# N256AY: 1993 Boeing 767-2B7, registration cancelled 2022-02-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 5, 2022
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 767-2B7](https://openairdocs.org/model/boeing-767-2b7) (registry code 1385107)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 26847
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 1, 1993
- Certificate issued: October 21, 2015
- Last registry action: May 11, 2018
- Mode S code: A26DDF
- Owner when cancelled: [Kmw Leasing Xii 6-767 LLC](https://openairdocs.org/faa-owner/KMW%20LEASING%20XII%206-767%20LLC)
- Location: [Holladay, UT](https://openairdocs.org/faa-place/UT/Holladay)
- Owner type: LLC
- Owner's area on the map: 40.6617° N, 111.8356° W: Placed by OpenAirDocs at the center of ZIP code 84117, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N256AY
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=256AY
- Page: https://openairdocs.org/deregistered/N256AY-2022-02-05

From the FAA registry file of October 31, 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 767-2B7: https://openairdocs.org/model/boeing-767-2b7.md

## Service difficulty reports (121, newest 50)

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

- [SDR USAA2014122400005](https://openairdocs.org/sdr/USAA2014122400005), Dec 22, 2014: PUMP. LEAKING. ENROUTE, RT ENGINE OIL PRESSURE DROPPED TO 13 PSI, WITH OIL QTY LOSS. SHUTDOWN THE RT ENGINE. LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NR 2 ENGINE LUBE PUM
- [SDR USAA2014062300013](https://openairdocs.org/sdr/USAA2014062300013), Jun 21, 2014: HANDLE. LOOSE. FWD ENTRY DOOR WOULD NOT ARM & DIFFICULT TO CLOSE. MX FOUND L1 DOOR ARMING HANDLE LOOSE. SECURED HANDLE. PERFORMED SATISFACTORY OPERATIONAL TEST OF L1 DOOR OPEN
- [SDR USAA2014042100004](https://openairdocs.org/sdr/USAA2014042100004), Apr 17, 2014: POWER SUPPLY. INOPERATIVE. CLT L1 & L2 DOOR EXIT & THRESHOLD LIGHTS WOULD NOT TEST. REPLACED M1208 POWER SUPPLY.
- [SDR USAA2013122700003](https://openairdocs.org/sdr/USAA2013122700003), Dec 26, 2013: CONTROL PANEL. FAULTY. FLT 751 ENROUTE, RECEIVED FWD EQ OVERHEAT MESSAGE FOLLOWED BY UNCONTROLLABLE CABIN AIR PRESSURE. DECLARED AN EMERGENCY & PERFORMED A RAPID DESCENT TO 10,000 FT.
- [SDR USAA2013121200001](https://openairdocs.org/sdr/USAA2013121200001), Dec 12, 2013: SLIDE. UNSECURE. C1 CHECK, RT OFF WING ESCAPE SLIDE ASSEMBLY UNLACED, SLIDE NOT SECURED. REPLACED RT ESCAPE SLIDE ASSEMBLY & INSTALLED IAW B767 AMM 25-65-05-424-056.
- [SDR USAA2013112200005](https://openairdocs.org/sdr/USAA2013112200005), Nov 18, 2013: AILERON. DELAMINATED. C1 CHECK DELAMINATION ON RT AILERON AT APPROXIMATELY 75 INCHES OTBD OF INBD END & 13.5 INCHES FWD OF AFT TE. REPLACED RT AILERON IAW JOB CARD 12L56027004.
- [SDR USAA2013111400009](https://openairdocs.org/sdr/USAA2013111400009), Nov 13, 2013: SKIN. DELAMINATED. DURING C1 CHECK, DELAMINATION WAS FOUND ON RT OTBD AFT FLAP APPROX 85 INCHES OTBD FROM INBD END LOWER SURFACE & 13.5 INCHES FORWARD OF T/E. REPAIRED RT AFT FLAP
- [SDR USAA2013111400008](https://openairdocs.org/sdr/USAA2013111400008), Nov 10, 2013: SKIN. DELAMINATED. DURING C1 CHECK, DELAMINATION FOUND ON RT AFT FLAP APPROX 14 INCHES FROM INBD END & 12 INCHES FROM T/E. REPAIRED RT AFT FLAP IAW SRM 51-70-10.
- [SDR USAA2013110800007](https://openairdocs.org/sdr/USAA2013110800007), Nov 6, 2013: STIFFENER. CRACKED. DURING C1 CHECK, CRACK FOUND IN VERTICAL STIFFNER OF NOSE WHEEL WELL AT BS 287, WL 172, LBL 25. REPAIRED VERTICAL STIFFENER OF NOSE WHEEL WELL AT BS287, WL172, 
- [SDR USAA2013091600008](https://openairdocs.org/sdr/USAA2013091600008), Sep 15, 2013: SIGN. UNSECURE. EXIT SIGN OVER F/A J/S AT 2L DOOR IS OFF. R & R 2L EXIT SIGN.
- [SDR USAA2013091600006](https://openairdocs.org/sdr/USAA2013091600006), Sep 14, 2013: COVER. UNSECURE. EXIT SIGN COVER 2L JUMPSEAT FELL OUT. COVER REINSTALLED; OPC SATISF.
- [SDR USAA2013090900001](https://openairdocs.org/sdr/USAA2013090900001), Sep 7, 2013: CABLE. SHORTED. ENROUTE, ACFT RT AFT GALLEY A-302, CIRCUIT BREAKER TRIPPED. TRIED ONE RESET, STARTED SMOKING. PULLED CIRCUIT BREAKER AND UNPLUGGED CART. R & R AFT GALLEY CART C
- [SDR USAA2013072300001](https://openairdocs.org/sdr/USAA2013072300001), Jul 21, 2013: COVER. DISLODGED. EXIT SIGN OVERWING EXIT ACFT LT COVER FELL OFF DURING TAKEOFF ROLL STRIKING PASSENGER IN SEAT 12A. MX SECURED EXIT SIGN OVERWING AS REQUIRED.
- [SDR USAA2013070300003](https://openairdocs.org/sdr/USAA2013070300003), Jul 1, 2013: SERVICE CART. FAULTY. EN-ROUTE, THE GALLEY FOOD HEATING UNIT IN THE AFT GALLEY MELTED THE PLASTIC FOOD TRAYS AND EMITTED AN ODOR. THEY WERE NEW FOOD TRAYS. MX EXCHANGED ALL HEATING U
- [SDR USAA2013050600002](https://openairdocs.org/sdr/USAA2013050600002), May 4, 2013: BATTERY. DISCHARGED. PHL - FLASHLIGHT AT FWD F/A STATION BATTERY DEAD. REPLACED BATTERY.
- [SDR USAA2013042300002](https://openairdocs.org/sdr/USAA2013042300002), Apr 21, 2013: SIGN. MISSING. PHL - EXIT SIGN IN CEILING A/C RT AFT OF 1ST CLASS MISSING. RE-SECURED SIGN.
- [SDR USAA2013031900002](https://openairdocs.org/sdr/USAA2013031900002), Mar 16, 2013: CHECK VALVE. FAILED. FLT 1628 ENROUTE, NR 2 ENGINE FLAMED OUT DURING REVERSE SELECTION ON LANDING. THE FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REPLACED THE NR 2 ENGIN
- [SDR USAA2013030600010](https://openairdocs.org/sdr/USAA2013030600010), Mar 6, 2013: SLIDE RAFT. MALFUNCTIONED. DURING ESCAPE SLIDE/RAFT OPS CHECK, TWO FWD SLIDE/RAFTS FAILED TO INFLATE PROPERLY. SLIDE DID NOT UNFOLD. CENTER WEBBING ATTACH POINT (BELOW GIRT) DID NOT BREAK
- [SDR USAA2013012800001](https://openairdocs.org/sdr/USAA2013012800001), Jan 26, 2013: REHEATER. CONTAMINATED. FLT 9465 TEST FLIGHT. FL 360, IN CRUISE. CABIN AND COCKPIT SMOKE NOTED. CREW DONNED O2 MASKS AND ENDED TEST FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAIN
- [SDR USAA2013012200005](https://openairdocs.org/sdr/USAA2013012200005), Jan 18, 2013: POWER UNIT. BROKEN. C4 CHECK - AFT CRT LEFT FLASHLIGHT POWER UNIT HAS A BROKEN WIRE. REPLACED AFT CRT LEFT FLASHLIGHT POWER UNIT IAW DME CORPORATION CMM 25-60-02.
- [SDR USAA2013012200004](https://openairdocs.org/sdr/USAA2013012200004), Jan 17, 2013: SIGN. BROKEN. C4 CHECK - L2 DOOR LINER EXIT SIGN "L333" HAS BROKEN LIGHT COVER. REPLACED L-2 DOOR LINER EXIT SIGN "L333" & OPS CHECKS GOOD IAW B767 AMM 33-51-022-029 & 33-51-
- [SDR USAA2013011800010](https://openairdocs.org/sdr/USAA2013011800010), Jan 17, 2013: LIGHT. BROKEN. C4 CHECK - WORN & BROKEN FORWARD & AFT GALLEY MAT EMERGENCY PATH LIGHT REQUIRES REPLACEMENT. REPLACED FORWARD & AFT GALLEY MAT EMERGENCY PATH LIGHT IAW DRAWING 
- [SDR USAA2013011600005](https://openairdocs.org/sdr/USAA2013011600005), Jan 14, 2013: LIGHT. CRACKED. C4 CHECK - RIGHT CEILING PANEL 11 EMERGENCY LIGHT ASSY IS BROKEN. REPLACED RIGHT CEILING PANEL 11 EMERGENCY LIGHT ASSY (AISLE LIGHT). OPS CHECK GOOD IAW B767 AM
- [SDR USAA2013011500004](https://openairdocs.org/sdr/USAA2013011500004), Dec 29, 2012: FLAP. DAMAGED. C4 CHECK - FIBER DAMAGE ON RIGHT OUTBOARD FLAP LOWER TRAILING EDGE BETWEEN DTEF265.88 TO DTEF267.88. REPAIRED RIGHT OUTBOARD FLAP LOWER TRAILING EDGE BETWEEN DT
- [SDR USAA2013010300027](https://openairdocs.org/sdr/USAA2013010300027), Dec 27, 2012: FLOORBEAM. CORRODED. C4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT BS 303, LBL 13. REPAIRED FLOORBEAM AT BS 303, LBL 13 IAW B767 SRM 53-00-51-2R-1 FIG 201.
- [SDR USAA2012122800018](https://openairdocs.org/sdr/USAA2012122800018), Dec 20, 2012: FLOORBEAM. CORRODED. C4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT BS 1518, LBL 30. REPAIRED FLOORBEAM AT BS 1518, LBL 30 IAW B767 SRM 53-00-51-2R-1 FIG 201.
- [SDR USAA2013012500014](https://openairdocs.org/sdr/USAA2013012500014), Dec 19, 2012: CHANNEL. CRACKED. C4 CHECK - CRACK ON FLOOR SUPPORT CHANNEL BETWEEN BS 347 & BS 357, RBL 34. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 347 & BS 357, RBL 34 IAW B767 SRM 51-40-02-
- [SDR USAA2013011500005](https://openairdocs.org/sdr/USAA2013011500005), Dec 19, 2012: FLOORBEAM. CORRODED. C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 347, RBL 46.25. REPAIRED FLOORBEAM T-CAP AT BS 347, RBL 46.25 IAW B767 SRM 53-00-51-2R-1, FIG 201.
- [SDR USAA2013012500015](https://openairdocs.org/sdr/USAA2013012500015), Dec 18, 2012: ATTACH FITTING. CRACKED. C4 CHECK - CRACK ON FRAME ATTACH CLIP AT BS 1562, S33L. REPLACED FRAME ATTACH CLIP AT BS 1562, S33L IAW BOEING DRAWING 216T1014.
- [SDR USAA2013012500013](https://openairdocs.org/sdr/USAA2013012500013), Dec 18, 2012: FLOOR SUPPORT. CRACKED. C4 CHECK - CRACK ON FLOOR SUPPORT WEB UPPER CHORD AT B S1412, LBL 40. REPLACED FLOOR SUPPORT WEB UPPER CHORD AT BS 1412, LBL 40 IAW B767 SRM 51-40-02-0G, PAR. 4
- [SDR USAA2012121800026](https://openairdocs.org/sdr/USAA2012121800026), Dec 14, 2012: FLOORBEAM. CORRODED. C4 CHECK - CORROSION ON FLOORBEAM REPAIR STRAP AT BS 347, RBL 68. REPLACED FLOORBEAM REPAIR STRAP AT BS 347, RBL 68 IAW B767 SRM 53-00-51-2R-2 FIG 201.
- [SDR USAA2012121300006](https://openairdocs.org/sdr/USAA2012121300006), Dec 9, 2012: PLACARD. MISSING. C4 CHECK - LEFT AND RIGHT OVERWING HATCHES MISSING PLACARD. INSTALLED LEFT AND RIGHT OUTER WING HATCHES MISSING PLACARD IAW B767 AMM 20-10-13-964-001.
- [SDR USAA2013010300024](https://openairdocs.org/sdr/USAA2013010300024), Dec 7, 2012: SHEAR WEB. CRACKED. C4 CHECK - CRACK IN LEFT PYLON FORWARD SPAR UPPER SHEAR WEB AT NAC STA 227, LBL 5. REPAIRED LEFT PYLON FORWARD SPAR UPPER SHEAR WEB AT NAC STA 227, LBL 5 IAW EO
- [SDR USAA2013011500003](https://openairdocs.org/sdr/USAA2013011500003), Dec 4, 2012: FLOOR SUPPORT. DAMAGED. C4 CHECK - ELONGATED HOLES ON CABIN FLOOR STRUCTURE SUPPORT WEB AT BS 1412, LBL 40. REPLACED CABIN FLOOR STRUCTURE SUPPORT WEB AT BS 1412, LBL 40 IAW B767 SRM 5
- [SDR USAA2012120700005](https://openairdocs.org/sdr/USAA2012120700005), Dec 4, 2012: FASTENER. DAMAGED. C4 CHECK - RIGHT OFF WING SLIDE LATCH ACTUATOR HAS DAMAGED HARDWARE. REMOVED AND REPLACED HARDWARE IAW B767 AMM 20-11-00-427-003. USED TW 1111113012
- [SDR USAA2012120700004](https://openairdocs.org/sdr/USAA2012120700004), Dec 4, 2012: FASTENER. DAMAGED. C4 CHECK - RIGHT OFF WING SLIDE INTEGRATOR HAS DAMAGED HARDWARE. REMOVED AND REPLACED HARDWARE IAW B767 AMM 20-11-00-422-003. USED TW 1111113012.
- [SDR USAA2012120600005](https://openairdocs.org/sdr/USAA2012120600005), Dec 4, 2012: SPRING. WEAK. C4 CHECK, L-2 DOOR DEPLOYMENT BAR GAS SPRING WEAK. REMOVED AND REPLACED L-2 DOOR DEPLOYMENT BAR GAS SPRING IAW B767 AMM 25-66-03-004-053 AND 25-66-03-404-067.
- [SDR USAA2012120600004](https://openairdocs.org/sdr/USAA2012120600004), Dec 4, 2012: SPRING. WEAK. C4 CHECK, L-1 DOOR DEPLOYMENT BAR GAS SPRING WEAK. REMOVED AND REPLACED L-1 DOOR DEPLOYMENT BAR GAS SPRING IAW B767AMM 25-66-03-004-053 AND 25-66-03-404-067.
- [SDR USAA2013011500010](https://openairdocs.org/sdr/USAA2013011500010), Dec 1, 2012: SKIN. CORRODED. C4 CHECK - CORROSION FUSELAGE SKIN AT BS 959, LBL 94. REPAIRED FUSELAGE SKIN AT BS 959, LBL 94 IAW EA 131979.
- [SDR USAA2013011500009](https://openairdocs.org/sdr/USAA2013011500009), Dec 1, 2012: SKIN. CORRODED. C4 CHECK - CORROSION FUSELAGE SKIN AT BS 955, RBL 92. REPAIRED FUSELAGE SKIN AT BS 955, RBL 92 IAW EA 131979.
- [SDR USAA2013010300025](https://openairdocs.org/sdr/USAA2013010300025), Dec 1, 2012: FRAME. CRACKED. C4 CHECK - CRACK IN LEFT PYLON FRAME AT NAC STA 285.30, WL 148.0, LBL 12. REPAIRED LEFT PYLON FRAME AT NAC STA 285.30, WL 148.0, LBL 12 IAW B767 SRM 51-40-02-0G
- [SDR USAA2013012500016](https://openairdocs.org/sdr/USAA2013012500016), Nov 30, 2012: STRUCTURE. CORRODED. C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CENTER WING UPPER SKIN AT BS 955, RBL 4. REPAIRED CENTER WING UPPER SKIN AT BS 955, RBL4 IAW EA 504597A.
- [SDR USAA2013010800024](https://openairdocs.org/sdr/USAA2013010800024), Nov 29, 2012: FLOORBEAM. CORRODED. C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 1480, LBL 44. REPAIRED FLOORBEAM AT BS 1480, LBL 44 IAW B767 SRM 53-00-51-2R-1 FIG 201.
- [SDR USAA2013010300026](https://openairdocs.org/sdr/USAA2013010300026), Nov 29, 2012: ATTACH ANGLE. CRACKED. C4 CHECK - CRACK ON CABIN FLOOR SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS 1087 TO BS 1109, LBL 39. REPLACED CABIN FLOOR SUPPORT WEB UPPER ATTACH ANGLE CHO
- [SDR USAA2013011500006](https://openairdocs.org/sdr/USAA2013011500006), Nov 28, 2012: SEAT TRACK. CORRODED. C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN BS 1263 TO BS 1285, RBL 88.5. REPLACED SEAT TRACK BETWEEN BS 1263 TO BS 1285, RBL 88.5 IAW B767 S
- [SDR USAA2012121800023](https://openairdocs.org/sdr/USAA2012121800023), Nov 28, 2012: STRUCTURE. CRACKED. C3 CHECK - CRACK ON CHORD AT BS 1382, RBL 39. REPLACED CHORD AT BS 1382, RBL 39 IAW B767 SRM 51-40-02-0G FIG 3.
- [SDR USAA2012122100022](https://openairdocs.org/sdr/USAA2012122100022), Nov 27, 2012: STRUCTURE. CRACKED. C4 CHECK - CRACKS ON CABIN FLOOR STRUCTURE SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS1241 TO BS 1262, RBL 39. REPLACED CABIN FLOOR STRUCTURE SUPPORT WEB UP
- [SDR USAA2013012500012](https://openairdocs.org/sdr/USAA2013012500012), Nov 27, 2012: FLOOR SUPPORT. CRACKED. C4 CHECK - CRACK ON FLOOR SUPPORT WEB UPPER CHORD BETWEEN BS 1087 TO BS 1109, RBL 39. REPLACED FLOOR SUPPORT WEB UPPER CHORD BETWEEN BS 1087 TO BS 1109, RBL 39 
- [SDR USAA2013011500008](https://openairdocs.org/sdr/USAA2013011500008), Nov 19, 2012: FAILSAFE. CRACKED. C4 CHECK - CRACK ON RIGHT FUSELAGE FAIL SAFE STRAP AT BS 959, RBL 92. REPAIRED RIGHT FUSELAGE FAIL SAFE STRAP AT BS 959, RBL 92 IAW EA 131979.
- [SDR USAA2013011500007](https://openairdocs.org/sdr/USAA2013011500007), Nov 19, 2012: FAILSAFE. CRACKED. C4 CHECK - CRACK ON LEFT FUSELAGE FAIL SAFE STRAP AT BS 959, LBL92. REPAIRED LEFT FUSELAGE FAIL SAFE STRAP AT BS 959, LBL92 IAW EA 131979.

All 121: https://openairdocs.org/deregistered/N256AY-2022-02-05/reports.md

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