# N475HA: 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: 55121
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 12, 2001
- Certificate issued: June 29, 2011
- Expires: June 30, 2027
- Mode S code: A5D45D
- 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=475HA
- Page: https://openairdocs.org/aircraft/N475HA

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/N475HA/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 N475HA.

## FAA accident and incident reports

None matched to N475HA.

## 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 ASAA2026090766779](https://openairdocs.org/sdr/ASAA2026090766779), Sep 7, 2026: STEERING SYS. FAULTED. LOST ALL STEERING WHEN CLEARING RUNWAY. HAD TO SLAM RIGHT BRAKE TO AVOID GOING INTO THE GRASS. GROUNDED - YES. PERFORMED INSPECTION OF NOSE GEAR TIRES + STEERIN
- [SDR HALA20241031063](https://openairdocs.org/sdr/HALA20241031063), Oct 31, 2024: VALVE. DISCONNECTED. "BLEED AIR R FAIL" IN FLIGHT. COMPLIED WITH QRH PROCEDURE. MSG REMAINED ILLUMINATED WITH ADDITIONAL "AIR SYS R NOT OFF". RIGHT SYSTEM INDICATED 80 PSI. FOUND PR
- [SDR HALA20231013043](https://openairdocs.org/sdr/HALA20231013043), Oct 12, 2023: UNKNOWN. UNKNOWN. ATB-NOSE GEAR WOULD NOT RETRACT ON DEPARTURE. PERFORMED FIM TSK 32-60 TASK 817.NO DESCREPANCIES OR FAULTS NOTED.FURTHER T/S REQ.HA 19257 ALL 3 LANDING GEAR PINN
- [SDR HALA2023090100041](https://openairdocs.org/sdr/HALA2023090100041), Aug 31, 2023: UNKNOWN. UNKNOWN. ENG R SYS FAIL, ATB - PERFORMED EEC 2 CURRENT FAULTS AND FAULT REVIEW. FAULTING 732166, 801101, 81102, 732165. PERFORMED FIM TASK 73-21 TASK 839 UP TO STEP F(3)
- [SDR HALA2023081000037](https://openairdocs.org/sdr/HALA2023081000037), Aug 8, 2023: EEC. FAULTY. ATB - ENG L SYS FAIL. EE 2 FAULT REVIEW INDICATED NO DISPATCH FAULT CODES 732165 & 732166 (EEC BOX FAULT). REMOVED AND REPLACED EEC PER AMM 73-21-01.RTS OK. IDL
- [SDR HALA2023062700034](https://openairdocs.org/sdr/HALA2023062700034), Jun 26, 2023: UNKNOWN. UNKNOWN. OVERWING EMERGENCY LIGHTS FWD LEFT AND RIGHT INOP. CHARGED BATTERIES. RAN OPERATION CHECK GOOD OF EMERGENCY LIGHTS PER AMM 33-51-00.
- [SDR HALA2023040600017](https://openairdocs.org/sdr/HALA2023040600017), Apr 5, 2023: UNKNOWN. UNKNOWN. SUPPLEMENTAL SUBMISSION TO HALA2023040600016. CORRECTION OF AIRCRAFT MANUFACTURER FROM AIRBUS TO BOEING. AFTER GEAR EXTENSION "GEAR DOOR OPEN" APPEARED AND THEN
- [SDR HALA2023040600016](https://openairdocs.org/sdr/HALA2023040600016), Apr 5, 2023: UNKNOWN. UNKNOWN. AFTER GEAR EXTENSION "GEAR DOOR OPEN" APPEARED AND THEN CLEARED AFTER A FEW SECONDS. REMOVED AND REPLACED MAIN GEAR DOOR ASSY PER AMM 32-34-03. OPS CHECK GOOD. 
- [SDR HALA2023040100014](https://openairdocs.org/sdr/HALA2023040100014), Apr 1, 2023: UNKNOWN. UNKNOWN. WHILE CONDUCTING T/C 717-25-060-03-01, SLIDE DEPLOYMENT SYSTEM, THE SLIDE IS UNSERVICEABLE. REMOVED AND REPLACED FWD MAIN ENTRY DOOR ESCAPE SLIDE. REF. AMM 25-6
- [SDR HALA2023031400008](https://openairdocs.org/sdr/HALA2023031400008), Mar 11, 2023: UNKNOWN. UNKNOWN. ANTI SKID FAIL - ON APPROACH TO OGG. OK TO CONTINUE PER MEL 32-45-01 MDDR #401785. PLACARD INSTALLED. MIC UPDATED. PERFORMED FIM 32-41 TASK 805. RTS PASSED NO C
- [SDR HALA2022021700049](https://openairdocs.org/sdr/HALA2022021700049), Feb 16, 2022: NONE. NONE. ATB - ENG 2 SYS FAIL ALERT MESSAGE DURING CLIMBOUT // PER FIM 73-21 TASK 864 STEP E.5. NEED TO REPLACE EEC 18053 2/16/22. REPLACED EEC #2 ENG REF AMM 73-21-01-4
- [SDR HALA2021112900176](https://openairdocs.org/sdr/HALA2021112900176), Nov 29, 2021: NONE. NONE. C-CHECK - DURING REP HFEC INSPECTION GP306929-1 - FOUND MATERIAL FLAW INDICATION AT L/H WINDOW BELT BETWEEN STA 598 AND STA 617 FWD UPPER CORNER // E105-475407-
- [SDR HALA2021080900095](https://openairdocs.org/sdr/HALA2021080900095), Aug 8, 2021: BATTERY PACK. INOPERATIVE. EMER EQ - OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION BATTERY PER AMM 33-51-06. OPS CHK GOOD. OK FOR SERVICE.
- [SDR HALA2020070600136](https://openairdocs.org/sdr/HALA2020070600136), Jul 4, 2020: ACTUATOR. LEAKING. HYD R QTY LO LEVEL 2 ALERT AFTER LOWERING L/G. RT INBOARD ACTUATOR FOUND TO BE LEAKING. REMOVED AND REPLACED ACTUATOR PER AMM 27-55-03. OPS AND LEAK CHECK GOOD.
- [SDR HALA2020040800082](https://openairdocs.org/sdr/HALA2020040800082), Apr 7, 2020: DOOR. CRACKED. CRACK FOUND ON LH TRACK 8 SLAT DOOR ASSY. // REPLACED TRACK DOOR ASSY PER AMM 27-80-01, OPS CHECK GOOD.
- [SDR HALA2020040800081](https://openairdocs.org/sdr/HALA2020040800081), Apr 7, 2020: DOOR. CRACKED. FOUND CRACK ON L/H SLAT TRACK DOOR ASSY BETWEEN SLAT 2 AND 3. // REMOVED SLAT TRACK DOOR ASSY PER AMM 27-80-01-00-806 (STEP(8)(E)-(G)21555 REPLACED DOOR PER DRG
- [SDR HALA2020031600063](https://openairdocs.org/sdr/HALA2020031600063), Mar 13, 2020: DOOR. OBSTRUCTED. ATB - FLIGHT ATTENDANT REPORTED WHISTLING SOUND FROM L1 DOOR AND TAIL CONE ENTRANCE DOOR. // REMOVED DEBRIS FROM L1 AND TAIL CONE ENTRANCE DOOR. PERFORMED FUSEL
- [SDR HALA2019102100429](https://openairdocs.org/sdr/HALA2019102100429), Oct 19, 2019: EEC. FAULTED. ATB - SEL FADEC ALTN MSG FL210 FOR #2 ENGINE.// UPON FURTHER INVESTIGATION, FOUND FAULT CODES 732115, 732116. REMOVED AND REPLACED P20/T20 PROBE PER FIM 73-21-0
- [SDR HALA2019061200292](https://openairdocs.org/sdr/HALA2019061200292), Jun 11, 2019: SMOKE DETECTOR. FAULTED. CGO AFT SMOKE DETECTOR FAULT DISPLAYED. PER FLT CREW. // RESET C/B S29, 30, 31 AND PERFORMED TEST ON CARGO SMOKE. MSG EXTINGUISHED.
- [SDR HALA2019052000249](https://openairdocs.org/sdr/HALA2019052000249), May 17, 2019: CIRCUIT BREAKER. TRIPPED. CARGO SMK TEST FAIL AFT. RESET CB FOR PERFORM CARGO SMK TEST. CHECK GROUND. OK FOR SVC.
- [SDR HALA2019041200187](https://openairdocs.org/sdr/HALA2019041200187), Apr 11, 2019: MOTOR. INOPERATIVE. ATB - AIR RETURN TO BASE, PRIMARY STAB TRIM INOP. DID NOT WORK AFTER 5 MIN COOLING. // REMOVED AND REPLACED PRIMARY TRIM DRIVE MOTOR PER AMM 27-41-10. OPS CHECK
- [SDR HALA2019040500176](https://openairdocs.org/sdr/HALA2019040500176), Apr 4, 2019: DISCONNECT UNIT. MALFUNCTIONED. DURING YOKE FOR AND AFT MOVEMENT CLUNKING SOUND AND BINDING FELT. RE-SET CONTROL COLUMN DISCONNECT PER B717 AMM 27-31-10-440-801, PERFORMED VISUAL INSP OF ELEVA
- [SDR HALA2018111500588](https://openairdocs.org/sdr/HALA2018111500588), Nov 14, 2018: COVER. LEAKING. ATO - GEN LEFT FAIL DURING TAKEOFF ROLL. FOUND BOTTOM OF ENGINE WET WITH OIL AND IDG SIGHT GAGE HAD NO OIL, VISIBLE OIL LEAK PINPOINT TO IDG FILTER COVER REMOVE
- [SDR HALA2018100800476](https://openairdocs.org/sdr/HALA2018100800476), Oct 7, 2018: SENSOR. INOPERATIVE. COCKPIT DUCT OVHT DURING FLIGHT. COCKPIT OUTFLOW VALVE TEMP, INDICATION READ 212'F HOT AIR BLOWING THRU COCKPIT VENTS. FOLLOWED QRH PROCEDURE TEMP DROPPED TO NO
- [SDR HALA2017103000264](https://openairdocs.org/sdr/HALA2017103000264), Oct 28, 2017: ENGINE. VIBRATION. NR 2 ENGINE HIGH VIBRATION AFTER TAKEOFF, RETURNED TO DEPARTURE. REPLACED THE NR 2 ENGINE.
- [SDR HALA2017012000011](https://openairdocs.org/sdr/HALA2017012000011), Jan 20, 2017: INVERTER. DEFECTIVE. WHEN PERFORMING EMERGENCY PWR TEST "EMER AC BUS OFF" DISPLAYED. REMOVED AND REPLACED EMERGENCY AC BUS SENSING AND EMERGENCY POWER RELAY PER 24-24-00 OPS CHK GOO
- [SDR HALA2016112900373](https://openairdocs.org/sdr/HALA2016112900373), Nov 29, 2016: KEELBEAM. CRACKED. LEFT SIDE UNDERWING BARREL KEEL BEAM AT BS 715 OB SIDE CRACKED. REPAIRED IAW E105-B10214-PERM AND DRAWING 9923454 REV F.
- [SDR HALA2016112900001](https://openairdocs.org/sdr/HALA2016112900001), Nov 18, 2016: FORMER. CRACKED. LEFT UNDERWING BARREL KEEL BEAM AT BS 715 OTBD SIDE FORMER CRACKED. REPAIRED THE FORMER IAW DRAWING 9923454 REV F.
- [SDR HALA2016081800329](https://openairdocs.org/sdr/HALA2016081800329), Aug 18, 2016: WARNING SYSTEM. FALSE ACTIVATION. STAB TRIM TAKE OFF WARNING DURING TAKE OFF ROLL WITH STAB SET AT PROPER POSITION. ACCOMPLISHED FIM 31-51 TASK 817. VIA 1&2 RESET. GROUND OPS CHECKED OK IAW AMM 
- [SDR HALA2016021800049](https://openairdocs.org/sdr/HALA2016021800049), Feb 18, 2016: PSEU. MALFUNCTIONED. AIR DIVERSION - DIPSEU FAIL ILLUMINATED IN FLIGHT AFTER SLAT RETRACTION, REMAINED ON, WENT OFF AT SLAT EXTENSION. R & R PSEU CONTROL BOX IAW AMM 32-61-01-400-80
- [SDR HALA2015111200235](https://openairdocs.org/sdr/HALA2015111200235), Nov 12, 2015: TIRE. FAILED. NR 4 MAIN OTBD TIRE DAMAGE, TREAD SEPARATED ON TAKEOFF. REPLACED NR 4 MAIN TIRE & WHEEL ASSY IAW AMM 32-41-01 VISUALLY INSPECTED BRAKE AND SPIN CHECK GOOD. RIGH
- [SDR HALA2015082400166](https://openairdocs.org/sdr/HALA2015082400166), Aug 24, 2015: UNKNOWN. ODOR. ELECTRICAL ODOR THROUGHOUT CABIN & COCKPIT, DURING CLIMB & DESCENT. CHECKED E & E COMPARTMENT AND TAIL COMPARTMENT, NO ELECTRICAL ODOR NOTED THROUGHOUT CABIN & 
- [SDR HALA2015080300150](https://openairdocs.org/sdr/HALA2015080300150), Aug 3, 2015: PITOT TUBE. DAMAGED. BIRD HIT THE CAPTAIN`S PITOT PROBE. LOST CAPTAIN`S AIRSPEED INDICATIONS. RETURN TO AIRPORT. REMOVED THE DAMAGED PITOT PROBE IAW AMM 34-11-01-000-801. INSTALLED 
- [SDR HALA2014122300217](https://openairdocs.org/sdr/HALA2014122300217), Dec 23, 2014: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS AT ROWS 14-18 INOPERATIVE. R & R EMERGENCY LIGHTS POWER SUPPLY B5-119 IAW AMM 33-51-03. OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR HALA2014102600175](https://openairdocs.org/sdr/HALA2014102600175), Oct 26, 2014: LEAD. FAILED. SMOKE COMING OUT BY THE APU PANEL. RUBBER LEAD COVERS OF STARTER WERE SMOKING. REPLACED STARTER MOTOR IAW AMM 49-44-01. REPLACED STARTER CLUTCH AS A PRECAUTION 
- [SDR HALA2014050500062](https://openairdocs.org/sdr/HALA2014050500062), May 5, 2014: WARNING MESSAGE. ACTIVATED. DURING TAKEOFF ROLL AT APPROXIMATELY 100 KTS, RECEIVED AN AURAL WARNING "FLAPS", MASTER CAUTION, RED BOX FOR FLAPS, ABORTED TAKEOFF. OPEN.
- [SDR HALA2013050400054](https://openairdocs.org/sdr/HALA2013050400054), May 4, 2013: TIRE. FAILED. LOUD VIBRATION UPON LANDING FROM MAIN GEAR NR 3 MLG TIRE RECAP FAILED. (CAME OFF). PERFORMED GVI OF RT MLG AND FLAP. FLAP DAMAGE ON T/E, INBD FLAP PANEL. APPROX
- [SDR HALA2012011600032](https://openairdocs.org/sdr/HALA2012011600032), Jan 16, 2012: CABLE. BROKEN. OPEN - AIR/GROUND SENSOR CABLE AT NOSE WHEEL STRUT BROKEN.
- [SDR HALA2011062600287](https://openairdocs.org/sdr/HALA2011062600287), Jun 26, 2011: SKIN. DENTED. MED OUTER LOWER SKIN FWD AREA APPROX 9" X 1". MED OUTER LOWER SKIN AFT AREA APPROX 1" X .5" DENTED IN. RE-WORKED AREA IAW HAL M105 FILE B10085/SRM 52-00-00 HAL 
- [SDR HALA2011052000263](https://openairdocs.org/sdr/HALA2011052000263), May 20, 2011: SLAT SYSTEM. MALFUNCTIONED. AFTER T/O AT SLAT RETRACT SPEED & RETRACT SLAT, SLAT DISG ILLUMINATED & REMAIN ON. REPLACED LT WING NR1 SLAT OTBD IDLER TRACK ASSY IAW DWG 5926751. OPS CHECKED 
- [SDR HALA2011011700120](https://openairdocs.org/sdr/HALA2011011700120), Jan 17, 2011: BULKHEAD. CORRODED. LEVEL 2 CORROSION ON "AFT CARGO AFT BULKHEAD CENTER LOWER AREA ANGLE & DOUBLER.//REMOVED ANGLE, CLEANED CORROSION,TREATED AND PRIMED, REF. B717 SRM 51-10-04. RE
- [SDR HALA2011011400075](https://openairdocs.org/sdr/HALA2011011400075), Jan 14, 2011: SEAT TRACK. CORRODED. LEVEL 2 CORROSION AT CABIN SEAT TRACK STA 224, RBL 44. R & R SEAT TRACK AT STA 224, RBL 44, IAW DWG SR0953985.
- [SDR HALA2011011400072](https://openairdocs.org/sdr/HALA2011011400072), Jan 14, 2011: SEAT TRACK. CORRODED. LEVEL 2 CORROSION FOUND ON CABIN SEAT TRACK AT STA 224, RBL 22. REMOVED CORROSION IAW SRM 51-10-04, NDT ACCOMPLISHED, CHECKED LIMITS, FOUND TO BE OUT OF LIMITS 
- [SDR HALA2011011300073](https://openairdocs.org/sdr/HALA2011011300073), Jan 13, 2011: STRAP. CORRODED. LEVEL 2 CORROSION AT AFT CARGO COMPARTMENT STA 986 THRU 994, BETWEEN LONGERON 30 THRU 29R AREA WITH SPOT CORROSION. R & R STRAP AT AFT CARGO COMPARTMENT, STA 98
- [SDR HALA2011011200074](https://openairdocs.org/sdr/HALA2011011200074), Jan 12, 2011: SILL. CORRODED. LEVEL 2 CORROSION AT AFT CARGO COMPARTMENT DOOR FRAME, LOWER SILL. REMOVED CORROSION AT AFT CARGO DOOR LOWER SILL, CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 5
- [SDR HALA2010092000425](https://openairdocs.org/sdr/HALA2010092000425), Sep 20, 2010: CABLE. FRAYED. LEFT SLAT FOUND PARTICALLY EXTENDED W/FLAP/SLAT HANDLE RETRACTED. FOUND LT OTBD SLAT EXTEND CABLE FRAYED REPLACED CABLE PN 54913810EF09724 IAW AMM20-00-02. ADJU
- [SDR HALA2010090600400](https://openairdocs.org/sdr/HALA2010090600400), Sep 6, 2010: SKIN. DAMAGED. SCRATCH FWD OF LANDING LAMP ON WING TIP RT LOWER SURFACE. WITHIN LIMITS OF REPAIR IAW SRM 57-30-01, OK TO CONTINUE, EDDY CURRENT, NO CRACKS NOTED.
- [SDR HALA2010042800197](https://openairdocs.org/sdr/HALA2010042800197), Apr 28, 2010: SENSOR. FAILED. 2ND ATB: SPOILER OTBD FAIL. R & R THE OTBD (F/O) WHEEL ROLL CONTROL POSITION SENSOR IAW AMM 27-61-02 SPOILER SYS RTS PASSED.
- [SDR HALA2010042800196](https://openairdocs.org/sdr/HALA2010042800196), Apr 28, 2010: WARNING LIGHT. ILLUMINATED. "SPOILER OTBD FAIL" MESSAGE ALERT CAME ON PASSING THRU 2000". PERFORMED FIM 27-60, TASK 804 RTS PASSED NO FAULTS NOTED. OK FOR SERVICE. IAW MANAGEMENT, CHECKED 
- [SDR HALA2010042500189](https://openairdocs.org/sdr/HALA2010042500189), Apr 25, 2010: TURBINE. FAILED. NR 2 ENG INFLIGHT ENG SHUTDOWN, ON CLIMB AT 4,000 FT NR 2 ENGINE OVERTEMP WITH LOUD BANG AND ENGINE SHUTDOWN. ACFT RETURNED TO DEPARTURE WHERE AN UNEVENTFUL LAN

All 84: https://openairdocs.org/aircraft/N475HA/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/N475HA/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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