Beech Bnanza HID Light Assembly Kit Manual N. HID-B-001 Issue Date: 5-8-05 STC N. SA01834CH Revisin Date: 12-22-07 Beechcraft Bnanza HID Landing Light Assembly Kit INSTALLATION MANUAL N. HID-B-001 Beechcraft 33 / 35 / 36 / YT-34 / T-34A / T-34B Mdels KNOTS 2U, LTD. 709 Airprt Rad Burlingtn, WI 53105 262 763-5100 www.knts2u.cm REV # DATE EFFECT A 11-23-05 Changed ballast munting and assciated hardware t three munt ballast B 3-21-06 Added EMI Checklist as Sectin 8.0. Changed ballast part numbers as fllws: RMD-2281-08 became RMD-2281-08A, RMD-2281-09 became RMD-2281-09A. C 12-22-07 ECO 0119 Knts 2U, Ltd. 709 Airprt Rad Burlingtn, WI 53105 ph 262 763-5100 fax 262 763-5125 www.knts2u.cm Page 1 f 7
Beech Bnanza HID Light Assembly Kit Manual N. HID-B-001 Issue Date: 5-8-05 STC N. SA01834CH Revisin Date: 12-22-07 TABLE OF CONTENTS Cver Page.. 1 Table f Cntents 2 Sectin 1.0 Intrductin. 3 Sectin 2.0 Bulb And Ballast Installatin. 3 Sectin 3.0 Parts List.. 3 Sectin 4.0 Specificatins and Paperwrk 3 Sectin 5.0 Figure B.... 4 Sectin 6.0 Maintenance / Trubleshting Guide. 5 Sectin 7.0 Typical Wiring Schematic.. 6 Sectin 8.0 EMI Checklist.. 7 Sectin 9.0 Supplemental Type Certificate.. Knts 2U, Ltd. 709 Airprt Rad Burlingtn, WI 53105 ph 262 763-5100 fax 262 763-5125 www.knts2u.cm Page 2 f 7
Beech Bnanza HID Light Assembly Kit Manual N. HID-B-001 Issue Date: 5-8-05 STC N. SA01834CH Revisin Date: 12-22-07 Sectin 1.0 Intrductin This manual describes the installatin f a cwl munted HID light which replaces the factry cwl munted landing light. This apprval des nt extend t mdels nt listed n the AML. The installatin must be accmplished in accrdance with AC43.13-1B and 2A. The installatin requires the munting f a ballast and bulb. Befre installing cnfirm the vltage f the ballast being installed is crrect fr the aircraft vltage. Sectin 2.0 Bulb And Ballast Installatin A) Remve the landing light retainer and bulb frm the cwling, remve the air cleaner and the left hand cwl access dr t allw mre rm fr ballast installatin. B) Install HID ballast ff t the side f, and in prximity t, the air filter as shwn in Figure A. Reference Figure B fr installatin details. (Alternate ballast munting lcatins may be chsen by the installer, prvided that they will withstand the inertia frces stipulated in AC43.13-2A Chapters 1 & 3 t Sectin 2 A) C) Cnnect black lead f cable # RMD-2281-11 t aircraft grund. verify grund cntinuity per AC43.13 1B/2A sectin 11. (Lead may be shrtened if necessary) D) Cnnect red r white lead f cable # RMD-2281-11 t riginal aircraft landing light pwer wire. (Lead may be shrtened if necessary) E) Per Figure B, install Part N. RMD-2280-09 t Part N. BON-HID-001, 002, r 003 using bulb retainer frm riginal assembly. F) Cnnect cable # RMD-2281-10 frm ballast t bulb. G) Cnfirm that all wires are secured with tie wraps r Adel clamps. Fr further infrmatin reference AC43.13-1B sectin 11-126 H) Install new Light Assembly t cwling. (Figure B) I) Test HID light, cnfirm there are n circuit breakers ppped with all electrical equipment turned n. Als check fr any electrical/magnetic interference with all radi and navigatin equipment per EMI checklist, sectin 8.0 f this manual. J) Re-install air filter and left hand cwl access dr. Figure A- Sectin 3.0 Parts List See Figure B fr Parts List Sectin 4.0 Specificatins And Paperwrk Cmplete FAA Frm 337 fr return t service and lg bk entry. Place a cpy f the supplemental type certificate and maintenance / truble shting manual with aircraft lgs. HID Assembly Weight.... Minus Weight f Assembly Remved. Weight Change... HID Amperage 12/14 Vlt... HID Amperage 24/28 Vlt....95 lbs..84 lbs..11 lbs. - Negligible 2.9 Amps 1.5 Amps Amperage chart f stck bulb(s) remved: 12 / 14 Vlt Systems 24 / 28 Vlt Systems 50 watt 4.2 Amps 50 watt 2.1 Amps 100 watt 8.3 Amps 100 watt 4.2 Amps 150 watt 12.5 Amps 150 watt 6.3 Amps 200 watt 16.7 Amps 200 watt 8.3 Amps 250 watt 20.8 Amps 250 watt 10.4 Amps 300 watt 25 Amps 300 watt 12.5 Amps Knts 2U, Ltd. 709 Airprt Rad Burlingtn, WI 53105 ph 262 763-5100 fax 262 763-5125 www.knts2u.cm Page 3 f 7
Beech Bnanza HID Light Assembly Kit Manual N. HID-B-001 Issue Date: 5-8-05 STC N. SA01834CH Revisin Date: 12-22-07 FRONT OF AIRCRAFT Ø.2280 TYP. 1.7300 2.9150 AIRCRAFT POWER AIRCRAFT GROUND 4.3400 4.9390 VIEW FROM SIDE FIGURE B INDEX N. PART N. DESCRIPTION UNITS PER ASSY. 1 BON-HID-001 HID RETAINER... 1 Or BON-HID-002 HID RETAINER... 1 Or BON-HID-003 HID RETAINER... 1 2 RMD-2280-08 REFLECTOR HOUSING, HID LIGHT, CLEAR... 1 OR RMD-2280-09 REFLECTOR HOUSING, HID LIGHT, DIFFUSED... 1 3 36-GASK PAR 36.0625 GASKET - SILICONE... 1 4 *002-410000-143 BEECHCRAFT RETAINER (ORIGINAL)... 1 5 AN507C-632R-8 S.S. C/S SCREW... 11 6 AN960-6 WASHER... 3 7 AN365-632A NUT FIBER LOCK... 3 8 RMD-2281-08A BALLAST, HID, 24 VOLT... 1 OR RMD-2281-09A BALLAST, HID, 12 VOLT... 1 9 AN3-12A BOLT... 3 10 MS21044N3 NUT-FIBERLOCK... 3 11 AN970-3 WASHER, WIDE AREA... 3 12 RMD-2281-10 HID CABLE, BALLAST TO LAMP... 1 13 RMD-2281-11 CABLE, A/C TO BALLAST... 1 14 MS35333-39 INTERNAL TOOTH LOCKWASHER... 3 15 HID-2281-13 SPACER NEOPRENE... 3 16 RMD-2280-06 BULB, D1S... 1 Hardware sizes are recmmended, apprpriate substitutins may be used. Beechcraft Part N. (r equivalent) Sectin 5 Figure B Knts 2U, Ltd. 709 Airprt Rad Burlingtn, WI 53105 ph 262 763-5100 fax 262 763-5125 www.knts2u.cm Page 4 f 7
Beech Bnanza HID Light Assembly Kit Manual N. HID-B-001 Issue Date: 5-8-05 STC N. SA01834CH Revisin Date: 12-22-07 Sectin 6.0 Maintenance / Trubleshting Guide Knts 2U, Ltd. 703 Airprt Rad Burlingtn, WI 53105 262.763.5100 www.knts2u.cm Truble Shting Prblem Slutin Cmments Light circuit breaker pps frequently. HID Light des nt illuminate, illuminates slwly r des nt g t full pwer. Check wires fr a shrt circuit. Remve and replace ballast. Replace bulb and / r ballast, verify functin. Cntact Knts 2U, Ltd. fr a replacement. Cntact Knts 2U, Ltd. fr a replacement. Maintenance / Inspectin Requirements Scheduled Inspectins Inspectin Time interval Cmments Remve landing light retainer and lens, inspect; A) Ballast fr munting security and general cnditin. B) Bulb husing, bulb and retainer plate fr security and general cnditin. Unscheduled Inspectins Annual r 200 hurs, whichever cmes first. Inspectin Event Cmments Remve landing light retainer and lens, inspect; A) Ballast fr munting and security B) Bulb husing, bulb and retainer plate fr security and general cnditin. C) Perfrm functin test. Hard landing, Lightning Strike. Cntact Knts 2U, Ltd. fr a replacement. Cntact Knts 2U, Ltd. fr a replacement. Knts 2U, Ltd. 709 Airprt Rad Burlingtn, WI 53105 ph 262 763-5100 fax 262 763-5125 www.knts2u.cm Page 5 f 7
Beech Bnanza HID Light Assembly Kit Manual N. HID-B-001 Issue Date: 5-8-05 STC N. SA01834CH Revisin Date: 12-22-07 Sectin 7.0 Typical Wiring Schematic This wiring schematic is typical f the aircraft apprved by this Manual and is shwn as reference. See the apprpriate Beechcraft Service Manual fr wiring schematics applicable t yur aircraft. HID BALLAST HID BULB TYPICAL 24/28 VOLT SYSTEM RMD-2281-10 10A TYPICAL 12/14 VOLT SYSTEM 16 RMD-2281-11 RMD-2281-11 HID BALLAST RMD-2281-10 HID BULB 20A 12 Knts 2U, Ltd. 709 Airprt Rad Burlingtn, WI 53105 ph 262 763-5100 fax 262 763-5125 www.knts2u.cm Page 6 f 7
Beech Bnanza HID Light Assembly Kit Manual N. HID-B-001 Issue Date: 5-8-05 STC N. SA01834CH Revisin Date: 12-22-07 Sectin 8.0 EMI Checklist 1. This EMI checklist must be cmpleted after installatin f the HID light(s). The purpse f this checklist is t insure that there is n ut f tlerance interference between the HID lighting system and ther systems already installed in the aircraft. If ut f tlerance interference is detected, the installatin may be mdified by adding external filters, relcating equipment, r re-ruting cables as necessary t eliminate interference. Fr further assistance, the installer may cntact Knts 2U, Ltd. a. VHF Radi Check With the VHF Radi n, adjust t the squelch activatin threshld. Test the fllwing frequencies, 121.7, 122.95, 128.7, and 131.3. Nte any nrmal backgrund nise. Activate HID light(s) and repeat frequency check. Nte any deviatin in readings between tests. Repeat check n any additinal radis. b. VOR Check With the nav radi n adjust squelch t the activatin threshld. Test the fllwing frequencies, 108.00, 111.4, 116.4 and 117.95. Nte any nrmal backgrund nise. Activate HID light(s) and repeat frequency check. Nte any deviatin in readings between tests. Repeat check n any additinal nav radis. c. ADF Check With the ADF/NDB n, adjust t the squelch activatin threshld. Test at least three frequencies ne near the lw ADF/NDB frequency range, ne near the middle ADF/NDB frequency range and ne in the higher ADF/NDB frequency range. Nte any nrmal backgrund nise. Activate HID light(s) and repeat frequency check. Nte any deviatin in readings between tests. Repeat check n any additinal ADF/NDB driven equipment d. GPS Check Turn n GPS and set t a way - pint at least 100 miles away. Nte GPS readings Activate HID light(s). Nte any deviatin in readings between tests. Repeat test fr each additinal GPS. e. Additinal Equipment Operate any ther equipment and test fr interference with the HID light(s). Individual equipment installatin and/r peratin manuals may be referenced fr specific test prcedures. Knts 2U, Ltd. 709 Airprt Rad Burlingtn, WI 53105 ph 262 763-5100 fax 262 763-5125 www.knts2u.cm Page 7 f 7