By Ray Wagner
;North American Sabre Jet F-86D/K/L half One: layout / constitution / checking out (Air strength Legends quantity 202) ВОЕННАЯ ИСТОРИЯ,ТЕХНИКА Название: North American Sabre Jet F-86D/K/L half One: layout / constitution / checking out (Air strength Legends quantity 202)Автор: Ray WagnerИздательство: Ginter BooksISBN: 094261299XГод: 1999Страниц: 100Формат: PDF в RARРазмер: 124.55МБЯзык: английскийThe value of this unmarried seat all-weather bomber/interceptor has been continually overshadowed through the Korean battle classic F-86A/E/F sequence of day opponents. construction of F-86D's on my own accounted for 2,506 plane. even if un-glamorous in comparison to its day fighter brother, the "Dog" was once accountable for numerous global pace files. This publication covers each element of F-86D/K and L layout, constitution and checking out and so on. It manages to hide many rarely-seen developmental elements, and brings jointly loads of new images. additionally an exceptional modelling spouse, it has a excessive variety of Tech Order extracts and element images. Скачать: DepositfilesUploading Hotfile zero
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Extra info for North American Sabre Jet F-86D/K/L Part One: Design / Structure / Testing (Air Force Legends Number 202)
5rE') Or PHASE:) 4~ PILOT:S ACTION: AFTER LOCK-ON IS ACCOMPLISHED, THE PI-lASE I DISPLAY APPEARS ON SCOPE. RANGF C\DSUAE RATE. KNOTS HAAO STEERING SHRINKING. iNOICATING T,M€. "".... S""~) ~NDICATES m TI"'IO:. fltGe:T ON RANGE G"TE P~ASE SEt:. TIME TO IMPACT l£5S T"'AN 4~ SEC. m IN PHASE THE PILOT IMIN1A1NS WINGS ABOUT LEVE L AND STEERS IN ElEVATiON ONLY. THE POD LOWER 5 AND THE. D AU1'OMATICALLY. NALAPPEAR5 ON TI-4E SCPPI:. R FIRE . ION S LOCK· ON 53 LOCI\-ON I ROCKET RH MAIN RELAY P A N E l - - - - - - - - - - - - , SYSTEM L\RMING (ARM GS-I nmOUGH ARM GS-8), SEQUENCE CONrnOL (ARM FI nmOUGH ARM F1), TRJGGItR CONrnOL (ARM FT2-1 nmOUGH ARM FT2-4), AUTO EXTEND (ARM A), AUTO RETRACT (ARM S24), AND FIRE CONrnOL (ARM FT3) RELA YS] ENGINE SECTION ACCESS DOOR RELAY PANEL (NOSE STEER" RX CONTROL CIRCUIT BREAKER) INTERVAlOMETERPROTECTING RESISTOR RH CIRCUIT-BREAKER P A N E l - - - - -....
LANDING GEAR EMERGENCY RELEASE HANDLE 10. 11. 2) 12. VOLTMETER CONTROL PANEL -Som. , (,•• applicabl. -. tAP BelT INrnA TOR HOSE" * SHOULDER HARNESS MAINTENANCE SAFETY PINS ~. MAINTENANCE SAFETY PIN M-4 tAP BELT m/""" D£1AY •• • • tAP SELT INITIATOR FIRING LEVER / /. -_ .. _. -ll-03-1111 BRAKE SPEED • GLT UNDERSIDE DOOR HING~F \ PILOT'S STEP 41 J47-GE-17, -178, OR -33 ENGINE The Model J47-GE-17, -17B (F-86D-45 airplanes 52-3898 through 52-4135) or -33 (F-86D45 airplanes 52-4136 and all later versions) turbojet engine was characterized by an afterburner and a variable-area jet nozzle (clamshell).
At 15% and 8" aft in line 45° down and aft. 0:35 0:45 0:15 0:20 0:30 0:35 0:30 0:15 0:20 0:10 0:15 0:30 0:30 0:30 0:30 0:30 The radar nose on the F-86D caused stability problems with the original tail design, and many fixes were tried, primarily on 50-455 & 50-457. The YF-86D, 5Q-577, also tested a completely new tail that greatly resembled future F-100 tails. 44 At top, 4° expansion cone aspirator as tested on flight 39. Above, original F-86D tail on 50-455 with tufts installed after flight #8 on 6-27-51.
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