# N490HA: 2000 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 Deutschland BR700-715A130](https://openairdocs.org/engine/rolls-royce-deutschland-br700-715a130) (registry code 54006) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company), [TCDS E00061EN](https://openairdocs.org/tcds/E00061EN) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs) - Serial number: 55151 - Year built: 2000 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 10, 2008 - Certificate issued: June 28, 2011 - Expires: June 30, 2027 - Mode S code: A610C8 - 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=490HA - Page: https://openairdocs.org/aircraft/N490HA 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. ## ADs that may apply (OpenAirDocs): 64 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 Deutschland BR700-715A130) - [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 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 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 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 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 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 2005-16-12](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 ### 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 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 All 74: https://openairdocs.org/aircraft/N490HA/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 N490HA. ## FAA accident and incident reports None matched to N490HA. ## Service difficulty reports (37) 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 ASAA2026092467059](https://openairdocs.org/sdr/ASAA2026092467059), Sep 24, 2026: ACTUATOR. ABNORMAL. AT FL210 AND 330 KNOTS WHILE EXTENDING THE FLIGHT SPOILERS THE PLANE ROLLS TO THE LEFT DURING THE INITIAL SPOILER DEPLOYMENT. ONCE SPOILERS FULLY DEPLOYED THE P - [SDR ASAA2026052864975](https://openairdocs.org/sdr/ASAA2026052864975), May 28, 2026: LATCH. INOPERATIVE. IL BOARDING DOOR LATCH NOT WORKING. GROUNDED - YES. PASSENGER DOOR LATCH LUBRICATED AND CHECK GOOD. - [SDR ASAA2026022463555](https://openairdocs.org/sdr/ASAA2026022463555), Feb 24, 2026: LAMP. INOPERATIVE. FWD FLIGHT ATTENDANT LAV SMOKE RED LIGHT ON THE CEILING IS INOP. GROUNDED - YES. RELAMPED FWD FA LAV SMOKE LIGHT OPS CHECK GOOD. OK FOR SVC. - [SDR ASAA2026021663450](https://openairdocs.org/sdr/ASAA2026021663450), Feb 16, 2026: LOCK. LACK OF LUBE. 1L DOOR HARD TO CLOSE. GROUNDED - YES. 1L DOOR HOLD OPENLOCK WAS LUBRICATED. THE DOOR OPERATES AS INTENDED. OPS CHECK GOOD. A/C OK FOR SVC. - [SDR HALA20240621031](https://openairdocs.org/sdr/HALA20240621031), Jun 20, 2024: POWER SUPPLY. NO TEST. OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLCAED OVERWING EMERGENCY LIGHTS POWER SUPPLY PER AMM 33-51-05. OPS CHECK GOOD. OK FOR SERVICE - [SDR HALA20240422021](https://openairdocs.org/sdr/HALA20240422021), Apr 19, 2024: EEC. FAULTED. ATB - ENG LEFT SYS FAIL. PERFORMED WIRE CHECK PER FIM 77-21 TASK 803 ENGINE 1 J8, PIN 42 AND 43 - AVERAGE 9.15 OHMS NO SHORT TO GROUND. J7, PIN 42 AND 43 - AVER - [SDR HALA20240212007](https://openairdocs.org/sdr/HALA20240212007), Feb 9, 2024: BUNGEE. FAULTED. "WHEN LNDG GEAR EXTENDED NOSE GEAR UNSAFE LT. MANUAL GEAR EXTESION PERFORMED. REMOVED LANDING GEAR CONTROL VALVE PER AMM 32-31-01. NEED TO INSTALL REF AMM 32-31 - [SDR HALA2023053000031](https://openairdocs.org/sdr/HALA2023053000031), May 29, 2023: UNKNOWN. UNKNOWN. GEAR DOOR OPEN' ALERT, FOUND INBD MLG DOOR OPEN. RIGHT SYSTEM ACCUMULATOR NITROGEN PRE-CHARGE AT ZERO. REMOVED AND REPLACED RIGHT SYSTEM ACCUMULATOR PER AMM 29- - [SDR HALA2023051000025](https://openairdocs.org/sdr/HALA2023051000025), May 10, 2023: UNKNOWN. UNKNOWN. ATB - PSEU FAIL ALERT IN FLIGHT. REMOVED AND REPLACED NLG LOCK PROX SENSOR PER 32-61-03. SENSOR TEST GOOD (5742). NS. OK FOR SERVICE. - [SDR HALA2023032900012](https://openairdocs.org/sdr/HALA2023032900012), Mar 28, 2023: UNKNOWN. UNKNOWN. SUPPLEMENTAL SUBMISSION TO HALA2023032700011. RESOLUTION UPDATED. ENG L COMP STALL ON TAKE OFF ROLL BTB ALERT DISAPPEARED WHEN ENG IDLE. BORESCOPE PER AMM 72-00 - [SDR HALA2023032700011](https://openairdocs.org/sdr/HALA2023032700011), Mar 27, 2023: UNKNOWN. UNKNOWN. ATO - L ENG COMPRESSOR STALL. NEED TO INSTALL ENG S/N 13105 TO REPAIR. - [SDR HALA2020092800189](https://openairdocs.org/sdr/HALA2020092800189), Sep 26, 2020: ACTUATOR. DEFECTIVE. ATB - AP1 DISCONNECTED DURING CLIMB WHEN RE-ENGAGED IN AP2. PLANE TURNED SEVERAL DEGREES OFF COURSE BEFORE FINDING COURSE AGAIN. PERFORMED FCC 1 & 2 BITE TEST, - [SDR HALA2020092800188](https://openairdocs.org/sdr/HALA2020092800188), Sep 26, 2020: EEC. DEFECTIVE. ATB AT CRUISE JUST PRIOR TO DESCENT "SELECT FADEC ALTN" MSG CAME ON LT ENGINE PERFORMED QRH PROCEDURE. ATB TO HNL ADVISED BY MOC. PERFORMED BITE TEST OF EEC1, P - [SDR HALA2020073000160](https://openairdocs.org/sdr/HALA2020073000160), Jul 29, 2020: PROBE. MALFUNCTIONED. RIGHT ENGINE IGNITER INTERMITTENTLY COMES ON IN IDLE DURING DESCENT. PERFORMED FIM 72-00, TASK 803, REMOVED & REPLACED N2 SPEED PROBE IAW AMM 77-12-01, OPS & LE - [SDR HALA2020052900117](https://openairdocs.org/sdr/HALA2020052900117), May 28, 2020: POWER SUPPLY. INOPERATIVE. OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY PER AMM 33-51-05. OPERATION CHECK GOOD. - [SDR HALA2020052500114](https://openairdocs.org/sdr/HALA2020052500114), May 24, 2020: FIRE DETECTOR. FAILED. "FIRE R-B FAULT' ON STATUS.// PERFORMED TROUBLESHOOTING PER FIM 26-11 TASK 806 UP TO ITEM F STEP 2. PENDING AVIONICS WIRE CHECK. PERFORM FIM 26-11 TASK 806 FROM - [SDR HALA2019101500415](https://openairdocs.org/sdr/HALA2019101500415), Oct 14, 2019: CAP. MISSING. ANTI SKID L FAIL LEVEL 2 ALERT AT 75 KIAS. FOUND WHEEL XDUCER HUB CAP MISSING. VERIFIED WHEEL XDUCER WORKING PER AMM 32-45-00-730-802. INSTALLED NEW HUB CAP ASS - [SDR HALA2018121000640](https://openairdocs.org/sdr/HALA2018121000640), Dec 9, 2018: WIRE. DISCONNECTED. EMERGENCY EXIT SIGN JUST AFT OF L2 DOOR (GALLEY SERVICE DOOR) INOP. // RECONNECTED WIRES. OPS CHECK OK. - [SDR HALA2018081700383](https://openairdocs.org/sdr/HALA2018081700383), Aug 16, 2018: ELECTRICAL SYS. NO TEST. EMERGENCY POWER NOT TESTING. PERFORMED FUNCTIONAL TEST OF EMERGENCY POWER SYSTEM IAW AMM 24-24-00. OPS CHECKED OK, NO FAULTS NOTED. - [SDR HALA2018022000046](https://openairdocs.org/sdr/HALA2018022000046), Feb 18, 2018: COMPRESSOR. STALLED. ENG L COMP STALL, BTB. BORESCOPED NR 1 ENG LPC MM 72-31-00-200-802, MM HPC 72-33-00-200-801, MM HPT 72-50-00-200-802 AND LPT MM 72-50-00-200-801 FOUND NO DEFECT - [SDR HALA2017082100229](https://openairdocs.org/sdr/HALA2017082100229), Aug 18, 2017: TUBE. LEAKING. OIL ODOR NOTED WHILE RUNNING ON APU. REMOVED AND REPLACED FILLER TUBE ASSY IAW 49-91-11. LEAK CHECKED GOOD. - [SDR HALA2017012300013](https://openairdocs.org/sdr/HALA2017012300013), Jan 23, 2017: SIGN. DAMAGED. LIGHTED EXIT SIGN ON FWD CABIN CEILING DAMAGED. REMOVED AND REPLACED FWD CABIN EMERGENCY EXIT SIGN CEILING LIGHT PER WDM 33-51-12. OPS CHECKS OK. OFF: PN: BR906 - [SDR HALA2017010800012](https://openairdocs.org/sdr/HALA2017010800012), Jan 8, 2017: CONTROL UNIT. FAILED. AIR TURN BACK FOR SPOILER FAULT. SPOILER OTB FAILED. FAULT CODES - 276162, 182, 200, 165, 185, 125. R & R SECU IAW AMM 27-61-01. OPS CHECKED GOOD IAW AMM 27-60- - [SDR HALA2016030000072](https://openairdocs.org/sdr/HALA2016030000072), Mar 1, 2016: SKIN. CRACKED. A .2500" FUSELAGE SKIN CRACKED BETWEEN LONGERON 14R AND 15R AT BS 1096. INSTALLED EXTERNAL DOUBLER. - [SDR HALA2014120900205](https://openairdocs.org/sdr/HALA2014120900205), Dec 9, 2014: COALESCER BAG. ODOR. ATB F/A CALLED TO REPORT STRONG ELECTRICAL ODOR IN THE AFT AND FWD CABIN. STRONG ODOR IN THE COCKPIT, GALLEY SWITCH TURNED OFF AND RETURNED FOR LANDING. RAN LT - [SDR HALA2014081800115](https://openairdocs.org/sdr/HALA2014081800115), Aug 18, 2014: LATCH. DAMAGED. AIR TURNBACK AFTER TAKE OFF, CABIN WOULD NOT PRESSURIZE. OUTFLOW VALVE WAS INDICATING "CLOSED POSITION". CABIN INFLOW LOW ALERT. FOUND FWD CARGO DOOR AFT LATCH - [SDR HALA2014013000019](https://openairdocs.org/sdr/HALA2014013000019), Jan 30, 2014: UNKNOWN. ODOR. F/A REPORTED BURNING ODOR IN BACK OF AIRCRAFT AFTER TAKEOFF. AIR TURN BACK. NO INDICATIONS UP FRONT. INSPECTED AFT OF ACFT, NO BURNING ODOR NOTED. SUSPECT PRESE - [SDR HALA2013102300137](https://openairdocs.org/sdr/HALA2013102300137), Oct 23, 2013: DISPLAY. INOPERATIVE. CAPTAIN'S MCDU BLANK AFTER TAKE OFF. REPLACED MCDU. GROUND CHECK OK IAW 31-65-01. - [SDR HALA2013100400129](https://openairdocs.org/sdr/HALA2013100400129), Oct 7, 2013: FMS. MALFUNCTIONED. ATB/FMS BOTH UNUSABLE, CYCLED BOTH VIA NR 1 & VIA NR 2 SYS, PERFORMED RTS TEST PASS ACFT OK FOR SERVICE. - [SDR HALA2013052700070](https://openairdocs.org/sdr/HALA2013052700070), May 27, 2013: PSEU. INOPERATIVE. GEAR UNSAFE LIGHT ON LANDING PULL EMERGENCY GEAR EXTENSION, THREE GREEN. R & R PSEU IAW AMM 32-61-01. RTS PASSED. NO FAULTS NOTED. GEAR SWING, OPS CHECKED GOOD. - [SDR HALA2012031100115](https://openairdocs.org/sdr/HALA2012031100115), Mar 11, 2012: SKIN. DAMAGED. LIGHTING STRIKE - LT ELEVATOR LOW T/E SKIN IS BURNED ALL THE WAY THROUGH. REPAIRED IAW HALM105 FILE NR 490047 INTERIM REPAIR. PERMANENT REPAIR AT NEXT C-CHECK I - [SDR HALA2012031100114](https://openairdocs.org/sdr/HALA2012031100114), Mar 11, 2012: SKIN. DAMAGED. LIGHTING STRIKE - LT ELEVATOR UPPER T/E SKIN IS BURNED ALL THROUGH. DAMAGED AREA IS .7500" X .7500" BETWEEN XH 217.2 & 218., .762 ADJ TO TIP AND MOST FWD FASTEN - [SDR HALA2012030900109](https://openairdocs.org/sdr/HALA2012030900109), Mar 9, 2012: UNKNOWN. DAMAGED. LIGHTNING STRIKE - REPAIR IN WORK. - [SDR HALA2012022600079](https://openairdocs.org/sdr/HALA2012022600079), Feb 26, 2012: HEADREST. OUT OF ADJUST. MAIN CABIN DOOR BINDING AND WAS DIFFICULT TO OPEN. INSPECTED & FOUND MAIN CABIN DOOR INNER PANEL BINDING ON F/A JUMPSEAT HEAD REST. ADJUSTED HEADREST BRACKET. O - [SDR HALA2011043000174](https://openairdocs.org/sdr/HALA2011043000174), Apr 30, 2011: EEC. FAILED. INFLIGHT LEVEL 2 SELECT FADEC ALT LIGHT CAME ON (RT) PERFORMED CHECKLIST. EVERYTHING OK. ADVISED DISP/MAINT. DISP/MAINT ADVISED RETURN TO DEPARTURE. R & R NR 2 - [SDR HALA2010050600204](https://openairdocs.org/sdr/HALA2010050600204), May 6, 2010: SWITCH. FAULTY. ON CLIMBOUT AOA, HEAT FAIL L & R, RUDDER PITOT LIMITER FAIL AND RUDDER IGNITER FAULT LIGHT ILLUMINATED. AIR TURNBACK TO HNL. REPLACED AIR DATA HEAT SWITCH PER W - [SDR HALA2010020200047](https://openairdocs.org/sdr/HALA2010020200047), Feb 2, 2010: BLEED VALVE. MALFUNCTIONED. LT HYD TEMP HI EAD DISPLAY. PERFORMED FIM 29-30 TASK 803 FOUND LT T/R ACCUMULATOR BLEED VALVE KNURLED KNOB NOT FULLY CLOSED. CLOSED VALVE PERFORMED REPAIR CONFI ## 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/N490HA/stcs.md ## Related - Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md - The Rolls-Royce Deutschland BR700-715A130 engine: https://openairdocs.org/engine/rolls-royce-deutschland-br700-715a130.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.