# N408LC: 1975 Lockheed 382G

- Status: Valid registration
- Airframe: [Lockheed 382G](https://openairdocs.org/model/lockheed-382g) (registry code 526414U, 3 seats)
- Engine: [Allison 501-D22A](https://openairdocs.org/engine/allison-501-d22a) (registry code 03006)
- Data sheets: [TCDS A1SO](https://openairdocs.org/tcds/A1SO) (Lockheed Martin Corporation), [TCDS E-282](https://openairdocs.org/tcds/E-282) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 4600
- Year built: 1975
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Restricted, other
- Airworthiness date: January 16, 2025
- Certificate issued: March 6, 2023
- Expires: March 31, 2030
- Mode S code: A4CB56
- 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=408LC
- Page: https://openairdocs.org/aircraft/N408LC

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): 54 in force

### Matched by airframe (Lockheed 382G)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2024-01-02](https://openairdocs.org/ad/2024-01-02): Fuselage · Lockheed 382, 382B, 382E and 9 more. Effective Jan 24, 2024
- [AD 2023-22-06](https://openairdocs.org/ad/2023-22-06): Powerplant · Lockheed Martin 382, 382B, 382E and 8 more. Effective Nov 21, 2023
- [AD 2023-11-10](https://openairdocs.org/ad/2023-11-10): Fuselage · Lockheed Martin 382, 382B, 382E and 9 more. Effective Jul 11, 2023
- [AD 2023-09-13](https://openairdocs.org/ad/2023-09-13): Wings · Lockheed Martin 382, 382B, 382E and 7 more. Effective May 31, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-09-15](https://openairdocs.org/ad/2021-09-15): Wings · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Jun 1, 2021
- [AD 2019-25-20](https://openairdocs.org/ad/2019-25-20): Flight controls · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Feb 28, 2020
- [AD 2015-22-11](https://openairdocs.org/ad/2015-22-11): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 28, 2015
- [AD 2015-18-02](https://openairdocs.org/ad/2015-18-02): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 17, 2015
- [AD 2015-06-08](https://openairdocs.org/ad/2015-06-08): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 14, 2015
- [AD 2015-05-08](https://openairdocs.org/ad/2015-05-08): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Apr 24, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2012-06-09](https://openairdocs.org/ad/2012-06-09): Standard practices/structures · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 15, 2012
- [AD 2011-15-02](https://openairdocs.org/ad/2011-15-02): Fuel · Lockheed Martin 382, 382B, 382E and 2 more. Effective Aug 19, 2011
- [AD 2009-11-03](https://openairdocs.org/ad/2009-11-03): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 4, 2009
- [AD 2009-08-01](https://openairdocs.org/ad/2009-08-01): Honeywell FMSs · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R), CL-600-2B16 (CL-604) and 11 more. Effective May 14, 2009
- [AD 2008-14-10](https://openairdocs.org/ad/2008-14-10): Upper engine mount bolts · Lockheed Martin 382, 382B, 382E and 3 more. Effective Jul 22, 2008
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2003-14-16](https://openairdocs.org/ad/2003-14-16): Latch mechanism · Lockheed Martin 382G. Effective Aug 25, 2003
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [AD 99-25-04](https://openairdocs.org/ad/99-25-04): Floor to Ring Fittings · Lockheed Martin 382, 382B, 382E and 3 more. Effective Jan 7, 2000
- [AD 97-21-13](https://openairdocs.org/ad/97-21-13): AFM - Power Levers · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 24, 1997
- [AD 97-05-07](https://openairdocs.org/ad/97-05-07): AFM Supplement 382-16 · Lockheed Martin 382, 382E and 382G. Effective Apr 4, 1997
- [AD 97-04-15](https://openairdocs.org/ad/97-04-15): Fire Extinguisher Bottle Cartridges · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 24 more. Effective Mar 7, 1997
- [AD 96-24-14](https://openairdocs.org/ad/96-24-14): Main Landing Gear Brakes Inspection · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jan 27, 1997
- [AD 95-07-03](https://openairdocs.org/ad/95-07-03): Auxiliary Power Units · Allliedsignal Aerospace Auxiliary Power Units, 707-100 Long Body, 707-100B Long Body and 46 more. Effective May 3, 1995
- [AD 94-26-15](https://openairdocs.org/ad/94-26-15): Outer Wing Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective Feb 3, 1995
- [AD 92-10-14](https://openairdocs.org/ad/92-10-14): AFM Changes - Cabin Pressure · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 29, 1992
- [AD 90-04-02](https://openairdocs.org/ad/90-04-02): Fire Extinguisher Squibs · Lockheed Martin 382G. Effective Feb 26, 1990
- [AD 89-16-09](https://openairdocs.org/ad/89-16-09): Nose Landing Gear Strut Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 7, 1989
- [AD 88-09-03](https://openairdocs.org/ad/88-09-03): Control Column Base · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 7, 1988
- [AD 88-10-06](https://openairdocs.org/ad/88-10-06): Wing Panel Risers · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 25, 1988
- [AD 88-10-05](https://openairdocs.org/ad/88-10-05): Wing Panel Doublers · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 25, 1988
- [AD 87-18-04](https://openairdocs.org/ad/87-18-04): Circuit Breaker Panels · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 17, 1987
- [AD 85-23-03](https://openairdocs.org/ad/85-23-03): Fire Estinguisher Squib Insp. · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 24, 1985
- [AD 81-12-02](https://openairdocs.org/ad/81-12-02): Longerons · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 5, 1981
- [AD 79-05-05](https://openairdocs.org/ad/79-05-05): Throttle Cables · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jan 2, 1980
- [AD 79-25-06](https://openairdocs.org/ad/79-25-06): Window Latch Catches · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 19, 1979
- [AD 79-18-12](https://openairdocs.org/ad/79-18-12): Auxiliary Power Units · Airbus BAC 1-11 200 Series, BAC 1-11 400 Series, Manufacturing Company Auxiliary Power Units and 46 more. Effective Oct 8, 1979
- [AD 79-03-04](https://openairdocs.org/ad/79-03-04): Ballscrew Assembly in MLG · Lockheed Martin 382, 382B, 382E and 2 more. Effective Feb 5, 1979
- [AD 74-12-06](https://openairdocs.org/ad/74-12-06): Outer Wing Beam Cap · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 8, 1978
- [AD 75-17-04](https://openairdocs.org/ad/75-17-04): Main Frames · Lockheed Martin 382, 382B, 382E and 2 more. Effective Apr 21, 1978
- [AD 75-19-02](https://openairdocs.org/ad/75-19-02): Wing Beam Caps · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978
- [AD 75-18-04](https://openairdocs.org/ad/75-18-04): Outer Wing Lower Panels · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978
- [AD 75-18-03](https://openairdocs.org/ad/75-18-03): Outer Wing Spar Cap · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978
- [AD 76-09-11](https://openairdocs.org/ad/76-09-11): Crank Arm or Servo Valve Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 14, 1976
- [AD 75-17-35](https://openairdocs.org/ad/75-17-35): Propeller Torque Check · Lockheed Martin 382, 382B, 382E and 2 more. Effective Aug 13, 1975
- [AD 74-24-08](https://openairdocs.org/ad/74-24-08): Engine Throttle Cables · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 27, 1974
- [AD 74-24-04](https://openairdocs.org/ad/74-24-04): Lower Center Wing · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 20, 1974

### 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 2019-18-09](https://openairdocs.org/ad/2019-18-09) (historical): Wings · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Oct 11, 2019
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2011-09-04](https://openairdocs.org/ad/2011-09-04) (historical): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 22, 2011
- [AD 2011-09-03](https://openairdocs.org/ad/2011-09-03) (historical): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 26, 2011
- [AD 2008-20-01](https://openairdocs.org/ad/2008-20-01) (historical): Fuel tank systems · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 3, 2008
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 96-12-20](https://openairdocs.org/ad/96-12-20) (historical): Upper Truss Mounts · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jul 15, 1996
- [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) (2 in force)

- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008

## NTSB investigations

None matched to N408LC.

## FAA accident and incident reports

None matched to N408LC.

## Service difficulty reports (190, 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 LR7A2026101103992](https://openairdocs.org/sdr/LR7A2026101103992), Oct 11, 2026: STIFFENER. CRACKED. DURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH OUTER WING REAR SPAR VERTICAL STIFFENER CRACKED AT OWFS90. / REPAIR BY REPLACEMENT ACCOM
- [SDR LR7A2026101103991](https://openairdocs.org/sdr/LR7A2026101103991), Oct 11, 2026: RIB. CRACKED. DURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH ELEVATOR RIBS CRACKED AT HSS71L AND HSS84L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOC
- [SDR LR7A2026101103990](https://openairdocs.org/sdr/LR7A2026101103990), Oct 11, 2026: RIB. BROKEN. DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB2703, FOUND LT ELEVATOR RIBS BROKEN AT HSS76L AND HSS80L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-
- [SDR LR7A2026101103989](https://openairdocs.org/sdr/LR7A2026101103989), Oct 11, 2026: WEB. CRACKED. DURING SCHEDULED B-3 CHECK UNDER SP-316, FOUND LH OUTER WING AFT SPAR WEB CRACKED AT OWS54-108L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, C
- [SDR LR7A2026101103988](https://openairdocs.org/sdr/LR7A2026101103988), Oct 11, 2026: ANGLE. CRACKED. DURING SCHEDULED B-3 CHECK UNDER ST-25, FOUND FORWARD FUSELAGE CHINE ANGLE CRACKED AT FS116, LBL49, WL198. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP
- [SDR LR7A2026101103987](https://openairdocs.org/sdr/LR7A2026101103987), Oct 11, 2026: ANGLE. CRACKED. DURING SCHEDULED B-3 CHECK UNDER ST-25, FOUND FORWARD FUSELAGE LH CHINE ANGLE, FS132, LBL55, WL195. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM
- [SDR LR7A2026101103986](https://openairdocs.org/sdr/LR7A2026101103986), Oct 11, 2026: STIFFENER. CRACKED. DURING SCHEDULED B-3 CHECK UNDER ST-25, FOUND LT FORWARD FUSELAGE WEB STIFFENER CRACKED AT FS180-196, LBL30, WL195. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 5
- [SDR LR7A2025102803793](https://openairdocs.org/sdr/LR7A2025102803793), Oct 28, 2025: SKIN. CRACKED. DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND RH V-STAB SKIN CRACKED AT FS1124, RBL10, VSS 257. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12.
- [SDR LR7A2025102803792](https://openairdocs.org/sdr/LR7A2025102803792), Oct 28, 2025: CAP. CRACKED. DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND RH FS902 BULKHEAD OB CAP CRACKED AT RBL62, WL195. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. 
- [SDR LR7A2025060103774](https://openairdocs.org/sdr/LR7A2025060103774), Jun 1, 2025: LONGERON. GROUND DAMAGE. DURING SCHEDULED INSPECTION FOUND GROUND HANDLING DAMAGE ON RIGHT SLOPING LONGERON AT FS792, RBL61, WL160 / REPAIRED IAW ERO 5350ERO3927.
- [SDR LR7A2025052303763](https://openairdocs.org/sdr/LR7A2025052303763), May 23, 2025: SKIN. CRACKED. DURING UNSCHEDULED MAINTENANCE 1.5 INCH CRACK ON UPPER SURFACE OF HORIZONTAL STAB HSS 219, FS 1094.06 / REPAIRED IAW SMP583 FOG. 55-20-06 MEA 382-55-25-030
- [SDR LR7A2024090603587](https://openairdocs.org/sdr/LR7A2024090603587), Sep 6, 2024: STANCHION. DAMAGED. DURING SCHEDULED FLIGHT RH STANTION AT FS 792 RBL 62 WAS DAMAGED BY LOOSE CARGO. / REMOVED DAMAGED STANTION AND REPAIR BY REPLACEMENT ACCOMPLISHED IAW LKHD SMP5
- [SDR LR7A2024032803414](https://openairdocs.org/sdr/LR7A2024032803414), Mar 28, 2024: RIB. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH ELEVATOR RIB LOWER FLANE CRACKED AT FS1142, HSS89R, WL276. / REPAIRED IAW LOCKHEED SMP58
- [SDR LR7A2024032803413](https://openairdocs.org/sdr/LR7A2024032803413), Mar 28, 2024: RIB. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH ELEVATOR RIB CRACKED AT FS1143, WL276, HSS52.75R. / REPAIRED IAW LOCKHEED SMP583 SRM, FI
- [SDR LR7A2024032803412](https://openairdocs.org/sdr/LR7A2024032803412), Mar 28, 2024: SKIN. CHAFED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH ELEVATOR INNER LOWER SKIN CHAFFED AT , FS1132, HSS80R, WL274. / REPAIR BY REPLACEMENT AC
- [SDR LR7A2024032803411](https://openairdocs.org/sdr/LR7A2024032803411), Mar 28, 2024: RIB. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH ELEVATOR RIB CRACKED AT HSS80R. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583
- [SDR LR7A2024032803410](https://openairdocs.org/sdr/LR7A2024032803410), Mar 28, 2024: SPAR CAP. CORRODED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5501, FOUND RH ELEVATOR LEADING EDGE UPPER SPAR CAP CORRODED AT HSS94R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 5
- [SDR LR7A2024032803409](https://openairdocs.org/sdr/LR7A2024032803409), Mar 28, 2024: SKIN. DAMAGED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5511, FOUND RUDDER SKIN TRAILING EDGE DAMAGED AT FS1155, BL0, VSS206. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-
- [SDR LR7A2024032803408](https://openairdocs.org/sdr/LR7A2024032803408), Mar 28, 2024: SKIN PANEL. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH LOWER CENTER WING SKIN PANEL AND STRINGER WITH A HOLE AT FS548, CWS81R, WL257. / REPAIRE
- [SDR LR7A2024032803407](https://openairdocs.org/sdr/LR7A2024032803407), Mar 28, 2024: SKIN. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH ELEVATOR LOWER INNER SKIN CRACKED AT FS1120, HSS196L. / REPAIRED IAW LOCKHEED SMP583 SRM
- [SDR LR7A2024032803406](https://openairdocs.org/sdr/LR7A2024032803406), Mar 28, 2024: WEB. CHAFED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC3212, FOUND RH AFT WHEEL WELL BULKHEAD WEB CHAFED AT FS617. RBL75, WL215. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE
- [SDR LR7A2024032803405](https://openairdocs.org/sdr/LR7A2024032803405), Mar 28, 2024: RIB. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FORWARD FUSELAGE RIB ASSY. CRACKED AT FS116.7, RBL43, WL231.7. / REPAIRED IAW LOCKHEED SMP5
- [SDR LR7A2024032803404](https://openairdocs.org/sdr/LR7A2024032803404), Mar 28, 2024: WEB. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH WHEEL WELL WEB CORRODED AT FS582-588, WL146, LBL61.62. / REPAIR BY REPLACEMENT ACCOMPLIS
- [SDR LR7A2024032803403](https://openairdocs.org/sdr/LR7A2024032803403), Mar 28, 2024: BEAM. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING SP-200, FOUND FS588 LH MLG BEAM CRACKED AT LBL62, WL144 / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-21. NR# 100
- [SDR LR7A2024032803402](https://openairdocs.org/sdr/LR7A2024032803402), Mar 28, 2024: WEB. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH MLG WELL WEB CORRODED AT FS596-614, LBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCK
- [SDR LR7A2024032803401](https://openairdocs.org/sdr/LR7A2024032803401), Mar 28, 2024: BEAM. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING SP-200, FOUND FS528 LH MLG BEAM CRACKED AT LBL62, WL144. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-21. NR# 10
- [SDR LR7A2024032803400](https://openairdocs.org/sdr/LR7A2024032803400), Mar 28, 2024: SKIN. GOUGED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC4914, FOUND LH FUSELAGE SKIN GOUGED AT FS472, LBL84.5, WL192. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. 
- [SDR LR7A2024032803399](https://openairdocs.org/sdr/LR7A2024032803399), Mar 28, 2024: BEAM. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING SP-309, FOUND FS517 RH MLG BEAM CRACKED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 5
- [SDR LR7A2024032803398](https://openairdocs.org/sdr/LR7A2024032803398), Mar 28, 2024: CAP. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LOWER FRAME CAP CORRODED AT FS657, LBL62-RBL62, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED
- [SDR LR7A2024032803397](https://openairdocs.org/sdr/LR7A2024032803397), Mar 28, 2024: CAP. CORRODED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LOWER FRAME CAP CORRODED AT FS617, LBL62-RBL62, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED
- [SDR LR7A2024032803396](https://openairdocs.org/sdr/LR7A2024032803396), Mar 28, 2024: SKIN. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH AFT FUSELAGE SKIN CRACKED AT FS847, LBL62, WL182. / REPAIRED IAW LOCKHEED SMP583 SRM, FI
- [SDR LR7A2024032803395](https://openairdocs.org/sdr/LR7A2024032803395), Mar 28, 2024: RIB. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING ST-5, FOUND LH H-STAB LEADING EDGE RIB LOWER AFT END CRACKED AT FS1039, HSS156L, WL256. / REPAIRED IAW LOCKHEED SMP5
- [SDR LR7A2024032803394](https://openairdocs.org/sdr/LR7A2024032803394), Mar 28, 2024: RIB. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING ST-5, FOUND RH H-STAB LEADING EDGE RIB UPPER AFT END CRACKED AT FS1041.5, HSS197R, WL264. / REPAIRED IAW LOCKHEED SM
- [SDR LR7A2024032803393](https://openairdocs.org/sdr/LR7A2024032803393), Mar 28, 2024: SKIN. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH FUSELAGE CURB CRACKED AT FS623, WL152, RBL62. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE
- [SDR LR7A2024032803392](https://openairdocs.org/sdr/LR7A2024032803392), Mar 28, 2024: ANGLE. CORRODED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CHINE ANGLE CORRODED AT FS626, WL148-150, LBL59. / REPAIR BY REPLACEMENT ACCOMPLISHED IA
- [SDR LR7A2024032803391](https://openairdocs.org/sdr/LR7A2024032803391), Mar 28, 2024: CAP. DAMAGED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING SP-303, FOUND RH CHINE CAP 10K D-RING HOLES WITH FREEZE PLUGS AT RBL59.7, FS257.0E, 337.0E, 537 & 577, WL146. / REPA
- [SDR LR7A2024032803390](https://openairdocs.org/sdr/LR7A2024032803390), Mar 28, 2024: CAP. DAMAGED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING SP-303, FOUND LH CHINE CAP 10K D-RING HOLES WITH FREEZE PLUGS AT LBL59.7, FS537 &577, WL146. / REPAIRED IAW LAC MEA 
- [SDR LR7A2024032803389](https://openairdocs.org/sdr/LR7A2024032803389), Mar 28, 2024: SKIN. DENTED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5712, FOUND RH AILERON UPPER SKIN DENTED AT FS616, AS21.1R, WL279. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140
- [SDR LR7A2024032803388](https://openairdocs.org/sdr/LR7A2024032803388), Mar 28, 2024: SKIN. DENTED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5712, FOUND RH OB FLAP UPPER TRAILING EDGE SKIN DENTED AT OWFS41R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140
- [SDR LR7A2024032803387](https://openairdocs.org/sdr/LR7A2024032803387), Mar 28, 2024: SKIN. CORRODED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5712, FOUND RH AILERON UPPER SKIN CORRODED AT AS117.1, FS598 WL282. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-14
- [SDR LR7A2024032803386](https://openairdocs.org/sdr/LR7A2024032803386), Mar 28, 2024: SKIN. CRACKED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5712, FOUND RH OB FLAP UPPER SURFACE BAFFLE ASSEMBLY CRACKED AT OWFS2R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 5
- [SDR LR7A2024032803385](https://openairdocs.org/sdr/LR7A2024032803385), Mar 28, 2024: LONGERON. CRACKED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5511, FOUND RH DORSAL FIN LONGERON EXISTING REPAIR CRACKED AT FS822, RBL11, WL285. / REPAIRED IAW LOCKHEED SMP583 SR
- [SDR LR7A2024032803384](https://openairdocs.org/sdr/LR7A2024032803384), Mar 28, 2024: LONGERON. CRACKED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5511, FOUND LH DORSAL FIN LONGERON EXISTING REPAIR CRACKED AT FS825-850, LBL11, WL285. / REPAIRED IAW LOCKHEED SMP58
- [SDR LR7A2024032803383](https://openairdocs.org/sdr/LR7A2024032803383), Mar 28, 2024: STIFFENER. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING ST-5, FOUND LH V-STAB STIFFENER CRACKED AT FS1109.5, LBL10.5, VSS74. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-1
- [SDR LR7A2024032803382](https://openairdocs.org/sdr/LR7A2024032803382), Mar 28, 2024: WEB. CORRODED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5314, FOUND PRESSURIZED WEB CORRODED AT FS492-507, RBL60, WL147. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED S
- [SDR LR7A2024032803381](https://openairdocs.org/sdr/LR7A2024032803381), Mar 28, 2024: WEB. CORRODED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5323, FOUND LH MLG WEB CORRODED AT FS528-530, LBL61.6, WL145-146.5. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEE
- [SDR LR7A2024032803380](https://openairdocs.org/sdr/LR7A2024032803380), Mar 28, 2024: WEB. CORRODED. DURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5323, FOUND LH MLG WEB CORRODED AT FS557-577, LBL61.6, WL144-148.5. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEE
- [SDR LR7A2024032803379](https://openairdocs.org/sdr/LR7A2024032803379), Mar 28, 2024: FRAME. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND BATTERY BOX FRAME CRACKED AT FS140.5, LBL46, WL154. / REPAIR BY REPLACEMENT ACCOMPLISHED IA
- [SDR LR7A2024032803378](https://openairdocs.org/sdr/LR7A2024032803378), Mar 28, 2024: SUPPORT. CRACKED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND BATTERY BOX HORIZONTAL SUPPORT CRACKED AT FS140.5, WL154, LBL47. / REPAIRED IAW LOCKHEED SM
- [SDR LR7A2024032803377](https://openairdocs.org/sdr/LR7A2024032803377), Mar 28, 2024: STRUCTURE. CORRODED. DURING SCHEDULED C-4 CHECK WHILE PERFORMING SP-303, FOUND SEVERAL D-RING LOCATIONS CORRODED AT FS597, LBL60, WL146. / REPAIRED IAW LAC MEA 382-53-24-020. NR# 10

All 190: https://openairdocs.org/aircraft/N408LC/reports.md

## STCs that may be installed (OpenAirDocs) (77, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Lockheed 382G)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC SA7757SW](https://openairdocs.org/stc/SA7757SW): Interior installation for 97 passengers. Lynden Air Cargo LLC
- [STC ST02537LA](https://openairdocs.org/stc/ST02537LA): Installation of below the floor retardant tank. Coulson Aviation (USA) Inc
- [STC ST02584LA](https://openairdocs.org/stc/ST02584LA): Installation of Retardant Aerial Delivery System (RADS) XXL. Coulson Aviation (USA) Inc
- [STC ST02254CH](https://openairdocs.org/stc/ST02254CH): Installation of Honeywell Enhanced Ground Proximity Warning System and Honeywell Multi Function Radar Display. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02583AK](https://openairdocs.org/stc/ST02583AK): Installation of Pallet Retention Aerial Delivery System (PRADS). Lynden Air Cargo LLC
- [STC ST02771AT](https://openairdocs.org/stc/ST02771AT): Installation of an Enhanced Ground Proximity Warning System (EGPWS). Woven Electronics, LLC
- [STC ST02773AT](https://openairdocs.org/stc/ST02773AT): Installation of an Global Positioning System (GPS). Woven Electronics, LLC
- [STC ST02772AT](https://openairdocs.org/stc/ST02772AT): Installation of a Honeywell CAS-81 Traffic Alert and Collision Avoidance System (TCAS) and a single TRA-67 Mode-S Transmitter System. Woven Electronics, LLC
- [STC ST02571AK](https://openairdocs.org/stc/ST02571AK): Installation of the Propeller Pre-Heat System. Lynden Air Cargo, LLC
- [STC ST02109CH](https://openairdocs.org/stc/ST02109CH): Installation of a Honeywell RESCU 406AF/AFN Emergency Locator Transmitter (ELT) System. Honeywell International Inc
- [STC ST02550AK](https://openairdocs.org/stc/ST02550AK): Installation of a Digital Fuel Quantity Indication System. Lynden Air Cargo LLC
- [STC ST03679NY](https://openairdocs.org/stc/ST03679NY): Installation of the Propeller Pre-Heat System. Lynden Air Cargo LLC
- [STC ST03680NY](https://openairdocs.org/stc/ST03680NY): Installation of the Propeller Pre-Heat System. Lynden Air Cargo LLC
- [STC ST02511AK](https://openairdocs.org/stc/ST02511AK): Installation of aft fuselage microvanes. Lynden Air Cargo LLC
- [STC ST02495LA](https://openairdocs.org/stc/ST02495LA): Installation of a multipurpose hatch system. R4 Integration Inc
- [STC ST01162LA](https://openairdocs.org/stc/ST01162LA): Activation of the Enhanced Mode S Transponder function and installation of the Avionics Upgrade on the Lockheed 382G airplane. Honeywell International Inc
- [STC ST00221BO](https://openairdocs.org/stc/ST00221BO): Installation of a BAE Systems IRCM. BAE SYSTEMS Information and Electronic Systems Integration Inc
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA3589SW](https://openairdocs.org/stc/SA3589SW): Installation of an auxiliary power unit and freon air conditioning system in each of two wing pods. Aircraft Technical Development Inc. dba Aerocon Engineering Company
- [STC ST00113AT](https://openairdocs.org/stc/ST00113AT): Installation of a replacement coalescer filter, P/N 21BC107. Purolator Facet, Inc
- [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC SA2929WE](https://openairdocs.org/stc/SA2929WE): Installation of palletized dual LTN-51 or dual LTN-72 INS or combination of either. Northrop Grumman Systems Corporation
- [STC ST03644NY](https://openairdocs.org/stc/ST03644NY): See STC: Attachment - ST03644NY.pdf. First Air
- [STC SA3934NM](https://openairdocs.org/stc/SA3934NM): Fabrication of Biegert Airborne dispersant delivery system (ADDS). Oil Spill Response (Americas) Limited
- [STC ST00772CH](https://openairdocs.org/stc/ST00772CH): Install Cargo Handling System. Telair US LLC
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02437AK](https://openairdocs.org/stc/ST02437AK): Installation of Software Version 6.1 on Honeywell FMZ-2000, ADS-B Out and WAAS/LPV capabilities. Lynden Air Cargo LLC
- [STC ST01635WI-D](https://openairdocs.org/stc/ST01635WI-D): Modification of Rockwell Collins, Inc. VHF-4000 and VHF-4000E installations. Rockwell Collins Inc
- [STC SA3132NM](https://openairdocs.org/stc/SA3132NM): Installation of a de-icing system on the Hamilton Standard P/N 554654 propeller spinner. ROBERT W. MURRAY
- [STC SA3407NM](https://openairdocs.org/stc/SA3407NM): Installation of a de-icing system on the Hamilton Standard P/N 560501 propeller spinner afterbody. ROBERT W. MURRAY
- [STC ST02369LA](https://openairdocs.org/stc/ST02369LA): : Installation of provisions for Mission System Equipment (MSE), in accordance with FAA approved BAE Master Data List, 0139A1003, Revision A, dated August 26, 2011, or later FAA approved revisions. BAE Systems
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC ST03600AT](https://openairdocs.org/stc/ST03600AT): Installation of a Wingspeed Iridium Communication Management System and Dual DAC International Electronic Flights Bags (EFBs). Avionics Support Group Inc
- [STC ST02282LA](https://openairdocs.org/stc/ST02282LA): ONE ONLY STC, SN 4954: Installation of Potable Water and Waste System. Dynamo Aviation Inc
- [STC ST01256WI-D](https://openairdocs.org/stc/ST01256WI-D): Modification of a Collins TPR-720, TPR-900 or TPR-901 Mode S Transponder System installation with an ATC/TCAS Control Panel to an Elementary Surveillance Compliant Collins TPR-901 Mode S Transponder System installation with a Flight ID/ATC/TCAS Control Panel in accordance with Collins Drawing Index as listed on AML No. ST01256WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST00435CH-D](https://openairdocs.org/stc/ST00435CH-D): Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS-II) system. Duncan Aviation Inc
- [STC ST434CH-D](https://openairdocs.org/stc/ST434CH-D): Installation of Dual Trimble TNL8100 GPS Navigation Systems. Duncan Aviation Inc
- [STC SA1625WE](https://openairdocs.org/stc/SA1625WE): Pallet assembly provisions. Lockheed Martin Aeronautics Company
- [STC ST00224AT](https://openairdocs.org/stc/ST00224AT): Installation of an Expanded Parameters Digital Flight Data Recorder. ASB Avionics
- [STC ST02020NY](https://openairdocs.org/stc/ST02020NY): Installation of Ayles Fernie International (AFI) NIMBUS Oil Dispersant Spraying System. Amtech Aeronautical Limited
- [STC SA02365CH](https://openairdocs.org/stc/SA02365CH): Installation of NASI Supplemental Air-Conditioning System. National Aircraft Service Inc
- [STC ST02274AK](https://openairdocs.org/stc/ST02274AK): Manufacture and install bulk fuel tank system. Lynden Air Cargo LLC
- [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc
- [STC ST01574LA](https://openairdocs.org/stc/ST01574LA): Installation of the Integral Dorsal Fin Shunt High Frequency Antenna on the Lockheed 382G airplane in accordance with FAA approved ASB Avionics Master Document List No. 23-103, Revision "NC", dated December 01, 2003, or later FAA approved revision. ASB Avionics
- [STC SA3171WE](https://openairdocs.org/stc/SA3171WE): The auxiliary power unit Model GTC 85-71 located in the forward end of the left hand main landing gear wheel well fairing has been replaced by an AiResearch Gas turbine compressor Model GTCP85-98CK(A). Kellstrom Defense Aerospace Inc
- [STC SA1877SO](https://openairdocs.org/stc/SA1877SO): Fabrication of cargo system. Pemco Engineers Inc
- [STC ST00957CH](https://openairdocs.org/stc/ST00957CH): Installation of AlliedSignal GNS-XLS flight management system in accordance with Europe Aero Design Master Data List, EP903-0131-00, Rev 3, dated 9/14/98, or later FAA approved revision. EAC North America, Inc. (s/b EAD Aerospace)

All 77: https://openairdocs.org/aircraft/N408LC/stcs.md

## Related

- Other Lockheed 382G aircraft: https://openairdocs.org/model/lockheed-382g/aircraft.md
- The Allison 501-D22A engine: https://openairdocs.org/engine/allison-501-d22a.md

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