# N304AA: 1983 Boeing 767-223, registration cancelled 2017-06-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 19, 2017
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 767-223](https://openairdocs.org/model/boeing-767-223) (registry code 1385123)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 22310
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 25, 1983
- Certificate issued: August 9, 2007
- Last registry action: August 9, 2007
- Mode S code: A32E2F
- Owner when cancelled: [Icg Aircraft Holdings LLC](https://openairdocs.org/faa-owner/ICG%20AIRCRAFT%20HOLDINGS%20LLC)
- Location: [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles)
- Owner type: Corporation
- Owner's area on the map: 34.0454° N, 118.4459° W: Placed by OpenAirDocs at the center of ZIP code 90025, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N304AA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=304AA
- Page: https://openairdocs.org/deregistered/N304AA-2017-06-19

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 (24)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR AALA20021903](https://openairdocs.org/sdr/AALA20021903), Dec 28, 2002: ENGINE. LEAKING. SHORLTY AFTER TAKEOFF, AIRCRAFT AIR INTERRUPTED DUE TO SMOKE/VAPOR IN AFT CABIN ON CLIMB-OUT. AIRCRAFT RETURNED TO JFK LANDED WITHOUT INCIDENT. RELACED RIGHT EN
- [SDR AALA20011837](https://openairdocs.org/sdr/AALA20011837), Sep 30, 2001: MODULE. DEFECTIVE. JFK - FLT 21 - EN ROUTE JFK-LAX - DETECTED LOSS OF CENTER HYDRAULIC SYSTEM FLUID. RETURNED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT CENTER PRESSU
- [SDR AALA20010025](https://openairdocs.org/sdr/AALA20010025), Jan 5, 2001: LIGHT. INOPERATIVE. LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 11B BROKEN. REPLACED EMERGENCY EXIT AFT AISLE LIGHT STRIP AT SEAT 11B. SYSTEM GROUND CHECKED NO
- [SDR AALA20001737](https://openairdocs.org/sdr/AALA20001737), Oct 20, 2000: CONNECTOR. DAMAGED. LAX - DURING OVERNIGHT MAINTENANCE, TWO CROSS AISLE EMERGENCY EXIT LIGHTS UNDER FORWARD GALLEY FLIGHT ATTENDANT SEAT INOPERATIVE. REPAIRED CONNECTOR PIN AT BATT
- [SDR AALA991901](https://openairdocs.org/sdr/AALA991901), Dec 14, 1999: SOCKET. FAILED. LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEATS 7B AND 28B INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT SOCKET AT SEATS 7B AND 28B. SY
- [SDR AALA994181](https://openairdocs.org/sdr/AALA994181), Oct 29, 1999: SKIN. CORRODED. AFW - LEFT/RIGHT WINGS UPPER SKIN HAS CORROSION BLENDOUTS. CORROSION BLENDED, FASTENERS REPLACED, AREA CHECKED FOR CRACKS. RE-FINISHED PER MB 767-196. TST: 55,7
- [SDR AALA994182](https://openairdocs.org/sdr/AALA994182), Oct 15, 1999: BULKHEAD STRAP. CRACKED. AFW - FAIL SAFE STRAP ON LEFT WHEELWELL REAR SPAR BULKHEAD IS CRACKED. SHORED AN BRACED AIRCRAFT. DISASSEMBLED REAR SPAR AND INSTALLED NEW FAIL SAFE STRAP. RE-A
- [SDR AALA984073](https://openairdocs.org/sdr/AALA984073), Apr 17, 1998: STRINGER. CORRODED. AFW - FOUND CORROSION WAS FOUND ON STRINGER 539R UNDER THE STATION 130. FABRICATE A REPLACEMENT STRINGER SPLICE FROM THE SAME MATERIAL AND THICKNESS AS ORIGINAL
- [SDR AALA984077](https://openairdocs.org/sdr/AALA984077), Apr 16, 1998: STRAP. CORRODED. AFW - BLENDED OUT TWO AREAS OF CORROSION ON THE UPPER SURFACE OF THE 146T1043-3 FAIL/SAFE CHORD OF THE FRAME AT STATION 1270. REFINISHED THE BLENDED AREAS PER S
- [SDR AALA984076](https://openairdocs.org/sdr/AALA984076), Apr 16, 1998: FRAME. CORRODED. AFW - BLENDED OUT AN AREA OF CORROSION ON THE AFT SIDE OF THE VERTICAL FLANGE OF THE 146T1044-2 INNER CHORD JUST OUTBOARD OF STRINGER 36R. REFINISHED THE BLENDE
- [SDR AALA984075](https://openairdocs.org/sdr/AALA984075), Apr 16, 1998: SKIN. CORRODED. AFW - WING BOX UPPER SKIN AT STATION N955 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION PER SRM 51-10-00. EDDY CURRENT REWORKED AREA FOR CRACKS.
- [SDR AALA984072](https://openairdocs.org/sdr/AALA984072), Apr 16, 1998: SKIN. CORRODED. AFW - FUSELAGE HAS CUTOUT DUE TO CORROSION ON THE INTERIOR SURFACE OF SKIN AT STATION 1356.5 TO 1362. ACCOMPLISHED REPAIR TO THE SKIN AT STATION 1356.5-1362 USI
- [SDR AALA984074](https://openairdocs.org/sdr/AALA984074), Mar 16, 1998: BEAM. CORRODED. AFW - MAINTENANCE FOUND AND BLENDED OUT AN AREA OF CORROSION ON THE UPPER SURFACE OF THE INBOARD FLANGE OF THE OUTER CHORD AT STATION 1307. EN SURE THE BLENDOUT
- [SDR AALA951044](https://openairdocs.org/sdr/AALA951044), Jun 5, 1995: SKIN. CORRODED. AFW - FUSELAGE SKIN FOUND CORRODED. REFINISH BLENDED AREA. FABRICATE AND INSTALL DOUBLER .071 THICK PER 767 SRM 53-00-01 FIGURE 201. APPLY CORROSION INHIBITING 
- [SDR AALA951042](https://openairdocs.org/sdr/AALA951042), Jun 5, 1995: SKIN. CORRODED. AFW - FUSELAGE SKIN UNDER ANTENNA HAS CORROSION BEYOND SRM LIMITS AFTER BLENDOUT. REFINISH BLENDED AREA PER 767 SRM 53-00-01 FIG 101 AND ENGINEERING MRB 767-238
- [SDR AALA951041](https://openairdocs.org/sdr/AALA951041), Jun 5, 1995: STRINGER. CORRODED. AFW - STRINGER CORRODED UNDER PRODUCTION SPLICE. FABRICATE A NEW SPLICE 3.25 INCHES LONGER. INSTALLED AND FINISH WITH FAY SURFACE SEALANT PER 767 SRM AND ENGINE
- [SDR AALA951040](https://openairdocs.org/sdr/AALA951040), Jun 5, 1995: FRAME. CORRODED. AFW - FRAME WEB CORRODED BEYOND SRM LIMITS AFTER BLEND-OUT. FABRICATE DOUBLER 0.040 INCH THICK FROM 7075-T6 AND INSTALL WET WITH BMS 5-25 SEALANT PER B767 SRM A
- [SDR AALA951039](https://openairdocs.org/sdr/AALA951039), Jun 5, 1995: FLOOR BEAM. CORRODED. AFW - FLOOR BEAM CORRODED BEYOND LIMITS SRM AFTER BLEND-OUT. INSTALL ANGLE 0.10 INCH THICK 7075-T6 EXTRUSION WET WITH BMS 5-95 FAY SURFACE SEALANT PER B767 SRM 
- [SDR AALA951038](https://openairdocs.org/sdr/AALA951038), Jun 5, 1995: SKIN. GOUGED. AFW - LEFT OUTBOARD PYLON SKIN BOTTOM EDGE, HAS GOUGE BEYOND SRM LIMITS AFTER BLEND-OUT. REFINISH BLENDED AREA PER B767-SRM. APPROVED FOR CONTINUED SERVICE PER 
- [SDR AALA951037](https://openairdocs.org/sdr/AALA951037), Jun 5, 1995: FLOOR BEAM. CORRODED. AFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS AFTER BLEND OUT. REFINISH BEAM PER B767-SRM. BEAM IS SATISFACTORY FOR CONTINUED SERVICE PER ENGINEERING MRB 767
- [SDR AALA951036](https://openairdocs.org/sdr/AALA951036), Jun 5, 1995: SKIN. CORRODED. AFW - TEAR STRAP ON FUSELAGE SKIN CORROSION OUT OF LIMITS AFTER BLEND-OUT. INSTALL A TAPERED SHIM WET WITH SEALANT AND CORROSION INHIBITING COMPOUND PER B767 SR
- [SDR AALA951046](https://openairdocs.org/sdr/AALA951046), Jun 2, 1995: STRINGER. CORRODED. AFW - STRINGERS ARE CORRODED UNDER THE PRODUCTION SPLICE JUST AFT OF FRAME 1307. REMOVED EXISTING SPLICE. FABRICATE NEW SPLICE 5 INCHES LONGER. REFINISH AND INS
- [SDR AALA951045](https://openairdocs.org/sdr/AALA951045), Jun 2, 1995: SKIN. CORRODED. AFW - FUSELAGE SKIN HAS CORROSION. BLEND AND REFINISH PER 767 SRM 53-00-01 FIG 101. BLEND-OUTS ARE SATISFACTORY PER ENGINEERING MRB-933. (M)
- [SDR AALA951035](https://openairdocs.org/sdr/AALA951035), Jun 2, 1995: SKIN. CORRODED. AFW - FUSELAGE CABIN WING BOX SKIN (UPPER) HAS CORROSION, REMOVED AT STATION 955 LBBL 30, 20, AND 74.81. REPAIRED CORROSION AT STATION 955, LBL 74.81 BY INSTALL

## 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 19930820035349I](https://openairdocs.org/incident/19930820035349I), Aug 20, 1993: Boeing 767223 (N304AA), Seattle, WA. Hydraulic quantity light on in flight. Returned. Found leak in hose assembly in tail section of aircraft.
- [Incident 19880115003719I](https://openairdocs.org/incident/19880115003719I), Jan 15, 1988: Boeing 767223 (N304AA), San Antonio, TX. No indication that nose landing gear down. Landed safely. Found landing gear light module was loose.

## Other aircraft with N304AA

- [Registered now](https://openairdocs.org/aircraft/N304AA): Textron Systems Unmanned Systs AEROSONDE MK 4.8, S/N X3004

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