# N480HA: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55125
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 20, 2001
- Certificate issued: June 28, 2011
- Expires: June 30, 2027
- Mode S code: A5E949
- 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=480HA
- Page: https://openairdocs.org/aircraft/N480HA

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 BMW Rolls 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 (BMW Rolls 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/N480HA/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 N480HA.

## FAA accident and incident reports

None matched to N480HA.

## Service difficulty reports (77, 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 ASAA2026092967162](https://openairdocs.org/sdr/ASAA2026092967162), Sep 29, 2026: SIGN. DETACHED. FORWARD EXIT SIGN FELL OFF. GROUNDED - YES. RESECURED EMERGENCY EXIT SIGN AT ROW 2. OK FOR SERVICE.
- [SDR ASAA2026081966418](https://openairdocs.org/sdr/ASAA2026081966418), Aug 19, 2026: GUST LOCK. LACK OF LUBE. MAIN ENTRY DOOR GUST LOCK HARD TO RELEASE TO CLOSE DOOR. GROUNDED - YES. CLEANED AND LUBRICATED MAIN ENTRY DOOR LATCH. OPS CHECK GOOD. OK FOR SVC.
- [SDR ASAA2026051264720](https://openairdocs.org/sdr/ASAA2026051264720), May 12, 2026: LATCH. UNSECURE. MAIN CABIN DOOR (1L) HAVING DIFFICULTY CLOSING/ STICKING. GROUNDED - YES. RESECURED 1L DOOR LATCH SCREWS. 2 EA . OPS AND SECURITY CHECK GOOD. OK FOR SVC.
- [SDR ASAA2026040464164](https://openairdocs.org/sdr/ASAA2026040464164), Apr 4, 2026: BATTERY. INOPERATIVE. LINE REPORTED EMERGENCY LIGHTS AT ROWS 21- 25 INOP. GROUNDED - YES. REPLACED EMERGENCY LIGHT BATTERY AT POSITION B5-231 PER AMM 33-51-03. OPS CHECK GODD.
- [SDR HALA20231002042](https://openairdocs.org/sdr/HALA20231002042), Sep 29, 2023: UNKNOWN. UNKNOWN. TAIL CATWALK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BOTH THE EMERGENCY LIGHT BATTERY AND BATTERY POWER SUPPLY UNIT PER AMM 33-51-03. OPS CHECK GOOD. OK FOR
- [SDR HALA2023031400006](https://openairdocs.org/sdr/HALA2023031400006), Mar 7, 2023: UNKNOWN. UNKNOWN. INTERMITTENT L HYD PUMP FAIL. REMOVED AND REPLACED LH ENGINE DRIVEN HYD PUMP PER B717 AMM 29-11-01. CONDITION SAME. REMOVED AND REPLACED LH ENGINE EDP LOW PRESS
- [SDR HALA2022052300104](https://openairdocs.org/sdr/HALA2022052300104), May 22, 2022: NONE. NONE. ATB- ENG L FADEC ALTERNATE (AIRBORNE) WOULD NOT RESET // PERFORMED FIM 71-00 TASK 812. NO FAULTS FOUND. RAN #1 ENG TWICE. BOTH RUNS NO DEFECTS NOTED. OK FOR SVC
- [SDR HALA2020102700195](https://openairdocs.org/sdr/HALA2020102700195), Oct 26, 2020: PIN. BROKEN. DOOR 1L LIFERAFT PIN BROKEN. RESECURED GIRT BAR AT 1L DOOR. OPERATIONS CHECK OK.
- [SDR HALA2020050200102](https://openairdocs.org/sdr/HALA2020050200102), May 1, 2020: BATTERY. DISCHARGED. EXTERIOR EMERGENCY LIGHTS WILL NOT ILLUMINATE. // REMOVED AND REPLACED OVER WING EMERGENCY EVACUATION BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. OK 
- [SDR HALA2019040400168](https://openairdocs.org/sdr/HALA2019040400168), Apr 3, 2019: CONTROL UNIT. UNKNOWN. ATB - ANTI-SKID FAIL. // REMOVED AND REPLACED BCU PER AMM 37-45-01. RTS TEST PASSED. OK FOR SVC.
- [SDR FOTR20180926001](https://openairdocs.org/sdr/FOTR20180926001), Sep 11, 2018: SKIN. DENTED. DENT AND GOUGE FOUND ON LEFT HAND AFT FUSELAGE BETWEEN STATION 927-946 STRINGER 18-15L.
- [SDR HALA2018062900316](https://openairdocs.org/sdr/HALA2018062900316), Jun 28, 2018: SMOKE DETECTOR. MALFUNCTIONED. LAVATORY SMOKE ALERT DISPLAYED. MOVED LAVATORY SMOKE DETECTOR TEST SWITCH TO OFF POSITION. MESSAGE CLEARED. OK FOR SERVICE.
- [SDR HALA2018062100293](https://openairdocs.org/sdr/HALA2018062100293), Jun 20, 2018: THERMOCOUPLE. MALFUNCTIONED. DURING CLIMB OUT, A LEVEL 2 APU EGT HIGH LIGHT ILLUMINATED INTERMITTENT. APU THERMOCOUPLE 1 OPEN CIRCUIT MESSAGE. REMOVED AND REPLACED NR 1 APU THERMOCOUPLE IAW
- [SDR HALA2017120300290](https://openairdocs.org/sdr/HALA2017120300290), Dec 3, 2017: RETRACT CYLINDER. FAULTY. AFTER T/O L&R MAIN GEAR INDICATED UNSAFE. REMOVED & REPLACED LT MAIN LANDING GEAR RETRACT CYLINDER.
- [SDR HALA2017080800218](https://openairdocs.org/sdr/HALA2017080800218), Aug 8, 2017: COMPRESSOR. STALLED. COMPRESSOR STALL LEFT ENG, LOUD BANG/SMELLED FUMES THEN ENG L COMP STALL ON EAD. ENGINE CHANGE IN WORK.
- [SDR HALA2017071200183](https://openairdocs.org/sdr/HALA2017071200183), Jul 12, 2017: ENGINE. DAMAGED. LEFT ENGINE HAD SEVERE DAMAGE.
- [SDR HALA2017052500123](https://openairdocs.org/sdr/HALA2017052500123), May 25, 2017: UNKNOWN. ODOR. ODOR THROUGH TAKEOFF TO 3000FT, THE ELECTRICAL BURNING ODOR EVENTUALLY WENT AWAY. CHECKED CIRCUIT BREAKERS, TURNED ON ALL FLIGHT DECK LIGHTS, CHECKED E & E BAY,
- [SDR HALA2017053000124](https://openairdocs.org/sdr/HALA2017053000124), May 24, 2017: FAN. FAILED. AFTER TAKEOFF TO 3000 FT, HAD AN ELECTRICAL BURNING ODOR, EVENTUALLY WENT AWAY. FOUND THE NR 1 ADIRU FAN FROZEN AND BURNED. REPLACED THE FAN IAW AMM 34-43-05. O
- [SDR HALA2016101140368](https://openairdocs.org/sdr/HALA2016101140368), Oct 14, 2016: LATCH. OUT OF ADJUST. OPEN: ATB, RT GEAR UNSAFE LIGHT AFTER TO. MX NEEDS TO ADJUST THE RT MLG UPLOCK LATCH AND OPS CHK. MX IS REPLACING THE DOWN LOCK ELEC CONDUIT.
- [SDR HALA2016101100368](https://openairdocs.org/sdr/HALA2016101100368), Oct 11, 2016: LATCH. OUT OF ADJUST. RIGHT GEAR UNSAFE LIGHT ILLIMINATED AFTER TAKE OFF. ACCOMPLISHED FUNCTIONAL TEST OF MAIN & NOSE GEAR IAW AMM 32-30-00-720-801. OPS CHECKED OK. FOUND MAIN GEAR R
- [SDR HALA2016091400352](https://openairdocs.org/sdr/HALA2016091400352), Sep 14, 2016: BATTERY. DISCHARGED. EMERGENCY LIGHT IN COCKPIT DOES NOT ILLUMINATE WHEN ON POSITION. R & R BATTERY AT B5-123 IAW WDM 33-51-12. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2016063000265](https://openairdocs.org/sdr/HALA2016063000265), Jun 30, 2016: DUCT. DISCONNECTED. F/A REPORTED AFT DOOR HOT TO FEEL. FOUND LEFT PACK DISHCHARGE ELBOW DUCT DISSCONECTED. REATTACHED DUCT RAN PACK, NO LEAK NOTED OK TO CONTINUE SECURITY CHECK GOO
- [SDR HALA2016051400247](https://openairdocs.org/sdr/HALA2016051400247), May 14, 2016: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK HAS SCRATCHES AND GOUGES BETWEEN STA 646-823, RBL 22. BLENDED OUT SCRATCHES AND GOUGES AT MAIN CABIN SEAT TRACK BETWEEN STA 646-823, RBL 2
- [SDR HALA2016051400249](https://openairdocs.org/sdr/HALA2016051400249), May 14, 2016: TAB. CRACKED. MAIN CABIN TAB CRACKED ON DOOR SURROUNDED INNER SKIN AT STA 210, LONG 15L, CRACK IS 1" LONG. REMOVED DAMAGED TAB ON INNER SKIN AT FS 210 AND REPAIRED IAW SRM 53
- [SDR HALA2016051400248](https://openairdocs.org/sdr/HALA2016051400248), May 14, 2016: TAB. CRACKED. MAIN CABIN TAB CRACKED ON DOOR SURROUNDED INNER SKIN AT STA 210, LONG 15L, CRACK IS 1" LONG. REMOVED DAMAGED TAB ON INNER SKIN AT FS 210 AND REPAIRED IAW SRM 53
- [SDR HALA2016051300245](https://openairdocs.org/sdr/HALA2016051300245), May 13, 2016: PAN. CORRODED. FUSE AFT CARGO COMPARTMENT LOWER DOOR PAN BS 974 HAS EXFOLIATED CORROSION. REPAIRED PAN AT AFT CARGO COMPARTMENT LOWER DOOR, BS 974 TO 954 IAW SRM 53-20-15-2R-7
- [SDR HALA2016051300182](https://openairdocs.org/sdr/HALA2016051300182), May 13, 2016: PAN. CORRODED. AFT CARGO COMPARTMENT LOWER DOOR PAN BS 974 HAS EXFOLIATED CORROSION.
- [SDR HALA2016051200246](https://openairdocs.org/sdr/HALA2016051200246), May 12, 2016: SUPPORT. CORRODED. CORROSION ON FALSE TRACK STA 1002, RBL 18. REMOVED -65 AND -67 SUPPORTS IAW SRM 51-41-01. REMOVED CORROSION FROM SUPPORTS, -65 SUPPORT WITHIN LIMITS, -67 SUPPOR
- [SDR HALA2016051000248](https://openairdocs.org/sdr/HALA2016051000248), May 10, 2016: DOUBLER. CRACKED. CRACK ON GROUND CONDITION AIR ACCESS DOOR LANDING, FWD INBD CORNER AND AFT INBD CORNER. R & R CRACKED DOUBLER AT GROUND CONDITIONED AIR ACCESS DOOR LANDING IAW 
- [SDR HALA2016050700175](https://openairdocs.org/sdr/HALA2016050700175), May 7, 2016: HF COMM. MALFUNCTIONED. HF RADIO UNABLE TO UNDERSTAND TRANSMISSIONS FROM OTHER ACFT AND FROM ATC, VERY GARBLED. TRIED 3 DIFFERENT FREQUENCIES ALL SAME. SET HF FOR USB OPERATION. OPS CH
- [SDR HALA201512060242](https://openairdocs.org/sdr/HALA201512060242), Dec 9, 2015: HYDRAULIC SYSTEM. CONTAMINATED. ATO- HYD L TEMP HIGH ON T/O ROLL. MAINTENANCE FOUND EXCESSIVE AIR IN HYDRAULIC SYS RESERVOIR, BLEED OFF HYD SYS. CHECKED BYPASS VALVES. OPS CHECK GOOD, ACFT REL
- [SDR HALA2015FA0000640](https://openairdocs.org/sdr/HALA2015FA0000640), Dec 9, 2015: HYDRAULIC SYSTEM. MALFUNCTIONED. ABORTED TAKEOFF. HYD LOW TEMP HIGH ON T/O ROLL. MAINTENANCE FOUND EXCESSIVE AIR IN HYD SYS RES. BLEED OFF HYD SYS. CHECKED BYPASS VALVES. OPS CHECK GOOD, ACFT R
- [SDR HALA2015090300182](https://openairdocs.org/sdr/HALA2015090300182), Sep 3, 2015: SENSOR. FAULTED. DURING CLIMB, ENROUTE, LEVEL 1 ENGINE RT SYS. FAIL ALERT DISPLAYED ON SECONDARY ENGINE PAGE. FOUND FAULT CODE 771202, R & R HP SPEED PROBE SENSOR U1019 IAW AMM 
- [SDR HALA2015072400141](https://openairdocs.org/sdr/HALA2015072400141), Jul 24, 2015: MOTOR. INOPERATIVE. PRIMARY TRIM INOPERATIVE. R & R PRIMARY STABILIZER TRIM MOTOR IAW AMM 27-41-10-400-801.
- [SDR HALA2013120200174](https://openairdocs.org/sdr/HALA2013120200174), Dec 2, 2013: SKIN. DAMAGED. RT INBD FLAP T/E HAS IMPACT DAMAGE. OPEN
- [SDR HALA2013101300134](https://openairdocs.org/sdr/HALA2013101300134), Oct 13, 2013: PRESSURE SWITCH. MALFUNCTIONED. LEFT ENGINE FUEL PRESSURE LEVEL ALERT DISPLAYED DURING TAXING FOR TAKEOFF. R & R LT ENGINE LOW PRESSURE SWITCH. OPS CHECK COMPLETE, LEAK CHECK COMPLETE IAW AMM 
- [SDR HALA2013080900099](https://openairdocs.org/sdr/HALA2013080900099), Aug 9, 2013: PROXIMITY SENSOR. MALFUNCTIONED. DIVERSION TO ALTERNATE STATION. RED GEAR UNSAFE LIGHT ON RT GEAR AFTER ROTATION CYCLED GEAR DOWN/UP AND ALL INDICATIONS NORMAL. R & R LT MAIN GEAR UP & LATCH PR
- [SDR HALA2012011500030](https://openairdocs.org/sdr/HALA2012011500030), Jan 15, 2012: SLIDE. DAMAGED. SERVICE DOOR SLIDE LOWER RELEASE PIN, MISSING TAMPER STRING. R & R FWD SERVICE DOOR EMERGENCY SLIDE IAW AMM 25-61-03 CONDITION & SECURITY CHECK OK. OK FOR SERVI
- [SDR HALA2011062000272](https://openairdocs.org/sdr/HALA2011062000272), Jun 20, 2011: CONTROL VALVE. DEFECTIVE. GEAR DOOR OPEN ALERT CAME ON APPROX 10 SEC AFTER GEAR EXTENTION, STAYED ON F/O APPROX 6SEC. PERFORMED AMM 32-33-00-720-801, FUNCTIONAL TEST OF THE LANDING GEAR 
- [SDR HALA2011020400076](https://openairdocs.org/sdr/HALA2011020400076), Feb 4, 2011: UNKNOWN. ODOR. F/A REPORTED STRONG ELECTRICAL ODOR IN FWD CABIN AFTER ENGINE START. INSPECTED E/E, AFT ACCESS COMPT, APU COMPT, BAG BINS, WHEEL WELLS, CABIN O/H COMPTS. CLOSED
- [SDR HALA2010050400203](https://openairdocs.org/sdr/HALA2010050400203), May 5, 2010: DUCT. DISLODGED. ENROUTE, DUCTING FOR EXTERNAL AC CAME LOOSE, LOST PRESSURIZATION. REINSTALLED FLEX HOSE COUPLING TO RIGID TUBING IN EXTERNAL AIR CONDITIONING DUCT ABOVE CHECK V
- [SDR HALA2010041800181](https://openairdocs.org/sdr/HALA2010041800181), Apr 18, 2010: RELEASE CABLE. FRAYED. TAIL CONE RELEASE HANDLE LT SIDE CABLE ASSY HAS SEVERAL BROKEN STRANDS AND IS RUSTED AT TERMINAL END. REMOVED TAIL CONE RELEASE HANDLE, LT SIDE CABLE ASSY REF B
- [SDR HALA2010021800064](https://openairdocs.org/sdr/HALA2010021800064), Feb 18, 2010: EEC. FAULTED. SELECT FADEC ALTN ALERT DURING CLIMB LT ENG. OK TO CONTINUE IAW A 73-21-01.CODE 73-21-05. R & R NR 1 ENG EEC ASSY IAW AMM 73-21-0111. OPS CK OK, NO FAULTS NOTED
- [SDR HALA2010020100042](https://openairdocs.org/sdr/HALA2010020100042), Feb 1, 2010: SKIN. DAMAGED. ON WALK AROUND F/O NOTICED DENT JUST BELOW AFT STATIC PORT ON RT SIDE OF ACFT. FOUND CREASE BELOW AFT STATIC PORT APPROX 7" X 3/4', DEPTH .020" AT STA 342 BETWE
- [SDR HALA2009101900477](https://openairdocs.org/sdr/HALA2009101900477), Oct 19, 2009: BULB. INOPERATIVE. 11D EMERGENCY PATH LIGHT INOP. REPLACED 11D EMERGENCY LIGHT BULB AND LENS. OPS CK GOOD.
- [SDR HALA2009083000394](https://openairdocs.org/sdr/HALA2009083000394), Aug 30, 2009: LATCH. SHEARED. "GEAR DOOR OPEN" LIGHT ILLUMINATED AT GATE. FOUND UPLATCH SHEARED OFF. INSPECTED LT MLG. REMOVED AND REPLACED LT GEAR DOOR UP LATCH ARM. OPS CHK OK. NO OTHER DE
- [SDR HALA2009072000318](https://openairdocs.org/sdr/HALA2009072000318), Jul 20, 2009: SKIN. CORRODED. LEVEL 2 CORROSION ON THE LOWER TCAS ANTENNA BASE. REPAIR IN WORK.
- [SDR HALA2009040700137](https://openairdocs.org/sdr/HALA2009040700137), Apr 7, 2009: LONGERON. CRACKED. CRACK, 2 1/2 INCH LONG ON AFT ACCY, FUSELAGE FRAME STATION 1116, LONGERON 12R. REPAIR IN WORK.
- [SDR HALA2009040500125](https://openairdocs.org/sdr/HALA2009040500125), Apr 5, 2009: ACTUATOR. MALFUNCTIONED. ENROUTE TO LIH OTBD SPOILER FAIL LIGHT ILLUMINATED IN FLIGHT. RETURNED TO HNL. SECU FAULT REVIEW FOUND SPOILER HOLD DOWN FAULT LT OTBD LVDT PROBABLY CAN'T HOLD 
- [SDR HALA2009032000096](https://openairdocs.org/sdr/HALA2009032000096), Mar 20, 2009: ANTI-ICE VALVE. INOPERATIVE. "ENG R ANTI-ICE DISAG" LEVEL ALERT ILLUMINATED DURING IN-FLIGHT ANTI-ICE CHECK. REMOVED AND REPLACED RT ENG NOSE COWL ANTI-ICE VALVE IAW AMM 30-21-01. OPS CK GO

All 77: https://openairdocs.org/aircraft/N480HA/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/N480HA/stcs.md

## Related

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

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