# N660CP: 2008 Boeing 737-7BD

- Status: Valid registration
- Airframe: [Boeing 737-7BD](https://openairdocs.org/model/boeing-737-7bd) (registry code 1384511, 149 seats)
- Engine: [CFM International CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043)
- Serial number: 36721
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 14, 2008
- Certificate issued: September 16, 2026
- Expires: September 30, 2033
- Mode S code: A8B479
- Registered owner: [Eastern Air Express LLC](https://openairdocs.org/faa-owner/EASTERN%20AIR%20EXPRESS%20LLC)
- Location: [Greensboro, NC](https://openairdocs.org/faa-place/NC/Greensboro)
- Owner type: LLC
- Owner's area on the map: 36.1154° N, 79.7346° W: Placed by OpenAirDocs at the center of ZIP code 27405, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=660CP
- Page: https://openairdocs.org/aircraft/N660CP

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. The registry lists only the engine series, so ADs for every CFM International CFM56-7B22 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-7BD)

None in force.

### Matched by engine (CFM International CFM56-7B22 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998

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

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000

## Information bulletins (advisory) (1 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations

None matched to N660CP.

## 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 20090528857409I](https://openairdocs.org/incident/20090528857409I), May 28, 2009: Boeing 737-7BD (N660CP), Fairbanks, AK, Minor damage. Ptrs # AL01200902501INCIDENT # IAL012009275/28/2009 at 1049AM fai FSDO received a phone call from roc of a B737-700 that hit a flock of ducks on takeoff.…

## Service difficulty reports (21)

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 SROM20200810002](https://openairdocs.org/sdr/SROM20200810002), Aug 10, 2020: SKIN. CRACKED. TWO CRACKS IN LT HORIZONTAL STABILIZER LOWER SKIN, HSS 157, 9 AND 16 FROM THE AFT SPAR. REPAIRED THE SKIN IAW SRM 55-10-01-2R-11, REV 70.
- [SDR SROM20200810001](https://openairdocs.org/sdr/SROM20200810001), Aug 10, 2020: SKIN. CRACKED. CRACK IN LH HORIZONTAL STABILIZER LOWER SKIN, STAB STA. 101, 19” FORM THE FORWARD SPAR. REPAIRED CRACK IN LH HORIZONTAL STABILIZER LOWER SKIN AT STA. 101, 19” F
- [SDR SROM2020051300000](https://openairdocs.org/sdr/SROM2020051300000), May 13, 2020: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS ROW 14 AND 16 AIRCRAFT LEFT INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AT ROW 14 AND 16 LH IAW B737-700 AMM 33-51-00. OPS CHECK O
- [SDR 2019FA0000385](https://openairdocs.org/sdr/2019FA0000385), Nov 26, 2019: BATTERY PACK. DISCHARGED. RH OVERWING EMERGENCY LIGHTS INOP.
- [SDR SROM2019F00225](https://openairdocs.org/sdr/SROM2019F00225), Jul 1, 2019: BATTERY. DISCHARGED. EMERGENCY EXIT SIGN/LIGHT AT LH OVERWING EXIT WILL NOT STAY LIT.
- [SDR 2016F00108](https://openairdocs.org/sdr/2016F00108), Apr 26, 2016: FRAME. DENTED. INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR T
- [SDR 2016F00111](https://openairdocs.org/sdr/2016F00111), Apr 26, 2016: FRAME. DENTED. INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME, PN 146A1285-70, AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM RE
- [SDR 2016F00113](https://openairdocs.org/sdr/2016F00113), Apr 26, 2016: INTERCOSTAL. DEFORMED. DURING INSPECTION, DAMAGE WAS NOTED IN THE UPPER FLANGE OF THE INTERCOSTAL RUNNING BETWEEN BS 787 & BS 807 AT STRINGER 22L. FABRICATED & INSTALLED REPLACEMENT I
- [SDR SROM2016F00098](https://openairdocs.org/sdr/SROM2016F00098), Apr 26, 2016: SHEAR TIE. DENTED. INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA AND THERE ARE NOR SRM REPAIRS FOR SHEA
- [SDR 2016F00110](https://openairdocs.org/sdr/2016F00110), Apr 26, 2016: FRAME. DENTED. INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR T
- [SDR SROM2016042600118](https://openairdocs.org/sdr/SROM2016042600118), Apr 26, 2016: FRAME. DENTED. INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA AND THERE ARE NO SRM REPAIRS FOR SHEAR
- [SDR 2016F00109](https://openairdocs.org/sdr/2016F00109), Apr 26, 2016: FRAME. DENTED. INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR T
- [SDR 2016F00117](https://openairdocs.org/sdr/2016F00117), Apr 26, 2016: FRAME. DENTED. INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR T
- [SDR SROM091220141](https://openairdocs.org/sdr/SROM091220141), Sep 12, 2014: WARNING LIGHT. FALSE ACTIVATION. DURING TAKEOFF ROLL, FORWARD ENTRY DOOR LIGHT ILLUMINATED AT 80 KNOTS. REJECTED TAKEOFF, RETURNED TO GATE. INSPECTED AND TESTED FORWARD ENTRY DOOR IAW FAULT ISO
- [SDR SROM0418201403](https://openairdocs.org/sdr/SROM0418201403), Apr 18, 2014: INTERCOSTAL. CRACKED. FOUND CRACK IN INTERCOSTAL NEXT TO FLOOR PANEL ATTACH NUTPLATE.
- [SDR SROM0418201402](https://openairdocs.org/sdr/SROM0418201402), Apr 18, 2014: FLOOR PANEL. CRACKED. FLOOR PANEL FOUND CRACKED.
- [SDR SROM0418201401](https://openairdocs.org/sdr/SROM0418201401), Apr 18, 2014: FLOOR PANEL. CRACKED. FLOOR PANEL FOUND CRACKED.
- [SDR SROM201311210001](https://openairdocs.org/sdr/SROM201311210001), Nov 19, 2013: DOWNLOCK SWITCH. OUT OF TOLERANCE. DURING CLIMB OUT, AFTER GEAR RETRACTION, FORWARD PANEL GEAR INDICATOR SHOWED RT MAIN GEAR STILL DOWN AND LOCKED. OVERHEAD GEAR INDICATOR SHOWED ALL 3 GEAR UP AN
- [SDR SROM2010017](https://openairdocs.org/sdr/SROM2010017), Dec 16, 2010: COMPRESSOR BLADE. NICKED. NR 2 ENG BIRD STRIKE AND INGESTION AT THE 9 O’CLOCK POSITION. BLOOD AND FEATHERS FOUND ON BLADES IN BYPASS PATH AND BOOSTER INLET. CONDITIONAL INSP COMPLIED WIT
- [SDR SROM20100001](https://openairdocs.org/sdr/SROM20100001), Feb 19, 2010: AUTOPILOT SYS. DISCONNECTED. SPEED TRIM FAIL LIGHT ILLUMINATED AND YAW DAMPER WON'T ENGAGE DURING TAKEOFF. MADE UNEVENTFUL RETURN TO DEPARTURE AIRPORT. PERFORMED YAW DAMPER SYS TEST IAW AMM
- [SDR SROM20090001](https://openairdocs.org/sdr/SROM20090001), May 28, 2009: WINDSHIELD. CRACKED. MULTIPLE BIRD STRIKES ON DEPARTURE, RETURNED TO AIRPORT. REPLACED F/O WINDSHIELD. REPLACED 5 RIVETS UNDER INBD STRAFE OF NR 2 ENGINE NOSE COWL. CLEANED MULTIPLE

## STCs that may be installed (OpenAirDocs) (2)

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 (CFM International CFM56-7B22 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc

## Related

- Other Boeing 737-7BD aircraft: https://openairdocs.org/model/boeing-737-7bd/aircraft.md
- The CFM International CFM56-7B22 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b22-series.md

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