N15MA - 1943 DOUGLAS DC 3/C 47

1943

DOUGLAS

DC-3/C-47

19286

N15MA

Used

IFR

Working DC-3 on a part 135 Certificate

28621.0

P&W 1830-92 Date: 2/6/2012 2/6/2012 Aircraft 28,625.8 Engine #1 TSO: 564.5 P&W 1830-92 Spec-TC-5E4 S/N BP-457816 Engine #2 TSO: 203.9 P&W 1830-92 Spec-TC-5E4 S/N 145985 Propeller #1 TSO: 1,590.1 L Prop Gov. TSO: 195.8 Prop Hamilton Standard 23E50 S/N P5331 Propeller #2 TSO: 1,590.1 R Prop Gov. TSO: 1,068.7 Prop Hamilton Standard 23E50 S/N 12032

Hamilton Standard 23E50 TBO C/W DUE Hours Days Hours Date Hours Days Left Engine 1600 28,061.3 1,035.5 Right Engine 1600 28,421.9 1,396.1 Left Propeller 1600 28,621.2 1,595.4 LH PROP. TTSN: 10,390.1 Right Propeller 1600 28,621.2 1,595.4 RH PROP TTSN: 11,840.1 Left Prop Gov. 1600 28,430.0 1,404.2 Right Prop Gov. 1600 27,557.1 531.3

Cargo Configuration

3

Type of Inspection Frequency Last Done Remaining Due Date Hours Days Hours Days Hours Days 10 day Inspection 10 2/6/2012 10 2/16/2012 50 Hour Service Check 50 28,588.9 13.1 #1 Airframe and Engine Inspection 150 365 28,236.7 11/1/2010 118.5 44 #2 Airframe and Engine Inspection 300 365 28,384.7 3/22/2011 179.5 44 #3 Airframe and Engine Inspection 450 365 28,432.6 6/20/2011 256.8 134 Propeller Static Feathering Check 150 28,621.2 145.4 Aircraft Lubrication 150 28,537.6 61.8 Engine Ground Check 150 28,580.0 104.2 Propeller De-Sludging 450 28,482.5 306.7 Avionics Check 365 01/31/2012 359 Compass Swing On Condition Transponder Inspection (91.413) 730 01/31/2012 724 Altimeter Inspection (91.411) 730 01/31/2012 724 ELT Inspection and Test (91.207(d)) 365 3/22/2011 44 Aircraft Weight Check (135.185) 1095 5/7/2010 455 VOR Check 30 1/27/2012 20 Oil Filter Change / Inspection 50 28588.9 13.1 Cargo Restaint System 150 28537.6 61.8 Corrosion Control AC 135.10A/AC 91.56 AD 41-47-01 Control Surface ReBalance Recovering or Painting AD 56-06-02 Cyl. Flange Attach Stud At O/H AD 63-23-01 Wing Attach Angles Part A 450 28482.5 306.7 AD 63-23-01 Wing Attach Angles Part B 8000 26444.7 5,818.9 AD 66-18-02 Wing Attach Angles Part A 450 28482.5 306.7 AD 66-18-02 Wing Attach Angles Part B 16000 26444.7 13818.9 AD 66-18-02 Wing Attach Angles Part C WP 8000 26444.7 5818.9 AD 66-18-02 Wing Attach Angles Part C WP 12000 26444.7 9818.9 AD 66-18-02 Wing Attach Angles Part C WP 2000 28482.5 1856.7 AD 68-07-05 Elevator Ribs 250 28482.5 106.7 AD 81-13-06 R2 Propeller Blade Failure (Left) 1,825 4/14/2010 1,162 AD 81-13-06 R2 Propeller Blade Failure (Right) 1,825 7/12/2009 886 AD 92-06-15 Wing Structural Failure 2000 28482.5 1,856.7 Aircraft Status Report For N15MA Suplemental Inspection Document (L26-013) Type of Inspection Frequency Last Done Threshold Remaining Due At Hours Days Hours Days Hours Hours Total Time 32.03.01C Main Landing Gear Upper Truss Penetrant 20,000 28,085.3 36,000 19,459.5 48,085.3 53.03.01B Fuselage to Vert. Stab Support Frame 10,000 24,888.0 53,500 6,262.2 34,888.0 54.03.01A Engine Mount Bolts at Firewall 3,200 28,085.3 20,000 2,659.5 31,285.3 55.03.01B Elevator Hinge Brackets 2,000 28,085.3 60,000 1,459.5 30,085.3 55.03.02A Lower Rudder Support 3,000 28,085.3 30,000 2,459.5 31,085.3 55.03.03B Rudder Hinge Brackets #1 and #2 7,000 28,085.3 34,000 6,459.5 35,085.3 55.03.05A Upper Rudder Support 3,000 28,085.3 30,000 2,459.5 31,085.3 57.03.01B Outer Wing Spanwise Skin at Front Center and Rear Spar Caps (Outboard) 4,000 28,085.3 54,000 3,459.5 32,085.3 57.03.04B Aileron Hinge Support Structure 10,000 28,085.3 60,000 9,459.5 38,085.3 57.03.05A Main Landing Gear Rear Strut CTT. STR. 4,000 28,085.3 73,000 3,459.5 32,085.3 57.03.06B Lower Wing Skin Chordwise Splice 4,000 28,085.3 54,000 3,459.5 32,085.3 57.03.07B Outer Wing Lower Spanwise Skin Splice At Center and Rear Spar Caps 4,000 28,085.3 54,000 3,459.5 32,085.3

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