# N479HA: 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: 55124
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 12, 2001
- Certificate issued: June 29, 2011
- Expires: June 30, 2027
- Mode S code: A5E339
- 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=479HA
- Page: https://openairdocs.org/aircraft/N479HA

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/N479HA/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 N479HA.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20160112001419I](https://openairdocs.org/incident/20160112001419I), Jan 12, 2016: Boeing 717-200 (N479HA), HI, Minor damage. While in cruise flight between honolulu and Kahului, maui a hawaiian airlines Boeing 717 flight crew received a cargo smoke indication from the aft cargo…
- [Incident 20010917025219I](https://openairdocs.org/incident/20010917025219I), Sep 17, 2001: Boeing 717200 (N479HA), Kahului, HI. (-23) Pilot started right engine during pushback. He had a tailwind of at least 20 knots. Winds at time of start was 080 at 31 knots. The start went hot and…

## Service difficulty reports (122, 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 ASAA2026060465093](https://openairdocs.org/sdr/ASAA2026060465093), Jun 4, 2026: DOOR. BINDING. 1L DOOR HARD TO CLOSE. GROUNDED - YES. FOUND EXCESS SEALANT INHIBITING/BLOCKING DOOR STOPS 1L. REMOVED EXCESS SEALANT. LUBRICATED DOOR HANDLE MECHANISM, BOYNNET
- [SDR ASAA2026041664326](https://openairdocs.org/sdr/ASAA2026041664326), Apr 16, 2026: HANDLE. BINDING. FWD ENTRY DOOR HANDLE HARD TO CLOSE. GROUNDED - YES. MED OP CHECKS GOOD. OK FOR SERVICE.
- [SDR ASAA2026031263792](https://openairdocs.org/sdr/ASAA2026031263792), Mar 12, 2026: DOOR. FOD. BOARDING DOOR HARD TO CLOSE. GROUNDED - YES. REMOVED DEBRIS FROM MAIN ENTRY DOOR. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR ASAA2026010962824](https://openairdocs.org/sdr/ASAA2026010962824), Jan 9, 2026: BATTERY. INOPERATIVE. CABIN AND COCKPIT EMERGENCY LIGHTS NOT WORKING. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY SUPPLIES 221CC, 221FC, & 222AR, OPS CHKD OK. OK FO
- [SDR ASAA2025112161814](https://openairdocs.org/sdr/ASAA2025112161814), Nov 21, 2025: HANDLE. LACK OF LUBE. MAIN CABIN DOOR INSIDE HANDLE DIFFICULT TO MOVE. GROUNDED - YES. LUBRICTED MED HANDLE. OPS CHECK GOOD.
- [SDR HALA20250908049](https://openairdocs.org/sdr/HALA20250908049), Sep 5, 2025: BATTERY PACK. INOPERATIVE. CAT WALK EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY ASSY. B5-260 PER AMM 33-51-03. OPERATIONAL CHECKED OK.
- [SDR HALA20250731041](https://openairdocs.org/sdr/HALA20250731041), Jul 30, 2025: POWER SUPPLY. INOPERATIVE. OVERWING EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. AC OK TO CONTINUE SERVIC
- [SDR HALA20250218008](https://openairdocs.org/sdr/HALA20250218008), Feb 16, 2025: PUMP. FAULTED. "INFO TO MX" RTO;BTB TAKEOFF AND THROTTLE ADVANCE LEFT ENGINE N1 STAGNANT. L ENGINE N1 AT 25 WHEN R ENGINE AT N1 55. REMOVED AND REPLACED FUEL PUMP ENG #1 REF A
- [SDR HALA20250213006](https://openairdocs.org/sdr/HALA20250213006), Feb 12, 2025: COMPRESSOR. STALLED. LVL 2- ENG L COMP STALL ON EAD DURING LANDING ( NO OTHER INDICATIONS). PERFORMED FIM 72-00 TASK 803, REMOVED AND REPLACED LH ENG N2 SHARED SPEED PROBE PER AMM 7
- [SDR HALA202411290077](https://openairdocs.org/sdr/HALA202411290077), Nov 28, 2024: WINDOW. CRACKED. POSSIBLE CRACK IN LOWER PORTION OF CO PILOT WINDSHEILD APPROX 1 INCH. REMOVED RIGHT AND CENTER FAIRING COVER AND WINDSHEILD WIPER AMM 56-11-02-801 25000. REMOVE
- [SDR HALA20240819041](https://openairdocs.org/sdr/HALA20240819041), Aug 17, 2024: WINDSHIELD. CRACKED. CAPTAIN SIDE WINDSHIELD CRACKED IN FLIGHT. REMOVED AND INSTALLED NEW CAPTAIN SIDE WINDSHIELD PER AMM 56-11-02 UP TO STEP E (7).(B) NEED TO CONTINUOUS FROM E.(8)
- [SDR HALA20240223009](https://openairdocs.org/sdr/HALA20240223009), Feb 22, 2024: POWER SUPPLY. INOPERATIVE. MULTIPLE CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY (B5-231, B5-119, B5-259 & B5-227) PER AMM 33-51-03. OPS CHECK GOOD. OK FOR SVC
- [SDR HALA20240102001](https://openairdocs.org/sdr/HALA20240102001), Dec 29, 2023: UNKNOWN. UNKNOWN. BTB L ENGINE COMPRESSOR STALL ON TAKEOFF ROLL AS SOON AS TAKEOFF POWER APPLIED LOUD BANG. REMOVED L/H ENG PER T/C E1128-717-71-003-REMOVAL W/O 280784
- [SDR HALA20231219051](https://openairdocs.org/sdr/HALA20231219051), Dec 19, 2023: COMPUTER. FAULTY. ATB - DUAL FMS FAIL INFLIGHT. PERFORMED FIM 34-63 TASK 830 "FMS DUAL FAIL". VIA 1 & 2 RTS PER AMM 31-43-00-741-803, TESTS OK. REMOVED AND REPLACED FCC-1 AS PREC
- [SDR HALA20231103048](https://openairdocs.org/sdr/HALA20231103048), Nov 2, 2023: UNKNOWN. UNKNOWN. COCKPIT OVERHEAD EMERGENCY LIGHT DOESNT STAY ON (ILLUMINATES MOMENTARILY) WHEN "EMER LT" SWITCH IS PLACED "ON". ALL OTHER EMER LIGHTS APPEAR OPERATIONAL. REMOVE
- [SDR HALA2023012600001](https://openairdocs.org/sdr/HALA2023012600001), Jan 24, 2023: BATTERY PACK. INOPERATIVE. FWD 1/3 OVHD EMER CEILING LTS INOP. REMOVED AND REPLACED EMER LIGHT BATTERIES ON EMER LIGHT BATTERY POWER SUPPLIES B5-227, B5-230 AND B5-259. OPS CHECK OK PER A
- [SDR HALA2022102100002](https://openairdocs.org/sdr/HALA2022102100002), Oct 20, 2022: APU. ODOR. PER LINE MX MANGEMENT PILOT / CREW REPORT DIRTY SOCK SMELL FROM A/C SYS FOUND OIL LEAKING IN APU. REMOVED AND REPLACED APU PER TASK CARD 717-49-HWI-04-01, OPS C
- [SDR HALA2022072700137](https://openairdocs.org/sdr/HALA2022072700137), Jul 26, 2022: WATER SEPARATOR. DIRTY. FIRST FLIGHT ATTENDANT REPORTS ODOR SMELL COMING FWD AIR CONDITIONING DUCT//REPLACED BOTH AC WATER SEPARATORPER AMM 21-54-01. SECURITY CHECK OK. NO ODOR SMELL N
- [SDR HALA2022070500125](https://openairdocs.org/sdr/HALA2022070500125), Jul 2, 2022: NONE. NONE. ELECTRICAL ODOR THROUGHOUT CABIN & COCKPIT.// OPERATED #1 &2 ENGINE WITH L/R PACKS & HAD SLIGHT SMELL OF OIL, REPLACED COALESSER BAGS PER AMM 21-54-08-400-801 P
- [SDR HALA2021051700062](https://openairdocs.org/sdr/HALA2021051700062), May 16, 2021: LIFE VEST. UNPACKED. EMER EQ - LIFE PRESERVER AT PASSENGER SEAT 16B HAS BEEL PULLED OUT FROM HOUSING // REMOVED AND REPLACED LIFEVEST SEAL. SECURITY CHECK GOOD. OK FOR SVC.
- [SDR HALA2021012000009](https://openairdocs.org/sdr/HALA2021012000009), Jan 19, 2021: EEC. DEFECTIVE. ATB - INFLIGHT SEL FADEC ALT AND ENGINE L SYSTEM FAULT WITH ACCOMPANYING LOUD BANG FROM ENGINE. REMOVED AND REPLACED NR 1 ENGINE EEC, IAW AMM 73-21-01/401. SECU
- [SDR HALA2020050100101](https://openairdocs.org/sdr/HALA2020050100101), Apr 30, 2020: ACCESS PANEL. DELAMINATED. FOUND #1 ENGINE ACCESS PANEL 412CR DE-LAMINATED. // REMOVED AND REPLACED #1 ENGINE ACCESS PANEL 412CR PER AMM 74-20-04 SECURITY CHECK GOOD OK FOR SERVICE.
- [SDR HALA2020032800079](https://openairdocs.org/sdr/HALA2020032800079), Mar 27, 2020: TERMINAL. BROKEN. AIR DIVERSION - R ENG SYS FAIL. // INSPECTED #2 ENG TGT HARNESS AND FOUND TERMINAL T1040-2 LEG BROKEN. REMOVED AND REPLACED PER 71-52-01. OPS CK PENDING. RAN EN
- [SDR HALA2020013110023](https://openairdocs.org/sdr/HALA2020013110023), Jan 30, 2020: WARNING MESSAGE. ILLUMINATED. ENGINE LEFT FUEL PRESSURE ON STATUS PAGE., OK TO CONTINUE, DEFERED PER MEL 73-33-01
- [SDR HALA2019121900524](https://openairdocs.org/sdr/HALA2019121900524), Dec 18, 2019: COALESCER BAG. ODOR. ON TAKEOFF OR FINAL GETTING STRONG CHEMICAL SMELL IN COCKPIT. // REMOVED & REPLACED LEFT PACK COALESCER BAG PER AMM 21-54-08. NO SMELL FROM PACK LEFT OR PACK RI
- [SDR HALA2019102500458](https://openairdocs.org/sdr/HALA2019102500458), Oct 24, 2019: LAMP. INOPERATIVE. "AFT EMERGENCY EXIT LIGHT INOP'. // RELAMPED AFT EMERGENCY EXIT LIGHT AS REQUIRED. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2019031500128](https://openairdocs.org/sdr/HALA2019031500128), Mar 14, 2019: CONTROL SYSTEM. LACK OF LUBE. BINDING IN YOKE AT ABOUT 30 DEG. OF LEFT YOKE. ACCOMPLISHED FIM TASK 27-10-803 CLEANED AND LUBED AILERON TRANSITION SECTOR. AILERON CONTROL SYSTEM TEST OK.
- [SDR HALA2018110600569](https://openairdocs.org/sdr/HALA2018110600569), Nov 5, 2018: INDICATION SYS. FALSE INDICATION. INFLIGHT BRAKE OVERHEAT QRH PROCEDURES WERE COMPLETED.// INSPECTED ALL MLG BRAKES NO DEFECTS NOTED PER 32-43-01, BRAKES COOLED DOWN TO DISPATCH ABLE LEVEL WHEN 
- [SDR HALA2018102400539](https://openairdocs.org/sdr/HALA2018102400539), Oct 23, 2018: CONTROL CABLE. SEVERED. OPEN - RIGHT WING NR 5 SLAT RETRACT CABLE (204A) FOUND SEVERED. REPAIR IN WORK.
- [SDR HALA2017122000307](https://openairdocs.org/sdr/HALA2017122000307), Dec 19, 2017: SENSOR. MALFUNCTIONED. RECEIVED A BLEED AIR LT FAIL, WHILE CLIMBING THRU 10,000. RETURNED TO DEPARTURE. REPLACED THE LT PM SENSOR IAW AMM 36-12-04. ENGINE RUN CHECKED GOOD. WIRING CHE
- [SDR HALA2017071700189](https://openairdocs.org/sdr/HALA2017071700189), Jul 14, 2017: CONTROL CABLE. FRAYED. LEFT SLAT BY WING TIP, IT'S NOT FLUSH LIKE OTHER SIDE. INSPECTED LT SLAT AND FOUND NR 5 SLAT RETRACT CABLE FRAYED. REMOVED NR 5 SLAT CABLE PER AMM 27-81-02-000-
- [SDR HALA2016042500122](https://openairdocs.org/sdr/HALA2016042500122), Apr 25, 2016: TIRE. DELAMINATED. NR 3 MLG TIRE DELAMINATED. TIRE PRESSURE AT REMOVAL 170PSI. R & R NR 3 MLG TIRE IAW AMM 32-41-01. SPIN CK OK.
- [SDR HALA2016011200006](https://openairdocs.org/sdr/HALA2016011200006), Jan 12, 2016: SMOKE DETECTOR. ACTIVATED. AFT CARGO SMOKE ALERT ILLUMINATED INFLT. BOTH BOTTLES DISCHARGED, LOWER CARGO COMP FIRE SUPPRESSION SYS. R & R CARGO COMPARTMENT FIRE EXTINGUISHER CONTAINER 1 A
- [SDR HALA2014070400097](https://openairdocs.org/sdr/HALA2014070400097), Jul 4, 2014: PROXIMITY SENSOR. MALFUNCTIONED. DURING DEPARTURE, SELECTED GEAR UP, LT MAIN UNSAFE, RED, CONDITION INDICATION. CYCLED ONCE, ALL OK. REPLACED MLG DOWN/LOCKED PROXIMITY SENSOR. GROUND OPS CHECK 
- [SDR HALA2014022400028](https://openairdocs.org/sdr/HALA2014022400028), Feb 24, 2014: DOOR. OUT OF ADJUST. F/A UNABLE TO OPEN L1 DOOR. TRIED SEVERAL TIMES. DOOR HAD TO BE OPENED FROM OUTSIDE. PERFORMED VERTICAL ADJUSTMENT OF DOOR IAW 52-11-01. OPS & LEAK CHECKED OK. 
- [SDR HALA2013073000097](https://openairdocs.org/sdr/HALA2013073000097), Jul 30, 2013: LINE. LEAKING. HYDRAULIC RT QTY LOW, ZERO QTY, RT, DECLARED AN EMERGENCY. R & R RT MLG RETRACT CYLINDER GLAND HYD LINE IAW AMM 32-33-05. LEAK CHECKED OK. AN UNEVENTFUL LANDING
- [SDR HALA2013072900095](https://openairdocs.org/sdr/HALA2013072900095), Jul 29, 2013: FMS. MALFUNCTIONED. FMS FROZE AFTER TAKEOFF. NO THRUST CHANGE. NO NAV FUNCTION. UNABLE TO TUNE RADIO. NO AUTOPILOT. NO AUTO TUNE NAV RADIO. NO FMS SPEED BUGS. RESET NR 1 AND NR 2 V
- [SDR HALA2013022300024](https://openairdocs.org/sdr/HALA2013022300024), Feb 23, 2013: WARNING LIGHT. ILLUMINATED. DURING REVERSE THRUST AFTER LANDING, THROTTLES IN EMERGENCY REVERSE. RT ENGINE HAD COMPRESSOR STALL FOR ABOUT 15 SECONDS, ALERT WAS DISPLAYED ON EAD. NO LIMITAT
- [SDR HALA2013024100015](https://openairdocs.org/sdr/HALA2013024100015), Jan 24, 2013: TIRE. SEPARATED. DURING FLIGHT F/A ADVISE SOME NOISE WHEN GEAR RETRACTED, NO ABNORMAL INDICATIONS. FOUND NR 4 MAIN TIRE RECAP SEPARATED FROM CORE, R & R NR 4 TIRE IAW AMM 32-41-
- [SDR HALA2011111900531](https://openairdocs.org/sdr/HALA2011111900531), Nov 19, 2011: CONTROL UNIT. MALFUNCTIONED. UPON PREFLIGHT OBSERVED RT ENGINE FIRE LEVEL 3 ALERT DISPLAYED WITH AURAL WARNING, FOLLOWED BY ENGINE DETECTION RT FAILED LEVEL 1 ALERT. R & R RT ENGINE FCDU IA
- [SDR HALA2011072300329](https://openairdocs.org/sdr/HALA2011072300329), Jul 23, 2011: COMPUTER. MALFUNCTIONED. ON CLIMBOUT YAW DAMP FAIL LIGHT. ACCOMPLISHED FIM 22-23 TASK 801. R & R NR 1 FCC COMPUTER, GROUND CHECKED OK IAW AMM 22-01-03.
- [SDR HALA2011062500286](https://openairdocs.org/sdr/HALA2011062500286), Jun 25, 2011: ENGINE. SURGES. AIR TURN BACK - ON CLIMB, IGNITION CAME ON, LT ENG WITH SLIGHT PWR SURGE. REPAIR IN WORK. OPEN
- [SDR HALA2011051000243](https://openairdocs.org/sdr/HALA2011051000243), May 10, 2011: PAN. CORRODED. FWD CARGO LOWER PAN BY DOOR WAY HAS CORROSION FWD TO AFT END. REMOVED DAMAGED LOWER FWD CARGO PAN IAW SRM 51-41-00-06-0. INSTALLED NEW (1EA) LOWER PAN ASSY IAW 
- [SDR HALA2011051000194](https://openairdocs.org/sdr/HALA2011051000194), May 10, 2011: SLIDE. NO TEST. R1 DOOR SLIDE FAILED DEPLOYMENT SYS CHECK. SLIDE DID NOT DROP OUT OF ACFT. REMOVED SHIM FROM LINER COVER DOOR CLIP. ACCOMPLISHED OPS CHECK OF SERVICE DOOR SLIDE
- [SDR HALA2011013000054](https://openairdocs.org/sdr/HALA2011013000054), Jan 30, 2011: STRUCTURE. DAMAGED. OPEN - AFT CARGO DOOR FWD EDGE 13" FROM BOTTOM DAMAGED, IN WORK.
- [SDR HALA2010110400517](https://openairdocs.org/sdr/HALA2010110400517), Nov 4, 2010: WARNING LIGHT. ACTIVATED. TEMPORARY NR 2 ENGINE DISPLAYED FOLLOWED BY A LOSS OF THRUST, ENG REGAINED NORMAL THRUST. INSPECTED NR 1 & NR 2 ENG INLETS & EXHAUSTS. NO DEFECTS NOTED. PERFORM
- [SDR HALA2010102000480](https://openairdocs.org/sdr/HALA2010102000480), Oct 20, 2010: LAMP. BURNED OUT. A FEW MINTURES AFTER TAKE-OFF, F/A'S SMELLED & SAW SMOKE IN FWD CABIN NEAR "MOOD" LIGHTS. F/A'S SAID IT LASTED ABOUT 5 MINS THEN DISAPATED. TURNED OFF GALLEY PO
- [SDR HALA2010090500394](https://openairdocs.org/sdr/HALA2010090500394), Sep 5, 2010: DCU. FAILED. RUDDER PITOT FAIL, RAT PROBE FAIL, AOA HEAT R FAIL, AOA HEAT LT FAIL DURING CLIMBOUT. R & R DCU PER AMM 31-43-02 OPS CHECK OK.
- [SDR HALA2009122100600](https://openairdocs.org/sdr/HALA2009122100600), Dec 21, 2009: ANGLE. CRACKED. "Z" ANGLE CRACKED AT NR 3 LWR COWL LATCH CUTOUT. AFT CORNER BELOW GUSSET. NR 1 ENG CHANGE. REPAIRED DAMAGE AREA IAW HAL M105 NR 479141. PERMANENT REPAIR.
- [SDR HALA2009052300187](https://openairdocs.org/sdr/HALA2009052300187), May 23, 2009: FUEL FILTER. OBSTRUCTED. ARB - "ENG L SYS FAIL" ALERT ILLUMINATED DURING INITIAL CLIMB. PERF FIM 73-33 TASK 802. FOUND MSG 733401 LT FUEL FILTER IMPENDING BLOCKAGE. REMOVED AND REPLACED

All 122: https://openairdocs.org/aircraft/N479HA/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/N479HA/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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