# N476HA: 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: 55118
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 5, 2001
- Certificate issued: June 29, 2011
- Expires: June 30, 2027
- Mode S code: A5D814
- 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=476HA
- Page: https://openairdocs.org/aircraft/N476HA

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/N476HA/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 N476HA.

## FAA accident and incident reports

None matched to N476HA.

## Service difficulty reports (87, 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 ASAA2026031563862](https://openairdocs.org/sdr/ASAA2026031563862), Mar 15, 2026: SMOKE DETECTOR. FAULTED. CRG SMK FWD FAIL, (1B). ( LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM DETECTOR UNITS [ONE DETECTOR AT EACH LOCATION MAY BE INOPERATIVE AND THE REMAINING PORT
- [SDR HALA20241018053](https://openairdocs.org/sdr/HALA20241018053), Oct 17, 2024: TEST UNIT. FAULTED. CARGO SMOKE FWD FAIL. RESET CARGO SMOKE TEST C/B. TEST PASSED. OK FOR SERVICE.
- [SDR HALA20241004046](https://openairdocs.org/sdr/HALA20241004046), Oct 3, 2024: BATTERY. INOPERATIVE. COCKPIT EMER LT COMES ON MOMENTARILY THEN TURNS OFF. REMOVE/REPLACE FLT COMPT. OVERHEAD LIGHT BATTERY B5-123. OPS CHECK GOOD OK FOR SVC.
- [SDR HALA20231226052](https://openairdocs.org/sdr/HALA20231226052), Dec 24, 2023: UNKNOWN. UNKNOWN. FWD 1/3 EMERGENCY OVHD LIGHTS INOP WILL SWITCH ON. REMOVED AND REPLACED POWER SUPPLY AT B5-227 PER FIM 33-50 TASK 801. OPS CHECK GOOD. OK FOR SVC.
- [SDR HALA2023042800021](https://openairdocs.org/sdr/HALA2023042800021), Apr 26, 2023: UNKNOWN. UNKNOWN. E105-C10453-TER. REPAIR - AFT CARGO DOOR EXTERNAL SURFACE CLUSTERED DENTS
- [SDR HALA2023042800020](https://openairdocs.org/sdr/HALA2023042800020), Apr 26, 2023: UNKNOWN. UNKNOWN. (S/M) S/C FOUND ON RH UPPER PYLON T/E ON UPR SFC (MARKED). REPAIRED PER E105-B10616-PERM.
- [SDR HALA2023042800019](https://openairdocs.org/sdr/HALA2023042800019), Apr 26, 2023: UNKNOWN. UNKNOWN. LH BRAKES (#1 & 2) DIDN'T OPERATE DURING HIGH PWR RUNS. BRAKE TEMP COLD. 1. REMOVED AND REPLACED BCU PER B717 AMM 32-45-01-400-801. BLEED #1 AND #2 MAIN WHEEL B
- [SDR HALA2023022200003](https://openairdocs.org/sdr/HALA2023022200003), Feb 21, 2023: NONE. NONE. SMOKE & FUMES IN CKPT ORIGINATING CAPT'S SIDE WINDOW UPPER NEAR GRAB HANDLE, O2 MASK USED ( WINDSHIELD HEAT SYSTEM-ANTI-ICE SYSTEM ) MX FOUND WINDSHIELD HEAT TE
- [SDR HALA2022022500057](https://openairdocs.org/sdr/HALA2022022500057), Feb 24, 2022: NONE. NONE. BTB - ON TAXI OUT “ENG L SYS FAIL” ALERT ILLUMINATED, ACFT RETURN TO THE GATE // PERFORM DUAL ENG RUN AT IDLE PER FIM 73-22 TASK 806 AND RESET FCC1 AND FCC2, VI
- [SDR HALA2022011800015](https://openairdocs.org/sdr/HALA2022011800015), Jan 15, 2022: BRACKET. LOOSE. EMER EQ - COCKPIT EMERGENCY EXIT WINDOW FO SIDE WILL NOT CLOSE // FOUND F/O LOWER TRACK SUPPORT BRACKET AFT BOLT LOOSE. REIINSTALLED NEW BOLT, OP HECK GOOD OK F
- [SDR HALA2021101800139](https://openairdocs.org/sdr/HALA2021101800139), Oct 17, 2021: NONE. NONE. EMER EQ - EMERGENCY PATH LIGHTS NEAR SEAT 18B NEEDS TO BE RESECURRED // RESECURRED EMERGENCY PATH LIGHTING AS REQUIRED AT 18B. OK FOR SVC
- [SDR HALA2020121000218](https://openairdocs.org/sdr/HALA2020121000218), Dec 10, 2020: BATTERY PACK. INOPERATIVE. EMERGENCY EQUIPMENT AFT SECTION OF EMERGENCY LIGHTS ARE NOT WORKING. REMOVE AND REPLACED TWO EMERGENCY LIGHT BATTERIES AT AFT SECTION (ABOVE SEAT 23 AND 16), PE
- [SDR HALA2020102100193](https://openairdocs.org/sdr/HALA2020102100193), Oct 20, 2020: ENGINE. FAILED. ATO-UPON BRINGING THROTTLES UP TO TAKEOFF WE HEARD A BANG. ABORTED TAKEOFF. RIGHT ENGINE COMPRESSOR STALL ILLUMINATED. HIGH TGT (1037*C) 1-PER PILOTS: SLOW SPEE
- [SDR HALA2020070600138](https://openairdocs.org/sdr/HALA2020070600138), Jul 6, 2020: BALL END. DISENGAGED. ATB- TAIL CONE UNLOCK ALERT, LEVEL 2 AFTER TAKEOFF. FOUND CABLE BALL END NOT FULLY ENGAGED WITH SWITCH. RE-SECURED PER AMM 53-52-01-400-801.
- [SDR HALA2020070700140](https://openairdocs.org/sdr/HALA2020070700140), Apr 2, 2020: FORMER. CORRODED. THREE PLACES OF MODERATE CORROSION ON FORMER AT BS 1021, LONGERON 30. CUT OUT THE CORROSION, FABRICATED A FILLER, AND REPAIRED DOUBLER. REPAIRED IAW SRM 51-70-1
- [SDR HALA2020030200050](https://openairdocs.org/sdr/HALA2020030200050), Feb 29, 2020: NOT REPORTED. DAMAGED. OPEN - DAMAGE TO RIGHT SIDE OF FUSELAGE.// REPAIR IN WORK. REPAIRED PER E105 476309-PERM AND E105 476310-PERM.
- [SDR HALA201910310461](https://openairdocs.org/sdr/HALA201910310461), Oct 30, 2019: DUCT. DISCONNECTED. ATB - LEVEL AT FL260 FELT A PRESSURE BUMP FOLLOWED BY A CABIN RATE LEVEL ONE. 2 MINS LATER GOT CABIN ALT LEVEL 3 ALERT. EMERGENCY DESCENT TO MAUI. // PERFORMED 
- [SDR HALA2019102100433](https://openairdocs.org/sdr/HALA2019102100433), Oct 19, 2019: TRIM SYSTEM. MULTIPLE FAIL. SUP - TRIM FAIL BOTH.HORIZONTAL STAB WILL NOT MOVE, STUCK AT 2.5 DEGREES. // REMOVED SCREWS FROM DOGHOUSE PANEL ON TOP OF VERTICAL STAN. FOUND CABLE RUN 129E BR
- [SDR HALA2019061400298](https://openairdocs.org/sdr/HALA2019061400298), Jun 6, 2019: STRUCTURE. CRACKED. A 1 INCH CRACK WAS FOUND ON THE LH THRUST REVERSER INTERIOR SURFACE. CLEANED AREA, STOP DRILLED THE CRACK WITH A 0.19 IN. DIAMETER HOLE. PERFORMED A DETAILED VI
- [SDR HALA2019042320200](https://openairdocs.org/sdr/HALA2019042320200), Apr 20, 2019: SKIN. CRACKED. 2.25 IN CRACK FOUND UNDER FUSELAGE TAIL SECTION APPROX 1197 RIGHT LONGERON L25-L30. // CUT OUT AND REPAIRED CRACK PER 717 SRM 53-00-00-2R-2. TREATED, PRIMED AND
- [SDR HALA2019040900183](https://openairdocs.org/sdr/HALA2019040900183), Apr 8, 2019: DUCT. DISCONNECTED. LOST CABIN PRESSURE AT 25,000 FT, NO STRUCTURAL DAMAGE WAS SUSPECTED, RAPID EMERGENCY DESCENT, CONTINUED TO NORMAL EMERGENCY LANDING. // FOUND RT AIR CONDITION 
- [SDR HALA2019040900182](https://openairdocs.org/sdr/HALA2019040900182), Apr 8, 2019: SMOKE DETECTOR. NO TEST. LAVATORY SMOKE DETECTOR NOT TESTING PROPERLY. INSPECTED, RAN OPS TEST ON LAV SMOKE DETECTOR SYSTEM OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2018072300337](https://openairdocs.org/sdr/HALA2018072300337), Jul 22, 2018: DUCT. DISCONNECTED. ON GROUND WITH APU RUNNING. PODS FAILED. TAIL TEMP HIGH. CHECK FOUND THE RT PACK OUTLET DUCT DISCONNECTED IN AFT ACCESSORY BAY. RECONNECTED THE RT PACK OUTLET D
- [SDR HALA2018051600227](https://openairdocs.org/sdr/HALA2018051600227), May 10, 2018: CABLE. FRAYED. LEFT NR 4 SLAT DRIVE CABLE WAS FOUND FRAYED. RETRACT CABLE 192A. REMOVED AND REPLACED THE LT WING NR 4 SLAT RETRACT CABLE IAW E105-476304-PERM, GMM VOL 1 CHAP 2
- [SDR HALA2017031600068](https://openairdocs.org/sdr/HALA2017031600068), Mar 16, 2017: SIGN. DETACHED. EMERGENCY EXIT SIGN FELL WHEN DOOR WAS OPENED. INSTALLED THE EXIT SIGN. SECURITY CHECKED OK.
- [SDR HALA2016052200204](https://openairdocs.org/sdr/HALA2016052200204), May 22, 2016: CONTROL HANDLE. CONTAMINATED. UPON GEAR EXTENSION, ALL GEAR UNSAFE, RED, LIGHTS ILLUMINATED. GEAR HANDLE WAS FOUND TO BE STICKY AND TIGHT. SUSPECT GEAR HANDLE WAS NOT MOVED TO THE FULL DOWN 
- [SDR HALA2015111600238](https://openairdocs.org/sdr/HALA2015111600238), Nov 16, 2015: STARTER. FAILED. NR 1 ENGINE FIRE INDICATION ILLUMINATED UPON START WITH FUEL SWITCH ON. FOUND NR 1 ENGINE STARTER DISINTEGRATED. R & R NR 1 ENGINE STARTER IAW AMM 80-11-01, LEA
- [SDR HALA2015110600227](https://openairdocs.org/sdr/HALA2015110600227), Nov 6, 2015: INSERT. MISSING. FORWARD LEFT EMERGENCY SLIDE GIRT BAR INSERT MISSING. RESECURED FORWARD PORT DOOR GIRT BAR. CKS GOOD. OK FOR FLIGHT IAW AMM 25-61-01.
- [SDR HALA2015092700198](https://openairdocs.org/sdr/HALA2015092700198), Sep 27, 2015: ELECTRONIC UNIT. FAILED. RIGHT ENGINE IDG INOPERATIVE, BTB AFTER NR 2 ENGINE START, RT GENERATOR FAILED TO COME ONLINE. SMOKED ODOR INSIDE AND REPORTED OUTSIDE BY LINE SERVICE. ENGINE I
- [SDR HALA2014070600105](https://openairdocs.org/sdr/HALA2014070600105), Jul 6, 2014: DRIVE ASSY. MALFUNCTIONED. SLAT DISAGREE, LEVEL 2 ALERT DISPLAYED DURING SLAT RETRACTION. FOUND LT SLAT LATCH MECHANISM ON SLAT DRIVE ASSY, DAMAGED. REMOVED LT SLAT DRIVE ASSY IAW AMM TAS
- [SDR HALA2014070600104](https://openairdocs.org/sdr/HALA2014070600104), Jul 6, 2014: FLAP TRACK. DAMAGED. LOWER INBD L/E BEHIND FLAP TRACK DAMAGED. SLAT ANTI ICE COVER LT INBD BENT AT AFT INBD CORNER. COLD WORKED IAW SEM 51-10-02/OGO1.
- [SDR HALA2014050100059](https://openairdocs.org/sdr/HALA2014050100059), May 1, 2014: SLIDE. LOOSE. PAX DOOR EVACUATION SLIDE COVER PINS HAVE FALLEN OUT AND SECURITY TIE STRING IS BROKEN. R & R SLIDE IAW AMM 25-61-01. CONDITION & SECURITY CHECK OK. OK FOR SERV
- [SDR HALA2013050900056](https://openairdocs.org/sdr/HALA2013050900056), May 9, 2013: WARNING MESSAGE. ILLUMINATED. JUST AFTER TAKEOFF "APU FIRE" ALERT DISPLAYED. APU MASTER WAS OFF.
- [SDR HALA2012050600136](https://openairdocs.org/sdr/HALA2012050600136), May 6, 2012: LINE. FAILED. BEFORE LANDING, HAD HYD RT QTY LOW MESSAGE. PERFORMED QRH HYD RT QTY LOW PROCEDURE, INCLUDING EMERGENCY GEAR EXTENSION. R & R LT MLG BUNGEE HYD LINE IAW MM 29-0
- [SDR HALA2012041100122](https://openairdocs.org/sdr/HALA2012041100122), Apr 11, 2012: CONTROL UNIT. INTERMITTENT. PRIMARY STAB TRIM FAILURE. REPLACED TRIM BRAKE RELAYS R2-830 & R2-831, AMM 27-41-02. REPLACED PRIMARY STAB TRIM DAV UNIT IAW MM 27-41-01. OPS CHECKED OK IAW AMM
- [SDR HALA2011122500609](https://openairdocs.org/sdr/HALA2011122500609), Dec 25, 2011: SENSOR. FAULTED. RT DUCT PRESSURE ON AIR PAGE INDICATES X. BITE CHECKED PNEU SYS CONTROLLER. FOUND RT PM SENSOR FAULT. R & R PM SENSOR IAW AMM 36-12-09. OPS CHECKED GOOD. OK FOR
- [SDR HALA2011051700208](https://openairdocs.org/sdr/HALA2011051700208), May 18, 2011: CONNECTOR. UNSECURE. EMERGENCY LIGHT AT ROW 5 INOPERATIVE. RESECURED CONNECTOR AT ROW 5. OPS CHECKED OK IAW AMM33-51-00.
- [SDR HALA2011051700200](https://openairdocs.org/sdr/HALA2011051700200), May 17, 2011: CONNECTOR. UNSECURE. EMERGENCY LIGHT AT ROW 5 INOP. RE-SECURED CONNECTOR AT ROW 5, OPS CHECK OK IAW AMM 33-51-00.
- [SDR HALA2011051600199](https://openairdocs.org/sdr/HALA2011051600199), May 16, 2011: SLIDE. DIRTY. UNABLE TO ARM SLIDE ON FWD GALLEY DOOR. CLEANED DEBRIS FROM GROUND ON FWD GALLEY DOOR SLIDE. OPS & CONDITION & SECURITY CHECKED OK.
- [SDR HALA2011050400179](https://openairdocs.org/sdr/HALA2011050400179), May 4, 2011: UNKNOWN. UNKNOWN. DISCONTINUED TAKE OFF AT APPROX 40 KTS, DUE TO UNABLE RNP ON EAD. PERFORMED FIM 34-63, TASK 822, GND CHECK OK. OK FOR SERVICE.
- [SDR HALA2010103000506](https://openairdocs.org/sdr/HALA2010103000506), Oct 30, 2010: OIL SYSTEM. LEAKING. ETOPS SIGNIFICANT SYS - ATB - LOW OIL QUANTY ON THE LT SIDE NR1 ENGINE ON TAKEOFF ROLL. R & R NR1 ENGINE. OPS AND LEAK CHECK OK, IAW TASK CARD M143-717.
- [SDR HALA2010103000505](https://openairdocs.org/sdr/HALA2010103000505), Oct 30, 2010: OIL SYSTEM. LEAKING. ETOPS SIGNIFICANT SYS - ATB - LOW OIL QUANTY ON THE LT SIDE NR 1 ENGINE ON TAKEOFF ROLL. R & R NR 1 ENGINE. OPS AND LEAK CHECK OK, IAW TASK CARD M143-717.
- [SDR HALA201007160303](https://openairdocs.org/sdr/HALA201007160303), Jul 16, 2010: SUPPORT BRACKET. CRACKED. RT AILERON NR 1 SLAT DRIVE DOOR SUPPORT BRACKET CRACKED. DEFERRED AND TRANSCRIBED TO HAL LOG PAGE.
- [SDR HALA201007160302](https://openairdocs.org/sdr/HALA201007160302), Jul 16, 2010: SUPPORT BRACKET. CRACKED. LEFT NR 1 SLAT DRIVE DOOR SUPPORT BRACKET CRACKED. DEFERRED AND TRANSCRIBED TO HAL LOG PAGE 339060.
- [SDR HALA2010071600301](https://openairdocs.org/sdr/HALA2010071600301), Jul 14, 2010: CONTROL CABLE. BROKEN. LEFT AILERON CONTROL CABLE (7F) HAS BROKEN STRANDS. REPLACED LEFT AILERON TAB CONTROL CABLE (7F) IAW M/M 20-00-02 & 27-10-00. OPERATION & RIG CHECK GOOD.
- [SDR HALA2010060300239](https://openairdocs.org/sdr/HALA2010060300239), Jun 3, 2010: COMPRESSOR. STALLED. OPEN - AIR TURN BACK - AT APPROX 3'000 FT. LT ENGINE SHUTDOWN. COMPRESSOR STALL ALERT WAS FIRST VISIBLE ALERT DISPLAYED. REPAIR IN WORK.
- [SDR HALA2010052500230](https://openairdocs.org/sdr/HALA2010052500230), May 25, 2010: DUCT. UNSECURE. AIR RETURN - PACK RT FLOW DISAGREE. SECURED DUCT - RT SIDE OF TAIL COMPARTMENT. - OPS AND SECURITY CHECK OK.
- [SDR HALA2010050400202](https://openairdocs.org/sdr/HALA2010050400202), May 4, 2010: PSEU. FAILED. PSEU FAIL. R & R PSEU IAW AMM 32-61-01. RETURN TO SERVICE TEST PASSED. OK FOR SERVICE.
- [SDR HALA201004200170](https://openairdocs.org/sdr/HALA201004200170), Apr 15, 2010: UNKNOWN. ODOR. A/C SMELLED OF ELECTRICAL BURNING. CK E&E COMPT FWD EQUIP COMPT AFT ACCY APU COMPT CARGO COMPTS COCKPIT & CABIN AREAS NO OBVIOUS DEFECT NOTED OR FOUND. SOURCE O
- [SDR HALA2010022300071](https://openairdocs.org/sdr/HALA2010022300071), Feb 23, 2010: WIRE. DAMAGED. SEAT 7 DEF EMERGENCY LIGHTNING INOP. REPAIRED WIRE AND CONNECTOR TO EMERGENCY LIGHTING FOR SEAT 7DEF. OPS CHECK OKAY OK FOR SERVICE.

All 87: https://openairdocs.org/aircraft/N476HA/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/N476HA/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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