# Service difficulty reports: N908HA, cancelled Sep 20, 2016

A list on [N908HA, cancelled Sep 20, 2016](https://openairdocs.org/deregistered/N908HA-2016-09-20.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 · 87 reports

- [SDR HNAA2013112200583](https://openairdocs.org/sdr/HNAA2013112200583.md): Bulb · inoperative · Nov 21, 2013 · N908HA · Dhav DHC8102 · Emergency Lighting
  > MIDDLE O/H EMERGENCY LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.
- [SDR HNAA2013082800479](https://openairdocs.org/sdr/HNAA2013082800479.md): Bulb · failed · Aug 28, 2013 · N908HA · Dhav DHC8102 · Emergency Lighting
  > CEILING ESCAPE PATH EMERGENCY LIGHT IS INOPERATIVE AT ROW 5DF. R & R BULB IAW AMM 33-51-00. OPS CHECKED GOOD.
- [SDR HNAA2013073000434](https://openairdocs.org/sdr/HNAA2013073000434.md): Trim System · out of adjust · Jul 30, 2013 · N908HA · Dhav DHC8102 · Elevator Tab Control System
  > REJECTED TAKEOFF AT 20 KNOTS FOR WARNING HORN. ADJUSTED ELEVATOR TRIM, OPS NORMAL. PERFORMED WC 31-50-00Q, TAKEOFF WARNING SYS OPS CHECKED GOOD.
- [SDR HNAA2013071900412](https://openairdocs.org/sdr/HNAA2013071900412.md): Proximity Sensor · malfunctioned · Jul 19, 2013 · N908HA · Dhav DHC8102 · Landing Gear Position and Warning
  > AFTER MLG RETRACTION, LEFT AMBER DOOR LIGHT ILLUMINATED. CYCLED LANDING GEAR HANDLE AND AFTER GEAR RETRACTION, BOTH AMBER LIGHTS FLICKERED AND STAYED OUT. R & R AFT PROXIMITY SENSOR AND GAPED IAW MM 32-10-21. OPS CHECKED GOOD ON RT SIDE SURGE DAMPER WAS REPA
- [SDR HNAA2013062600369](https://openairdocs.org/sdr/HNAA2013062600369.md): Actuator · failed · Jun 26, 2013 · N908HA · Dhav DHC8102 · Drag Control Actuator
  > IN FLIGHT, LEFT TURNS ARE EXTREMELY DIFFICULT, FOUR TIMES MORE FORCE TO TURN LT THAN TO TURN RIGHT. R & R LT INBD SPOILER ACTUATOR. OPS CHECKED GOOD.
- [SDR HNAA2013062600366](https://openairdocs.org/sdr/HNAA2013062600366.md): Switch · failed · Jun 26, 2013 · N908HA · Dhav DHC8102 · Emergency Lighting
  > F/A EMERGENCY LIGHT SWITCH WILL NOT ILLUMINATE. R & R F/A EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD.
- [SDR HNAA2013030600113](https://openairdocs.org/sdr/HNAA2013030600113.md): Bulb · inoperative · Mar 6, 2013 · N908HA · Dhav DHC8102 · Emergency Lighting
  > FLOOR EMERGENCY LIGHT AT ROW 4 INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013030600112](https://openairdocs.org/sdr/HNAA2013030600112.md): Bulb · burned out · Mar 6, 2013 · N908HA · Dhav DHC8102 · Emergency Lighting
  > LEFT SIDE, AFT EMERGENCY LIGHT IS DIM. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013020400033](https://openairdocs.org/sdr/HNAA2013020400033.md): Bulb · failed · Feb 4, 2013 · N908HA · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHT, 4TH FROM FORWARD POSITION IS INOPERATIVE. R & R BULB FOR EMERGENCY PATH FLOOR LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2013010701148](https://openairdocs.org/sdr/HNAA2013010701148.md): Pseu · warning light · Jan 7, 2013 · N908HA · Dhav DHC8102 · Landing Gear Position and Warning
  > AFTER TAKEOFF, WITH GEAR UP, ALL UNSAFE LIGHTS FOR GEAR ARE ON. ALTERNATE INDICATION SHOWS THAT ALL ARE UP AND LOCKED. EXTENDED GEAR WITH ALTERNATE EXTENSION. JACKED ACFT. SWUNG GEAR SEVERAL TIMES. NO DEFECTS NOTED. R & R PSEU IAW MM 32-61-50. OPS CHECK
- [SDR HNAA2012120301083](https://openairdocs.org/sdr/HNAA2012120301083.md): Oil System · low · Dec 3, 2012 · N908HA · Dhav DHC8102 · Turbine Engine Oil System
  > AFTER DEICING, ON TAKEOFF, NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF AND SHUTDOWN NR 1 ENGINE. WARNING LIGHT WAS ILLUMINATED FOR APPR0X 5 SECONDS. INSPECTED NR 1 ENGINE AND FOUND ENGINE 3 QUARTS LOW. SERVICED ENGINE WITH 3 QUARTS O
- [SDR HNAA2012112701073](https://openairdocs.org/sdr/HNAA2012112701073.md): Warning Light · false activation · Nov 27, 2012 · N908HA · Dhav DHC8102 · Engine Temperature Indicating System
  > NR 1 ITT INCREASED AND DECREASED ON CLIMBOUT. BOTH ANAOLOG AND DIGITAL. ALL OTHER PARAMETERS NORMAL. INSPECTED ENGINE WIRING FOR CONDITION AND SECURITY. CHECKED TRIM RESISTOR, READ WIRING FROM ENGINE TO GAUGE. CHECKED READING AT BOTH TERMINAL BLOCKS ON ENGI
- [SDR HNAA2012112601068](https://openairdocs.org/sdr/HNAA2012112601068.md): Lens · dirty · Nov 26, 2012 · N908HA · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY EXIT BETA LIGHT IS DIM. R & R BETA LIGHTS ON AFT EMERGENCY DOORS. CLEANED LENS COVER AND REINSTALLED. OPS CHECKED GOOD.
- [SDR HNAA2012103101024](https://openairdocs.org/sdr/HNAA2012103101024.md): Bulb · failed · Oct 31, 2012 · N908HA · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 2DF. R & R BULB AT ROW 2DF EMERGENCY FLOOR PATH LIGHTING.
- [SDR HNAA2012062200834](https://openairdocs.org/sdr/HNAA2012062200834.md): Aileron · out of adjust · Jun 22, 2012 · N908HA · Dhav DHC8102 · Aileron Control System
  > CONTROL COLUMN IS 10-15 DEGREES RT OF CENTER ON TAKEOFF. LARGE CONTROL INPUTS REQUIRED AT 150 TO MAINTAIN LEVEL FLIGHT. ADJUSTED LT AILERON IAW MM 27-13-00. ACFT RELEASED FOR EVALUATION FLIGHT.
- [SDR HNAA2012020800567](https://openairdocs.org/sdr/HNAA2012020800567.md): Recorder · failed · Feb 8, 2012 · N908HA · Dhav DHC8102 · Data Recorders (Flight/Maintenance)
  > FDR CAUTION LIGHT ILLUMINATED. R & R FDR IAW 31-33-02. OPS CHECKED GOOD.
- [SDR HNAA2012011600481](https://openairdocs.org/sdr/HNAA2012011600481.md): Stringer · corroded · Jan 16, 2012 · N908HA · Dhav DHC8102 · Nacelle/Pylon, Longeron/Stringer
  > STRINGER 31 RT AT STA X336 IS CORRODED. BLENDED MINOR SURFACE CORROSION IAW SRM 51-20-11. ALODINED AND PRIMED AREA IAW AMM 51-25-03.
- [SDR HNAA2012011600480](https://openairdocs.org/sdr/HNAA2012011600480.md): Structure · corroded · Jan 16, 2012 · N908HA · Dhav DHC8102 · Fuselage Main, Structure
  > CORROSION FOUND AT S31, STA 207. BLENDED MINOR SURFACE CORROSION IAW SRM 51-20-11. ALODINED AND PRIMED AREA IAW AMM 51-25-03.
- [SDR HNAA2012011600479](https://openairdocs.org/sdr/HNAA2012011600479.md): Channel · corroded · Jan 16, 2012 · N908HA · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD CHANNEL IS CORRODED. CLEANED MINOR CORROSION OFF CHANNEL, ALODINED AND PRIMED.
- [SDR HNAA2012011600478](https://openairdocs.org/sdr/HNAA2012011600478.md): Threshold · corroded · Jan 16, 2012 · N908HA · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD IS CORRODED. R & R PAX DOOR THRESHOLD IAW ENG DWG 8531241.
- [SDR HNAA2012011300475](https://openairdocs.org/sdr/HNAA2012011300475.md): Battery Pack · inoperative · Jan 13, 2012 · N908HA · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY LIGHTS ABOVE RT FWD EMERGENCY EXIT, GALLEY AND RT FWD FUSELAGE IS NOT WORKING. R & R LOWER EMERGENCY LIGHT BATTERY PACK.
- [SDR HNAA2012011100471](https://openairdocs.org/sdr/HNAA2012011100471.md): Bolt · corroded · Jan 11, 2012 · N908HA · Dhav DHC8102 · Elevator, Tab Structure
  > LT TRIM TAB CONTROL ROD ATTACH HARDWARE HAS SURFACE CORROSION. R & R TRIM TAB CONTROL ATTACH HARDWARE IAW AMM 27-36-21.
- [SDR HNAA2012010600456](https://openairdocs.org/sdr/HNAA2012010600456.md): Light · broken · Jan 6, 2012 · N908HA · Dhav DHC8102 · Emergency Lighting
  > CENTER FLOOR PANEL NR 6 EMERGENCY LIGHT STRIP BROKEN. R & R EMERGENCY LIGHT STRIP ON PANEL.
- [SDR HNAA2011111700386](https://openairdocs.org/sdr/HNAA2011111700386.md): Lens · misinstalled · Nov 17, 2011 · N908HA · Dhav DHC8102 · Emergency Lighting
  > EXIT LIGHT LENS COVER ABOVE RT FORWARD EMERGENCY EXIT NOT PROPERLY INSTALLED, CANNOT REMOVE EXIT FROM OPENING. REMOVED EXIT LENS COVER AND REINSTALLED DOOR CORRECTLY. OPERATES NORMALLY.
- [SDR HNAA2011071400204](https://openairdocs.org/sdr/HNAA2011071400204.md): Pressure Switch · malfunctioned · Jun 30, 2011 · N908HA · Dhav DHC8102 · Drag Control System
  > UPON ADVANCING POWER LEVERS FOR TAKEOFF, THE ROLL SPOILERS OTBD HYD CAUTION LIGHT ILLUMINATED AND THE ROLL OTBD ADVISORY LIGHT STAYED ON. R & R ROLL SPOILER PSI SWITCH, GROUND RAN NR 2 ENGINE, OPS AND LEAKED CHECKED GOOD.
- [SDR HNAA2011061300167](https://openairdocs.org/sdr/HNAA2011061300167.md): Electronic Unit · failed · Jun 7, 2011 · N908HA · Dhav DHC8102 · Communications System
  > CAN NOT TRANSMITT EITHER RADIO FROM NR1 ACP. R & R REU. OPS CHECKED GOOD. OK FOR SERVICE IAW -8 MM 23-50-00.
- [SDR HNAA2011042400079](https://openairdocs.org/sdr/HNAA2011042400079.md): Spoiler Sys · malfunctioned · Apr 13, 2011 · N908HA · Dhav DHC8102 · Drag Control System
  > ABORTED TAKEOFF DUE TO RT INBD AND OTBD SPOILERS NOT RETRACTING AFTER POWER LEVERS ADVANCED. AFTER CYCLING FLIGHT TAXI SWITCH AND ALL SPOILERS RETRACTED AFTER ADVANCING POWER LEVERS. INSPECTED RT SPOILERS, NO DEFECTS NOTED, GROUND RAN ACFT, CYCLED SPOILERS S
- [SDR HNAA2011032000053](https://openairdocs.org/sdr/HNAA2011032000053.md): Bulb · burned out · Mar 10, 2011 · N908HA · Dhav DHC8102 · Emergency Lighting
  > ROW 6 EMERGENCY FLOOR PATH LIGHT IS INOP. R & R LIGHT BULB AT ROW 6, OPS CHECKED GOOD.
- [SDR HNAA2011030900040](https://openairdocs.org/sdr/HNAA2011030900040.md): Inverter · failed · Feb 21, 2011 · N908HA · Dhav DHC8102 · AC Inverter
  > 26AC AND SECONDARY INVERTER CAUTION LIGHTS ILLUMINATED IN FLIGHT. SECONDARY INVERTER AND 115AC CIRCUIT BREAKER POPPED. LOST INSTRUMENT POWER RT SIDE INVERTERS WITH SECONDARY CIRCUIT BREAKER OUT 115 AC BUSS CIRCUIT BREAKER RESETS. R & R SECONDARY INVERTER IA
- [SDR HNAA2011021500021](https://openairdocs.org/sdr/HNAA2011021500021.md): Switch · failed · Feb 2, 2011 · N908HA · Dhav DHC8102 · Airfoil Anti/De-ice System
  > LT ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT. REMOVED SWITCH 3015-S4 AND RETERMINATED WIRING 33A16-1 AND 9C16A-1 REF, WIRING DIAGRAM 30-25-02. OPS CHECKED GOOD IAW WORKCARD 30-10-10F.
- [SDR HNAA2011021500008](https://openairdocs.org/sdr/HNAA2011021500008.md): Lamp · burned out · Jan 26, 2011 · N908HA · Dhav DHC8102 · Emergency Lighting
  > ROW 2 CEILING EMERGENCY LIGHT INOP. RELAMP ROW 2 CEILING EMERGENCY LIGHT, OPS CHECKED GOOD.
- [SDR HNAA2010091600216](https://openairdocs.org/sdr/HNAA2010091600216.md): Oil Cooler · malfunctioned · Sep 16, 2010 · N908HA · Dhav DHC8102 · Engine Oil Cooler
  > ON CLIMBOUT, NR1 ENGINE OIL TEMP CLIMBED TO 125 DEGREES C. CYCLED ENGINE INTAKE DOOR TO SEE IF TEMP WOULD DECREASE. TEMP STAYED THE SAME. THEN REDUCED TORQUE TO 50 PERCENT. TEMP WENT TO 120 DEGREES C AFTER 18 MINUTES. REDUCED TORQUE TO 37.5 PERCENT. THEN
- [SDR HNAA2010071300176](https://openairdocs.org/sdr/HNAA2010071300176.md): Control Handle · malfunctioned · Jul 5, 2010 · N908HA · Dhav DHC8102 · Landing Gear Selector
  > AT ROTATION, AN ABNORNAL THUMP SOUND WAS HEARD FROM NOSE GEAR. RED NOSE GEAR UNSAFE LIGHT STAYED ON AND LT AND RT MAIN DOOR AMBER LIGHTS STAYED ON. AFTER APPR0X 4 MINUTES, GEAR RETRACTED AND LIGHTS EXTINGUISHED. PERFORMED ALTERNATE EXTENSION AT DESTINATION.
- [SDR HNAA2009090300273](https://openairdocs.org/sdr/HNAA2009090300273.md): Frame Splice · cracked · Jun 23, 2009 · N908HA · Dhav DHC8102 · Fuselage Main, Frame
  > SPLICE IS CRACKED ON LT SIDE OF FLIGHT COMPARTMENT FRAME JOINT AT STA X136.8 AND STR. 15P. ON LT SIDE OF FLIGHT COMPARTMENT FRAME JOINT AT STA. 136.8 AND STR 15P SPLICE REMOVED AND REPLACED IAW SRM 51-40-00 PD 1777.
- [SDR HNAA2009090300278](https://openairdocs.org/sdr/HNAA2009090300278.md): Housing · corroded · Jun 22, 2009 · N908HA · Dhav DHC8102 · Fuel Boost Pump
  > LEFT AUX BOOST PUMP RECEIVER FOUND CORRODED ON THREAD. LT AUX BOOST PUMP ASSY REMOVED AND REINSTALLED. TRANSFERED ON TASK CARD 005-55-13I. REMOVED AND REINSTALLED PLUG-IN ELEMENT IAW 28-21-16. NEW AUX PUMP RECEIVER INSTALLED IAW 28-21-16. OPS AND LEAK CHECKE
- [SDR HNAA2009090300276](https://openairdocs.org/sdr/HNAA2009090300276.md): Angle · corroded · Jun 22, 2009 · N908HA · Dhav DHC8102 · Passenger/Crew Doors
  > CORROSION FOUND ON PAX DOOR SHELL ANGLE AT BOTTOM AFT CORNER. PAX DOOR SHELL ANGLE REPLACED IAW MM 52-10-00 WITH SERVICABLE PART ON CARD SEC 2518.
- [SDR HNAA2009090300275](https://openairdocs.org/sdr/HNAA2009090300275.md): Fitting · corroded · Jun 22, 2009 · N908HA · Dhav DHC8102 · Fuselage Main, Attach Fittings
  > CABIN INTERNAL LAVATORY FITTING CORRODED. CABIN INTERNAL LAVATORY FITTING REPLACED AND NEW PART INSTALLED IAW SRM 51-40-00, DWA 85320983 AND RD8-511-102
- [SDR HNAA2009090300274](https://openairdocs.org/sdr/HNAA2009090300274.md): Bracket · corroded · Jun 22, 2009 · N908HA · Dhav DHC8102 · Passenger/Crew Doors
  > CORROSION FOUND ON PAX DOOR STEP BRACKETS (UNDERNEATH STAIRS, BOTH CTR BRACKETS AND FWD BOTTOM BRACKETS). PAX DOOR STEP BRACKET (BOTH CTR AND FWD BOTTOM) REPLACED IAW MM 20-14-01.
- [SDR HNAA2009090300272](https://openairdocs.org/sdr/HNAA2009090300272.md): Intercostal · corroded · Jun 22, 2009 · N908HA · Dhav DHC8102 · Horizontal Stabilizer Structure
  > CABIN UNDER FLOOR STA X396 RUDDER BELLCRANK INTERCOSTAL CORRODED. RUDDER CABLE TENSION RELEASED 07-06-09. UPPER CHANNEL OF CONTROL RUDDER SYS CTR BELLCRACK REPLACED WITH NEW PART LOCALLY FABRICATED, (FABRICATION COVERED ON WC SEQ 20-70) INSTALLED WITH SOL
- [SDR HNAA2009082900266](https://openairdocs.org/sdr/HNAA2009082900266.md): Skin · corroded · Jun 22, 2009 · N908HA · Dhav DHC8102 · Wing, Plate/Skin
  > CATEGORY 1 CORROSION FOUND UNDER THE LT WING AUX BOOST PUMP EXTERNAL ANTI FRET RING ON THE LWR WING SKIN. LT AUX BOOST PUMP EXTERNAL AND INTERNAL SURFACE OF DOUBLER REPAIRED IAW RD8-57-4320 AND RD8-57-1907.
- [SDR HNAA2009082700263](https://openairdocs.org/sdr/HNAA2009082700263.md): Skin · dented · Jun 22, 2009 · N908HA · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK THE FOLLOWING DENTS FOUND ON RT FUSELAGE SKIN BETWEEN STA X136.8 AND 151.6 BETWEEN STR 23S-24S. BOTH DENTS FOUND TO BE IN LIMITS IAW EA 01-09233 AND EO 8-53-09-304.
- [SDR HNAA2009082700259](https://openairdocs.org/sdr/HNAA2009082700259.md): Structure · dented · Jun 22, 2009 · N908HA · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK A DENT WAS REPORTED AT 2 INCHES AFT OF THE PRESSURE BULKHEAD, HAS AN INSPECTION INTERVAL ESTABLISHED BY AN EO SIGNED BY A PERSON NOT AUTHORIZED AS A DT ENGINEER TO DETERMINE AN INSPECTION INTERVAL. THE DENT MAY NOT BE LOCATED IN THIS AREA S
- [SDR HNAA2009090300277](https://openairdocs.org/sdr/HNAA2009090300277.md): Panel · corroded · Jun 21, 2009 · N908HA · Dhav DHC8102 · Wing Miscellaneous Structure
  > RIGHT WING STRESS PANEL 623AT CORRODED. RT WING STRESS PANEL 623AT REPLACED IAW AMM 57-20-05 PG 2425. RT WING STRESS PANEL 623AT INSTALLATION COVERED BY CARD 57-25-02R.
- [SDR HNAA2009090300270](https://openairdocs.org/sdr/HNAA2009090300270.md): Angle · corroded · Jun 20, 2009 · N908HA · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > BAGGAGE COMPARTMENT FLOOR LEVEL AT STA 597, STEP ANGLE FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-40-00 AT FLOOR LEVEL STA X 597 STEP ANGLE.
- [SDR HNAA2009012000005](https://openairdocs.org/sdr/HNAA2009012000005.md): Apu · smoke · Jan 15, 2009 · N908HA · Dhav DHC8102 · APU Core Engine
  > WITH AUXILIARY POWER UNIT RUNNING AND BLEEDS ON, SMOKE IN CABIN AND LAVATORY SMOKE DETECTOR SOUNDS. RAN AUXILIARY POWER UNIT WITH BLEED ON, VISIBLE HAZE APPEARS. INSP AUXILIARY POWER UNIT AREA NO DEFECTS NOTED. RAN ENGINES WITH BLEEDS NO HAZE NOTED. R&R AUXI
- [SDR HNAA2009011200395](https://openairdocs.org/sdr/HNAA2009011200395.md): Ahrs · failed · Jan 8, 2009 · N908HA · Dhav DHC8102 · Integrated Flight System
  > NR 2 ATTITUDE HEADING AND REFERENCE SYSTEM. R&R NR 2 ATTITUDE HEADING AND REFERENCE SYSTEM COMPUTER. OPS CHECK GOOD IAW MM 34-20-01.
- [SDR HNAA2008121000347](https://openairdocs.org/sdr/HNAA2008121000347.md): Light · inoperative · Dec 13, 2008 · N908HA · Dhav DHC8102 · Emergency Lighting
  > THE 2ND CEILING EMERGENCY LIGHT INOP. RELAMP 2ND CEILING EMERGENCY LIGHT BULB.
- [SDR HNAA2008120800341](https://openairdocs.org/sdr/HNAA2008120800341.md): Hydraulic System · contaminated · Dec 8, 2008 · N908HA · Dhav DHC8102 · Hydraulic System, Main
  > JUST AFTER TAKEOFF, THE 'RUDDER PRESSURE' AND 'RUDDER FULL PRESSURE' CAUTION LIGHTS ILLUMINATED. THE CREW ELECTED TO RETURN TO THE ORIGINATING AIRFIELD. AFTER THE LANDING GEAR AND FLAPS WERE EXTENDED, THE CAUTION LIGHTS EXTINGUISHED. BOTH HYDRAULIC SYSTEMS
- [SDR HNAA2008120600339](https://openairdocs.org/sdr/HNAA2008120600339.md): Smoke Detector · malfunctioned · Dec 6, 2008 · N908HA · Dhav DHC8102 · Smoke Detection
  > DURING OPERATIONS, THE LAVATORY SMOKE DETECTOR BEGAN SOUNDING CONTINUOUSLY. THE TEST SWITCH WAS CYCLED AND THE UNIT OPERATED NORMALLY. THE AIRCRAFT WAS NOT TAKEN OUT OF SERVICE.
- [SDR HNAA2008112100337](https://openairdocs.org/sdr/HNAA2008112100337.md): Smoke Detector · defective · Nov 21, 2008 · N908HA · Dhav DHC8102 · Smoke Detection
  > THE LAVATORY SMOKE DETECTOR SOUNDED OFF ABOUT 10 TIMES WITHOUT EVIDENCE OF SMOKE OR FUMES. THE SMOKE DETECTOR WAS DE-ACTIVATED IAW SPECIAL PROCEDURES. MAINTENANCE REPLACED THE DEFECTIVE UNIT, RE-ACTIVATED THE SYSTEM AND OPS CHECKED THE UNIT. OPS CHECKS WERE

Next page: https://openairdocs.org/deregistered/N908HA-2016-09-20/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 = 'N908HA' AND deregistration_id = 'N908HA-2016-09-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N908HA-2016-09-20/reports

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