# N220CY: 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: 24729
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 2, 2012
- Certificate issued: October 16, 2014
- Expires: October 31, 2027
- Mode S code: A1E14A
- 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=220CY
- Page: https://openairdocs.org/aircraft/N220CY

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 N220CY.

## FAA accident and incident reports

None matched to N220CY.

## Service difficulty reports (78, 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 ABXA20260922431](https://openairdocs.org/sdr/ABXA20260922431), Sep 22, 2026: FRAME. DAMAGED. DURING T/S OF R IDG, FOUND FRAME AT BS 698, STR 22R DAMAGED FROM ELECTRICAL DISCHARGE AC GROUNDED AND TEMP REPAIR WAS ACCOMPLISHED IAW ABX REA-5330-66263-01 AND
- [SDR ABXA20260720327](https://openairdocs.org/sdr/ABXA20260720327), Jul 20, 2026: INDICATOR. FAULTED. DURING TAXI OUT, RT ELEVATOR DOESN'T INDICATE FULL TRAVEL. ACFT RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED FLIGHT CONTROL POSITION INDICATION
- [SDR ABXA20260530233](https://openairdocs.org/sdr/ABXA20260530233), May 30, 2026: WARNING LIGHT. FALSE ACTIVATION. DURING TAXI OUT RUDDER RATIO EICAS MSG & DISCREET LIGHT ILLUMINATED ON A/C RETURENED TO GATE (BTB) AND MTX GROUNDED A/C. T/S AS PER FIM 27-09 FT 814, PERFORMED 
- [SDR ABXA20260520218](https://openairdocs.org/sdr/ABXA20260520218), May 20, 2026: ELEVATOR SYSTEM. FAULTED. DURING FLIGHT CONTROL, RIGHT ELEVATOR STOPS HALF WAY BEFORE FULL TRAVEL. CREW RETURNED TO THE GATE (BTB). MTC VERIFIED ELEVATOR INDICATION. C/W MAINT. PROCEDURE
- [SDR ABXA20260204048](https://openairdocs.org/sdr/ABXA20260204048), Feb 4, 2026: HEATER. INOPERATIVE. DURING TAXI OUT, RT WINDOW HEAT INOPERATIVE. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED RT SIDE WINDOW NR 2 HEAT SYS EPR MEL ABX-30-41-1-2. PLACRAD
- [SDR ABXA2026131042](https://openairdocs.org/sdr/ABXA2026131042), Jan 31, 2026: LAMP. INOPERATIVE. DURING TAXI OUT CREW REPORTS LH ENG BLEED OFF LIGHT INOP. ACFT RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC. MTX RELAMPED LH BLEED OFF LIGHT IAW AMM 33-11-00,
- [SDR ABXA202601186016](https://openairdocs.org/sdr/ABXA202601186016), Jan 16, 2026: LOCK. CRACKED. LEFT FWD ENTRY DOOR EICAS MSG AT 4,000 FEET. T/S PER W.D. 52-71-11 FOUND S195 L FWD ENTRY DOOR LOCKED FACE CRACKED. R & R SAME IAW W.D.52-71-11 OPS CK RIGGING C
- [SDR ABXA20260107005](https://openairdocs.org/sdr/ABXA20260107005), Jan 7, 2026: TRANSMITTER. DEFECTIVE. DURING TAXI OUT, RIGHT ELEVATOR INDICATOR IS NOT SHOWING FULL DEFLECTION DURING CONTROL CHECK. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED ELEVATOR INDICATION I
- [SDR ABXA20251227358](https://openairdocs.org/sdr/ABXA20251227358), Dec 27, 2025: WARNING MESSAGE. ILLUMINATED. DURING TAXI OUT, EICAS MESSAGE CARGO A/C CONT.ILLUMINATED, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C . MTX THEN DEFERRED FWD CARGO A/C SYSTEM IAW MEL 21-2
- [SDR ABXA20251011265](https://openairdocs.org/sdr/ABXA20251011265), Oct 11, 2025: INDICATOR. FLUCTUATES. ON INITIAL CLIMB FROM KCVG STATNDY ATTITUDE INDICATOR BECAME ERRACTIC AND UNRELIABLE AC RETURNED TO FIELD AND RETURNED TO BLOCKS ,MTX GROUNDED AC .MTX TROUBLE S
- [SDR ABXA20250902206](https://openairdocs.org/sdr/ABXA20250902206), Sep 2, 2025: SEAL. BROKEN. DURING SERVICE CHECK SECURITY SEAL MISSING ON FIRST AID KIT. INVENTORY NON-COMPLIANT. MTX REMOVED AND REPLACED FIRST AID KIT IAW B767 AMM 25-64-03. AC COMPLIANT
- [SDR ABXA20250723165](https://openairdocs.org/sdr/ABXA20250723165), Jul 23, 2025: ELEVATOR. MALFUNCTIONED. DURING CRITICAL CHECK, RT ELEVATOR INDICATION WAS 2/3 FROM TOP AND BOTTOM. LEFT ELEVATOR INDICATION WAS NORMAL. AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE DEFERRE
- [SDR ABXA20250424084](https://openairdocs.org/sdr/ABXA20250424084), Apr 24, 2025: FIRE DETECTOR. FALSE ACTIVATION. AFT CARGO FIRE MESSAGE DURING TAKE-OFF ROLL AT 100 KNOTS, ABORT ACTIVATED, (ATO) MSG EXTINGISHED ON TAXIWAY - (CREW MENTIONED THE BRAKE TEMPS WERE NORMAL). A/C 
- [SDR ABXA20250411075](https://openairdocs.org/sdr/ABXA20250411075), Apr 11, 2025: START VALVE. INOPERATIVE. DURING TAXI OUT WHILE STARTING #2 ENGINE ,#2 ENGINE START VALVE WILL NOT OPEN DURING START. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED #2 STA
- [SDR ABXA20250322063](https://openairdocs.org/sdr/ABXA20250322063), Mar 23, 2025: OIL SYSTEM. LOW. DURING TAXI OUT ON ENGINE START, RT ENGINE QUANTITY WAS 9. A/C RETURNED TO GATE (BTB). SERVICED RT ENGINE IAW B767 AMM 12-13-01. VERIFIED OIL CAP AND ACCESS PAN
- [SDR ABXA20250319061](https://openairdocs.org/sdr/ABXA20250319061), Mar 19, 2025: ELEVATOR. UNKNOWN. DURING TAXI OUT, RIGHT ELEVATOR ONLY SHOWS ~ 80% TRAVEL UP AND DOWN. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED IAW MEL AMM 27-38-00. RETURNE
- [SDR ABXA20250115011](https://openairdocs.org/sdr/ABXA20250115011), Jan 15, 2025: START VALVE. MALFUNCTIONED. DURING TAXI WHILE STARTING RH ENGINE ,R STARTER CUTOUT AFTER STARTING RIGHT ENGINE.AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC . TROUBLE SHOT AND PERFORME
- [SDR ABXA20241210250](https://openairdocs.org/sdr/ABXA20241210250), Dec 10, 2024: APU. FAULTED. APU AIR PRESSURE LOW DURING START (11 PSI)DURING LH ENGINE START HUNG AT 25% N2 ON TAXI OUT. AC RETURNED TO GATE (BTB) . MTX GROUNDED AC AND DEFERRED APU IAW ME
- [SDR ABXA20240828159](https://openairdocs.org/sdr/ABXA20240828159), Aug 28, 2024: START VALVE. MALFUNCTIONED. "DURING PUSHBACK AFTER SELECTING RIGHT ENGINE TO GROUND, R ENG STARTER EICAS MESSAGE APPEARED WITH NO ENGINE ROTATION A/C RETURNED TO GATE AND MTX GROUNDED AC .
- [SDR ABXA20240614113](https://openairdocs.org/sdr/ABXA20240614113), Jun 14, 2024: WARNING MESSAGE. ILLUMINATED. FWD CARGO AC CONTROL STATUS MESSGE DURING TAXI , AC RETURED TO THE GATE AND MAINTENANCE GROUNDED AC AND DEFERRED THE FWD CARGO AIR COND.SYSTEM IAW ABX 21-28-1 A
- [SDR ABXA2024032161](https://openairdocs.org/sdr/ABXA2024032161), Mar 21, 2024: EEC. FAULTED. ON ENGINE START, STATUS MESSAGE: R ENG EEC C1. DEFERRED PER ABX-73-21-1-4.
- [SDR ABXA20231130218](https://openairdocs.org/sdr/ABXA20231130218), Nov 30, 2023: UNKNOWN. UNKNOWN. TWO ENGINE SURGES DURING LEVEL OFF. COULD NOT DETERMINE WHICH ENGINE WAS. (AUTO EVENT SHOWS LEFT ENGINE) AC GROUNDED AND BEING WORKED THIS SDR WILL BE AMENDED W
- [SDR ABXA202311076212](https://openairdocs.org/sdr/ABXA202311076212), Nov 6, 2023: UNKNOWN. UNKNOWN. L. ENG HUNG START. FOLLOWED CHECKLIST- NO HELP. 2ND START ALSO HUNG.DURING TAXI AC RETURNED TO GATE AND GROUNDED BY MAINTENANCE .FOUND LOOSE CONNECTOR ON L ENGI
- [SDR ABXA20230829181](https://openairdocs.org/sdr/ABXA20230829181), Aug 28, 2023: UNKNOWN. UNKNOWN. RT FWD FUEL PUMP EICAS MESSAGE & RT FWD PRESSURE LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE. T/S AND VERIFIED PRESS LIGH
- [SDR ABXA20230623129](https://openairdocs.org/sdr/ABXA20230623129), Jun 19, 2023: SKIN. DAMAGED. DURING AIRCRAFT C-CHECK IN GSO (GREENSBORO, NORTH CAROLINA), HAECO MAINTENANCE DISCOVERED LIGHTNING STRIKE DAMAGE AND PREVIOUS BLENDOUT REPAIRS ON THE RIGHT HAN
- [SDR ABXA20230623127](https://openairdocs.org/sdr/ABXA20230623127), Jun 15, 2023: SKIN. CRACKED. DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, DENT AND CRACK DAMAGE WAS FOUND ON THE FUSELAGE SKIN P/N 148T3251-4. THE DAMAGE IS LOCATED AT STA 1710.5 BELOW T
- [SDR ABXA20230623126](https://openairdocs.org/sdr/ABXA20230623126), Jun 7, 2023: SKIN. FAULTY. DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MX WAS REQUIRED TO RE-INSPECT AND REPLACE (5/32”) BLIND FASTENERS IN AN EXISTING REPAIR DESCRIBED IN ABX “WATCH 
- [SDR ABXA20230623133](https://openairdocs.org/sdr/ABXA20230623133), May 25, 2023: FAIRING. DAMAGED. DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED THAT THE NO. 2 PYLON AFT FAIRING INBOARD HYDRAULIC BAY CLOSEOUT PANEL (313T3381-212) HAS NU
- [SDR ABXA20230623128](https://openairdocs.org/sdr/ABXA20230623128), May 25, 2023: SKIN. CORRODED. "DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MX REPORTED CORROSION DAMAGE ON THE RH WING LOWER SKIN NO. 1 PANEL, 112T4701-4, BETWEEN RSS 852.00 AND RSS 879.
- [SDR ABXA202306 23131](https://openairdocs.org/sdr/ABXA202306%2023131), May 19, 2023: SEAL DEPRESSOR. GOUGED. DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED GOUGE DAMAGE ON THE NO. 2 STRUT, OUTBOARD FIRE SEAL DEPRESSOR (113T4011-14). THE POST-BLEND
- [SDR ABXA2023O623134](https://openairdocs.org/sdr/ABXA2023O623134), May 17, 2023: PIN. OUT OF TOLERANCE. MDCD LATCH CAM PIN #'S 12,10, 6,4,2 AND FAILED DIMENSION CHECK WHILE IN C-CHECK HAECO AMERICAS. MAINTENANCE REPLACED MDCD LATCH CAM PINS IAW 767 AMM 52-32-11. O
- [SDR ABXA20230623132](https://openairdocs.org/sdr/ABXA20230623132), May 17, 2023: WEB. CORRODED. DURING C21 MAINTENANCE CHECK AT HAECO AMERICAS,MAINTENANCE FOUND FWD CARGO DOOR CUTOUT, LOWER TORQUE BOX WEB UPPER SURFACE IS CORRODED FROM APPROX STA 515-544 R
- [SDR ABXA20230623130](https://openairdocs.org/sdr/ABXA20230623130), May 17, 2023: FLAP. DENTED. WHILEIN C-CHECK IN HAECO MAINTENANCE DISCOVERED R/W I/B FLAP, AFT FLAP TOP SIDE HAS A DENT. MARKED IN RED. EVALUATED DENT ON R/W I/B FLAP AFT FLAP UPPER SURFACE
- [SDR ABXA2023041255](https://openairdocs.org/sdr/ABXA2023041255), Apr 11, 2023: PUMP. OVERHEATED. L PRIM HYD OVHT DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED CASE DRAIN FILTER I/A/W AMM 29-11-17. REMOVED 
- [SDR ABXA2023032838](https://openairdocs.org/sdr/ABXA2023032838), Mar 27, 2023: VALVE. DEFECTIVE. LEFT ENGINE BLEED OVERHEAT EICAS MESSAGE PERFORMED QRH PROCEDURE, LIGHT EXTINGUISHED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE AS PER FIM
- [SDR ABXA20221024118](https://openairdocs.org/sdr/ABXA20221024118), Oct 21, 2022: CIRCUIT BOARD. DEFECTIVE. R PACK OFF EICAS MESSAGE APPEARS DURING TAXI, UNABLE TO TROUBLESHOOT VIA QRH, MEL NOT CREW DEFERRABLE ETOPS 180, IN AUTO POSITION OR N POSITION PACK OFF STAYS I
- [SDR ABXA2022082985](https://openairdocs.org/sdr/ABXA2022082985), Aug 29, 2022: SWITCH. STICKING. DURING T.O. ROLL, AIRSPEED ,80KTS. UNSCHEDULED STAB TRIM EICAS/ MASTER CAUTION. ABORTED TAKE-OFF. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENACE. MAINTENANCE
- [SDR ABXA2022081496](https://openairdocs.org/sdr/ABXA2022081496), Aug 14, 2022: MODULE. FAULTED. ON TAKEOFF ROLL EICAS MESSAGE "UNSCHD STAB TRIM" EXECUTED SLOW SPEED ABORT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED MCDP TEST 
- [SDR ABXA2022080289](https://openairdocs.org/sdr/ABXA2022080289), Aug 2, 2022: EICAS. FALSE INDICATION. T.O. WARNING ALERT ON TAKE OFF ROLL WITH UNSCHED STAB TRIM EICAS MSG W. ASSOCIATED MASTER CAUTION LIGHTS AND TAKE OFF WARNING HORN (STAB TRIM DISCRETE LIGHT ILL
- [SDR ABXA2022070475](https://openairdocs.org/sdr/ABXA2022070475), Jul 4, 2022: NONE. DEFECTIVE. SLOW DEPRESSURIZATION OCCURRED AT 36,000 FEET. CONTROL OF CABIN PRESSURE REGAINED SOMEWHERE BETWEEN 20,000 FEET. AIRCRAFT DIVERTED TO JAX WITH NO ADDITIONALPROB
- [SDR ABXA2022060765](https://openairdocs.org/sdr/ABXA2022060765), Jun 7, 2022: NONE. NONE. AT FL380 CABIN ALT WARNING AND HORN WENT ON, CABIN ALT APPROX 12000 FT MODE SELECT AUTO 1 CREW ELECTED TO PERFORM AN AIR TURN BACK. AIRCRAFT LANDED WITHOUT FURT
- [SDR ABXA202252658](https://openairdocs.org/sdr/ABXA202252658), May 26, 2022: NONE. NONE. UNSCHED STAB TRIM EICAS MESSAGE ON TAKEOFF ROLL AT APPROX 65 KTS. ABORTED TAKEOFF. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLESHOT SY
- [SDR ABXA202241455](https://openairdocs.org/sdr/ABXA202241455), May 14, 2022: NONE. NONE. AFT CARGO OVHT DURING TAXI, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED PER MEL 21-40-2-1A2. MBCB 05/24/2022. AIRCRAFT REMAINS ETOP
- [SDR ABXA20211212128](https://openairdocs.org/sdr/ABXA20211212128), Dec 12, 2021: NONE. NONE. ON TAXI OUT IT WAS FOUND THAT LOW SYSTEM HYDRAULIC PRESSURE LIGHT INOP, AIRCTAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RELAMPED & DIODE CARD CL
- [SDR ABXA20211119119](https://openairdocs.org/sdr/ABXA20211119119), Nov 19, 2021: SURGE VALVE. STICKING. DURING LEFT ENGINE START ONLY, DUCT PRESSURE GAUGE FLUCTUATIONS 10-30PSI AND ONLY ABLE TO ACHIEVE 16% N2 VERY SLOW TO SPOOL, NO PARAMETERS EXCEEDED. RT START NO
- [SDR ABXA20211116113](https://openairdocs.org/sdr/ABXA20211116113), Nov 16, 2021: NONE. NONE. APU PNEUMATICS DROP ALL CYCLE BETWEEN 15-20 PSI DURING LEFT ENGINE START.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE APU PER ME
- [SDR ABXA2021924095](https://openairdocs.org/sdr/ABXA2021924095), Sep 24, 2021: NONE. NONE. F/O WINDOW OPENED DURING TO ROLL. CREW ABORTED TAKE OFF, BRAKE TEMP LIGHT ON AFTER 80 KT ABORT, WHEELS #2 AND #3 BOXED AND SHOWING 5 ON EICAS. AIRCRAFT RETURNED
- [SDR ABXA2021923094](https://openairdocs.org/sdr/ABXA2021923094), Sep 23, 2021: STARTER. SPARKS. R STARTER CUT OUT EICAS GROUND PERSONAL REPORTS LARGE AMOUNT OF SPARK EXITING RT ENG.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE.DURING INSPECTION FOUND 
- [SDR ABXA202162057](https://openairdocs.org/sdr/ABXA202162057), Jun 2, 2021: TRANSCEIVER. MALFUNCTIONED. LEFT HF RECEIVES BUT UNABLE TO XMIT, ALL THREE STATIONS.CREW DECIDED TO PERFORM AIR TURN BACK AS A PRECAUTION. AIRCRAFT WAS GROUNDED BY MAINTENANCE. CIRCUIT BRE
- [SDR ABXA202159041](https://openairdocs.org/sdr/ABXA202159041), May 9, 2021: STRAP. CORRODED. WHILE IN C-CHECK AFT CARGO SILL BEAM UPPER STRAP WAS FOUND TO HAVE CORROSION FROM STATION 1263 TO 1351. REPLACED CHORD IAW B767-300 SRM 51-40-05 AND 51-40-02

All 78: https://openairdocs.org/aircraft/N220CY/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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