# N760AS: 2007 Cessna 560

- Status: Valid registration
- Airframe: [Cessna 560](https://openairdocs.org/model/cessna-560) (registry code 2076750, 11 seats)
- Engine: [Pratt & Whitney Canada PW535B](https://openairdocs.org/engine/pratt-whitney-canada-pw535b) (registry code 52184)
- Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE) (Textron Aviation Inc.), [TCDS E00053EN](https://openairdocs.org/tcds/E00053EN) (Pratt & Whitney Canada Inc.) (OpenAirDocs)
- Serial number: 560-0760
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 29, 2019
- Certificate issued: March 28, 2019
- Expires: March 31, 2029
- Mode S code: AA4199
- Registered owner: [Norsan Investors LLC](https://openairdocs.org/faa-owner/NORSAN%20INVESTORS%20LLC)
- Location: [Concord, CA](https://openairdocs.org/faa-place/CA/Concord)
- Owner type: LLC
- Owner's area on the map: 37.9932° N, 122.0356° W: Placed by OpenAirDocs at the center of ZIP code 94520, 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=760AS
- Page: https://openairdocs.org/aircraft/N760AS

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): 27 in force

### Matched by airframe (Cessna 560)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-11-09](https://openairdocs.org/ad/2025-11-09): Fire Protection · Textron 560 and 560XL. Effective Jul 11, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2015-17-12](https://openairdocs.org/ad/2015-17-12): Air conditioning · Freon air conditioning system (Textron STC SA3849SW or 3 others). Effective Sep 29, 2015
- [AD 2014-18-01](https://openairdocs.org/ad/2014-18-01): Navigation · Bombardier ATR42-200, ATR42-300, ATR42-320 and 23 more. Effective Oct 14, 2014
- [AD 2013-09-11](https://openairdocs.org/ad/2013-09-11): Air Conditioning · Cessna 500, 501, 550 and 5 more. Effective Jul 5, 2013
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2008-26-04](https://openairdocs.org/ad/2008-26-04): Airspeed placards · Cessna 560. Effective Jan 28, 2009
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2007-11-17](https://openairdocs.org/ad/2007-11-17): Wires for the positive and negative terminal studs of the engine and/or auxiliary power unit (APU) fire extinguishing bottles. · Cessna 500, 501, 550 and 5 more. Effective Jul 6, 2007
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-06-03](https://openairdocs.org/ad/2006-06-03): Airplane flight manual (AFM) · Cessna 500, 501, 550 and 3 more. Effective Apr 20, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2003-23-02](https://openairdocs.org/ad/2003-23-02): Ptich trim and autopilot servo · Cessna 560. Effective Nov 28, 2003
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 2000-03-09](https://openairdocs.org/ad/2000-03-09): Residual Ice · Cessna 560 and 560XL. Effective Apr 3, 2000
- [AD 97-05-03 R1](https://openairdocs.org/ad/97-05-03-R1): Global Positioning Systems · BAE Systems Avro 146-RJ100A, BAe 146-200A, Jetstream Model 4101 and 27 more. Effective Apr 20, 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 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [AD 98-04-38](https://openairdocs.org/ad/98-04-38): AFM - Limitations Section - Icing · Cessna 500, 501, 550 and 2 more. Effective Mar 25, 1998
- [AD 95-25-10](https://openairdocs.org/ad/95-25-10): Outflow/Safety Valve · Cessna 441, 500, 550 and 1 more. Effective Jan 22, 1996
- [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995
- [AD 94-01-04](https://openairdocs.org/ad/94-01-04): Traffic Alert and Collision Avoidance System · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 136 more. Effective Feb 4, 1994
- [AD 93-05-15](https://openairdocs.org/ad/93-05-15): Thrust Reverser Throttle Load Limiter · Cessna 500, 501, 550 and 4 more. Effective Apr 23, 1993
- [AD 90-06-13](https://openairdocs.org/ad/90-06-13): Vertical Gyro · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 14 more. Effective Mar 30, 1990
- [AD 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978

### Matched by engine (Pratt & Whitney Canada PW535B)

None in force.

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

- [AD 2007-23-13](https://openairdocs.org/ad/2007-23-13) (historical): Installing new minimum airspeed placards · Cessna 560. Effective Nov 30, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-04-10](https://openairdocs.org/ad/2006-04-10) (historical): Identification sleeves · Cessna Aircraft Company, The 500, 550, 560 and 3 more. Effective Mar 24, 2006
- [AD 96-24-06](https://openairdocs.org/ad/96-24-06) (historical): AFM - Limitations Section · Cessna Aircraft Company, The 560 Series (all). Effective Dec 10, 1996

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

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB NM-14-08](https://openairdocs.org/saib/NM-14-08): Fuselage: Aerodynamic Fairings. Issued Jan 23, 2014
- [SAIB CE-10-49R1](https://openairdocs.org/saib/CE-10-49R1): Equipment/Furnishings Drain Mast Heater. Issued Jan 5, 2011
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021
- [SAIB CE-10-49](https://openairdocs.org/saib/CE-10-49) (historical): Equipment/Furnishings Drain Mast Heater. Issued Sep 23, 2010

## NTSB investigations

None matched to N760AS.

## FAA accident and incident reports

None matched to N760AS.

## 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 N760AS not matched to an aircraft (283, newest 50)

They name N760AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ASAA2017050420653](https://openairdocs.org/sdr/ASAA2017050420653), May 4, 2017: DOOR. OUT OF ADJUST. L-1 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. ADJUSTED L1 DOOR, TORQUE CHECKED WITHIN LIMITS IAW AMM 52-11-00-705-007, AND 52-11-00-755-051.
- [SDR ASAA2017041220447](https://openairdocs.org/sdr/ASAA2017041220447), Apr 12, 2017: LENS. DETACHED. EXIT LIGHT COVER NEAR L1 DOOR DETACHED. ACFT GROUNDED. REATTACHED EXIT LIGHT COVER NEAR L1 DOOR. OK FOR SERVICE.
- [SDR ASAA2017032921279](https://openairdocs.org/sdr/ASAA2017032921279), Mar 29, 2017: SHEAR TIE. CORRODED. SHEAR TIE AT BS 480, BL 0 SHOWS SIGNS OF CORROSION. ACFT GROUNDED. CUT OFF LOWER LEG OF SHEAR TIE FOR REPAIR IAW SRM 53-00-07-2R, REPAIR 17. REPLACED SHEAR TIE.
- [SDR ASAA2017032621296](https://openairdocs.org/sdr/ASAA2017032621296), Mar 26, 2017: SKIN. CRACKED. WHILE ACCOMPLISHING T/C AD 20161004-400-53-1 SKIN CRACK FOUND AT THE FWD END OF NR 2 VHF ANTENNA. PERFORMED HFEC, MEASURED CRACK TO BE 4.5" IN LENGTH AROUND LEF
- [SDR ASAA2017032520356](https://openairdocs.org/sdr/ASAA2017032520356), Mar 25, 2017: FRAME. CRACKED. FRAME BS 500 VERTICAL WEB IS CRACKED IN TWO PLACES, RBL 1.5 & LBL 1.5. ACFT GROUNDED. CONFIRMED WITH HFEC. REMOVED THE FRAME. DRILLED & INSTALLED A NEW FRAME IA
- [SDR ASAA2016042016616](https://openairdocs.org/sdr/ASAA2016042016616), Apr 20, 2016: SKIN. CRACKED. FUSELAGE SKIN IS CRACKED AT THE R1 DOOR LOWER HINGE CUTOUT NDT HAS VERIFIED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW 53-10-01-2R-15. THIS IS A CAT B REPAIR WI
- [SDR ASAA2016042016592](https://openairdocs.org/sdr/ASAA2016042016592), Apr 20, 2016: SUPPORT FITTING. CRACKED. RIGHT WING LANDING GEAR BEAM SUPPORT FITTING CRACKED AT UPPER FASTENER HOLE 4TH FROM INBD. ACFT GROUNDED. ACCOMPLISHED INSPECTIONS TO RT MLG BEAM AFT SUPPORT FI
- [SDR ASAA2016042016578](https://openairdocs.org/sdr/ASAA2016042016578), Apr 20, 2016: FRAME. CRACKED. FS 500B IS CRACKED AT WIRE PENETRATION HOLE BELOW STR 20L. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-13. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 6600
- [SDR ASAA2016042016577](https://openairdocs.org/sdr/ASAA2016042016577), Apr 20, 2016: FRAME. CRACKED. FS 500F IS CRACKED AT WIRE PENETRATION HOLE BELOW STR 20L. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-13. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 6600
- [SDR ASAA2016041916604](https://openairdocs.org/sdr/ASAA2016041916604), Apr 19, 2016: RIB. CRACKED. RT WING RT WS 135 RIB CHORD CRACKED. ACFT GROUNDED. REPAIRED RT WS 135 RIB CHORD IAW EA 400-57EA-17072.
- [SDR ASAA2016041816629](https://openairdocs.org/sdr/ASAA2016041816629), Apr 18, 2016: SKIN. DELAMINATED. NR 3 SLAT OTBD LOWER T/E DELAMINATED. ACFT GROUNDED. BONDED PERMANENT REPAIR TO NR 3 SLAT, OTBD LOWER T/E DELAMINATION IAW BOEING SRM 51-70-10-2R-4, REPAIR NR 4
- [SDR ASAA2016021515459](https://openairdocs.org/sdr/ASAA2016021515459), Feb 15, 2016: LENS. DETACHED. F/A REPORTED THAT EXIT SIGN ROW 16 DEF FELL DOWN DURING FLIGHT/IS NOT SECURE. ACFT GROUNDED. R & R EXIT SIGN ASSY ON WALL OF ROW 16 DEF AS REQUIRED. OPS CHECKED
- [SDR ASAA2015120814250](https://openairdocs.org/sdr/ASAA2015120814250), Dec 8, 2015: COVER. MISSING. F/A REPORTS EMERGENCY EXIT LIGHT COVER MISSING AT ROW 17 RT SIDE. ACFT GROUNDED. INSTALLED NEW EMERGENCY EXIT LIGHT COVER.
- [SDR ASAA2015062712244](https://openairdocs.org/sdr/ASAA2015062712244), Jun 27, 2015: COVER. DETACHED. L1 DOOR EMERGENCY EXIT SIGN COVER FELL OFF. ACFT GROUNDED. REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSY IAW WDM 33-51-12. OPS TEST NORMAL.
- [SDR ASAA2015051514492](https://openairdocs.org/sdr/ASAA2015051514492), May 15, 2015: SKIN. GOUGED. LEFT FUSELAGE SKIN AT GROUND A/C DOOR CUTOUT IS GOUGED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT AC DOOR CUTOUT IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B REPA
- [SDR ASAA2015051511870](https://openairdocs.org/sdr/ASAA2015051511870), May 15, 2015: ANGLE. CORRODED. KEEL BEAM INTERIOR AFT ANGLE CORRODED, FWD ACCESS AREA AFT OF ROTATING BEACON. ACFT GROUNDED. REMOVED CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-12-1A
- [SDR ASAA2015051511869](https://openairdocs.org/sdr/ASAA2015051511869), May 15, 2015: SKIN. GOUGED. LT FUSELAGE SKIN AT GROUND, ACFT DOOR CUTOUT IS GOUGED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT ACFT DOOR CUTOUT IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B RE
- [SDR ASAA2015051511868](https://openairdocs.org/sdr/ASAA2015051511868), May 15, 2015: DOUBLER. CORRODED. LOWER ROTATING BEACON ATTACH DOUBLER CORRODED, INSIDE KEEL BEAM FWD ACCESS AREA. ACFT GROUNDED. REMOVED CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-12-
- [SDR ASAA2015051411886](https://openairdocs.org/sdr/ASAA2015051411886), May 14, 2015: SKIN. CRACKED. R2 DOOR CRACKED IN SKIN FWD LWR CORNER NDT VERIFIED. ACFT GROUNDED. REPAIRED R2 CRACKED FWD LOWER SKIN IAW SRM 53-00-01-2R-32, REPAIR 32. THIS REPAIR IS A CATEG
- [SDR ASAA2015051411872](https://openairdocs.org/sdr/ASAA2015051411872), May 14, 2015: FLOORBEAM. CRACKED. FOUR CRACKS IN BBL 0.07 FLOORBEAM WEB LT SIDE AT BS 710.1. ACFT GROUNDED. REPAIRED BBL 0.07 FLOORBEAM WEB LT SIDE AT BS 710 IAW ASA T/C AD20080421-400-57-6.
- [SDR ASAA2015051411871](https://openairdocs.org/sdr/ASAA2015051411871), May 14, 2015: CHANNEL. CORRODED. AFT WASTE WATER DRAIN MAST CHANNEL IS CORRODED. ACFT GROUNDED. REPAIRED THE AFT WASTE WATER DRAIN MAST CHANNEL IAW EA 400, 53EA, 15136.
- [SDR ASAA2015011010211](https://openairdocs.org/sdr/ASAA2015011010211), Jan 10, 2015: ARM. OUT OF ADJUST. L1 DOOR IS DIFFICULT TO LATCH CLOSE. ACFT GROUNDED. ADJUSTED L1 DOOR GUIDE ARM IAW MM 52-11-00-705-007 PG 2, STEPS 3H (1 AND 2).
- [SDR ASAA2014031307227](https://openairdocs.org/sdr/ASAA2014031307227), Mar 13, 2014: FLOOR PANEL. CRACKED. DENT FOUND IN FWD CARGO BAY FLOOR PANEL AT APPROXIMATELY FS 500 WITH SMALL CRACK APPROX 1 INCH IN LENGTH. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL IAW SRM 51-4
- [SDR ASAA2014022606996](https://openairdocs.org/sdr/ASAA2014022606996), Feb 26, 2014: FRAME. CRACKED. FRAME BS 500F RT SIDE IS CRACKED AT 1 INCH WIRE PENETRATION HOLE EXTENDING INBD FROM EDGE OF HOLE APPROX .75" IN THE FWD CARGO BAY. ACFT GROUNDED. REPAIRED CRAC
- [SDR ASAA2014022507086](https://openairdocs.org/sdr/ASAA2014022507086), Feb 25, 2014: STIFFENER. CORRODED. APU BAY INLET CUTOUT AFT OTBD ANGLE CORRODED FOUND DURING AFT STRAP REPAIR. ACFT GROUNDED. APU BAY INLET CUTOUT AFT OTBD ANGLE REMOVED. FABRICATED NEW AND INSTA
- [SDR ASAA2014022407153](https://openairdocs.org/sdr/ASAA2014022407153), Feb 24, 2014: STRINGER. CORRODED. APU INLET DUCT CUTOUT LOWER STRINGER CORRODED. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014022407152](https://openairdocs.org/sdr/ASAA2014022407152), Feb 24, 2014: CHANNEL. CRACKED. FWD CARGO BAY CENTER CHANNEL BS 500A FOR VHF NR 1 ANTENNA IS CRACKED. ACFT GROUNDED. REMOVED, FABRICATED NEW AND INSTALLED NEW CHANNEL IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014022407119](https://openairdocs.org/sdr/ASAA2014022407119), Feb 24, 2014: ATTACH BRACKET. CRACKED. FWD CARGO BAY CENTER CHANNEL FOR NR 1 VHF ANTENNA STA 500A AFT ATTACH BRACKET IS CRACKED. ACFT GROUNDED. REMOVED ATTACH BRACKET FOR NR 1 VHF ANTENNA SUPPORT CHA
- [SDR ASAA2014022107071](https://openairdocs.org/sdr/ASAA2014022107071), Feb 21, 2014: FLOOR SUPPORT. CORRODED. DURING REMOVAL OF BS 500G BULKHEAD LOWER CENTER ANGLE FOUND FLOOR SUPPORT CORRODED AT RBL 13.8. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE 
- [SDR ASAA2014021907461](https://openairdocs.org/sdr/ASAA2014021907461), Feb 19, 2014: FRAME. CRACKED. BS 348.2 FRAME LOWER ANGLE WAS FOUND CRACKED AT LWR FASTENER HOLE. ACFT GROUNDED. R & R FRAME IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014021907229](https://openairdocs.org/sdr/ASAA2014021907229), Feb 19, 2014: SUPPORT FRAME. CRACKED. UPON REMOVAL OF THE L1 MOP SILL THE BS 348.20 FRAME LOWER ANGLE WAS FOUND CRACKED AT LOWER FASTENER HOLE. ACFT GROUNDED. R & R FRAME ANGLE IAW SRM 51-40-02-0G-0
- [SDR ASAA2014021407120](https://openairdocs.org/sdr/ASAA2014021407120), Feb 14, 2014: SHEAR TIE. CORRODED. AFT CARGO PIT SHEAR TIE AT BL0, BS 867 CORRODED. ACFT GROUNDED. SHEAR TIE REPAIR IAW SRM 53-00-07-2R-17, REPAIR 17.
- [SDR ASAA2014021407095](https://openairdocs.org/sdr/ASAA2014021407095), Feb 14, 2014: SHEAR TIE. CORRODED. SHEAR TIE, BL 0 CENTER AND RT IN AFT CARGO BAY CORRODED. ACFT GROUNDED. SHEAR TIE REPAIRED IAW SRM 53-00-07-2R-7, REPAIR 7 AND 53-00-07-2R-17, REPAIR 17 .
- [SDR ASAA2014021407084](https://openairdocs.org/sdr/ASAA2014021407084), Feb 14, 2014: ANGLE. CORRODED. AFT CARGO BAY LT BS 827-947, S25L, FLOOR TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS, FOUND TO BE OUT 
- [SDR ASAA2014021407072](https://openairdocs.org/sdr/ASAA2014021407072), Feb 14, 2014: FLOOR SUPPORT. CORRODED. AFT CARGO BAY BS 907, S26R FLOOR SUPPORT CORRODED AT NUTPLATE. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1, FIG 101. RE
- [SDR ASAA2014021307179](https://openairdocs.org/sdr/ASAA2014021307179), Feb 13, 2014: FLOORBEAM. CORRODED. FLOORBEAM BS 947.5 RBL 12 AREA HAS CORROSION. ACFT GROUNDED. REPAIRED FLOORBEAM IAW EA 12265 REV.
- [SDR ASAA2014021307121](https://openairdocs.org/sdr/ASAA2014021307121), Feb 13, 2014: ATTACH ANGLE. CORRODED. AFT CARGO LT LOWER SIDEWALL LOWER ATTACHMENT LANDING CORRODED AROUND SCREW HOLES IN MULTIPLE AREAS FROM BS 727E-767. ACFT GROUNDED. REMOVED CORRODED AND CHECKED
- [SDR ASAA2014021307088](https://openairdocs.org/sdr/ASAA2014021307088), Feb 13, 2014: ATTACH ANGLE. CORRODED. AFT CARGO, LT LOWER SIDEWALL, ATTACHMENT LANDING CORRODED AROUND SCREW HOLES IN MULTIPLE AREAS FROM FWD BULKHEAD OF AFT CARGO TO FRAME 727 F. ACFT GROUNDED. REM
- [SDR ASAA2014021307085](https://openairdocs.org/sdr/ASAA2014021307085), Feb 13, 2014: ATTACH ANGLE. CORRODED. AFT CARGO RT LOWER SIDEWALL LOWER ATTACHMENT LANDING CORRODED AROUND SCREW HOLES IN MULTIPLE AREAS FROM BS 727D-727 F. ACFT GROUNDED. REMOVED, FABRICATED AND IN
- [SDR ASAA2014021207228](https://openairdocs.org/sdr/ASAA2014021207228), Feb 12, 2014: STRINGER. CRACKED. R1 DOOR STRINGER CRACKED AT FS 294.5 AND S14R. ACFT GROUNDED. R & R R1 DOOR STRINGER IAW SRM-51-40-02.
- [SDR ASAA2014021207226](https://openairdocs.org/sdr/ASAA2014021207226), Feb 12, 2014: TRANSITION PANEL. CORRODED. TRANSITION PANEL ON LT SIDE AT FS 500G IS CORRODED. ACFT GROUNDED. TRANSITION PANEL REMOVED, FABRICATED NEW AND INSTALLED IAW SRM 51-40-02.
- [SDR ASAA2014021206974](https://openairdocs.org/sdr/ASAA2014021206974), Feb 12, 2014: STRINGER. CRACKED. R2 DOOR STRINGER 11R CRACKED AT BS 294.5. ACFT GROUNDED. R & R R1 DOOR STRINGER ANGLE IAW SRM 51-40-02.
- [SDR ASAA2014021206973](https://openairdocs.org/sdr/ASAA2014021206973), Feb 12, 2014: STRINGER. CRACKED. R1 DOOR STRINGER CRACKED AT FS 294.5 AND S-14R. ACFT GROUNDED. R & R R1 DOOR STRINGER ANGLE AT FS 294.5 AND S-14R IAW SRM 51-40-02.
- [SDR ASAA2014021206972](https://openairdocs.org/sdr/ASAA2014021206972), Feb 12, 2014: STRINGER. CRACKED. R1 DOOR STRINGER CRACKED AT FS 294.5 AND S-13R. ACFT GROUNDED. R & R R1 DOOR STRINGER ANGLE AT FS 294.5 AND S-13R IAW SRM 51-40-02.
- [SDR ASAA2014021206912](https://openairdocs.org/sdr/ASAA2014021206912), Feb 12, 2014: STRINGER. CRACKED. R1 DOOR STRINGER 12R CRACKED AT BS 294.5. ACFT GROUNDED. R & R R1 DOOR STRINGER IAW SRM 51-40-02.
- [SDR ASAA2014021206905](https://openairdocs.org/sdr/ASAA2014021206905), Feb 12, 2014: STRINGER. CRACKED. R1 DOOR STRINGER CRACKED AT FS 294.5 AND S10R. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02.
- [SDR ASAA2014021107177](https://openairdocs.org/sdr/ASAA2014021107177), Feb 11, 2014: FLOOR PANEL. CORRODED. AFT CARGO BAY NR 5 FLOOR PANEL HAS MANY AREAS OF CORROSION ON LOWER SURFACE. ACFT GROUNDED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR PA
- [SDR ASAA2014021107171](https://openairdocs.org/sdr/ASAA2014021107171), Feb 11, 2014: FLOORBOARD. CORRODED. AFT CARGO BAY NR 4 FLOORBOARD CORRODED AROUND HOLES. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW FLOORBOARD IAW SRM 53-60-53-1A-1, FIG 1 AND SRM 51-40-05
- [SDR ASAA2014021107170](https://openairdocs.org/sdr/ASAA2014021107170), Feb 11, 2014: FLOOR PANEL. CORRODED. FWD CARGO BAY NR 4 FLOOR PANEL HAS CORRODED ON LWR AFT SIDE. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53-1A-1, FIG 101. FABR
- [SDR ASAA2014021107167](https://openairdocs.org/sdr/ASAA2014021107167), Feb 11, 2014: FLOOR PANEL. CORRODED. AFT CARGO BAY NR 1 FLOOR PANEL HAS CORROSION AROUND HOLES. ACFT GROUNDED. BLENDED CORRODED AREA FOUND TO BE OUT OF LIMITS. FABRICATED, LOCATED AND DRILLED NEW F

All 283: https://openairdocs.org/aircraft/N760AS/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (258, 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 (Cessna 560)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST01823WI](https://openairdocs.org/stc/ST01823WI): Installation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders with ADS-B Out. Blackhawk Aerospace Technologies Inc
- [STC ST04201NY](https://openairdocs.org/stc/ST04201NY): Installation of ENode Engine Data Acquisition Unit & IONode Digital Data Recorder. TBO Extension, LLC
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST02016WI](https://openairdocs.org/stc/ST02016WI): Installation of the Meggitt Wireless Tire Pressure Sensor. 3S Certification LLC
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST02718LA](https://openairdocs.org/stc/ST02718LA): Modification to replace the existing standby instrument. Acron Aviation Inc
- [STC ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc
- [STC ST09854AC](https://openairdocs.org/stc/ST09854AC): Installation of a Lumin Media Server. L2 Aviation
- [STC ST155CH](https://openairdocs.org/stc/ST155CH): Installation of BF Goodrich Avionics systems TCAS791 traffic alert and collison avoidance system I (TCASI). Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST04742NY](https://openairdocs.org/stc/ST04742NY): Installation of SkyVue 1000 Cockpit Upgrade including dual Avidyne IFD540 FMS with LPV i. Aerospace Design & Compliance LLC
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST02427LA](https://openairdocs.org/stc/ST02427LA): Installation of Dual Garmin GTN 6XX/7XX Series Global Navigation System with Structural Antenna and WAAS approval; Garmin GMA 35 Audio Panel; and Dual Garmin GTX 33 Mode S Transponders, Weather Radar, and ADS-B Link. JETTECH LLC
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST02029WI](https://openairdocs.org/stc/ST02029WI): Installation of Garmin GI 275 Standby Instrument and GSB 15 USB Port. Blackhawk Aerospace Technologies
- [STC ST00116MC](https://openairdocs.org/stc/ST00116MC): Installation of an Avionics Upgrade consisting of a Data-Link System, a High Frequency Radio System, and a Tactical Air Navigation System. L3Harris Technologies Integrated Systems L.P
- [STC ST00129MC](https://openairdocs.org/stc/ST00129MC): Installation of a Cabin Communication System consisting of a Satellite Communications System and an In-Flight Internet System. L3Harris Technologies Integrated Systems L.P
- [STC ST11217DS](https://openairdocs.org/stc/ST11217DS): Installation of search and rescue upgrade to the factory installed Rockwell Collins Pro Line 21 Flight Management System (FMS-3000). Textron Aviation Inc
- [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [STC ST00011WI](https://openairdocs.org/stc/ST00011WI): Installation of Concorde RG380E/40 and 40B battery. Aero-Mach Wilco LLC
- [STC ST01994WI](https://openairdocs.org/stc/ST01994WI): Installation of Honeywell Primus Elite Enhanced Functionality Modification and Honeywell Primus Elite Drop-in Modification. TurboJet Engineering Pty Ltd
- [STC ST00212MC](https://openairdocs.org/stc/ST00212MC): ARC-210 RT-2036(C) Network Communications Airborne Radio (Provisions). Meta Special Aerospace
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST04473CH](https://openairdocs.org/stc/ST04473CH): Installation of a Honeywell RDR -7000 Weather Radar System. Honeywell International Inc
- [STC ST03035NY](https://openairdocs.org/stc/ST03035NY): Replacement of certain Goodrich pneumatic deicer boots. SMR Technologies Inc
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC ST01149WI](https://openairdocs.org/stc/ST01149WI): Installation of IS&S Air Data System with Reduced Vertical Separation Minimum (RVSM) compliant Dual Air Data System. Blackhawk Aerospace Technologies Inc
- [STC ST01252WI](https://openairdocs.org/stc/ST01252WI): Reduced Vertical Separation Minimum (RVSM) group airworthiness approval of Cessna Model S550 and 560 Citation Aircraft in accordance with Columbia Avionics, Inc. Master Document List RVSM Group Approval Cessna S550/560, Document No. 30141243, Rev. 3, dated June 4, 2004, or later FAA approved revision. Blackhawk Aerospace Technologies Inc
- [STC ST01466WI](https://openairdocs.org/stc/ST01466WI): Installation of Universal Avionics EFI-890R Flat Panel EFIS System. Blackhawk Aerospace Technologies Inc
- [STC ST01691WI](https://openairdocs.org/stc/ST01691WI): Installation of Garmin GTN Series GPS/Comm/Nav Systems with optional Garmin GDL-69/A XM Weather Data Link, GTX-33 Series Transponders and optional Bendix/King KMR-675 Marker Beacon Receiver. Blackhawk Aerospace Technologies Inc
- [STC ST01929WI](https://openairdocs.org/stc/ST01929WI): Installation of Garmin G700 TXi EFIS system and GWX 75 Weather Radar. Blackhawk Aerospace Technologies Inc
- [STC ST04258CH](https://openairdocs.org/stc/ST04258CH): Installation of Gogo Business Aviation Avance High Speed Data System. Ross Aviation Flight Maintenance
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04510CH](https://openairdocs.org/stc/ST04510CH): Installation of a Digital Flight Data Recorder (DFDR) System in accordance with Dan Buzz & Associates LLC, Master Data List, Document No. DB2006001, Revision B, dated February 23, 2021, or later FAA approved revision. Dan Buzz & Associates LLC
- [STC ST02642AT](https://openairdocs.org/stc/ST02642AT): Installation of a RVSM Air Data System. Carlisle Interconnect Technologies Inc
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc
- [STC ST00539LA](https://openairdocs.org/stc/ST00539LA): ONE ONLY STC, SN 560-0004: Installation of Honeywell Differential Global Positioning System (DGPS) Airborne System (SLS-2000). Honeywell International Inc
- [STC ST01069LA](https://openairdocs.org/stc/ST01069LA): Installation of Honeywell/Racal SCS-1000 Mini-M Aero Satellite Communication System. Honeywell International Inc

All 258: https://openairdocs.org/aircraft/N760AS/stcs.md

## Related

- Other Cessna 560 aircraft: https://openairdocs.org/model/cessna-560/aircraft.md
- The Pratt & Whitney Canada PW535B engine: https://openairdocs.org/engine/pratt-whitney-canada-pw535b.md

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