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The Snick Werks
Consolidated PBY-5A
Aircraft Specifications

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These are the most complete specifications we could find on the PBY-5A (and many on the 6A).  If you know of any information that is incorrect, or is missing, please contact me.  Needed most are weights of the sub assemblies (engines, wings, tail etc...).

Specification: PBY-5A PBY-6A
Wing span 104’ 0" 104’ 0"
Length (over-all) 63’ 10 7/16" 62’ 11" (63’ 6")
Height over Wing 13’ 5 ½"  
Height (on landing gear with propeller blade vertical at top) 21’ 01" (20’ 2") 20’ 01"
Height to top of rudder   22’ 04" (22’ 6")
Wings ------------------------- --------------------
Airfoil Section NACA 21 NACA 21
Chord at root 15’ 0"  
Chord at tip 10’ 0"  
Incidence 6 deg positive  
Dihedral (outer panel taper) 2 deg 20’  
Sweepback (at outer panel) 2 deg 58’  
Area (less ailerons) 1300 sq ft  
Ailerons (total) 100 sq ft  
Area (total) 1400 sq ft 1400 sq ft
Width of center section 42’ 0"  
Width of outer wing (start of dihedral) 31’ 0"  
Distance from tip of bow to leading edge of wing 16’ 11"  
Ailerons ------------------------- --------------------
Length 20’ 0"  
Width at wing tip 25.98"  
Width toward wing root 34.08"  
Wing Struts ------------------------- --------------------
Location 231" from tip of bow and 305" from tip of bow  
Stabilizer ------------------------- --------------------
Span 30’ 06" 30’ 06"
Maximum chord 8’ 0"  
Incidence 4 deg positive  
Area (including hull-fin area and 18.4 sqft of contained elevator balance) 138.2 sq ft  
Sweepback 10deg 50’  
Elevator ------------------------- --------------------
Elevators area (2, including tabs) 66.6 sq ft  
Elevator trim tabs area (total) 3.9 sq ft  
Elevator position (from rudder center) 2’ 4"  
Width 9’ 5 15/16"  
Depth to hinge 3’ 6 3/8"  
Total Depth 4’ 6 ½"  
Rudder ------------------------- --------------------
Fin 3.5 sq ft  
Rudder (including tabs) 40.4 sq ft  
Rudder trim tab 2.6 sq ft  
Hull ------------------------- --------------------
Width (Maximum) 10’ 2 ½"  
Height (Maximum) 8’ 0"  
Length 63’ 10 7/16"  
Wingtip Floats ------------------------- --------------------
Length 10’ 3 7/8"  
Tread (from keel to keel) 89’ 04" 89’ 04"
Landing Gear ------------------------- --------------------
Tread (from center of tire to center of tire) 16’ 09" 16’ 09"
Center of nose gear to center of main gear 17’ ¾" 17’ ¾"
Nose gear tire

?

30x8
Main gear tire

?

47x10
Gear strength

?

 
Propeller ------------------------- --------------------
Type Hamilton Std Hamilton Std
Blade Des No 6353A-12 6353A-12
Aspect Ratio 7.7 7.7
Diameter (greatest distance) 12’ 01" 12’ 01"
Min/Max pitch

?

 
Weights and Loading    
Empty Weight 20,910 lbs 21,000 lbs
Maximum all-up weight 35,420 lbs 34,450 lbs
Wing loading 24.3 lbs per sq ft  
Power loading 14.7 lbs per hp  
Fuel 712/513 (US) galls per lb  
Engine weight ?  
Wing Outer ?  
Wing Center ?  
Vertical Stab. ?  
Horiz. Stab. ?  
Landing Gear ?  
Float

?

 
C of G Limits 27,880 lbs AUW  
Forward CG limit 22.9% MAC (242.2 ins)  
Aft CG limit 28.5% MAC (251.5 ins)  
Datum 3 inches aft of bow nose  
Engine ------------------------- --------------------
Type 2 P&W R-1830-92 Radials

twin row 14 cylinder

2 P&W R-1830-92 Radials

twin row 14 cylinder

Horsepower (each engine) 1,200 hp @ 2,700 rpm 1,200 hp @ 2,700 rpm
Location 6’ 11" from fuselage center to engine center  
Depth from center of propeller to leading edge of wing 5’ 2"  
Performance ------------------------- --------------------
Max Speed 179 mph 178 mph @ 7,000 ft
Cruising speed 125 mph 113 mph
Rate of climb 620 ft per min  
Range (cruising) (cruising) 17 hrs  
Range (miles) 2,350 miles 2,535 miles
Service Ceiling 13,000 ft 16,200 ft
Fuel ------------------------- --------------------
Capacity 825 gal/wing  
Tank location(s) 2 mid wing over fuselage

(both unsealed and self sealing)

65 gallon sump in engine nacelle

 
Weapons ------------------------- --------------------
  1 - .50 Caliber in each bubble  (2 total)

2 - .30 Caliber in bow

1 - .30 Caliber in ventral

5 - .50 Caliber Machine Guns

(There were also interesting field modifications like a quad 5 in the nose or twin 20mm cannon in addition to existing guns)

  4 – 325 lb Depth Charges>
or 2 – Mark XIII Torpedoes or

4 – 500 or 1000 lb Bombs or

24 - Retro firing ASW rockets

(Basically up to 4000 lbs of ordinance)

4 – 325 lb Depth Charges or 2 – Mark XIII Torpedoes or

4 – 500 or 1000 lb Bombs

(Basically up to 4000 lbs of bombs)

Speed Limits ------------------------- --------------------
Never exceed speed (Vne) 199 mph  
Structural cruising speed (Vc) 158 mph  
Maximum Float Operating Speed 150 mph  
Maximum gear lowering speed 140 mph  
Maximum with gear extended 160 mph  
Maneuvering speed (Vp) 122 mph  
Minimum speed at which airplane is controllable in flight with one engine inoperative, its propeller windmilling, floats and gear up, other engine at T/O power 96 mph  
Stalling speeds 27,880 lbs AUW  
Aircraft clean, throttles closed 73 mph  
Gear down, 2300 RPM 12 in boost 63 mph  
Floats down, 2300 RPM 12 in boost 66 mph  
General Operation Speeds ------------------------- --------------------
V1 – Decision speed 75 mph  
Vmca – Minimum control speed in flight 98 mph  
Vs – Stall speed clean 73 mph  
Vmu – Minimum unstick speed 81 mph  
V2min – Minimum take-off safety speed 75 mph  
V2 – Initial climb out speed 104 mph  
Best water takeoff speed 75-81 mph  
Best land takeoff speed 86 mph  
Best turbulence speed 122 mph  
Diving ------------------------- --------------------
G- limit 3 g at 27,000 lbs  
I would like to thank Michael "Mad" Moe for the amazing amount of data he has collected.  I know of no other place on the web where so much detailed information on the PBY has been pulled together.