2003-13-17 Hartzell Propeller, Inc., McCauley Propeller .
2003-13-17 Hartzell Propeller, Inc., McCauley Propeller Systems, SensenichPropeller Manufacturing Company, Inc., and Raytheon Aircraft CompanyPropellers: Amendment 39-13219. Docket No. 2003-NE- 13-AD.Effective Date(a) This airworthiness directive (AD) becomes effective July 18, 2003.Affected ADs(b) None.Applicability: (c) This AD applies to Hartzell Propeller, Inc., McCauley PropellerSystems, Sensenich Propeller Manufacturing Company, Inc., and Raytheon AircraftCompany (formerly Beech Aircraft Corporation) propellers returned to service by T andW Propellers, Inc. of Chino, CA, and that have a propeller hub serial number (SN) listedin Table 1 of this AD. Table 1 1-Jun-022421926-Jul-021BFBHC-C2YF- AN2991E2CLKUF
01AU69202312721-Jan-02
YK1BFHC-C2YK1BFHC-C2YK1BFHC-C2YK1BF
6-Mar-01
4615-Sep-0202-Jan-01
HC-C2YK1BFCH80322411017-May-02
HC-C2YR1BFCH9804E2418010-Jul-02HC-F2YR-1F CM1111A HC-F2YR-1F CM413HC-F2YR-1F CM610HC-F2YR-1F CM713E HC-F2YR-1F Sep-02HC-E2YR-1BF DK1244EHC-E2YR-1BF DK1812A22HC-C2YR2CLEUF ul-0202-Aug-02
2YR2CEUFHC-M2YR2CLEUF 41282742274128-May-0218-May-0118-May-01
HC-M2YR1BFFB692268316-Apr-01
ep-02HC-B3TN-3D BUA243443268016-Apr-01HC-B3TN-2B BUA24927HC-B3TN-5 4502-Oct-02DG2873434502-Oct-02
Cauley -Feb-0123-Feb-0118-May-0111-Apr-01
Feb-0105-Feb-0226-Oct-02
0210-May-02
l-0115-Oct-0216-Jul-0108-Jan-01
Apr-0102-Aug-0214-May-0124-Oct-0230-Dec-02
8-Oct-02
1 2-Apr-02Fixedpitch410415-May-02
1C160/DTM7557M1 7339071C160/DTM7557M1 7343501C160/DTM7557M1 7357961C160/DTM7557M1 57M1 821611C160/DTM7557M1 BL1931C160/DTM7557M1 CC0421C160/DTM7557M1 -01pitchFixedpitch
LA0441C160/DTM7557M1 M7653P79270pitchFixedpitch1A170/FFA7563 P80498Fixedpitch424005-Aug-021A103/TCM6958 TCM6958 PR7752111C235/LFA7570 QF0161C235/LFA7570 QK0081A103/TCM6958 R7716351A103/TCM6958 R771922
1A103/TCM6958 R772681Fixedpitch287914-Aug-011A103/TCM6958 1-Feb-01401420-Mar-021A103/TCM6958 R7742131A103/TCM6958 R7745091A103/TCM6958 R7749501A103/TCM6958 R7753951A103/TCM6958 R7761491A103/TCM6958 R7761501A103/TCM6958 RG0381A103/TCM6958 RGA0261A103/TCM6958 RP7736611A103/TCM6958 RP774339Sensenich 861K76EM8S5-0-6015777K76EM8S510-0-63 18122KM74DM6-0-561889376EM8S5-0-6019209K
6EM8S5-0-6025510K76EM8S10-0-62 26282K76EM8S14-0-60 5-0-62 26714KFixedpitch279113-Jun-0176EM8S10-0- 27114K6276EM8S5-0-62 0276EM8S14-0- 28769K6076EM8S5-0-60 tchFixedpitch
M74DM-0-56K1225672CKS12-0-52 K327874DM6-0-58K3364474DM6S5-0-54 K3422974DM6-2-62K3655274DM6S5-0-54 3225-May-02Unsafe Condition(d) This AD is prompted by the results of a National Transportation Safety Board(NTSB) investigation of a failed propeller blade and subsequent inspections of variouspropeller models returned to service by T and W Propellers, Inc. We are issuing this ADto detect unsafe conditions that could result in separation of a propeller blade and loss ofcontrol of the airplane.Compliance: (e) If you have not already performed the actions required by this AD, youmust perform the actions within the compliance times specified in this AD.Required Actions(f) For propellers listed in Table 1 of this AD, that have been overhauled since beingreturned to service by T and W Propellers, Inc by an authorized repair station other thanT and W Propellers, Inc., no further action is required.Propellers With Fewer Than 10 Hours Time-in-Service (TIS) Since Return toService(g) Before further flight, perform the actions specified in paragraph (h) of this AD onpropellers listed in Table 1 of this AD, that have fewer than 10 hours time-in-service(TIS) since return to service by T and W Propellers, Inc. You can find information onperforming the actions in the applicable propeller manufacturer's service documentation.(h) Perform the following actions:
(1) Disassemble,(2) Clean,(3) Inspect for the following:(i) Cracks,(ii) Corrosion,(iii) Nicks,(iv) Scratches,(v) Blade minimum dimensions,(vi) Chemical conversion coat or paint or both applied over corrosion,(vii) Lack of chemical conversion coating,(viii) Lack of paint on internal surfaces,(ix) Bolts incorrectly torqued,(x) Incorrect parts,(xi) Incorrect installation of parts,(xii) Reinstallation of parts intended for one-time use, and(xiii) Lack of proper shot peening.(4) Repair and replace with serviceable parts, as necessary(5) Reassemble and test.Propellers With 10 Hours or More TIS Since Return to Service(i) Within 10 hours TIS after the effective date of this AD or one year after the effectivedate of this AD, whichever is earlier, perform the actions specified in paragraph (h) ofthis AD on propellers listed in Table 1 of this AD, that have 10 hours or more TIS sincereturn to service by T and W Propellers, Inc. You can find information on performing theactions in the applicable propeller manufacturer's service documentation.Required Actions Before Installation(j) After the effective date of this AD, do not install any propeller that has a SN listed inTable 1 of this AD returned to service by T and W Propellers, Inc. unless you haveperformed paragraph (h) of this AD on the propeller.Alternative Methods of Compliance (AMOCs)
(k) You must request AMOCs as specified in 14 CFR 39.19. All AMOCs must beapproved by the Manager, Chicago Aircraft Certification Office, FAA.Special Flight Permits(l) We will not issue special flight permits for propellers with fewer than 10 hours TISsince return to service by T and W Propellers, Inc.Material Incorporated by Reference(m) None.Related Information(n) The applicable propeller manufacturer's service documents contain instructions forperforming the required overhaul actions.
Model. Propeller: Hub. S/N. Number of. Blades: Work Order Number. Work Order Date: Beech 278-204 7-2148 2 4077 30-Apr-02 Hartzell
Hartzell Propeller Inc. Service Bulletin No. HC-SB-61-272, “PROPELLER - PROPELLER INSTALLATION”, Issued: January 17/05 or subsequent revision; Hartzell Propeller Inc. Service Letter No. HC-SL-61-239, “PROPELLER - SLIP RING SPLIT MOUNTING PLATE INSPECTION A
the propeller, pressure developed by the propeller, stresses, deformations and strains developed within the propeller when subjected to a thrust. The modifications made to the propeller in terms of material, number of blades and rake angles suggested which variant of the propeller is best suited for different requirements of the Ship.
Propeller Owner's Manual and Logbook Hartzell Propeller Inc. One Propeller Place Piqua, OH 45356 - 2634 U.S.A. . Eddy current equipment is recommended for hub inspection, since cracks are usually not apparent. . Added recommendation for dynamic balance to 0.2 IPS or less Revised the Placement of Balance Weights for Dynamic
Hartzell Propeller Inc. 2020 Price List (1) Sales of DA Items are restricted to select operators and repair stations. (2) Reference for Line Replaceable Units. Original Effectivity Date 1/1/2020 Page 1. F7498 PCP:BLADE UNIT, ALUM [6,1,1] 1/1/2020 4,565.00 A
extended hub Hartzell constant speed propeller (HC C1YK-1BF/F7666A-2). An extended hub Hartzell constant speed propeller should not be used with our 180 hp. options. The 180 hp. options (#2 and #3) also require a different exhaust than the standard Glasair kit supplies for the 150
Aircraft propeller is sometimes colloquially known as an air screw propeller The present work is directed towards the study of composite aircraft propeller working and its terminology, simulation and flow simulation of composite aircraft propeller has been performed. To analyze the composi
Removal and Installation 0 Put match marks on flanges and separate propeller shaft from differential carrier. SPD103 0 Draw out propeller shaft from transmission and plug up rear end of transmission rear extension housing. Transmission 7 SPD359 Inspection Inspect propeller shaft runout. If runout exceeds specifications, replace propeller shaft .
ANATOMI & HISTOLOGI JARINGAN PERIODONTAL Oleh: drg Ali Taqwim . terbentuk dari tulang haversi (haversian bone) dan lamela tulang kompak (compacted bone lamellae). drg Ali Taqwim/ KG UNSOED 29 Lamina dura Alveolar bone proper GAMBARAN HISTOLOGIS GAMBARAN RADIOGRAFIS It appears more radiodense than surrounding supporting bone in X-rays called lamina dura . drg Ali Taqwim/ KG UNSOED 30 1. Cells .
