# N485HA: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55130
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 18, 2001
- Certificate issued: June 28, 2011
- Expires: June 30, 2027
- Mode S code: A5FBDC
- Registered owner: [Hawaiian Airlines Inc](https://openairdocs.org/faa-owner/HAWAIIAN%20AIRLINES%20INC)
- Location: [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu)
- Owner type: Corporation
- Owner's area on the map: 21.3477° N, 157.8767° W: Placed by OpenAirDocs at the center of ZIP code 96819, 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=485HA
- Page: https://openairdocs.org/aircraft/N485HA

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 Rolls-Royce BR-700 model are included.

## ADs that may apply (OpenAirDocs): 78 in force

### Matched by airframe (Boeing 717-200)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [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 2025-21-05](https://openairdocs.org/ad/2025-21-05): Landing Gear · Boeing 717-200. Effective Jan 2, 2026
- [AD 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025
- [AD 2024-21-01](https://openairdocs.org/ad/2024-21-01): Wings · Boeing 717-200. Effective Nov 7, 2024
- [AD 2024-20-02](https://openairdocs.org/ad/2024-20-02): Fuselage · Boeing 717-200, DC-9-11, DC-9-12 and 16 more. Effective Oct 21, 2024
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [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 2021-12-12](https://openairdocs.org/ad/2021-12-12): Wings · Boeing 717-200. Effective Jul 29, 2021
- [AD 2021-02-16](https://openairdocs.org/ad/2021-02-16): Ice and rain protection · Boeing 717-200. Effective Mar 30, 2021
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-10-08](https://openairdocs.org/ad/2018-10-08): Stabilizers · Boeing 717-200. Effective May 31, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-01-03](https://openairdocs.org/ad/2017-01-03): Standard practices/structures · Boeing 717-200. Effective Mar 14, 2017
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-05-22](https://openairdocs.org/ad/2014-05-22): Fuselage · Boeing 717-200. Effective Apr 15, 2014
- [AD 2013-19-22](https://openairdocs.org/ad/2013-19-22): JASC Code 53, Fuselage · Boeing 717-200. Effective Nov 6, 2013
- [AD 2012-12-09](https://openairdocs.org/ad/2012-12-09): Horizontal Stabilizer Structure · Boeing 717-200. Effective Jul 23, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-07-07](https://openairdocs.org/ad/2009-07-07): Main landing gear (MLG) · Boeing 717-200. Effective May 5, 2009
- [AD 2008-18-05](https://openairdocs.org/ad/2008-18-05): Elevator standby cable system · Boeing 717-200. Effective Oct 14, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-11-06](https://openairdocs.org/ad/2008-11-06): Gray water drain hose · Boeing 717-200. Effective Jul 3, 2008
- [AD 2008-02-12](https://openairdocs.org/ad/2008-02-12): Center fuel tank · Boeing 717-200. Effective Feb 28, 2008
- [AD 2008-02-08](https://openairdocs.org/ad/2008-02-08): Main fuel tanks · Boeing 717-200. Effective Feb 26, 2008
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-03](https://openairdocs.org/ad/2007-19-03): Power conversion distribution unit (PCDU) · Boeing 717-200. Effective Oct 17, 2007
- [AD 2007-17-11](https://openairdocs.org/ad/2007-17-11): In-line fuel float switch fuses · Boeing 717-200. Effective Oct 2, 2007
- [AD 2007-13-09](https://openairdocs.org/ad/2007-13-09): Fuel boost pump container · Boeing 717-200. Effective Aug 3, 2007
- [AD 2007-13-01](https://openairdocs.org/ad/2007-13-01): Wiring of the first officer's pitot static heater system · Boeing 717-200. Effective Jul 25, 2007
- [AD 2007-05-06](https://openairdocs.org/ad/2007-05-06): Bulkhead nipple assemblies of the left and right wing vent boxes · Boeing 717-200. Effective Apr 9, 2007
- [AD 2006-20-12](https://openairdocs.org/ad/2006-20-12): Replaces clamp bases on fuel tank vent systems. · Boeing 717-200. Effective Nov 8, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2005-16-08](https://openairdocs.org/ad/2005-16-08): Oxygen release system in the forward cabin · Boeing 717-200. Effective Sep 13, 2005
- [AD 2005-11-03](https://openairdocs.org/ad/2005-11-03): Brake fuses. · Boeing 717-200. Effective Jul 1, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-08-02](https://openairdocs.org/ad/2004-08-02): Left and right hand horizontal stabilizer hinge fitting bolts · Boeing 717-200. Effective May 19, 2004
- [AD 2004-03-21](https://openairdocs.org/ad/2004-03-21): Inboard Ends of Outer Skin Panels of Horizontal Stabilizer at Station Xh=7.234 · Boeing 717-200. Effective Mar 17, 2004
- [AD 2004-01-15](https://openairdocs.org/ad/2004-01-15): Auxiliary hydraulic pump · Boeing 717-200. Effective Feb 17, 2004
- [AD 2003-14-05](https://openairdocs.org/ad/2003-14-05): Main spoiler actuators · Boeing 717-200. Effective Jul 31, 2003
- [AD 2003-10-10](https://openairdocs.org/ad/2003-10-10): Rear spar · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-10-08](https://openairdocs.org/ad/2003-10-08): Upper center fuselage · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-04-24](https://openairdocs.org/ad/2003-04-24): Support Fitting Assemblies and Stop Pads of Main Spoiler Actuators · Boeing 717-200. Effective Mar 17, 2003
- [AD 2002-21-01](https://openairdocs.org/ad/2002-21-01): Electrical terminal contact pins · Airbus A319-111, A319-112, A319-113 and 66 more. Effective Nov 27, 2002
- [AD 2002-16-09](https://openairdocs.org/ad/2002-16-09): Solenoid operated shut-off valve (SOV) · Boeing 717-200. Effective Sep 3, 2002
- [AD 2002-14-16](https://openairdocs.org/ad/2002-14-16): Spoiler Hold-Down Actuator Supports on Left and Right Wing Rear Spar · Boeing 717-200. Effective Aug 16, 2002
- [AD 2001-18-11](https://openairdocs.org/ad/2001-18-11): Rudder Trim · Boeing 717-200. Effective Oct 1, 2001

### Matched by engine (Rolls-Royce BR-700 series)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

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

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2020-03-20](https://openairdocs.org/ad/2020-03-20) (historical): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Feb 18, 2020
- [AD 2016-09-05](https://openairdocs.org/ad/2016-09-05) (historical): Stabilizers · Boeing 717-200. Effective Jun 8, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2007-11-13](https://openairdocs.org/ad/2007-11-13) (historical): Principal structural elements (PSEs) · Boeing 717-200. Effective Jun 29, 2007
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2003-17-01](https://openairdocs.org/ad/2003-17-01) (historical): Flap system · McDonnell Douglas 717-200. Effective Sep 23, 2003
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

All 92: https://openairdocs.org/aircraft/N485HA/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## NTSB investigations

None matched to N485HA.

## FAA accident and incident reports

None matched to N485HA.

## Service difficulty reports (65, 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 ASAA2026031463860](https://openairdocs.org/sdr/ASAA2026031463860), Mar 14, 2026: WINDSHEAR SYS. FALSE INDICATION. -RTO- REJECTED TAKEOFF TWICE FOR WINDSHEAR WARNINGS. 1ST AT 85 KIAS. 2ND AT 100 KIAS. GROUNDED - YES. A/C INSP C/W PER FIM 05-50- TASK 809. NO DEFECTS NOTED. FC
- [SDR HALA20251015052](https://openairdocs.org/sdr/HALA20251015052), Oct 11, 2025: ACCUMULATOR. BLOWN. BRAKE PRESSURE LOW PULLING UP TO THE GATE. FOUND LT BRAKE ACCUMULATOR BLOWN. REMOVED AND REPLACED LT BRAKE ACCUMULATOR IAW AMM 32-44-01, OPS & LEAK CHECKED GOOD
- [SDR HALA20240802036](https://openairdocs.org/sdr/HALA20240802036), Aug 1, 2024: HYDRAULIC LINE. LEAKING. ATB: L HYD QTY LO CLIMIBING THROUGH 11,000. REMOVED LEAKING HYD LINE PN- 7972138-616 - ROUTED TO HYD SHOP. REPAIRED HYD LINE PER AMM 20-10-01. INSALLATION, OPS 
- [SDR HALA20240228010](https://openairdocs.org/sdr/HALA20240228010), Feb 26, 2024: LINE. FAILED. L HYDRACLIC QUANTITY LOSS. REMOVED AND REPLACED HYDRAULIC LINES TO "ANTISKID CONTROL VALVE" PER AMM 32-45-11.PER PILOT SHUT-OFF LH SYSTEM PUMPS AT 5QTS.LEAK CHE
- [SDR HALA202310240047](https://openairdocs.org/sdr/HALA202310240047), Oct 23, 2023: UNKNOWN. UNKNOWN. EMERGENCY PATH LIGHTING ADJACENT TO SEAT 1B NEEDS REPAIR. REMOVED AND REPLACED EMERGENCY PATH LIGHTING ADJACENT TO SEAT 1B PER AMM 31-51-07-200-801.OPS CHECK GO
- [SDR HALA2023081400038](https://openairdocs.org/sdr/HALA2023081400038), Aug 12, 2023: HYDRAULIC LINE. DAMAGED. HYDRAULIC LT PRESSURE LOW AT TOP OF DESCENT FOLLOWED BY HYDRAULIC LT QUANTITY LOW (3.7 INDICATED QUANITY). TRIED TO REPRESSURIZE PER QRH PROCEDURE UNABLE TO REP
- [SDR HALA2022123000014](https://openairdocs.org/sdr/HALA2022123000014), Dec 28, 2022: FRAME. CORRODED. FRAME TEE CORRODED AT LT 6:10 POSITION. CLEANED AND TREATED IAW SRM 51-10-04. REMAINING THICKNESS .012. REPAIRED PER E105-485299-PERM.
- [SDR HALA2022123000013](https://openairdocs.org/sdr/HALA2022123000013), Dec 28, 2022: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT WAS FOUND WITH SURFACE CORROSION. REMOVED THE FLOOR SUPPORT. FABRICATED A NEW FLOOR SUPPORT IAW DWG 9936534 AND INSTALLED.
- [SDR HALA2020062500133](https://openairdocs.org/sdr/HALA2020062500133), Jun 24, 2020: WIRE. PULLED. OPEN - LOUD NOISE ON TAKEOFF ROLL IN AFT OF AIRCRAFT, LEFT AIR CYCLE MACHINE DUCTS BLOWN AND SENSOR AND TEMPERATURE CONTROL WIRES DAMAGED. FOUND DUCTING TO HEAT
- [SDR HALA2020052700115](https://openairdocs.org/sdr/HALA2020052700115), May 26, 2020: SLAT. UNKNOWN. OPEN - ON WALK AROUND FOUND LEFT WING NR 5 SLAT STICKING OUT. REPAIR IN WORK.
- [SDR HALA2020050700106](https://openairdocs.org/sdr/HALA2020050700106), May 6, 2020: ENGINE. MALFUNCTIONED. SUP - AIRTURN BACK AFTER TAKE ENG R SYS FAIL. // FAULT REVIEW ENG 2 FAULT CODE 732138. BITE TEST ENG SYS POWER UP TEST PASSED. PERFORMED FIM TASK 73-21 TASK 837
- [SDR HALA2020042100093](https://openairdocs.org/sdr/HALA2020042100093), Apr 20, 2020: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHTS ABOVE ENTRY WAY AND BOTH AFT CENTER EXIT DOOR INTERMITTENT ON AND SHUTS OFF. // REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY BATTERY
- [SDR HALA2020021800037](https://openairdocs.org/sdr/HALA2020021800037), Feb 14, 2020: DUCT. FAILED. ATB - CABIN ALTITUDE ABOVE 18000 RIGHT PACK WENT INOP O2 MASK CABIN DEPLOYED. // REMOVED AND REPLACED DUCT ASSY ABOVE DUCT CHECK VALVE (PART # 5971880-1HAL). LE
- [SDR HALA2020011400014](https://openairdocs.org/sdr/HALA2020011400014), Jan 11, 2020: EEC. MALFUNCTIONED. DURING CLIMB OUT, "ENG L FADEC ALT" ALERT DISPLAYED. WOULD NOT RESET - ATB. PERFORMED FIM 73-21 TASK 814. OPS CHECK GOOD. FAULT CLEARED. OK FOR SVC. REMOVED AND
- [SDR HALA2020011400013](https://openairdocs.org/sdr/HALA2020011400013), Jan 10, 2020: PROBE. FAULTY. ATB - SELECT FADEC ALTERNATE (L) ILLUMINATED DURING CLIMBOUT - ABOUT 1,300 FEET C/W QRH PROCEDURES, LIGHT DID NOT GO OUT - RETURNED TO HNL. PER FIM 73-21 TASK 8
- [SDR HALA2019111200481](https://openairdocs.org/sdr/HALA2019111200481), Nov 11, 2019: TIRE. OUT OF ROUND. RTO. EXCESSIVE NOSE GEAR VIBRATION FROM 30-60 KNOTS. REJECTED TAKE OFF. // ACCOMPLISHED INSPECTION FOR HIGH ENERGY STOP PER AMM 05-53-01. NOSE TIRES FOUND OUT O
- [SDR HALA2018121700655](https://openairdocs.org/sdr/HALA2018121700655), Dec 13, 2018: LIGHT. MALFUNCTIONED. FLIGHT ATTENDANT REPORTING EMERGENCY LIGHTS FLASHING ON EACH LANDING. CYCLED EMERGENCY PWR LTS SEVERAL TIMES. NO FAULTS NOTED ON GROUND.
- [SDR HALA2018121700654](https://openairdocs.org/sdr/HALA2018121700654), Dec 13, 2018: RELAY. MALFUNCTIONED. CABIN EMERGENCY LIGHTS FLICKERED AFTER LANDING AFTER A COUPLED APPROACH. DID NOT FLASH ON A NON COUPLED APPROACH. REMOVED AND REPLACED EMERGENCY POWER RELAY R2-
- [SDR HALA2018092200430](https://openairdocs.org/sdr/HALA2018092200430), Sep 22, 2018: TRIM MOTOR. INTERMITTENT. ATB / AUTO TRIM FAIL INFLT & STAB OUT OF TRIM DISPLAYED. FOUND ALTERNATE FOUND ALTERNATE STAB TRIM MOTOR INTERMITTENTLY INOP. REMOVED AND REPLACED ALTERNATE TRI
- [SDR HALA2018062000292](https://openairdocs.org/sdr/HALA2018062000292), Jun 19, 2018: WARNING MESSAGE. FALSE ACTIVATION. BLEED AIR RIGHT TEMP HIGH ALERT MESSAGE DURING ANTI-ICE CHECK. ACCOMPLISHED FIM 36-10 TASK 804. PERFORMED PSC BITE PROCEDURE, NO FAULTS WERE OBSERVED. RAN THE N
- [SDR HALA2018062000291](https://openairdocs.org/sdr/HALA2018062000291), Jun 18, 2018: CONTROL CABLE. OUT OF ADJUST. ROLL AXIS ON CONTROL YOKE HAS MUCH MORE THAN USUAL PLAY, CREATING A NULL CONTROL ZONE, ENOUGH TO MAKE THE AUTO PILOT DRIFT. AUTO PILOT DID NOT DISCONNECT. ACCOM
- [SDR HALA2018060700286](https://openairdocs.org/sdr/HALA2018060700286), Jun 6, 2018: SMOKE DETECTOR. MALFUNCTIONED. LAVATORY SMOKE WARNING MESSAGE HAD INTERMITTENT ACTIVATIONS. PERFORMED A SMOKE DETECTOR OPS CHECK. OPS CHECKED GOOD, OK TO CONTINUE.
- [SDR HALA2017081800228](https://openairdocs.org/sdr/HALA2017081800228), Aug 17, 2017: THERMOCOUPLE. FAILED. AIR TURN BACK. RT ENGINE SYSTEM FAILED, LT ENGINE SYSTEM FAILED ON CLIMB. PERFORMED FIM TASK 77-22-801, NR 1 ENGINE NO DEFECTS, NR 2 ENGINE TURBINE OVERHEAT CHN
- [SDR HALA2017041400100](https://openairdocs.org/sdr/HALA2017041400100), Apr 14, 2017: SHUTOFF VALVE. FAULTY. ATB, AIR SYS L PRESS LO INDICATION IN CLIMB OUT ( PRESSURE REGULATOR AND SHUTOFF VALVE (PR ). REMOVED AND REPLACED LEFT ENGINE PRSOV PILOT VLV PER AMM 36-12-03.
- [SDR HALA2016030100064](https://openairdocs.org/sdr/HALA2016030100064), Mar 1, 2016: LANDING GEAR. MALFUNCTIONED. ON FIRST ATTEMPT, GEAR DID NOT COME DOWN. GEAR INDICATIONS ALL RED, ALSO ALL RED ON CONFIGURATION PAGE. 2ND ATTEMPT OK. COMPLIED WITH INSPECTION OF NLG AND MLGS
- [SDR HALA2016012500018](https://openairdocs.org/sdr/HALA2016012500018), Jan 25, 2016: EEC. WARNING MESSAGE. DURING FLIGHT, SELECT FADEC ALTN FOR RT ENGINE EAD MSG. R & R RT ENGINE ELECTRONIC ENGINE CONTROL MM 73-21-01, RTS AND RUN CK GOOD.
- [SDR HALA2016011400009](https://openairdocs.org/sdr/HALA2016011400009), Jan 14, 2016: TIRE. DAMAGED. RIGHT INBD TIRE TREADING CAME OFF DURING LANDING ROLL OUT. R & R NR 3 MAIN WHEEL TIRE IAW AMM 32-41-01-000-803 & AMM 32-41-01-400-802. ACCOMPLISHED CHECK ON NR 
- [SDR HALA2015100600206](https://openairdocs.org/sdr/HALA2015100600206), Oct 6, 2015: COMPRESSOR. STALLED. LEFT ENGINE COMPRESSOR STALL WITH ASSOCIATED ALERT INFLIGHT. HIGH TGT 1055 DEGREES. PERFORMED ENGINE COMPRESSION STALL CHECKLIST AND ENGINE FAIL SHUTDOWN INFLIG
- [SDR HALA201507160137](https://openairdocs.org/sdr/HALA201507160137), Jul 16, 2015: ENGINE. VIBRATION. RT ENGINE HIGH VIBRATION WITH LOUD NOISE. N2 ENGINE VIBRATION PEAK OF 8.0 IN FLIGHT PEAK OF 9.8 BEFORE SHUTOWN, COULD NOT CONTROL VIBRATION LEVEL WITH THROTTLE 
- [SDR HALA0604201500104](https://openairdocs.org/sdr/HALA0604201500104), Jun 4, 2015: SLIDE. UNSECURE. SERVICE DOOR SLIDE CHUTE CAME UNDONE. R & R SERVICE DOOR SLIDE CHUTE MM 25-61-03, OK FOR SERVICE.
- [SDR HALA2014122000213](https://openairdocs.org/sdr/HALA2014122000213), Dec 20, 2014: DCU. MALFUNCTIONED. AIR DATA HEAT COMPLETE FAILURE AOA, STATIC, PITOT, RAT, RUDDER, AIR TURNBACK. ACCOMPLISHED FIM TASK 30-30, TASK 814. REPLACED AIR DATA HEATER SWITCH IAW WDM 30-
- [SDR HALA2014061800087](https://openairdocs.org/sdr/HALA2014061800087), Jun 18, 2014: LATCH. UNSECURE. DURING CLIMB AT 5000' "ACCESS COMPT DOOR ALERT DISPLAYED, RETURNED TO DEPARTURE. FOUND FWD NOSE ACCESSORY OVAL COMPARTMENT DOOR, 2, LATCHES OPEN. RESECURED FWD 
- [SDR HALA2014061700087](https://openairdocs.org/sdr/HALA2014061700087), Jun 18, 2014: LATCH. UNSECURE. DURING CLIMB AT 5000 FT "ACCESS COMPT DOOR ALERT DISPLAYED. FOUND FWD NOSE ACCESSORY OVAL COMPARTMENT DOOR 2 LATCHES OPEN. RESECURED FWD NOSE ACCESSORY OVAL COM
- [SDR HALA2013112000169](https://openairdocs.org/sdr/HALA2013112000169), Nov 20, 2013: WARNING MESSAGE. ILLUMINATED. "ENGINE LT SYSTEM FAIL" ALERT AFTER ENG START. ACCOMPLISHED FIM 73-21-801, EEC-1 BITE. NO FAULTS NOTED. RTS-PASSED. OK FOR SERVICE. MESSAGE EXTINGUISHED. IAW MO
- [SDR HALA2013030200027](https://openairdocs.org/sdr/HALA2013030200027), Mar 2, 2013: PROXIMITY SENSOR. INOPERATIVE. LEFT GEAR RED AFTER TAKEOFF, ALL THREE GREEN (NO RED) ON ARRIVAL. KEPT AIRSPEED BELOW 230 KTS. R & R D1-1057 LT MAIN GEAR UP & LATCHED PROXIMITY SENSOR IAW AMM 
- [SDR HALA2013021800022](https://openairdocs.org/sdr/HALA2013021800022), Feb 18, 2013: ACTUATOR. MALFUNCTIONED. AFTER TAKEOFF, OBSERVED LT MAIN GEAR LIGHT ON. CYCLED THE GEAR IAW ABNORMAL PROCEDURE. OBSERVED TWO MAIN GEAR DOOR LIGHTS ON. SHORTLY THERE AFTER ALL LIGHTS WEN
- [SDR HALA2013020300017](https://openairdocs.org/sdr/HALA2013020300017), Feb 3, 2013: SENSOR. FAILED. TAIL MANIFOLD FAIL. R & R PODS AND TAIL OVERHEAT DETECTOR SINGLE POINT SENSOR. REF AMM 36-23-01 AND 36-23-10. RTS TEST PASSED. OK FOR SERVICE.
- [SDR HALA2013012800013](https://openairdocs.org/sdr/HALA2013012800013), Jan 28, 2013: WARNING LIGHT. ILLUMINATED. TAIL MANIFOLD FAIL LIGHT ILLUMINATED, RAN CHECKLIST, LIGHT REMAINED ON AFTER LANDING FOR 1 MIN, EXTINGUISHED AND CAME ON ONE MORE TIME FOR 30 SECONDS. OPEN
- [SDR HALA2012021000053](https://openairdocs.org/sdr/HALA2012021000053), Feb 10, 2012: COMPRESSOR. STALLED. AT 2000' HAD A LEFT ENGINE COMPRESSOR STALL WITH MODERATE VIBRATION, ENGINE SHUTDOWN. REPLACED NR 1 ENG IAW HAL M143-717.
- [SDR HALA2011101500459](https://openairdocs.org/sdr/HALA2011101500459), Oct 15, 2011: WIRE. UNSECURE. CARGO SMOKE DETECT LIGHTS DO NOT TEST. SECURED WIRE CONNECTION AT S3-830 MASTER DIM & TEST OPS CHECKED OK IAW AMM 33-11-00 & CARGO SMOKE OPS CHECKED OK IAW AMM 
- [SDR HALA2011091700412](https://openairdocs.org/sdr/HALA2011091700412), Sep 17, 2011: SEAT TRACK. CORRODED. CABIN SEAT TRACK STA 44.5 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK IAW SR09530085 REV D APPLIED TOP COAT TO NEW SEAT TRACK. INSTALLED SEAT TRACK IAW DRAWING S
- [SDR HALA2011091700411](https://openairdocs.org/sdr/HALA2011091700411), Sep 17, 2011: SEAT TRACK. CORRODED. CABIN SEAT TRACK STA 204, RBL 22 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK IAW SRM 51-40-02. TREATED, PRIMED AND TO COATED SEAT TRACK IAW SRM 51-10-04. INSTALL
- [SDR HALA2011091200417](https://openairdocs.org/sdr/HALA2011091200417), Sep 12, 2011: DOOR FRAME. CORRODED. AFT CARGO COMP DOOR JAMB LWR SIDE HAS SEVERAL SPOTS OF CORROSION. REMOVED CORROSION AT AFT CARGO COMP DOOR JAMB LWR SIDE(PAN). AFTER CORROSION REMOVAL FOUND ARE
- [SDR HALA2011082400384](https://openairdocs.org/sdr/HALA2011082400384), Aug 24, 2011: WARNING LIGHT. INOPERATIVE. OPEN - AFT LAV FIRE WARNING LIGHT WILL NOT ILLUMINATE WHEN TESTED. (LAV LOCKED-OUT). OK TO CONTINUE IAW MEL 26-14-01.
- [SDR HALA2011041700158](https://openairdocs.org/sdr/HALA2011041700158), Apr 17, 2011: WARNING LIGHT. ILLUMINATED. SPOILER INBD FAIL CAME ON AFTER TURNING OFF HYD PUMPS DURING CLIMB CHECK. REVIEWED LOG FOR LAST 7 DAYS NO SIMILAR OCCURANCE FOUND. GROUND RAN BOTH ENG & CYCLED 
- [SDR HALA2011010700013](https://openairdocs.org/sdr/HALA2011010700013), Jan 7, 2011: SKIN. DENTED. SMALL CREASE FOUND UNDER FUSELAGE BELOW AFT CARGO DOOR. BLENDED DAMAGED AREA. EDDY CURRENT CK OK, NO CRACK INDICATION. DENT DAMAGE CONDITION 1A IAW DWG SG095300
- [SDR HALA2010120200576](https://openairdocs.org/sdr/HALA2010120200576), Dec 2, 2010: ENGINE. FAILED. OPEN - ABORTED TAKE-OFF DUE NR 1 ENGINE FAILED. ENGINE REPLACEMENT STILL IN WORK.
- [SDR HALA2010031500110](https://openairdocs.org/sdr/HALA2010031500110), Mar 15, 2010: UNKNOWN. ODOR. F/A'S NOTICED EMERGENCY LIGHTS FLICKER DURING FLIGHT. THEN ON LANDING EMERGENCY LIGHTS FLICKERED AGAIN AND THE FWD F/A'S DETECTED AN ELECTRICAL TYPE OR ELECTRIC
- [SDR HALA2009101400465](https://openairdocs.org/sdr/HALA2009101400465), Oct 14, 2009: UNKNOWN. ODOR. STRONG CHEMICAL ODOR ON TAKEOFF THAT DECREASED DURING CLIMBOUT ALL A/C SYSTEM INDICATIONS NORMAL. RAN ENGINES WITH BOTH PACKS ON. NO ODOR NOTED. OK FOR SERVICE.
- [SDR HALA2009072900339](https://openairdocs.org/sdr/HALA2009072900339), Jul 29, 2009: VIA. FAILED. AFTER DEPARTURE EXPERIENCED MAP SHIFT AND NAVIGATION UNREALABLE, NR 2 DU FAILED ALSO. REPLACED NR 1 VIA, GND CHECK OK IAW MM 31-43-00.

All 65: https://openairdocs.org/aircraft/N485HA/reports.md

## STCs that may be installed (OpenAirDocs) (71, 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 (Boeing 717-200)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04122AT](https://openairdocs.org/stc/ST04122AT): Installation of an oven. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST04816NY](https://openairdocs.org/stc/ST04816NY): Installation of Electronically Steerable (ESA) Antenna and Power Supply. ALOFT AeroArchitects
- [STC ST12026AT](https://openairdocs.org/stc/ST12026AT): Installation of Portable Emergency Locator Transmitter. Delta Flight Products LLC
- [STC ST02478NY](https://openairdocs.org/stc/ST02478NY): Installation of an advertisement container on the bottom of a seat back tray table on Weber Model 5300 passenger seats (Weber Part Numbers 852454, 852455, 852456, 852457, 852458, and 852459). Atin OOH, LLC
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST04813NY](https://openairdocs.org/stc/ST04813NY): Installation of Hughes Satellite Connectivity and Wifi Cabin Distribution System. ALOFT AeroArchitects
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing 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 ST03682AT](https://openairdocs.org/stc/ST03682AT): Installation of an Aircell Broadband Service (ABS) Passenger Cabin Air-To-Ground (ATG) Voice/Data Communication System. Amphenol Cable and Interconnect Technologies Inc
- [STC ST11388DS](https://openairdocs.org/stc/ST11388DS): Expansion of the Delta Comfort+® Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST02637AT](https://openairdocs.org/stc/ST02637AT): Installation of SafTGlo Inc. photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC SA9024NM-D](https://openairdocs.org/stc/SA9024NM-D): Installation of Scandinavian Bellyloading Company, sliding carpet loading system. SBC-America LLC
- [STC ST04416AT](https://openairdocs.org/stc/ST04416AT): Installation of the Rockwell Collins Multi-Mode Receiver (MMR). Woven Electronics LLC
- [STC ST04418AT](https://openairdocs.org/stc/ST04418AT): Installation of the Rockwell Collins Automatic Dependent Surveillance - Broadcast (ADS-B) Out System. Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST01465LA-D](https://openairdocs.org/stc/ST01465LA-D): Installation of B/E Aerospace, Inc. Air Chiller Part Number 374-8. B/E Aerospace Inc
- [STC ST01023SE](https://openairdocs.org/stc/ST01023SE): Installation of a the TPA-81A Traffic Alert and Collision Avoidance System (TCAS) Processor in accordance with Master Drawing List 756-0119-001, Revision D, dated November 21, 2003, or later FAA approved revisions. Honeywell International Inc
- [STC ST01096SE](https://openairdocs.org/stc/ST01096SE): Installation of the Mark III Aircraft Communications Addressing and Reporting System (ACARS). Honeywell International Inc
- [STC ST01640SE](https://openairdocs.org/stc/ST01640SE): Installation of the Mark III Aircraft Communications Addressing and Reporting System (ACARS). Honeywell International Inc
- [STC ST03418NY](https://openairdocs.org/stc/ST03418NY): Installation of a UTC Electronic Flight Bags. Rockwell Collins Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04029CH](https://openairdocs.org/stc/ST04029CH): Modification of an existing Aircell Broadband Services (ABS) System with ATG4 Enhancements. Intelsat Inflight LLC
- [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST04425CH](https://openairdocs.org/stc/ST04425CH): Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04424CH](https://openairdocs.org/stc/ST04424CH): TPED Compatibility Test in accordance with StandardAero Master Data List 1037140, Revision (B), dated June 1, 2020 or later FAA approved revision. Standard Aero Business Aviation Services LLC
- [STC ST04468NY](https://openairdocs.org/stc/ST04468NY): Installation of Honeywell ADS-B Transponder Upgrade. H4 Aerospace (UK) Ltd
- [STC ST02152LA](https://openairdocs.org/stc/ST02152LA): Installation of AmSafe Aviation Inflatable Restraint (AAIR) System. AMSAFE Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA8339SW](https://openairdocs.org/stc/SA8339SW): Installation of a fuselage nose radome shell. The NORDAM Group LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04229NY](https://openairdocs.org/stc/ST04229NY): Introduction of a 16G New Generation Stretcher XL P/N 1120030-Series. Bucher Leichtbau AG
- [STC ST04167NY](https://openairdocs.org/stc/ST04167NY): Installation of TCAS System upgrade to Change 7.1. H4 Aerospace (UK) Ltd
- [STC ST03846NY](https://openairdocs.org/stc/ST03846NY): Installation of SuperSeal UltraLite (SSUL) PHOTOLUMINESCENT AISLE PATH MARKING SYSTEM. STG Aerospace Ltd
- [STC ST04242CH](https://openairdocs.org/stc/ST04242CH): Installation of ACSS Automatic Dependent Surveillance-Broadcast (ADS-B) compliant Mode S Transponders. Canard Aerospace Corporation
- [STC ST04186CH](https://openairdocs.org/stc/ST04186CH): Retrofit installation of Rosemount Aerospace Model 0861EW2 Angle of Attack (AOA) Sensors. Rosemount Aerospace Inc
- [STC ST02479SE](https://openairdocs.org/stc/ST02479SE): Installation of class dividers and cross aisle curtain headers. Northwest Aerospace Technologies Inc
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST02991AT](https://openairdocs.org/stc/ST02991AT): Installation of LiveTV XM Satellite Radio System. Thales Avionics Inc
- [STC ST03449CH](https://openairdocs.org/stc/ST03449CH): Installation of LH and RH Passenger Window - STA 218 to STA 237. AAR Aircraft Services
- [STC ST04206AT](https://openairdocs.org/stc/ST04206AT): Interior reconfiguration. Delta Air Lines Inc
- [STC ST03442CH](https://openairdocs.org/stc/ST03442CH): Installation of New Interior Arrangement. AAR Aircraft Services
- [STC ST03817AT](https://openairdocs.org/stc/ST03817AT): Installation of a Thales-KANNAD Emergency Locator Transmitter. Avionics Support Group Inc

All 71: https://openairdocs.org/aircraft/N485HA/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce BR-700 series engine: https://openairdocs.org/engine/rolls-royce-br-700-series.md

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