# N315AA: 1985 Boeing 767-223, registration cancelled 2016-03-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 8, 2016
- Exported to: Malaysia
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-223](https://openairdocs.org/model/boeing-767-223) (registry code 1385123)
- Engine: [GE CF6-80A](https://openairdocs.org/engine/ge-cf6-80a) (registry code 30093)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 22317
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 29, 2010
- Certificate issued: January 13, 2010
- Last registry action: January 12, 2016
- Mode S code: A35965
- Owner when cancelled: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC)
- Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N315AA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=315AA
- Page: https://openairdocs.org/deregistered/N315AA-2016-03-08

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 (112, newest 50)

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

- [SDR ABXA20151014189](https://openairdocs.org/sdr/ABXA20151014189), Oct 14, 2015: SKIN. CORRODED. CORROSION ON LT FUSELAGE SKIN, STATION 955 C/T FAILSAFE TRIM OUT AREA GOING FWD UNDER FAILSAFE STRAP. FAIL SAFE REMOVED ON EA 53500013-008. REMOVED ALL CORROSIO
- [SDR ABXA20151013173](https://openairdocs.org/sdr/ABXA20151013173), Oct 13, 2015: SKIN. CORRODED. RIGHT STATION 18.09 PREVIOUS REPAIR DOUBLER, BETWEEN STRINGERS 9RT & 10RT. REQUEST ENGINEERING INSTRUCTIONS. REMOVED DOUBLER, CLEANED HOLES TO LEVEL 3, PERFORME
- [SDR ABXA20151012175](https://openairdocs.org/sdr/ABXA20151012175), Oct 12, 2015: FRAME. CRACKED. RIGHT FRAME INNER CHORD AT STATION 883.5, RBL 89 HAS A .250 CRACK IN TRANSITION RADIUS. REPAIRED CHORD IAW EA 53000050-101. CRACKED .50, PN 691T0003-44, PART NA
- [SDR ABXA20151007190](https://openairdocs.org/sdr/ABXA20151007190), Oct 7, 2015: TEE FITTING. CORRODED. UPON CURSORY INSPECTION, FOUND CORROSION WITHIN AREA UNDER THIRD INBD HEAT SHIELD PANEL AT LOWER AFT PYLON AREA, APPROX NAC STATION 400. R & R CORRODED T FITTIN
- [SDR ABXA20151003188](https://openairdocs.org/sdr/ABXA20151003188), Oct 3, 2015: FAILSAFE. CRACKED. LEFT STATION 955, FAIL SAFE STRAP HAS .125 CRACK APPROX 2:00 POSITION AT THE BOTTOM FASTENER HOLE. LT FAIL SAFE STRAP IS BEING REPLACED. NEW FAIL SAFE STRAP PN 
- [SDR ABXA20151002165](https://openairdocs.org/sdr/ABXA20151002165), Oct 2, 2015: STIFFENER. CORRODED. LEFT WW AFT SPAR BULKHEAD FS 955, LBL 9, INBD VERTICAL ANGLE HAS TOOLING MARKS ON INBD SIDE IN NUMEROUS PLACES. BLENDED TOOLING MARKS ON REAR SPAR STIFFENER IAW
- [SDR ABXA20151001170](https://openairdocs.org/sdr/ABXA20151001170), Oct 1, 2015: LONGERON. CORRODED. CORROSION ON UPPER SIDE OF OVERWING LONGERON IN UPPER FWD OTBD CORNER OF RT WW, AROUND FASTENERS & ON FASTENER HEADS FROM FS 975 - 985. REMOVED CORROSION ORIGIN
- [SDR ABXA20151001169](https://openairdocs.org/sdr/ABXA20151001169), Oct 1, 2015: LONGERON. CORRODED. CORROSION ON UPPER SIDE OF OVERWING LONGERON IN UPPER FWD OTBD CORNER OF RT WW FROM FS 965 - 975. REMOVED CORROSION ORIGINAL .080, REMOVED .012, REMAINING .068 
- [SDR ABXA20150930186](https://openairdocs.org/sdr/ABXA20150930186), Sep 30, 2015: SKIN. CORRODED. FOUND CORROSION AT APPROX WS 110 RT WING TE FLANGE. REMOVED CORROSION AT UPPER RT WING TE WBL110, PN 112T3101-6 IAW REA B657-61760-MR. SDR INFO, CORRODED LEVEL 
- [SDR ABXA20150929168](https://openairdocs.org/sdr/ABXA20150929168), Sep 29, 2015: LONGERON. CORRODED. LEFT WW FS APPROX 980 OVERWING LONGERON TOP SIDE HAS CORRODED FASTENERS & POSSIBLY AROUND BASE OF FASTENERS. REMOVED CORROSION, ORIGINAL MATERIAL .080, REMOVED 
- [SDR ABXA20150928187](https://openairdocs.org/sdr/ABXA20150928187), Sep 28, 2015: FAILSAFE. CRACKED. FOUND CRACK AT LOWER OF 3 FASTENER HOLES INSPECTED. CRACK PLAINLY VISIBLE. REPAIRED AREA IAW DOCUMENT 470080RD06 & EA 53500014-003. SDR, CRACKED, LENGTH : 1.7 I
- [SDR ABXA20150924191](https://openairdocs.org/sdr/ABXA20150924191), Sep 21, 2015: ANGLE. CORRODED. UPON CURSORY INSPECTION FOUND CORROSION WITHIN AREA UNDER FWD HEAT SHIELD PANEL AT LOWER AFT PYLON AREA, JUST ABOVE AFT EDGE OF EXHAUST NOZZLE, APPROX NAC STATI
- [SDR ABXA20150918171](https://openairdocs.org/sdr/ABXA20150918171), Sep 18, 2015: SPAR. CORRODED. CORROSION UNDER NUTPLATE ON UPPER CHORD OF WING REAR SPAR TO TE BEAM AT WING STATION 434, OTBD SIDE AS SEEN THRU PANEL 561AB. R & R UPPER CHORD OF WING REAR SPA
- [SDR ABXA20150914185](https://openairdocs.org/sdr/ABXA20150914185), Sep 14, 2015: SUPPORT FITTING. CORRODED. FLAP SUPPORT NR 1, TENSION BOLT HOLE NR 1 HAS A DEFECT INDICATION, REFERENCE JC EA5750006-001. REAMED HOLE TO .672, NO FURTHER DEFECTS NOTED, REFERENCE REA B657
- [SDR ABXA20150914184](https://openairdocs.org/sdr/ABXA20150914184), Sep 14, 2015: SUPPORT FITTING. CORRODED. FLAP SUPPORT NR 2, TENSION BOLT HOLE NR 3 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED FASTENER HOLE TO .8285, NO DEFECTS NOTED REFERENCE REA B65
- [SDR ABXA20150914183](https://openairdocs.org/sdr/ABXA20150914183), Sep 14, 2015: SUPPORT FITTING. CORRODED. FLAP SUPPORT NR 2, TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED HOLE TO .829, NO DEFECTS NOTED REFERENCE REA B657-61708-MR
- [SDR ABXA20150914182](https://openairdocs.org/sdr/ABXA20150914182), Sep 14, 2015: SUPPORT FITTING. CORRODED. FLAP SUPPORT NR 2, TENSION BOLT HOLE NR 1 HAS DEFECT INDICATION, REFERENCE JC EA57500018-001. REAMED FASTENER HOLE TO .8285, NO FURTHER DEFECTS, REFERENCE REA B
- [SDR ABXA20150914181](https://openairdocs.org/sdr/ABXA20150914181), Sep 14, 2015: SUPPORT FITTING. CORRODED. FLAP SUPPORT NR 7, TENSION BOLT HOLE NR 4 HAS DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708
- [SDR ABXA20150914180](https://openairdocs.org/sdr/ABXA20150914180), Sep 14, 2015: SUPPORT FITTING. CORRODED. FLAP SUPPORT NR 7 TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-6170
- [SDR ABXA20150914179](https://openairdocs.org/sdr/ABXA20150914179), Sep 14, 2015: SUPPORT FITTING. CORRODED. FLAP SUPPORT NR 7 TENSION BOLT HOLE 1 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-M
- [SDR ABXA20150914178](https://openairdocs.org/sdr/ABXA20150914178), Sep 14, 2015: SUPPORT FITTING. CORRODED. FLAP SUPPORT 8 TENSION BOLT HOLE 4 HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .875, NO DEFECTS NOTED IAW REA B657-61708-MR REV 
- [SDR ABXA20150914177](https://openairdocs.org/sdr/ABXA20150914177), Sep 14, 2015: SUPPORT FITTING. CORRODED. NUMBER 8 FLAP SUPPORT TENSION BOLT HOLE 3 HAS A DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .672, NO DEFECTS NOTED IAW REA B657-6107
- [SDR ABXA20150914176](https://openairdocs.org/sdr/ABXA20150914176), Sep 14, 2015: SUPPORT FITTING. CORRODED. NUMBER 8 FLAP SUPPORT TENSION BOLT HOLE NR 1, HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .672, NO DEFECTS NOTED IAW REA B657-61
- [SDR ABXA20150910172](https://openairdocs.org/sdr/ABXA20150910172), Sep 10, 2015: BEAM. CRACKED. NUMBER 2 STRUT INSIDE PANEL 447BR, LOWER BEAM IS CHAFED & CRACKED AT THIRD HOLE FROM THE FWD END. R & R LOWER BEAM INSIDE NR 2 PYLON PANEL 447BR IAW SRM 54-51-7
- [SDR ABXA20140915293](https://openairdocs.org/sdr/ABXA20140915293), Sep 15, 2014: INVERTER. DAMAGED. CREW REPORTED EICAS MESSAGE STBY INVERTER DISPLAYED, SMOKE IN THE CABIN & A STRONG ELEC BURNING ODOR. THE FLIGHT WAS DIVERTED TO NEAREST SUITABLE AIRPORT. THE S
- [SDR ABXA20140910291](https://openairdocs.org/sdr/ABXA20140910291), Sep 10, 2014: ENGINE. BIRD INGESTION. ON ROTATION, BIRD STRIKE TO THE LT ENG. CREW HEARD LOUD NOISE & FELT AIRFRAME VIBRATION. LT ENG VIBRATION INDICATED OVER 4.5 & LT THRUST LEVER BEGAN REDUCING TO
- [SDR ABXA20131213659](https://openairdocs.org/sdr/ABXA20131213659), Dec 11, 2013: POWER SUPPLY. SHORTED. DURING EXTENDED GROUND TAXI, LT FLIGHT MANAGEMENT COMPUTER FAILED MESSAGE DISPLAYED, FOLLOWED BY SMOKE FROM THE LT CDU & THE LT CDU CIRCUIT BREAKER TRIPPED OPEN
- [SDR ABXA20131106643](https://openairdocs.org/sdr/ABXA20131106643), Nov 6, 2013: RIB. CRACKED. LEFT WING MAIN TRACK RIB AT OSS 1094 IS CRACKED WHERE TRACK BEARING ATTACHES. REMOVED DAMAGE IAW BCSF 767-200 57-41-09 FIG 101 & COMPLIED WITH RGA NR B657 - 607
- [SDR ABXA20131106634](https://openairdocs.org/sdr/ABXA20131106634), Nov 6, 2013: FAIRING. CRACKED. VERTICAL STABILIZER AFT AT BASE UNDER 324AL METAL CHAFED & KNIFE EDGED. SRM 51-40-02 APPLIED TOP COAT IAW BOE 767 SRM 51-20-00. CRACKED CHAFED 4 INCHES, LOC FRO
- [SDR ABXA20131105644](https://openairdocs.org/sdr/ABXA20131105644), Nov 5, 2013: RIB. CRACKED. LEFT WING MAIN TRACK RIB AT OSS 1097 IS CRACKED WHERE THE TRACK BEARING ATTACHES. R & R IAW B767-200 SR SRM 51-40-02, REPAIRED 21E1 IAW REA NR B657-60774 MR. PN
- [SDR ABXA20131105635](https://openairdocs.org/sdr/ABXA20131105635), Nov 5, 2013: STRINGER CLIP. CRACKED. CLIP ON STRINGER 2 RT AT STATION 1678 CRACKED. R & R CLIP IAW DRAWING 148T1121 & SRM 51-20- 02. PN 148T1303-1 SN NA CRACKED 1/4 INCH, PN CLIP FS & BS LOCATION 1
- [SDR ABXA20131104641](https://openairdocs.org/sdr/ABXA20131104641), Nov 4, 2013: INTERCOSTAL. CORRODED. FORWARD LOWER CARGO FUSELAGE STATION 549 RBL 6 THE STRUCTURE FOR THE LATERAL GUIDE NUTPLATES IS CORRODED. R & R 452T2704-1 INTERCOSTAL IAW DRAWING 451T2501 & SR
- [SDR ABXA20131104627](https://openairdocs.org/sdr/ABXA20131104627), Nov 4, 2013: STRUCTURE. CORRODED. FORWARD LOWER CARGO FUSELAGE STATION 412 LBL 46 LOWER SIDE OF UPPER CHORD, BELOW CARGO FLOOR, IS SPLIT WITH INTERNAL CORROSION AT NUTPLATE LOCATION. REMOVED PDU
- [SDR ABXA20131102642](https://openairdocs.org/sdr/ABXA20131102642), Nov 2, 2013: PLATE. CRACKED. UPPER CARGO FLOOR PANEL MOUNTING PLATE UNDER CARGO LOCK MOUNT IS CRACKED FS 1021 LBL 45. R & R MATCH DRILLED TO FLOOR PANEL, FLOOR PANEL MOUNTING PATE AT FS 102
- [SDR ABXA20131101632](https://openairdocs.org/sdr/ABXA20131101632), Nov 1, 2013: KEELBEAM. CORRODED. CORROSION ON FLAT PANEL IN WW AT STATION 973 LBL 6 & ON ANGLE AT STATION 977 LBL 6. REMOVED CORROSION IAW B767-200 SRM 53-50-12. COMPLIED WITH REA NR B653-60754
- [SDR ABXA20131101629](https://openairdocs.org/sdr/ABXA20131101629), Nov 1, 2013: FRAME. CORRODED. FORWARD LOWER CARGO FUSELAGE STATION 478 AFT SIDE OF CHORD AT LBL 20 UNDERSIDE OF CHORD IS CORRODED AT NUTPLATE. REMOVED OLD CORD DRILLED NEW ONE IAW BOE 767 SR
- [SDR ABXA20131101628](https://openairdocs.org/sdr/ABXA20131101628), Nov 1, 2013: FRAME. CORRODED. FORWARD LOWER CARGO FUSELAGE STATION 478 AFT SIDE OF CHORD AT LBL 38 UNDERSIDE OF CHORD IS CORRODED AT NUTPLATE. R & R CORD ON NR 0259. NEW CORD WAS DRILLED IAW
- [SDR ABXA20131031638](https://openairdocs.org/sdr/ABXA20131031638), Oct 31, 2013: SHEAR TIE. CORRODED. AREA BEHIND FWD LOWER CARGO AT FUSELAGE STATION 742 STRINGER 38L - STRINGER 39L SHEAR TIE CORRODED. INSTALLED SHEER TIE IN FWD LOWER CARGO AT STATION 742 BETWEE
- [SDR ABXA20131031636](https://openairdocs.org/sdr/ABXA20131031636), Oct 31, 2013: SHEAR TIE. CORRODED. BEHIND FWD LOWER CARGO AFT SIDE OF FUSELAGE STATION 742 SHEAR TIE CORRODED BETWEEN STRINGER 35L - STRINGER 36L. INSTALLED NEW SHEET TIE IN FWD LOWER CARGO AT ST
- [SDR ABXA20131030631](https://openairdocs.org/sdr/ABXA20131030631), Oct 30, 2013: FLOORBEAM. CORRODED. FORWARD LOWER CARGO FUSELAGE STATION 720 LBL 41 UPPER & LOWER CHORD IS CORRODED & SEPARATING INCLUDING 3 INCHES OTBD ON LOWER SIDE. REPLACED T CHORD. LOCATED, D
- [SDR ABXA20131030630](https://openairdocs.org/sdr/ABXA20131030630), Oct 30, 2013: INTERCOSTAL. CORRODED. FORWARD LOWER CARGO FUSELAGE STATION 580 LBL 13 ON LOWER SIDE OF INTERCOSTAL CORRODED. REPLACED & INSTALLED NEW INTERCOSTAL AT STATION S80 LBL 13 IAW B767 SRM 5
- [SDR ABXA20131029640](https://openairdocs.org/sdr/ABXA20131029640), Oct 29, 2013: PANEL. CORRODED. FORWARD LOWER CARGO FUSELAGE STATION 630 BILGE PANEL COVER CORRODED ON TOP AT LBL PO 0039309. LEVEL 2 CORROSION PN 143T5000-122, PN BILGE PANEL, SN NA. LOCATION
- [SDR ABXA20131029637](https://openairdocs.org/sdr/ABXA20131029637), Oct 29, 2013: SHEAR TIE. CORRODED. BEHIND FWD LOWER CARGO AFT SIDE OF FUSELAGE STATION 742 SHEAR TIE CORRODED BETWEEN STRINGER 38R - STRINGER 39R. R & R SHEAR TIE AT STATION 742 BETWEEN G38R & 39
- [SDR ABXA20131029633](https://openairdocs.org/sdr/ABXA20131029633), Oct 29, 2013: KEELBEAM. CORRODED. LEFT HAND KEEL CHORD UPPER FLANGE HAS CORROSION AT STATION 985 - 995 LBL 10.75. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-6
- [SDR ABXA20131029626](https://openairdocs.org/sdr/ABXA20131029626), Oct 29, 2013: KEELBEAM. CORRODED. CORROSION ON KEEL BEAM UPPER & LOWER SURFACE ADJACENT TO NUTPLATE AT STATION 801 LBL 9. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA N
- [SDR ABXA20131029625](https://openairdocs.org/sdr/ABXA20131029625), Oct 29, 2013: KEELBEAM. CORRODED. SPOT OF CORROSION ON KEEL BEAM UPPER SURFACE AT STATION 814 RBL 9 ADJACENT TO NUTPLATE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101. COMPLIED WITH REA N
- [SDR ABXA20131029624](https://openairdocs.org/sdr/ABXA20131029624), Oct 29, 2013: KEELBEAM. CORRODED. CORROSION ON KEEL BEAM AT STATION 827 LBL 11. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5,
- [SDR ABXA20131029623](https://openairdocs.org/sdr/ABXA20131029623), Oct 29, 2013: KEELBEAM. CORRODED. CORROSION ON KEEL BEAM AT STATION 955 LBL 12. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, PN 145T8611-5,
- [SDR ABXA20131029622](https://openairdocs.org/sdr/ABXA20131029622), Oct 29, 2013: KEELBEAM. CORRODED. CORROSION ON KEEL BEAM AT STATION 951 RBL 12 LOWER SURFACE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, 
- [SDR ABXA20131029621](https://openairdocs.org/sdr/ABXA20131029621), Oct 29, 2013: KEELBEAM. CORRODED. CORROSION ON KEEL BEAM AT STATION 808 RBL 10 LOWER SURFACE. REMOVED CORROSION IAW B767-200 SRM 53-50-12 FIG 101, COMPLIED WITH REA NR B653-60753-MR. CORROSION, 

All 112: https://openairdocs.org/deregistered/N315AA-2016-03-08/reports.md

## FAA accident and incident reports (1)

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 19911026057939I](https://openairdocs.org/incident/19911026057939I), Oct 26, 1991: Boeing 767223 (N315AA), London, UK, Minor damage. Left wing leading edge flap slat assymetric after takeoff. Diverted for maintenance.

## Other aircraft with N315AA

- [Registered now](https://openairdocs.org/aircraft/N315AA): Ceres Air C31, S/N 21578540702C1

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