Safety record in brief:1 NTSB accident (substantial damage, Dec 2024)8 ADs may apply833 service difficulty reports
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The fatigue failure of the forward pressure bulkhead canted web that originated from stress corrosion cracking areas. Contributing to the failure were inspection procedures and intervals inadequate to identify the fatigue cracks.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA25LA061)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2009-11-03 | Lockheed Model 382, 382B, 382E, 382F, and 382G Series Airplanes | Jun 4, 2009 | Airframe (382G-44K-30) |
| 2008-20-01 | Lockheed Model 382, 382B, 382E, 382F, and 382G Series Airplanes | Nov 3, 2008 | Airframe (382G-44K-30) |
| 2008-14-10 | Lockheed Model 382, 382B, 382E, 382F, 382G, and 382J Series Airplanes | Jul 22, 2008 | Airframe (382G-44K-30) |
| 2006-25-12 | Rolls-Royce Corporation 501-D Series Turboprop Engines | Jan 23, 2007 | Engine (501-D22A) |
| 2005-22-03 | Rolls-Royce Corporation (Formerly Allison Engine Company) 501-D22A, 501-D22C, and… | Nov 29, 2005 | Engine (501-D22A)Serial numbers per Table 1 of this AD (turbine wheel serial numbers). Only with: Engines with turbine wheels installed: P/N 6875431 1st stage S/N KK50152-KK50199; P/N 6845592 2nd stage S/N KK40998-KK41057; P/N 6845593 3rd stage S/N KK36452-KK36461 and KK36492-KK36532; P/N 6870434 4th stage S/N KK40320-KK40393 and KK40485-KK40535. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2003-14-16 | Lockheed Model 382G Series Airplanes | Aug 25, 2003 | Airframe (382G-44K-30)Serial numbers per Hercules Service Bulletin 382-52-9, dated July 5, 2000 |
| 97-21-13 | Lockheed Model 382 Series Airplanes | Nov 24, 1997 | Airframe (382G-44K-30) |
| 97-05-07 | Lockheed Model 382 Series Airplanes | Apr 4, 1997 | Airframe (382G-44K-30)Only with: Equipped with a servo-type valve housing assembly P/N 714325-3 or 714325-7 installed on any outboard engine. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
DURING SCHEDULED C-15 WHILE PERFORMING OTHER MAINTENANCE, FOUND FS777.0E UNDERFLOOR BULKHEAD VERTICAL CHANNEL DEFORMED AT LBL18, WL126-143. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS 777 BULKHEAD WEB CRACKED AT LBL14-18, WL126-143. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0319.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS 777.0E BULKHEAD WEB CRACKED AT RBL14-18, WL126-143. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK UNDER WHILE PERFORMING OTHER MAINTENANCE, FOUND FS 777.0E BULKHEAD LOWER CAP FLANGE DEFORMED AT LBL10 TO RBL18, WL126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 IAW SRM 51-60 & 51-70.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5324, FOUND RH MLG UPPER WHEEL WELL FS617 BULKHEAD RAISER PANEL CRACKED AT RBL73, WL241. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0329.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5324, FOUND RH MLG UPPER WHEEL WELL BEAM ASSY CRACKED AT FS570, RBL61, WL241. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5324, FOUND LH MLG UPPER WHEEL WELL AFT BULKHEAD RAISER PANEL CRACKED AT FS617, LBL70, WL220-245. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0331.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5314, FOUND FS337.0E UNDERFLOOR TIE DOWN END FITTING CRACKED AT LBL61, WL145. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5314, FOUND BS 557 CARGO COMPARTMENT UNDERFLOOR BULKHEAD LOWER CAP AFT FLANGE CORRODED AT LBL02, WL126. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0336.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS777.0E LH CHINE ANGLE LOWER CAP FASTENER HOLES WITH LOWER EDGE DISTANCE AT LBL61, WL145. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 833 reports.