Lo cate ex ist ing wire number JK- PA12A18; push wire out of pin 8 of #1 regu ... Func tion ally check op era tion of al ter na tor(s) per POH/AFM, Sec tion IV, Nor ...
INTRODUCTION: THE 24 VOLT ELECTRICAL SYSTEM IS WIRED IN A MANNER THAT RENDERS THE OVERVOLTAGE WARNING LIGHT IN THE ANNUNCIATOR PANEL ASSEMBLY INOPERATIVE SHOULD AN ALTERNATOR OVERVOLTAGE OCCUR. THIS S. B. PROVIDES INSTRUCTIONS TO REWIRE A PORTION OF THE CIRCUIT TO ENABLE THIS WARNING LIGHT. INSTRUCTIONS: 1. Disconnect VR-802 voltage regulator (for Alternator #1) located under the instrument panel on the co-pilot’s side. 2. Locate existing wire number JK-PA12A18; push wire out of pin 8 of #1 regulator main harness receptacle. 3. Cut pin from wire, JK-PA12A18; cap wire end using AMP 324485 wire cap (included in kit). 4. Remove Glareshield per instructions in the appropriate S & M manual, Section 39-10-01. 5. Insert wire number JK-PA12B18 (included in kit) into pin 8 of voltage regulator receptacle and reconnect regulator. 6. Route wire number JK-PA12B18 along existing wire bundle to annunciator panel connector (JK-WT104A). Secure with lacing cord or Ty-Raps. 7. Locate wire number JK-WT02A22 connected to pin 1 of annunciator panel connector, JKWT104A, and cut JK-WT02A22 wire approximately 6 inches back from connector. 8. Use AMP 320559 wire splice to re-connect wire number JK-WT02A22 and the unconnected end of new wire JK-PA12B18 (SEE FIGURE M20-245-1). 9. If Dual Alternators are installed, repeat Steps 1 through 5 with #2 regulator but on wire numbers JK-PA30A18 (Steps 1, 2 & 3) and JK-PA30C18 (Step 5). Route unconnected end of wire number JK-PA30C18 to vacuum switch on back of Artifical Horizon and connect to “white” terminal. 10. Remove the 1 amp Annunciator C/B and replace with a 2 amp C/B, included in Rev. A kit. 11. Functionally check operation of alternator(s) per POH/AFM, Section IV, Normal Procedures, Before Takeoff. 12. Enter compliance note in aircraft logbook and return aircraft to service. WARRANTY: This kit should be ordered from the Mooney Service Center in your area. Normal warranty billing policies will be in affect for this kit. Mooney Aircraft Corporation will allow up to 2.0 hours labor to accomplish this modification if a completed War ranty Claim is received within 1 year from the date of this Service Bulletin. REFERENCE DATA: PARTS LIST:
hours la bor for all S/N's within origi nal war ranty agree ment time frame. War ranty credit will ... in voice within 180 days of date of this Serv ice Bul le tin. REF ER ...
Re move clutch (no- back) spring (Item 9) from clutch hous ing us ing in put gear ... Us ing gear as sem bly (Item 6) as in ser tion tool, place new clutch spring on ...
attaques venant du ciel. Dotée d'un central opérations (CO) particulièrement performant, la FDA peut ainsi gérer l'activité aérienne de toute une zone d'opérations. L'hélicoptère Caïman Marine donne par ailleurs de l'allonge et permet de détecter l'e
SECTION VIII. FIRST AID MEASURES. Rev. ... FIRE AND EXPLOSION HAZARD DATA ... Ingestion: Call physician or Poison Control Center immediately. Induce ...
Mécanique. Transmission. Le moteur M1 entraîne par la poulie 121 (rapport 4,5:1) la poulie 122 sur l'arbre intermédiaire 140 via une courroie crantée 101.
été construits il y a plus de 150 ans. La Commission de la. Capitale nationale (CCN) en a fait l'acquisition afin de protéger le « mille historique », parcours ...
5 Mesures de lutte contre l'incendie ... 4,5. · Changement d'état. Point de fusion: Non déterminé. Point d'ébullition: .... DOT: US Department of Transportation.
Tell her she looks lovely, smells good, is intelligent, have a beautiful house - ... coffee shop; it affords you both a chance to talk and get to know each other a little ...
Le Nouvel Houdini – Chapitres 3 et 4. A. Chapitre Trois : Répondez aux questions en anglais et en phrases complètes. 1. Why did Brandon get up at 6:00 in the ...
The example situ- ation has about one pound of water for each 1000 pounds of air (1/1000). The air flow at 16:1 fuel air ratio is: Air rate = .3 gals./hr. * 6 Ibs./gal.
burn. The adiabatic compression raises the temperature of the mixture, some of the liquid fuel on the piston and cylinder walls vaporizes absorbing some of the.
Hello,. Welcome to MusicParts.Com, Inc. your online resource for technical documents and service information. This PDF package may contain information, ...
Si cet onglet ne s'affiche pas, confirmez votre utilisation de ... Cette configuration s'effectue dans l'onglet Dir Access figurant dans les paramètres utilisateurs.
Sep 5, 2007 - a higher refractory feature which should minimized the vaporization of oxide ... A subsequent shock led to a burst of the device. The empirical ...
