# N401LC: 1975 Lockheed 382G-44K-30 - Status: Valid registration - Airframe: [Lockheed 382G-44K-30](https://openairdocs.org/model/lockheed-382g-44k-30) (registry code 526414Z, 3 seats) - Engine: [Allison 501-D22A](https://openairdocs.org/engine/allison-501-d22a) (registry code 03006) - Data sheets: [TCDS E-282](https://openairdocs.org/tcds/E-282) (Rolls-Royce Corporation) (OpenAirDocs) - Serial number: 4606 - Year built: 1975 - Type: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Restricted, other - Airworthiness date: January 8, 2025 - Certificate issued: April 21, 1997 - Expires: January 31, 2030 - Mode S code: A4B155 - Registered owner: [Lynden Air Cargo LLC](https://openairdocs.org/faa-owner/LYNDEN%20AIR%20CARGO%20LLC) - Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage) - Owner type: LLC - Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=401LC - Page: https://openairdocs.org/aircraft/N401LC From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 4 in force ### Matched by airframe (Lockheed 382G-44K-30) None in force. ### Matched by engine (Allison 501-D22A) - [AD 2006-25-12](https://openairdocs.org/ad/2006-25-12): Removal from service of certain turbine rotor components · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 6 more. Effective Jan 23, 2007 - [AD 2005-22-03](https://openairdocs.org/ad/2005-22-03): 1st stage, 2nd stage, 3rd stage, and 4th stage turbine wheels · Rolls-Royce 501-D22A, 501-D22C and 501-D22G. Effective Nov 29, 2005 - [AD 75-07-06](https://openairdocs.org/ad/75-07-06): Second Stage Turbine Blades · Rolls-Royce 501-D22A. Effective Apr 7, 1975 - [AD 69-21-03](https://openairdocs.org/ad/69-21-03): First Stage Compressor Wheels · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 6 more. Effective Oct 21, 1969 ### Historical (superseded or no longer in force) - [AD 2003-07-02](https://openairdocs.org/ad/2003-07-02) (historical): Turbine rotor components · 501-D13, 501-D13A, 501-D13D and 6 more. Effective May 7, 2003 ## Information bulletins (advisory) None matched. ## NTSB investigations (3) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA16LA096](https://openairdocs.org/ntsb/DCA16LA096), Feb 12, 2016: Lockheed 382G (N401LC), Iliamna, AK, substantial damage. Probable cause: 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… - [NTSB ANC07LA067](https://openairdocs.org/ntsb/ANC07LA067), Jul 19, 2007: Lockheed 382G-44K-30 (N401LC), McGrath, AK, substantial damage. Probable cause: The pilot's excessive rotation of the airplane during takeoff, which resulted in dragging the tail on the runway and substantial damage. - [NTSB ANC01LA081](https://openairdocs.org/ntsb/ANC01LA081), Jul 2, 2001: Lockheed L-382G (N401LC), Lake Minchumina, AK, substantial damage. Probable cause: 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. ## FAA accident and incident reports (3) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20160212002039A](https://openairdocs.org/incident/20160212002039A), Feb 12, 2016: Lockheed 382G-44K-30 (N401LC), Iliamna, AK, Substantial damage. Aircraft departed bethel AK, en route to elmendorf afb AK, pilot declared emergency after a rapid decompression indication. Pilot requested and was cleared to… - [Accident 20070718014889A](https://openairdocs.org/incident/20070718014889A), Jul 18, 2007: Lkheed 382G (N401LC), Mcgrath, AK, Substantial damage. (-23) Aircraft struck tail during takeoff rotation from a remote Alaska mining strip. The first indication of a problem occurred during climbout when the… - [Accident 20010702017079A](https://openairdocs.org/incident/20010702017079A), Jul 2, 2001: Lkheed 382G (N401LC), Minchumina, AK, No damage. (-23) Captain was landing on a 4,200 feet long, 90 feet wide, gravel runway. The runway had a number of frost-heaves that had developed during the past winter.… ## Service difficulty reports (1,007, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR LR7A2026061603833](https://openairdocs.org/sdr/LR7A2026061603833), Jun 16, 2026: SPAR. CRACKED. DURING SCHEDULED B-2 CHECK WHILE PERFORMING SP-123, FOUND RH OUTER WING FORWARD SPAR EXTERNAL TANK ATTACH FITTING HOLES DAMAGED AT FS517, OWS72R & OWS90R, WL266 - [SDR LR7A2026061603832](https://openairdocs.org/sdr/LR7A2026061603832), Jun 16, 2026: SPAR. DAMAGED. DURING SCHEDULED B-2 CHECK WHILE PERFORMING SP-123, FOUND LH OUTER WING FORWARD SPAR EXTERNAL TANK ATTACH FITTING HOLES DAMAGED AT FS517, OWS72L & OWS90L, WL266 - [SDR LR7A2026061603831](https://openairdocs.org/sdr/LR7A2026061603831), Jun 16, 2026: BULKHEAD WEB. CRACKED. 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 - [SDR LR7A2026061603830](https://openairdocs.org/sdr/LR7A2026061603830), Jun 16, 2026: FITTING. CRACKED. DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND FS 858 BULKHEAD FITTING CRACKED AT LBL66, WL190. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP58 - [SDR LR7A2026061603829](https://openairdocs.org/sdr/LR7A2026061603829), Jun 16, 2026: BULKHEAD WEB. CRACKED. 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 - [SDR LR7A2026061603828](https://openairdocs.org/sdr/LR7A2026061603828), Jun 16, 2026: RETAINER. CRACKED. DURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND NR 3 FUEL TANK OUTBOARD SURGE BOX COVER SEAL RETAINER CRACKED. REPAIR BY REPLACEMENT ACCOMP - [SDR LR7A2026061603827](https://openairdocs.org/sdr/LR7A2026061603827), Jun 16, 2026: SKIN. CRACKED. 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, FIGU - [SDR LR7A2026061603826](https://openairdocs.org/sdr/LR7A2026061603826), Jun 16, 2026: FITTING. CRACKED. 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 - [SDR LR7A2026061603825](https://openairdocs.org/sdr/LR7A2026061603825), Jun 16, 2026: BULKHEAD WEB. CRACKED. DURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH AFT BULKHEAD WEB CRACKED AT FS858, LBL64, WL190. REPAIRED IAW LOCKHEED SMP583 SRM, FIGUR - [SDR LR7A2026061603824](https://openairdocs.org/sdr/LR7A2026061603824), Jun 16, 2026: CAP. CRACKED. 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 - [SDR LR7A2026061603823](https://openairdocs.org/sdr/LR7A2026061603823), Jun 16, 2026: FRAME. CRACKED. 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. N - [SDR LR7A2026061603822](https://openairdocs.org/sdr/LR7A2026061603822), Jun 16, 2026: TEE ANGLE. CRACKED. 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 - [SDR LR7A2025031103751](https://openairdocs.org/sdr/LR7A2025031103751), Mar 11, 2025: INTERCOSTAL. CORRODED. DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND 9G BARRIER NET INTERCOSTAL CORRODED AT FS317.0E, LBL81, WL206. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW - [SDR LR7A2025031103750](https://openairdocs.org/sdr/LR7A2025031103750), Mar 11, 2025: INTERCOSTAL. CORRODED. DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND 9G BARRIER NET INTERCOSTAL CORRODED AT FS317.0E, RBL70, WL161. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW - [SDR LR7A2025031103749](https://openairdocs.org/sdr/LR7A2025031103749), Mar 11, 2025: BULKHEAD. CRACKED. DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FS902 BULKHEAD CAP CRACKED AT RBL62, WL215. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. NR#100 - [SDR LR7A2024081603474](https://openairdocs.org/sdr/LR7A2024081603474), Aug 16, 2024: SKIN. DAMAGED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH CENTER FUSELAGE SKIN WITH DAMAGED FASTENER HOLES AT FS245.5, WL267-276, RBL29-54. / REP - [SDR LR7A2024081603473](https://openairdocs.org/sdr/LR7A2024081603473), Aug 16, 2024: FRAME. DAMAGED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT WITH DAMAGED FASTENER HOLES AT FS330, WL166, LBL79. / REPA - [SDR LR7A2024081603472](https://openairdocs.org/sdr/LR7A2024081603472), Aug 16, 2024: SKIN. DAMAGED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT WITH DAMAGED FASTENER HOLES AT FS324, WL146-156, LBL173. / - [SDR LR7A2024081603471](https://openairdocs.org/sdr/LR7A2024081603471), Aug 16, 2024: SKIN. DAMAGED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH FUSELAGE SKIN DAMAGED AT FS284-289, RBL80, WL165.5. / REPAIRED IAW LOCKHEED SMP583 SRM, - [SDR LR7A2024081603470](https://openairdocs.org/sdr/LR7A2024081603470), Aug 16, 2024: FRAME. DAMAGED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH CENTER FUSELAGE RING SEGMENT DAMAGED AT FS324, WL183, RBL80. / REPAIRED IAW LOCKHEED SM - [SDR LR7A2024081603469](https://openairdocs.org/sdr/LR7A2024081603469), Aug 16, 2024: FRAME. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT CORRODED AT FS330, LBL62, WL142. / REPAIRED IAW LOCKHEED S - [SDR LR7A2024081603468](https://openairdocs.org/sdr/LR7A2024081603468), Aug 16, 2024: SKIN. DAMAGED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE SKIN WITH DAMAGED FASTENER HOLES AT FS305-310, LBL61, WL144. / REPAIRED - [SDR LR7A2024081603467](https://openairdocs.org/sdr/LR7A2024081603467), Aug 16, 2024: ANGLE. CRACKED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE SKIN ATTACH ANGLE CRACKED AT FS517-597, LBL64. / REPAIR BY REPLACEMENT - [SDR LR7A2024081603466](https://openairdocs.org/sdr/LR7A2024081603466), Aug 16, 2024: SKIN. CRACKED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE SKIN CRACKED AT FS341, LBL61, WL144. / REPAIRED IAW LOCKHEED SMP583 SRM - [SDR LR7A2024081603465](https://openairdocs.org/sdr/LR7A2024081603465), Aug 16, 2024: FRAME. CRACKED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT CRACKED AT FS310, LBL61, WL145. / REPAIRED IAW LOCKHEED SM - [SDR LR7A2024081603464](https://openairdocs.org/sdr/LR7A2024081603464), Aug 16, 2024: STRINGER. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE STRINGER CORRODED AT FS537-557, LBL24. / REPAIR BY REPLACEMENT ACCOMPLI - [SDR LR7A2024081603463](https://openairdocs.org/sdr/LR7A2024081603463), Aug 16, 2024: STRINGER. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTER FUSELAGE STRINGER AT FS537-557, BL0. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKH - [SDR LR7A2024081603462](https://openairdocs.org/sdr/LR7A2024081603462), Aug 16, 2024: CHINE. CRACKED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH CHINE CAP CRACKED AT FS737.0E-817.0E RBL60, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED - [SDR LR7A2024081603461](https://openairdocs.org/sdr/LR7A2024081603461), Aug 16, 2024: STIFFENER. CRACKED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH AFT FUSELAGE STIFFENER CRACKED AT FS831, LBL62, WL160. / REPAIR BY REPLACEMENT ACCOMPLI - [SDR LR7A2024081603460](https://openairdocs.org/sdr/LR7A2024081603460), Aug 16, 2024: FRAME. CRACKED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH FS825 AFT FUSELAGE RING SEGMENT CRACKED AT LBL62, WL160. / REPAIRED IAW LOCKHEED SMP583 - [SDR LR7A2024081603459](https://openairdocs.org/sdr/LR7A2024081603459), Aug 16, 2024: STIFFENER. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND NOSE WHEEL WELL HORIZONTAL STIFFENER CORRODED AT FS148. / REPAIR BY REPLACEMENT ACCOMPLISH - [SDR LR7A2024081603458](https://openairdocs.org/sdr/LR7A2024081603458), Aug 16, 2024: BEAM. CRACKED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH MLG BOW BEAM CRACKED AT FS577, WL150, LBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW L - [SDR LR7A2024081603457](https://openairdocs.org/sdr/LR7A2024081603457), Aug 16, 2024: ATTACH ANGLE. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH PORK CHOP ATTACH ANGLE CORRODED AT FS577, LBL60, WL136. / REPAIR BY REPLACEMENT ACCOMPL - [SDR LR7A2024081603456](https://openairdocs.org/sdr/LR7A2024081603456), Aug 16, 2024: PRESSURE BLKHD. CRACKED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH MLG PRESSURE SKIN TO INTERCOSTAL ATTACH ANGLE CRACKED AT FS507, RBL62, WL160. / REPAIRE - [SDR LR7A2024081603455](https://openairdocs.org/sdr/LR7A2024081603455), Aug 16, 2024: LONGERON. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH SLOPING LONGERON END FITTING CORRODED AT FS817.0E/737-750, LBL61. / REPAIR BY REPLACEME - [SDR LR7A2024081603454](https://openairdocs.org/sdr/LR7A2024081603454), Aug 16, 2024: CHINE. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH FS517 CHINE CAP CORRODED AT LBL60, WL146. / REPAIRED IAW LAC MEA 382-53-24-130. NR# 100 - [SDR LR7A2024081603453](https://openairdocs.org/sdr/LR7A2024081603453), Aug 16, 2024: STIFFENER. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTER FUSELAGE BELLY SKIN STIFFENER CRACKED AT FS587, LBL10, WL129. / REPAIRED IAW LOCKHE - [SDR LR7A2024081603452](https://openairdocs.org/sdr/LR7A2024081603452), Aug 16, 2024: FRAME. CORRODED. DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND RH CENTER FUSELAGE RING SEGMENT CORRODED AT FS627, RBL75, WL161. / REPAIRED IAW LOCKHEED SMP583 SRM, FI - [SDR LR7A2024081603451](https://openairdocs.org/sdr/LR7A2024081603451), Aug 16, 2024: CHINE. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CHINE END FITTING CORRODED AT FS345.0E/245, WL145, LBL61. / REPAIR BY REPLACEMENT ACCOMPLI - [SDR LR7A2024081603450](https://openairdocs.org/sdr/LR7A2024081603450), Aug 16, 2024: PRESSURE BLKHD. CORRODED. DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND LH UPPER MLG PRESSURIZED WEB CORRODED AT FS603, LBL62, WL228. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGUR - [SDR LR7A2024081603449](https://openairdocs.org/sdr/LR7A2024081603449), Aug 16, 2024: BEAM. CORRODED. DURING SCHEDULED C-15 CHECK UNDER SP-309, FOUND RH FWD MLG BEAM CORRODED AT FS517, RBL62.5-65, WL140-145. / REPAIRED IAW LAC MEA 382-53-24-088. NR# 1001136902, - [SDR LR7A2024081603448](https://openairdocs.org/sdr/LR7A2024081603448), Aug 16, 2024: BEAM. CORRODED. DURING SCHEDULED C-15 CHECK UNDER SP-309, FOUND LH FWD MLG BEAM CORRODED AT FS517, WL140-146, LBL62. / REPAIRED IAW LAC MEA 382-53-24-089. NR# 1001136901, 10011 - [SDR LR7A2024081603447](https://openairdocs.org/sdr/LR7A2024081603447), Aug 16, 2024: CHINE. CORRODED. DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND LH CHINE CAP CORRODED AT FS597, LBL61, WL146. / REPAIRED IAW LAC MEA 382-53-24-107. NR# 1001136818. / P - [SDR LR7A2024081603446](https://openairdocs.org/sdr/LR7A2024081603446), Aug 16, 2024: FLOORBEAM. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FLOOR BEAM LOWER CAP CORRODED AT FS245, BL0-LBL40, WL128. / REPAIR BY REPLACEMENT ACCOMPLI - [SDR LR7A2024081603445](https://openairdocs.org/sdr/LR7A2024081603445), Aug 16, 2024: FRAME. CORRODED. DURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT CORRODED AT FS290.0E, LBL63, WL143. / REPAIRED IAW LOCKHEE - [SDR LR7A2024081603444](https://openairdocs.org/sdr/LR7A2024081603444), Aug 16, 2024: SKIN. DAMAGED. DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5712, FOUND RH OUTBOARD WING FLAP LOWER SKIN DAMAGED AT WOFS176-182R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51 - [SDR LR7A2024081603443](https://openairdocs.org/sdr/LR7A2024081603443), Aug 16, 2024: FRAME. CORRODED. DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5317, FOUND LH AFT FUSELAGE RING SEGMENT CORRODED AT FS748, WL156, LBL67. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGUR - [SDR LR7A2024081603442](https://openairdocs.org/sdr/LR7A2024081603442), Aug 16, 2024: BEAM. CORRODED. DURING SCHEDULED C-15 CHECK UNDER JOB CARD WHILE PERFORMING OTHER MAINTENANCE, FOUND RH MLG BEAM CORRODED AT FS597, RBL63, WL150. / REPAIRED IAW LAC MEA 382-53- - [SDR LR7A2024081603441](https://openairdocs.org/sdr/LR7A2024081603441), Aug 16, 2024: FRAME. DAMAGED. DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5302, FOUND RH CENTER FUSELAGE RING SEGMENT DAMAGED AT FS697, WL152, RBL63. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG - [SDR LR7A2024081603440](https://openairdocs.org/sdr/LR7A2024081603440), Aug 16, 2024: FRAME. DAMAGED. DURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5302, FOUND RH CENTER FUSELAGE RING SEGMENT DAMAGED AT FS687, RBL63, WL152. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG All 1,007: https://openairdocs.org/aircraft/N401LC/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Lockheed 382G-44K-30 aircraft: https://openairdocs.org/model/lockheed-382g-44k-30/aircraft.md - The Allison 501-D22A engine: https://openairdocs.org/engine/allison-501-d22a.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.