# N491HA: 2003 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55175
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 6, 2003
- Certificate issued: February 28, 2024
- Expires: February 28, 2031
- Mode S code: A6147F
- 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=491HA
- Page: https://openairdocs.org/aircraft/N491HA

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 Rolls-Royce 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 (Rolls-Royce 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/N491HA/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 N491HA.

## FAA accident and incident reports

None matched to N491HA.

## Service difficulty reports (53, 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 ASAA2026100967366](https://openairdocs.org/sdr/ASAA2026100967366), Oct 9, 2026: GIRT BAR. STICKING. PAX ENTRY DOOR GIT BAR STICKING IN FLOOR FITTING WHEN FLIGHT ATTENDANTS DISARM DOOR. GROUNDED - YES. LUBRICATED MED GIRTH BAR ATTACH FLOOR FITTING. OPS CHECK GO
- [SDR ASAA2026092367042](https://openairdocs.org/sdr/ASAA2026092367042), Sep 23, 2026: DOOR. BINDING. 1L DOOR DIFFICULT TO OPEN. GROUNDED - YES. PASSENGER FORWARD DOOR SEAL INSPECTED AND OPERATIONAL CHECK GOOD IAW AMM 52-11-02.
- [SDR ASAA2026081266278](https://openairdocs.org/sdr/ASAA2026081266278), Aug 12, 2026: HOLDER. FOD. FA REPORTS THAT 1L DOOR GRIT BAR IS HARD TO REMOVE FROM HOLDER. GROUNDED - YES. REMOVED DEBRIS FROM 1L GRIT BAR HOLDER AS REQUIRED. OPS CHECK GOOD. OK FOR SVC.
- [SDR ASAA2026051764772](https://openairdocs.org/sdr/ASAA2026051764772), May 17, 2026: BATTERY. INOPERATIVE. OVERWIND EMERGENCY LIGHTS INOP. GROUNDED - YES. LAMPS OK. REPLACED BATTERY PER AMM 33-51-06. OPS CK GOOD. OK FOR SVC.
- [SDR ASAA2026041164256](https://openairdocs.org/sdr/ASAA2026041164256), Apr 11, 2026: GIRT BAR. LACK OF LUBE. MAIN CABIN DOOR GRIT BAR HARD ENGAGE / DISENGAGE INTO FLOOR BRACKETS. GROUNDED - YES. CLEANED AND LUBED GIRT BAR HOLDER AS REQUIRED ACFT OK FOR SERVICE.
- [SDR ASAA2026011162827](https://openairdocs.org/sdr/ASAA2026011162827), Jan 11, 2026: INDICATOR. FAILED. LANDING GEAR POSITION INDICATING POPPED AFTER T/O. ATB. GROUNDED - YES. REMOVED AND REPLACED NOSE LANDING GEAR POSITION INDICATOR CAP PER FIM 32-60 TASK 803. RT
- [SDR ASAA2025113061951](https://openairdocs.org/sdr/ASAA2025113061951), Nov 30, 2025: LAMP. INOPERATIVE. L1 ENTRY LIGHT TURNS ON EMERGENCY EXIT LIGHT (EMERGENCY EXIT LIGHT OPS NORMAL) ( CABIN INTERIOR ILLUMINATION CONFIG WITH PHOTOLUMINESCENT EMERGENCY ESCAPE PATH 
- [SDR HALA20250818046](https://openairdocs.org/sdr/HALA20250818046), Aug 17, 2025: PLACARD. DAMAGED. FUSELAGE AFT L EMERGENCY EXIT PLACARD DAMAGED. REMOVED DAMAGED AFT L EMERGENCY EXIT PLACARD, INSTALLED NEW EMERGENCY EXIT PLACARD. OK FOR SERVICE.
- [SDR HALA20250716038](https://openairdocs.org/sdr/HALA20250716038), Jul 14, 2025: COMPRESSOR. STALLED. LEFT ENGINE COMPRESSOR STALL ON TAKEOFF. PERFORMED B717 FIM TASK 72-00 TASK 801 AND AMM 72-00-00-200-801 UP TO STEP 2(E)4 21794. REMOVED AND REPLACED #1 ENG. OK
- [SDR HALA20250627035](https://openairdocs.org/sdr/HALA20250627035), Jun 24, 2025: COMPRESSOR. STALLED. DIVERSION TO HNL - LT ENG COMPRESSOR STALL AT 400 FT, 2 LOUD THUDS BEFORE FOLLOWING PHASE 1'S. NO MORE THUDS TO FOLLOWS LEVEL 2 MESSAGE COMPRESSOR STALL. FOUND 
- [SDR HALA20250206004](https://openairdocs.org/sdr/HALA20250206004), Feb 5, 2025: BLEED VALVE. FAULTED. DIVERSION TO HNL. DURING FLIGHT LEFT BLEED FLUCTUATES FROM 8-67. WITH NO POWER CHANGES FLUCTUATIONS HAPPENING DURING ALL PHASES OF FLIGHT. REMOVED AND REPLACED 
- [SDR HALA20241230082](https://openairdocs.org/sdr/HALA20241230082), Dec 28, 2024: LIGHT. INOPERATIVE. EVERY OTHER OVERHEAD EMERGENCY LIGHT IS INOP IN CABIN. REMOVED AND REPLACED EMER. LTS PER AMM 33-51-08/401. OPS CHECK OK. SECURITY CHECK OK. OK TO CONTINUE SERV
- [SDR HALA20241118072](https://openairdocs.org/sdr/HALA20241118072), Nov 15, 2024: BATTERY. INOPERATIVE. OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERY PER 33-51-00. OPS CHK GPPD. OK FOR SERVICE.
- [SDR HALA20241119075](https://openairdocs.org/sdr/HALA20241119075), Nov 8, 2024: FITTING. CORRODED. SEVERE CORROSION ON RIGHT AFT NOSE GEAR DOOR AFT FITTING (M). 1. REMOVED AND REPLACE RIGHT AFT NOSE GEAR DOOR AFT HINGE FITTING PER LBD #5914984. PERFORMED ADJU
- [SDR HALA20241119074](https://openairdocs.org/sdr/HALA20241119074), Nov 8, 2024: CABLE. DAMAGED. RH INBD FLAP TRACK PULLEY AFT CABLE NYLON TORN. COMPLETED REPLACING 4EA FLAP BUS CABLES 33A, 33B, 34A, AND 34B. PER B717 DRAWING # 5940898 REV5.
- [SDR HALA2022030200060](https://openairdocs.org/sdr/HALA2022030200060), Mar 1, 2022: NONE. NONE. AIR TURN BACK - SELECT FADEC ALTN ALTERT ILLUMINATES IN-FLIGHT #1 ENGINE // REMOVED=REPLACED #1 EEC PER AMM 73-21-01. FUNCTION TEST OF. RTS PASSED. NO FAULTS. O
- [SDR HALA2021060900066](https://openairdocs.org/sdr/HALA2021060900066), Jun 8, 2021: LAMP. INOPERATIVE. MAIN DOOR (1L) EXIT SIGN LIGHT INOP. RELAMPED DOOR 1L EXIT SIGN LIGHT. LIGHT OPS CHK OK.
- [SDR HALA2021030100022](https://openairdocs.org/sdr/HALA2021030100022), Feb 26, 2021: BATTERY PACK. INOPERATIVE. EMER EQ - CATWALK EMERGENCY EXIT FLOOR LIGHTS INOP. // REMOVED & REPLACED EMERGENCY BATTERY PER AMM 33-51-03, OPS CHECK GOOD
- [SDR HALA2020061000124](https://openairdocs.org/sdr/HALA2020061000124), Jun 9, 2020: UNKNOWN. UNKNOWN. IN FLIGHT - ENG L FUEL PRESS FUEL LINES IN FUEL PAGE WERE GREEN. NO DEVIATIONS ON ENGINE INDICATIONS. FROM OTHER ENGINE. CREW DECLARED AN EMERGENCY. PERFORMED F
- [SDR HALA2019100400400](https://openairdocs.org/sdr/HALA2019100400400), Oct 3, 2019: OIL SYSTEM. OVERSERVICED. SMELL IN CABIN AND COCKPIT-DESCRIBED AS BURNING PLASTIC, OILY, VOMIT 2-3 MINUTES AFTER TAKEOFF. SMELL LASTED 1-2 MINUTES. // FOUND ENGINE 1 AND 2 OIL OVER SERVI
- [SDR HALA2019090500368](https://openairdocs.org/sdr/HALA2019090500368), Aug 26, 2019: VALVE. CORRODED. NR00112 - RIGHT FUEL VENT VALVE CORRODED (M). REMOVED AND REPLACED THE RIGHT WING FUEL VENT VALVE PER AMM 28-12-04. OP'S AND LEAK CHECK GOOD.
- [SDR HALA2019090600378](https://openairdocs.org/sdr/HALA2019090600378), Aug 25, 2019: BRACKET. CORRODED. S/M AFT ACCESSORY COMPARTMENT: CATWALK PANEL RETAINING BRACKET RIGHT SIDE SURFACE CORROSION AND LOOSE RIVET. (AFT PANEL) (MARKED) 1. REMOVED AFT ACCRY CATWALK P
- [SDR HALA2019090600377](https://openairdocs.org/sdr/HALA2019090600377), Aug 25, 2019: TEE FITTING. CORRODED. MODERATE CORROSION ON TEE FITTING IN APU ENCLOSURE AT STA 1095. 1. CUT-OUT CORROSION DAMAGE PER SRM 51-70-11-2R-2. HFEC CHECK OK NO CRACK NOTED. FABRICATED ANGL
- [SDR HALA2019090600376](https://openairdocs.org/sdr/HALA2019090600376), Aug 25, 2019: SPAR. CORRODED. LEFT WING REAR SPAR LOWER TANG SERVERE CORROSION STATION 360 - 366 (M) O/B OF O/B FLAP HINGE. 1. REPAIRED PER E105-491102-PERM VER A.
- [SDR HALA2019090600375](https://openairdocs.org/sdr/HALA2019090600375), Aug 25, 2019: SPAR. CORRODED. LEFT WING REAR SPAR LOWER TANG MODERATE CORROSION STATION XRS 184 - 188 (M) 1. REMOVED CORROSION PER SRM 51-10-04. 2. HFEC OK. CHORD 1.0 SPAN 3.75 ADJ .173 REM 
- [SDR HALA2019090600374](https://openairdocs.org/sdr/HALA2019090600374), Aug 25, 2019: FORMER. CRACKED. KEEL AREA - RIGHT SIDE - UNDERWING BARREL KEEL BEAMS AND CANTED KEEL - FORMER CRACKED AT STA Y = 694.500 (FORMER INSL 9923453-509) REPAIRED PER E105-491104-PERM
- [SDR HALA2019090600373](https://openairdocs.org/sdr/HALA2019090600373), Aug 25, 2019: FITTING. CRACKED. FORWARD CARGO COMPARTMENT BULKHEAD FITTING CRACKED ALONG LONGERON 24 RIGHTHAND SIDE, FITTING P/N 3971162-2. 1) REMOVED FITTING AS REQUIRED. PICKED UP HOLES ON N
- [SDR HALA2019090600372](https://openairdocs.org/sdr/HALA2019090600372), Aug 25, 2019: FITTING. CORRODED. AFT ACCY MODERATE CORROSION ON LONGERON END FITTING PN 3914653-1 STA 1054 AT L24L. REMOVED END FITTING 8-5-19 NEW FITTING PILOT HOLES DO NOT LINE UP WITH EXISTI
- [SDR HALA2019090600371](https://openairdocs.org/sdr/HALA2019090600371), Aug 25, 2019: BRACKET. CORRODED. AFT ACCY COMP.FWD CATWALK LOWER BRACKET MOD CORROSION//1. REMOVED AND INSTALLED NEW CATWALK LOWER SUPPORT BRACKET P/N 9915537-25 PER DRAWING# 9915537.
- [SDR HALA2019090500370](https://openairdocs.org/sdr/HALA2019090500370), Jul 7, 2019: ATTACH ANGLE. CRACKED. LT LOWER WING TO FUSELAGE ATTACH ANGLE FOUND CRACKED AROUND ONE FASTENER HOLE. ANGLE IS LOCATED AT STA 661 BETWEEN L-22L AND L-21L. TRIMED OUT CRACK AS REQUIRED
- [SDR HALA2019090500367](https://openairdocs.org/sdr/HALA2019090500367), Jul 7, 2019: SPLICE ANGLE. CRACKED. LEFT WING T/E 4981366-1 SPLICE ANGLE CRACKED FWD OF INBD SPOILER. REMOVED AND REPLACED ANGLE, 4981366-1 PER DWG 59Y2156. PRIMED AND PAINTED AREA PER SRM 51-22-0
- [SDR HALA2019090500366](https://openairdocs.org/sdr/HALA2019090500366), Jul 7, 2019: SPAR. CORRODED. LEFT WING REAR SPAR LOWER TANG SERVER CORROSION STATION 360. 366 (M) 0/B OF 0/B FLAP HINGE. TRIMMED OUT CORRODED FLANGE AT XRS 360 TO 366. PERFORMED HIGH FREQUE
- [SDR HALA2019011500026](https://openairdocs.org/sdr/HALA2019011500026), Jan 13, 2019: RETRACT CYLINDER. DEFECTIVE. SUP - ATB LEFT GEAR INDICATION REMAINING RED WITH GEAR HANDLE UP. CHECKED LT MLG UP AND LATCHED PROX SENSOR PER AMM 32-61-00-820-804 CHECKED GOOD AND SENSOR REA
- [SDR HALA2018111500589](https://openairdocs.org/sdr/HALA2018111500589), Nov 14, 2018: PIN. MISSING. SERVICE DOOR SLIDE NEEDS TO BE REPLACED. RETAINING PIN MISSING. REPLACED FWD SERVICE DOOR SLIDE PER AMM 25-61-03. SECURITY CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2018100800477](https://openairdocs.org/sdr/HALA2018100800477), Oct 7, 2018: TIRE. RUPTURED. NR 3 MAIN TIRE FOUND BLOWN OUT, AT THE GATE. FOUND NR 3 MAIN TIRE INNER SIDEWALL RUPTURED. REPLACED NR 3 MAIN TIRE ASSY PER AMM 32-41-01 SPIN CHK OK. INSPECTED 
- [SDR HALA2018062900317](https://openairdocs.org/sdr/HALA2018062900317), Jun 28, 2018: DRAIN LINE. LOOSE. FOUND EXTERNAL EMERGENCY LIGHT DOES NO TURN OFF WITH THE SWITCH IN THE OFF POSITION. FOUND THE DRAIN LINE LOOSE, RECONNECTED THE DRAIN LINE THAT WAS LEAKING ON 
- [SDR HALA2018040500135](https://openairdocs.org/sdr/HALA2018040500135), Apr 3, 2018: COALESCER BAG. UNKNOWN. COCKPIT AND CABIN TEMPERATURES IN EXCESS OF 90 F, UNABLE TO CONTINUE NORMAL OPERATIONS WITH THE DEFERRED RIGHT PACK. REMOVED AND REPLACED THE COALESCER BAGS IAW
- [SDR HALA2018031200089](https://openairdocs.org/sdr/HALA2018031200089), Mar 9, 2018: VIA. MALFUNCTIONED. FMS SUDDENLY WENT TO STANDBY MODE MID FLIGHT. RETURNED TO DEPARTURE. REPLACED THE NR 1 VIA IAW AMM 31-43-01. OK FOR SERVICE.
- [SDR HALA2017070400179](https://openairdocs.org/sdr/HALA2017070400179), Jul 4, 2017: UNKNOWN. ODOR. POTENTIAL BURNED ELECTRICAL WIRE ODOR AT ROWS 18 AND 19. INSPECTED SURROUNDING AREA ROWS 17-19 FOR POSSIBLE ELECTRICAL BURNING ODOR. NO ODOR NOTED.
- [SDR HALA2017031000057](https://openairdocs.org/sdr/HALA2017031000057), Mar 10, 2017: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY AND BATTERY IAW AMM 31-51-03. OPS CHECK OK.
- [SDR HALA2016022000053](https://openairdocs.org/sdr/HALA2016022000053), Feb 20, 2016: TARGET. LOOSE. RIGHT LANDING GEAR LIGHT REMAINED RED UPON DEPARTURE, AFTER RAISING GEAR. FOUND MLG DOOR SENSOR TARGET LOOSE AND OUT OF POSITION. REPOSITIONED AND RESECURED DOO
- [SDR HALA2015122100248](https://openairdocs.org/sdr/HALA2015122100248), Dec 21, 2015: SMOKE DETECTOR. FALSE ACTIVATION. CARGO SMOKE AFT INDICATION AND WARNING ILLUMINATED ON GROUND WHILE LOADING BAGS. CARGO SMOKE TEST, OK. NO DEFECTS. OK FOR SERVICE.
- [SDR HALA2015082500168](https://openairdocs.org/sdr/HALA2015082500168), Aug 25, 2015: ENGINE. FLAMED OUT. NR 1 ENGINE FLAMED OUT AT 40 KNOTS, DURING TAKEOFF ROLL. ENGINE CHANGE IN PROCESS.
- [SDR HALA2015070900134](https://openairdocs.org/sdr/HALA2015070900134), Jul 9, 2015: SWITCH. MALFUNCTIONED. EMERGENCY EXIT LIGHTS IN FWD GALLEY FLASHING ON DESCENT AND TAXI INTO GATE. DID SHAKE TEST FROM B1-4 EMERGENCY LT ARM & CHECKED CIRCUIT BREAKERS TO ALL CONNECTI
- [SDR HALA2015032000049](https://openairdocs.org/sdr/HALA2015032000049), Mar 20, 2015: BULKHEAD WEB. DAMAGED. BS 110 BULKHEAD WEB JUST AFT OF NLG CENTER LOCKING DAMAGED. REPAIRED IAW SRM 53-02-01, REPAIR FIG 202, SHEET 3.
- [SDR HALA2015031200050](https://openairdocs.org/sdr/HALA2015031200050), Mar 12, 2015: FLOOR SUPPORT. CRACKED. CABIN FLOOR SUPPORT CRACKED BS 655, LBL 15. R & R FLOOR SUPPORT IAW SRM 51-41-05.
- [SDR HALA2015030700034](https://openairdocs.org/sdr/HALA2015030700034), Mar 7, 2015: NONE. NONE. REPLACED TAILCONE SLIDE DUE TO PRECAUTIONARY, DID NOT DEPLOY. REPLACED TAILCONE SLIDE IAW AMM 25-61-02-400-801.
- [SDR HALA2014061700085](https://openairdocs.org/sdr/HALA2014061700085), Jun 17, 2014: WARNING MESSAGE. ILLUMINATED. AIR SYS FAULT, LT ENGINE, FAN AIR VALVE AIR TURN BACK. OPEN
- [SDR HALA2014040500040](https://openairdocs.org/sdr/HALA2014040500040), Apr 5, 2014: TIRE. FAILED. NR 1 MLG TIRE TREAD SEPARATING AND THROWN. REPLACED NR 1 MAIN TIRE IAW AMM 32-41-01. SPIN CHECKED GOOD.
- [SDR HALA2014022100031](https://openairdocs.org/sdr/HALA2014022100031), Feb 21, 2014: SENSOR. MALFUNCTIONED. AIR DIVERSION, AIR SYS FAULT DURING FLIGHT, FAN AIR VALVE, TROUBLESHOT AIR SYS FAULT IAW FIM 36-10 TASK 829. INSPECTED FAV PILOT FILTER AND LINES FOR LEAKS AND 

All 53: https://openairdocs.org/aircraft/N491HA/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/N491HA/stcs.md

## Related

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

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