# N405LC: 1985 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: 5025
- Year built: 1985
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Restricted, other
- Airworthiness date: January 8, 2025
- Certificate issued: July 21, 1999
- Expires: October 31, 2027
- Mode S code: A4C031
- 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=405LC
- Page: https://openairdocs.org/aircraft/N405LC

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 N405LC.

## FAA accident and incident reports

None matched to N405LC.

## Service difficulty reports (430, 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 LR7A2026091803919](https://openairdocs.org/sdr/LR7A2026091803919), Sep 18, 2026: TEE FITTING. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO UNDER FLOOR SKIN HORIZONTAL ATTACH TEE AT FS797.0E TO FS817.0E, 
- [SDR LR7A2026091803918](https://openairdocs.org/sdr/LR7A2026091803918), Sep 18, 2026: TEE FITTING. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO CARGO UNDERFLOOR SKIN HORIZONTAL ATTACH TEE AT 797.0E TO FS817.0
- [SDR LR7A2026091803917](https://openairdocs.org/sdr/LR7A2026091803917), Sep 18, 2026: CHANNEL. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FS797.0E BULKHEAD VERTICAL DIAGONAL CHANNEL LOWER EDGE CRACKED A
- [SDR LR7A2026091803916](https://openairdocs.org/sdr/LR7A2026091803916), Sep 18, 2026: PLATE. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FUSELAGE LOWER BELLY SKIN AFT SKID PLATE CRACKED AT FS797.0E, LB
- [SDR LR7A2026091803915](https://openairdocs.org/sdr/LR7A2026091803915), Sep 18, 2026: STIFFENER. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FS797.0E TO FS817.0E WEB ATTACH ANGLE STIFFENER AT RBL10, WL127-
- [SDR LR7A2026091803914](https://openairdocs.org/sdr/LR7A2026091803914), Sep 18, 2026: STIFFENER. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FS797.0E TO FS817.0E UNDERFLOOR WEB VERTICAL ANGLE AND STIFFENER
- [SDR LR7A2026091803913](https://openairdocs.org/sdr/LR7A2026091803913), Sep 18, 2026: CHANNEL. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FS797.0E BULKHEAD U CHANNEL STIFFENER CRACKED AT LBL10, WL127-14
- [SDR LR7A2026091803912](https://openairdocs.org/sdr/LR7A2026091803912), Sep 18, 2026: CHANNEL. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO 797.0E BULKHEAD U CHANNEL STIFFENER CRACKED AT RBL10, WL127-145.
- [SDR LR7A2026091803911](https://openairdocs.org/sdr/LR7A2026091803911), Sep 18, 2026: BULKHEAD WEB. DEFORMED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FS797.0E BULKHEAD WEB DEFORMED AT LBL8-32, WL127-132. / REPAIR B
- [SDR LR7A2026091803910](https://openairdocs.org/sdr/LR7A2026091803910), Sep 18, 2026: BULKHEAD WEB. DEFORMED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FS797.0E BULKHEAD WEB DEFORMED AT RBL8 TO RBL32, WL 127-132. / R
- [SDR LR7A2026091803909](https://openairdocs.org/sdr/LR7A2026091803909), Sep 18, 2026: WEB. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO UNDERFLOOR WEB CRACKED AT FS797.0E TO FS817.0E RBL10, WL130-135.
- [SDR LR7A2026091803908](https://openairdocs.org/sdr/LR7A2026091803908), Sep 18, 2026: WEB. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO UNDERFLOOR WEB CRACKED AT FS797.0E TO FS817.0E LBL10, WL130-135.
- [SDR LR7A2026091803907](https://openairdocs.org/sdr/LR7A2026091803907), Sep 18, 2026: SKIN. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FUSELAGE LOWER BELLY SKIN CRACKED AT FS797.0E, RBL7 TO RBL13, WL
- [SDR LR7A2026091803906](https://openairdocs.org/sdr/LR7A2026091803906), Sep 18, 2026: CAP. CRACKED. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FS797.0E BULKHEAD LOWER CAP LBL12 - RBL12, WL128. / REPAIRED IAW
- [SDR LR7A2026091803905](https://openairdocs.org/sdr/LR7A2026091803905), Sep 18, 2026: SKID. WORN. DURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO THE LH AND RH BELLY SKID BAR ASSY WORN. / REPAIR BY REPLACEMENT 
- [SDR LR7A2026090603901](https://openairdocs.org/sdr/LR7A2026090603901), Sep 6, 2026: SKIN. DAMAGED. DURING SCHEDULED FLIGHT AND SUBSEQUENT INSPECTION, FOUND DAMAGED SKIN AND MISSING RIVER HEADS JUST FORWARD OF THE BELLY BUMPER ASSEMBLY DUE TO TAIL STRIKE / REP
- [SDR LR7A2026041603818](https://openairdocs.org/sdr/LR7A2026041603818), Apr 16, 2026: BULKHEAD WEB. CRACKED. DURING ULTRASONIC SPECIAL NDI INSP IAW LOCKHEED SERVICE FLO CS1370999, FOUND FS93 CANTED BULKHEAD CRACKING IN THE WEB. DOCUMENTED ON KF AERO NDT RPT NDT26-1078 
- [SDR LR7A2026041603817](https://openairdocs.org/sdr/LR7A2026041603817), Apr 16, 2026: FLAP TRACK. CRACKED. DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND LH OUTBOARD WING FLAP TRACK FITTING CRACKED AT OWFS241. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED 
- [SDR LR7A2026041603816](https://openairdocs.org/sdr/LR7A2026041603816), Apr 16, 2026: SKIN. WORN. DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND LH OUTER WING FLAP UPPER TRAILING EDGE SKIN WITH WORN COUNTERSINK RIVET HOLES / REPAIRED IAW SMP583 SRM,
- [SDR LR7A2025030303747](https://openairdocs.org/sdr/LR7A2025030303747), Mar 3, 2025: ATTACH FITTING. CRACKED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS817.0E BULKHEAD FWD ATTACH FITTING UPPER SURFACE BOLT HOLES CRACKED AT LBL61, WL145. / R
- [SDR LR7A2025030303746](https://openairdocs.org/sdr/LR7A2025030303746), Mar 3, 2025: ATTACH FITTING. CRACKED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS817.0E BULKHEAD LOWER OUTBOARD ATTACH FITTING LOWER INBOARD BOLT HOLES CRACKED AT LBL61,
- [SDR LR7A2025030303745](https://openairdocs.org/sdr/LR7A2025030303745), Mar 3, 2025: SKIN. CRACKED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH INBOARD FLAP UPPER TRAILING EDGE SKIN CRACK AT CWS210L. / REPAIRED IAW LOCKHEED SMP583 
- [SDR LR7A2025030303744](https://openairdocs.org/sdr/LR7A2025030303744), Mar 3, 2025: RIB. CRACKED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH INBOARD FLAP LOWER RIB CRACKED AT CWS195L, CWS206L, CWS212L. / REPAIR BY REPLACEMENT AC
- [SDR LR7A2025030303743](https://openairdocs.org/sdr/LR7A2025030303743), Mar 3, 2025: TEE ANGLE. CORRODED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH INBOARD FLAP LOWER TEE FLANGE CORRODED AT CWS189L-CWS214L. / REPAIR BY REPLACEMENT ACCO
- [SDR LR7A2025030303742](https://openairdocs.org/sdr/LR7A2025030303742), Mar 3, 2025: SKIN. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5712, FOUND RH OUTBOARD FLAP UPPER TRAILING EDGE SKIN CRACKED AT OWS44R AND OWS63R. / REPAIRED IAW LOCKHEED SMP583 
- [SDR LR7A2025030303741](https://openairdocs.org/sdr/LR7A2025030303741), Mar 3, 2025: BULKHEAD WEB. CORRODED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS817.0E BULKHEAD WEB CORRODED AT LBL24-RBL24, WL138. / REPAIR BY REPLACEMENT ACCOMPLISHED
- [SDR LR7A2025030303740](https://openairdocs.org/sdr/LR7A2025030303740), Mar 3, 2025: BULKHEAD WEB. CORRODED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS817.0E BULKHEAD WEB CORRODED AT RBL24-RBL54, WL135. / REPAIR BY REPLACEMENT ACCOMPLISHED
- [SDR LR7A2025030303739](https://openairdocs.org/sdr/LR7A2025030303739), Mar 3, 2025: BULKHEAD WEB. CORRODED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS817.0E BULKHEAD WEB CORRODED AT LBL24-LBL54, WL135. / REPAIR BY REPLACEMENT ACCOMPLISHED
- [SDR LR7A2025030303738](https://openairdocs.org/sdr/LR7A2025030303738), Mar 3, 2025: TEE FITTING. CRACKED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND AFT FUSELAGE TEE FITTING CRACKED AT LOWER ATTACHMENT TO SLOPING LONGERON, FS770, RBL61, WL
- [SDR LR7A2025030303737](https://openairdocs.org/sdr/LR7A2025030303737), Mar 3, 2025: STIFFENER. CRACKED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND AFT FUSELAGE STIFFENER CRACKED AT LOWER ATTACHMENT TO SLOPING LONGERON AT FS743, RBL63, WL
- [SDR LR7A2025030303736](https://openairdocs.org/sdr/LR7A2025030303736), Mar 3, 2025: SKIN. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5304, FOUND RH WHEEL WELL SKIN CRACKED AT UPPER MIXING CHAMBER MOUNTING SCREW HOLE, FS494, RBL61, WL260. / REPAIRED
- [SDR LR7A2025030303735](https://openairdocs.org/sdr/LR7A2025030303735), Mar 3, 2025: RISER PANEL. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5323, FOUND LH FS477 BULKHEAD RISER PANEL CRACKED AT LBL67-LBL69, WL156-WL160. / REPAIR BY REPLACEMENT ACCOMPLISHED
- [SDR LR7A2025030303734](https://openairdocs.org/sdr/LR7A2025030303734), Mar 3, 2025: TEE FITTING. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5712, FOUND RH CENTER WING CWS174.3R VERTICAL SPLICE TEE CRACKED AT LOWER EDGE, FS517, WL269. / REPAIR BY REPLACEME
- [SDR LR7A2025030303733](https://openairdocs.org/sdr/LR7A2025030303733), Mar 3, 2025: TEE FITTING. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH CENTER WING CWS174.3L VERTICAL SPLICE TEE CRACKED AT LOWER EDGE, FS517, WL258. / REPAIR BY REPLACEME
- [SDR LR7A2025030303732](https://openairdocs.org/sdr/LR7A2025030303732), Mar 3, 2025: CAP. CRACKED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS817.0E LOWER CAP OUTBOARD FASTENER HOLES CRACKED, LBL61-RBL61, WL128-WL143. / REPAIR BY 
- [SDR LR7A2025030303731](https://openairdocs.org/sdr/LR7A2025030303731), Mar 3, 2025: ANGLE. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC3211, FOUND LH MLG WHEEL WELL FS517 CHINE ANGLE CRACKED AT LBL61, WL142. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE
- [SDR LR7A2025030303730](https://openairdocs.org/sdr/LR7A2025030303730), Mar 3, 2025: ATTACH FITTING. CHAFED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH FS847 SIDE BULKHEAD ATTACH FITTING CHAFED AT RBL61, WL186. / REPAIR BY REPLACEMENT ACCO
- [SDR LR7A2025030303729](https://openairdocs.org/sdr/LR7A2025030303729), Mar 3, 2025: RISER PANEL. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5323, FOUND LH MAIN LANDING GEAR FS477 FWD SIDE BULKHEAD EXTRUDED RISER PANEL CRACKED AT LBL61-LBL82, WL175-WL200. 
- [SDR LR7A2025030303728](https://openairdocs.org/sdr/LR7A2025030303728), Mar 3, 2025: ATTACH ANGLE. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH OUTBOARD FLAP RIB ATTACH ANGLE CRACKED AT FWD EDGE, OWS0. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW L
- [SDR LR7A2025030303727](https://openairdocs.org/sdr/LR7A2025030303727), Mar 3, 2025: SKIN. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH INBOARD FLAP UPPER LEADING EDGE SKIN CRACKED AT CWS80L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 5
- [SDR LR7A2025030303726](https://openairdocs.org/sdr/LR7A2025030303726), Mar 3, 2025: SKIN. CHAFED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH OUTBOARD FLAP UPPER TRAILING EDGE SKIN CHAFED AT OWS28L-OWS52L. / REPAIR BY REPLACEMENT ACCOMPLISHED
- [SDR LR7A2025030303725](https://openairdocs.org/sdr/LR7A2025030303725), Mar 3, 2025: SKIN. DENTED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH OUTBOARD FLAP UPPER TRAILING EDGE SKIN DENTED AT OWS59L-OWS96L. / REPAIR BY REPLACEMENT ACCOMPLISHED
- [SDR LR7A2025030303724](https://openairdocs.org/sdr/LR7A2025030303724), Mar 3, 2025: FRAME. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC3215, FOUND NLG WHEEL WELL FS140 FRAME REPAIR DOUBLER CRACKED AT LBL46, WL154. / REPAIRED IAW LOCKHEED SMP583 SRM, 
- [SDR LR7A2025030303723](https://openairdocs.org/sdr/LR7A2025030303723), Mar 3, 2025: FITTING. CORRODED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5315, FOUND RH SLOPING LONGERON FS817.0E FWD ATTACHMENT FITTING INBOARD AND OUTBOARD BOLT HOLES CORRODED AT RBL61, 
- [SDR LR7A2025030303722](https://openairdocs.org/sdr/LR7A2025030303722), Mar 3, 2025: FITTING. CRACKED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5315, FOUND RH SLOPING LONGERON FS817.0E FWD ATTACHMENT FITTING INBOARD BOLT HOLES CRACKED AT FLOOR TO RING BULKHEA
- [SDR LR7A2025030303721](https://openairdocs.org/sdr/LR7A2025030303721), Mar 3, 2025: BULKHEAD WEB. CRACKED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS1012 BULKHEAD WEB CRACKED AT LBL61, WL272. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCK
- [SDR LR7A2025030303720](https://openairdocs.org/sdr/LR7A2025030303720), Mar 3, 2025: SKIN. DAMAGED. DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH AFT FUSELAGE SKIN DAMAGED AT FS737-FS803, WL144-WL174, RBL61-RBL80. / REPAIR BY REPLACE
- [SDR LR7A2025030303719](https://openairdocs.org/sdr/LR7A2025030303719), Mar 3, 2025: CHINE. CORRODED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS737.0E-FS817.0E CARGO FLOOR LH CHINE CAP AT TIEDOWN RING WELL CORRODED, LBL60, WL145. / REPAIR BY REP
- [SDR LR7A2025030303718](https://openairdocs.org/sdr/LR7A2025030303718), Mar 3, 2025: CAP. CORRODED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND CARGO UNDERFLOOR FS817.0E UPPER CAP CORRODED AT BL0-LBL20, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED 
- [SDR LR7A2025030303717](https://openairdocs.org/sdr/LR7A2025030303717), Mar 3, 2025: CAP. CORRODED. DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND CARGO UNDERFLOOR FS737 BULKHEAD ASSEMBLY LOWER CAP CORRODED AT LBL8, WL128. / REPAIR BY REPLACEMENT ACC

All 430: https://openairdocs.org/aircraft/N405LC/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/N405LC/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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