# N492HA: 2004 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: 55181
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 27, 2004
- Certificate issued: March 6, 2024
- Expires: March 31, 2031
- Mode S code: A61836
- 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=492HA
- Page: https://openairdocs.org/aircraft/N492HA

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/N492HA/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 N492HA.

## FAA accident and incident reports

None matched to N492HA.

## Service difficulty reports (40)

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 ASAA2026082466519](https://openairdocs.org/sdr/ASAA2026082466519), Aug 24, 2026: BATTERY. UNSERVICEABLE. OVERWING EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. REPLACED OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. AC OK TO CONTINU
- [SDR ASAA2026081666366](https://openairdocs.org/sdr/ASAA2026081666366), Aug 16, 2026: LIGHT. INOPERATIVE. FWD LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. GROUNDED - YES. OPS CHECK OK PER AMM 33-51-00.
- [SDR ASAA2026063065628](https://openairdocs.org/sdr/ASAA2026063065628), Jun 30, 2026: COMPRESSOR. STALLED. RETURN TO AIRPORT -LEFT ENGINE COMP STALL ON TAKEOFF DOUBLE BANG AT GEAR RETRACTION - RAN AT IDLE. GROUNDED - YES. PERFORME EEC BITE & FAULT REVIEW - NO FAULTS.
- [SDR ASAA2026021763443](https://openairdocs.org/sdr/ASAA2026021763443), Feb 17, 2026: WINDSHEAR SYS. FALSE INDICATION. INFO TO MX ABORT/ REJECTED TAKEOFF IN OGG DUE TO HEAD WINDSHEAR AURAL MESSAGE GROUND SPEED AUPPROX 80 KTS. IAS APPROX 100 KTS. GROUNDED - YES. PERFORM TEST WIND
- [SDR HALA20241004047](https://openairdocs.org/sdr/HALA20241004047), Oct 3, 2024: LAMP. INOPERATIVE. COCKPIT EMERGENCY LIGHT INOP. RELAMPED CP EMERGENCY LIGHTS AND INSTALLED NEW BATTERY PACK AT B5-123, OPS TEST PER AMM 33-51-03 OK.
- [SDR HALA20240528028](https://openairdocs.org/sdr/HALA20240528028), May 26, 2024: COMPRESSOR. STALLED. LEFT ENG COMPRESSOR STALL. REMOVED ENG1 BOOSTER BLEED VALVE (BBV) PER AMM 75-32-01 5/26/24 24713. INSTALLED BOOSTER BLEED VALVE IN SERVCABLE CONDITION ON #1 ENG
- [SDR HALA20240524026](https://openairdocs.org/sdr/HALA20240524026), May 23, 2024: COMPRESSOR. STALLED. ENG L COMP STALL ON TAKE OFF @ 1600' (ATB). PERFORMED EEC 1 BITE - FC 801105 STARTER AIR VALVE OUT OF POSITION. REPLACED #1 ENGINE START VALVE PER AMM 80-11-03.
- [SDR HALA20240521025](https://openairdocs.org/sdr/HALA20240521025), May 20, 2024: COMPRESSOR. STALLED. ATB - ENG L. COMP STALL @ APPX 1500' ON CLIMBOUT. CONDITION IMPROVED ON POWER REDUCTION. NORMAL LANDING PERFORMED. COMPLETED INSPECTION OF THE ENGINE AFTER HIGH
- [SDR HALA20240401017](https://openairdocs.org/sdr/HALA20240401017), Mar 30, 2024: BLADE. DAMAGED. #5 FAN BLADE #2 ENGINE MAJOR DAMAGE. REMOVED #2 ENG BLADE SET PER AMM72-38-15. 17601 3-29-24 PERFORMED INSPECTION OF #2 ENGINE FOR FOD PER AMM 72-00-00--200-809
- [SDR HALA2022100600269](https://openairdocs.org/sdr/HALA2022100600269), Oct 6, 2022: NONE. NONE. BOTH OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. OK FOR SVC.
- [SDR HALA2022011800016](https://openairdocs.org/sdr/HALA2022011800016), Jan 14, 2022: CABLE. INOPERATIVE. EMER EQ - LFT MAIN CABIN DOOR EMER SLIDE ARMING CABLE INOP // REMOVED AND REPLACED 1L DOOR EMERG SLIDE ARMING CABLE. SECURE OK TO CONTINUE.
- [SDR HALA2021120800183](https://openairdocs.org/sdr/HALA2021120800183), Dec 7, 2021: ENGINE. INOPERATIVE. CREW REPORTED THAT INBND TO OGG THEY HAD ENG1 BRG OVHT MSG, PER FCOM PROCEDURES CREW SHUT DOWN AFFECTED ENG // MX TROUBLESHOOTING, FOUND METAL FINDINGS FROM OIL
- [SDR HALA2021050300053](https://openairdocs.org/sdr/HALA2021050300053), May 2, 2021: DOOR. OUT OF ADJUST. EMER EQ - MAIN ENTRY DOOR WILL NOT CLOSE PROPERLY -REPEAT WRITE UP // ACCOMPLISHED AMM 52-11-01/501 ADJUSTMENT TEST DOOR ,PASSENGER FORWARD ENTRY TEST OPS CK OK
- [SDR HALA2021043000052](https://openairdocs.org/sdr/HALA2021043000052), Apr 29, 2021: LOCK. OBSTRUCTED. EMER EQ - MAIN ENTRY DOOR WILL NOT CLOSE PROPERLY // FOUND SAFETY WIRE ON LOCK ADJUSTMENT ARM CAUSING JAM. REMOVED AND REPLACED SAFETY. OPS CHECK OK. OK FOR SER
- [SDR HALA2020120800216](https://openairdocs.org/sdr/HALA2020120800216), Dec 7, 2020: ENGINE. FAILED. ATB-RT ENGINE COMP STALL RT ENGINE OIL PRESS 0. REMOVED & REPLACED #2 ENG PER W/O 181624 REF TASK CARD E1128-717-72-003-INSTALL OPS/LEAK CHECK OK.
- [SDR HALA2020100100190](https://openairdocs.org/sdr/HALA2020100100190), Sep 30, 2020: LENS. DETACHED. MISSING EMERGENCY LIGHT COVER AT ROW 11 RT. COVER DOES NOT HOLD ONTO ASSEMBLY. REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHT ASSEMBLY AT ROW 11 RTM, PER AMM
- [SDR HALA2020092903138](https://openairdocs.org/sdr/HALA2020092903138), Sep 29, 2020: BEAM. CRACKED. 492 C CHECK. SMALL CRACKS ON THE MED NR 6 BEAM (P/N: 9955757-503) AT/NEAR THE BAYONET CRANK FITTING BOLT HOLE. REPAIRED MED NR 6 BEAM, PER E105-B10650-PERM 08/1
- [SDR HALA2020092903137](https://openairdocs.org/sdr/HALA2020092903137), Sep 29, 2020: STRUCTURE. CORRODED. 492 C CHECK. SM S/C AROUND STA 974 AND LONG 30 (M). REMOVED CORROSION, PER B717SRM 51-10-04-OG-O. FOUND TO BE BEYOND LIMITS, PER SRM 53-00-090-1A 0 FIG 103 M66 
- [SDR HALA2020092903136](https://openairdocs.org/sdr/HALA2020092903136), Sep 29, 2020: FORMER. CORRODED. 492 C CHECK. CORROSION UNDERNEATH BONDING WIRE ON LEFT FILLET FORMER 4TH BACK FROM FWD (M). REMOVED CORROSION, PER SRM 51-10-04. FOUND TO BE OUT OF LIMITS. M66 
- [SDR HALA2020092903135](https://openairdocs.org/sdr/HALA2020092903135), Sep 29, 2020: FLANGE. CRACKED. 492 C CHECK. CRACKED END FLANGE OF THE KEEL TO CANTED PANEL ATTACH FORMER AT Y=715. REMOVED FORMER FOR REPAIR. 08/18/2020 MECH 16912 M66 SUBMITTED 2. REPAIRED P
- [SDR HALA2020092903134](https://openairdocs.org/sdr/HALA2020092903134), Sep 29, 2020: FRAME. CORRODED. 492 C CHECK. CORROSION DISCOVERED ON THE STA 1098.868 FRAME TEE (PN 9971144-61) AT L-28L. THE CORROSION WAS MECHANICALLY REMOVED WITH MORE THAN 50% MATERIAL LOS
- [SDR HALA2020092903133](https://openairdocs.org/sdr/HALA2020092903133), Sep 29, 2020: DOUBLER. CRACKED. 492 C CHECK, DURING ROUTINE MAINTENANCE TASKS, HWI DISCOVERED A CRACK IN THE STA 1178 BULKHEAD DOUBLER (PN 9911839-265) AND SKIN PANEL (PN 5912141-77), JUST INB
- [SDR HALA202001300019](https://openairdocs.org/sdr/HALA202001300019), Jan 30, 2020: OXYGEN MASK. FAILED. BTB - CAPTAIN OXYGEN MASK LEAKING AT HEADSTRAP AND UNABLE TO BROADCAST ON ON VHF1 OR VHF2,MULTIPLE RESET ATTEMPTS UNSUCESSFUL // REPLACED FAULTY O2 MASK. LOG PA
- [SDR HALA2019111400483](https://openairdocs.org/sdr/HALA2019111400483), Nov 13, 2019: VANE. DENTED. FOUND A DENT L-1/2 " W 1/4 " D 0.006 " WITH A CRACK 9/32 " LONG AT THE CENTER OF THE DENT DAMAGE LOCATED ON L/H AFT MOVEABLE VANE 15 1/2 " FROM INBOARD EDGE 12 
- [SDR HALA2019103100463](https://openairdocs.org/sdr/HALA2019103100463), Oct 31, 2019: PUMP. FAILED. ETOPS OPEN - BTB, HYDRAULIC FAIL //PER FIM REPLACE ENG HYD PUMP I.A.W. AMM 29-11-01-400-801. OPS AND LK CK GOOD. OK FOR SVC. REF LOG PAGE DEFECT 764801
- [SDR FOTR2018110918001](https://openairdocs.org/sdr/FOTR2018110918001), Nov 9, 2018: DOUBLER. DENTED. LH ELEVATOR HAS A DENT, 1" X 1" ON THE TOP, O/B SIDE, IN BETWEEN XE 225.834 AND XE 204.114, OR HINGE POINTS 5 AND 6
- [SDR HALA208082000386](https://openairdocs.org/sdr/HALA208082000386), Aug 19, 2018: CONTROL UNIT. FALSE INDICATION. AT ABOUT 1200 FT. EMERGENCY POWER CAME ON IN FLT, DURING SHORT FINAL, PERFORMED OPS TEST OF EPCU IAW AMM 24-21-02-700-801. OPS CHECKED OK, OK FOR SERVICE.
- [SDR HALA2018032100118](https://openairdocs.org/sdr/HALA2018032100118), Mar 20, 2018: ENGINE. WARNING MESSAGE. CREW REPORTED THE RT ENGINE LOW OIL PRESSURE WARNING AND ENGINE RT SYS FAIL ALERT MESSAGE. REMOVED AND REPLACED THE NR 2 ENGINE IAW M143-717. OPS AND LEAK CHECK
- [SDR HALA2017122600330](https://openairdocs.org/sdr/HALA2017122600330), Dec 25, 2017: COMPRESSOR BLADE. MISSING. ATB/ RIGHT ENGINE COMP STALL ON EICAS AUDIBLE BANG HEARD BY CREW. BORESCOPE REQUIRED. REMOVED HIGH PRESSURE COMPRESSOR FAIRING AND 6 EA PLUGS. REMOVED HP TURBIN
- [SDR HALA2017122600318](https://openairdocs.org/sdr/HALA2017122600318), Dec 25, 2017: BLADE. MISSING. NR 2 ENGINE COMPRESSOR STALLED IN FLIGHT. REMOVED HIGH PRESSURE COMPRESSOR FAIRING AND SIX PLUGS. REMOVED HP TURBINE STAGE 2, LP TURBINE STAGE 1, LP TURBINE STA
- [SDR HALA201708210230](https://openairdocs.org/sdr/HALA201708210230), Aug 19, 2017: UNKNOWN. UNKNOWN. VIOLENT BUFFETING AND ROLLING MOMENTS IN BOTH DIRECTIONS ON FLAP EXTENSION. NO INDICATIONS. RETRACTED, EXTENDED AGAIN SLOWLY. OPS NORMAL SECOND ATTEMPT.
- [SDR HALA2017080400217](https://openairdocs.org/sdr/HALA2017080400217), Aug 4, 2017: COMPRESSOR. STALLED. RT ENGINE COMPRESSOR STALLED, FOLLOWED BY ENGINE VIBRATION HIGH. SHUT DOWN THE ENGINE. ENGINE CHANGE IN WORK.
- [SDR HALA2016041700113](https://openairdocs.org/sdr/HALA2016041700113), Apr 17, 2016: PITOT HEAD. OBSTRUCTED. ON TAKEOFF ROLL AT 80 KTS F/O'S AIRSPEED INDICATOR STARTED DROPPING OFF DUE TO A BEE IN F/O'S PITOT TUBE. CONFIRMED BEE STUCK TO F/O'S PITOT PROBE, CLEARED LINE
- [SDR HALA2015082700174](https://openairdocs.org/sdr/HALA2015082700174), Aug 27, 2015: TIRE. SEPARATED. NR 3 MAIN TIRE CAP COMING OFF. TIRE SEPARATED ON TAKEOFF. R & R NR 3 MAIN WHEEL AND TIRE IAW TASK 32-41-01-400-802. SPIN CHECK OK. OPS CHECK OK, ACFT OK FOR SER
- [SDR HALA2015040400058](https://openairdocs.org/sdr/HALA2015040400058), Apr 4, 2015: SWITCH. MALFUNCTIONED. LAVATORY SMOKE TEST STAYS ON AFTER TEST. RESET TEST SWITCH FOR LAVATORY SMOKE. MESSAGE EXTINGUISHED. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA2014011600006](https://openairdocs.org/sdr/HALA2014011600006), Jan 16, 2014: DISPLAY. INOPERATIVE. NR 1 MCDU/FMC WENT BLANK AFTER TAKE OFF. REPLACED NR 1 MCDU. OPS CHECKED OK IAW MM 31-65-01.
- [SDR HALA2013100400131](https://openairdocs.org/sdr/HALA2013100400131), Oct 8, 2013: SHUTOFF VALVE. INOPERATIVE. DURING START ANTI-SKID FAIL, RETURNED TO GATE, BRAKE RETURN LINE SHUTOFF VALVES. FOUND RT BRAKE LINE, SHUTOFF VALVE INOPERATIVE.
- [SDR HALA2012060100154](https://openairdocs.org/sdr/HALA2012060100154), Jun 1, 2012: SMOKE DETECTOR. FALSE ACTIVATION. STATIS MESSAGE FOR LAVATORY SMOKE ON. RESET SMOKE DETECTOR AFT LT, TEST SMOKE DETECTOR CHECKED GOOD.
- [SDR HALA2012022400072](https://openairdocs.org/sdr/HALA2012022400072), Feb 24, 2012: PUMP. FAILED. LAVATORY SMOKE ALERT WITH ODOR. RETURN TO GATE, AFT RT LAVATORY LOCKED CLOSED. R & R CHEMICAL INJECTION PUMP AND ENVIROMENTAL CLEAN, OPS AND LEAK CHECKED OK IAW
- [SDR HALA2012022300069](https://openairdocs.org/sdr/HALA2012022300069), Feb 23, 2012: POWER SUPPLY. MALFUNCTIONED. AFT EMERGENCY EXIT SIGN ILLUMINATED. R & R AFT EXIT DOOR POWER SUPPLY. OPS CHECKED EMERGENCY LIGHTING, OK.

## 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/N492HA/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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