V2500PW_OVHL2A3448NOZZLE&SUPPORT ASSY-1
V2500PW_OVHL2A3448NOZZLE&SUPPORT ASSY-5
V2500PW_OVHL2A3448NOZZLE&SUPPORT ASSY-3
V2500PW_OVHL2A3092-01TUBE ASSY OF-SCAVENGE,#5BRG1
V2500PW_OVHL5A1342TUBE,A/O OIL FEED1
V2500PW_OVHL5R8226TUBE A/O-NO.4 BRG. OIL WEEP LINE1
V2500PW_OVHL6A5012TUBE ASSY FUEL- HP SERVO RETR B.A.B.ACTR1
V2500PW_OVHL6A5025TUBE-FUEL-FLOWMETER TO SPLIT CONN-ASSY O1
V2500PW_OVHL6A5254TUBE, OIL, DIFFUSER TO STRUT N 9 -1
V2500PW_OVHL6A5311TUBE, ASSY OF1
V2500PW_OVHL6A6038TUBE A/O-OIL NO.5 BEARING D1
V2500PW_OVHL6A6484TUBE, ASSY OF-LP-FUEL-FCOC TO DIVERTER V1
V2500PW_OVHL740-5273-505TUBE ASSY,COOLING1
V2500PW_OVHL740-5692-507TUBE ASSY,DRAIN1
 
 CONTACT TIMKOHL@3CAERO.COM FOR DETAILS
Posted by No comments:
Labels: , , , , , , , , , , , , ,

MD80 SERIES AIRCRAFT APU FOR SALE GTCP85-98CKB GTCP85-98DCB GTCP85-98DCK GTCP85-98DHF GTCP85-98DHFA GTCP85-98DCA GTCP85-98CKD GTCP85-98D




AIRCRAFT AUXILIARY POWER UNITS 
FOR SALE


3C AERO LLC.  Is now supporting the MD80, MD82, MD83, MD87, MD88, MD90, and MD95 Series Aircraft.  3C Aero maintains a very large pool of MD80 series rotables in tagged SV serviceable and OH overhauled conditions and expendables in NS new surplus and FN factory new conditions.  We keep the rotables pool restocked with fresh tags 8130-3's and Dual Release EASA forms. We try and maintain stock on most of the high failure or critical items for the aircraft. 3C AERO's AOG (aircraft on the ground requirements) is always available for your support and can be reached at 

Email: marketing@3caero.com 
Phone: 1-405-466-5053


Because of the high demand and low supply for the APU's and Wheels and Brakes for the MD80 Series Aircraft. 3C Aero has purchased a large MD80 series inventory pool of Auxiliary Power Units for the MD80 series aircraft as well as the wheels and brakes. We are offering the APU's and Wheels and Brakes in both Overhauled and Serviceable conditions for outright sale.  The parts are tagged in SV and OH condition and in stock ready to ship. If you have any active requirements for spare parts or wheels brakes or APU''s contact us at marketing@3caero.com 

We are stocking most major components for the the McDonnell Douglas MD series aircraft including the McDonnell Douglas MD 81,  McDonnell Douglas MD 82,  McDonnell Douglas MD 83,  McDonnell Douglas MD 87, McDonnell Douglas MD 88 aircraft, McDonnell Douglas MD-90, and the McDonnell Douglas MD-95, or Boeing 717 aircraft. 


APU'S FOR SALE AND OR EXCHANGE 



DC8, DC9, MD-80, MD-81, MD-82, MD-83, MD-87, MD-88, MD-90, MD-95, AND BOEING 717 AIRCRAFT AUXILIARY POWER UNITS ( APU )FOR SALE   

  • MODEL NUMBER GTCP85-98CKB -  PART NUMBER 380678-3-1
  • MODEL NUMBER GTCP85-98DCB - PART NUMBER 3800368-1-1
  • MODEL NUMBER GTCP85-98DCK -  PART NUMBER 381015-1-2
  • MODEL NUMBER GTCP85-98DHF - PART NUMBER 381276-1
  • MODEL NUMBER GTCP85-98DHFB - PART NUMBER 381276-3
  • MODEL NUMBER GTCP85-98DHFA - PART NUMBER 381276-2
  • MODEL NUMBER GTCP85-98DCA - PART NUMBER 3800362-1
  • MODEL NUMBER GTCP85-98CKD - PART NUMBER 380678-5-1
  • MODEL NUMBER GTCP85-98D - PART NUMBER 380256-1-1




SOME SHARED EDUCATIONAL WIKI FACTS ARE BELOW:
MD-81 
The MD-81 (or as it was originally known the DC-9 Super 81 or DC-9-81) was the first production model of the MD-80, and apart from the MD-87, the differences between the various long body MD-80 variants is relatively minor. The four long body models (MD-81, MD-82, MD-83, and MD-88) only differ from each other in having different engine variants, fuel capacities, and weights. The MD-88 and later build versions of the other models have more up-to-date flight decks featuring for example EFIS.
MD-82
An Alitalia MD-82
Announced on April 16, 1979, the MD-82 (DC-9-82) was a new MD-80 variant with similar dimensions to those of the MD-81 but equipped with more powerful engines. The MD-82 was intended for operation from 'hot and high' airports but also offered greater payload/range when in use at 'standard' airfields. American Airlines is the world's largest operator of the MD-82, with at one point over 300 MD-82s in the fleet.
Originally certificated with 20,000 lbf (89 kN) thrust JT8D-217s, a -217A-powered MD-82 was certificated in mid-1982 and became available that year. The new version featured a higher MTOW (149,500 lb (67,800 kg)), while the JT8D-217As had a guaranteed take-off thrust at temperature of up to 29 degrees C or 5,000 ft (1,500 m) altitude. The JT8D-217C engines were also offered on the MD-82, giving improved sfc. Several operators took delivery of the -219-powered MD-82s, while Balair ordered its MD-82s powered by the lower-thrust -209 engine.[4][16]
The MD-82 features an increased standard MTOW initially to 147,000 lb (67,000 kg), and this was later increased to 149,500 lb (67,800 kg). Standard fuel capacity is the same as that of the MD-81, 5,840 US gal (22,100 l), and typical range with 155 passengers is 2,050 nautical miles (3,800 km).[4][16]




MD-83
The MD-83 (DC-9-83) is a longer range version of the basic MD-81/82 with higher weights, more powerful engines, and increased fuel capacity.
Powerplant: Compared to earlier models, the MD-83 is equipped with slightly more powerful 21,000 lbf (93 kN) thrust Pratt and Whitney JT8D-219s as standard.
Performance: The MD-83 features increased fuel capacity as standard (to 6,970 US gal (26,400 l)), which is carried in two 565 US gal (2,140 l) auxiliary tanks located fore and aft of the centre section. The aircraft also has higher operating weights, with MTOW increased to 160,000 lb (73,000 kg) and MLW to 139,500 lb (63,300 kg). Typical range for the MD-83 with 155 passengers is around 2,504 nautical miles (4,637 km). To cope with the higher operating weights, the MD-83 incorporates strengthened landing gear including new wheels, tires, and brakes, changes to the wing skins, front spar web and elevator spar cap, and strengthened floor beams and panels to carry the auxiliary fuel tanks. From MD-80 line number 1194, an MD-81 delivered in September 1985, it is understood that all MD-80s have the same basic wing structure and in theory could be converted to MD-83 standard.[4]
MD-87 
In January 1985 McDonnell Douglas announced that it was to produce a shorter fuselage MD-80 development aircraft, designated the MD-87 (DC-9-87), which would seat between 109 and 130 passengers depending upon configuration. The designation was intended to indicate its planned date of entry into service, 1987.
Dimensions: With an overall length of 130 feet 5 inches (39.75 m), the MD-87 is 17 feet 4 inches (5.28 m) shorter than the other MD-80s but is otherwise generally similar to them, employing the same engines, systems and flight deck. The MD-87 features modifications to its tail, with a fin extension above the tailplane. It also introduced a new low drag "beaver" tail cone, which became standard on all MD-80s.
Powerplant: The MD-87 was offered with either the 20,000 lbf (89 kN) thrust JT8D-217C or the 21,000 lbf (93 kN) thrust -219.
Performance: Two basic versions of the MD-87 were made available with either an MTOW of 140,000 lb (64,000 kg) and MLW of 128,000 lb (58,000 kg) or an MTOW of 149,000 lb (68,000 kg) and an MLW of 130,000 lb (59,000 kg). Fuel capacity is 5,840 US gallons (22,100 l), increasing to 6,970 US gallons (26,400 l) with the incorporation of two auxiliary fuel tanks. Typical range with 130 passengers, is 2,370 nautical miles (4,390 km) increasing to 2,900 nautical miles (5,400 km) with two auxiliary fuel tanks.
Cabin: The MD-87 provides typical mixed-class seating for 114 passengers or 130 in an all economy layout (five-abreast 31 in and 32 in seat pitch). The maximum seating, exit limited, is for 139 passengers.

MD-88
The MD-88 was the last variant of the MD-80, which was launched on January 23, 1986 on the back of orders and options from Delta Air Lines for a total of 80 aircraft.
The MD-88 is, depending on specification, basically similar to the MD-82 or MD-83 except that it incorporates an EFIS cockpit instead of the more traditional analog flight deck of the other MD-80s. Other changes incorporated into the MD-88 include a wind shear warning system and general updating of the cabin interior/trim. These detail changes are relatively minor and were written back as standard on the MD-82/83. The wind shear warning system was offered as a standard option on all other MD-80s and has been made available for retrofitting on earlier aircraft including the DC-9.
Delta's earlier delivered MD-82s were upgraded to MD-88 specification. When McDonnell Douglas was asked why these aircraft were MD-88s and not MD-82s they said that the customer, Delta Air Lines, thought that its specification was sufficiently different to warrant a new designation. Although delivered in December 1987, Delta put the aircraft into service only in January 1988.
Performance: The MD-88 has the same weights, range, and airfield performance as the other long-body aircraft (MD-82 and MD-83) and is powered by the same engines. MDC quotes a typical range for the MD-88 as 2,050 nautical miles (3,800 km) with 155 passengers. Range with 155 passenger is increased to 2,504 nautical miles (4,637 km) with two additional auxiliary fuel tanks (similar to the MD-83).
MD-80 Advanced
McDonnell Douglas revealed at the end of 1990 that it would be developing an MD-80 improvement package with the intent to offer beginning in early 1991 for delivery from mid-1993. The aircraft became known as the MD-80 Advanced. The main improvement was the installation of Pratt & Whitney JT8D-290 engines with a 1.5 in larger diameter fan and would, it was hoped, allow a 6 dB reduction in exterior noise.
Due to lack of market interest, McDonnell Douglas dropped its plans to offer the MD-80 Advanced during 1991. Then in 1993 a "mark 2" MD-80 Advanced version reappeared with the modified JT8D-290 engines as previously proposed. The company also evaluated the addition of winglets on the MD-80. In late 1993, Pratt & Whitney launched a modified version of the JT8D-200 series, the -218B, which was being offered for the DC-9X re-engining program, and was also evaluating the possibility of developing a new JT8D for possible retrofit on the MD-80. The engine would also be available on new build MD-80s.
The 18,000 lbf (80 kN) to 19,000 lbf (85 kN) thrust -218B engine version shares a 98% commonality with the existing engine, with changes designed to reduce NOx, improve durability, and reduce noise levels by 3 dB. The 218B could be certificated in early to mid-1996. The new engine, dubbed the "8000", was to feature a new fan of increased diameter (by 1.7 in), extended exhaust cone, a larger LP compressor, a new annular burner, and a new LP turbine and mixer. The initial thrust rating would be around 21,700 lbf (97 kN) thrust. A launch decision on the new engine was expected by mid-1994, but never occurred. The MD-80 Advanced was also to offer a new flight deck instrumentation package and a completely new passenger compartment design. These changes would be available by retrofit to existing MD-80s, and was forecast to enter service by July 1993.
The MD-80 Advanced was to incorporate the advanced flight deck of the MD-88, including a choice of reference systems, with an inertial reference system as standard fitting and optional attitude-heading equipment. It was to be equipped with an electronic flight instrument system (EFIS), an optional second flight management system (FMS), light emitting diode (LED) dot matrix electronic engine and system displays. A Honeywell windshear computer and provision for an optional traffic-alert and collision avoidance system (TCAS) were also to be included. A new interior would have a 12% increase in overhead baggage space and stowage compartment lights that come on when the door opens, as well as new video system featuring drop-down LCD monitors above.[5] The lack of market interest for the MD-80 Advanced during 1991 led McDonnell Douglas to drop its plans for the development. Derivatives The MD-90-30 is a stretched variant with updated glass cockpit and two V2500 engines, also Extended Range (ER) version as the MD-90-30ER. The MD-95 was developed as a replacement for the earlier DC-9-30, produced as the Boeing 717

  The McDonnell Douglas MD-80 series aircraft is a narrow body twin-engine, short- to medium-range, single-aisle commercial jet aircraft operated by leasing companies commercial aircraft freight companies and commercial airliners. The MD-80 series were lengthened, updated and modified from the older legacy DC-9 model aircraft. The airliner family can seat from 130 up to 172 passengers depending on variant and seating configuration. The MD-80 series was introduced into commercial operations and passenger service in 1980 by Swissair. 

The  McDonnell Douglas MD series includes the  McDonnell Douglas MD-81,  McDonnell Douglas MD-82,  McDonnell Douglas MD-83,  McDonnell Douglas MD-87, and  McDonnell Douglas MD-88 aircraft.  These all have the same fuselage length except the shortened MD-87. The MD-80 series was followed into service in modified form by the  McDonnell Douglas MD-90 in 1995 and the  McDonnell Douglas MD-95/Boeing 717 in 1999. 



GTCP85-98CKB GTCP85-98DCB GTCP85-98DCK GTCP85-98DHF 
GTCP85-98DHFA GTCP85-98DCA GTCP85-98CKD GTCP85-98D



Posted by No comments:
Labels: , , , , , , , , , , , , , , , , , , ,
Subscribe to: Posts (Atom)

3C MOST POPULAR PAGES

3C AERO LLC MONTHLY VIEWS