P-3 Numbers for website.txt

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scott.vanfleet
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151190
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P-3 Numbers for website.txt
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2012-04-30 16:26:11
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P-3 Numbers
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  1. Min air duct temperature (turbine howl)
    5 C
  2. Max time at full hot
    1 minute
  3. Max cabin temp
    27 C
  4. PPI drives to full hot max
    90 seconds
  5. Operate A.C. in manual if not stabalized
    30 minutes
  6. Max duct temperature (dehumidification)
    40 C
  7. Dehumidify if in high humidity for
    30 minutes or longer
  8. When dehumidifing, operate A.C. for
    15 minutes to stabalize temps
  9. Wing span
    99' 8"
  10. Length
    116' 10"
  11. Height
    34' 3"
  12. Electronic Bays on Starboard Side
    K F C
  13. Maneuver flaps
    275kts
  14. Takeoff/approach flaps
    190kts
  15. Land flaps
    170kts
  16. Gear extended
    300kts
  17. gear extension 1g
    300kts
  18. gear extension >1g
    190kts
  19. gear retraction
    190kts
  20. Landing lights
    260kts
  21. Bomb bay doors open
    Vne (limit dive speed)
  22. Overwing exit
    170kts
  23. Main cabin door
    300kts (max tested)
  24. APU door open
    225kts
  25. IRDS extended
    Vne (limit dive speed)
  26. IRDS extension/retraction
    375kts
  27. AIMS extended
    Vne (limit dive speed) (degraded above 350)
  28. AIMS extension/retraction
    350 kts
  29. Fuel dump airspeed
    140-300kts
  30. Air start minimums
    170kts min, 210kts range critical
  31. Air start maximum
    345kts - 6kts/1000ft
  32. Any internal store may be jettisoned
    180-330 knots in 1.0g level flight
  33. Max speed for buoy launch internally
    250 kts
  34. Any external store may be jettisioned
    180-200 kts
  35. Harpoon launch/jettison airspeeds
    200-350 launch. Max 350 jettison
  36. Maverick launch/jettison airspeeds
    180-Vne launch. 180-250 jettison
  37. Max cross wing component
    35 kts (max tested), 9deg AOB max at touchdown
  38. Cross wind landing speeds
    130kts until touchdown for >30kts x-wind, <15deg B
  39. Flap retraction speed
    140kts (160, 180 for heavy wt, turbulence, etc)
  40. Min speed during 2 engine approach
    1.35 + 5 not less than 145 kts
  41. Non-precison approach speed
    1.35 + 5 kts not less than 130kts
  42. AOA for 1.3, 1.35, 1.42. 1.52 speed/flap combination
    12 units
  43. Max range AOA
    9 units
  44. Loiter AOA - maneuver flaps
    9.8 units (square)
  45. Loiter AOA - clean
    10.5 units (triangle)
  46. Max endurance AOA
    12 units (amber donut)
  47. Pitchlocked prop fuel critical AOA
    12 units
  48. Min fuel flow AOA
    14 units
  49. Best Climb angle AOA
    14 units
  50. Ditching AOA
    15 units
  51. Max AOA for No-Flap
    15 units
  52. Stall recovery AOA
    16 units
  53. Stall buffet AOA
    19-22 units
  54. Stall AOA
    30 units
  55. APU operating increases AOA reading by
    1 unit (1/2 unit with just exhaust door open)
  56. Autopilot CWS - AOB held if released
    7-45degs
  57. Autopilot CWS - Pitch held if released
    0-25degs
  58. APU burn rate
    300pph
  59. APU Fire Warning Temp
    400 F
  60. GTCP95-2 Max Temp
    710C 10 sec, 715 c max peak
  61. GTCP95-2 Max continous
    688 C
  62. GTCP95-3 Max Temp
    704 C
  63. GTCP95-3 Max continous
    649 C
  64. GTCP95-10 Max continuous
    649 C
  65. GTCP95-10 Max 10 seconds
    710 C
  66. GTCP95-10 Max peak
    732 C
  67. APU RPM limits
    98-102% ground, 98-103% flight
  68. APU max RPM
    106%
  69. APU max altitude
    20,000ft
  70. APU max engine start altitude
    6,000ft
  71. APU type
    GTPC 95-2 -3 or -10
  72. Bomb bay can carry up to ____ weapons
    8
  73. Max reverse coordinator and blade angle
    0 and -13
  74. Ground Idle coordinator and blade angle
    9 and -6
  75. Ground Start coordinator and blade angle
    15 and 0
  76. Flight Idle coordinator and blade angle
    32 and 11 (beta followup) or 13 (low pitch stop)
  77. Pitchlock reset coordinator
    28 degs, reset to 109% RPM
  78. Inducing, Flight Idle stop and Prop Sync
    32 degs
  79. RPM autoshift
    36 degs
  80. Landing gear warning Coordinators
    48 and 60
  81. Autofeather Coordinator
    60 degs
  82. Temp limiting to temp controlling
    66 degs coord
  83. Fthr coordinator and blade angle
    110 and 86.65 deg
  84. Min crew rest for flights < 6 hours
    Eat and obtain 8 hours uninterrupted sleep
  85. Minimum crew rest for flight >6 hours
    12 hours
  86. Multiple flights crew rest
    12 hours for first 3 flights then 15 hours between
  87. Crew Day
    18 hours
  88. Max flight time with one FE
    6 hours, 8 if non-asw (VX-20 SOP)
  89. Max flight time with two pilots
    6 hours, 8 if non-asw (VX-20 SOP)
  90. Battery
    24v, 31amperhour
  91. AC Power
    120v, 400hz, 3 phase
  92. Generator power rating
    60kva ground, 90kva flight
  93. APU gen power rating
    90kva
  94. PMG
    39v, 600hz
  95. Undervoltage
    105v, 4sec
  96. Overvoltage
    129v, inverse time delay
  97. TR Overheat
    150 C
  98. Bus A cont
    Transfer Relay 2
  99. Bus B cont
    Transfer Relay 3
  100. Gen4 Transfer
    gen 4 cont aux, Transfer Rel 5+6
  101. Gen 4 aux cont
    Transfer Relay 7 - Gen 4 over APU
  102. External Power Cont
    Transfer Relay 4 - Ext power over APU
  103. Transformer rectifier rating
    28v 200Amp
  104. Min Recommend alt for bailout
    3000ft
  105. Placard Ditch speed is ____ kts above what speed
    10kts above land flap zero thrust stall buffet speed
  106. Portable O2 depletion during FOUO
    5-10 minutes
  107. Portable O2 depletion during transit
    22 minutes
  108. Flight Station O2 will supply O2 for
    3 1/2 hours at 25,000ft
  109. #1 Raft crew positions
    "P T IFT 8, 18, 19, 20"
  110. #2 Raft crew positions
    "CP N FE SS1 SS2 11,12, 13, 14, 16, 17"
  111. #3 Raft crew positions
    "SS3 15 21, 22, 23"
  112. Max reverse SHP 2&3
    1250 +-150
  113. Max reverse SHP 1&4
    1150 +- 150
  114. Engine Oil tank capacity
    8.65 gal usable (5.7 foaming space)
  115. Engine Oil system capacity
    15.75 gal
  116. Engine actual RPM @100%
    13820 RPM
  117. Prop actual RPM @ 100%
    1020 RPM
  118. Reduction Ratio of RGB
    13.54 to 1
  119. Compressor and Turbine Stages
    14 and 4
  120. Igniters located on Cans
    2 and 5
  121. Fire extinguisher bottle (engine)
    10.5 lbs at ~600psi
  122. Engine type
    T-56-A-14
  123. Max roll rate at ____ KIAS
    265kts
  124. Keep sideslip approximately zero above
    385kts
  125. "At high speed, aft c.g. make pitch inputs"
    2 seconds or longer to complete the input
  126. Landing gear warning
    "153+-3 / 48deg , 142+-3 / 60deg, land flaps"
  127. Stick force per g
    "80 lbs/g at 18% MAC, 20 lbs/g at 32% MAC."
  128. "2 Engine out at heavy gross weight, speed + AOB"
    1.52Vs and 20degs AOB or less toward failed eng
  129. Bomb bay effect on stick force per g
    reduced 10 lbs/g
  130. Wing Deice system check - note temp rise
    10 C
  131. Engine anti-ice SHP Drop and % fuel increase
    "9% drop in shp, 5% increase in FF to reset power"
  132. Fuel required for engine and wing anti/deice
    500pph increase
  133. LE Hot light
    110 C
  134. Wing Deice system use
    "look for 10 degree rise in LE temp, takes 20-30 sec "
  135. Icing conditions without operative emp deice - accel above
    200kts
  136. Windshiel heat warmup time in low
    10minutes
  137. Windsear criteria
    "+-15kts, +-500fpm"
  138. Windshear precautions
    "5-10kts faster, stabalized speed prior 1000ft"
  139. Turbulent air penetration speed (moderate - extreme)
    220 kts
  140. Turbulent air penetration speed (light-mod for crew comf)
    190 kts
  141. Carry 10kts extra speed - increase in landing distance
    1000ft
  142. Takeoff not recommended with ____ inches of snow
    5 in
  143. G limit in turbulent air
    2.0g
  144. Wind gust adjustment to approach and landing speeds
    "5-10kts faster, touchdown speed normal"
  145. Time for side windshield heat to become effective
    45 minutes
  146. Time to open bleed air or inducing valve
    8 seconds
  147. Fuel log required
    "500nmi from suitable, 6hours, or indicator failure "
  148. Fuel log entries
    "hourly or 5,000lb increments"
  149. Normal Crossfeed pressure from boost pump
    15-30psi
  150. Min fuel in tanks 2&3 for hyd cooling
    1000 lbs
  151. #1 and #1A Hyd lights on with gear retract
    5 Seconds max
  152. Charge accumulator will hold brakes for
    30 hours
  153. Fully charged accumulator will give ____ brake applications
    8
  154. Do not use landing lights without cooling air
    longer than 30 seconds
  155. Normal Descent
    "Flight Idle, 250-260 kts, 2000fpm"
  156. Start descent at what distance vs altitude
    2XALT + 10
  157. MOSA definition
    "1,000ft above the highest obstacle within 30nmi"
  158. Within MOSA - Nav fixes
    "DR every 15min, fix every 30 min"
  159. MOSA ICS updates
    "30, 25, 20, 15, 10, 9, 8 .... Nmi, or every DR and fix"
  160. Config D or E adjustment to approach speed
    700 drag count add 5KIAS to 1.35 and 1.3 Vs
  161. Maximum x-wind component tested
    35kts
  162. Outboard prop strike ground for
    bank angles in excess of 9 degrees @ touchdown
  163. Brake cooling airborne - delay retraction
    2 minutes
  164. Brake cooling while taxing - Ground START
    5 minutes
  165. Brake cooling while parked
    "1000shp, no minumum time"
  166. "During shiftdown, secure engine TIT/RPM"
    exceeds 850 C or drops below 71%
  167. turbine cooling and fuel nozzle coking due to soak - Low
    2 Minutes prior to shutdown
  168. Circling airspeed
    1.35 + 5 kts not less than 140kts
  169. Circling Cat D distance and obstacle clearance
    2.3 miles and 300ft
  170. When to set approach speed
    by the FAF or 3 nmi from field
  171. Use O2 prior to descent at night
    "15 min out of last 45min when cabin alt > 5,000ft"
  172. Max altitude for airstart JP-4
    "35,000ft"
  173. Max altitude for airstart JP-5 & 8
    "25,000ft"
  174. Max SHP transient
    >4600 for 3 sec
  175. TIT in low RPM
    410-730 C
  176. low RPM limits
    71-73.8%
  177. RGB Oil press in low RPM
    50-250 psig (except start + w/up)
  178. P/S oil press in low RPM
    "50-60 psig (if low, check at 100%)"
  179. Max P/S oil press during start + w/up
    100 psig
  180. "RGB Oil press start, reverse, flight idle"
    150-250 psig @ 100% RPM (w/up)
  181. RGB maximum fluctuations
    +-20 psi within 150-250
  182. P/S maximum oil press fluctuations
    +-5 psi within 50-60
  183. Fluctuating oil press following 0/neg G
    "15 seconds flux, only momentary 0"
  184. TIT at start position normal RPM
    445-645 C
  185. TIT at Max Reverse
    580-790 C
  186. TIT at Flight Idle
    430-705 C
  187. TIT at Max Power
    1077 (5 minutes max)
  188. TIT at Military Power
    1049 (30 minutes max)
  189. TIT at Max Cruise
    1010 C
  190. TIT max allowable overtemp
    1175 C for 5 seconds
  191. TIT Warning light
    1080 +-2 C
  192. RPM at start position
    96.3-99.1%
  193. RPM at Max Reverse
    96.7-104.9%
  194. RPM at Flight Idle
    94.5-98.4%
  195. RPM at max Power
    99-101
  196. RPM max overshoot/undershoot takeoff
    106-96% 10seconds
  197. PRM max overshoot/undershoot inflight
    "+-1% sync on, +-2% sync off 10sec"
  198. P/S oil press not in low RPM
    50-60 psig
  199. P/S and RGB oil press during start
    "positive by 35%, P/S 100psig max"
  200. Oil Temperature limits
    60-90 C
  201. Oil Temp extremely cold conditions
    "50-60 C, provided all oil press limits are maintained"
  202. Oil Temp for max power addition
    "40 C, RGB has no fluctuations"
  203. Max Oil Temp allowed
    "100 C 30min in beta, 5 min in alpha"
  204. Max time at zero or negative G
    10 seconds
  205. SHP with OIL Temp < 0 C
    minumum
  206. SHP with OIL Temp 0-40 C
    1000 shp max
  207. Floppover SHP
    5300 shp
  208. Normal Hydraulic Pressure
    2960-3200 psig
  209. TIT and RPM values on ground based on
    "no speed, no bleed, no accessory, temp -54 +55C"
  210. Overtemp During power change
    1083-1175 for more than 5 seconds or >1175 C
  211. max bank angle for rolling maneuver
    60 degrees
  212. Max bank angle for coordinated turn
    60 degrees
  213. "Max ZFW, no AFC 517"
    "80,400 lb (include stores on 12, 13, 14, 15)"
  214. "Max ZFW, with AFC 517"
    "82,400 lbs (include stores on 12, 13, 14 15)"
  215. Max ZFW increased by stores on stations
    "9, 10, 11, 16, 17, 18"
  216. g limit with ZFW exceeded
    2.1g
  217. Max differntial fuel/store loading takeoff
    "1400 1+4, 5025 for 2+3"
  218. Max differntial fuel/store loading land/inflight
    "4389 tanks 1+4, no restriction on 2+3"
  219. Max gross weight
    "135,000lbs"
  220. Max gross weight with CO permission
    "139,760 lbs"
  221. Max Landing weight
    "114,000 lbs"
  222. Record landings above
    "103,880 lbs"
  223. Minimum fuel in Tanks 1+4
    "based on gross weight, bagged out at 120k"
  224. fwd C.G. limit - gear down < 135K
    16-22.5% mac
  225. aft C.G limit - gear up or down < 135K
    29-32% mac
  226. Min Altitude w/ RADALT and RAWS
    200 Day/VMC 300 Night/IMC
  227. Min Altitude no RADALT or RAWS w/ updated Baro
    300 Day/VMC 500 Night/IMC
  228. Min Altitude no RADALT and no Baro update
    500 Day/VMC 1000 Night/IMC
  229. "NAVAIR: Airspeed GW < 125,000lbs"
    300 KIAS
  230. NAVAIR: Airspeed GW 125-135k
    "225 up to 15K, 235 to 20K, 245 to 25K, 255 above"
  231. NAVAIR: Airspeed GW 135-139760
    215 KIAS
  232. NAVAIR: Symetrical Flight G loading
    "0.0 G to 2.0 G > 125K, 2.5 G for <125K"
  233. Reverse thrust most effective above
    80kts
  234. Reverse thrust on snow can obscure vision
    below 50kts at high reverse power
  235. Ground Idle has ___% of max aerobraking
    90%
  236. Fight Idle thrust is positive below what speed
    80kts
  237. Climb schedule airpseed 4 engine
    "220 kts - 2/1000ft above 10,000ft "
  238. Climb 2000ft when TIT has reduced to
    "890 C no wind, 880 headwind, 900 tailwind"
  239. All rotation speeds are above Vmc air by a margin of
    5%
  240. Max range airspeed formula
    205 + 1/2 GW - Alt - 10kts/loitered engine
  241. Correction to TAS for winds
    + 30% headwind or - 25% tailwind (2/3 indicated)
  242. Notify crew on ascent above
    FL250 EEBDs readily available
  243. Pressurization formulas
    ALT-14 X 5 or 1/2 ALT - 7000
  244. Cabin Press Light on
    "10,000 +- 500ft"
  245. Isoberic range
    "0-13.3 "" Hg"
  246. Differential range
    13.3 - 13.9 in Hg
  247. Safety Relief range
    13.9 - 14.4 in Hg
  248. Fuel governor RPM
    104.2 -106.7 %
  249. Limit time on fuel topping gov
    1 minute
  250. Conditions for NTS check
    "8,000ft or less, 180+-10kts, 800 shp min"
  251. NTS SHP
    neg 150-500 (1&4) neg 100-500 (2&3)
  252. Min speed during NTS check
    1.52
  253. Pitchlock RPM
    103.5%
  254. "Pitchlock reset blade angle, coordinator, RPM"
    ">10deg BA, <28deg Coordinator, 109%"
  255. Prop pitchlock test switches reset governor to
    106%
  256. Secure generator above ___% RPM
    109%
  257. Pitchlock is cammed out
    Above 57 and below 17 degrees blade angle
  258. NTS check setup
    "180 +-10kts, <8,000ft, >800 SHP"
  259. NTS SHP
    #1&4 -150 to -500 #2&3 -100 to -500
  260. NTS is cammed out
    < 24 deg Coordinator
  261. Decoupler SHP Range
    -500 to -1700 SHP
  262. Limit time running Aux Pump (ie FTF)
    45 seconds
  263. Min RPM and airspeed for fuel chop of pitchlocked prop
    95% and 130kts
  264. Speed bias motor changes
    +- 2.5%
  265. Autofeather Priority
    4132
  266. Backup valve closes
    Less than 24 degs Blade Angle
  267. Backup valve opens
    <28� coordinator or >24� BA
  268. Low Pitch Stop
    13�
  269. Beta Followup
    11-22.5 � 68-88 coordinator
  270. Pitchlock
    103.5%
  271. Front spinners (amps)
    76-100
  272. Cuffs (amps)
    51-72 or ~60
  273. Aft spinners and islands
    63-82 or ~70
  274. Prop deice cycle time
    160 seconds (20 seconds each area)
  275. RAWS warnings
    "3 sec @ 380 +-20ft, continuous 170 +-10ft"
  276. RAWS warnings inhibited
    500-1000 ft above reference altitude (power on)
  277. RAWS breakers pulled for __ seconds @ ___ ft
    "10 seconds @ 4,000ft"
  278. PP1 may not extinguish when temp
    < -30 C OAT
  279. NTS Inop - blade angle cycle about
    45 deg
  280. PP1 should be out by ___% RPM inflight
    55%
  281. 210kts will exceed max allowable restart at
    "22,000ft "
  282. wait time to use dipstick
    3 minutes
  283. wait time to use dipstick - AFC 517
    15 minutes
  284. Min fuel for good dipstick reading
    "5,500 1&4 9,500 2&3 (30,000lbs)"
  285. Max refuel rate
    600 gallons per minute with 2 trucks
  286. Approximate refuel rate with one truck
    2000lbs/min
  287. Location and amount of min fuel in tank 5
    fuselage section with <4000lbs
  288. Min fuel loading in outboard tanks
    "0-40K, outboards should have at least 1/2 the fuel"
  289. Max refueling pressure
    55psi
  290. Total capacity of fuel tanks (gallons)
    1606 1671 2646 1671 1606 9200gal
  291. Primary fuels
    "JP-4, 5 and 8"
  292. Alternate fuels
    "Jet A-1, Jet A, Jet B"
  293. Emergency fuels
    "AVGAS 80, 100, 100LL"
  294. Tank 5 fuel verified with sight guage
    >4300 lbs
  295. Air starter unit min air ppm and pressure
    90 ppm @ 32psig
  296. Relative density of fuels least to most
    "JP-4, JP-8 then JP-5"
  297. Hearing damage w/out protecton dB
    140db
  298. Double hearing protection required dB
    104dB
  299. Refer unit min servicing
    3/4 sight glass
  300. Bomb bay emerg reservoir
    0.75 gal
  301. Head water breaker
    4.5 gal
  302. #1 Hydraulic reservoir qty (service)
    5.6 gal (4.8)
  303. #1 Hyd reservoir - accumulator charged qty (service)
    5.0 gal (4.2)
  304. #1 Hyd reservoir - gear up qty (service)
    4.0 gal (3.2)
  305. #2 Hyd reservoir qty (service)
    1.0 gal (0.75)
  306. Accumulator air charge
    800 psi
  307. Emergency Brake Pressure
    1900 - 3000 psig
  308. APU oil tank servicing required
    1/2 lower sight guage
  309. Air multiplier package servicing required
    1/2 on sight guage
  310. Cargo Loading LBS/Square Foot
    "60 lbs/sqft, no cargo in electronic bays."
  311. Max residual TIT for ground start
    200 C
  312. Max residual TIT for airstart
    150 C
  313. Max residual TIT for prime
    100 C
  314. "Hot start, discontinue, overtemp"
    "830 C, 850 C, 965 C"
  315. Cold Start Temps
    "<720 discontinue, 720 - 750 record and continue"
  316. Min oil temp for start
    -40 C (-54 C for -7808 oil)
  317. Fuel flow with prime used
    700-1200 pph then ~500 after 2 seconds
  318. Secure start if no lightoff by
    33% or max motoring
  319. Torch
    Discontinue - Overtemp inspection > 3 sec
  320. Pull Start button
    57-64 % RPM
  321. PRT-5 frequencies
    243 Mhz and 8.364 Mhz
  322. PRT-90 frequencies
    243 and 282.8 Mtz

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