# N478HA: 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: 55123
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 9, 2001
- Certificate issued: June 29, 2011
- Expires: June 30, 2027
- Mode S code: A5DF82
- 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=478HA
- Page: https://openairdocs.org/aircraft/N478HA

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/N478HA/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 N478HA.

## FAA accident and incident reports

None matched to N478HA.

## Service difficulty reports (84, 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 ASAA2026021763444](https://openairdocs.org/sdr/ASAA2026021763444), Feb 17, 2026: CHARGER. FAULTED. EMERGENCY PWR FAIL. GROUNDED - YES. PER FIM 24-24 TASK 803 RESET BATT CHARGER. MESSAGE CLEARED. OK FOR SVC.
- [SDR ASAA2026011862922](https://openairdocs.org/sdr/ASAA2026011862922), Jan 18, 2026: BATTERY. INOPERATIVE. OVERWING EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THE EMERGENCY LIGHT BATTERY FOR OVERWING LIGHTS IAW 33-51-06. OPS CHKD GOOD. OK FOR SERVICE.
- [SDR ASAA2025121962452](https://openairdocs.org/sdr/ASAA2025121962452), Dec 19, 2025: SEAL. LACK OF LUBE. MAIN CABIN DOOR STICKS WHEN CLOSING. GROUNDED - YES. CLOSED MAIN CABIN DOOR FROM THE OUTSIDE AND INSDIE. FOUND NO FAULTS. APPLIED VASOLINE TO MAIN CABIN DOOR SE
- [SDR HALA20250804044](https://openairdocs.org/sdr/HALA20250804044), Aug 2, 2025: HYDRAULIC SYSTEM. CONTAMINATED. REJECTED T/O 8L DUE TO R HYD HIGH TEMP. UNABLE TO MITIGATE W/ MOVEMENT OF FLT CONTROLS / SPOILERS. PERFORMED FIM 29-30 TASK 803. FOUND EXCESSIVE AIR IN R HYD SY
- [SDR HALA20250630037](https://openairdocs.org/sdr/HALA20250630037), Jun 28, 2025: WARNING MESSAGE. FALSE ACTIVATION. ATB - LEFT GEAR INDICATION RED/UNSAFE WITH GEAR HANDLE UP AFTER TAKE OFF. JACKED UP THE AIRCRAFT PER AMM 07-00-582-811. PERFORMED FUNCTIONAL TEST OF MLG AND NLG
- [SDR HALA20250204003](https://openairdocs.org/sdr/HALA20250204003), Jan 31, 2025: MANIFOLD. FAILED. "DIVERSION TO HNL" TAIL ANTI-ICE MANIFOLD FAILED IN ICING CONDITIONS, FLAP 25 LANDING AS PER QRH. FOUND "PODS SYSTEM FAULT" ON FAULT REVIEW. REMOVED AND REPLACE
- [SDR HALA20240819040](https://openairdocs.org/sdr/HALA20240819040), Aug 16, 2024: CONTROL UNIT. FAULTED. AT 1300FT AUTOPILOT DISCONNECTED, AUTO THROTTLES WENT MAX POWER, ALL DU'S WENT BLANK FOR A SECOND. REMOVED AND REPLACED EPCU PER AMM 24-21-02. EPCU OP CK GOOD. 
- [SDR HALA20240819039](https://openairdocs.org/sdr/HALA20240819039), Aug 16, 2024: RELAY. FAILED. AFTER EPCU DOWNLOAD FOUND EMERGENCY POWER RELAY FAULT ( 54 EPR FAILED CLOSED.). REMOVED AND REPLACED EMERGENCY DC POWER RELAY PER AMM 24-34-05. FUNCTIONAL TEST 
- [SDR HALA2023051200027](https://openairdocs.org/sdr/HALA2023051200027), May 11, 2023: UNKNOWN. UNKNOWN. CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT MOMENTARILY TURNS ON THEN GOES OUT. REPLACED BATTERY B5120 AT ROW 17DEF, PERFORMED OPS TEST OF EMERGENCY LIGHTING SYS
- [SDR HALA2022042000095](https://openairdocs.org/sdr/HALA2022042000095), Apr 20, 2022: PSEU. FAULT MESSAGE. ATB - PSEU FAULT MESSAGE ON CLIMB OUT // REPLACED NLG LOCKED PROXIMITY SENSOR ASSY PER AMM 32-61-03-400-804. OPS CHK OK PER AMM 32-61-00-820-802. (FAULT CODE 32
- [SDR HALA2022032100080](https://openairdocs.org/sdr/HALA2022032100080), Mar 19, 2022: NONE. NONE. ATB - DURING CLIMB "SELECT FADEC R ALTN" MESSAGE DISPLAYED YELLOW X ON RIGHT EPR FOLLOWED QRH PROCEDURE. DID NOT RESET // FOUND LTD FAULT CODES 732115 732116ON 
- [SDR HALA2020070100135](https://openairdocs.org/sdr/HALA2020070100135), Jul 1, 2020: PIN. OUT OF POSITION. MED SLIDE PINS CAME OUT. REMOVED AND REPLACED MAIN ENTRY DOOR SLIDE PER AMM 25-61-01. OPS AND SECURE CHECKS GOOD.
- [SDR HALA2019071500354](https://openairdocs.org/sdr/HALA2019071500354), Jul 13, 2019: PROBE. OUT OF LIMITS. ATB: ENG R SYS FAIL LIGHT ON RIGHT, TGT GAUGE X THROUGH IT. PER TSM 77-21-803 STEP F4(A) 4(O) MEASURING 8.7 OHMS. STEP K PROBES 6 & 7 OUT OF TOLERANCE 8.2 & 8.3
- [SDR HALA2019061000286](https://openairdocs.org/sdr/HALA2019061000286), Jun 8, 2019: EEC. MALFUNCTIONED. ATB - ENG L SYS FAIL ENROUTE FOLLOWED BY REV L FAULT. PERFORMED EEC1 RTS TEST. TEST FAILED. EEC BOX FAULT. REMOVED & REPLACED EEC1 PER AMM 73-21-01. RTS TEST PA
- [SDR HALA2019050300216](https://openairdocs.org/sdr/HALA2019050300216), May 2, 2019: POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT CEILING LIGHT @ ROW 17 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51-03. BATTERY POWER SUPPLY (B5-120). OPS. CHEC
- [SDR HALA2019042320199](https://openairdocs.org/sdr/HALA2019042320199), Apr 21, 2019: POWER SUPPLY. INOPERATIVE. ETOPS SIGNIFICATION - LEFT WING EMERGENCY EXIT LIGHT INOP // REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY CONTROL MODULE. PER AMM 33-51-03. OPS CHE
- [SDR HALA2019041500189](https://openairdocs.org/sdr/HALA2019041500189), Apr 12, 2019: MANIFOLD. FAILED. ATO - TAIL MANF FAIL DURING T/O ROLL. // PER FLIGHT CREW TAIL ANTI ICE WAS NOT ON. FAULT CODE 362164. FOUND WIRE E9142-35-20 BETWEEN RIGHT & LEFT HORIZONTAL SEN
- [SDR HALA2018121000641](https://openairdocs.org/sdr/HALA2018121000641), Dec 7, 2018: STATIC INVERTER. MALFUNCTIONED. CA'S FMS GOES OFF ON APP WHEN EMER PWR ON MESSAGE IS ON.// REMOVE & REPLACE STATIC INVERTER PER AMM 24-24-01. OPS CK OK. REMOVED & REPLACE CAPT MCDU PER AMM 31-
- [SDR HALA2018110500560](https://openairdocs.org/sdr/HALA2018110500560), Nov 3, 2018: COMPRESSOR. DAMAGED. HIGH SPEED ABORT DUE TO LEFT ENGINE FAILURE / COMPRESSOR STALL.// FOUND #1 ENG HP COMPRESSOR STAGE 5 TO 6 DAMAGE DURING BORESCOPE. // REMOVED AND REPLACED #1 EN
- [SDR HALA2018061800285](https://openairdocs.org/sdr/HALA2018061800285), Jun 17, 2018: ACTUATOR. MALFUNCTIONED. HYD RT TEMP CAUTION LIGHT ON WHILE TAXING TO GATE. ACCOMPLISHED FIM 29-30-TASK 803, BLED THE RT HYDRAULIC SYSTEM TEMP ACTUATORS. OK, WITHIN LIMITS, OK FOR SERVI
- [SDR HALA2016040400111](https://openairdocs.org/sdr/HALA2016040400111), Apr 4, 2016: SUPPORT FITTING. CORRODED. WING TO BS 832 LOWER END OF SUPPORT FAIRING CORRODED. LT SIDE, ON EXISTENT REPAIR. REMOVED CORROSION AT WING TO BS 832 LOWER END OF SUPPORT FAIRING LT SIDE ON E
- [SDR HALA2016032800107](https://openairdocs.org/sdr/HALA2016032800107), Mar 28, 2016: SPAR. CRACKED. LT WING AFT SPAR CRACKED AT XR 5324 INSIDE OF FUEL TANK ACCESS PANEL 520HB. REPAIRED THE SPAR IAW PRI EA 16126- P1 AND FINAL EA 16126, REV IR AND E105-478280-PE
- [SDR HALA2016032300110](https://openairdocs.org/sdr/HALA2016032300110), Mar 23, 2016: FITTING. CORRODED. WING TO BS 832 FITTING ON LONGERON 30 CORRODED. REMOVED CORROSION AT WING TO BODY BS 832 FITTING ON LONGERON 30 ORIGINAL MATERIAL 125" REMAINING .098" AND LOSS 
- [SDR HALA2016032200109](https://openairdocs.org/sdr/HALA2016032200109), Mar 22, 2016: FITTING. CORRODED. LT WING FLAP INBD FLAP TRACK FITTING CORRODED. REMOVED CORROSION ON L/W FLAP INBD FLAP TRACK FITTING EDGE DAMAGED. REMOVED OVER .100, OUT OF LIMITES IAW SRM 57-
- [SDR HALA2016032800108](https://openairdocs.org/sdr/HALA2016032800108), Mar 21, 2016: KEELBEAM. CRACKED. KEELBEAM BARREL BS 696 OTBD END OF FORMER CRACKED. RT SIDE. R & R EXISTING REPAIR DAMAGE, REPAIR AT KEELBEAM BARREL BS 696 OTBD END OF FORMER RT SIDE IAW DW6 99
- [SDR HALA2016020300025](https://openairdocs.org/sdr/HALA2016020300025), Feb 3, 2016: FMS. MALFUNCTIONED. AIR TURNBACK. BOTH FMS LOCKED IN STANDBYE F-PLAN MODE. DOWN POWERED ACFT. ACCOMPLISHED VIA 1 & 2 RTS. NO FAULTS NOTED, AMM 31-43-00.
- [SDR HALA2015122400251](https://openairdocs.org/sdr/HALA2015122400251), Dec 24, 2015: FAIRING. DAMAGED. DURING DESCENT, THE PLANE MOMENTARILY OVERSPEED TO 341 KNOTS. PERFORMED OVER SPEED INSPECTION IAW AMM TASK 05-51-05-210-801. NO DAMAGE FOUND IN SKIN OR STRUCTUR
- [SDR HALA2015111500236](https://openairdocs.org/sdr/HALA2015111500236), Nov 15, 2015: GIRT BAR. UNSECURE. ESCAPE SLIDE GIRT BAR HANGING FROM CASING. REINSTALLED ESCAPE SLIDE GIRT BAR IAW AMM25-61-01. SECURITY CHECK GOOD, OK TO CONTINUE SERVICE.
- [SDR HALA2013040600035](https://openairdocs.org/sdr/HALA2013040600035), Apr 6, 2013: TIRE. FAILED. AIR TURN BACK, NR 1 TIRE FAILURE ON TAKE OFF. R & R NR 1 MLG WHEEL IAW AMM 32-41-01. SPIN CHECK OK. MLG TIRES 2,3,4 CONDITION AND SECURITY CHECKED OK.
- [SDR HALA2012072100181](https://openairdocs.org/sdr/HALA2012072100181), Jul 21, 2012: TIRE. DAMAGED. LEFT MAIN OTBD TIRE DAMAGED. R & R LT MAIN OTBD TIRE IAW AMM 32-41-01.
- [SDR HALA2012011400029](https://openairdocs.org/sdr/HALA2012011400029), Jan 14, 2012: SLIDE. BINDING. SERVICE DOOR SLIDE UNSAFE, BINDING. R & R SERVICE DOOR SLIDE IAW AMM 25-61-03. SECURITY CHECKED GOOD.
- [SDR HALA2011070400304](https://openairdocs.org/sdr/HALA2011070400304), Jul 4, 2011: INDICATION SYS. MALFUNCTIONED. UPON GEAR RETRACTION OUT OF DEPARTURE, LT MAIN GEAR RED ( UNSAFE INDICATION) CAME BACK TO DEPARTURE. RETRACTION CHECK IAW MM 32-30-00, LT MAIN GEAR LIGHTS GOOD.
- [SDR HALA2011052600230](https://openairdocs.org/sdr/HALA2011052600230), May 26, 2011: PROXIMITY SENSOR. MALFUNCTIONED. AFTER TAKEOFF WITH THE GEAR HANDLE UP, THE LT MAIN GEAR LIGHT WAS ILLUMINATED RED. WITH THE GEAR HANDLE DOWN, ALL 3 LIGHTS GREEN. TROUBLESHOT IAW SRM 32-61-0 IA
- [SDR HALA2011052300222](https://openairdocs.org/sdr/HALA2011052300222), May 23, 2011: EEC. MALFUNCTIONED. SELECT FADEC ALTN FOR LT ENG DISPLAYED, DID NOT RESET TO NORMAL MODE WHEN CHECKLIST ACCOMP. BITE EEC FAULT 732115/732116. R & R P2/T2 PROBE IAW MM 73-21-05. RTS
- [SDR HALA2011052200214](https://openairdocs.org/sdr/HALA2011052200214), May 22, 2011: PROXIMITY SENSOR. MALFUNCTIONED. LT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. DISCONNECTED D1-1057, LT MLG UPLATCH PROX SENSOR & CLAMPS. REPLACED LT MLG UP & LATCHED PROXIMITY S
- [SDR HALA2010051100209](https://openairdocs.org/sdr/HALA2010051100209), May 11, 2010: WIRE. DAMAGED. ATB: DURING CLIMB ENG RT SYS FAIL ILLUMINATED. RETURNED HNL PER DISPATCH AND MOC. FOUND FAULT (772263) ACCOMPLISHED FIM 77-22 TASK 803. REPAIRED WIRING AT TURBI
- [SDR HALA2010042400188](https://openairdocs.org/sdr/HALA2010042400188), Apr 24, 2010: THRUST REVERSER. MALFUNCTIONED. AFTER LANDING, ACFT WENT INTO EMERGENCY REVERSE FOR APPROX 5 SECONDS. INSP NR1 & NR2 ENGINES IAW MM 71-00-05. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA2010033100143](https://openairdocs.org/sdr/HALA2010033100143), Mar 31, 2010: SMOKE DETECTOR. MALFUNCTIONED. LAVATORY SMOKE WARNING WILL NOT EXTINGUISH AFTER TESTING. RESET LAV SMOKE DETECTOR. OPS CK GOOD.
- [SDR HALA2010031600118](https://openairdocs.org/sdr/HALA2010031600118), Mar 16, 2010: PIN. FAULTY. RETURNED TO HNL, ATB, NOSE GEAR WOULD NOT RETRACT. NOSE GEAR PIN FAULTY. WHEN REMOVED AFTER TOW, PORTION REMAINED IN GEAR LOCK, CLEARED LOCK.
- [SDR HALA2010020800081](https://openairdocs.org/sdr/HALA2010020800081), Feb 8, 2010: FLOOR SUPPORT. CORRODED. LEVEL 2 CORROSION ON FLOOR SUPPORT ANGLE, 3EA SPOTS, BY L-1 ENTRY DOOR BETWEEN STA 160-200. REMOVED CORROSION AT L-1 ENTRY DOOR BETWEEN STA 160-200, IAW SRM 51-
- [SDR HALA2010020800068](https://openairdocs.org/sdr/HALA2010020800068), Feb 8, 2010: FLOORBEAM. CORRODED. LEVEL 2 CORROSION ON FWD CABIN FLOOR SUPPORT ANGLE AT STATION 200, RBL 19 TO RBL 31. REMOVED CORROSION AT FWD CABIN FLOOR SUPPORT ANGLE AT STA 200, RBL 19 - RBL
- [SDR HALA2010020700069](https://openairdocs.org/sdr/HALA2010020700069), Feb 7, 2010: STIFFENER. GOUGED. STIFFENER GOUGED AT FWD ENG AT LT W/W HYD SYSTEM SERVICING STATION INTERIOR UPPER. REMOVED STIFFENER AT LT W/W HYD SYSTEM SERVING STATION INTERIOR UPPER SIDE PE
- [SDR HALA2009122000591](https://openairdocs.org/sdr/HALA2009122000591), Dec 20, 2009: DCU. MALFUNCTIONED. AFTER TAKEOFF CREW REPORTED MULTIPLE ALERT ILLUMINATED, RUDDER PITOT FAIL, AOA HEAT L/R FAIL, RAT PROBE FAIL. PERFROMED FIM TASK ON AOA HEAT (L) IAW TASK 30-30 
- [SDR HALA2009121600586](https://openairdocs.org/sdr/HALA2009121600586), Dec 16, 2009: PSEU. MALFUNCTIONED. WITH AC CONFIGURED FOR LANDING OUT OF 1000 FT FINAL APPROACH PSEU FAIL FLASHED ON AND OFF SEVERAL TIMES, A/S FAST REF +10, AUTO THROTTLES WENT INTO LO SPEED PRO
- [SDR HALA2009101600471](https://openairdocs.org/sdr/HALA2009101600471), Oct 16, 2009: DUCT. DISCONNECTED. WHILE AT FL LEVEL 270, HEARD A BOOM FOLLOWED BY PACK R FLOW DISAGREE ALERT. JUST PRIOR TO LANDING, ALL ALERTS WENT AWAY. FOUND RT A/C PACK DUCT DISLODGED. RECON
- [SDR HALA2009052300186](https://openairdocs.org/sdr/HALA2009052300186), May 23, 2009: VIA. FAILED. ATB - AIR DATA 1 FAIL, GPWS FAIL, DCU FAIL, VIA FAIL, COLUMN DISC, FCC 1 FAIL, PROBLEM IS UNKNOWN. REPLACED NR 2 VIA GND OPS CHK OK AMM 31-43-01.
- [SDR HALA2009052200186](https://openairdocs.org/sdr/HALA2009052200186), May 22, 2009: VIA. MULTIPLE FAIL. ATB - AIR DATA 1 FAIL, GPWS FAIL, DCU FAIL, VIA FAIL, COLUMN DISC, FCC 1 FAIL, PROBLEM IS UNKNOWN. REPLACED NR 2 VIA GND OPS CHK OK AMM 31-43-01.
- [SDR HALA2009041000138](https://openairdocs.org/sdr/HALA2009041000138), Apr 10, 2009: INDICATOR. MALFUNCTIONED. ATO - ON TAKEOFF LEVEL 3 STAB TRIM IN "RED" ABORT RTN TO RAMP. PERFORMED INSP OF ACFT AFTER HIGH ENERGY RTO STOP IAW AMM 05-53-01. NO DEFECTS NOTED. PERFORMED R
- [SDR HALA2009032000095](https://openairdocs.org/sdr/HALA2009032000095), Mar 20, 2009: WARNING LIGHT. FALSE ACTIVATION. WING ANTI-ICE MANIFOLD FAIL LIGHT ILLUMINATED AT FL220 THEN WENT AWAY AT 6,000. PERFORMED DODS RTS TEST OK. NO FAULTS NOTED. PERFORMED FIM 30-81-00-810-801. NO 
- [SDR HALA2009022500066](https://openairdocs.org/sdr/HALA2009022500066), Feb 25, 2009: BEARING. DAMAGED. IN ORDER TO FLY STRAIGHT AND LEVEL THE AILERON TRIM AND RUDDER TRIM HAD TO BE ALIGNED GREATLY TO THE RIGHT. VISUAL CKS OF A/C FLT CONTROL, CONDITION SECURE CKS 

All 84: https://openairdocs.org/aircraft/N478HA/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/N478HA/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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