AD 48-26-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed Aircraft Corporation | 649-79 | LOCKHEED Models 649 and 749 Series Aircraft |
| aircraft | Lockheed Aircraft Corporation | 749-79 | LOCKHEED Models 649 and 749 Series Aircraft |
Unsafe Condition
Failures under certain operating conditions due to engine speed operation outside specified ranges.
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Required Actions
Install two placards in the cockpit (temporary by July 8, 1948, and permanent by August 1, 1948), mark all tachometers with specified bands and radial lines by August 1, 1948.
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Compliance Time
Compliance required by July 7, 1948, and August 1, 1948.
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Affected Aircraft
Lockheed Models 649 and 749 Series Aircraft equipped with Curtiss C632S-A14/850-4C2-0 Propellers.
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Federal Register Abstract
Engine Speed Restrictions-Curtiss Prop
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_48-26-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 48-26-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED Models 649 and 749 Series Aircraft Subject: Engine Speed Restrictions-Curtiss Prop Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Lockheed Aircraft Corporation Model: 649-79 | 749-79 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 48-26-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 48-26-01 SUBJECT HEADING: LOCKHEED Models 649 and 749 Series Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 48-26-01 LOCKHEED: Applies to 649 and 749 Series Aircraft Equipped With Curtiss C632S-A14/850-4C2-0 Propellers. Compliance required by July 7, 1948, and August 1, 1948. To avoid failures under certain operating conditions, the following engine speed restrictions must be observed and two placards covering these restrictions must be installed in the cockpit. (Temporary placards must be installed not later than July 8, 1948, and permanent placards to be supplied by Lockheed installed not later than August 1, 1948.) One placard must be in full view of the pilots and one in full view of the flight engineer. Placards should read as follows: "In flight avoid continuous operation below 1,625 r.p.m. and between 1,725 and 1,850 r.p.m., 1,900 and 2,000 r.p.m., and between 2,100 and 2,375 r.p.m. On ground avoid continuous operation between 1,200 and 1,450 r.p.m." For visual reference, all tachometers in the airplane must be marked as follows not later than August 1, 1948: "Red Band 1,200 to 1,625 r.p.m. Green band 1,625 to 1,725 r.p.m. with green radial line at 1,675 r.p.m. Red band 1,725 to 1,850 r.p.m. with green radial line at 1,875 r.p.m. Red band 1,900 to 2,000 r.p.m. Green band 2,000 to 2,100 r.p.m. with green radial line at 2,050 r.p.m. Red band 2,100 to 2,375 r.p.m. with green radial line at 2,400 r.p.m. Yellow band 2,400 to 2,800 r.p.m. with red radial line at 2,800 r.p.m." FOOTER:
Document Text
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AD Final Rules - DRS_48-26-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 48-26-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED Models 649 and 749 Series Aircraft Subject: Engine Speed Restrictions-Curtiss Prop Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Lockheed Aircraft Corporation Model: 649-79 | 749-79 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 48-26-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 48-26-01 SUBJECT HEADING: LOCKHEED Models 649 and 749 Series Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 48-26-01 LOCKHEED: Applies to 649 and 749 Series Aircraft Equipped With Curtiss C632S-A14/850-4C2-0 Propellers. Compliance required by July 7, 1948, and August 1, 1948. To avoid failures under certain operating conditions, the following engine speed restrictions must be observed and two placards covering these restrictions must be installed in the cockpit. (Temporary placards must be installed not later than July 8, 1948, and permanent placards to be supplied by Lockheed installed not later than August 1, 1948.) One placard must be in full view of the pilots and one in full view of the flight engineer. Placards should read as follows: "In flight avoid continuous operation below 1,625 r.p.m. and between 1,725 and 1,850 r.p.m., 1,900 and 2,000 r.p.m., and between 2,100 and 2,375 r.p.m. On ground avoid continuous operation between 1,200 and 1,450 r.p.m." For visual reference, all tachometers in the airplane must be marked as follows not later than August 1, 1948: "Red Band 1,200 to 1,625 r.p.m. Green band 1,625 to 1,725 r.p.m. with green radial line at 1,675 r.p.m. Red band 1,725 to 1,850 r.p.m. with green radial line at 1,875 r.p.m. Red band 1,900 to 2,000 r.p.m. Green band 2,000 to 2,100 r.p.m. with green radial line at 2,050 r.p.m. Red band 2,100 to 2,375 r.p.m. with green radial line at 2,400 r.p.m. Yellow band 2,400 to 2,800 r.p.m. with red radial line at 2,800 r.p.m." FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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