# N67158: 2001 Boeing 767-224, registration cancelled 2012-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2012 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Boeing 767-224](https://openairdocs.org/model/boeing-767-224) (registry code 1385170) - 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: 30437 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 29, 2001 - Certificate issued: June 14, 2012 - Last registry action: June 14, 2012 - Mode S code: A8E297 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N67158 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=67158 - Page: https://openairdocs.org/deregistered/N67158-2012-08-23 From the FAA registry file of November 5, 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 767-224: https://openairdocs.org/model/boeing-767-224.md ## Service difficulty reports (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UALA2012F00145](https://openairdocs.org/sdr/UALA2012F00145), Aug 1, 2012: SKIN. DAMAGED. FUSELAGE SKIN REPAIR PERFORMED IAW REO-G15199, REV A, AT FUSELAGE BS 368, AT STRINGER 31 LEFT. - [SDR 2012FA0000521](https://openairdocs.org/sdr/2012FA0000521), Aug 1, 2012: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 1714 BETWEEN STRINGER 36 AND 37 RT. PERFORMED REPAIR IAW REO-G15177 REVB. REPAIR IS A CATEGORY A REPAIR AS DEFINED IN SRM 51-00-06. - [SDR 2012FA0000518](https://openairdocs.org/sdr/2012FA0000518), Jul 30, 2012: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 1898.45 ON UPPER LEFT SURFACE. REPAIRED IAW SRM 53-00-01 FIG 201. - [SDR 2012FA0000498](https://openairdocs.org/sdr/2012FA0000498), Jul 20, 2012: SKIN. MISREPAIRED. SKIN AT BS 325 AT STRINGER 31 LT, MISREPAIRED. REPAIRED SKIN IAW SRM 53-00-01, FIG 201. - [SDR 2012FA0000493](https://openairdocs.org/sdr/2012FA0000493), Jul 20, 2012: SKIN. MISREPAIRED. DURING REPAIR ASSESSMENT IT WAS DETERMINED THAT SKIN AT BS 1793 BETWEEN STRINGERS 34 AND 35 LT WAS MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201. - [SDR CALA2011052700396](https://openairdocs.org/sdr/CALA2011052700396), May 26, 2011: SPRING. WRONG PART. SUPPORT TASK CABIN - R1 DOOR SLIDE DEPLOYMENT BAR AFTER POSITION SEPARATION LINK ATTACH SPRING FOUND INCORRECT PARTS. CABIN R1 DOOR SLIDE DEPLOYMENT BAR AFTER P - [SDR CALA2011051700369](https://openairdocs.org/sdr/CALA2011051700369), May 16, 2011: SEAT TRACK. CRACKED. 767-53-3-0164U CABIN - RT STA 412 RBL 20 SEAT TRACK FLANGE FOUND CRACKED. CABIN RT STA 344 TO STA 412 RBL 20 SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALL - [SDR CALA2011051600366](https://openairdocs.org/sdr/CALA2011051600366), May 15, 2011: FLOORBEAM. CORRODED. BS 325 LBL 26 TO 55 FLOORBEAM CORRODED. REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201. HFEC NO CRACK FOUND. - [SDR CALA2009080400414](https://openairdocs.org/sdr/CALA2009080400414), Aug 4, 2009: LIGHT. INOPERATIVE. L2 DOOR THRESHOLD EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT, OPS CHECKS GOOD. - [SDR CALA2009080400413](https://openairdocs.org/sdr/CALA2009080400413), Aug 4, 2009: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT FWD OF CARGO DOOR IS INOPERATIVE. RELAMPED LIGHT, OPS CHECKS GOOD. - [SDR CALA2009051400250](https://openairdocs.org/sdr/CALA2009051400250), May 7, 2009: LIGHT. INOPERATIVE. LEFT WING SLIDE GROUND ILLUMINATION LIGHT INOP, EXTERIOR EMERGENCY LIGHT AT STATION 1230. REPLACED EMERGENCY LIGHT ASSY, OP CHECKED GOOD PER MM 33-51-06. - [SDR CALA2008112401097](https://openairdocs.org/sdr/CALA2008112401097), Nov 23, 2008: SKIN. GOUGED. LIGHTNING STRIKE DAMAGE AT 4 LOCATIONS SEE L/P 8072815 STA 111, 129, 412 STA 111 S-30 DMG DIAM 0.184 IN RIVET HEAD DMG 0.066 IN. STA 129 S-30 DMG DIAM 0.170 IN - [SDR CALA2008112401096](https://openairdocs.org/sdr/CALA2008112401096), Nov 23, 2008: SKIN. GOUGED. FOUND FASTENER AT STA 368 AROUND S-30 DAMAGED BY LIGHTNING STRIKE. TOTAL DAMAGE 0,250 IN RIVET HEAD DAMAGE 0,091 IN. PER SRM 53-00-01 P103 TABLE III DETAIL IV N - [SDR CALA2008112401095](https://openairdocs.org/sdr/CALA2008112401095), Nov 23, 2008: SUPPORT. CORRODED. CABIN - BS 325 LBL 27- LBL 60 FLOOR SUPPORT FOUND CORRODED. CABIN BS 325 LBL 16- LBL 62 FLOORBEAM SUPPORT REPAIRED PER SRM 53-00-51 REPAIR 1, FIG 201. HFEC NO C - [SDR CALA2008112401089](https://openairdocs.org/sdr/CALA2008112401089), Nov 21, 2008: FLOORBEAM. CORRODED. CABIN - BS 303 LBL 26-44 FLOOR SUPPORT FOUND CORRODED. CABIN - BS 303 LBL 7 TO LBL 62 FLOOR SUPPORT BEAM UPPER FLANGE REPAIRED PER SRM 33-00-51 REPAIR 1, FIG 20 - [SDR CALA0600286](https://openairdocs.org/sdr/CALA0600286), Jul 31, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 30-60. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1. - [SDR CALA0600284](https://openairdocs.org/sdr/CALA0600284), Jul 31, 2006: STIFFENER. CRACKED. INSPECTION FOUND NR 2 PYLON I/B CLIP, FRAME, AND STIFFENER CRACKED AT STA 275. THE CLIP, FRAME, AND STIFFENER WERE REPLACED IAW SRM 51-10-02. - [SDR CALA0600285](https://openairdocs.org/sdr/CALA0600285), Jul 21, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 25-60. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1. - [SDR CALA0600262](https://openairdocs.org/sdr/CALA0600262), Jul 20, 2006: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 32. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02 AND 51-40-02. - [SDR CALA0600283](https://openairdocs.org/sdr/CALA0600283), Jul 6, 2006: SKIN. CRACKED. INSPECTION FOUND NR 2 PYLON I/B MID-SPAR AREA ONE EACH FASTENER HOLE HAD A 0.06" CRACK IN SKIN AT STA 285. THE SKIN WAS REPAIRED IAW ECRA 5430-01784. - [SDR CALA050110](https://openairdocs.org/sdr/CALA050110), Apr 18, 2005: ENGINE. FAILED. ON TAKEOFF, AT APPROXIMATELY 90 KNOTS, RT ENGINE FAILED. REPLACED ENGINE. ## Other aircraft with N67158 - [Cancelled 1977-07-14](https://openairdocs.org/deregistered/N67158-1977-07-14): Sikorsky S-55B, S/N 551202. Owner: [Aircraft Specialties Inc](https://openairdocs.org/faa-owner/AIRCRAFT%20SPECIALTIES%20INC), [Mesa, AZ](https://openairdocs.org/faa-place/AZ/Mesa) --- 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.