Safety record in brief:3 NTSB accidents (substantial damage at worst, latest Feb 2016)8 ADs may apply1006 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 crack.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA16LA096)
The pilot's excessive rotation of the airplane during takeoff, which resulted in dragging the tail on the runway and substantial damage.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC07LA067)
The flight crew's improper recovery from a bounced landing. Factors associated with the accident were the selection of an unsuitable landing area, and a rough/uneven landing surface.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC01LA081)
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 B-2 CHECK UNDER JOB CARD HB5302, FOUND BS 858 LT AFT BULKHEAD CRACKED AT LBL 75, WL 225. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. NR 1001384845.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND LH AFT RING SEGMENT CRACKED AT FS869, LBL65, WL195. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-07. NR# 1001384883.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND FS968 UPR AFT BULKHEAD UPR CAP CRACKED AT LBL35, WL278. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-06. NR# 1001384884
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH AFT BULKHEAD WEB CRACKED AT FS858, LBL64, WL190. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR 1001385720.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND RT OUTER WING TRAILING EDGE FLAP TRACK FITTING CRACKED AT OWFS241.6R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR 1001385898.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK WHILE PERFORMING SP-157, FOUND LT OUTER WING FLAP BAFFLE UPPER FORWARD SKIN CRACKED AT OWFS0L. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR 1001386070.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND NR 3 FUEL TANK OUTBOARD SURGE BOX COVER SEAL RETAINER CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR 1001386245.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND FS836 LH AFT BULKHEAD WEB CRACKED AT LBL73, WL220 . / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR# 1001386651.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND FS 858 BULKHEAD FITTING CRACKED AT LBL66, WL190. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001387284.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2900, FOUND FS477 BULKHEAD WEB CRACKED AT RBL81, WL207. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001388967.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 1006 reports.