# N486HA: 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: 55131
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 17, 2001
- Certificate issued: June 29, 2011
- Expires: June 30, 2027
- Mode S code: A5FF93
- 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=486HA
- Page: https://openairdocs.org/aircraft/N486HA

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/N486HA/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 N486HA.

## FAA accident and incident reports

None matched to N486HA.

## Service difficulty reports (83, 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 ASAA2026080666175](https://openairdocs.org/sdr/ASAA2026080666175), Aug 6, 2026: BATTERY PACK. INOPERATIVE. OVERWING EMERGENCY LIGHTS OUT. GROUNDED - YES. REPLACED OVERWING EMERGENCY LIGHT BATTERY PER AMM 33-51-06-400-801. OPS CHECK GOOD, OK FOR SERVICE.
- [SDR ASAA2026070865667](https://openairdocs.org/sdr/ASAA2026070865667), Jul 8, 2026: WHEEL. ABNORMAL. BTB EXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF ROLL - ABORTED BELOW 80 KTS. GROUNDED - YES. REMOVED AND REPLACED L AND R NLG TIRES PER AMM TASK 32-42-01-400-801. SP
- [SDR ASAA2026031463861](https://openairdocs.org/sdr/ASAA2026031463861), Mar 14, 2026: WINDSHEAR SYS. ACTIVATED. WINDSHEAR ON TAKEOFF RUNWAY 17 IN KONA, ABORTED AT 79 KTS. GROUNDED - YES. INSPECTED AIRCRAFT PER AMM 05-53-01. NO BRAKE OVERHEAT ALERT SHOWN. AIRCRAFT OK FOR S
- [SDR HALA20250331022](https://openairdocs.org/sdr/HALA20250331022), Mar 27, 2025: BRACKET. CORRODED. SURFACE CORROSION ON "L" BRACKET UNDER MAINT PLATFORM STATION 1095 . MARKED. 1. REMOVED TEE EXTRUSION FROM WALKWAY STRUCTURE. FABRICATED NEW TEE PER BOEING DRAW
- [SDR HALA20250331021](https://openairdocs.org/sdr/HALA20250331021), Mar 27, 2025: FRAME. CORRODED. NUMEROUS CORROSION ON FRAME 1138 (M). CUTOUT APPROX 4 INCHES OF OUT OF LIMITS CORROSION ON STA 1138 FRAME BETWEEN LEFT L29 AND L30, HFC CUTOUT NO CRACKS NOTED. 
- [SDR HALA20241024058](https://openairdocs.org/sdr/HALA20241024058), Oct 23, 2024: SPRING. FAULTED. AFTER T/O LEFT GEAR UNSAFE LIGHT ILLUMINATE WITH GEAR HANDLE UP. REMOVED AND REPLACED UP LATCH SPRING FOR LEFT MLG DOOR. OPS CHK AND SECURITY CHK OK. OK FOR SVC
- [SDR HALA20240528027](https://openairdocs.org/sdr/HALA20240528027), May 25, 2024: COMPRESSOR. STALLED. ENG R COMP STALL IN CRUISE. COMPLIED WITH QRH PROCEDURE. "ENGINE VIB HI" AT HIGH POWER SETTINGS. PREPPED FOR BOROSCOPE INSP. PER AMM 72-00-00-200-801 TO STEP 2E
- [SDR HALA20240403018](https://openairdocs.org/sdr/HALA20240403018), Apr 2, 2024: ENGINE. FAULTED. FLIGHT DECK CREW AND CABIN HEARD 2 LOUD POPS. ENG LEFT COMPRESSOR STALL ALERT CAME ON. CREW FOLLOWED QRH CHECKLIST, LEFT ENGINE WAS SHUT DOWN. ENG GAUGES SHOWED
- [SDR HALA20240401016](https://openairdocs.org/sdr/HALA20240401016), Mar 29, 2024: BATTERY PACK. INOPERATIVE. FWD ATTENDANT WORK LIGHT AND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSEMBLY AND POWER SUPPLY PER AMM 33-51-03. OPS CHECK GOOD. OKAY FOR SERVICE.
- [SDR HALA20240207006](https://openairdocs.org/sdr/HALA20240207006), Feb 6, 2024: BATTERY. INOPERATIVE. EMER LT. NOT STAY ON. REMOVED AND REPLACED 13 EA CABIN EMERGENCY EXIT LIGHT BATTERIES PER AMM 33-51-03/401. OPS TEST GOOD. OK FOR SVC.
- [SDR HALA20231213050](https://openairdocs.org/sdr/HALA20231213050), Dec 12, 2023: UNKNOWN. UNKNOWN. EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY BATTERY POWER SUPPLY PER AMM 33-51-06. OPERATION GOOD.
- [SDR HALA2022092700263](https://openairdocs.org/sdr/HALA2022092700263), Sep 26, 2022: NONE. NONE. EMERGENCY LIGHTS IN CEILING FROM ROW 4 TO 11 INOP AND CEILING TAIL CONE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY B5-116
- [SDR HALA2022022300054](https://openairdocs.org/sdr/HALA2022022300054), Feb 22, 2022: NONE. NONE. ATB - ENG R SYS FAIL ON CLIMBOUT // REFERENCE LOG PG 878257-2 FOR CH B REPLACED LUG ATT1043-2, PERFORMED WIRING CHECKS PER FIM 73-21 TASK 875 FOR CH A ALL WIRIN
- [SDR HALA2021122700201](https://openairdocs.org/sdr/HALA2021122700201), Dec 25, 2021: COVER. ABNORMAL. EMER EQ - SLIDE - FORWARD SERVICE DOOR GIRT BAR DISCONNECTED FROM EMERGENCY SLIDE // RESECURED FWD SVC DOOR COVER. FOUND SLIDE COVER DISENGAGED. SECURITY CHK GO
- [SDR HALA2021040600042](https://openairdocs.org/sdr/HALA2021040600042), Apr 5, 2021: CYLINDER. DEFECTIVE. LANDING GEAR DOOR - GEAR DOOR OPEN ALERT LOWERING LANDING GEAR. ALERT REMAINS FOR 15 SECONDS BEFORE EXTINGUISHING. // REMOVED + REPLACED L/H MLG DOOR ACTUATOR C
- [SDR HALA2020042200095](https://openairdocs.org/sdr/HALA2020042200095), Apr 21, 2020: RING. CORRODED. OPEN - ENGINE 1 SYSTEM FAIL, UNABLE TAKEOFF POWER. // ACCOMPLISHED BOROSCOPE, FOUND VSV RING AND SUSPECTED CORROSION CAUSING VSV RING TO BIND. REPLACEMENT OF EN
- [SDR HALA2020032500073](https://openairdocs.org/sdr/HALA2020032500073), Mar 24, 2020: RELAY. FAILED. AUTO TRIM FAIL ILLUMINATED DURING DESCENT APPROXIMATED 10000 FEET. WARNING WENT OUT AFTER LANDING.// REMOVED AND REPLACED ELV UP AND DOWN TRIM REPLAY PER 27-43-
- [SDR HALA2020031900066](https://openairdocs.org/sdr/HALA2020031900066), Mar 18, 2020: CABLE. OUT OF POSITION. TAIL CONE JETTISON KEVLAR CABLE ROUTED INCORRECTLY FROM PAINT. // RE-ROUTED TAIL CONE RELEASE KEVLAR CABLE PER AMM 53-52-01, SECURITY CHECK OK.
- [SDR HALA2019120900281](https://openairdocs.org/sdr/HALA2019120900281), Nov 5, 2019: FLOOR SUPPORT. CORRODED. FOUND CORROSION ON FLOORTRACK OF RH SIDE OF FUSELAGE AT STA 1037//REPAIRED FLOOR PANEL SUPPORT PER E105-486293-PERM
- [SDR HALA2019100750402](https://openairdocs.org/sdr/HALA2019100750402), Oct 5, 2019: BATTERY PACK. INOPERATIVE. BATTERIES FOR EMERGENCY PER NOT CHARGING. REMOVED AND REPLACED 3 BATTERIES PER AMM 24-34-01. BATTERIES CHECK GOOD.
- [SDR HALA2019080100377](https://openairdocs.org/sdr/HALA2019080100377), Jul 31, 2019: WATER SEPARATOR. ODOR. ON GROUND BURNING OIL SMELL WHEN PACKS ON APU. APU BLEED AIR MODULATING VALVE. REMOVED AND REPLACED BOTH WATER SEPERATORS FOR AIR CONDITIONING. APU COMPARTMENT 
- [SDR HALA2019021500057](https://openairdocs.org/sdr/HALA2019021500057), Feb 15, 2019: PROXIMITY SENSOR. FAILED. ATB / RIGHT MAIN GEAR "RED" INDICATION UPON RETRACTION. THREE GREEN ON DOWN POSITION.// REMOVED AND REPLACED MLG DOWN/LOCK PROX SENSOR ASSY PER AMM TASK 32-61-0
- [SDR HALA2018122400676](https://openairdocs.org/sdr/HALA2018122400676), Dec 23, 2018: UNKNOWN. ODOR. FA'S REPORT FOUL SMELL COMING FROM CABIN A/C.PERFORMED FIM 21-22 TASK 815. NO DEFECTS NOTED. AS PRECAUTION REPLACED BOTH COALESCER BAGS PER AMM 21-54-08. OPS TE
- [SDR HALA2018101500500](https://openairdocs.org/sdr/HALA2018101500500), Oct 13, 2018: SENSE LINE. CONTAMINATED. IN ALT (FADEC) WITH THROTTLES AT IDLE, ENG 1 STUCK AT 71% N1 FOLLOWED BY ENG COMP STALL LEFT, AFTER 3 MIN ENG WENT TO IDLE. PERFORMED WIRING CHECK ON OIL PRESSU
- [SDR HALA2018101500499](https://openairdocs.org/sdr/HALA2018101500499), Oct 13, 2018: FMU. MALFUNCTIONED. DIVERSION - APPROACHING OUT CRUISE ALTITUDE OF 25000' WE HAD A "ENG L SYS FAIL AND ENG L FADEC ALTN" PERFORMED QRH LEFT ENG INDICATING HAD A X TALKED TO MTN AND
- [SDR HALA2018101200491](https://openairdocs.org/sdr/HALA2018101200491), Oct 11, 2018: EEC. FAULTY. DURING CRUISE AT FL250 AMBER X DISPLAYED ON LEFT EPR AND SELECT FADEC L ALTN DISPLAYED. BONDING CHECK OFF NR 1 ENG EEC CHECK OK. REMOVED AND REPLACED EEC CONTRO
- [SDR HALA2018062200298](https://openairdocs.org/sdr/HALA2018062200298), Jun 21, 2018: CONNECTOR. DAMAGED. RIGHT HYD TEMP HIGH DURING TAXI OUT. REMOVED AND REPLACED THE RT HYD RESERVOIR HIGH WARNING TEMP PLUG IAW WDM 29-33-01. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HALA2018022000045](https://openairdocs.org/sdr/HALA2018022000045), Feb 17, 2018: RESERVOIR. CONTAMINATED. ON TAXI OUT, "HYD R TEMP HI" MASTER CAUTION. BLEED RIGHT HYD RES. CYCLED ALL KNURLED KNOBS. RAN PUMPS MESSAGE DID NOT RETURN.
- [SDR HALA2018020600031](https://openairdocs.org/sdr/HALA2018020600031), Feb 2, 2018: FUEL LINE. LEAKING. AFTER STARTING APU, NOTICE A STRONG FUEL ODOR, SHUT APU DOWN AND FUEL ODOR WENT AWAY. FOUND FUEL LEAKING FROM APU FCU HARD LINE TO FUEL NOZZLE. REMOVED AND REPL
- [SDR HALA2017022500046](https://openairdocs.org/sdr/HALA2017022500046), Feb 25, 2017: RELAY. FAILED. BURNING ODOR NOTICED AFTER LANDING. PERFORMED FIM 21-22-815 FOR ODOR. RAN NR 1 & 2 ENGINES SPERATELY. AS NR 1 AND 2 PACKS ISOLATED, COULD NOT DUPLICATE ON GROUN
- [SDR HALA2016092600359](https://openairdocs.org/sdr/HALA2016092600359), Sep 26, 2016: PROXIMITY SENSOR. OUT OF ADJUST. WHILE ENROUTE, RED GEAR UNSAFE LIGHT ILLUMINATED ON RT GEAR AND ON CONFIGURATION PAGE. PERFORMED INSPECTION OF RT MLG DOOR LATCH IAW AMM 32-34-01. NO DEFECTS NO
- [SDR HALA2015122500252](https://openairdocs.org/sdr/HALA2015122500252), Dec 25, 2015: WASHER. DAMAGED. NLG LOWER SPRING BEVEL WASHER BELOW TRUNNION DAMAGED AND REMOVED. R & R NLG BELLEVILLE WASHER IAW AMM 32-21-01. SERVICE AND LUBRICATED NLG STRUT. SECURITY CHECK
- [SDR HALA2015010500002](https://openairdocs.org/sdr/HALA2015010500002), Jan 5, 2015: TIRE. SEPARATED. TIRE RECAP PEELING RT MAIN INBD TIRE. REPLACED NR 3 MAIN TIRE IAW AMM 32-41-01. CONDITION & SECURITY OK, TORQUE & SPIN CK OK AND CHECKED DENTS ON T/E FLAP. DENT
- [SDR HALA2014122600223](https://openairdocs.org/sdr/HALA2014122600223), Dec 26, 2014: WIRE. LOOSE. EMERGENCY LIGHT WIRES 6F FOUND LOOSE DURING PREFLIGHT. SECURED EMERGENCY LIGHT WIRE AT 6F. SECURITY, OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HALA2014110400179](https://openairdocs.org/sdr/HALA2014110400179), Nov 4, 2014: ENGINE. VIBRATION. ENGINE VIBRATION HIGH ALERT FOLLOWED BY SUDDEN GROWLING NOISE, CLIMBING THROUGH 5000 FEET LT N2 VIB. REACHED 6.2 AND DROPPED LOWER WITH REDUCED POWER. ALL OTHER
- [SDR HALA2014062500091](https://openairdocs.org/sdr/HALA2014062500091), Jun 25, 2014: BOLT. FAILED. DURING AN A-CHECK, FOUND A MISSING NAS6204-9, BOLT COMMON TO THE RT WING SLAT DRIVE ASSY. CONFIRMED THAT THE BOLT WAS MISSING BECAUSE OF THE NAS679A4. NUT WAS D
- [SDR HALA2014052900072](https://openairdocs.org/sdr/HALA2014052900072), May 29, 2014: TRIM SYSTEM. MALFUNCTIONED. PRIMARY TRIM FAILED DURING FLIGHT. ALT TRIM OK. TROUBLESHOT PRIMARY TRIM FAULT IAW FIM TASK 27-40, TASK 801, PERFORMED OPS CHECK OF THE PRIMARY TRIM DRIVE MOTOR
- [SDR HALA2014052900071](https://openairdocs.org/sdr/HALA2014052900071), May 29, 2014: TRIM SYSTEM. MALFUNCTIONED. PRIMARY TRIM FAILED DURING FLIGHT. ALTERNATE TRIM OK. TROUBLESHOT PRIMARY TRIM FAULT IAW FIM TASK 27-40 TASK 801, PERFORMED OPS CHECK OF THE PRIMARY TRIM DRIVE 
- [SDR HALA2014042500055](https://openairdocs.org/sdr/HALA2014042500055), Apr 25, 2014: HOSE. LEAKING. DURING FLIGHT, RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE. R & R RT MAIN GEAR ACTUATOR HOSE ASSY SERVICED HYDR
- [SDR HALA2013091800118](https://openairdocs.org/sdr/HALA2013091800118), Sep 17, 2013: FAN. UNKNOWN. APU AUTO SHUTDOWN. R & R APU OIL COOLING FAN ASSEMBLY IAW AMM 49-50-01, LEAK AND OPS CHECKED GOOD.
- [SDR HALA2013022200025](https://openairdocs.org/sdr/HALA2013022200025), Feb 22, 2013: TIRE. FAILED. NR 4 TIRE FAILURE CAUSED NR 2 ENG ATTRITION LINING DAMAGE AT 3 PLACES FROM 10 TO 11 0'CLOCK POSITION. INSTALLED NR 2 ENG IAW HAL M143-717. OPS AND LEAK CHECK GO
- [SDR HALA2013022200023](https://openairdocs.org/sdr/HALA2013022200023), Feb 22, 2013: WARNING LIGHT. FALSE ACTIVATION. ON TAKEOFF CLIMB AT 1000FT MSL RT ENGINE SYS FAIL CAUTION LIGHT CAME ON. YELLOW X CAME ON OVER TGT. TGT FLUCTUATED 10-20 DEG NO EXEEDANCE. EEC-2 FAULT CODE 7721
- [SDR HALA2012080200189](https://openairdocs.org/sdr/HALA2012080200189), Aug 2, 2012: TIRE. SEPARATED. NR 4 MAIN TIRE, RECAP SHOWING. OTBD TREAD SEPARATED. R & R NR 4 MAIN TIRE IAW AMM 32-41-01, SPIN CHECKED GOOD.
- [SDR HALA2012011200017](https://openairdocs.org/sdr/HALA2012011200017), Jan 11, 2012: BRAKE. OVERHEATED. HOT BRAKES AT NR 1 MLG REACHED AT 450 DEGREES. FAN COOLED NR 1 MLG BRAKE. OK TO CONTINUE IAW AMM 32-47-00, INSPECTED BRAKES & FUSE PLUG. CHECKED OK, NO FAULTS N
- [SDR HALA2011042500166](https://openairdocs.org/sdr/HALA2011042500166), Apr 25, 2011: DETECTION SYS. MALFUNCTIONED. ON PREFLIGHT AFTER CARGO SMOKE TEST BUTTON RELEASED "ABENT 1 DISCH" BUTTONS CONTINUED TO FLASH & CARGO SMOKE ANNUNICATED ON EAD & ATR PAGE. RESET NR 1 VIA PERFO
- [SDR HALA2010082500379](https://openairdocs.org/sdr/HALA2010082500379), Aug 25, 2010: EEC. FAILED. ENROUTE "ENG R SYS FAIL" LIGHT CAME ON - ATB. ACCOMPLISHED RT EEC BITE PROCEDURE 73-21, TASK 801. SHOW FAULT CODE 732165 & 166 & MX MSG 732140, START SWITCH LAT
- [SDR HALA201007160299](https://openairdocs.org/sdr/HALA201007160299), Jul 8, 2010: CONNECTOR. DEFECTIVE. ATB - AFTER T/O MESSAGE HYD R TEMP HI ILLUMINATED. REPLACED ELECTRICAL PLUG FOR RIGHT HYD TEMP HI SWITCH. OPS CHECK OK, WDM 29-33-01.
- [SDR HALA2010062100291](https://openairdocs.org/sdr/HALA2010062100291), Jun 21, 2010: CAP. CORRODED. LEVEL 2 CORROSION ON END CAP AT STATION 1053 LONGERON 23RT. REMOVED AND REPLACED END CAP PRIMED AND PAINTED PER SRM 51-22-01.
- [SDR HALA2010062100290](https://openairdocs.org/sdr/HALA2010062100290), Jun 21, 2010: FASTENER. CORRODED. LEVEL 2 CORROSION ON HI - LOKS BETWEEN STATION 1053 AND 1076, LONGERON 25R. REPLACED CORRODED FASTENERS. PRIMED AND PAINTED PER SRM 51-22-01.
- [SDR HALA2010062100289](https://openairdocs.org/sdr/HALA2010062100289), Jun 21, 2010: HINGE. CRACKED. APU RT ACCESS DOOR HINGE CRACKED AFT END. REMOVED CRACKED HINGE, REPAIRED IAW M-105 PRIMED AND PAINTED HINGE. PICKED UP FASTENER HOLES ON NEW DOOR HINGE. INSTAL

All 83: https://openairdocs.org/aircraft/N486HA/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/N486HA/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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