SERVICE LETTER NO. 52

Transcription

1 SUBJECT: SERVICE LETTER NO. 52 New Alternator Control System. 21 June 1983 Page 1 of 1 Rev. A dated 9/26/86 Rev. B dated 10/3/90 AIRPLANES AFFECTED: Maule Model M-5-235C, Ser. No. 's 7104C, 7121C thru 7355C, 7357C thru 7376C; M-6-235, Ser. No.'s 7249C,7356C, 7379C thru 7434C. COMPLIANCE: Optional. STATUS: To provide a replacement Alternator Control System. AUTHORITY: This Service Letter is FAA approved. BACKGROUND: Voltage Regulators and Overvoltage Relays are no longer available for replacement in electrical system. New Alternator Control System replaces these items. ACTION T013ETAKEN. AND MATERIAL REQUIRED: (1) Attac.hAFM SuppLemen.t ' No. 12 to FAA Approved M-S-23SC Airplane Flight Manual dated 6 April 1976 or AFM Supplement No. 9 to FAA Approved M-5-235C Airplane Flight Manual dated 12 August 1981 or AFM Supplement No. 6 to FAA Approved M Airplane Flight Manual dated 25 June (2) Installation Instructions: (a) Install the following 'per drawing 7127B: 1 ea. 1 ea. 2 ea. 2 ea. 2 ea. 2 ea. B B-1 AN526-1O-R8 AN AN R10 AN970-3 Alternator Control (Lamar) Alternator Control Mount Screw Nut Screw Washer (b) Install the following per drawing 7128B: 1 ea. A Alternator Inop. Switch 2 ea. AN Nut 2 ea. AN Screw 1 ea Alternator Out Indicator Light 1 ea. 7130A Plate, Alternator Out Ind. Light 1 ea. 6074F-51 "ALTERNATOR OFF WARNING" Placard (d) Install the following per drawings 7047F, Sht 1 and 7047E, Sht 2: 1 set Wiring for Alternator Control System When modification is completed, make proper log entries, fill out Service Letter #52 Compliance Record Sheet and return.

2 MAULE AEROSPACE TECHNOLOGY, INC. SERVICE LETTER #52 - COMPLIANCE RECORD Airplane Serial Number Airplane Registration Number The following action was taken with respect to this service letter: Service letter #52 completed Certified by (Signature) (Printed Name) Title (Owner, A&P), IA, etc.) In an effort to keep our mailing list current for sending Service Letters, Service Bulletins, etc., please fill in the following: Owner's name Owner's address Mail this Compliance Record to: Maule Aerospace Technology, Inc. Engineering Records 2099 GA Hwy. 133 S. Moultrie, GA 31788

3 MAULE AIRCRAFT CORPORAliON AIRPLANE FLIGHT MANUAL MAULE M-5-235C LOG OF SUPPLEMENTS Page ii supp NO. OF DESCRIPTION APPROVAL 1 3 Installation of FluiDyne C2200H or C3000H Skis. 03/ Installation of Pee Kay 2300 Floats. 0511om - 4 Installation of Aqua 2400 GW. 05l27m 3 2 Installation of EDO 248A2440 or Floats. (07/07f77) Rev. A 09/07fi8 4 3 Installation of FIi-L1te 3000 MK lila Skis 06120/ # GW Modification. (N1Ato AFM, rev. C dated 4/22181) 09110/ Installation of 20"140" Flap Ratchet (@2300# GW / Installation of FluiDyne A2500A Wheel Replacement Skis / Inst. of EDO Amphibious 2750# GW per Dwg 9057A (06129/82) Rev. A Installation of Hartzell HC-C2YR-1BF/F8468A-3R (81") Propeller. 09/ Installation of SW Instrument Cluster pin / Installation of 20"/40" Flap Ratchet & 2500#GW Modification. (N1Ato AFM. rev. C ( ); use AFMS #fi) 04101/ Installation of lamar Alternator Control System Instructions to drain Main Fuel Tank Sumps at Preflight Inspection 05105/ Inst. of EDO GW. (FIP per Maule Dwg 9143A only) (09/13/85) Rev. A Installation of F/i-lite 3000 MK ilia GW. (Skiplane per Maule Drawing 9081A only) Installation of FluiDyne C3000 (Manually Operated) Skis Inst. of FluiDyneC3000 (Manually Operated) GW. (Skiplane per Maule Dwg 9158A only) 11/ Installation of McCauley B2D37C224-B1G-90RA -9 (81") 2 Blade Propeller. (03/05/92) Rev. B 03/ Installation of McCauley B3D32C414-C/G-82NDA-2 (80") 3 Blade Propeller. (03/05192) Rev. B Right operation with either one (not both) of the Front Doors removed. ( ) Rev. A 03101/ Installation of Lycaning B5 Engine. ( ) Rev. A Installation of Ly<:aning0-54O-J3A5 or WIA5 Engine. (09/12194) Rev. A 03/01/ Inst. of Aqua 2400 (FIP per Maule Dwg 9166A only) ( ) Rev. A 03130/ Inst. of McCauley B3D32C414-[)/[]-82NDA 2 (80") or -4 (78") Prop (with Engine) / Operation of airplane when modified per Maule Mod Kit No.2 (has the expanded Oil Pressure Umits). 10/29/98-2 Inst of 2110X-30 Wing Assemblies with 2167X Main Fuel Tanks - Maule Modification Kit No / Installation of Aqua 2200 Floats. 09/18/ Installation of Hartzell HC-C2YR-1BF/84nD-6 Q[ HC-C3YR 1RF/F-7693(F)-() Propeller (5279F). Rev. A 04/ Inst. of S-TEC System 55 Two Axis Autopilot ST-620 (14 volt) - Maule Dwg 9196A, Rev. A or later. (Land) 04/04/ Inst. of S-TEC System 55 Two Axis Autopilot ST-620 (14 volt) - Maule Dwg 9196A, Rev. A or later. (Sea) 04/04/ Inst. of S-TEC System 50 Two Axis Autopilot ST (14v) - Maule Dwg 9193A, Rev. B or later. 01/05/ Inst. of S-TEC System 30 Two Axis Autopilot ST (14v) - Maule Dwg 9197A, Rev. A or later. (Land) 01/21/ Inst. of S-TEC System 30 Two Axis Autopilot ST (14v) - Maule Dwg 9197A. Rev. A or later. (Sea) 01121/ Inst. of S-TEC System 20 Single Axis Autopilot ST (14v) - Maule Dwg 9197A, Rev. B or later. (Land) Inst. of S-TEC System 20 Single Axis Autopilot ST (14v) - Maule Dwg 9197A, Rev. B or later. (Sea) 03120/ Installation of FluiDyne C3000H GW - Drawing 9174A, Rev. C or later revision. 01/30/ Inst. of S-TEC System 40 Single Axis Autopilot ST (14v) - Maule Dwg 9193A, Rev. C or later. 10/29/01-5 Installation of Apollo MX20 Multi-Function Display - Maule Drawing 7265A

4 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 13 FOR MAULE M-5-235C Reg. No Sere No. This Supplement must be attached to the FAA Approved Airplane Manual dated 6 April 1976 when Ouick Drains are installed in the Main Fue l Tanks in accordance with Service Bullet±n U5 (considered mandatory). The information contained herein supersedes or supplements the information of the basic Airplane Fli~ht Manual; for limitations, procedures and performance information not contained in this Supplement, consult the basic Airplane Flight Manual. OFFICE, FAA, CENTRAL REGION DATE: May 1, 1984 :0.---'- Page 1 of 2

5 MAULE AIRCRAFT CORPORATION MOULTRIE, GEORGIA AFM SUPPLEMENT NO. 13 for M-S-23SC NORMAL OPERATING PROCEDURES PREFLIGHT INSPECTION: EXTERIOR: Sa. Wing Main Fuel Tank Drain DRAIN 18a. Wing Main Fuel Tank Drain DRAIN FAA APPROVED DATE: 5/1/84 Pa ge 2 of 2

6 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 12 FOR MODEL M-5-235C Reg. No. Ser. No This.S'tpp17111ent must be attached to the FAA Approved Airplane Flight Manualdat~d6 April 1976 when Alternator Control System is installed in'accordance with Maule Service Letter No. 52. Thei,~tormation contained herein supersedes and supplements the information - ~'f, th e b a s i c :Ai t pl ane Flight Manual; for -limitat i ons. procedures and performance inf6rmation ri~t contained in. this Supplement. consult the basic Airplane Flight Manual.. - '~~..".,.. Ma ager. Atlanta R rcraft Certification Office. FAA. Central Region DATE:.::;.;:,..'--=...:.:--:...:...:;.;::.. JUt J Page 1 of 2

7 MAULE AIRCRAFT CORPORATION MOULTRIE, GEORGIA AFM SUPPLEMENT NO. 12 for M-S-23SC SECTION III EMERGENCY PROCEDURES: 3.2 ALTERNATOR FAILURE: Alternator output should be mon ir o r ed b y r o Le r once to til l' ;JnUO( ' t (, [ l o c a ted on the right side of the engine instrument cluster. Should the ammeter indicate a minus deflection when engine RPM is above 900 and/or red "ALTERNATOR OFF WARNING" light is illuminated, push ALT switch OFF then ON. Repeat two times as necessary to reset. If system will not reset, reduce the electrical load as much as possible, land as soon as practicable and investigate the electrical system malfunction before further flight. FAA APPROVED DATE: 12 JUL 1983 Page 2 of 2

8 MAULE AIRCRAFT CORPORATION AIRPLANE FLIGHT MANUAL MAULE M 5-235C (sin 7321C,7347C,7351C,7363C,7369C-7373C,7375C,7445C,7451C,7460C,7467C) LOG OF SUPPLEMENTS Page ii supp NO. OF APPROVAL DESCRIPTION NO. PAGES DATE - 4 Installation of Aqua 2400 OS/ Installation of Lycoming 0-540"",3A5 or WIA5 Engine. 09/12/ Installation of FluiDyne C3000H Wheel-5kis - Maule Drawing 9174A, Rev. C or later. 01/30/ Installation of FluiDyne A2500A Wheel Replacement Skis / Inst. of EDO Amphibious Floats - Maule Dwg 9057A. (06/29/82) Rev. A 12108/ Installation of Hartzell HC-C2YR-18F/F8468A-3R (81") Propeller. 09/ Installation of SW Instrument Cluster pin /03/ Installation of Lamar Alternator Control System. 07/12f Installation of EOO Floats - Maule Drawing 9143A. (05/06/85) Rev. A 12108f Installation of Lycoming Engine. (04/25/88) Rev. A 09/ Installation of McCauley 82037C224-8fG-90RA-9 (81") Propeller. (03f05/92) Rev. A 08/10f Installation of McCautey 83032C414-C/G-82NOA-2 (80") Propeller (03/05/92 ) Rev. A 08/10/ Flight operation with either one (not both) of the Front Doors removed. 06/25/ Installation of McCauley 83D32C414-[ ]/[ ]-82NDA-2 (80") or -4 (78") Propeller with Lycoming Engine. 04/26/96-2 Inst. of2110x-30 Wing Assemblies with 2167X Main Fuel Tanks per Mod Kit No /08/96-4 Installation of Aqua 2200 Floats. 09/18/ Installation of Hartzell HC-C2YR-18F/8477D-6 or HC-C3YR-1RF/F-7693(F)-( ) Propellers - Maule Drawing 5279F. Rev. A Installation of S-TEC System 55 Two Axis Autopilot Model ST-620 (14v) - Maule Dwg 9196A. Rev. A or later. (Land) Installation of S-TEC System 55 Two Axis Autopilot Model ST-620 (14v) - Maule Dwg 9196A, Rev. A or later. (Sea) Installation ofs-tec System 50 Two Axis Autopilot Model ST (14v) - Maule Dwg 9193A, Rev. 8 or later revision. Installation of S-TEC System 30 Two Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. A or later revision, (Land). Installation of S-TEC System 30 Two Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. A or later revision, (Sea). Installation of S-TEC System 20 Single Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. B or later. (Land) Installation of S-TEC System 20 Single Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. 8 or later. (Sea) 04/16/02 04/04fOO 04/04/00 01/05/00 01/21fOO 01/ /00 03/20/ Installation ofs-tec System 40 Single Axis Autopilot Model ST (14v) - Maule Dwg 9193A, Rev. C or later. 10/29/01-5 Installation of Apollo MX20 Multi-Function Display - Maule Drawing 7265A. 08/15/02

9 MAULE AEROSPACE TECHNOLOGY, INC. AIRPLANE FLIGHT MANUAL MAULE M-5-235C (sin 7470C and up) LOG OF SUPPLEMENTS Page ii supp NO. OF APPROVAL DESCRIPTION NO. PAGES DATE - 4 Installation of Aqua 2400 GW 05/ Installation of Lycoming J3A5 or IO-540-W1A5 Engine. 09/ Inst. of FluiDyne C3000H Wheel-5kis - Maule Dwg 9174A, Rev. C or later. 01/30/ Installation of FluiDyne A2500A Wheel Replacement Skis / Installation of EDO Amphibious Floats - drawing 9057A. Rev. A 12108/ Installation of Hartzell HC-C2YR-18F/F8468A-3R (81") Propeller. 09/02/ Installation of SW Instrument Cluster PIN /03/ Installation of Lamar Alternator Control System. 07/12/ Installation of EDO Floats per drawing 9143A. (05/06/85) Rev. A 12108/ Installation of Lycoming B4B5 Engine. (04/25/88) Rev. A 09/12/ Installation of McCauley 82D37C224-B/G-90RA-9 (81") Propeller. Rev. A 08110/ Installation of McCauley B3D32C414-C/G-82NDA-2 (80") Propeller Rev. A 08/10/ Flight operation with either one (not both) of the Front Doors removed. 06/25/ Installation of McCaUley 83D32C414-[ ]/[ ]-82NDA.-2 (80") or 4 (78") Propeller with Lycoming Engine. 04/26/96-2 Inst. of 2110X-30 Wing Assemblies with 2167X Main Tanks - Mod Kit No /96-4 Installation of Aqua 2200 Floats. 09/18/ Installation of Hartzell HC-C2YR-1BF/8477D-6 or HC-C3YR-1RF/F-7693(F)-( ) Propellers per Maule Drawing 5279F. Rev. A 04/16/ Installation of S-TEC System 55 Two Axis Autopilot Model ST-620 (14v) - Maule Drawing 9196A, Rev. A or later. (Land) 04/04/ Installation of S-TEC System 55 Two Axis Autopilot Model ST-620 (14v) - Maule Drawing 9196A. Rev. A or later. (Sea) 04/04/ Installation of S-TEC System 50 Two Axis Autopilot Model ST (14v)- Maule Dwg 9193A, Rev. 8 or later revision. 01/05/ Installation of S-TEC System 30 Two Axis Autopilot Model ST (14v)- Maule Dwg 9197A, Rev. A or later revision. (Land) 01/ Installation of S-TEC System 30 Two Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. A. or later revision. (Sea) 01/21/ Installation of S-TEC System 20 Single Axis Autopilot Model ST (14v)- Maule Drawing 9197A. Rev. B or later. (Land) 03/ Installation of S-TEC System 20 Single Axis Autopilot Model ST (14v) - Maule Drawing 9197A, Rev. 8 or later. (Sea) 03/20/00 Installation of S-TEC System 40 Single Axis Autopilot Model ST (14v) /29/01 Maule Drawing 9193A. Rev. C or later. - 5 Installation of Apollo MX20 Multi-Function Display - Maule Drawing 7265A. 08/15/02

10 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO.9 FOR MAULE M-S-23SC sin 7321C, 7347C, 7351C, 7363C, 7369C and up ' Reg. No. No''"""'"" This Supplement must beattachedtcithe FAA Approved Airplane Flight Manual dated 12 August 1981 whenals~rnat'c:)"i:'.control System is installed in accordance with Maule Service LetterNo.52~. -./::..;;, / ~.::;~~,.~,.~; The information contained herein supe~~~des stlpplements the information of the basic Airplane Flight Manual; for l~~~taiions, procedures and performance information not contained in this Supylement, consult the basic Airplane Flight Manual. FAA APPROVED :--/.P3!:::1.!~~-!"::::'~+==---~~----- Certification Office, FAA, Central Region DATE: JUL Page 1 of 2

11 MAULE AIRCRAFT CORPORATION MOULTRIE, GEORGIA AFM SUPPLEMENT NO. 9 for M-S-23SC sin's 7321C, 7347C, 73S1C, 7363C, 7369C and up SECTION III EMERGENCY PROCEDURES: 3.2 ALTERNATOR FAILURE: Alternator output should be monitored by reference to the ammeter located on the right side of the engine instrument cluster. Should the ammeter indicate a minus deflection when engine RPM is above 900 and/or red "ALTERNATOR OFF WARNING" light is illuminated, push ALT switch OFF then ON. Repeat two times as necessary to reset. If system will not reset, reduce the electrical load as much as possible, land as soon as practicable and investigate the electrical system malfunction before further flight. FAA APPROVED DATE: 1 2 JUL 1983 Page 2 of 2

12 MAULE AIRCRAFT CORPORATION AIRPLANE FLIGHT MANUAL MAULE M (s/n 7249C-7465C) LOG OF SUPPLEMENTS Page ii SUPP. NO. OF DESCRIPTION APPROVAL NO. PAGES DATE 1 3 Installation of EDO Amphibious Floats Maule Dwg 9134A. (09/02182) Rev.C 12/08/ Installation of Safe Flight SC-150 Angle of Attack System - Maule Dwg 6024A. 09/ Installation of EDO Floats - Maule Drawing 9138A. (04/07/83) Rev. B 12108/ Installation of FII-L1te Model 3000 MK ilia Skis - Maule Drawing 9081A. 10/28/ Installation of SW Instrument Cluster pin /03/ Installation of Lamar Alternator Control System. 07/ Installation of FluiDyne A2500A Wheel Replacement Skis. 01/06/ Inst. of complete Wing Assemblies 2150X-36U-36R, Aileron Assemblies 3225F , and Rudder Assembly 3212F 02119/ Maule Service Kit # 7 or # 10. Rev. A 03/ Installation of FluiDyne Model C2200, C3000H, or C3000AH "Airglide" Wheel Skis / Inst. of FluiDyne C3000M (Manually Operated) Skis at 2500# GW. (Applicable alethatare UAIWMaule Dwg9158A.) 11/15/ Installation of McCauley 82D37C224-B/G-90RA-9 (81") 2 Blade Propeller. (Forusewith lo-54o-w or o-54o-j engine only.) (AFMS is notrequiredwithrev. I or later AFM.) Installation of McCauley 83D32C414.C/G-82NDA-2 (80") 3 Blade Propeller. (Forusewith lo-54o-w or 0-54O-J engine only.) (AFMS is notrequiredwith rev.1or laterafm.) 03/05/92 03/05/ Inst. of McCauley B3D32C414-[ ]/[ ]-82NDA-2 (80") Q.[ -4 (78") 3 Blade Propeller with Lycoming engine. 04/26/ Installation of Wing Assemblies 2150X Maule Modification Kit No /08/97-5 Installation of AQUA 2400 GW. (07/02/82) Rev'd 01/29/ Inst. of 21 Gallon Auxiliary Fuel Tanks pin 2117X-21/-22 - Maule Mod Kit No /04/ Inst. of Hartzell HC-C2YR-18F/8477D-6 Q.[ HC-C3YR-1RF/F-7693(FH) Propeller - Maule Dwg 5279F. Rev. A 04/16/ Inst. of S-TEC System 55 Two Axis Autopilot Model ST-620 (14v) - Maule Dwg 9196A. Rev. A or later. (Land) 04/04/ Inst. of S-TEC System 55 Two Axis Autopilot Model ST-620 (14v) - Maule Dwg 9196A, Rev. A or later. (Sea) 04/04/ Inst. of S-TEC System 50 Two Axis Autopilot Model ST (14v) - Maule Dwg 9193A, Rev. 8 or later. 01/05/ Inst. of S-TEC System 30 Two Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. A or later. (Land) 01/21/ Inst. ofs-tec System 30 Two Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. A or later. (Sea) 01/21/ Inst. of S-TEC System 50 Two Axis Autopilot Model ST (28v) - Maule Dwg 9200A, Rev. A or later / Inst. of S-TEC System 20 Single Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. 8 or later. (Land) 03120/ Inst. of S-TEC System 20 Single Axis Autopilot Model ST (14v) - Maule Dwg 9197A, Rev. 8 or later. (Sea) 03/20/ Inst. of S-TEC System 20 Single Axis Autopilot Model ST (28v) - Maule Dwg 9201A, Rev. A or later. 03/20/ Inst. of S-TEC System 40 Single Axis Autopilot Model ST (14v) - Maule Dwg 9193A, Rev. C or late r. 10/29/ Inst. of S-TEC System 40 Single Axis Autopilot Model ST (28v) - Maule Dwg 9200A, Rev. B or later. 10/29/ Inst. of Wipline 3000 Amphibious Floats-Dwg 9188A, Rev. C or later. (Limited to sin 7249C-7465Cwith MK#26or 27 cjw.) 06/02/00-4 Inst. of S-TEC System 20 Single Axis Autopilot Model ST (28v) - Maule Dwg 9211A. (Land ) 06/25/01-5 Inst. of S-TEC System 30 Two Axis Autopilot Model ST (28v) - Maule Dwg 9211A. (Land) 06/25/01-5 Inst. of S-TEC System 20 Single Axis Autopilot Model ST (28v) - Maule Dwg 9211A. (Sea) 06/25/01-5 Inst. of S-TEC System 30 Two Axis Autopilot Model ST (28v) - Maule Dwg 9211A. (Sea) 06/25/01-5 Inst. of S-TEC System 20 Single Axis Autopilot Model ST (14/28v) - Maule Dwg 9212A. (Land) 10/15/01-5 Inst. of S-TEC System 30 Two Axis Autopilot Model ST (14128v) - Maule Dwg 9212A. (Land) 10/15/01-5 Installation.of Apollo MX20 Multi-Function Display - Maule Drawing 7265A /02

13 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO.6 FOR MODEL M Reg. No. Ser. No This Supplement must be attached to the FAA Approved Airplane Flight Manual dated 25 June 1981 when Alternator Control System is installed in accordance with Maule Service Letter No. 52. The information contained herein supersedes and supplements the information of the basic Airplane Flight Manual;for limitations, procedures and performance information not contained in this Supplement, consult the basic Airplane Flight Manual. FAA APPROVED :-A=Y~~L1J,.,,--~~~~'!9:.~---- Atlanta A craft Certification FAA, Central Region JUL DATE: Page 1 of 2

14 MAULE AIRCRAFT CORPORATION MOULTRIE. GEORGIA AFM SUPPLEMENT NO.6 for M-6-235C SECTION III EMERGENCY PROCEDURES: 3.2 ALTERNATOR FAILURE: Alternator output should be monitored by reference to the ammeter located on the right side of the engine instrument cluster. Should the ammeter indicate a minus deflection when engine RPM is above 900 and/ o r red "ALTERNATOR OFF WARNING" light is illuminated, push ALT switch OFF then ON. Repeat two times as necessary to reset. If system will not reset, reduce the electrical load as much as possible, land a s soon as practicable a nd investigate the electrical system malfunction before further fli~lt.., ".'. FAA APPROVED DATE:1 2 JUl 1 83 Page 2 of 2