# Service difficulty reports: N478HA

A list on [N478HA](https://openairdocs.org/aircraft/N478HA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 84 reports

- [SDR ASAA2026021763444](https://openairdocs.org/sdr/ASAA2026021763444.md): Charger · faulted · Feb 17, 2026 · N478HA · Boeing 717200 · Electrical Power System
  > EMERGENCY PWR FAIL. GROUNDED - YES. PER FIM 24-24 TASK 803 RESET BATT CHARGER. MESSAGE CLEARED. OK FOR SVC.
- [SDR ASAA2026011862922](https://openairdocs.org/sdr/ASAA2026011862922.md): Battery · inoperative · Jan 18, 2026 · N478HA · Boeing 717200 · Emergency Lighting
  > OVERWING EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THE EMERGENCY LIGHT BATTERY FOR OVERWING LIGHTS IAW 33-51-06. OPS CHKD GOOD. OK FOR SERVICE.
- [SDR ASAA2025121962452](https://openairdocs.org/sdr/ASAA2025121962452.md): Seal · lack of lube · Dec 19, 2025 · N478HA · Boeing 717200 · Passenger/Crew Doors
  > MAIN CABIN DOOR STICKS WHEN CLOSING. GROUNDED - YES. CLOSED MAIN CABIN DOOR FROM THE OUTSIDE AND INSDIE. FOUND NO FAULTS. APPLIED VASOLINE TO MAIN CABIN DOOR SEAL. OK FOR SERVICE.
- [SDR HALA20250804044](https://openairdocs.org/sdr/HALA20250804044.md): Hydraulic System · contaminated · Aug 2, 2025 · N478HA · Boeing 717200 · Hydraulic System, Main
  > REJECTED T/O 8L DUE TO R HYD HIGH TEMP. UNABLE TO MITIGATE W/ MOVEMENT OF FLT CONTROLS / SPOILERS. PERFORMED FIM 29-30 TASK 803. FOUND EXCESSIVE AIR IN R HYD SYSTEM. BLEEDED AIR FROM SYSTEM AS REQUIRED. OPS CHECK GOOD. FAULT FOUND TO BE INTERMITENT. NO DEFECTS
- [SDR HALA20250630037](https://openairdocs.org/sdr/HALA20250630037.md): Warning Message · false activation · Jun 28, 2025 · N478HA · Boeing 717200 · Landing Gear Position and Warning
  > ATB - LEFT GEAR INDICATION RED/UNSAFE WITH GEAR HANDLE UP AFTER TAKE OFF. JACKED UP THE AIRCRAFT PER AMM 07-00-582-811. PERFORMED FUNCTIONAL TEST OF MLG AND NLG EXTENSION AND RETRACTION PER AMM 32-30-00. NO DEFECTS NOTED. PERFORMED SENSOR READOUTS FOR LT AND R
- [SDR HALA20250204003](https://openairdocs.org/sdr/HALA20250204003.md): Manifold · failed · Jan 31, 2025 · N478HA · Boeing 717200 · Airfoil Anti/De-ice System
  > "DIVERSION TO HNL" TAIL ANTI-ICE MANIFOLD FAILED IN ICING CONDITIONS, FLAP 25 LANDING AS PER QRH. FOUND "PODS SYSTEM FAULT" ON FAULT REVIEW. REMOVED AND REPLACED PODS PER AMM 36-23-01. RTS TEST "PASS". NO FAULTS FOUND. A/C OK FOR SVC
- [SDR HALA20240819040](https://openairdocs.org/sdr/HALA20240819040.md): Control Unit · faulted · Aug 16, 2024 · N478HA · Boeing 717200 · Autopilot System
  > AT 1300FT AUTOPILOT DISCONNECTED, AUTO THROTTLES WENT MAX POWER, ALL DU'S WENT BLANK FOR A SECOND. REMOVED AND REPLACED EPCU PER AMM 24-21-02. EPCU OP CK GOOD. PERFORMED VIA 1 &2 EIS OPS TEST PER AMM 31-61-00-720-801. ALSO PERFORMED AFS TEST ON FCC 1&2 PER AMM
- [SDR HALA20240819039](https://openairdocs.org/sdr/HALA20240819039.md): Relay · failed · Aug 16, 2024 · N478HA · Boeing 717200 · Electrical Power System
  > AFTER EPCU DOWNLOAD FOUND EMERGENCY POWER RELAY FAULT ( 54 EPR FAILED CLOSED.). REMOVED AND REPLACED EMERGENCY DC POWER RELAY PER AMM 24-34-05. FUNCTIONAL TEST GOOD PER AMM 24-24-00. OK FOR SERVICE
- [SDR HALA2023051200027](https://openairdocs.org/sdr/HALA2023051200027.md): Unknown · unknown · May 11, 2023 · N478HA · Boeing 717200 · Emergency Lighting
  > CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT MOMENTARILY TURNS ON THEN GOES OUT. REPLACED BATTERY B5120 AT ROW 17DEF, PERFORMED OPS TEST OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-51-00, OPS CHK GOOD, OK FOR SVC.
- [SDR HALA2022042000095](https://openairdocs.org/sdr/HALA2022042000095.md): Pseu · fault message · Apr 20, 2022 · N478HA · Boeing 717200 · Landing Gear Position and Warning
  > ATB - PSEU FAULT MESSAGE ON CLIMB OUT // REPLACED NLG LOCKED PROXIMITY SENSOR ASSY PER AMM 32-61-03-400-804. OPS CHK OK PER AMM 32-61-00-820-802. (FAULT CODE 326083)
- [SDR HALA2022032100080](https://openairdocs.org/sdr/HALA2022032100080.md): None · none · Mar 19, 2022 · N478HA · Boeing 717200 · Fuel Controlling System
  > ATB - DURING CLIMB "SELECT FADEC R ALTN" MESSAGE DISPLAYED YELLOW X ON RIGHT EPR FOLLOWED QRH PROCEDURE. DID NOT RESET // FOUND LTD FAULT CODES 732115 732116ON EEC-2 REF FIM TASK 73-21 TASK 815 STEP E (1) (B) 1) NEED TO REPLACE EEC MECH 15202 03/19/22 REMOVED
- [SDR HALA2020070100135](https://openairdocs.org/sdr/HALA2020070100135.md): Pin · out of position · Jul 1, 2020 · N478HA · Boeing 717200 · Escape Slide
  > MED SLIDE PINS CAME OUT. REMOVED AND REPLACED MAIN ENTRY DOOR SLIDE PER AMM 25-61-01. OPS AND SECURE CHECKS GOOD.
- [SDR HALA2019071500354](https://openairdocs.org/sdr/HALA2019071500354.md): Probe · out of limits · Jul 13, 2019 · N478HA · Boeing 717200 · Engine EGT/TIT Indicating System
  > ATB: ENG R SYS FAIL LIGHT ON RIGHT, TGT GAUGE X THROUGH IT. PER TSM 77-21-803 STEP F4(A) 4(O) MEASURING 8.7 OHMS. STEP K PROBES 6 & 7 OUT OF TOLERANCE 8.2 & 8.3. P1000-J8 CONNECTOR REMOVED. INSTALLED CONNECTOR P1000-J8. #2 ENGINE, NR 6 TGT PROBE INOPERABLE.
- [SDR HALA2019061000286](https://openairdocs.org/sdr/HALA2019061000286.md): Eec · malfunctioned · Jun 8, 2019 · N478HA · Boeing 717200 · Turbine Engine Air Inlet Section
  > ATB - ENG L SYS FAIL ENROUTE FOLLOWED BY REV L FAULT. PERFORMED EEC1 RTS TEST. TEST FAILED. EEC BOX FAULT. REMOVED & REPLACED EEC1 PER AMM 73-21-01. RTS TEST PASSED. PERFORMED FUNCTIONAL CHECK OK L REV PER AMM 78-30-00-720-801. OPS NORMAL. OK FOR SVC.
- [SDR HALA2019050300216](https://openairdocs.org/sdr/HALA2019050300216.md): Power Supply · inoperative · May 2, 2019 · N478HA · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT CEILING LIGHT @ ROW 17 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51-03. BATTERY POWER SUPPLY (B5-120). OPS. CHECK GOOD, OK FOR SVC.
- [SDR HALA2019042320199](https://openairdocs.org/sdr/HALA2019042320199.md): Power Supply · inoperative · Apr 21, 2019 · N478HA · Boeing 717200 · Emergency Lighting
  > ETOPS SIGNIFICATION - LEFT WING EMERGENCY EXIT LIGHT INOP // REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY CONTROL MODULE. PER AMM 33-51-03. OPS CHECK OK. OK FOR SVC
- [SDR HALA2019041500189](https://openairdocs.org/sdr/HALA2019041500189.md): Manifold · failed · Apr 12, 2019 · N478HA · Boeing 717200 · Ice/Rain Protection System
  > ATO - TAIL MANF FAIL DURING T/O ROLL. // PER FLIGHT CREW TAIL ANTI ICE WAS NOT ON. FAULT CODE 362164. FOUND WIRE E9142-35-20 BETWEEN RIGHT & LEFT HORIZONTAL SENSORS SHORTED TO SHIELD. FABRICATED WIRE E9142-35-20 AND INSTALLED PER SWPM 20-10-01 AND WDM 36-23
- [SDR HALA2018121000641](https://openairdocs.org/sdr/HALA2018121000641.md): Static Inverter · malfunctioned · Dec 7, 2018 · N478HA · Boeing 717200 · Pitot/Static System
  > CA'S FMS GOES OFF ON APP WHEN EMER PWR ON MESSAGE IS ON.// REMOVE & REPLACE STATIC INVERTER PER AMM 24-24-01. OPS CK OK. REMOVED & REPLACE CAPT MCDU PER AMM 31-65-00. OPS CK OK. OK FOR SERVICE.
- [SDR HALA2018110500560](https://openairdocs.org/sdr/HALA2018110500560.md): Compressor · damaged · Nov 3, 2018 · N478HA · Boeing 717200 · Engine (Turbine/Turboprop)
  > HIGH SPEED ABORT DUE TO LEFT ENGINE FAILURE / COMPRESSOR STALL.// FOUND #1 ENG HP COMPRESSOR STAGE 5 TO 6 DAMAGE DURING BORESCOPE. // REMOVED AND REPLACED #1 ENGINE. OPS AND LEAK CHECK OK. OK FOR SERVICE.
- [SDR HALA2018061800285](https://openairdocs.org/sdr/HALA2018061800285.md): Actuator · malfunctioned · Jun 17, 2018 · N478HA · Boeing 717200 · Hydraulic System, Main
  > HYD RT TEMP CAUTION LIGHT ON WHILE TAXING TO GATE. ACCOMPLISHED FIM 29-30-TASK 803, BLED THE RT HYDRAULIC SYSTEM TEMP ACTUATORS. OK, WITHIN LIMITS, OK FOR SERVICE
- [SDR HALA2016040400111](https://openairdocs.org/sdr/HALA2016040400111.md): Support Fitting · corroded · Apr 4, 2016 · N478HA · Boeing 717200 · Fuselage, Wing Attach Fittings
  > WING TO BS 832 LOWER END OF SUPPORT FAIRING CORRODED. LT SIDE, ON EXISTENT REPAIR. REMOVED CORROSION AT WING TO BS 832 LOWER END OF SUPPORT FAIRING LT SIDE ON EXISTENT REPAIR, FOUND 100 PERCENT TO BE OUT OF LIMITS IAW SRM 53-00-00 AND R & R PREVIOUS REPAIR I
- [SDR HALA2016032800107](https://openairdocs.org/sdr/HALA2016032800107.md): Spar · cracked · Mar 28, 2016 · N478HA · Boeing 717200 · Wing Spar
  > LT WING AFT SPAR CRACKED AT XR 5324 INSIDE OF FUEL TANK ACCESS PANEL 520HB. REPAIRED THE SPAR IAW PRI EA 16126- P1 AND FINAL EA 16126, REV IR AND E105-478280-PERM.
- [SDR HALA2016032300110](https://openairdocs.org/sdr/HALA2016032300110.md): Fitting · corroded · Mar 23, 2016 · N478HA · Boeing 717200 · Fuselage, Wing Attach Fittings
  > WING TO BS 832 FITTING ON LONGERON 30 CORRODED. REMOVED CORROSION AT WING TO BODY BS 832 FITTING ON LONGERON 30 ORIGINAL MATERIAL 125" REMAINING.098" AND LOSS OF.027", FOUND OUT OF LIMITS IAW SRM 53-00-00. R & R FITTING IAW DWG 5971098, REV E AND DWG S1440
- [SDR HALA2016032200109](https://openairdocs.org/sdr/HALA2016032200109.md): Fitting · corroded · Mar 22, 2016 · N478HA · Boeing 717200 · Trailing Edge Flaps
  > LT WING FLAP INBD FLAP TRACK FITTING CORRODED. REMOVED CORROSION ON L/W FLAP INBD FLAP TRACK FITTING EDGE DAMAGED. REMOVED OVER.100, OUT OF LIMITES IAW SRM 57-00-00 R & R FITTING IAW MM-57-55-25.
- [SDR HALA2016032800108](https://openairdocs.org/sdr/HALA2016032800108.md): Keelbeam · cracked · Mar 21, 2016 · N478HA · Boeing 717200 · Fuselage Main, Keel
  > KEELBEAM BARREL BS 696 OTBD END OF FORMER CRACKED. RT SIDE. R & R EXISTING REPAIR DAMAGE, REPAIR AT KEELBEAM BARREL BS 696 OTBD END OF FORMER RT SIDE IAW DW6 9923453 REV C AND T/C E 105-B10214-PERM.
- [SDR HALA2016020300025](https://openairdocs.org/sdr/HALA2016020300025.md): Fms · malfunctioned · Feb 3, 2016 · N478HA · Boeing 717200 · Central Computers
  > AIR TURNBACK. BOTH FMS LOCKED IN STANDBYE F-PLAN MODE. DOWN POWERED ACFT. ACCOMPLISHED VIA 1 & 2 RTS. NO FAULTS NOTED, AMM 31-43-00.
- [SDR HALA2015122400251](https://openairdocs.org/sdr/HALA2015122400251.md): Fairing · damaged · Dec 24, 2015 · N478HA · Boeing 717200 · Horizontal Stabilizer Structure
  > DURING DESCENT, THE PLANE MOMENTARILY OVERSPEED TO 341 KNOTS. PERFORMED OVER SPEED INSPECTION IAW AMM TASK 05-51-05-210-801. NO DAMAGE FOUND IN SKIN OR STRUCTURE. FOUND FAIRING BROKEN ON LT SIDE OF HORIZONTAL STABILIZER. REMOVED HORIZONTAL STABILIZER UPPER
- [SDR HALA2015111500236](https://openairdocs.org/sdr/HALA2015111500236.md): Girt Bar · unsecure · Nov 15, 2015 · N478HA · Boeing 717200 · Emergency Equipment
  > ESCAPE SLIDE GIRT BAR HANGING FROM CASING. REINSTALLED ESCAPE SLIDE GIRT BAR IAW AMM25-61-01. SECURITY CHECK GOOD, OK TO CONTINUE SERVICE.
- [SDR HALA2013040600035](https://openairdocs.org/sdr/HALA2013040600035.md): Tire · failed · Apr 6, 2013 · N478HA · Boeing 717200 · Tire
  > AIR TURN BACK, NR 1 TIRE FAILURE ON TAKE OFF. R & R NR 1 MLG WHEEL IAW AMM 32-41-01. SPIN CHECK OK. MLG TIRES 2,3,4 CONDITION AND SECURITY CHECKED OK.
- [SDR HALA2012072100181](https://openairdocs.org/sdr/HALA2012072100181.md): Tire · damaged · Jul 21, 2012 · N478HA · Boeing 717200 · Tire
  > LEFT MAIN OTBD TIRE DAMAGED. R & R LT MAIN OTBD TIRE IAW AMM 32-41-01.
- [SDR HALA2012011400029](https://openairdocs.org/sdr/HALA2012011400029.md): Slide · binding · Jan 14, 2012 · N478HA · Boeing 717200 · Escape Slide
  > SERVICE DOOR SLIDE UNSAFE, BINDING. R & R SERVICE DOOR SLIDE IAW AMM 25-61-03. SECURITY CHECKED GOOD.
- [SDR HALA2011070400304](https://openairdocs.org/sdr/HALA2011070400304.md): Indication Sys · malfunctioned · Jul 4, 2011 · N478HA · Boeing 717200 · Landing Gear Position and Warning
  > UPON GEAR RETRACTION OUT OF DEPARTURE, LT MAIN GEAR RED ( UNSAFE INDICATION) CAME BACK TO DEPARTURE. RETRACTION CHECK IAW MM 32-30-00, LT MAIN GEAR LIGHTS GOOD. SECURITY AND CONDITION OK. ADJUSTMENT AND TEST OF LT-MLG UP LATCH PROX SENSOR GOOD IAW AMM 32-61
- [SDR HALA2011052600230](https://openairdocs.org/sdr/HALA2011052600230.md): Proximity Sensor · malfunctioned · May 26, 2011 · N478HA · Boeing 717200 · Landing Gear Position and Warning
  > AFTER TAKEOFF WITH THE GEAR HANDLE UP, THE LT MAIN GEAR LIGHT WAS ILLUMINATED RED. WITH THE GEAR HANDLE DOWN, ALL 3 LIGHTS GREEN. TROUBLESHOT IAW SRM 32-61-0 IAW WDM 32-61-00. ADJUSTED DIMENSION "A" OF PROX SENSOR D1-1057 IAW AMM 32-61-00-820-804. DIMENSIO
- [SDR HALA2011052300222](https://openairdocs.org/sdr/HALA2011052300222.md): Eec · malfunctioned · May 23, 2011 · N478HA · Boeing 717200 · Fuel Controlling System
  > SELECT FADEC ALTN FOR LT ENG DISPLAYED, DID NOT RESET TO NORMAL MODE WHEN CHECKLIST ACCOMP. BITE EEC FAULT 732115/732116. R & R P2/T2 PROBE IAW MM 73-21-05. RTS FAILED. CK GENERATOR/ WIRING IAW WDM 73-23-00. NO DEFECTS NOTED. R & R EEC 1 IAW MM 73-21-01. O
- [SDR HALA2011052200214](https://openairdocs.org/sdr/HALA2011052200214.md): Proximity Sensor · malfunctioned · May 22, 2011 · N478HA · Boeing 717200 · Landing Gear Position and Warning
  > LT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. DISCONNECTED D1-1057, LT MLG UPLATCH PROX SENSOR & CLAMPS. REPLACED LT MLG UP & LATCHED PROXIMITY SENSOR ASSY AMM32-61-02. OPS CHECKED GOOD, OPS CHECKED MLG EXTENSION & RETRACTION IAW AMM32-30-00-
- [SDR HALA2010051100209](https://openairdocs.org/sdr/HALA2010051100209.md): Wire · damaged · May 11, 2010 · N478HA · Boeing 717200 · Engine Indicating System Wiring
  > ATB: DURING CLIMB ENG RT SYS FAIL ILLUMINATED. RETURNED HNL PER DISPATCH AND MOC. FOUND FAULT (772263) ACCOMPLISHED FIM 77-22 TASK 803. REPAIRED WIRING AT TURBINE BRG O/H SENSOR. ENG RUN-UP OPS CHECK GOOD.
- [SDR HALA2010042400188](https://openairdocs.org/sdr/HALA2010042400188.md): Thrust Reverser · malfunctioned · Apr 24, 2010 · N478HA · Boeing 717200 · Engine Thrust Reverser
  > AFTER LANDING, ACFT WENT INTO EMERGENCY REVERSE FOR APPROX 5 SECONDS. INSP NR1 & NR2 ENGINES IAW MM 71-00-05. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA2010033100143](https://openairdocs.org/sdr/HALA2010033100143.md): Smoke Detector · malfunctioned · Mar 31, 2010 · N478HA · Boeing 717200 · Smoke Detection
  > LAVATORY SMOKE WARNING WILL NOT EXTINGUISH AFTER TESTING. RESET LAV SMOKE DETECTOR. OPS CK GOOD.
- [SDR HALA2010031600118](https://openairdocs.org/sdr/HALA2010031600118.md): Pin · faulty · Mar 16, 2010 · N478HA · Boeing 717200 · Nose/Tail Landing Gear
  > RETURNED TO HNL, ATB, NOSE GEAR WOULD NOT RETRACT. NOSE GEAR PIN FAULTY. WHEN REMOVED AFTER TOW, PORTION REMAINED IN GEAR LOCK, CLEARED LOCK.
- [SDR HALA2010020800081](https://openairdocs.org/sdr/HALA2010020800081.md): Floor Support · corroded · Feb 8, 2010 · N478HA · Boeing 717200 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION ON FLOOR SUPPORT ANGLE, 3EA SPOTS, BY L-1 ENTRY DOOR BETWEEN STA 160-200. REMOVED CORROSION AT L-1 ENTRY DOOR BETWEEN STA 160-200, IAW SRM 51-10-40. CORROSION FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-00. REMOVED DAMAGE SECTION OF FLOOR SUPP
- [SDR HALA2010020800068](https://openairdocs.org/sdr/HALA2010020800068.md): Floorbeam · corroded · Feb 8, 2010 · N478HA · Boeing 717200 · Fuselage Main, Floor Beam
  > LEVEL 2 CORROSION ON FWD CABIN FLOOR SUPPORT ANGLE AT STATION 200, RBL 19 TO RBL 31. REMOVED CORROSION AT FWD CABIN FLOOR SUPPORT ANGLE AT STA 200, RBL 19 - RBL 31 PER REF 717 SRM 51-10-04, ORIGINAL MAT THICKNESS.070 INCH, MAT. REMOVED.018 INCH, REMAINING
- [SDR HALA2010020700069](https://openairdocs.org/sdr/HALA2010020700069.md): Stiffener · gouged · Feb 7, 2010 · N478HA · Boeing 717200 · Fuselage Miscellaneous Structure
  > STIFFENER GOUGED AT FWD ENG AT LT W/W HYD SYSTEM SERVICING STATION INTERIOR UPPER. REMOVED STIFFENER AT LT W/W HYD SYSTEM SERVING STATION INTERIOR UPPER SIDE PER REF SPM 51-40-02. FABRICATED NEW STIFFENER PER BOEING DRAWING 5910784. HEAT TREATED STIFFENER F
- [SDR HALA2009122000591](https://openairdocs.org/sdr/HALA2009122000591.md): Dcu · malfunctioned · Dec 20, 2009 · N478HA · Boeing 717200 · Central Warning
  > AFTER TAKEOFF CREW REPORTED MULTIPLE ALERT ILLUMINATED, RUDDER PITOT FAIL, AOA HEAT L/R FAIL, RAT PROBE FAIL. PERFROMED FIM TASK ON AOA HEAT (L) IAW TASK 30-30 TASK 808. AOA HEAT IAW TASK 30-30 TASK 809. RUD PITOT FAIL TASK 30-30 TASK 809. RAT PROBE FAIL
- [SDR HALA2009121600586](https://openairdocs.org/sdr/HALA2009121600586.md): Pseu · malfunctioned · Dec 16, 2009 · N478HA · Boeing 717200 · Engine Controls
  > WITH AC CONFIGURED FOR LANDING OUT OF 1000 FT FINAL APPROACH PSEU FAIL FLASHED ON AND OFF SEVERAL TIMES, A/S FAST REF +10, AUTO THROTTLES WENT INTO LO SPEED PROTECT MODE, AND WENT FWD AUTO. REMOVED AND REPLACED PROX SENSE ELEC UNIT IAW AMM 32-41-01. RTS TEST
- [SDR HALA2009101600471](https://openairdocs.org/sdr/HALA2009101600471.md): Duct · disconnected · Oct 16, 2009 · N478HA · Boeing 717200 · Air Distribution System
  > WHILE AT FL LEVEL 270, HEARD A BOOM FOLLOWED BY PACK R FLOW DISAGREE ALERT. JUST PRIOR TO LANDING, ALL ALERTS WENT AWAY. FOUND RT A/C PACK DUCT DISLODGED. RECONNECTED A/C DUCT OPS CK GOOD, OK FOR SERVICE.
- [SDR HALA2009052300186](https://openairdocs.org/sdr/HALA2009052300186.md): Via · failed · May 23, 2009 · N478HA · Boeing 717200 · Indicating/Recording System
  > ATB - AIR DATA 1 FAIL, GPWS FAIL, DCU FAIL, VIA FAIL, COLUMN DISC, FCC 1 FAIL, PROBLEM IS UNKNOWN. REPLACED NR 2 VIA GND OPS CHK OK AMM 31-43-01.
- [SDR HALA2009052200186](https://openairdocs.org/sdr/HALA2009052200186.md): Via · multiple fail · May 22, 2009 · N478HA · Boeing 717200 · Indicating/Recording System
  > ATB - AIR DATA 1 FAIL, GPWS FAIL, DCU FAIL, VIA FAIL, COLUMN DISC, FCC 1 FAIL, PROBLEM IS UNKNOWN. REPLACED NR 2 VIA GND OPS CHK OK AMM 31-43-01.
- [SDR HALA2009041000138](https://openairdocs.org/sdr/HALA2009041000138.md): Indicator · malfunctioned · Apr 10, 2009 · N478HA · Boeing 717200 · Central Computers
  > ATO - ON TAKEOFF LEVEL 3 STAB TRIM IN "RED" ABORT RTN TO RAMP. PERFORMED INSP OF ACFT AFTER HIGH ENERGY RTO STOP IAW AMM 05-53-01. NO DEFECTS NOTED. PERFORMED RTS ON FCC NR 2 PER AMM 22-00-00. ELEVATOR AND STAB TEST PASS. REMOVED AND REPLACED NR 1 VIA PER
- [SDR HALA2009032000095](https://openairdocs.org/sdr/HALA2009032000095.md): Warning Light · false activation · Mar 20, 2009 · N478HA · Boeing 717200 · Ice/Rain Protection System
  > WING ANTI-ICE MANIFOLD FAIL LIGHT ILLUMINATED AT FL220 THEN WENT AWAY AT 6,000. PERFORMED DODS RTS TEST OK. NO FAULTS NOTED. PERFORMED FIM 30-81-00-810-801. NO FAULTS NOTED. OK FOR SERVICE.
- [SDR HALA2009022500066](https://openairdocs.org/sdr/HALA2009022500066.md): Bearing · damaged · Feb 25, 2009 · N478HA · Boeing 717200 · Flight Control System
  > IN ORDER TO FLY STRAIGHT AND LEVEL THE AILERON TRIM AND RUDDER TRIM HAD TO BE ALIGNED GREATLY TO THE RIGHT. VISUAL CKS OF A/C FLT CONTROL, CONDITION SECURE CKS OK. NO DEFECTS NOTED. FOUND RT INBD MOVEABLE VANE TRACK SUPPORT BOTTOM BEARING DAMAGED. REMOVED

Next page: https://openairdocs.org/aircraft/N478HA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N478HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N478HA/reports

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