# N487HA: 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: 55132
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 2001
- Certificate issued: June 29, 2011
- Expires: June 30, 2027
- Mode S code: A6034A
- 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=487HA
- Page: https://openairdocs.org/aircraft/N487HA

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/N487HA/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 N487HA.

## FAA accident and incident reports

None matched to N487HA.

## Service difficulty reports (64, 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 ASAA2026051864816](https://openairdocs.org/sdr/ASAA2026051864816), May 18, 2026: BATTERY PACK. INOPERATIVE. OVERWING EMERGENCY LAMPS INOP. GROUNDED - YES. REPLACED BATTERY PACK PER AMM 33-51-06. OPS TEST PASS. OK FOR SVC.
- [SDR ASAA2026031963889](https://openairdocs.org/sdr/ASAA2026031963889), Mar 19, 2026: A/C PACK. NOT REPORTED. WHEN ARRIVED AT PLANE TEMP WAS 84' INCREASED TO EXCESS OF 90'. GROUNDED - YES. TURN ON APU BLEED AND RUN RH PACK.GROUND AIR IN SUFFICIENT.
- [SDR ASAA2025122362496](https://openairdocs.org/sdr/ASAA2025122362496), Dec 23, 2025: GIRT BAR. NO DISCREPANCY. MCD GIRT BAR WONT LOCK INTO LEFT FLOOR BRACKET. GROUNDED - YES. VISUAL INSPECT MCD GIRT BAR PERFORM OPS CHECK LOCK AND SECURED.CHECK GOOD.OK FOR SVC.
- [SDR HALA20240709033](https://openairdocs.org/sdr/HALA20240709033), Jul 8, 2024: SEAL. LEAKING. ATB -AFTER GEAR RETACTION IN LOUD SOUND FROM NOSE GEAR FOLLOWED BY DISSARM SPOILER MESSAGE. THE CLIMB/RECORD NLG STRUT.REPLACED NLG STRUCTSEALS PER AMM 32-21-01
- [SDR HALA20231020044](https://openairdocs.org/sdr/HALA20231020044), Oct 19, 2023: UNKNOWN. UNKNOWN. AFT CEILING EMERGENCY LIGHTS NOT COMING ON. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY AT B5-231 PER AMM 33-51-03. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2023061400033](https://openairdocs.org/sdr/HALA2023061400033), Jun 13, 2023: UNKNOWN. UNKNOWN. ON CLIMBOUT LEFT ENGINE COMPRESSOR STALL. RETURNED BACK TO AIRPORT ATB. FOUND LEFT ENGINE NOSE CONE MISSING PROTECTIVE COATING. PERFOMED INSPECTION AFTER HIGH P
- [SDR HALA2023031400007](https://openairdocs.org/sdr/HALA2023031400007), Feb 28, 2023: UNKNOWN. UNKNOWN. GEAR WOULD NOT COME UP ALONG WITH LOUD GRINDING LIKE NOISE AND VIBRATION COMING FROM NOSE GEAR. RETURNED TO HNL. PERFOMED EXT/RET OF NOSE GEAR MULTIPLE TIMES PE
- [SDR HALA2022112900330](https://openairdocs.org/sdr/HALA2022112900330), Nov 28, 2022: POWER SUPPLY. FAULTED. EMERGENCY LIGHTS DISARM DISPLAYED IN "ON" SWITCH POSITION. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY B-123, PER AMM 33-51-03. OPS TEST OK.
- [SDR HALA2022112800303](https://openairdocs.org/sdr/HALA2022112800303), Nov 28, 2022: BATTERY. INOPERATIVE. EMERGENCY LIGHTS DISARM DISPLAYED IN "ON" SWITCH POSITION. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY B-123, PER AMM 33-51-03. OPS TEST OK.
- [SDR HALA2022101700001](https://openairdocs.org/sdr/HALA2022101700001), Oct 14, 2022: LINK. FAILED. ATB - AFTER GEAR UP, HEAVY VIBRATIONS OF NOSE WHEEL. RECYLED GEAR WITH SAME RESULT. FOUND RH NOSE GEAR FWD DOOR OPEN AT BLOCK IN. REMOVED AND REPLACED NLG FED D
- [SDR HALA2020032500075](https://openairdocs.org/sdr/HALA2020032500075), Mar 20, 2020: SKIN. CORRODED. UPPER WING SKIN IN LEFT HAND WHEEL AREA CORROSION, BLENDED XRS 37 OUT OF LIMITS, PER DRAWING # SG9557001. REPAIRED PER E105-487297- PERM.
- [SDR HALA2020032500074](https://openairdocs.org/sdr/HALA2020032500074), Mar 20, 2020: SPAR. CORRODED. RIGHT WING EXFOLIATION CORROSION IN REAR SPAR LOWER TANG, JUST O/B OF #44 AILERON HINGE. // CUT OUT CORROSION CHORD -70 SPAN - 280, HFEC CHECK OK. REPAIRED PER 
- [SDR HALA2019121900523](https://openairdocs.org/sdr/HALA2019121900523), Dec 18, 2019: IO CARD. FAILED. IN CRUISE FLIGHT ENG L SYS FAIL MESSAGE. // TROUBLESHOOT PER FIM 71-00 TASK 802. RECEIVED EEC-1 CURRENT FAULT 732177 IOP BOX FAULT. REMOVED AND REPLACED LH ENG 
- [SDR HALA2019102980459](https://openairdocs.org/sdr/HALA2019102980459), Oct 28, 2019: SECU. FAULTED. ABT - ADVANCED THROTTLES DURING TAKEOFF ROLL, SPOILER FAULT, ABORTED TAKEOFF <20 KTS. // SECU RTS TEST GOOD. CYCLE SPOILER 20 TIMES PER FIM 27-60 TASK 820. NO F
- [SDR HALA2019101800428](https://openairdocs.org/sdr/HALA2019101800428), Oct 17, 2019: SIGN. DAMAGED. EXIT SIGN 17DEF ROW DAMAGED. // REMOVED AND REPLACED HOUSING ON EMERGENCY LIGHT AT 17DEF (L2-834). OPS CHECK OK PER AMM 33-51-18. OK FOR SERVICE.
- [SDR HALA2019021200056](https://openairdocs.org/sdr/HALA2019021200056), Feb 12, 2019: VANE. OUT OF ADJUST. ATB / FCF FAILED = ACFT ROLLS RIGHT AT FLAP 40. ADJUSTED R/H MID FLAP FIX VANE PER AMM 24-20-02.
- [SDR HALA2018072600405](https://openairdocs.org/sdr/HALA2018072600405), Jul 25, 2018: CONDUIT. BROKEN. RIGHT MLG SLOW TO RETRACT. RED UNSAFE LIGHT ON CONSOLE AND CONFIG SD REMAINED ILLUMINATED FOR 2 MINUTES AFTER RETRACTION. FOUND RIGHT MAIN LANDING GEAR DOWN LOC
- [SDR HALA2018030800072](https://openairdocs.org/sdr/HALA2018030800072), Mar 7, 2018: SLIDE. PARTIAL DEPLOY. PARTIAL MAIN CABIN DOOR SLIDE DEPLOYMENT AT GATE. REPLACED MAIN DOOR SLIDE IAW AMM 25-61-01, SECURITY CHECKED GOOD. OK FOR SERVICE.
- [SDR HALA2017110800271](https://openairdocs.org/sdr/HALA2017110800271), Nov 8, 2017: SPRING. BROKEN. DIVERSION DUE TO A LOUD NOISE FROM NOSE GEAR AFTER TAKEOFF. FOUND A BROKEN ANTI-RETRACTION SPRING ON THE LANDING GEAR HANDLE MODULE. FOUND RIGHT UPPER BANANA FA
- [SDR HALA2016111700516](https://openairdocs.org/sdr/HALA2016111700516), Nov 17, 2016: VALVE. MALFUNCTIONED. RT ENGINE COMPRESSOR STALL AFTER START. REMOVED AND REPLACED THE BYPASS AND VENT VALVE IAW TASK 73-13-04-000-801, 73-13-04-400-801.ENGINE RUN AND LEAK CHECKED G
- [SDR HALA2016110400510](https://openairdocs.org/sdr/HALA2016110400510), Nov 5, 2016: BOLT. BACKED OUT. ATB, FLAP DISAGREE, SLAT DISAG LEVEL 2 DURING SLAT RETRACTION. PERFORMED VISUAL INSPECTION OF WING SLATS. FOUND NR 3 DRIVE SLAT TRACK ATTACHMENT BOLT HITTING LE
- [SDR HALA2016080400317](https://openairdocs.org/sdr/HALA2016080400317), Aug 4, 2016: APU. FAILED. WHILE ON THE GROUND AND BOARDING FOR NEXT FLIGHT, SMELLED ELECTRICAL SMOKE & HEARD 2 LOUD BANGS, AIRPLANE WENT DARK WHEN THE APU SHUTDOWN. VISUAL FLAMES NOTED F
- [SDR HALA2016072800267](https://openairdocs.org/sdr/HALA2016072800267), Jul 28, 2016: SLAT SYSTEM. MALFUNCTIONED. SPLIT SLAT CONDITION WITH ROLLING MOTION WHEN SLATS RETRACTED DURING CLIMBOUT. SLATS NORMAL WHEN EXTENDED. TROUBLESHOT IAW FIM 27-80 TASK 802. VISUAL INSPECTION
- [SDR HALA2016051100178](https://openairdocs.org/sdr/HALA2016051100178), May 11, 2016: LATCH. LOOSE. RIGHT GEAR UNSAFE LIGHT AFTER GEAR RETRACTION. FOUND THAT MLG LATCH WAS LOOSE. REPLACED 4 BOLTS, RESECURED BOLTS IAW AMM 32-34-01 ACCOMPLISHED DOOR LATCH AJUSTM
- [SDR HALA2016031900087](https://openairdocs.org/sdr/HALA2016031900087), Mar 19, 2016: TIRE. FAILED. NR 3 MAIN TIRE BLOWN. FOUND INBD 4" WIDE RETREAD SEPARATED AROUND 7500 PERCENT OF CIRCUMFERENCE OF NR 3 MAIN TIRE, FOUND PRESSURE AT 175 PSIG NR 3, 180 PSIG NR 
- [SDR HALA2016031300078](https://openairdocs.org/sdr/HALA2016031300078), Mar 13, 2016: TIRE. DELAMINATED. NR 2 TIRE DELAMINATING. R & R NR 2 MAIN WHEEL ASSY IAW TASK 32-41-01-00-803, SPIN CHECK, OK.
- [SDR HALA2015050300068](https://openairdocs.org/sdr/HALA2015050300068), May 3, 2015: SMOKE DETECTOR. FALSE ACTIVATION. PARKED AT GATE, LEVEL 1 ALERT CARGO SMOKE AFT SGL DISPLAYED. RESET AFT CARGO SMOKE DETECTOR SYS SWITCH TO NORM POSITION. MESSAGE CLEARED. CARGO SMOKE TEST OK.
- [SDR HALA2015010500006](https://openairdocs.org/sdr/HALA2015010500006), Jan 5, 2015: GUIDE VANE. DAMAGED. NEED TO REMOVE NR 2 ENGINE, DUE TO MISSING MATERIAL ON NGV. NR 2 ENGINE INSTALLED IAW M143-717 ENGINE INSTALLATION. LEAK AND POWER ASSURANCE CHECKED GOOD.
- [SDR HALA2014121300209](https://openairdocs.org/sdr/HALA2014121300209), Dec 13, 2014: COMPRESSOR. STALLED. COMPRESSOR STALL ON LT ENGINE 1000 FT, MAX POWER. ACCOMPLISHED AMM 72-00-00-200-801 FROM PAR D THRU E(3) 15856. REMOVED NR 1 ENGINE IAW M144-717. ENGINE RUN, LE
- [SDR HALA2014102600176](https://openairdocs.org/sdr/HALA2014102600176), Oct 26, 2014: UNKNOWN. SMOKE. EXCESSIVE SMOKE FROM LT ENGINE AFTER START REPORTED FROM RAMP. ALL ENGINE INDICATIONS NORMAL. INSPECTED INLET AND EXHAUST FOR FLUID LEAK NO FLUID FOUND ON NR 1 
- [SDR HALA2014052500067](https://openairdocs.org/sdr/HALA2014052500067), May 25, 2014: ENGINE. STALLED. LEFT ENGINE COMPRESSOR STALL AT ABOUT 1500 FT. INSPECTED ENG IAW AMM 72-00-00, FOUND STAGE 5 HPC ENTIRE TIP MISSING, FWD TO AFT, APPROX .2500. R & R NR 1 ENGINE
- [SDR HALA2014031100034](https://openairdocs.org/sdr/HALA2014031100034), Mar 11, 2014: PSEU. MALFUNCTIONED. PSEU FAULTS RT GEAR UP/LATCHED SENSOR. DIVERTED, REPLACED SENSOR D1-1058. OPS CHECKED OK IAW AMM 32-61-00. PSEU RTS TEST PASSED. OK FOR SERVICE.
- [SDR HALA2013081400102](https://openairdocs.org/sdr/HALA2013081400102), Aug 14, 2013: MOTOR. INOPERATIVE. PRIMARY TRIM CONTROL FAILED IN FLIGHT, DIVERTED. R & R PRIMARY DRIVE TRIM MOTOR IAW AMM TASK 27-41-10-400-801. OPS CHECKED OK. INSTALLED PANEL AND APPLIED SEALA
- [SDR HALA2012030600106](https://openairdocs.org/sdr/HALA2012030600106), Mar 6, 2012: COMPUTER. MALFUNCTIONED. RUDDER LIMIT FAILED HIGH SPEED PROTECTION A/S UNREADABLE BOTH SIDES A/P DISENGAGED AUTOTRIM FAIL. PERFORMED AMM 34-11-00-200-801 INSPECTION OF PITOT SYS FOR ACC
- [SDR HALA2012022700090](https://openairdocs.org/sdr/HALA2012022700090), Feb 27, 2012: STATIC WICK. BROKEN. RT WING SCRATCHED POSITION LIGHT LENS, SCRATCHED UNDERSIDE OF WINGTIP AND BROKE OFF STATICK WICK. BLENDED SCRATCH ON RT WINGTIP SKIN OTBD AREA NEAR STATIC WICKS
- [SDR HALA2012022500075](https://openairdocs.org/sdr/HALA2012022500075), Feb 25, 2012: SKIN. DAMAGED. RT WING TIP SKIN DAMAGE DURING PUSHBACK. OPEN
- [SDR HALA2011102100481](https://openairdocs.org/sdr/HALA2011102100481), Oct 21, 2011: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS AT ROW 12-18 SEATS, NOT WORKING. R & R EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-03. OPS CHECKED GOOD .
- [SDR HALA2011101800470](https://openairdocs.org/sdr/HALA2011101800470), Oct 18, 2011: FLAP SYSTEM. MALFUNCTIONED. AFTER TAKEOFF: WHEN RETRACTING FLAPS FROM 18 OR 13 DEGREES TO SLATS/0 DEGREES THERE IS A SHUDDER. THROUGH THE ACFT THAT FEELS LIKE A HYD PROBLEM NOT A FLAP POSI
- [SDR HALA2011020500077](https://openairdocs.org/sdr/HALA2011020500077), Feb 7, 2011: UNKNOWN. ODOR. STRANGE ODOR IN ACFT ON GRND. INSPECTED O/H BINS, AFT ACCESS COMPT, COCKPIT,GALLEYS, BAG BINS, WHEEL WELL, E/E COMPT, APU COMPT, RAN BOTH ENGS & PACK WITH AND W
- [SDR HALA2010120600578](https://openairdocs.org/sdr/HALA2010120600578), Dec 7, 2010: PROXIMITY SENSOR. OUT OF ADJUST. AIR TURN BACK DUE "ACC COMP DOOR" LIGHT CAME ON CLIMBING OUT OF 9,000' ACCOMPLISHED AMM 52-70-01 ADJUSTMENT OF THE FWD ACCESSORY COMPARTMENT DOOR PROXIMITY SENS
- [SDR HALA2010101800475](https://openairdocs.org/sdr/HALA2010101800475), Oct 18, 2010: DOUBLER. CRACKED. LT APRON LOWER AFT COWL LATCH CUTOUT DOUBLER REPAIR .2500" CRACK. REPLACED REPAIR DOUBLER IAW HALM105 FILE B10192, REV D.
- [SDR HALA2010022100067](https://openairdocs.org/sdr/HALA2010022100067), Feb 21, 2010: ACTUATOR. LEAKING. HYD R QTY LO, HYD R PRESS LO, HYD R OFF, DECLEARED AN EMERGENCY. FOUND LT MLG RETRACT ACTUATOR FAIL LEAK. REMOVED AND REPLACED LT MLG RETRACT ACT PER AMM 32-33-
- [SDR HALA2010011700028](https://openairdocs.org/sdr/HALA2010011700028), Jan 17, 2010: REGULATOR VALVE. FAULTED. BLEED AIR RIGHT OFF AND AIR SYSTEM FAULT. REMOVED AND REPLACED RIGHT ENGINE PILOT PRESS REGULATOR VALVE PER AMM 36-12-03-000-801, REMOVED AND REPLACED HOSE ALSO
- [SDR HALA200909150408](https://openairdocs.org/sdr/HALA200909150408), Sep 16, 2009: SKIN. CRACKED. .5 INCH CRACK ON FUSELAGE SKIN AT BS 1022, APPROX 4 INCHES ABOVE NR 2 PYLON. REPAIRED PER HAL105 487115 DOUBLER REPAIR.
- [SDR HALA2009042700164](https://openairdocs.org/sdr/HALA2009042700164), Apr 27, 2009: SKIN. CRACKED. 8 INCH CRACK ON LEFT VERTICAL SKIN FWD JACKSCREW CUTOUT. REPAIR IN WORK. CRACK VERIFIED BY EDDY CURRENT. REMOVED LT VERTICAL STABILIZER TIP SKIN. ALL GAPS CHECK
- [SDR HALA2009021000044](https://openairdocs.org/sdr/HALA2009021000044), Feb 10, 2009: STATOR. FAILED. ATB - ENG LEFT SYSTEM FAILURE DURING CLIMB. T/S IAW FIM 73-21 TASK 813 AND FIM 77-12 802. REMOVED AND REPLACED RIGHT DEDICATED GENERATOR STATOR IAW AMM 73-21-04
- [SDR HALA2009010500004](https://openairdocs.org/sdr/HALA2009010500004), Jan 5, 2009: LAMP. INOPERATIVE. ATB - PSEU FAIL LIGHT CAME ON INFLIGHT. PERFORMED FIM 32-60 TASK 801, FOUND FAULT CODE 326213 "R GEAR INDICATOR GREEN LAMP OPEN/GROUND" BOTH LAMPS WERE BURNED O
- [SDR HALA2008122700907](https://openairdocs.org/sdr/HALA2008122700907), Dec 27, 2008: UNKNOWN. VIBRATION. AIRFRAME VIBRATION ABOVE FL250 IN CLIMB AND LEVEL AT FL260. PERFORMED GENERAL VISUAL INSPECTION OF EXTERNAL AREAS OF AIRCRAFT. FLIGHT CONTROLS AND GEAR DOORS, F
- [SDR HALA0800607](https://openairdocs.org/sdr/HALA0800607), May 30, 2008: TIRE. SEPARATED. NR 4 TIRE RECAP SEAM SEPARATING. REMOVED AND REPLACED NR 4 MLG TIRE ASSY PER AMM 32-41-01. SECURITY CHECK OKAY.
- [SDR HALA0800520](https://openairdocs.org/sdr/HALA0800520), Apr 8, 2008: UNKNOWN. UNKNOWN. ENGINE AND ALERT DISPLAY WHITE BOXED FLAP INDICATION. ACCOMPLISHED AMM 27-50-01, NO FAULTS NOTED. ACCOMPLISHED FIM 27-50-00 FIG 104 NO FAULTS. ACCOMPLISHED FIM 

All 64: https://openairdocs.org/aircraft/N487HA/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/N487HA/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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