# N660AM: 2026 Bell Textron Canada 407

- Status: Valid registration
- Airframe: [Bell Textron Canada 407](https://openairdocs.org/model/bell-textron-canada-407) (registry code 1182215, 8 seats)
- Engine: [Rolls-Royce 250-C47E/4](https://openairdocs.org/engine/rolls-royce-250-c47e-4) (registry code 54236)
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) (Bell Textron Canada Limited), [TCDS E1GL](https://openairdocs.org/tcds/E1GL) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 56483
- Year built: 2026
- Type: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Standard, normal
- Airworthiness date: January 17, 2026
- Certificate issued: August 14, 2026
- Expires: August 31, 2033
- Mode S code: A8B445
- Registered owner: [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC)
- Location: [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village)
- Owner type: LLC
- Owner's area on the map: 39.6120° N, 104.8828° W: Placed by OpenAirDocs at the center of ZIP code 80111, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=660AM
- Page: https://openairdocs.org/aircraft/N660AM

From the FAA registry file of October 22, 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): 44 in force

### Matched by airframe (Bell Textron Canada 407)

- [AD 2026-14-07](https://openairdocs.org/ad/2026-14-07): Main rotor control · Bell Textron Canada 407. Effective Aug 21, 2026
- [AD 2026-10-04](https://openairdocs.org/ad/2026-10-04): Electrical connectors · Bell Textron Canada 407. Effective Jun 25, 2026
- [AD 2025-13-01](https://openairdocs.org/ad/2025-13-01): Main Rotor Blades · Bell Textron Canada 407 and 427. Effective Jul 8, 2025
- [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024
- [AD 2024-10-12](https://openairdocs.org/ad/2024-10-12): Fuel system wiring · Bell Textron Canada 407. Effective Aug 22, 2024
- [AD 2023-17-51](https://openairdocs.org/ad/2023-17-51): Tail Rotor Blades · Bell Textron Canada 407. Effective Sep 21, 2023
- [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 2022-27-08](https://openairdocs.org/ad/2022-27-08): Rotorcraft Tail Boom · Bell Textron Canada 407. Effective Jan 12, 2023
- [AD 2022-23-02](https://openairdocs.org/ad/2022-23-02): Fuselage Structure · Bell Textron Canada 407. Effective Jan 3, 2023
- [AD 2021-19-01](https://openairdocs.org/ad/2021-19-01): Cabin Equipment/Furnishings · Shoulder harness restraint system (Bell Helicopter Textron STC SH2073SO or SH2751SO). Effective Oct 13, 2021
- [AD 2019-08-10](https://openairdocs.org/ad/2019-08-10): Main Rotor Drive System · Bell Helicopter Textron Canada 206A, 206B, 206L and 4 more. Effective Jun 24, 2019
- [AD 2018-25-17](https://openairdocs.org/ad/2018-25-17): Air Conditioning System Wiring · Airbus Helicopters 206A, 206B, 206L and 13 more. Effective Jan 22, 2019
- [AD 2018-10-06](https://openairdocs.org/ad/2018-10-06): Tail Rotor Drive Shaft · Bell Helicopter Textron Canada 407. Effective Jun 25, 2018
- [AD 2015-17-02](https://openairdocs.org/ad/2015-17-02): Main Rotor Drive System · Bell Helicopter Textron Canada 206L-4, 407, 427 and 1 more. Effective Sep 24, 2015
- [AD 2015-05-04](https://openairdocs.org/ad/2015-05-04): Fuselage Main, Longeron/Stringer · Bell Helicopter Textron Canada 407. Effective Apr 20, 2015
- [AD 2013-22-21](https://openairdocs.org/ad/2013-22-21): Emergency Flotation Section · Apical Industries, Inc. Emergency Float Kits (Dart Aerospace ULC STC SR01535LA). Effective Dec 13, 2013
- [AD 2013-22-01](https://openairdocs.org/ad/2013-22-01): Main Rotor Drive System · Bell Helicopter Textron Canada 206L-4 and 407. Effective Dec 5, 2013
- [AD 2013-20-05](https://openairdocs.org/ad/2013-20-05): Turbine Section · Bell Helicopter Textron Canada 407. Effective Dec 5, 2013
- [AD 2013-18-06](https://openairdocs.org/ad/2013-18-06): Main Rotor Control · Bell Helicopter Textron Canada 206A, 206B, 206L and 10 more. Effective Oct 17, 2013
- [AD 2012-18-09](https://openairdocs.org/ad/2012-18-09): Rotorcraft tailboom · Bell Helicopter Textron Canada 407. Effective Oct 22, 2012
- [AD 2012-14-07](https://openairdocs.org/ad/2012-14-07): Rotorcraft Servo System · Bell Helicopter Textron Canada 407 and 427. Effective Aug 3, 2012
- [AD 2011-25-01](https://openairdocs.org/ad/2011-25-01): Liferafts · Agusta AB412, AB412 EP, 206A and 23 more. Effective Jan 17, 2012
- [AD 2010-26-51](https://openairdocs.org/ad/2010-26-51): Tail rotor blade · Bell Helicopter Textron Canada 206A, 206B, 206L and 10 more. Effective Mar 25, 2011
- [AD 2009-25-08](https://openairdocs.org/ad/2009-25-08): Hydraulic pump driveshaft assembly · Bell Helicopter Textron Canada 407 and 427. Effective Dec 28, 2009
- [AD 2009-22-11](https://openairdocs.org/ad/2009-22-11): Swashplate link assembly bearing · Bell Helicopter Textron Canada 407 and 427. Effective Nov 16, 2009
- [AD 2009-07-52](https://openairdocs.org/ad/2009-07-52): Cyclic control lever assembly · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 7 more. Effective May 1, 2009
- [AD 2008-14-06](https://openairdocs.org/ad/2008-14-06): Horizontal stabilizers · Bell Helicopter Textron Canada 206L, 206L-1, 206L-3 and 2 more. Effective Aug 14, 2008
- [AD 2004-10-07](https://openairdocs.org/ad/2004-10-07): Oil cooler blower bearings · Bell Helicopter Textron Canada 407. Effective Jun 4, 2004
- [AD 2003-05-11](https://openairdocs.org/ad/2003-05-11): Swashplate outer ring · Bell Helicopter Textron Canada 407. Effective Apr 2, 2003
- [AD 2003-02-06](https://openairdocs.org/ad/2003-02-06): Tailboom gearbox support castings · Bell Helicopter Textron Canada 407. Effective Feb 10, 2003
- [AD 2002-22-10](https://openairdocs.org/ad/2002-22-10): Horizontal stabilizer slat (slat) · Bell Helicopter Textron Canada 407. Effective Nov 21, 2002
- [AD 2002-20-05](https://openairdocs.org/ad/2002-20-05): Rescue hoists · Agusta A109, A109A, A109A II and 31 more. Effective Nov 7, 2002
- [AD 2002-17-03](https://openairdocs.org/ad/2002-17-03): Fuel Filler Cap · Bell Helicopter Textron Canada 407. Effective Sep 20, 2002
- [AD 2002-11-09](https://openairdocs.org/ad/2002-11-09): Forward Bearing Hanger Bracket · Bell Helicopter Textron Canada 407. Effective Jul 16, 2002
- [AD 2001-13-02](https://openairdocs.org/ad/2001-13-02): Cockpit Warning Horns · Bell Helicopter Textron Canada 407. Effective Aug 1, 2001
- [AD 2001-01-52 R1](https://openairdocs.org/ad/2001-01-52-R1): Tail Rotor Blades · Bell Helicopter Textron Canada 407. Effective Jul 25, 2001
- [AD 2000-14-16](https://openairdocs.org/ad/2000-14-16): Tail Rotor System · Bell Helicopter Textron Canada 407. Effective Aug 29, 2000
- [AD 2000-04-25](https://openairdocs.org/ad/2000-04-25): Door Latch Assembly · Bell Helicopter Textron Canada 407. Effective Apr 12, 2000
- [AD 2000-04-20](https://openairdocs.org/ad/2000-04-20): Hydraulic Relief Valve · Bell Helicopter Textron Canada 407. Effective Apr 5, 2000
- [AD 99-22-13](https://openairdocs.org/ad/99-22-13): Fin Assembly For Reduced Skin Thickness Inspection · Bell Helicopter Textron Canada 407. Effective Dec 2, 1999
- [AD 98-19-13](https://openairdocs.org/ad/98-19-13): Driveshaft · Bell Helicopter Textron Canada 407. Effective Jan 27, 1999
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-12-22](https://openairdocs.org/ad/98-12-22): Tail Rotor Drive System Bearing Supports · Bell Helicopter Textron Canada 407. Effective Jul 15, 1998
- [AD 97-24-17](https://openairdocs.org/ad/97-24-17): Tail Rotor Drive Coupling Disc Pack · Bell Helicopter Textron Canada 407. Effective Apr 16, 1998

### Matched by engine (Rolls-Royce 250-C47E/4)

None in force.

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

- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021
- [AD 2014-04-07](https://openairdocs.org/ad/2014-04-07) (historical): Rotorcraft Tail Boom and Middle Section · Bell Helicopter Textron Canada 407. Effective Jul 28, 2014
- [AD 2013-12-07](https://openairdocs.org/ad/2013-12-07) (historical): Rotorcraft tailboom · Bell Helicopter Textron Canada 407. Effective Aug 1, 2013
- [AD 2011-15-51](https://openairdocs.org/ad/2011-15-51) (historical): Hydraulic servo actuators · Bell Helicopter Textron Canada 407 and 427. Effective Nov 14, 2011
- [AD 2009-08-03](https://openairdocs.org/ad/2009-08-03) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 10 more. Effective Apr 24, 2009
- [AD 2009-07-51](https://openairdocs.org/ad/2009-07-51) (historical): Lever assembly bearing · Bell Helicopter Textron 206A, 206A-1 (OH-58A), 206B and 7 more
- [AD 2007-19-52](https://openairdocs.org/ad/2007-19-52) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 10 more. Effective Dec 5, 2007
- [AD 2005-03-07](https://openairdocs.org/ad/2005-03-07) (historical): Crosstube assembly · Bell Helicopter Textron Canada 407. Effective Mar 17, 2005
- [AD 2003-05-03](https://openairdocs.org/ad/2003-05-03) (historical): Tailboom · Bell Helicopter Textron Canada 407. Effective Apr 17, 2003
- [AD 2002-23-51](https://openairdocs.org/ad/2002-23-51) (historical): Swashplate drive link cup washers · Bell Helicopter Textron 407
- [AD 2002-06-52](https://openairdocs.org/ad/2002-06-52) (historical): Oil Cooler Blower Bearings · Bell Helicopter Textron 407. Effective May 2, 2002
- [AD 2001-13-51](https://openairdocs.org/ad/2001-13-51) (historical): Driveshafts · Bell Helicopter Textron Canada 206L-4, 407 and 427. Effective Oct 9, 2001
- [AD 2001-01-52](https://openairdocs.org/ad/2001-01-52) (historical): Airspeed · Bell Helicopter Textron 407. Effective Feb 21, 2001
- [AD 2000-20-18](https://openairdocs.org/ad/2000-20-18) (historical): Horizontal Stabilizer Slat · Bell Helicopter Textron 407. Effective Nov 22, 2000
- [AD 2000-06-10](https://openairdocs.org/ad/2000-06-10) (historical): Tail Boom · Bell Helicopter Textron 407. Effective Apr 14, 2000
- [AD 2000-02-12](https://openairdocs.org/ad/2000-02-12) (historical): Engine Oil Cooler Blower Shaft Bearings · Bell Helicopter Textron 407. Effective Mar 3, 2000
- [AD 99-23-18](https://openairdocs.org/ad/99-23-18) (historical): Revised Life Limit · Bell Helicopter Textron Canada 407. Effective Nov 30, 1999
- [AD 99-06-15](https://openairdocs.org/ad/99-06-15) (historical): Tail Rotor Blades · Bell Helicopter Textron 407. Effective Apr 22, 1999
- [AD 96-21-12 PL](https://openairdocs.org/ad/96-21-12-PL) (historical): Placard -- Inflight Engine Shut-downs · Bell Helicopter Textron 407

## Information bulletins (advisory) (6 in force)

- [SAIB SW-15-20](https://openairdocs.org/saib/SW-15-20): Air Conditioning System Wiring. Issued Aug 13, 2015
- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System. Issued Oct 3, 2012
- [SAIB SW-10-42R1](https://openairdocs.org/saib/SW-10-42R1): Emergency Float Kits. Issued Aug 11, 2010
- [SAIB SW-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits). Issued Aug 27, 2008
- [SAIB SW-05-70](https://openairdocs.org/saib/SW-05-70): . Issued Jul 21, 2005
- [SAIB SW-04-92](https://openairdocs.org/saib/SW-04-92): . Issued Sep 30, 2004
- [SAIB SW-10-42](https://openairdocs.org/saib/SW-10-42) (historical): Emergency Float Kits. Issued Aug 5, 2010

## NTSB investigations

None matched to N660AM.

## NTSB investigations on N660AM not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW97IA261](https://openairdocs.org/ntsb/FTW97IA261), Jul 10, 1997: Boeing 757-223 (N660AM), Dickinson, ND, incident, minor damage. Probable cause: an encounter with unforecast convection induced turbulence (CIT). Related factors were: the flight crew's improper evaluation of the weather, and an inaccurate preflight weather briefing by company…

## FAA accident and incident reports

None matched to N660AM.

## Reports on N660AM not matched to an aircraft (1)

They name N660AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19970710024449I](https://openairdocs.org/incident/19970710024449I), Jul 10, 1997: Boeing 757223 (N660AM), Denver, CO. Encountered clear air turbulence at cruise near iah. Landed. No structial damage. Passengers treated.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N660AM not matched to an aircraft (68, newest 50)

They name N660AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR AALA20150814003](https://openairdocs.org/sdr/AALA20150814003), Aug 10, 2015: ACM. SEIZED. DURING TAXI OUT, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. SECURING AIR CONDITIONING PACKS & RECIRCULATION FANS STOPPED SMOKE. FOUND RT ACM SEIZED. R & R AC
- [SDR AALA20150526005](https://openairdocs.org/sdr/AALA20150526005), May 25, 2015: CONNECTOR. LOOSE. EMERGENCY PATHWAY LIGHT ON SEAT 5 E - F INOPERATIVE. SECURED LOOSE CONNECTOR. SYS CHECKED NORMAL.
- [SDR AALA20140414003](https://openairdocs.org/sdr/AALA20140414003), Apr 14, 2014: SKIN. CRACKED. NUMBER 2 ENG PYLON HAS A CRACK INDICATION AT INBD UPPER AFT THRUST REVERSER HINGE MOUNT FASTENER HOLE, ALUMINUM SKIN LAYER ONLY. REMOVED CRACK BY ENLARGING HOLE
- [SDR AALA20130814001](https://openairdocs.org/sdr/AALA20130814001), Aug 13, 2013: PROBE. INOPERATIVE. AUS REPEAT ITEM. CREW REPORTED UNWANTED FUEL TRANSFER. AIRCRAFT FERRIED TO DFW FOR ADDITIONAL MAINTENANCE. REPLACED LT TANK COMPENSATOR NR 6 PROBE & DENSITOMETE
- [SDR AALA20130214011](https://openairdocs.org/sdr/AALA20130214011), Feb 14, 2013: RADAR. FAILED. DFW - INFLIGHT LAX-MIA. CREW REPORTED WEATHER RADAR FAILED. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR. SYSTEM GROUND CHECK NORMAL OPER
- [SDR AALA20121128010](https://openairdocs.org/sdr/AALA20121128010), Nov 28, 2012: HOUSING. CRACKED. MIA - CREW REPORTED RIGHT HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ENGINE DRIVEN
- [SDR AALA20120906015](https://openairdocs.org/sdr/AALA20120906015), Sep 5, 2012: SWITCH. MALFUNCTIONED. VVI INFLIGHT MIA-LPB CREW REPORTED SMOKE AND ODOR IN THE COCKPIT AND HIGH ALTITUDE SWITCH SHORTED. FLIGHT DIVERTED VVI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED
- [SDR AALA20120301022](https://openairdocs.org/sdr/AALA20120301022), Mar 1, 2012: PIN. BACKED OUT. JFK - CREW REPORTED RIGHT FUEL TANK AND TOTALIZER BLANKED DURING CLIMB. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. PLACARD RIGHT FUEL TANK INDICATION AND TOTA
- [SDR AALA20110916TUL08](https://openairdocs.org/sdr/AALA20110916TUL08), Sep 16, 2011: FLOORBEAM. CORRODED. IN THE CABIN AT STATION 1681 UNDER THE FORWARD LIP OF THE FLOORBEAM THE NUT PLATE MOUNT IS CORRODED AT RIGHT BUTTLINE 24. REMOVED DAMAGE AND INSTALLED DOUBLER P
- [SDR AALA20110915TUL09](https://openairdocs.org/sdr/AALA20110915TUL09), Sep 15, 2011: FRAME. CORRODED. FRAME AT STATION 1380 BETWEEN STRINGERS 27 AND 28 RIGHT CORRODED. INSTALLED REPAIR DOUBLER PER SRM 51-70-11-0G FIGURE 1.
- [SDR AALA20110915TUL08](https://openairdocs.org/sdr/AALA20110915TUL08), Sep 15, 2011: DOUBLER. DAMAGED. STATION 1400, STRINGER 24 LEFT EXTERNAL REPAIR DOUBLER DAMAGED. INSTALLED DOUBLER PER SRM 53-00-03-2R 1, EA PRELIM5 AND EA B757-53-019188.
- [SDR AALA20110915TUL07](https://openairdocs.org/sdr/AALA20110915TUL07), Sep 15, 2011: WEB. CRACKED. IN THE CABIN THE NEXT STRINGER END RUNOUT PIECE ABOVE STRINGER 12 RIGHT FORWARD OF THE RIGHT NUMBER 2 DOOR OPENING IS CRACKED IN THE OUTBOARD RADIUS AT THE JOGG
- [SDR AALA20110914TUL03](https://openairdocs.org/sdr/AALA20110914TUL03), Sep 14, 2011: STRINGER. CORRODED. LEVELING COMPOUND CRACKED AND DISTORTED INSIDE STRINGER 29 RIGHT AT STATION 1420. PERFORMED STRINGER SPLICE REPAIR PER SRM 53-00-03-2R 1.
- [SDR AALA20110912TUL06](https://openairdocs.org/sdr/AALA20110912TUL06), Sep 12, 2011: WEB. CORRODED. WEB CORRODED BETWEEN STATIONS 1600 AND 1620 AT STRINGER 28. ACCOMPLISHED REPAIR PER SRM 51-10-02-G9.
- [SDR AALA20110912TUL07](https://openairdocs.org/sdr/AALA20110912TUL07), Sep 12, 2011: ANGLE. CORRODED. IN THE CABIN AT THE RIGHT NUMBER 2 DOOR THRESHOLD THE Z ANGLE, TO THE CREASE BEAM, BETWEEN STATIONS 675 AND 755 IS CORRODED. REPLACED Z-ANGLE TO THE RIGHT CREAS
- [SDR AALA20110830TUL12](https://openairdocs.org/sdr/AALA20110830TUL12), Aug 30, 2011: ANGLE. CORRODED. MAIN CABIN, FLOOR STRUCTURE, CREASE ANGLE WEB CORRODED RIGHT SIDE STATIONS 940 TO 960. REPLACED WEB PER SRM 51-10-02-0G.
- [SDR AALA20110830TUL10](https://openairdocs.org/sdr/AALA20110830TUL10), Aug 30, 2011: FLOOR SUPPORT. CORRODED. FLOORBOARD SUPPORT CORRODED STATIONS 1640 TO 1661, WATERLINES 206 TO 208. INSTALLED FLOORBOARD SUPPORT AND VERTICAL STIFFENER PER SRM 51-10-02-0G.
- [SDR AALA20110829TUL13](https://openairdocs.org/sdr/AALA20110829TUL13), Aug 29, 2011: PRESSURE DECK. CORRODED. THE CABIN REAR PRESSURE DECK HAS A DOUBLER ON TOP THAT IS CORRODED IN SEVERAL PLACES BETWEEN STATIONS 1701 AND 1720 AND LEFT BUTTLINE 1 AND RIGHT BUTTLINE 54. I
- [SDR AALA20110829TUL04](https://openairdocs.org/sdr/AALA20110829TUL04), Aug 29, 2011: SLAT. CRACKED. NUMBER 10 SLAT COVE SKIN CRACKED AT OUTBOARD DRIVE TRACK. INSTALLED NEW SLAT SKIN PER ESO 90253.
- [SDR AALA20110826TUL08](https://openairdocs.org/sdr/AALA20110826TUL08), Aug 26, 2011: SUPPORT FITTING. DAMAGED. LEFT AFT G4 GALLEY MOUNT SUPPORT FITTING HAS TWO (2) DRILL STARTS IN UPPER SURFACE OF FITTING. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING IAW SRM 51-10-0
- [SDR AALA20110826TUL02](https://openairdocs.org/sdr/AALA20110826TUL02), Aug 26, 2011: SPAR. CRACKED. UPPER OUTER SPAR CHORD IS CRACKED ON RIGHT NUMBER 2 DOOR. ROUTED OUT DAMAGE, OVERSIZED 2 EACH OVERSIZED HOLES AND INSTALLED REPAIR PER ESO 90282 AND EA COMP- 52
- [SDR AALA20110825TUL05](https://openairdocs.org/sdr/AALA20110825TUL05), Aug 25, 2011: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED STATION 1580 TO 1600. REPLACED INTERCOSTAL PER SRM 51-10-02 OG.
- [SDR AALA20110825TUL03](https://openairdocs.org/sdr/AALA20110825TUL03), Aug 25, 2011: SKIN. DAMAGED. BLIND FASTENER AND DEEP BLEND ON NUMBER 8 SLAT UPPER SKIN. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER REPAIR PER AARD 57-43-00-1.
- [SDR AALA20110824TUL03](https://openairdocs.org/sdr/AALA20110824TUL03), Aug 24, 2011: WEB. CORRODED. WEB CORRODED STATION 1020. REPLACED WEB PER SRM 51-10-02-OG.
- [SDR AALA20110823TUL18](https://openairdocs.org/sdr/AALA20110823TUL18), Aug 23, 2011: CHANNEL. CORRODED. LEFT NUMBER 4 DOOR THRESHOLD HAT CHANNEL AT STATION 1672 LEFT BUTTLINE 60 CORRODED. INSTALLED NEW HAT CHANNEL AT LEFT NUMBER 4 DOOR AT STATION 1672 LEFT BUTTLIN
- [SDR AALA20110823TUL17](https://openairdocs.org/sdr/AALA20110823TUL17), Aug 23, 2011: TEE FITTING. CORRODED. T-FITTING LOCATED ON AFT DECK PLATE FRAME STATION 1720, LEFT BUTTLINE 5 CORRODED - ATTACHES IN BETWEEN THE 2 LEFT BATH TUB FITTINGS. INSTALLED T-ANGLE FITTING, 
- [SDR AALA20101110LGA01](https://openairdocs.org/sdr/AALA20101110LGA01), Nov 9, 2010: LIGHT. INOPERATIVE. ROW 16AB EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR ROW 16AB OVERHEAD BIN EMERGENCY LIGHT. OPS CHECK NORMAL.
- [SDR AALA20100201TUL07](https://openairdocs.org/sdr/AALA20100201TUL07), Feb 1, 2010: WEB. CORRODED. WEB CORRODED IN AFT CARGO FROM STATIONS 1360 TO 1380. WEB WAS REPLACED PER SRM 51-10-02-0G.
- [SDR AALA20100201TUL06](https://openairdocs.org/sdr/AALA20100201TUL06), Feb 1, 2010: FITTING. CORRODED. AFT CARGO TIE DOWN CORRODED. TIE DOWN ASSEMBLY WAS REPLACED.
- [SDR AALA20100201TUL02](https://openairdocs.org/sdr/AALA20100201TUL02), Feb 1, 2010: ANGLE. CORRODED. CHORD ANGLE CORRODED FROM STATIONS 730 TO 740. ANGLE WAS REPLACED PER 51-1-02-0G.
- [SDR AALA20100127TUL07](https://openairdocs.org/sdr/AALA20100127TUL07), Jan 27, 2010: SKIN. CRACKED. NUMBER 2 SLAT COVE SKIN IS CRACKED ADJACENT TO BOTH DRIVE TRACKS INBOARD OF ACCESS PANELS 524 CB AND OUTBOARD OF ACCESS PANELS 524 FB. STOPPED DRILLED CRACK AND
- [SDR AALA20091218JFK01](https://openairdocs.org/sdr/AALA20091218JFK01), Dec 18, 2009: LIGHT. INOPERATIVE. EMERGENCY LIGHTS AT SEAT 17B INOPERATIVE. REPLACED LIGHT ASSEMBLY.
- [SDR AALA20091216JFK01](https://openairdocs.org/sdr/AALA20091216JFK01), Dec 16, 2009: LIGHT. INOPERATIVE. SEAT MOUNTED EMERGENCY LIGHTS WILL NOT ILLUMINATE FROM ROW 16 THRU 25 ON TEST. FOUND EMERGENCY LIGHT AT SEAT 17DEF DEFECTIVE. REPLACED LIGHT ASSEMBLY.
- [SDR AALA20091109SJU01](https://openairdocs.org/sdr/AALA20091109SJU01), Nov 8, 2009: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT AT SEAT ROWS 16DEF TO 22DEF INOPERATIVE. REPLACED BATTERY PACK ABOVE SEAT ROW 20DEF.
- [SDR AALA20091101LGA04](https://openairdocs.org/sdr/AALA20091101LGA04), Nov 1, 2009: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS AT SEAT ROW 16 INOPERATIVE. REPLACED BATTERY PACK.
- [SDR AALA2009041000755](https://openairdocs.org/sdr/AALA2009041000755), Apr 10, 2009: WIRE. UNSECURE. DFW EMERGENCY LIGHT WIRE AT 3EF SIDEWALL NOT SECURED. RESECURED EMERGENCY LIGHT WIRE AT 3EF.
- [SDR AALA2009040800730](https://openairdocs.org/sdr/AALA2009040800730), Apr 8, 2009: MODULE. INOPERATIVE. SJU - RIGHT FLOOR EMERGENCY LIGHTS AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED NUMBER 2 DOOR OVERHEAD LIGHT MODULE.
- [SDR AALA200800328](https://openairdocs.org/sdr/AALA200800328), Feb 15, 2008: UNKNOWN. SMOKE. EWR INFLIGHT T164/15FEB - CREW REPORTS MID LAVATORY SMOKE DETECTORS ACTIVATED FOLLOWED BY SMOKE AND ODOR IN CABIN. LANDED EWR WITHOUT INCIDENT. REPLACED SMOKE D
- [SDR AALA200800240](https://openairdocs.org/sdr/AALA200800240), Feb 3, 2008: A/C PACK. CONTAMINATED. BWI INFLIGHT T775/03FEB LGA TO MIA AT FLIGHT LEVEL 400 FLIGHT ATTENDANT REPORTED AFT AND MID LAVATORY SMOKE DETECTORS ACTIVATED FOLLOWED BY VISIBLE SMOKE AND SM
- [SDR AALA200800230](https://openairdocs.org/sdr/AALA200800230), Feb 1, 2008: A/C PACK. CONTAMINATED. DTW INFLIGHT T398/01FEB ORD TO LGA - CREW REPORTED SMOKE IN CABIN WITH LEFT HYDRAULIC PRESSURE INDICATION AND RUDDER RATIO LIGHT ILLUMINATED. LANDED DTW WITHOUT
- [SDR AALA20070303](https://openairdocs.org/sdr/AALA20070303), Feb 8, 2007: LINE. LEAKING. CUN INFLIGHT T1688 - LEFT HYDRAULIC QUANTITY MESSAGE APPEARED FOLLOWED BY LEFT HYDRAULIC PRESSURE MESSAGE INDICATIONS. VERIFIED LOSS OF LEFT HYDRAULIC FLUID AND
- [SDR AALA20060726](https://openairdocs.org/sdr/AALA20060726), Sep 23, 2006: BULB. INOPERATIVE. DFW - EMERGENCY LIGHTS AT OVERHEAD ROWS 11 AND 34 INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT OVERHEAD ROWS 11 AND 34. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20060725](https://openairdocs.org/sdr/AALA20060725), Sep 23, 2006: LENS. BROKEN. DFW - AFT MOUNTED EMERGENCY LIGHT CLEAR PLASTIC SHROUD IS BROKEN. REPLACED CLEAR SHROUD FOR AFT MOUNTED EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20060724](https://openairdocs.org/sdr/AALA20060724), Sep 23, 2006: BULB. INOPERATIVE. DFW - EMERGENCY LIGHT AT LEFT HAND OVERWING EXIT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20060723](https://openairdocs.org/sdr/AALA20060723), Sep 23, 2006: BATTERY PACK. INOPERATIVE. DFW - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 15 TO 23 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 15 TO 23. SYSTEM
- [SDR AALA20060722](https://openairdocs.org/sdr/AALA20060722), Sep 23, 2006: PLACARD. MISSING. DFW - EMERGENCY EXIT LIGHT AT RIGHT HAND WING AFT MISSING DECAL. INSTALLED EXIT ARROW DECAL FOR EMERGENCY EXIT LIGHT AT RIGHT HAND WING AFT SYSTEM GROUND CHECKE
- [SDR AALA20060721](https://openairdocs.org/sdr/AALA20060721), Sep 23, 2006: BULB. INOPERATIVE. DFW - EMERGENCY EXIT LIGHT AT LEFT NR 1 DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20060501](https://openairdocs.org/sdr/AALA20060501), Jul 27, 2006: BATTERY PACK. DISCHARGED. DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AT STATION 1070 AND CHANGED WIRE HARNESS AT SEAT 17D FOR 
- [SDR AALA20060502](https://openairdocs.org/sdr/AALA20060502), Jul 27, 2006: LIGHT. INOPERATIVE. DFW - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. RELAMPED OUTSIDE EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050661](https://openairdocs.org/sdr/AALA20050661), Oct 11, 2005: BATTERY PACK. INOPERATIVE. SFO - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 16 TO 25. SYSTEM GROUND CHECKE

All 68: https://openairdocs.org/aircraft/N660AM/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (326, first 50)

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 airframe (Bell Textron Canada 407)

- [STC SR00222DE](https://openairdocs.org/stc/SR00222DE): Installation of a vapor cycle air conditioning system. Air Comm Corporation
- [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [STC SR00275DE](https://openairdocs.org/stc/SR00275DE): Installation of emergency medical interior system. Air Methods LLC
- [STC SR00368SE](https://openairdocs.org/stc/SR00368SE): Installation of a color video camera on either the left, right or both horizontal stabilizers. Turbolyft USA Corporation
- [STC SR00643SE](https://openairdocs.org/stc/SR00643SE): Installation of Geneva Aviation Video System. Turbolyft USA Corporation
- [STC SR12375NY](https://openairdocs.org/stc/SR12375NY): Demonstration of Aircraft Equipment Configurations Tolerance to Transmitting Portable Electronic Devices (TPED) in Part 27 Aircraft in accordance with the FAA-approved Rotorcraft Equipment Compatibility List (RECL). Kilroy Aviation, LLC
- [STC SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group Inc
- [STC SR00521SE](https://openairdocs.org/stc/SR00521SE): Installation of Geneva Aviation Audio System. AEM USA Inc
- [STC SR02301SE](https://openairdocs.org/stc/SR02301SE): Installation of Geneva Aviation 28 - 14 VDC Power Converter. AEM USA Inc
- [STC SR02445SE](https://openairdocs.org/stc/SR02445SE): Installation of P178 Failsafe Audio Mixer. AEM USA Inc
- [STC SR12385IB](https://openairdocs.org/stc/SR12385IB): Utility Basket Kit Installation. Alpine Aerotech LP
- [STC SR11898NY](https://openairdocs.org/stc/SR11898NY): Installation of Outerlink Corporation Air IP system. Sterling Helicopter
- [STC SR00279DE](https://openairdocs.org/stc/SR00279DE): Installation of Dual Aeronautical Accessories Nightscanner Searchlights. Air Methods LLC
- [STC SR12092IB](https://openairdocs.org/stc/SR12092IB): Manufacturing and Installation of Cargo Hold Nets. ICARUS AERO INC
- [STC SR12037DE](https://openairdocs.org/stc/SR12037DE): Installation of a Camera Mount. Century Helicopters Inc
- [STC SR04845NY](https://openairdocs.org/stc/SR04845NY): Installation of a Helifab East Equipment Mount. Helifab East LLC
- [STC SR04842NY](https://openairdocs.org/stc/SR04842NY): Installation of RMCI Inc. Expandable Rotorcraft Diagnostic System (XRDS). Sterling Helicopter
- [STC SR11869SE](https://openairdocs.org/stc/SR11869SE): Installation of Mechanical Specialties, LLC Human External Cargo (HEC) and non-HEC Hook System. Mechanical Specialties LLC
- [STC SR04047NY](https://openairdocs.org/stc/SR04047NY): Installation of a GPMS Foresight MX Condition Monitoring System (CMS). GPMS International Inc
- [STC SR00532SE](https://openairdocs.org/stc/SR00532SE): Installation of Certified Technology quick release door pins. Certified Technology
- [STC SR02827LA](https://openairdocs.org/stc/SR02827LA): Installation of Aerocraft's Bell 407 Slide Pull Kit (ARC-B407SP). Aerocraft Incorporated
- [STC SR04548CH](https://openairdocs.org/stc/SR04548CH): Installation of Appareo Systems AIRS-400 Flight Monitoring System. Appareo Systems
- [STC SR00425SE](https://openairdocs.org/stc/SR00425SE): Installation of a satellite phone. Turbolyft USA Corporation
- [STC SR00182IB](https://openairdocs.org/stc/SR00182IB): Installation of the Avidyne Integrated Flight Display (IFD) Navigator(s). Horizon Design Services Ltd
- [STC SR00891LA](https://openairdocs.org/stc/SR00891LA): Installation of aft utility mount. Airfilm Camera Systems LLC
- [STC SR00936LA](https://openairdocs.org/stc/SR00936LA): Installation of two-inch lift blocks. Airfilm Camera Systems LLC
- [STC SR01688LA](https://openairdocs.org/stc/SR01688LA): Installation of Aero Pacific Belly Utility Mount. Airfilm Camera Systems LLC
- [STC SR00335DE](https://openairdocs.org/stc/SR00335DE): Installation of snow pads. Dart Aerospace USA Inc
- [STC SR00611DE](https://openairdocs.org/stc/SR00611DE): Installation of a ram air vent control cable kit in. Dart Aerospace USA Inc
- [STC SR00682DE](https://openairdocs.org/stc/SR00682DE): Installation of Augmented Reality System. Dart Aerospace USA Inc
- [STC SR03474CH](https://openairdocs.org/stc/SR03474CH): Installation of Heli-Preheat Kit, p/n TSHB407-3083-115 for 115 volt application. Hartzell Propeller Inc
- [STC SR02120SE](https://openairdocs.org/stc/SR02120SE): Installation of Garmin GTN 6XX/7XX Navigation System. Garmin International Inc
- [STC SR00011DE](https://openairdocs.org/stc/SR00011DE): Installation of a monitor mount assembly to mount a video monitor. (206B S/N 914 and subs). Dart Aerospace USA Inc
- [STC SR00334DE](https://openairdocs.org/stc/SR00334DE): Installation of pneumatic door openers. Dart Aerospace USA Inc
- [STC SR00338DE](https://openairdocs.org/stc/SR00338DE): Installation of anti-torque extension adjustment system. Dart Aerospace USA Inc
- [STC SR00349DE](https://openairdocs.org/stc/SR00349DE): Installation of a searchlight. Dart Aerospace USA Inc
- [STC SR00449DE](https://openairdocs.org/stc/SR00449DE): Installation of removable dual pedal system. Dart Aerospace USA Inc
- [STC SR00486DE](https://openairdocs.org/stc/SR00486DE): Installation of mounting hardware in accordance with Paravion Technology Master Drawing List DL-407LS-100, Revision N/C, dated April 01, 2002, FAA approved dated January 27, 2003 or later FAA approved revision, and approval for the aircraft to be operated by a single pilot from the left crew seat. Dart Aerospace USA Inc
- [STC SR00654DE](https://openairdocs.org/stc/SR00654DE): Installation of Rotary Latch Seat Belts. Dart Aerospace USA Inc
- [STC SR00025DE](https://openairdocs.org/stc/SR00025DE): Installation of a shelf panel. Dart Aerospace USA Inc
- [STC SR00344DE](https://openairdocs.org/stc/SR00344DE): Installation of external mirror. Dart Aerospace USA Inc
- [STC SR00348DE](https://openairdocs.org/stc/SR00348DE): Installation of an infrared imaging system. Dart Aerospace USA Inc
- [STC SR00574DE](https://openairdocs.org/stc/SR00574DE): Installation of 407FL-100 FADEC/Check Instrument Auxiliary Annunciation System. Dart Aerospace USA Inc
- [STC SR00365BO](https://openairdocs.org/stc/SR00365BO): Installation of an Outerlink SATCOM Communications and Flight Data Monitoring System KIT B206-SAT-100 or KIT B407-SAT-100. Outerlink Corporation
- [STC SR09424RC](https://openairdocs.org/stc/SR09424RC): Installation of an OuterLink Automatic Flight Following System and optional Electronic Flight Bag provisions in accordance with OuterLink Corporation Master Installation List NL462065004, Revision J, dated June 29, 2007, or later FAA-approved revision. Outerink Corporation
- [STC SR03948NY](https://openairdocs.org/stc/SR03948NY): Installation of Frameless Crew Seat Cushion. HELIFAB East LLC
- [STC SR04669NY](https://openairdocs.org/stc/SR04669NY): Installation of Human External Cargo Y-Rope and Long-Line Kit. Boost Human External Cargo Systems Inc
- [STC SR04546AT](https://openairdocs.org/stc/SR04546AT): Installation of a Mission Console. Southeast Aerospace Incorporated
- [STC SR09441RC](https://openairdocs.org/stc/SR09441RC): Installation of Articulating Medical Litter. Helifab Inc
- [STC SR04458NY](https://openairdocs.org/stc/SR04458NY): Astronics (Max-Viz) 1200 or 1400 EVS Installation. Avio Design Group Inc

All 326: https://openairdocs.org/aircraft/N660AM/stcs.md

## Related

- Other Bell Textron Canada 407 aircraft: https://openairdocs.org/model/bell-textron-canada-407/aircraft.md
- The Rolls-Royce 250-C47E/4 engine: https://openairdocs.org/engine/rolls-royce-250-c47e-4.md

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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.