| AD Number | 47-10-15 | Status | Active |
| Effective Date | Not specified | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | N/A |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Lockheed Aircraft Corporation |
| Model(s) | 49-46 |
47-10-15 LOCKHEED: (Was Mandatory Note 17 of AD-763-3.) Applies to All Model 49 Serials Up to and Including 2075.
Compliance required prior to recertification.
Prior to recertification of all aircraft whose certificates were revoked by direction of the Administrator on July 11, 1946, the following Service Documents must be complied with.
LOCKHEED SERVICE BULLETINS:
*49/SB-50, revised August 24, 1946 - Revision of Cabin Air Recirculating Fan.
49/SB-58, dated July 22, 1946 - Sealing of Main Landing Gear Doors.
49/SB-86, dated July 18, 1946 - Rerouting of Thermocouple Wires.
*49/SB-91, revised September 10, 1946 - Replacements of Electrical Power Feed-Through Studs.
*49/SB-93, revised August 11, 1946 - Rework of Exhaust System Ball Joints and Collector Segment.
49/SB-95, dated July 22, 1946 - Insulation of Generator Circuit Breakers.
(a) 49/SB-97, revised October 28, 1946 - Sealing, Draining, and Ventilation of Nacelles.
49/SB-98, dated July 26, 1946 - Removal of Engine Filtered Air Components and Plumbing.
*49/SB-100, revised August 27, 1946 - Replacement of Fuel Pressure Warning Units.
49/SB-101, revised August 6, 1947 - Modification of Hydraulic Pump Case Drain Lines.
49/SB-102, dated July 23, 1946 - Relocation of Engine Fuel Pump Lines.
49/SB-104, revised July 23, 1946 - Replacement of Windshield Wiper Motor Circuit Fuse.
49/SB-106, dated July 22, 1946 - Replacement of Windshield Heater Wire.
49/SB-109, revised August 22, 1946 - Provision for Vacuum Pump Cooling.
49/SB-113, revised August 6, 1946 - Replacement of Aluminum Electrical Wires and Terminals.
49/SB-114, revised July 31, 1946 - Protection of Electrical Receptacle.
49/SB-115, dated July 23, 1946 - Insulation of Galley Circuit Breaker.
49/SB-116, revised August 2, 1946 - Installation of Generator Field Circuit Breaker (Switch Type).
*49/SB-117, revised September 5, 1946 - Insulation of Right Angle Electrical Terminals and Electrical Wiring.
49/SB-118, revised August 10, 1946 - Support of Electrical Wiring in Main Gear Wheel Well.
49/SB-119, revised July 27, 1946 - Sealing of Main Landing Gear Door Hinge.
49/SB-119A, revised August 13, 1946 - Sealing of Main Landing Gear Doors.
*49/SB-121, revised September 16, 1946 - Installation of Fire Resistant Hoses and Double Hose Clamps in Nacelle Zones 2 and 3.
49/SB-122, dated July 25, 1946 - Installation of Stainless Steel CO2 Lines.
*49/SB-123, revised August 27, 1946 - Replacement of Alcohol Tank, Supply Lines and Vent Line (4-pump system).
49/SB-125, dated June 23, 1946 - Removal of Cargo Compartment Insulation.
49/SB-126, dated July 23, 1946 - Protection of Electrical Junctions and Disconnects at Fire Wall.
49/SB-127, revised July 31, 1946 - Sealing of Cabin Heater Panel.
49/SB-131, revised August 10, 1946 - Rerouting of Drain Line for Deicer Distributor Oil Separator.
49/SB-132, revised August 12, 1946 - Attachment of Electrical Wire Bundles in Forward Passenger Compartment.
49/SB-133, revised July 31, 1946 - Installation of Brass Liners and Double Hose Clamps in Line Between Sump Tank and Propeller Feathering Pump.
(a) 49/SB-134, revised October 28, 1946 - Installation of Protective Shield for Engine Torquemeter Plumbing.
49/SB-135, revised August 11, 1946 - Addition of Fuselage Drain Provisions.
49/SB-136, dated July 31, 1946 - Protection of Cabin Heater Flexible Fuel Line.
49/SB-137, dated July 27, 1946 - Addition of Double Hose Clamps on Inboard Fuel Tank Interconnection Line.
*49/SB-138, revised September 25, 1946 - Provisions for Increase of CO2 Capacity.
*49/SB-155, revised August 28, 1946 - Installation of Copper Wires in Lieu of Aluminum Wires.
**49/SB-161, dated August 29, 1946 - Replacement of Alcohol Tank, Supply Lines, and Vent Line 2-pump system).
LOCKHEED SERVICE INSTRUCTIONS:
*49/SI-22, revised October 10, 1946 - Installation of Engine Plumbing and Electrical Wiring Heat Protective System. *49/SI-41, revised August 16, 1946 - Nacelle Fire Extinguishing System Revisions.
49/SI-105, revised August 7, 1946 - Replacement of Hydraulic Secondary Return Line.
LOCKHEED SERVICE INFORMATION LETTERS:
*No. 42, revised September 10, 1946 (Canceled).
No. 56, dated August 10, 1946 - Periodic Inspection of Vacuum Pump Pressure Hose.
No. 57, revised August 15, 1946 - Fuselage Fire Control and Smoke Elimination Procedures.
No. 58, revised August 15, 1946 - Combating Belly Cargo Compartment and Fuselage Fires.
No. 60, dated August 10, 1946 (Canceled).
TWA Engineering Order No. 2762 - Rework of Auxiliary Hydraulic Supply Tank and Discharge Line.
*Service Documents identified by an asterisk and by (a) have been revised subsequent to issuance of AD-763 (Special) dated Aug. 21, 1946, as indicated by the later revision date effective in each instance. Aircraft previously recertificated in accordance with AD-763 (Special) should be checked for compliance with these later revisions within next 200 hours of operations.
**Service Bulletin 49/SB-161 was not called for in AD-763 (Special), but has subsequently been found necessary, inasmuch as Bulletin 49/SB-123 does not adequately describe changes to 2-pump anti-icing systems. Aircraft incorporating 2-pump anti-icing systems should be checked for conformity with Bulletin 49/SB-161 prior to certification.