FAA Airworthiness Directives Compliance Record

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Ethelbert McDowell
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1 Aerometal International Phone: Airport Rd E #9 Aurora Oregon USA FAA Airworthiness Directives Compliance Record Company: DC3 Entertainment Airframe Boeing Commercial DC3D-R C P: S: Aircraft Registration o: 3006 Issue umber To ensure that flightcrews activate the wing and tail pneumatic deicing boots at the first signs of ice,contd. TO PREVET LOSS OF AIRPLAE COTROLLABILIT, OR EGIE OVERSPEED AD COSEQUET LOSS OF EGIE POWER CAUSED,COTD. TO MIIMIZE THE POTETIAL HAZARDS ASSOCIATED WITH OPERATIG THE AIRPLAE I SEVERE ICIG CODITIOS,COTD. [ring] TO PREVET STRUCTURAL FAILURE OF THE WIGS DA by boot type A OT A TURBOPROPELLER COVERSIO This AD has been previously incorporated into Aircraft Flight Manual CW Per para a, 1, i, ii, 2 b ext Due Cert o.type AP IA John p. Thomson A&P IA R. Talkington ATP 3:32 PM 113

2 Issue umber TO ESURE THE COTIUIG STRUCTURAL ITEGRIT OF THESE AIRPLAES TO MIIMIZE THE POSSIBILIT OF A JAMMED ELEVATOR COTROL SSTEM, DUE TO CABLE ITERFERECE TO ICREASE FIRE RESISTACE ITEGRIT OF THE PROPELLER FEATHERIG SSTEM AGAIST DAMAGE B A POWERPLAT FIRE [ring] Superseded by [ring] TO DETECT CRACKS BETWEE THE ATTACH BOLT HOLES OF THE WIG LOWER ATTACH AGLES [ring] TO DETECT CRACKS I THE WIG UPPER ATTACH AGLES O BOTH THE OUTER WIG AD CETER SECTIO BETWEE, COTD. SID program incorporated into Owner Established Inspection Program revision IR, dated Aircraft inspected IAW the requirements of Para 1&2 of this AD and was found to be in compliance with these requirements. o further compliance action required at this time. Flexible hose in feathering system forward of the firewall has been replaced with Parker Hannifin 124F hose in accordance with paragraph g of this AD and AMOC letter dated approving this type. AMOC letter is attached CW Per paragraph a. CW Para A ext Due Cert o.type AP D. Ian McGillivray U97A319L Ian McGillivray AP Ian McGillivray A&P TSS Tim Sisk ATP 3:32 PM 213

3 Issue umber [ring] TO PRECLUDE FAILURE OF THE ELEVATOR ISTALLATIO DUE TO CRACKIG OF THE ELEVATOR RIBS Superseded by TO CORRECT RUDDER FORCE REVERSAL TEDECIES O EXISTIG ISTALLATIOS TO PREVET IADVERTET OPEIG OF DOORS TO PREVET TOXICIT HAZARD FOR CREW AD PASSEGERS TO AVOID CRAKSHAFT BEDIG FAILURES Both left and right elevator control surfaces replaced on this date. ew surface inspected prior to recover and modification of both elevators IAW para. i. of this AD was confirmed.visual inspection again required IAW para b. Reinspected and found placard installed. o further compliance required at this time. CW per CAM 4B & -4 aux latch and cover. A per type of fire extinguishing agent used. o further compliance required at this time. A R-2000 engines (D series) not installed 2500 ext Due Cert o.type A&P ATP 3:32 PM 313

4 Issue umber TO MAKE SURE THAT THE AIRCRAFT IS OPERATED AT WEIGHTS OT TO EXCEED 25,200 POUDS FOR LADIG OR TAKEOFF TO GUARD AGAIST THE POSSIBILIT OF EXCESSIVE AIR TEMPERATURES AD ASSOCIATED FIRE HAZARDS, COTD. TO REDUCE THE POSSIBILIT OF IADVERTET OPEIG OF THE DOOR I FLIGHT TO CORRECT THE IABILIT TO FEATHER THE PROPELLER DUE TO IADEQUATE FEATHERIG OIL SUPPL Superseded by Aircraft axles and torque collars inspected IAW douglas SB 261 and found to be satisfactory for operations at weights exceeding 25,200 pounds. o further compliance required at this time. Replaced #2 vacuum pump - fusible plug installed. Genisco aiar oil separators installed. o further compliance required at this time. with sections 2 and 3 of this AD through visual inspection and verification that inspection windows (para 2.A.) were previously installed, a positive over center latch mechanism (para 2.B.) was previously installed, and lock mechanism positive stops (para 3), similar to those found on another door of the same make and model compliant with this AD were previously installed by persons unknown. o further action required. Visually verified that with both LH and RH engine oil tanks drained, feathering pump was still able to supply well over 1.5 measured gallons per side. o further compliance required with these tanks installed. ext Due Cert o.type U97A319L U97A319L D. Ian McGillivray U97A319L D. Ian McGillivray ATP 3:32 PM 413

5 Issue umber TO COMPL WITH THE FIRE PREVETIO REQUIREMETS TO REPLACE THE PRESET "O" RIGS I THE OIL SHUTOFF VALVES [ring] TO ESURE THE ITEGRIT OF THE CO2 FIRE EXTIGUISHIG SSTEM Superseded by TO PRECLUDE CARBURETOR ICIG TO PRECLUDE COWL FLAP HDRAULIC LIE FAILURES AD POSSIBLE SUBSEQUET FIRES Aircraft inspected IAW Douglas SB 250, 252, 258 and 259 (and the MFR drawings within). Aircraft has been previously modified accordingly. Aircraft complies with the requirements of this AD at this time. o further compliance required at this time. Installed correct O-rings IAW DC Due at next OH of FWSOV. with this AD in accordance with AMOC letter dated Aug 30, 2012 attached here. AMOC is to approve electrically operated system in Lieu of the cable operated system referenced. o further compliance required. A per airscoop type. o further compliance required. Reinspected on this date hardware & lines in compliance with this AD. o further action required at this time ext Due Cert o.type U97A319L U97A319L Ian McGillivray ATP 3:32 PM 513

6 Issue umber R Engine Pratt & Whitney [ring] TO DETECT CRACKS I ALL LADIG GEAR REAR BRACE STRUT FITTIG TO ASSURE THE ITEGRIT OF THE RUDDER PEDAL SLIDE TUBE SUPPORT TO DETECT CRACKS OR FLAWS I THE MATERIAL OF THE EGIE MOUT TO FIREWALL ATTACH FITTIGS TO REPLACE ALL CAVAS COTROL BOOT ASSEMBLIES [ring] TO DETECT CRACKS I THE ELEVATOR HIGE BRACKETS TO REBALACE THE COTROL SURFACE EACH TIME IT IS OVERHAULED OR REPAIRED LEFT P: S: Inspected rear brace strut fitting and determined pn has been installed previously and is currently installed. o further compliance is required at this time per para 5.b. Re-inspected - Confirmed 3rd bolt installed IAW this AD A per aircraft type Visual Insp. Canvas Boot Replaced Reinspected. Found not to be applicable per AC type. o further compliance required at this time. Both left and right ailerons rebalanced following re-covering IAW Douglas Service Bulletin o Both checked within limits. ext Due Cert o.type U97A319L D. Ian McGillivray A&P A&P R. Talkington U97A319L Ian McGillivray ATP 3:32 PM 613

7 Issue umber R Engine Pratt & Whitney CLIDER AD STUD FAILURES P: S: with (inspection of cylinder hold down studs & nuts) (ref P&W sb 1000). Compliance due upon condition or next overhaul. RIGHT ext Due Cert o.type DA7R134J Ray Anderson Issue umber Propeller CLIDER AD STUD FAILURES LEFT Engine disassembled and re-assembled. with inspection of cylinder hold down studs and nuts ref P&W SB Compliance due upon condition or next overhaul. ext Due Cert o.type DA7R134J Ray Anderson Hamilton Standard P: 23E50 S: Issue umber R [ring] TO PREVET PROPELLER BLADE FAILURE DUE TO CORROSIO AD FATIGUE CW 39 month inspection interval (b)(2). o corrosion noted. ext due in 60 months 1825 ext Due Cert o.type U97A319L Ian McGillivray ATP 3:32 PM 713

8 Issue umber Propeller ALUMIUM-ALLO PROPELLER BLADE [ring] TO DETECT AD EVALUATE ISTACES OF URECOGIZED BLADE Superseded by ALUMIUM ALLO PROPELLER TO MIIMIZE THE POSSIBILIT OF ADDITIOAL BLADE FAILURES RIGHT o known impact of any kind on any blade. o further compliance required at this time. ot applicable per blade type. o further compliance required at this time. with this AD at overhaul. o further compliance required at this time. Corrosion barrier applied at overhaul. See AD Inspect at next removal of blades from hub or IAW AD ext Due Cert o.type Hamilton Standard P: 23E50 S: Issue umber ext Due Cert o.type ATP 3:32 PM 813

9 Issue umber R GS 430 Garmin International [ring] TO PREVET PROPELLER BLADE FAILURE DUE TO CORROSIO AD FATIGUE ALUMIUM-ALLO PROPELLER BLADE [ring] TO DETECT AD EVALUATE ISTACES OF URECOGIZED BLADE Superseded by ALUMIUM ALLO PROPELLER TO MIIMIZE THE POSSIBILIT OF ADDITIOAL BLADE FAILURES P: S: o known impact of any kind on any blade. o further compliance required at this time. o known impact of any kind on any blade. o further compliance required at this time. ot applicable per blade type. o further compliance required at this time. with this AD at overhaul. o further compliance required at this time. Corrosion barrier applied at overhaul. See AD Inspect at next removal of blades from hub or IAW AD ext Due Cert o.type U97A319L Ian McGillivray ATP 3:32 PM 913

10 Issue umber Lavatory Receptacles To prevent external noise from causing inaccurate course deviation displays in the GS 430 unit's course,contd. A part number not installed ext Due Cert o.type U97A319LPart 135 Transport Category P: PAPERLIE RECEPTACLES S: Issue umber R R Appliance [ring] To prevent possible fires that could result from smoking materials being dropped into lavatory paper or linen,contd. [ring] To prevent possible fires that could result from smoking materials being dropped into lavatory paper or linen,contd VERIFIED PREVIOUSL COMPLIED WITH IAW AD R2 PARA. (a), (b), and (c) WHICH IS OW SECTIOS G, H, AD I. DUPLICATE 1000 ext Due Cert o.type U97A319LPart 135 D. IA MCGILLIVRA U97A319LPart 135 Honeywell, Inc. P: ART 2000 S: Issue umber ext Due Cert o.type ATP 3:32 PM 1013

11 Issue umber ext Due Cert o.type Appliance Honeywell, Inc. P: CM 2000 S: Issue umber ext Due Cert o.type Appliance Honeywell, Inc. P: KA 92 S: Issue umber ext Due Cert o.type Appliance Honeywell, Inc. P: KMH-820 S: ATP 3:32 PM 1113

12 Issue umber ext Due Cert o.type Seats DeCrane Aircraft P: Any Model S: Issue umber ext Due Cert o.type Oil Coolers Any Manufacturer P: Any Model S: Issue umber R Any Model Batteries Teledyne Battery [ring] TO PREVET THE LOSS OF EGIE OIL P: S: ot Applicable. AiResearch oil coolers on this aircraft ext Due Cert o.type ATP 3:32 PM 1213

13 Issue umber ext Due Cert o.type Radar Altimeter System Any Manufacturer P: Any Model S: Issue umber ext Due Cert o.type Radio Magnetic Indicator Any Manufacturer P: Any Model S: Issue umber TO PRECLUDE POSSIBLE ERROEOUS VOR BEARIG IFORMATIO PRESETATIO A these models not installed on this aircraft ext Due Cert o.type ATP 3:32 PM 1313

Aviation Services. Airworthiness Directive Compliance Record N800TS SIN BB-1032

Aviation Services. Airworthiness Directive Compliance Record N800TS SIN BB-1032 Aviation Services Airworthiness Directive Compliance Record N800TS SIN BB-1032 Compliments of Air Care Maintenance Department Repair Station No. ACOR030C Content Revision: 3/2/2015 Beech Aircraft Corp.