TYPE TIGER CUB 440, ROMAIN MODIFIED

Transcription

1 T>~hh =-~,~~.> D~~~ 1 ~+ BRTSH MCROLGHT ARCRAFT ASSOCATON MCROLGHT TYPE ACCEPTANCE DATA SHEET (TADS) NO: BMO-21 SSUE: 1 TYPE TGER CUB 440, ROMAN MODFED (1) MANUFACTURER: MCROBPLANE AVATON (Now ceased tradng) wth J Roman modfcatons. (2) (3) UK MPORTER: n/a CERTFCATON BASS: BCAR Secton S, Advance ssue, March 1983 n accordance wth CAA document dated 17 January 198E reference 9/30/UL18. (4) DEFNTON OF BASC DESGN STANDARD: Not avalable, but see buld standa owner's kt Buldng nstructons and J Roman drawngs for Tger Cub modfcatons. (5) DMENSONS/WEGHTS FOR COMPLANCE WTH MCROLGHT DEFNTON (a) Wng area (nc canard area. excud~ng wnglets): '"~ (b)' Spn: ' (c) Standard Mean Chord: (d) Dry Empty Weght: (e) Max Take-Off Weght: (f) Wng Loadng (Weght Empty/Wng Area): (g) Wng Loadng (Max Take-Off WeLght/Wng Area): (h) Fuel Capacty: 12.9 m2 Top: 6.5m Bottom: 6.3m 1.97m 146kg 250kg kg/m kgjm2 20 ltres DOCUMENT SSUE STATUS ssue Revson Date Authorsaton Pages Vald Number Reference affected ssue pages at th, ntroduced by MAANll03 5/1/93 BMAA ;-;tc All new Page No. Page s :3 c /"? , ,

2 MCROLGHT TYPE ACCEPTANCE DATA SHEET (TADS) NO: BMO-21 SSUE: 1 (6) POWER PLANTS Desgnaton! Roman Mod'd Tger Cub 44 1 ' Engne Type Fuj Robn! EC44PM, ny' td : ; Reducton 2.61:1 Gear/rato Exhaust Ncklow System! ntake - System, Propelle!" Type Propeller 58" x 33" Da x Ptch, Roman! ; Nose Type 33M, ss 2 Cert. No.., : Nose requremenṯ -LM Reqstered Pre 1/4/86 80 dba Rpn~tprpn Pn~t 1/4/~~ 7h lra 2 Seat 84 dba RO lra BCAR Reference ]3-6, h J Too A

3 MCROLGHT TYPE ACCEPTANCE DATA SHEET (TADS) NO: BMO-21 SSUE: 1 ~7) MANDATORY LMTATONS: * To be placarded *(a) Max Take-off Weght: 250kg *(b) C G Lmts: 30" to 32" AoD (c) C G Datum: Front face of frewall *(d) Cockpt Loadngs Plot or Ballast (mn) Plot or Ballast (max) (e) Permanent Ballast, Weght and Poston: Front Rear Total 55 kg - kg 55 kg 90 kg - kg 90 kg -None (f) Empty C G: 27.5" typcal *(g) Never Exceed Speed: 70 knots *(h) ~Maqpeuvrng Speed: *() Manoeuvre Lmtatons: *(j) Fuel Contents (Max Usable): 56 knots Aerobatcs prohbted, bank beyond 60 prohbted. 20 ltres (k) Power Plant: See Table be:low- ENGNE Fuj Robn EC44PM Max RPM 7000 Max CHT 230 C Max EGT N/A Fuel Spec & 92 octane mn petrol/ol Engne Non-synth Ol Spec prem 2-stroke Gearbox N/A Ol Spec Fuel/Ol Mx 40: 1 Ol Pressure N/A Ol Temp N/A Coolant Temp N/A ~ - ~,.. 1 ~

4 MCROLGHT TYPE ACCEPTANCE DATA SHEET (TAnS) ~ ~, ~ NO: BMO-21 SSUE: 1 (8 ) NSTRUMENTS REQURED FOR TYPE ACCEPTANCE: AS Al tmeter RPM CHT Com.Qass EGT Coolant Tem.Q Requred Requred Recommended n addton: Sl.Q ndcator (9 ) CONTROL DEFLECTONS (3-AXS SYSTEMS): Ptch Control Talplane Trm Alerons Rudder Steerng Spolers N/ A Up: 15 +/- 1 Up: N/A Up: 5" at T.E. Left: 4.5" at T.E. Left: 27 Down: 15 +/- 2 Down: N/A Down: 1" at T.E. Rght: 4.5" at T.E. Rght: 27 (10) PLOT'S NOTES, MAJNTENANCE MANUALS REFERENCES: Mcrolght Arworthness Approval Note.MAAN no 1103 Tg!r Ctl9 440 Plot's Operatng Manual Tger Cub 440 Kt Buldng nstructons n assocaton wth Roman ~odfcatons as Appendx 1. (11) Mfu~DATORYMODFCATONS/SERVCE BULLETNS/ARWORTHNESS DRECTVES ~ ETC: See Appendces. (12) APPROVED OPTONAL MODFCATONS (13) MNMUM PERFORMANCE AT MAX TLO WEGHT: Rate of Clmb: 5~0 ft/mnute Clmb Speed: 45 mph Stall or Mnmum Flyng Speed: 35 mph

5 MCROLGHT TYPE ACCEPTANCE DATA SHEET (TADS) NO: BMO-21 SSUE: 1 G A Drawngs and/or colour photographs llustratng the prncpal features the arcraft descrbed heren, shall be attached to, and form part of, ths Data Sheet. ssue Date BMAA Acce.Qtance ) _1C 4) f~ / 'f J CJ-;<;f1 r t-vu}'e~( r ~ :.S4 r-uarv L992 n_--,..

6 ",--- -_u_--~--- --~---,-, MCROLGHT TYPE ACCEPTANCE DATA SHEET (TADS) NO: BMO-21 SSUE 1 APPENDX 1 -eas affected by modfcatons requred for converson of standard Tger Cub.0 to Tger Cub 440 Roman Modfed. dfcatons affectng the followng areas are requred for the converson oj e standard Tger Cub 440 to the Tger Cub 440 Roman Modfed (as referred n MAAN 1103): Fn and rudder. Undercarrage. Aleron control system. Lower Upper alerons. alerons. Cross bracng between nter planar struts. Jury struts at root end of wng spars. rfue--l tank. Harness. Transparent sde panels and cockpt access door., Engne cowlng. Rear cylnder head. Propeller and reducton. Propeller shaft materal.

7 p" O"A 7 (")-F 1() MCROLGHT TYPE ACCEPTANCE DATA SHEET (TADS) NO: BNO-21 SSUE 1 APPENDX 2 equred modfcatons to T~er Cub 440 Roman Modfed for ssue of Permt To Flv rhe followng modfcatons must be ncorporated on each Tger Cub 440 Roman 1odfed n order to comply wth the requrements and to qualfy for the ssue of ( ermt To Fly. (Bulletns/modfcatons prefxed "TCD" are obtaned va Nr R Lght )f Tger Cub Developments Ltd). 1) Sl7l (a) Elevator trm and rudder centrng sprngs must be ftted n accordance wth TCD TM 013A and B. (b) Provde lftng aerodynamc centre secton as TCD TN ) S603 & S721(a) Man undercarrage axle to be re-enforced wth close fttng nner sleeve or modfed n accordance wth TCD TN 001. (b) Man wheels to be replaced as TCD TN ) S609 (a) Dran holes to be provded n flyng surfaces as TCD 023..(b).,- '" Wooden components of flyng stlrfaces to be provded wth addtonal protecton as TCD TM 031. ~) 867l Elevator hnge bearng sleeves to be bonded as TCD 022. :;) S959 Unusable fuel: a placard s to be provded statng: "THS ARCRAFT MUST NOT TAKE OFF WTH LESS THAN 2 GALLONS (MP) FUEL". ) S993 A fre resstant fuel lne s to be ftted between the engne bulkhead an the engne, and routed as far as possble on the opposte sde of the engne to the exhaust. ') S995 A fuel shut-off valve s to be ftted wthn easy reach of the plot, and clearly marked wth ts ON and OFF postons. ) Sl141 The wrng for the gnton swtch must be at least fre resstant from the engne at least as far as the bulkhead or be sleeved wth a fre.. reslstant materla..-,) S421 The stablator spar sleeve s to be replaced wth a longer sleeve measurng 43 nches, wth stress relevng "V" notches of 4 nches each end, materal HT30TF alloy, 1 nch dameter x 16 g. To be located centrally n the spar, TCD TN 026 refers and provdes an acceptable optor usng usng two sleeves of 17 g. 0) A slp ndcator must be ftted n full vew of the plot.

8 n addton, the followng servce bulletns ssued by the manufacturer or by Tger Cub Developments (for BMAA Godfather) must be actoned on each Tger Cub 440 Roman Modred aeroplane when beng nspected for the purpose of ssung the Permt To Fly: MB SB 002 Aleron hnges. MB 3B 003 Flyng and landng wre termnaton. MB 3B 004 Sharp gear down unts, prop bolts. MB 3B 005 Elevator operatng tube. MB S8 006 Recol pull starter. MB S8 007 Talplane bearng blocks. MB 3B 009 Flyng wre lengths. MB 3B 011 Throttle lever movement. MB SB 012 Rear landng wre root termnaton. MB SB 013 Correcton to assembly or rudder pulley guards. ~. u MB SB 014-Rer spar hnge bolts. MB 3B 015 Safety lockng of aleron pulley nuts. MB 5B 018 Wndscreen. MB SB 019 Flyng and landng wre crossover support. MB 3B 020 Rear fuselage bulkhead. TCD/SB 024 Engne mountng. TCD/SB 025 Wng tps durng ground transportaton. nsdecton. ~ The revew of the complance of the Tger Cub 440 Roman Modfed wth the arworthness requrements of BCAR Secton S has ndcated a number of areas where partcular attenton must be gven by each BMAA nspector responsble for the nspecton of the Tger Cub 440 Roman Modfed, and these areas are lsted below: (1) nspecton s requred to establsh that each or the modfcatons lsted above has been carred out to an arworthy standard and that the Servce Bulletns called up have been compled wth.' (2) The bond between the fuselage longerons and the roam sdes and tops s to be checked by ensurng that there s no wrnklng or the fabrc adjacent to these bonds when loads are appled at the tal. nternal nspecton must also be made..

9 Each hand fnshed component s to be checked for corroson and adequate protecton, n addton to normal overall nspecton for corroson. A check s to be made to ensure that the aleron spar has been modfed n accordance wth MBA Mantenance Manual, page 4-4. The stablator s to be examned for satsfactory performance of the bond between ts spar and the foam. Creasng of the surface fabrc n the vcnty of the spar run, on the upper or lower surfaces, whlst loads are appled to the stablator, must not be accepted.. n vew of the ndvdual nature of kt constructon, each control surface stop must be examned for satsfactory performance, together wth ensurng control surface range of movement s wthn lmts. Cables must be examned fdr any sgns of w~ar or frayng around pulleys. Ensure satsfactory guardng of cables at all pulleys, partcularly upper rudder pulleys. Ensure that, where turnbuckles are ftted n the control system, they do not bnd aganst any surface. Ensure throttle control provdes full travel of the throttle sldes. ( '" Ensure throttle and choke controls are clearly dstngushable and arrange for easy operaton wthout foulng. Ensure satsfactory electrcal bondng between engne and arframe. Ensure compatblty of engne + reducton + propeller and satsfactory performance. Ensure that the four exhaust sprngs are wred so that they wll be prevented from fallng away from the arcraft n the event of breakage. Ensure that the layout of the fuel lnes does not gve rse to potental vapour locks. Ensure that the nternal fuselage, partcularly n the vcnty of the fuel tank, s not sufferng fro~ damage, due to fuel seepage or spllage. Ensure that fuel tank s ether readly removable or provded wth means of dranage. Ensure that the requred nstrumentaton s ftted: Arspeed ndcator, Altmeter, Slp ndcator Cylnder Head Temperature Gauge. Ensure complance wth BMAA General Note GN-(89)-O14 concernng rear hnged doors. D~~~ () -~ ",

10 \,1, Page 10 TADS BMO-21 Tger Cub 440 Roman Me ~, '\ - ~. " MJ ~ ' ' ---, '11V..f',,"..j. ( " J~:":'!' --~., ~,.- ~. ",".' '. 1 '. c=,- ','