# N226CY: 1992 Boeing 767-383ER

- Status: Valid registration
- Airframe: [Boeing 767-383ER](https://openairdocs.org/model/boeing-767-383er) (registry code 1385310, 330 seats)
- Engine: [Pratt & Whitney PW4060](https://openairdocs.org/engine/pratt-whitney-pw4060) (registry code 52140)
- Data sheets: [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (Pratt & Whitney Division) (OpenAirDocs)
- Serial number: 26544
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 3, 2014
- Certificate issued: March 4, 2015
- Expires: March 31, 2028
- Mode S code: A1F794
- Registered owner: [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 is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=226CY
- Page: https://openairdocs.org/aircraft/N226CY

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 24 in force

### Matched by airframe (Boeing 767-383ER)

None in force.

### Matched by engine (Pratt & Whitney PW4060)

- [AD 2026-21-06](https://openairdocs.org/ad/2026-21-06): Engine Fuel and Control · Pratt & Whitney Division PW4052, PW4056, PW4060 and 10 more. Effective Nov 23, 2026
- [AD 2018-13-02](https://openairdocs.org/ad/2018-13-02): Turbine Engine Combustion Section · Pratt & Whitney Division PW4052, PW4056, PW4060 and 7 more. Effective Jul 20, 2018
- [AD 2016-08-09](https://openairdocs.org/ad/2016-08-09): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Jun 1, 2016
- [AD 2015-22-03](https://openairdocs.org/ad/2015-22-03): LPT 4th stage IAS · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Dec 1, 2015
- [AD 2012-22-16](https://openairdocs.org/ad/2012-22-16): 3rd stage LPT duct segments · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Dec 19, 2012
- [AD 2012-14-09](https://openairdocs.org/ad/2012-14-09): 3rd and 4th stage vane fractures · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Nov 7, 2012
- [AD 2012-18-17](https://openairdocs.org/ad/2012-18-17): HPC drum rotor disk assembly · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 22, 2012
- [AD 2012-18-03](https://openairdocs.org/ad/2012-18-03): 1st stage HPT air seal rings · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Oct 11, 2012
- [AD 2012-16-01](https://openairdocs.org/ad/2012-16-01): High-pressure turbine (HPT) stage 1 front hubs · Pratt & Whitney Division PW4052, PW4056, PW4060 and 14 more. Effective Sep 28, 2012
- [AD 2012-06-18](https://openairdocs.org/ad/2012-06-18): Engine · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 27, 2012
- [AD 2012-04-04](https://openairdocs.org/ad/2012-04-04): fuel metering units (FMUs) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 5, 2012
- [AD 2011-25-09](https://openairdocs.org/ad/2011-25-09): PW4000 turbofan engines · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Jan 10, 2012
- [AD 2010-24-14](https://openairdocs.org/ad/2010-24-14): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 17 more. Effective Jan 21, 2011
- [AD 2010-24-09](https://openairdocs.org/ad/2010-24-09): No. 3 bearing oil pressure tubes · Pratt & Whitney Division PW4050, PW4052, PW4056 and 34 more. Effective Dec 28, 2010
- [AD 2008-24-13](https://openairdocs.org/ad/2008-24-13): Electronic engine controls (EECs) · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Jan 8, 2009
- [AD 2005-25-09](https://openairdocs.org/ad/2005-25-09): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 26 more. Effective Jun 12, 2006
- [AD 2003-19-15](https://openairdocs.org/ad/2003-19-15): High-Pressure-Compressor (HPC) Surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Oct 30, 2003
- [AD 2002-12-15](https://openairdocs.org/ad/2002-12-15): Front Drum Rotors · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Jul 31, 2002
- [AD 2001-05-07](https://openairdocs.org/ad/2001-05-07): Low Pressure Turbine (LPT) 4th Stage Air Seal · Pratt & Whitney Division PW4052, PW4056, PW4060 and 11 more. Effective Mar 30, 2001
- [AD 98-23-08](https://openairdocs.org/ad/98-23-08): High Pressure Compressor  Blade Tips · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jan 12, 1999
- [AD 98-19-03](https://openairdocs.org/ad/98-19-03): High Pressure Turbine Rotating Airseals · Pratt & Whitney Division PW4052, PW4056, PW4060 and 9 more. Effective Nov 9, 1998
- [AD 96-13-08](https://openairdocs.org/ad/96-13-08): AFT Cascade Support Frame Assembly · Pratt & Whitney assembly Part Number 221D5015, Revision A (STC SE744NE). Effective Aug 1, 1996
- [AD 93-08-16](https://openairdocs.org/ad/93-08-16): Fuel Pump · Pratt & Whitney Division PW4050, PW4052, PW4056 and 2 more. Effective Jul 12, 1993
- [AD 90-22-02](https://openairdocs.org/ad/90-22-02): Low Pressure Turbine Shaft · Pratt & Whitney Division PW4050, PW4052, PW4056 and 6 more. Effective Oct 18, 1990

### Historical (superseded or no longer in force)

- [AD 2010-18-13](https://openairdocs.org/ad/2010-18-13) (historical): Blade · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 18, 2010
- [AD 2003-11-18](https://openairdocs.org/ad/2003-11-18) (historical): High-Pressure-Compressor (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jul 7, 2003
- [AD 2002-21-10](https://openairdocs.org/ad/2002-21-10) (historical): High pressure compressor (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Nov 12, 2002
- [AD 2002-03-08](https://openairdocs.org/ad/2002-03-08) (historical): Time Limits Section of Engine Manuals (EM's) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 25 more. Effective Apr 16, 2002
- [AD 2001-25-11](https://openairdocs.org/ad/2001-25-11) (historical): Compressor Surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jan 17, 2002
- [AD 2001-20-13](https://openairdocs.org/ad/2001-20-13) (historical): High Pressure Compressor Front Drum Rotors · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Nov 16, 2001
- [AD 2001-15-12](https://openairdocs.org/ad/2001-15-12) (historical): High Pressure Compressors (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Aug 10, 2001
- [AD 2001-09-07](https://openairdocs.org/ad/2001-09-07) (historical): High Pressure Compressor (HPC) Surge · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective May 14, 2001
- [AD 2001-08-52](https://openairdocs.org/ad/2001-08-52) (historical): Multiple-engine power loss due to HPC surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more
- [AD 2000-25-06](https://openairdocs.org/ad/2000-25-06) (historical): Low Pressure Turbine (LPT) 4th Stage Air Seal · Pratt & Whitney Division PW4052, PW4056, PW4060 and 11 more. Effective Dec 29, 2000
- [AD 2000-22-01](https://openairdocs.org/ad/2000-22-01) (historical): High Pressure Compressor Cutback Stator · Pratt & Whitney Division PW4050, PW4052, PW4056 and 6 more. Effective Nov 9, 2000
- [AD 2000-12-02](https://openairdocs.org/ad/2000-12-02) (historical): Critical Life-Limited Part · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Sep 13, 2000
- [AD 99-17-16](https://openairdocs.org/ad/99-17-16) (historical): Pratt & Whitney Division PW4050, PW4052, PW4056 and 11 more. Effective Sep 24, 1999
- [AD 99-08-15](https://openairdocs.org/ad/99-08-15) (historical): Pratt & Whitney Division PW4050, PW4052, PW4056 and 20 more. Effective May 13, 1999

## Information bulletins (advisory) (5 in force)

- [SAIB 2025-06](https://openairdocs.org/saib/2025-06): High Pressure Turbines. Issued Jul 22, 2025
- [SAIB NE-19-02](https://openairdocs.org/saib/NE-19-02): Turbine Engine Compressor Section -- Low-pressure turbine uncontainment. Issued Feb 19, 2019
- [SAIB NE-16-01R1](https://openairdocs.org/saib/NE-16-01R1): Turbine Section. Issued Jan 14, 2016
- [SAIB NE-15-19](https://openairdocs.org/saib/NE-15-19): Turbine Section. Issued Jul 14, 2015
- [SAIB NE-13-31](https://openairdocs.org/saib/NE-13-31): Turbine Engine Oil System  Scavenge Oil Tube Coking and Proper Cleaning at Overhaul. Issued May 9, 2013
- [SAIB NE-16-01](https://openairdocs.org/saib/NE-16-01) (historical): Turbine Section. Issued Oct 5, 2015

## NTSB investigations

None matched to N226CY.

## FAA accident and incident reports

None matched to N226CY.

## Service difficulty reports (66, newest 50)

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

- [SDR ABXA20260709312](https://openairdocs.org/sdr/ABXA20260709312), Jul 9, 2026: FIRE WARNING. FALSE ACTIVATION. CARGO FIRE B8 LIGHT ILLUMINATED ON CENTER CONSOLE. PERFORMED BITE PROCEDURE FOR THE CARGO COMPARTMENT SMOKE DETECTION SYSTEM. IAW IAI FIM 26-14-00. OPS CHECK GO
- [SDR ABXA20260531234](https://openairdocs.org/sdr/ABXA20260531234), May 31, 2026: VALVE. MALFUNCTIONED. DURING TAXI OUT R HYD SYS PRESS, QTY LIGHT, RH FLUID LO STATUS MESSAGE ALL ILLUMINATTED AFTER STARTING THE R ENGINE. R HYD QTY DRAINED TO "O.OO RF".A/C RETURNED
- [SDR ABXA20260527229](https://openairdocs.org/sdr/ABXA20260527229), May 27, 2026: SMOKE DETECTOR. NO TEST. DURING SERVICE CHECK, FOUND MAIN CARGO LOOP 2A IN AMBER DOES NOT RESET. REMOVED & REPLACED SMOKE DETECTOR 2A IAW AMM 26-14-01 OPS CK GOOD.LIGHT IN CONTROL PANEL
- [SDR ABXA20260519215](https://openairdocs.org/sdr/ABXA20260519215), May 19, 2026: ENGINE. FAULTED. DURING ENGINE START, LT ENG NO ROTATION DURING X-BLEED START - RT ENG BLEED NEVER OPENED - TRIED MULTIPLE BLEED ISOLATION VALVE COMBINATIONS WITH NO ROTATION. C
- [SDR ABXA20260213065](https://openairdocs.org/sdr/ABXA20260213065), Feb 13, 2026: DOOR. MISSING. DURING MAINTENANCE INSPECTION, FOUND NR 2 ENGINE OTBD PYLON PANEL MISSING, 446BR. MAINTENANCE DEFERRED IAW CDL 54-53-2. PLACARDS INSTALLED. REDUCE TAKEOFF AND L
- [SDR ABXA20260131050](https://openairdocs.org/sdr/ABXA20260131050), Jan 31, 2026: BATTERY. INOPERATIVE. DURING MPD - SEG 6 CK (WO# 16337064), FOUND SPARE BATTERY M735 FOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY M735 IAW B76
- [SDR ABXA20260128033](https://openairdocs.org/sdr/ABXA20260128033), Jan 28, 2026: APU. SHUTDOWN. ON TAXI OUT, APU AUTO SHUT OFF 2 TIMES. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW ABX-49-11-1A. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20260120023](https://openairdocs.org/sdr/ABXA20260120023), Jan 20, 2026: ANTI-SKID VALVE. LEAKING. AFTER ENGINE START UP RT HYD QTY - 0. RH ANTI-SKID SELF RESETTING FUSE VALVE HYD LEAK. AIRCRAFT RETURNED TO BLOCKS (BTB). FOUND #2 SELF RESETTING VALVE FUSE ON 
- [SDR ABXA20251226357](https://openairdocs.org/sdr/ABXA20251226357), Dec 26, 2025: FIRE LOOP. WARNING MESSAGE. DURING MAINTENANCE PREFLIGHT FOUND APU FIRE LP 2 STATUS MESSAGE . MTX GROUNDED AC .MTX THEN DEFERRED THE APU LP2 FIRE LOOP IAW MEL 26-15-1-1. AC REMAINS NO ETOP
- [SDR ABXA20251217343](https://openairdocs.org/sdr/ABXA20251217343), Dec 17, 2025: BATTERY. INOPERATIVE. DURIING MAINTENANCE INSPECTION, FOUND M735 EMERGENCY BATTERY INOPERATIVE. MOVED ACTIVE CONNECTOR D1084 TO BATTERY M734 (SPARE). EMERGENCY LIGHTS OPS CHECK GOOD.
- [SDR ABXA2025122321](https://openairdocs.org/sdr/ABXA2025122321), Dec 2, 2025: SHUTOFF VALVE. MALFUNCTIONED. DURING DESCENT TE DISAGREE EICAS MESS FLAPS SELECTED 5 REMAINED AT NR 1, TOOK 3 TRIES IN HOLDING TO GET FLAPS 5 M AFTER LANDING SAME ISSUE. MTX GROUNDED ACFT AN
- [SDR ABXA20251120304](https://openairdocs.org/sdr/ABXA20251120304), Nov 20, 2025: ADC. INOPERATIVE. DURING CRUISE, LEFT ADC BECAME INOPERATIVE. FOLLOWED QRH, CA SWITCHED TO ADC ALT REMAINDER OF FLIGHT OK. AIRCRAFT DIVERTED TO MIA DUE TO RVSM RESTRICTIONS AND T
- [SDR ABXA20251030285](https://openairdocs.org/sdr/ABXA20251030285), Oct 30, 2025: SMOKE DETECTOR. DEFECTIVE. DURIING MAINT. PRE-FLIGHT, MAIN CARGO FIRE TEST PNL, A2 AMBER LED LIGHT DID NOT RESET. DEFERRED IAW MEL 26-16-2-2 MBCB 11-09-25. REMOVED AND REPLACED A2 SMOKE D
- [SDR ABXA20251010263](https://openairdocs.org/sdr/ABXA20251010263), Oct 10, 2025: SMOKE DETECTOR. FAULTED. DURING PRE-DEPARTURE CHECK, FOUND MAIN CARGO DECK SMOKE DET 2A AND 2B WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTORS 2A AND 2B IAW B767 AMM 2
- [SDR ABXA20250830205](https://openairdocs.org/sdr/ABXA20250830205), Aug 30, 2025: WARNING MESSAGE. ILLUMINATED. DURING DESENT ON POST C CHECK EVALUATION FLIGHT "LEADING EDGE SLAT ASYMMETRY" @ FL340 IN DESCENT AND @ 270 KTS > POSSIBLE SLATS/FLAPS OVER SPEED FLT 080 (EMERGE
- [SDR ABXA20250820180](https://openairdocs.org/sdr/ABXA20250820180), Aug 20, 2025: STRUCTURE. DAMAGED. DURING C CHECK IN TPA, RUDDER DAMAGED DURING A/C WEIGH TASK (AMES NR 0426). AIRCRAFT IS CURRENTLY IN WORK. AN AMENDED SDR REPORT WILL BE FILED WHEN COMPLETE. AM
- [SDR ABXA20250525103](https://openairdocs.org/sdr/ABXA20250525103), May 25, 2025: PITOT HEAD. MALFUNCTIONED. WITH ENGINES STARTED (AFTER PUSHBACK) CAPT PITOT EICAS & OVERHEAD LIGHT ILLUMINATED A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C . MTX TROUBLE SHOT AND REMOV
- [SDR ABXA20241127237](https://openairdocs.org/sdr/ABXA20241127237), Nov 27, 2024: WARNING MESSAGE. FALSE ACTIVATION. CABIN ALT WARNING AT APPROX 14,000' NO OTHER INDICATIONS AC DOES NOT PRESSURIZE AC RETURNED TO FIELD (ATB) AND LANDED SAFELY PEREFORMED CABIN PRESSURE LEAK TEST
- [SDR ABXA20241120228](https://openairdocs.org/sdr/ABXA20241120228), Nov 20, 2024: WARNING MESSAGE. ILLUMINATED. DURING TAXI OUT L. WING HYD VALVE EICAS APPEARED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC .MTX PERFORMED FIM 27-23 FT 803. THE SYSTEM IS O.K . AND RETURNED
- [SDR ABXA20241114224](https://openairdocs.org/sdr/ABXA20241114224), Nov 14, 2024: HEATER. FAULTED. LEFT AUX PITOT MESSAGE AFTER ENGINE START AND AC RETURNED TO GATE (BTB) MTX GROUNDED AC . MTX REPLACED L AUX PITOT PROBE IAW AMM 34-11-00 OPS AND LEAK TEST GOOD
- [SDR ABXA20240916174](https://openairdocs.org/sdr/ABXA20240916174), Sep 16, 2024: CIRCUIT BREAKER. FAULTED. DURING TAXIOUT BEFORE TAKE OFF RUDDER POS INDICATOR DID NOT MOVE DURING RUDDER CHECK.AC RETURNED TO THE GATE AND MTX GROUNDED AC . THEY RESET CIRCUIT BREAKER E1
- [SDR ABXA20240906171](https://openairdocs.org/sdr/ABXA20240906171), Sep 6, 2024: HOSE. LEAKING. AFTER PUSHBACK WHILE STARTING LH ENGINE L HYD QTY DROPPED TO ZERO A/C RETURNED TO GATE AND MTX GROUNDED AC . FOUND LEFT PRESSURE HOSE ASSEMBLY BENT LEAK CODE 32
- [SDR ABXA20240529102](https://openairdocs.org/sdr/ABXA20240529102), May 29, 2024: INDICATOR. UNKNOWN. DURING TAXI STBY ATI IS NOT INDICATING ZERO ANU ON THE GROUND. AIRCRAFT RETURNED TO GATE. MAINTENANCE GROUNDED AIRCRAFT. PERFORMED ISU ADJUSTMENT/TEST PER ALTIT
- [SDR ABXA2024042886](https://openairdocs.org/sdr/ABXA2024042886), Apr 28, 2024: WARNING SYSTEM. UNKNOWN. ON FIRST APPROACH TO MIA GPS WWARNING TERRAIN. A/C HAD GEAR/FLAPS DOWN AND WAS ON GLIDE SLOPE FOR RWY 9. SECOND APPROACH WAS NORMAL. MAINTENCE GROUNDED AC AND A
- [SDR ABXA20230927189](https://openairdocs.org/sdr/ABXA20230927189), Sep 27, 2023: CONTROLLER. MALFUNCTIONED. EICAS CABIN ALT (AUTO 2 CONTROLLER) MAINTENANCE DEFERRED AUTO PRESSURIZATION.AFTER ONE FLIGHT, MAINTENANCE REMOVED AND INSTALLED AUTO PRESSURE CONTROLLER ASSY I
- [SDR ABXA20230807155](https://openairdocs.org/sdr/ABXA20230807155), Aug 4, 2023: UNKNOWN. UNKNOWN. APU AUTOMATIC SHUTDOWN AFTER PUSHBACK, AIRCRAFT BACK TO BLOCK. FLIGHT CREW RESTARTED NORMALLY, NO OTHER ISSUES. AIRCRAFT DEPARTED.
- [SDR ABXA20230725150](https://openairdocs.org/sdr/ABXA20230725150), Jun 29, 2023: BEAM. CRACKED. WHILE IN C CHECK AT PEMCO TAMPA IT WAS DISCOVERED THAT THE LH STUB BEAM AT STA 903.5 WAS CRACKED. REPAIRED LH STUB BEAM STA 903.5 IAW ABX-EA-5300-0051-101. AIRC
- [SDR ABXA20230725149](https://openairdocs.org/sdr/ABXA20230725149), Jun 29, 2023: BEAM. CRACKED. WHILE IN C CHECK AT PEMCO TAMPA IT WAS DISCOVERED THAT RH STUB BEAM AT STA 903.5 CRACKED. REPAIRED RH STUB BEAM STA 903.5 IAW ABX-EA-5300-0052-101. AIRCRAFT RET
- [SDR ABXA2023050270](https://openairdocs.org/sdr/ABXA2023050270), May 1, 2023: UNKNOWN. UNKNOWN. AFTER PUSHBACK WE GOT THE AIL LOCK LIGHT, RETURNED TO GATE AILERON LOCKOUT EICAS MSG. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE RESET AILERON LOCKOUT BOX (S
- [SDR ABXA2023042465](https://openairdocs.org/sdr/ABXA2023042465), Apr 20, 2023: UNKNOWN. UNKNOWN. AFTER L ENG START THE L ENG PRV STATUS MSG CAME ON. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED AIR SUPPLY MODULE BITE PER AMM 36-
- [SDR ABXA2023012314](https://openairdocs.org/sdr/ABXA2023012314), Jan 20, 2023: WARNING MESSAGE. ILLUMINATED. CARGO DOOR (MAIN) INDICATION LIGHT ON DURING CLIMB FROM CVG. AIRCRAFT RETURNED TO CVG WITHOUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANC
- [SDR ABXA2023010300101](https://openairdocs.org/sdr/ABXA2023010300101), Jan 1, 2023: WINDOW. CRACKED. LEFT FORWARD COCKPIT WINDOW CRACKED IN CRUISE AT FL 310 LARGE CRACKING PATTERN WITH SOME RESIDUAL VISION. AIRCRAFT TURNED BACK AND LANDED AT ORD. WITH OUT FURTH
- [SDR ABXA2022127148](https://openairdocs.org/sdr/ABXA2022127148), Dec 6, 2022: WARNING LIGHT. ILLUMINATED. STATUS MESSAGE R ENG REV POS, AIRCRAFT ABORTED TAKE OFF AT 90 KNOTS. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED RIGHT REVERSER PER
- [SDR ABXA2022125145](https://openairdocs.org/sdr/ABXA2022125145), Dec 3, 2022: SHUTOFF VALVE. FAULTED. AT FL320 WE HAND A RAPID DEPRESSURIZATION. LEFT PACK WAS 30PSI AND RIGHT 10PSI AND CABIN ALT SLOWLY CLIMBING. CREW DECLARED AN EMERGENCY AND DESCENDED TO A LOWE
- [SDR ABXA20221121130](https://openairdocs.org/sdr/ABXA20221121130), Nov 19, 2022: WARNING MESSAGE. FALSE INDICATION. AT 6,000 FEET, MAIN DECK CARGO DOOR LIGHT AND AURAL WARNING APPEARED, WHILE RETURNING TO THE AIRPORT, THE WARNING EXTINQUISHED AT 4,000 FEET. LANDED WITH OUT FU
- [SDR ABXA2022011709](https://openairdocs.org/sdr/ABXA2022011709), Jan 17, 2022: STARTER. SEIZED. ENGINE L LOW MAX N2 MOTORING SPEED DURING START, DUCT PRESSURE WAS NORMAL WITH START VALVE OPEN, N2 NOTED AT 26%.AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED. MA
- [SDR ABXA20211213130](https://openairdocs.org/sdr/ABXA20211213130), Dec 13, 2021: FLAP SYSTEM. FAULTED. DURING FLIGHT TO BOG THE TE FLAP DISAGREE EICAS MESSAGE ILLUMINATED. THE FLIGHT CREW ELECTED TO DIVERT TO PTY BECAUSE OF MECHANCAL ISSUE AND WEATHER CONDITIONS 
- [SDR ABXA20211117118](https://openairdocs.org/sdr/ABXA20211117118), Nov 17, 2021: NONE. NONE. LEFT ENGINE STARTER WOULD NOT ENGAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. DURING TROUBLESHOOTING FOUND ONE WIRE IN WIRE BUNDLE W368 CHAFING AGAI
- [SDR ABXA2021108098](https://openairdocs.org/sdr/ABXA2021108098), Oct 8, 2021: NONE. NONE. MAIN CARGO DOOR LIGHT CAME ON AT 400 AGL DURING TAKEOFF. AIR TURNBACK TO CVG. UNEVENTFUL LANDING AND GROUNDED BY MAINTENANCE. T/S PER IAI SUPP MM 52-71-09. FOUN
- [SDR ABXA2021318019](https://openairdocs.org/sdr/ABXA2021318019), Mar 18, 2021: FMC. MALFUNCTIONED. LEFT AND RIGHT FMC DISPLAYED IRS GROUND SPEEDS NOT CHANGING. AIRCRAFT BACK TO BLOCK AND GROUNDED, RE-SET RIGHT/LEFT FMC CB'S. RE-ALIGNED IRU'S. OP'S CHECK FMC C
- [SDR ABXA202126008](https://openairdocs.org/sdr/ABXA202126008), Feb 6, 2021: OIL SYSTEM. LEAKING. LEFTENGINE OIL LEAK, CREW NOTICED OIL QUANTITY DECREASE BACK TO BLOCK, AIRCRAFT GROUNDED BY MAINTENANCE. OIL LEAK WAS FOUND TO BE RESULT OF OIL CAP NOT BEING IN
- [SDR ABXA20200803212](https://openairdocs.org/sdr/ABXA20200803212), Nov 13, 2020: BPCU. FAULTY. DURING PUSHBACK WE LOST RT AC BUS DURING RIGHT ENGINE START. AIRCRAFT RETURNED BACK TO BLOCK AND WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED BPCU, IAW B767 A
- [SDR ABXA20200803155](https://openairdocs.org/sdr/ABXA20200803155), Aug 3, 2020: VANE. DEPARTED. #2 ENG THRUST REVERSER CASCADE VANE DEPARTED AIRCRAFT ON LANDING. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20200720146](https://openairdocs.org/sdr/ABXA20200720146), Jul 20, 2020: WARNING MESSAGE. ILLUMINATED. ON TAXI OUT EICAS STATUS MESSAGE EICAS SCC FLASHED ON AND OFF SEVERAL TIMES. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20200521062](https://openairdocs.org/sdr/ABXA20200521062), May 21, 2020: WARNING SYSTEM. ACTIVATED. ON PUSHBACK C HYD PRIM 1 LIGHT REMAINED ON AND EICAS MSG DISPLAYED. AIRCRAFT WAS GROUNDED.
- [SDR ABXA202005084057](https://openairdocs.org/sdr/ABXA202005084057), May 4, 2020: PRESSURE SWITCH. MALFUNCTIONED. APU SHUTDOWN DURING PUSH BACK WOULD NOT RESTART. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020050429053](https://openairdocs.org/sdr/ABXA2020050429053), Apr 29, 2020: UNKNOWN. MALFUNCTIONED. APU SHUTDOWN DURING PUSH BACK WOULD NOT RESTART. AIRCRAFT WAS GROUNDED.
- [SDR ABXA201910172160](https://openairdocs.org/sdr/ABXA201910172160), Oct 12, 2019: DUCT. LEAKING. WHILE CLIMBING AFTER TAKEOFF, STATUS MESSAGES "L ENG OH LP 2" AND "L ENG OH LP 2" DISPLAYED AND EICAS MESSAGE "L ENG OH" DISPLAYED. THE CREW SHUT DOWN THE LEFT 
- [SDR ABXA20190716124](https://openairdocs.org/sdr/ABXA20190716124), Jul 16, 2019: BATTERY. DISCHARGED. THE EMERGENCY LIGHTING BATTERY (M738) IS INOPERATIVE. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE EMERGENCY LIGHTING BATTERY WAS REPLACED. THE CAUS
- [SDR ABXA20190709123](https://openairdocs.org/sdr/ABXA20190709123), Jul 9, 2019: SKIN. CORRODED. CORROSION ON THE FUSELAGE SKIN AT FUSELAGE STATION 955, STRINGER 23R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

All 66: https://openairdocs.org/aircraft/N226CY/reports.md

## STCs that may be installed (OpenAirDocs) (3)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Pratt & Whitney PW4060)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic
- [STC SE00053AT-D](https://openairdocs.org/stc/SE00053AT-D): Modification of fan exit guide vane, to line replaceable unit configuration. Chromalloy Gas Turbine Corp
- [STC SE00131LA](https://openairdocs.org/stc/SE00131LA): Modification of the subject engines to incorporate an oil tank reservoir insulation blanket in accordance with Hi Temp Insulation Inc. Drawing List 46M1024-301, Revision N/C, dated December 5, 1995, or later FAA approved revision as an acceptable alternate to Pratt & Whitney part number 50R280-01 or 51R059-01 insulation blankets. Hi Temp Insulation Inc

## Related

- Other Boeing 767-383ER aircraft: https://openairdocs.org/model/boeing-767-383er/aircraft.md
- The Pratt & Whitney PW4060 engine: https://openairdocs.org/engine/pratt-whitney-pw4060.md

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