# N374AA: Anduril Industries BARRACUDA 500 - Status: Valid registration - Airframe: [Anduril Industries BARRACUDA 500](https://openairdocs.org/model/anduril-industries-barracuda-500) (registry code 06102KS) - Serial number: 006 - Type: Fixed wing single engine - Engine type: Turbo-jet - Mode S code: A442A8 - Registered owner: [Anduril Industries Inc](https://openairdocs.org/faa-owner/ANDURIL%20INDUSTRIES%20INC) - Location: [Costa Mesa, CA](https://openairdocs.org/faa-place/CA/Costa%20Mesa) - Owner type: Corporation - Owner's area on the map: 33.6796° N, 117.9085° W: Placed by OpenAirDocs at the center of ZIP code 92626, 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=374AA - Page: https://openairdocs.org/aircraft/N374AA 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): 0 in force ### Matched by airframe (Anduril Industries BARRACUDA 500) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N374AA. ## FAA accident and incident reports None matched to N374AA. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N374AA not matched to an aircraft (115, newest 50) They name N374AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR MK1Y20180515002](https://openairdocs.org/sdr/MK1Y20180515002), May 15, 2018: FRAME. CRACKED. DURING PERFORMANCE OF AD 2012-22-17 AND SB 53A0209, FOUND A CRACK, 0.200 INCH IN THE FRAME INNER TRANSITION RADIUS. BS 903.5, RBL 89. - [SDR MK1Y20180515001](https://openairdocs.org/sdr/MK1Y20180515001), May 15, 2018: FRAME. CRACKED. DURING PERFORMANCE OF AD 2012-22-17 AND SB 53A0209, FOUND A CRACK, 0.240 INCH, IN THE FRAME INNER TRANSITION RADIUS BS 883.5 RBL 89. - [SDR AALA201712059055](https://openairdocs.org/sdr/AALA201712059055), Dec 2, 2017: SLIDING WINDOW. OUT OF ADJUST. AIRCRAFT WAS IN BASE MAINTENANCE. FIRST OFFICER'S SLIDING WINDOW VERY DIFFICULT TO MOVE TO THE FORWARD POSITION AND OVERCOME MECHANISM SPRINGS AFT. ADJUSTED INB - [SDR AALA201712069028](https://openairdocs.org/sdr/AALA201712069028), Dec 2, 2017: WINDOW. FAILED. AIRCRAFT IN BASE MAINTENANCE. LEFT HAND WINDSHIELD CRACKED, SHATTERED WITH WINDOW HEAT ON. REPLACED WINDSHIELD PER AMM 56-11-01. - [SDR AALA20171126004](https://openairdocs.org/sdr/AALA20171126004), Nov 26, 2017: SPAR. DAMAGED. AIRCRAFT IN BASE MAINTENANCE, HOLE ON THE VERTICAL STABILIZER AUX SPAR WAS ELONGATED BETWEEN FSS 54 AND FSS 61, LHS. REPAIRED PER EA NR 271511. - [SDR AALA20170727007](https://openairdocs.org/sdr/AALA20170727007), Jul 27, 2017: PANEL. DELAMINATED. DELAMINATION ON RIGHT VERTICAL STABILIZER BETWEEN THE AUXILIARY SPAR AND FRONT SPAR, STABILIZER STATIONS 39 TO 92 REMOVED AND REPLACED PANEL PER SRM 51-70-10-2R - [SDR AALA20170727006](https://openairdocs.org/sdr/AALA20170727006), Jul 27, 2017: PANEL. DELAMINATED. DELAMINATION ON RIGHT VERTICAL STABILIZER BETWEEN THE AUXILIARY SPAR AND FRONT SPAR, VSS 195 TO 270. REMOVED AND REPLACED THE PANEL IAW SRM 51-70-10-2R, AND SRM - [SDR AALA20170724007](https://openairdocs.org/sdr/AALA20170724007), Jul 24, 2017: FLOORBEAM. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON CENTER WING SECTION FLOOR BEAM BETWEEN FUSELAGE STATIONS 800 AND 845, LBL11.5. ACCOMPLISHED SPLICE REPAIR PER SRM - [SDR AALA20170712003](https://openairdocs.org/sdr/AALA20170712003), Jul 12, 2017: FLOORBEAM. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON UPPER CHORD FLOORBEAM UNDER STRAP AND AT SPLICE STRAP, FUSELAGE STATION 1480, BETWEEN RBL65 AND RBL88. REPAIRED P - [SDR AALA20170712002](https://openairdocs.org/sdr/AALA20170712002), Jul 12, 2017: FLOORBEAM. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON UPPER CHORD FLOORBEAM AT FUSELAGE STATION 325, BETWEEN RBL20 AND RBL40. REPAIRED T-CHORD AT STATION 325 BETWEEN L - [SDR AALA20170706010](https://openairdocs.org/sdr/AALA20170706010), Jul 6, 2017: SKIN. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON FUSELAGE SKIN LAP SEAM AT THE 5:00 POSITION BEHIND THE RIGHT MAIN LANDING GEAR WHEEL WELL, FUSELAGE STATION 1197+ - [SDR AALA20170628015](https://openairdocs.org/sdr/AALA20170628015), Jun 28, 2017: STRINGER. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT PIT STRINGER 36R BETWEEN FUSELAGE STATIONS 1197+22 TO 1197+44. REMOVED AND REPLACED STRINGER SEGMENT IAW SRM - [SDR AALA20170628013](https://openairdocs.org/sdr/AALA20170628013), Jun 28, 2017: FLOORBEAM. CORRODED. AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON MAIN DECK FLOOR BEAM UPPER CHORD AT FUSELAGE STATION 764 BETWEEN LBL64 AND LBL80. REPAIRED IAW SRM 53-00-51-2R-1 - [SDR AALA20171201007](https://openairdocs.org/sdr/AALA20171201007), May 21, 2017: SKIN. CORRODED. AIRCRAFT IN BASE MAINTENANCE. AFT CARGO STATION 1087 TO 7 INCHES AFT OF STATION 1109, BETWEEN STRINGER 37L AND 39L, INNER SKIN HAS THREE AREAS OF CORROSION. REP - [SDR AALA20150911011](https://openairdocs.org/sdr/AALA20150911011), Aug 26, 2015: SKIN. CORRODED. LAP SEAM AT STRINGER 36R CORRODED AT FS 1197. - [SDR AALA20150616015](https://openairdocs.org/sdr/AALA20150616015), Jun 16, 2015: BATTERY PACK. DISCHARGED. 4L & 4R DOOR EMER EXIT SIGNS ARE INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07. OPERATIONS TESTED OK IAW AMM 33-51-00. - [SDR AALA20140616019](https://openairdocs.org/sdr/AALA20140616019), Jun 16, 2014: LIGHT. INOPERATIVE. LEFT NR 4 DOOR EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EMER EXIT SIGN. OPERATIONS CHECKED NORMAL. - [SDR AALA20140507002](https://openairdocs.org/sdr/AALA20140507002), May 7, 2014: CAP. CORRODED. CORROSION FOUND ON J CAP IN FWD CARGO AT STATION 566 & LBL 40. SPLICED IN NEW J CAP SECTION IAW SRM 53-00-07. - [SDR AALA20140428014](https://openairdocs.org/sdr/AALA20140428014), Apr 24, 2014: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR FAILED TEST. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR, OPERATIONS CHECKED NORMAL. - [SDR AALA20140428013](https://openairdocs.org/sdr/AALA20140428013), Apr 24, 2014: REFLECTOR. DEFECTIVE. EXTERIOR EMERGENCY LIGHT AT LT NR 4 DOOR FAILED TEST. REPLACED LAMP HOLDER REFLECTOR, OPERATIONS CHECKED NORMAL. - [SDR AALA20140228001](https://openairdocs.org/sdr/AALA20140228001), Feb 27, 2014: WIRE HARNESS. DEFECTIVE. JFK INFLIGHT ORD-LHR CREW REPORTED LT HAND ENG EXHAUST GAS TEMPERATURE ERRATIC. FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPL - [SDR AALA20131231004](https://openairdocs.org/sdr/AALA20131231004), Dec 31, 2013: PRESSURE SWITCH. INOPERATIVE. MIA CREW REPORTED CTR HYD SYS HAD LOSS PRESSURE LIGHT & EICAS MESSAGE. FLIGHT LANDED MIA WITHOUT INCIDENT. REPLACED CTR HYD PUMP PRESSURE SWITCH. SYSTEM GND CHE - [SDR AALA20131121010](https://openairdocs.org/sdr/AALA20131121010), Nov 21, 2013: BULKHEAD. DAMAGED. LT PYLON WAS FOUND TO AN OVERSIZED HOLE IN THE AFT BULKHEAD, COMMON TO THE MID SPAR FITTING. REMOVED HOLE IN BULKHEAD ROUND & TRUE TO DIAMETER OF .625 & INSTALL - [SDR AALA20131121008](https://openairdocs.org/sdr/AALA20131121008), Nov 21, 2013: FITTING. DAMAGED. RT PYLON WAS FOUND TO HAVE TWO OVERSIZED HOLES. THE HOLES ARE COMMON TO THE AFT BULKHEAD, SIDE LOAD FITTING INBD & OTBD, & MIDSPAR FITTING INBD & OTBD. REAMED T - [SDR AALA20131121006](https://openairdocs.org/sdr/AALA20131121006), Nov 21, 2013: SPAR. DAMAGED. LT HAND PYLON WAS FOUND TO AN OVERSIZED HOLE COMMON TO THE INBD MIDSPAR FITTING, MIDSPAR WEB & T-CHORD FITTING & STRAP. ACCOMPLISHED REPAIR IAW EA 767-54-032580 - [SDR AALA20131121003](https://openairdocs.org/sdr/AALA20131121003), Nov 21, 2013: SKIN. DAMAGED. LT HAND PYLON WAS FOUND TO AN OVERSIZED HOLE IN THE INBD SKIN, COMMON TO THE SIDE LOAD FITTING, NEAR A GSE FITTING. ACCOMPLISHED REPAIR IAW EA B767 54-032581 & - [SDR AALA20121107017](https://openairdocs.org/sdr/AALA20121107017), Nov 7, 2012: STRUCTURE. CRACKED. RIGHT PYLON INSIDE FORWARD TORQUE BOX ACCESS, UPPER SKIN AT CUTOUT FOR POWER FEEDER CABLES CRACKED AT NUT PLATE AT AFT INBOARD SIDE. INSTALLED DOUBLER PER AARD - [SDR AALA20121107016](https://openairdocs.org/sdr/AALA20121107016), Nov 7, 2012: TORQUE BOX. CRACKED. LEFT PYLON UPPER TORQUE BOX SKIN CRACKED AT GENERATOR FEEDER CABLE PASS THROUGH, OUTBOARD AFT NUT PLATE. INSTALLED DOUBLER REPAIR PER AARD 54-52-01. - [SDR AALA20121107015](https://openairdocs.org/sdr/AALA20121107015), Nov 7, 2012: CAP. CORRODED. SHORT J-CAP AT LOWER DOOR CUTOUT IN FORWARD CARGO HAS CORROSION ON BOTTOM SIDE AT NUT PLATE STATION 504. REPLACED J-CAP PER SRM 51-10-02. - [SDR AALA20121107006](https://openairdocs.org/sdr/AALA20121107006), Nov 7, 2012: FRAME. CRACKED. FORWARD CARGO BODY FRAME STATION 500 UPPER FLANGE IS BENT AND HAS A LONG CRACK, ABOVE AND AROUND STRINGER 31 LEFT. FABRICATED NEW SECTION OF FRAME UPPER FLANGE - [SDR AALA20121103003](https://openairdocs.org/sdr/AALA20121103003), Oct 31, 2012: FRAME. CORRODED. STATION 1219 CARGO FLOOR INNER J FRAME CORRODED. INSTALLED REPAIR STRAP PER SRM 53-00-07-2R. - [SDR AALA20121114014](https://openairdocs.org/sdr/AALA20121114014), Oct 30, 2012: SKIN. DAMAGED. UPPER FUSELAGE SKIN ON RIGHT SIDE OF VERTICAL STABILIZER BETWEEN STATIONS 1605 AND 1629 DAMAGED. INSTALLED EXTERNAL DOUBLER PER SRM 530-00-01-2R 1. - [SDR AALA20121113010](https://openairdocs.org/sdr/AALA20121113010), Oct 29, 2012: WEDGE. DELAMINATED. GOUGE/DELAMINATION TO NUMBER 6 SLAT TRAILING EDGE WEDGE, UNDER SIDE. LOCATED 8.5 INCHES INBOARD OF OUTBOARD END. ACCOMPLISHED METAL BOND REPAIR PER SRM. - [SDR AALA20121101002](https://openairdocs.org/sdr/AALA20121101002), Oct 28, 2012: SKIN. CRACKED. CRACK IN NUMBER 10 LEADING EDGE SLAT SKIN, 42 INCHES FROM INBOARD END. INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-01-2R 2. - [SDR AALA20121101001](https://openairdocs.org/sdr/AALA20121101001), Oct 28, 2012: SLAT. CRACKED. CRACK IN NUMBER 9 LEADING EDGE SLAT, 42 INCHES FROM INBOARD END. INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-01-2R 2. - [SDR AALA20121008005](https://openairdocs.org/sdr/AALA20121008005), Oct 8, 2012: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHTS 1 TO 4 FAILED TO ILLUMINATE. REPLACED LAMP. OPS CHECK NORMAL. - [SDR AALA20120924027](https://openairdocs.org/sdr/AALA20120924027), Sep 21, 2012: LIGHT. INOPERATIVE. LEFT NUMBER 1 DOOR LOWER EMERGENCY LIGHTS ON UPPER SIGN INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR LOWER EMERGENCY LIGHTS ON UPPER SIGN. OPS CHECK NORMAL - [SDR AALA20120921023](https://openairdocs.org/sdr/AALA20120921023), Sep 21, 2012: LIGHT. INOPERATIVE. LEFT NUMBER 2 DOOR LOWER EMERGENCY LIGHT ON UPPER SIGN INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR LOWER EMERGENCY LIGHT ON UPPER SIGN. OPS CHECK NORMAL. - [SDR AALA20120921022](https://openairdocs.org/sdr/AALA20120921022), Sep 21, 2012: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT ABOVE DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY IN COCKPIT FOR EMERGENCY EXIT LIGHT ABOVE DOOR. OPS CHECK NORMAL. - [SDR AALA20120921021](https://openairdocs.org/sdr/AALA20120921021), Sep 21, 2012: LIGHT. INOPERATIVE. LEFT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120921019](https://openairdocs.org/sdr/AALA20120921019), Sep 21, 2012: LIGHT. INOPERATIVE. RIGHT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120808007](https://openairdocs.org/sdr/AALA20120808007), Aug 8, 2012: LIGHT. INOPERATIVE. RIGHT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120222010](https://openairdocs.org/sdr/AALA20120222010), Feb 20, 2012: LENS. MISSING. EMERGENCY EXIT SIGN LENS MISSING AT SEAT 21G. REPLACED LENS FOR EMERGENCY EXIT SIGN AT SEAT 21G. OPS CHECKED NORMAL. - [SDR AALA20120210MIA02](https://openairdocs.org/sdr/AALA20120210MIA02), Feb 10, 2012: ENGINE. FAILED. MIA - CREW REPORTED LEFT ENGINE OIL LOSS. LEFT ENGINE SHUTDOWN (SINGLE ENGINE TIME 20 MINS). EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REM - [SDR AALA20120116MIA01](https://openairdocs.org/sdr/AALA20120116MIA01), Jan 15, 2012: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT RIGHT NUMBER 1 DOOR THRESHOLD INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER DOOR THRESHOLD EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20111021MIA02](https://openairdocs.org/sdr/AALA20111021MIA02), Oct 21, 2011: LIGHT. INOPERATIVE. LEFT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20111021MIA01](https://openairdocs.org/sdr/AALA20111021MIA01), Oct 21, 2011: LIGHT. INOPERATIVE. RIGHT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20110929DFW01](https://openairdocs.org/sdr/AALA20110929DFW01), Sep 28, 2011: CONNECTOR. DEFECTIVE. SEAT 33H EMERGENCY LIGHT INOPERATIVE. REPINNED SEAT 33H EMERGENCY LIGHT CONNECTOR OPS CHECK NORMAL. - [SDR AALA20110606AFW01](https://openairdocs.org/sdr/AALA20110606AFW01), Jun 3, 2011: SWIVEL FITTING. CORRODED. CORROSION ON THE LEFT MAIN LANDING GEAR SIDE STRUT SWIVEL FITTING. THE CORROSION IS LIMITED TO THE OUTBOARD LUG OUTBOARD FACE OF THE MAIN PIVOT JOINT TO THE MAI - [SDR AALA20110326DEN01](https://openairdocs.org/sdr/AALA20110326DEN01), Mar 25, 2011: OXYGEN MASK. LEAKING. DEN - INFLIGHT JFK-SFO. CREW REPORTED FLIGHT DECK O2 PRESSURE DROPPING DURING FLIGHT. FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. CAPTAINS O2 MASK FOUND TO BE All 115: https://openairdocs.org/aircraft/N374AA/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Anduril Industries BARRACUDA 500 aircraft: https://openairdocs.org/model/anduril-industries-barracuda-500/aircraft.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.