# N404LC: 1977 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: 4763
- Year built: 1977
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Multiple
- Airworthiness date: June 15, 2010
- Certificate issued: February 12, 2021
- Expires: February 29, 2028
- Mode S code: A4BC7A
- Registered owner: [Airplane Sales International Corp](https://openairdocs.org/faa-owner/AIRPLANE%20SALES%20INTERNATIONAL%20CORP)
- Location: [Sherman Oaks, CA](https://openairdocs.org/faa-place/CA/Sherman%20Oaks)
- Owner type: Corporation
- Owner's area on the map: 34.1492° N, 118.4319° W: Placed by OpenAirDocs at the center of ZIP code 91423, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=404LC
- Page: https://openairdocs.org/aircraft/N404LC

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 N404LC.

## FAA accident and incident reports

None matched to N404LC.

## Service difficulty reports (416, 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 LR7A2014061000733](https://openairdocs.org/sdr/LR7A2014061000733), Jun 10, 2014: SKIN. DENTED. DURING DAILY INSPECTION, EXTERIOR FUSELAGE SKIN WAS DISCOVERED DENTED AFT OF FLIGHT DECK PACK EXHAUST BS 210, WL 186, RT SIDE, REPAIRED IAW SMP 583, FIG 51-140-
- [SDR LR7A2013082300710](https://openairdocs.org/sdr/LR7A2013082300710), Aug 23, 2013: ATTACH ANGLE. CRACKED. DURING SCHEDULED B-3 CHECK, FOUND NR 2 DRY BAY FWD INBD VERTICAL ATTACH ANGLE TOP END HAD APPROX 3" LONG VERTICAL CRACK, FS 517, WL270. REPAIR BY REPLACEMENT AC
- [SDR LR7A2013082300709](https://openairdocs.org/sdr/LR7A2013082300709), Aug 23, 2013: FITTING. CRACKED. DURING SCHEDULED B-3 CHECK, FOUND FITTING HAD A CRACKED RADIUS; FS 924 61 WL 207. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM 51-70.
- [SDR LR7A2013082300708](https://openairdocs.org/sdr/LR7A2013082300708), Aug 23, 2013: BULKHEAD WEB. CRACKED. DURING SCHEDULED B-3 CHECK, FOUND BULKHEAD WEB CRACKED, FS924 LBL62 WL270. REPAIRED IAW SMP583, SRM FIG 51-140-17.
- [SDR LR7A2013082300707](https://openairdocs.org/sdr/LR7A2013082300707), Aug 23, 2013: FRAME. CRACKED. DURING SCHEDULED B-3 CHECK, FOUND LT FUSELAGE FRAME AT FS 814 HAD CRACKED AT THE LONGERON CUTOUT LBL 62, WL256. REPAIRED IAW SMP583, SRM FIG 51-140-21.
- [SDR LR7A2013060400646](https://openairdocs.org/sdr/LR7A2013060400646), Jun 4, 2013: LONGERON. CRACKED. DURING SCHEDULED SSID INSPECTION FOR AD 2012-06-09 (SP189), A CRACK WAS FOUND ON NR 3L LONGERON. R & R LONGEORN ASSY.
- [SDR LR7A2013051600645](https://openairdocs.org/sdr/LR7A2013051600645), May 16, 2013: TEE FITTING. CRACKED. DURING CRUISE FLIGHT VISUALLY OBSERVED CRACK AT FS 480. INSPECTION AFTER FLIGHT FOUND TEE FITTING CRACKED, FS 477, RBL 16.5 TO LBL 16.5, WL 285.
- [SDR LR7A2013010800433](https://openairdocs.org/sdr/LR7A2013010800433), Jan 8, 2013: STRUCTURE. CRACKED. DURING SCHEDULED B-2 CHECK, FOUND FWD TOP EMERGENCY EXIT DOOR ASSY'S INNER FLANGE HAD 2 INCH LONG CRACK. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-19 WITH 2024-
- [SDR LR7A2013010800432](https://openairdocs.org/sdr/LR7A2013010800432), Jan 8, 2013: RING ASSEMBLY. CRACKED. DURING SCHEDULED B-2 CHECK, FOUND RT AFT FUSELAGE INTERIOR FS 957 RING SEGMENT HAD 2.5" LONG CRACK AT WL 260, RBL 66. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-0
- [SDR LR7A2013010800431](https://openairdocs.org/sdr/LR7A2013010800431), Jan 8, 2013: BULKHEAD. CRACKED. DURING SCHEDULED B-2 CHECK, FOUND AFT FUSELGAE INTERIOR FS 968, UPPER BULKHEAD CRACKED AT RBL 18, WL 285 VERTICAL FIN ATTACHMENT. REPAIR ACCOMPLISHED IAW SMP583
- [SDR LR7A2013010800430](https://openairdocs.org/sdr/LR7A2013010800430), Jan 8, 2013: FORMER. CRACKED. DURING SCHEDULED B-2, , LT AFT FUSELAGE INTERIOR FORMER AT FS 834, LBL 66, WL 180 FOUND CRACKED. REPAIRED IAW SMP583 FIG 53-50-10.
- [SDR LR7A2012082500395](https://openairdocs.org/sdr/LR7A2012082500395), Aug 25, 2012: CONTROL UNIT. FAULTY. DURING CRUISE FLIGHT NR 1 ENGINE FIRE LIGHT ILLUMINATED, SHUTDOWN NR 1 ENGINE. INSPECTED ENGINE FOR EVIDENCE OF FIRE OR BLEED AIR LEAKAGE, REPLACED NR 1 FIRE CO
- [SDR LR7A2012081300394](https://openairdocs.org/sdr/LR7A2012081300394), Aug 13, 2012: SKIN. CRACKED. DURING SCHEDULED B-1 INSPECTION, FOUND RT HORIZONTAL STABILZER UPPER SKIN CRACKED BETWEEN RIVETS FS 1041, HSS61, WL285. REPAIR ACCOMPLISHED IAW MEA 382-55-12-08
- [SDR LR7A2012081300393](https://openairdocs.org/sdr/LR7A2012081300393), Aug 13, 2012: BULKHEAD. CRACKED. DURING SCHEDULED B-1 INSPECTION, FOUND LT AFT BULKHEAD CAP CRACK AT FS902, LBL63. REPAIR ACCOMPLISHED BY REPLACEMENT IAW SMP583, CH 51-6 AND 51-70.
- [SDR LR7A2012081300392](https://openairdocs.org/sdr/LR7A2012081300392), Aug 13, 2012: STRUCTURE. GOUGED. DURING SCHEDULED B-1 INSPECTION, FOUND LT SLOPING LONGERON GOUGED AT FS 859, LBL 61.62. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-12-088.
- [SDR LR7A2012081300391](https://openairdocs.org/sdr/LR7A2012081300391), Aug 13, 2012: WEB. CRACKED. DURING SCHEDULED B-1 INSPECTION, FOUND RT AFT BULKHEAD WEB CRACKED AT FS 880, RBL 63. REPAIR ACCOMPLISHED BY REPLACEMENT IAW SMP583, 51-60 AND 51-70.
- [SDR LR7A2012081300390](https://openairdocs.org/sdr/LR7A2012081300390), Aug 13, 2012: BULKHEAD WEB. CRACKED. DURING SCHEDULED B-1 INSPECTION, FOUND NLG WHEEL WELL BULKHEAD WEB CRACKED AT FS165, RBL70, WL171. REPAIR ACCOMPLISHED IAW SMP 583, FIG 51-140-17, NR 2-5-2.
- [SDR LR7A2012073100388](https://openairdocs.org/sdr/LR7A2012073100388), Jul 28, 2012: JACKSCREW. SEIZED. FLAPS STUCK AT 15 PERCENT LANDING WAS UNEVENTFUL. R & R NR 7 JACKSCREW IAW SMP 581 27-50-11.
- [SDR LR7A2012040500365](https://openairdocs.org/sdr/LR7A2012040500365), Apr 5, 2012: RIB. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND HORIZONTAL STAB LT L/E UPPER RIBS CRACKED AT HSS138.5, 149.5 & 150.5 AND LOWER RIBS AT HSS93, 99,N 111, 144, 168.6, & 278. RE
- [SDR LR7A2012040500375](https://openairdocs.org/sdr/LR7A2012040500375), Apr 5, 2012: BULKHEAD WEB. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB CRACKED AT FS517, WL165, RBL61. REPAIRED BY REPLACEMENT IAW SMP583 CHAPTER 51-60 & 51-70, NR 
- [SDR LR7A2012040500374](https://openairdocs.org/sdr/LR7A2012040500374), Apr 5, 2012: RIB. CRACKED. DURING SCHEDULED C-10 CHECK, UNDER JOB CARD HC5511 FOUND HORIZONTAL STABILIZER RT L/E LOWER RIB CRACKED AT HSS 197.5 AND 203.5. REPAIRED IAW SMP583 FIG 51-140-2
- [SDR LR7A2012040500373](https://openairdocs.org/sdr/LR7A2012040500373), Apr 5, 2012: BEAM. CORRODED. DURING SCHEDULED C-10 CHECK, FOUND RT MAIN WHEEL WELL BOW BEAM OUTBD CAP CORROSION AT FS557, WL150, RBL64 / REPAIRED BY REPLACEMENT IAW LOCKHEED SMP583 CHAPTER 
- [SDR LR7A2012040500372](https://openairdocs.org/sdr/LR7A2012040500372), Apr 5, 2012: BEAM. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND LT BEAM ASSY OTBD CAP CRACKED AT FS 517, LBL 64, WL 256. REPAIRED IAW LAC MEA 382-53-12-033.
- [SDR LR7A2012040500371](https://openairdocs.org/sdr/LR7A2012040500371), Apr 5, 2012: BULKHEAD. CORRODED. DURING SCHEDULED C-10 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD CORRODED AT FS 573 TO FS 577, WL 175, RBL 61.5. REPAIRED BY REPLACEMENT IAW SMP583 CHAPTER51-60 &
- [SDR LR7A2012040500370](https://openairdocs.org/sdr/LR7A2012040500370), Apr 5, 2012: DUCT. DAMAGED. DURING SCHEDULED C-10 CHECK, FOUND NR 4 QEC, SN LMG-1869-14 OIL COOLER DUCT FWD CHIN SCOOP ASSY WITH ELONGATED FASTENER HOLES AND CRACKS. REPAIRED IAW LAC MEA 3
- [SDR LR7A2012040500369](https://openairdocs.org/sdr/LR7A2012040500369), Apr 5, 2012: STRUCTURE. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND NR 4 POSITION QEC SN LMG-1869-14 FWD BULKHEAD RT OUTER CAP TEE CRACKED AT FS 410.70. REPAIRED IAW MEA 382-54-07-081.
- [SDR LR7A2012040500368](https://openairdocs.org/sdr/LR7A2012040500368), Apr 5, 2012: FLOORBEAM. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND CABIN FLOORBEAM LOWER CAP CRACKED AT FS 577, WL 140, RBL 60. REPAIRED IAW SMP583 FIG 53-40-29.
- [SDR LR7A2012040500367](https://openairdocs.org/sdr/LR7A2012040500367), Apr 5, 2012: WINDOW FRAME. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND RT SIDE WINDOW AFT FRAME LOWER CORNER CRACKED AT FS 156, WL 225, RBL 62. REPAIRED IAW SMP583, FIG 53-30-32.
- [SDR LR7A2012040500366](https://openairdocs.org/sdr/LR7A2012040500366), Apr 5, 2012: WEB. WARPED. DURING SCHEDULED C-10 CHECK, FOUND CARGO DOOR BULKHEAD WEB WARPED AT RS9, LBL15 TO LBL30. REPAIRED IAW SMP583 FIG 51-140-17.
- [SDR LR7A2012040500364](https://openairdocs.org/sdr/LR7A2012040500364), Apr 5, 2012: RIB. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND HORIZONTAL STAB LT L/E UPPER RIB CRACKED (COMPENSATOR MOUNTING POINT) AT HSS 156 & HSS 162. REPAIRED IAW SMP583, FIG 55-20-08
- [SDR LR7A2012040500362](https://openairdocs.org/sdr/LR7A2012040500362), Apr 5, 2012: ATTACH ANGLE. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND FUSELAGE TO WING FORWARD FAIRING ATTACH ANGLE CRACKED AT FS 476, LBL 59, WL 285. REPAIRED BY REPLACEMENT IAW SMP583 51-70.
- [SDR LR7A2012040500361](https://openairdocs.org/sdr/LR7A2012040500361), Apr 5, 2012: SKIN. DENTED. DURING SCHEDULED C-10 CHECK, FOUND STONE MARKS AND WRINKLES BEYOND LIMITS ON FUSELAGE SKIN AT FS 777E, WL 140-158, LBL 60 TO RBL 60. REPAIRED BY REPLACEMENT IAW
- [SDR LR7A2012040500360](https://openairdocs.org/sdr/LR7A2012040500360), Apr 5, 2012: STRUCTURE. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND AFT FUSELAGE INTERIOR BULKHEAD INNER CAP CRACKED AT FS 858, WL 200, LBL 68. REPAIRED IAW SMP583 FIG 53-50-14.
- [SDR LR7A2012040500359](https://openairdocs.org/sdr/LR7A2012040500359), Apr 5, 2012: FLOOR SUPPORT. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND CARGO BAY UNDERFLOOR SUPPORT CRACKED FS 477, WL 130, RBL 10. REPAIRED IAW SMP583, FIG 51-140-19.
- [SDR LR7A2012040500358](https://openairdocs.org/sdr/LR7A2012040500358), Apr 5, 2012: STIFFENER. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND CARGO DOOR FLOOR STIFFENER CRACKED AT FS 1012, LBL 26, WL 270. REPAIRED BY REPLACEMENT IAW SMP583, 51-60 & 51-70.
- [SDR LR7A2012040500357](https://openairdocs.org/sdr/LR7A2012040500357), Apr 5, 2012: POST. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND LT WINDOW POST CRACKED AT FS 134, WL 251, LBL 62. REPAIRED IAW LAC MEA 382-53-12-015.
- [SDR LR7A2012040500356](https://openairdocs.org/sdr/LR7A2012040500356), Apr 5, 2012: LONGERON. CORRODED. DURING SCHEDULED C-10 CHECK, FOUND NR 3 QEC RT LOWER LONGERON CORROSION AT INNER LOWER FLANGE AT FS 473. REPAIRED BY REPLACEMENT IAW SMP583 51-70 & 54-20, PAGES
- [SDR LR7A2012040500355](https://openairdocs.org/sdr/LR7A2012040500355), Apr 5, 2012: BEAM. CORRODED. DURING SCHEDULED C-10 CHECK, UNDER JOB CARD HC5324, FOUND MLG WHEEL WELL BEAM CORROSION UNDER REIMFORCEMENT PLATE AT FS577, WL160-163, RBL61. REPAIRED IAW LAC M
- [SDR LR7A2012040500354](https://openairdocs.org/sdr/LR7A2012040500354), Apr 5, 2012: BULKHEAD WEB. CRACKED. DURING SCHEDULED C-10 CHECK, FOUND NOSE WHEEL WELL LT BULKHEAD WEB CRACKED AT FS188, LBL30, WL154. REPAIRED IAW SMP583, FIG 51-140-17.
- [SDR LR7A2011101100239](https://openairdocs.org/sdr/LR7A2011101100239), Oct 10, 2011: WEB. CRACKED. DURING SCHEDULED B-3 CHECK IAW JOB CARD HB3200, FOUND LT MAIN WHEEL WELL BOW BEAM INBD WEB CRACKED AT FS497, LBL63, WL158. REPAIR ACCOMPLISHED IAW SMP583, FIG 5
- [SDR LR7A2011101100238](https://openairdocs.org/sdr/LR7A2011101100238), Oct 10, 2011: SKIN. CRACKED. DURING SCHEDULED B-3, CHECK IAW JOB CARD HB2703 FOUND LT INBD FLAP UPPER SKIN CRACKED AT CWS120 BUMPER PAD AREA. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-12.
- [SDR LR7A2011101100237](https://openairdocs.org/sdr/LR7A2011101100237), Oct 10, 2011: STRUCTURE. CRACKED. DURING SCHEDULED B-3 CHECK IAW FOUND AFT FUSELAGE RT BULKHEAD INNER CAP REPAIR MEMBER CRACKED AT FS814, RBL70, WL175. REPAIR ACCOMPLISHED BY REPLACING DOUBLER I
- [SDR LR7A2011101100236](https://openairdocs.org/sdr/LR7A2011101100236), Oct 10, 2011: SKIN. CRACKED. DURING SCHEDULED B-3 CHECK IAW JOB CARD HB5301, FOUND RAMP DOOR EXTERNAL SKIN CRACK AT RS1 TO RS1.6, BL0. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-12.
- [SDR LR7A2011080400223](https://openairdocs.org/sdr/LR7A2011080400223), Aug 3, 2011: SKIN. CRACKED. DURING REGULAR A-CHECK, FOUND FUSELAGE SKIN CRACK AT FS 196 TO 204, WL 126, LBL 27. MX FERRY TO FOR REPAIR. LOG PAGE NR 37654 M1.
- [SDR LR7A2011032300171](https://openairdocs.org/sdr/LR7A2011032300171), Mar 11, 2011: MOUNT. SCORED. DURING SCHEDULED B-2 CHECK PER JOBCARD HB7251 FOUND NR 2 ENGINE UPPER INBOARD AND OUTBOARD AND LOWER OUTBOARD TRUSS MOUNT BORES WITH SCORING DAMAGE AT CWS178L &
- [SDR LR7A2011032300170](https://openairdocs.org/sdr/LR7A2011032300170), Mar 11, 2011: MOUNT. SCORED. DURING SCHEDULED B-2 CHECK PER JOB CARD HB7251 FOUND NR 1 ENGINE UPPER INBOARD AND OUTBOARD TRUSS MOUNT BORES WITH SCORING DAMAGE AT OWS 162L & 197L. REPAIRED I
- [SDR LR7A2011032300169](https://openairdocs.org/sdr/LR7A2011032300169), Mar 11, 2011: FLOOR PANEL. CRACKED. DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND AFT CARGO DOOR FLOOR PANEL CRACKED AT FS 880 RBL 58. REPAIRED IAW LOCKHEED SRM SMP583 FIG 51-140-17.
- [SDR LR7A2011032300168](https://openairdocs.org/sdr/LR7A2011032300168), Mar 11, 2011: WEB. DENTED. DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND AFT CARGO DOOR WEB DENTED AT FS 902, BL 0. REPAIRED IAW LOCKHEED SRM SMP583CH 51-140, FIG 51-140-17.
- [SDR LR7A2011032300167](https://openairdocs.org/sdr/LR7A2011032300167), Mar 11, 2011: WEB. DENTED. DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND AFT CARGO DOOR WEB DENTED FS 880, BL 0. REPAIRED IAW LOCKHEED SRM SMP583 FIG 51-140-17.
- [SDR LR7A2011032300166](https://openairdocs.org/sdr/LR7A2011032300166), Mar 11, 2011: WEB. CRACKED. DURING SCHEDULED B-2 CHECK PER JOBCARD HB5302 FOUND CRACKED WEB AT FS 880, RBL 62, WL 250. REPAIRED IAW LOCKHEED SRM SMP583 CH 51-60 AND FIG 51-140-17.

All 416: https://openairdocs.org/aircraft/N404LC/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/N404LC/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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