# N302AA: 1982 Boeing 767-223, registration cancelled 2007-07-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 30, 2007 - Status when cancelled: Valid registration - Airframe: [Boeing 767-223](https://openairdocs.org/model/boeing-767-223) (registry code 1385123) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) (OpenAirDocs) - Serial number: 22308 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: November 18, 1982 - Certificate issued: September 23, 2005 - Last registry action: June 25, 2007 - Mode S code: A326C1 - Owner when cancelled: [Scroggins Aviation Inc](https://openairdocs.org/faa-owner/SCROGGINS%20AVIATION%20INC) - Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas) - Owner type: Corporation - Owner's area on the map: 36.2535° N, 115.2267° W: Placed by OpenAirDocs at the center of ZIP code 89130, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N302AA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=302AA - Page: https://openairdocs.org/deregistered/N302AA-2007-07-30 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 767-223: https://openairdocs.org/model/boeing-767-223.md ## Service difficulty reports (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA20040257](https://openairdocs.org/sdr/AALA20040257), Feb 20, 2004: BATTERY PACK. DISCHARGED. MIA - EMERGENCY LIGHT AT ROWS 16D AND 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 16D AND 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20011682](https://openairdocs.org/sdr/AALA20011682), Aug 23, 2001: LIGHT. DIRTY. LAX - DURING OVERNIGHT MAINTENANCE, AFT 'IN SEAT' EMERGENCY LIGHT AT SEAT 11H INOPERATIVE. CLEANED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20001352](https://openairdocs.org/sdr/AALA20001352), Aug 18, 2000: WIRE. SHORTED. LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEATS 9H THROUGH 19H INOPERATIVE. REPAIRED WIRE AT SEAT 19H. SYSTEM GROUND CHECK NORMAL - [SDR AALA20000148](https://openairdocs.org/sdr/AALA20000148), Jan 27, 2000: NOZZLE FEEDER. DAMAGED. ORD - FLT 180 - DURING FLIGHT, AIRCRAFT YAWED AND CREW NOTED N1 EGT AND N2 WINDING DOWN. SHUTDOWN ENGINE. ATTEMPTED INFLIGHT START NO SUCCESS. DIVERTED AND LAND - [SDR AALA991621](https://openairdocs.org/sdr/AALA991621), Oct 24, 1999: CONNECTOR. LOOSE. SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS FROM 9H TO 19H ON RIGHT SIDE OF AIRCRAFT INOPERATIVE. SECURED POWER SUPPLY CONNECTOR TO EMERGENCY - [SDR AALA994169](https://openairdocs.org/sdr/AALA994169), Oct 6, 1999: SKIN. CORRODED. AFW - RIGHT WING UPPER SURFACE SKIN HAS CORROSION AND INTERGRANULAR CORROSION AT FASTENER LOCATION. REPAIRED PER MRB 767-1960. DRILLED OUT THE CORRODED FASTENER - [SDR AALA994170](https://openairdocs.org/sdr/AALA994170), Oct 1, 1999: SKIN. CORRODED. AFW - FUSELAGE SKIN AT S2R STA 718 HAD CORROSION BLENDED BEYOND LIMITS. REPAIRED PER MRB 767-1962. REMOVED CORROSION PER 767-200 SRM 53 FIG 101. REPLACED FASTEN - [SDR AALA994172](https://openairdocs.org/sdr/AALA994172), Sep 30, 1999: FLOORBEAM. CORRODED. AFW - FLOORBEAM AT STA 286 RBL 49 HAD CORROSION BLENDED ON TOP SURFACE BEYOND SRM LIMITS. REPAIRED PER MRB 767-1959. FABRICATED STRAP OUT OF 301 1/2H 55 .050 IN - [SDR AALA990682](https://openairdocs.org/sdr/AALA990682), May 10, 1999: WIRE. LOOSE. SFO - DURING MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT SEAT ROW 24B INOPERATIVE. REPAIRED EMERGENCY EXIT WIRING AT SEAT ROW 24B. SYSTEM GROUND CHECKED NORMAL O - [SDR AALA981199](https://openairdocs.org/sdr/AALA981199), Jun 19, 1998: SWITCH. FAILED. LAX - FLT 10 - AFTER TAKEOFF LAX, AIR INTERRUPTURED WITH LEFT WING EVACUATION SLIDE EICAS MESSAGE. RETURN AND LANDED LAX WITHOUT INCIDENT. REPLACED AND ADJUSTED - [SDR AALA984105](https://openairdocs.org/sdr/AALA984105), May 13, 1998: STRINGER. CORRODED. AFW - FUSELAGE STRINGER AT STATION 1307 HAS CORROSION. FABRICATED NEW STRINGER SPLICE AND INSTALLED PER SRM. (M) - [SDR AALA984112](https://openairdocs.org/sdr/AALA984112), May 11, 1998: FRAME. CORRODED. AFW - FUSELAGE FRAME AT CAP UPPER SURFACE HAS CORROSION. BLENDED AND REFINISHED PER SRM 53-00-07 FIGURE 101. (M) - [SDR AALA984111](https://openairdocs.org/sdr/AALA984111), May 11, 1998: KEEL BEAM. CORRODED. AFW - LEFT KEEL BEAM OUTER FLANGE HAD SEVERE CORROSION. CUT OUT CORRODED AREA. FABRICATED A FILLER PIECE FROM 7075-T6 AND A STIFFENING ANGLE FROM 7075-T6 AND IN - [SDR AALA984106](https://openairdocs.org/sdr/AALA984106), May 11, 1998: SPLICE. CORRODED. AFW - STRINGER AND STRINGER SPLICE AT 537L HAD CORROSION. FABRICATED AND REPLACEMENT STRINGER SPLICE FROM .071 INCH THICK 7075-T6 ALCLAD. INSTALLED PER SRM 51-4 - [SDR AALA984114](https://openairdocs.org/sdr/AALA984114), May 8, 1998: FIRE SEAL. WORN. AFW - FOUND WEAR ON INBOARD AND OUTBOARD OF LEFT PYLON FIRE SEAL AND 2 GAUGES ON PYLON AFT OF PNL 416BR. BLENDED DAMAGED AREA PER SRM, VERIFIED NO CRACKS AND RE - [SDR AALA984113](https://openairdocs.org/sdr/AALA984113), May 8, 1998: SKIN. CORRODED. AFW - AREA OF CORROSION IN FORWARD CARGO AT ALTIMETER ANTENNA AT STATION 587.5, JUST LEFT OF BL 0. ENSURE THE BLENDOUT IS FLAT IN AREA OF NUTPLATE FOR PROPER RE - [SDR AALA984110](https://openairdocs.org/sdr/AALA984110), May 8, 1998: FRAME. CORRODED. AFW - WHILE IN FOR MBV, MAINTENANCE FOUND AN AREA OF CORROSION ON THE FWD FACE OF THE VERTICAL FLANGE OF THE INNER CHORD ABOVE STRINGER 33R. ENSURE BLENDOUT IS - [SDR AALA984109](https://openairdocs.org/sdr/AALA984109), May 8, 1998: FRAME. CORRODED. AFW - FAIL/SAFE CHORD HAS CORROSION. FABRICATE A REPAIR ANGLE FROM 7075T6 USING BAC1503400141 THE CORNER OF THE ANGLE SHOULD BE CHAMFERED TO ALOOW PROPER NESTIN - [SDR AALA984108](https://openairdocs.org/sdr/AALA984108), May 8, 1998: STRINGER. CORRODED. AFW - STRINGER SPLICE AND STRINGER HAD CORROSION. FABRICATE A REPLACEMENT STRINGER SPLICE FROM .071 THICK 7075-T6. (M) - [SDR AALA972252](https://openairdocs.org/sdr/AALA972252), Nov 26, 1997: SENSOR. DEFECTIVE. ABQ - FLT 0076 - EN ROUTE LAX/IAD DURING CRUISE, RIGHT WING SLIDE DEPLOYMENT LIGHT ON UPPER EICAS SCREEN ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES AND DIVERTED - [SDR AALA961740](https://openairdocs.org/sdr/AALA961740), Dec 1, 1996: HYD SYSTEM. REQ SERVICE. ORD - FLT 177 - EN ROUTE JFK-ORD, DURING CRUISE, CENTER HYDRAULIC SYSTEM LOW QTY MESSAGE. ACCOMPLISHED ALTERNATE LANDING GEAR AND ALTERNATE FLAP PROCEDURES AND - [SDR AALA951175](https://openairdocs.org/sdr/AALA951175), Jun 23, 1995: FITTING. CORRODED. AFW - FOUND INTERNAL CORROSION ON THE TEE FITTING LOCATED NEXT TO THE AFT FASTENER HOLE. TRIMMED OUT DISCREPANT AREA. APPLIED ALODINE AND PRIMED. FABRICATED AND - [SDR AALA951174](https://openairdocs.org/sdr/AALA951174), Jun 23, 1995: FRAME. CORRODED. AFW - FOUND AND BLENDED OUT CORROSION ON AFT CARGO FRAME WEB JUST BELOW INNER CHORD AT LBL 32. BLEND OUT GOES ALL OF THE WAY THROUGH THE WEB. FABRICATED AND INS - [SDR AALA951173](https://openairdocs.org/sdr/AALA951173), Jun 23, 1995: SKIN STRAP. CORRODED. AFW - TEAR STRAP CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGI - [SDR AALA951172](https://openairdocs.org/sdr/AALA951172), Jun 23, 1995: STRINGER. CORRODED. AFW - STRINGER CORRODED AROUND FASTENER HOLES. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NO - [SDR AALA951171](https://openairdocs.org/sdr/AALA951171), Jun 23, 1995: FLOORBEAM. CORRODED. AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF-HARD ST - [SDR AALA951170](https://openairdocs.org/sdr/AALA951170), Jun 23, 1995: FLOORBEAM. CORRODED. AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 H - [SDR AALA951169](https://openairdocs.org/sdr/AALA951169), Jun 23, 1995: FLOORBEAM. CORRODED. AFW - FLOORBEAM CORRODED. AFTER BLENDING, FOUND DAMAGE BEYOND SRM LIMITS. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED A REPAIR STRAP USING .050 - [SDR AALA951167](https://openairdocs.org/sdr/AALA951167), Jun 23, 1995: FLOORBEAM. CORRODED. AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE IN NOTED CONDITION BY ENGINE - [SDR AALA951160](https://openairdocs.org/sdr/AALA951160), Jun 23, 1995: STRAP. CORRODED. AFW - FAIL SAFE STRAP LOCATED ON THE FORWARD SIDE OF THE AFT CARGO DOOR CUT-OUT CORRODED JUST BELOW 533R AND JUST BELOW 532R. BOTH EXCEEDED SRM LIMITS AFTER BLE - [SDR AALA951159](https://openairdocs.org/sdr/AALA951159), Jun 23, 1995: SILL. CORRODED. AFW - INNER CHORD CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REINSTALLED FASTENERS WITH SHIM AS REQUIRED AFTER ALODING BLENDED AREAS. APPROVED BY ENGINEE - [SDR AALA951158](https://openairdocs.org/sdr/AALA951158), Jun 23, 1995: DOOR FRAME. CORRODED. AFW - FOUND CORROSION ON THE FORWARD SIDE OF THE VERTICAL LEG OF THE INNER CHORD. ALODINED BLENDED AREA AND REINSTALLED FASTENERS. APPROVED FOR CONTINUED SERVIC - [SDR AALA951156](https://openairdocs.org/sdr/AALA951156), Jun 23, 1995: SEAT TRACK. CORRODED. AFW - FOUND CORROSION ON THE SEAT TRACK OUTBOARD FLANGE AT LBL 11 AND ON THE INBOARD FLANGE AT RBL 11. FLAP PEENED BLENDED AREAS. PRIMED BLENDED AREAS. APPROVED - [SDR AALA951155](https://openairdocs.org/sdr/AALA951155), Jun 23, 1995: SKIN. CORRODED. AFW - LOWER FUSELAGE SKIN OUTER SURFACE UNDERNEATH VHF ANTENNA CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REINSTALLED ANTENNA WITH NEW FASTENERS. APPROVE ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19860116013309I](https://openairdocs.org/incident/19860116013309I), Jan 16, 1986: Boeing 767223 (N302AA), Mina, NV. Alert system activated when controller issued a heading change to 2 aircraft. Lost separation. - [Incident 19831017066949I](https://openairdocs.org/incident/19831017066949I), Oct 17, 1983: Boeing 767 (N302AA), Chicago, IL. Taxiing to gate passenger threatened crew with bodily harm. Tried to skyjack airplane. ## Other aircraft with N302AA - [Cancelled 2020-05-01](https://openairdocs.org/deregistered/N302AA-2020-05-01): DJI INSPIRE 1, S/N W13DCB04020614. Registration expired, pending cancellation. Owner: [Robinson Jeffrey Aaron](https://openairdocs.org/faa-owner/ROBINSON%20JEFFREY%20AARON), [Waupaca, WI](https://openairdocs.org/faa-place/WI/Waupaca) --- 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.