MIflyer
1st Lieutenant
From Air Force Magazine:
Hundreds of F-35s could have the wrong fasteners in "critical areas," according to the Defense Contract Management Agency. But F-35 builder Lockheed Martin says the problem may not need to be fixed.
"All aircraft produced prior to discovery of this [problem] have titanium fasteners incorrectly installed in locations where the design calls for Inconel," the F-35 Joint Program Office said in an email in response to a query from Air Force Magazine. "Because of this, the engineering safety analysis of the issue has assumed that each critical F-35 joint was assembled with the incorrect fasteners."
Inconel is an alloy of nickel and chromium, and is supposed to be used in places where greater strength and corrosion resistance are required, while the titanium bolts are used in areas where its strength and lightness helps reduce weight. Titanium, however, has a lower shear strength than Inconel.
Both fasteners are called "eddie bolts" and are similar in appearance except for a number stamped on them. The titanium bolts cost about $5 apiece, while the Inconel parts cost about $20 each. A Lockheed spokeswoman said the two parts are "very difficult to distinguish, visually."
The Lockheed spokesman said an initial analysis concluded that "titanium has sufficient strength in locations that called for Inconel eddie bolts." Another Lockheed official said components are built with "twice the strength specified," but he did not specify whether this was the case with the titanium eddie bolts.
The JPO said analysis as of Jan. 9 concluded "that no aircraft operating restrictions or inspections are necessary at this time." It added that "the JPO will release a fleet guidance report" at the conclusion of the Root Cause and Corrective Action (RCCA) analysis, now being performed by Lockheed. The DCMA said it and the JPO are supervising Lockheed's analysis to ensure it is performed without bias.
In addition to the F-35 production line at Ft. Worth, Texas, the commingling of the two types of bolts was also discovered at the Italian F-35 Final Assembly and Check-Out (FACO) facility, but not the one in Japan, the DCMA reported.
Lockheed plans to submit its report to the DCMA and JPO in February, and the company expects it "to be approved," its spokeswoman said. As to how the issue occurred, she explained that "several fastener bins were found on the factory floor with commingled fasteners at Lockheed Martin locations and several supplier locations."
Inspections of some aircraft—Lockheed did not specify how many, or who had conducted the inspections—"indicated high levels of compliant fastener installations," and
an engineering review "has been completed and is in review with the customer," the spokeswoman said.
The company believes that once its analysis is approved, "no rework will be required for aircraft in the fleet," she said, but did not identify other corrective actions.
Similar quality issues occurred with the F-16, where workers threw leftover fasteners into the wrong bin at the end of a shift. Such problems can often take months to be discovered.
According to the DCMA, there are more than 48,000 fasteners of the two types on an F-35 fighter. The Air Force's F-35As have 848 Inconel bolts out of 48,919 total fasteners, or about 1.7 percent of the total. The Marine Corps' F-35B model has 877 Inconel fasteners out of 50,603, also 1.7 percent. The Navy's F-35C carrier-capable model, though, which has to endure the shock of repeated hard landings on an aircraft carrier, and is larger and heavier than the other two variants, has 51,353 fasteners, of which 1,813, or 3.5 percent, are made of Inconel.
Hundreds of F-35s could have the wrong fasteners in "critical areas," according to the Defense Contract Management Agency. But F-35 builder Lockheed Martin says the problem may not need to be fixed.
"All aircraft produced prior to discovery of this [problem] have titanium fasteners incorrectly installed in locations where the design calls for Inconel," the F-35 Joint Program Office said in an email in response to a query from Air Force Magazine. "Because of this, the engineering safety analysis of the issue has assumed that each critical F-35 joint was assembled with the incorrect fasteners."
Inconel is an alloy of nickel and chromium, and is supposed to be used in places where greater strength and corrosion resistance are required, while the titanium bolts are used in areas where its strength and lightness helps reduce weight. Titanium, however, has a lower shear strength than Inconel.
Both fasteners are called "eddie bolts" and are similar in appearance except for a number stamped on them. The titanium bolts cost about $5 apiece, while the Inconel parts cost about $20 each. A Lockheed spokeswoman said the two parts are "very difficult to distinguish, visually."
The Lockheed spokesman said an initial analysis concluded that "titanium has sufficient strength in locations that called for Inconel eddie bolts." Another Lockheed official said components are built with "twice the strength specified," but he did not specify whether this was the case with the titanium eddie bolts.
The JPO said analysis as of Jan. 9 concluded "that no aircraft operating restrictions or inspections are necessary at this time." It added that "the JPO will release a fleet guidance report" at the conclusion of the Root Cause and Corrective Action (RCCA) analysis, now being performed by Lockheed. The DCMA said it and the JPO are supervising Lockheed's analysis to ensure it is performed without bias.
In addition to the F-35 production line at Ft. Worth, Texas, the commingling of the two types of bolts was also discovered at the Italian F-35 Final Assembly and Check-Out (FACO) facility, but not the one in Japan, the DCMA reported.
Lockheed plans to submit its report to the DCMA and JPO in February, and the company expects it "to be approved," its spokeswoman said. As to how the issue occurred, she explained that "several fastener bins were found on the factory floor with commingled fasteners at Lockheed Martin locations and several supplier locations."
Inspections of some aircraft—Lockheed did not specify how many, or who had conducted the inspections—"indicated high levels of compliant fastener installations," and
an engineering review "has been completed and is in review with the customer," the spokeswoman said.
The company believes that once its analysis is approved, "no rework will be required for aircraft in the fleet," she said, but did not identify other corrective actions.
Similar quality issues occurred with the F-16, where workers threw leftover fasteners into the wrong bin at the end of a shift. Such problems can often take months to be discovered.
According to the DCMA, there are more than 48,000 fasteners of the two types on an F-35 fighter. The Air Force's F-35As have 848 Inconel bolts out of 48,919 total fasteners, or about 1.7 percent of the total. The Marine Corps' F-35B model has 877 Inconel fasteners out of 50,603, also 1.7 percent. The Navy's F-35C carrier-capable model, though, which has to endure the shock of repeated hard landings on an aircraft carrier, and is larger and heavier than the other two variants, has 51,353 fasteners, of which 1,813, or 3.5 percent, are made of Inconel.