# Service difficulty reports: Boeing DHC-8-102

A list on [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 186 · 9,272 reports

- [SDR CA190802005](https://openairdocs.org/sdr/CA190802005.md): Bearing · seized · Jul 30, 2019 · Dhav DHC8102 · Aileron Control System
  > (CAN) FLIGHT CREW REPORTED AILERON CONTROL HAD AN ODD FEELING IN FLIGHT, SOMEWHAT STIFF AND HEAVY. UPON AN UNEVENTFUL LANDING, MAINTENANCE PERSONNEL CARRIED OUT A FULL OPERATIONAL CHECK OF THE ROLL CONTROL SYSTEM I.A.W DH8 AMM 27-10-00-06 WHICH INCLUDED CHECKI
- [SDR CA190821005](https://openairdocs.org/sdr/CA190821005.md): Unknown · smoke · Jul 25, 2019 · Dhav DHC8102 · Air Distribution System
  > (CAN) WHILE TAXIING THE CREW HEARD A CLUNKING SOUND AND THEN OBSERVED SMOKE IN THE FLIGHT DECK AND CABIN AREAS. THE AIRCRAFT RETURNED TO THE GATE.. (TC# 20190821005)
- [SDR CA190726022](https://openairdocs.org/sdr/CA190726022.md): Acm · seized · Jul 25, 2019 · Dhav DHC8102 · Cabin Compressor System
  > (CAN) THE CREW MADE A GATE RETURN AS CABIN TEMP COULD NOT BE CONTROLLED IN MANUAL OR AUTO MODE. AFTER A SYSTEM RESET AND ENGINE START THEY BEGAN TO LEAVE THE APRON WHEN THEY HEARD A CLUNKING SOUND FOLLOWED BY VISIBLE SMOKE IN THE FLIGHT DECK AND CABIN. THEY RE
- [SDR CA190729013](https://openairdocs.org/sdr/CA190729013.md): Pressure Switch · failed · Jul 17, 2019 · Dhav DHC8102 · Bleed Air Indicating System
  > (CAN) #2 BLEED HOT ILLUMINATED DURING CRUISE. SYSTEM GOT TURNED OFF, AFTER THAT #1 SYSTEM FAILED. EMERGENCY DECENT WAS EXECUTED, PLANE DIVERTED TO YQT FOR MAINTENANCE. (TC# 20190729013)
- [SDR CA190711001](https://openairdocs.org/sdr/CA190711001.md): Valve · damaged · Jul 8, 2019 · Dhav DHC8102 · Engine Oil Cooler
  > (CAN) DURING CRUISE FLIGHT, #2 ENGINE WAS SHUTDOWN DUE TO HIGH ENGINE OIL TEMPS. THE OIL COOLER THERMO VALVE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC# 20190711001)
- [SDR CA190730010](https://openairdocs.org/sdr/CA190730010.md): Oil System · overtemp · Jul 8, 2019 · Dhav DHC8102 · Turbine Engine Oil System
  > (CAN) DURING THE FLIGHT, THE FLIGHT CREW NOTICED A HIGH OIL TEMPERATURE ON THE NUMBER 2 ENGINE. AS THE TEMPERATURE CONTINUED TO INCREASE, THE FLIGHT CREW ELECTED TO RETURN TO THE AIRPORT OF ORIGIN. SINCE THE HIGH OIL TEMPERATURE WAS TIME LIMITED, THE FLIGHT CR
- [SDR CA190625001](https://openairdocs.org/sdr/CA190625001.md): Lever · binding · Jun 22, 2019 · Dhav DHC8102 · Aileron Control System
  > (CAN) WHILE CARRYING AILERON ROLL DISCONNECT, FOUND CLUNKING NOISE COMING FROM UNDERFLOOR QUADRANT. FOUND COPILOT AILERON PULLEY QUADRANT BEARING CAUSING THE NOISE. AILERON PULLEY QUADRANT LEVER AND BEARINGS REPLACED REFERENCE AMM 27-12-41. AILERON SYSTEM RIGG
- [SDR CA190704001](https://openairdocs.org/sdr/CA190704001.md): Engine · surges · Jun 20, 2019 · Dhav DHC8102 · Engine (Turbine/Turboprop)
  > (CAN) PILOT REPORTED THAT #2 ENGINE STARTED SURGING IMMEDIATELY AFTER THE AIRCRAFT WAS AIRBORNE AND WITH THE GEAR SELECTED UP. PILOT INITIALLY HEARD THE CYCLING CHANGE IN ENGINE SOUND, AND FELT THE YAW. #2 ENGINE TORQUE WAS OBSERVED TO BE FLUCTUATING BETWEEN 8
- [SDR CA190604014](https://openairdocs.org/sdr/CA190604014.md): Eec · malfunctioned · Jun 2, 2019 · Dhav DHC8102 · Fuel Controlling System
  > (CAN) AFTER DEPARTURE #2 ENGINE TORQUE ROLLED BACK 16 % TWO SEPARATE TIMES WITH NO ECU LIGHT. TORQUE INDICATION RETURNED TO NORMAL AFTER A FEW SECONDS. MOMENTARY DROP IN R/H PROP RPM ALSO OBSERVED. AIRCRAFT CONTINUED TO DESTINATION WITH NO FURTHER ISSUES. PER
- [SDR CA190531011](https://openairdocs.org/sdr/CA190531011.md): Hmu · failed · May 30, 2019 · Dhav DHC8102 · Fuel Controlling System
  > (CAN) DURING CRUISE THE CREW REPORTED A #2 PROP OVER SPEED INDICATION AND SHUT DOWN THE ENGINE. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO BASE, LANDING WITHOUT INCIDENT. MAINTENANCE CONDUCTED WIRING CHECKS BETWEEN THE HMU AND ECU AND HAVE CHANGED THE HMU
- [SDR CA190523003](https://openairdocs.org/sdr/CA190523003.md): Control Box · shorted · May 21, 2019 · Dhav DHC8102 · AC Inverter
  > (CAN) MULTIPLE INVERTER FAILURE `PRI INV`, `SEC INV`, `AUX INV`, `LVAC26` AND `R26VAC` CAUTION LIGHTS ILLUMINATED. LOST ALL FLIGHT INSTRUMENTS ON CAPT, F/O SIDE OF AIRCRAFT. QRH PG 9.11 ACTIONED AND 115V BUS TIE CB PULLED. STRONG ELECTRICAL SMELL IN FLIGHT DEC
- [SDR CA190521032](https://openairdocs.org/sdr/CA190521032.md): Fitting · leaking · May 18, 2019 · Dhav DHC8102 · Turbine Engine Oil System
  > (CAN) DURING POST FLIGHT INSPECTION, OIL WAS NOTED LEAKING FROM #1 ENGINE. MAINTENANCE FOUND THAT A FITTING WAS LOOSE ON THE ACCESSORY OIL PUMP DRIVE COVER. THE THREADS HAD PULLED OUT FROM THE COVER ALLOWING OIL TO LEAK OUT. (TC# 20190521032)
- [SDR CA190517008](https://openairdocs.org/sdr/CA190517008.md): Relay · malfunctioned · May 16, 2019 · Dhav DHC8102 · Starter-Generator
  > (CAN) AFTER BOTH ENGINES WERE STARTED AT THE GATE FOR DEPARTURE, SMOKE WAS OBSERVED COMING FROM THE RHS ENGINE BY RAMP CREW. CAPTAIN WAS ADVISED TO SHUT DOWN ENGINE BY THE RAMP CREW. CAPTAIN SHUT THE ENGINES DOWN AND INSTRUCTED FLIGHT ATTENDANT TO CONDUCT A RA
- [SDR CA190703018](https://openairdocs.org/sdr/CA190703018.md): Fuel Heater · malfunctioned · May 15, 2019 · Dhav DHC8102 · Fuel Heater
  > (CAN) DURING INSTALL OF FUEL HEATER ON #1 ENGINE IT WAS DISCOVERED THAT THERE WAS WHAT APPEARED TO BE MEDIA BLAST (GLASS BEAD) IN THE FILTER BOWL. THE UNIT WAS FLUSHED AND A NEW FILTER WAS INSTALLED. 2 ADDITIONAL UNITS FROM THE SAME VENDOR WERE REMOVED FROM ST
- [SDR CA190516006](https://openairdocs.org/sdr/CA190516006.md): Gcu · failed · May 15, 2019 · Dhav DHC8102 · DC Generating System
  > (CAN) ON DESCENT THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. BOTH DC GENERATORS TRIPPED BUT WERE ABLE TO RESET. THIS WAS FOLLOWED BY A LOSS OF THE DC BUS AND THE FO`S INSTRUMENTS. AFTER SHUTTING OFF THE MAIN BATTERY AND #2 DC GEN AS PER THE QRH THEY REGAINED AL
- [SDR CA190425024](https://openairdocs.org/sdr/CA190425024.md): Torque Tube · chafed · Apr 22, 2019 · Dhav DHC8102 · Trailing Edge Flap Control System
  > (CAN) WHILE PERFORMING UNRELATED MAINTENANCE, AN AME OBSERVED THAT A FLAP DRIVE TORQUE TUBE LOCATED ON THE LEFT WING, INBOARD OF THE OUTER FLAP ACTUATOR HAD SEVERE CHAFING DAMAGE DUE TO INTERFERENCE WITH A CLAMP SUPPORTING WIRES FOR THE ROLL SPOILER CLUTCH SWI
- [SDR CA190422003](https://openairdocs.org/sdr/CA190422003.md): Switch · failed · Apr 20, 2019 · Dhav DHC8102 · Power Lever
  > (CAN) NR 1 ENGINE ECU MANUAL CAUTION ILLUMINATED AT 50FT AGL, TORQUE SPLIT IN CRUISE NOT WITHIN MEL CRITERIA, SOC ELECTED TO RETURN AC TO DEPARTURE AIRPORT. MAINTENANCE REPLACED 6121-S11 MICRO-SWITCH, C/O TEST IAW AMM 76-10-16. BETA BACKUP SWITCH 1&2 BACK TO
- [SDR CA190424005](https://openairdocs.org/sdr/CA190424005.md): Switch · malfunctioned · Apr 19, 2019 · Dhav DHC8102 · Cabin Cooling System
  > (CAN) CREW RECEIVED PACK HOT CAUTION MESSAGE, FOLLOWED QRH AND DESCENDED TO 14,000 FEET. DECLARED AN EMERGENCY WITH ATC AND LANDED WITHOUT INCIDENT. NO PASSENGERS ONBOARD AS THIS WAS A POSITIONING FLIGHT AFTER OPERATING A CHARTER. MAINTENANCE RECTIFICATION: PA
- [SDR CA190410016](https://openairdocs.org/sdr/CA190410016.md): Wire · chafed · Apr 9, 2019 · Dhav DHC8102 · Electrical Power System Wiring
  > (CAN) AFTER GROUND CREW HAD CONNECTED AC POWER THE RH AC CONTACTOR BOX AREA BEGAN TO EMIT SMOKE AND VISIBLE ARCHING. MAINTENANCE DISCOVERED THAT A 20GAUGE AC WIRE CONNECTED TO A CURRENT LIMITER HAD CONTACTED THE CURRENT LIMITER HOUSING AND CHAFFED THROUGH CAUS
- [SDR CA190409009](https://openairdocs.org/sdr/CA190409009.md): Bearing Race · fractured · Apr 8, 2019 · Dhav DHC8102 · Propeller Hub Section
  > (CAN) WHILE TROUBLESHOOTING A LH PROP LEAK MAINTENANCE DISCOVERED THE INNER BEARING RACE FOR THE #2 BLADE TO HAVE BROKEN AND FAILED. LH PROP HUB AND BLADES HAVE BEEN REPLACED, AND THE A/C RETURNED TO SERVICE. P/N: 782303-1 S/N: NSN A/C HOURS: 67769 A/C CYCLES
- [SDR CA190402006](https://openairdocs.org/sdr/CA190402006.md): Control Panel · odor · Mar 31, 2019 · Dhav DHC8102 · Audio Integrating System
  > (CAN) ON INITIAL CLIMB OUT FLIGHT CREW REPORTED LIGHT ELECTRICAL BURN SMELL. MAINTENANCE IDENTIFIED THAT THE SMELL WAS COMING FROM #1 AUDIO CONTROL PANEL. PANEL REPLACED AND TESTED. AIRCRAFT RETURNED TO SERVICE. PN 5061-1-1, SN 560, AC HOURS: 67723 AC CYCLES:
- [SDR CA190326008](https://openairdocs.org/sdr/CA190326008.md): Impeller · damaged · Mar 24, 2019 · Dhav DHC8102 · Turbine Engine Compressor Section
  > (CAN) DURING MAINTENANCE THE #2 ENGINE WAS DISCOVERED TO HAVE IMPELLER DAMAGE. AFTER A BOROSCOPE WAS CARRIED OUT FURTHER DAMAGE WAS FOUND ON THE DIFFUSER CHANNELS AND ENGINE CASING. AFTER CONSULTING WITH THE ENGINE MANUFACTURER, IT WAS DETERMINED THAT THE DAMA
- [SDR CA190325017](https://openairdocs.org/sdr/CA190325017.md): Transducer · failed · Mar 24, 2019 · Dhav DHC8102 · Stall Warning System
  > (CAN) IMMEDIATELY AFTER TAKEOFF THE STICK SHAKER ACTIVATED. IT REMAINED ON UNTIL THE CREW RETURNED TO BASE. THE AIRCRAFT LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOOTING FOUND THE L/H STALL WARNING TRANSDUCER AT FAULT. THE TRA
- [SDR CA190301005](https://openairdocs.org/sdr/CA190301005.md): Case · cracked · Feb 28, 2019 · Dhav DHC8102 · Turbine Engine Combustion Section
  > (CAN) ENGINE WAS REMOVED DUE TO HIGHER THAN NORMAL ITT. AN APPROXIMATELY 4 INCH CRACK WAS FOUND ADJACENT TO THE NO. 1 FUEL NOZZLE IN THE GAS GENERATOR CASE.
- [SDR CA190227007](https://openairdocs.org/sdr/CA190227007.md): Tube · chafed · Feb 25, 2019 · Dhav DHC8102 · Hydraulic System, Main
  > (CAN) AIRCRAFT DEPARTED AND LOST ALL HYDRAULIC FLUID FROM #1 HYDRAULIC SYSTEM AFTER 45 MINUTES IN CRUISE. THEY CAME BACK TO LAND AND DECLARED EMERGENCY. THEY HAD TO LAND FLAP LESS WITHOUT NORMAL BRAKES. INVESTIGATION REVEALED THAT #1 EDP PRESSURE LINE ABOVE EX
- [SDR CA190226007](https://openairdocs.org/sdr/CA190226007.md): Bearing Race · fractured · Feb 23, 2019 · Dhav DHC8102 · Propeller Blade Section
  > (CAN) DURING REMOVAL OF LH2 BLADE FOR RESTORATION A TECHNICIAN FOUND ONE OF THE TWO PIECE INNER BEARING RACES FRACTURED. THE PROP HUB AND BLADE SHOWED SIGNS OF PITTING AND OTHER DAMAGE CAUSED BY THE FAILURE. THE DAMAGED ITEMS HAVE BEEN REPLACED AND THE AIRCRAF
- [SDR CA190409007](https://openairdocs.org/sdr/CA190409007.md): Smoke Detector · failed · Jan 18, 2019 · Dhav DHC8102 · Smoke Detection
  > (CAN) INTERNAL FAILURE OF PART (SMOKE DETECTOR TYPE II) CAUSING `SMOKE WARNING` ANNUNICATOR TO ILLUMINATE (TC# 20190409007)
- [SDR CA180706015](https://openairdocs.org/sdr/CA180706015.md): Control Unit · no test · Jul 4, 2018 · Dhav DHC8102 · Brake Anti-Skid Section
  > (CAN) AIRCRAFT TAXIED FOR DEPARTURE AND WAS HOLDING SHORT OF RUNWAY FOR TAKE OFF, FLIGHT CREW REPORTED TO MAINTENANCE CONTROL THAT THE AIRCRAFT WOULDN`T MOVE WHEN PARK BRAKE WAS RELEASED AND POWER APPLIED FROM A FULLY STOPPED POSITION. PARK BRAKE WAS RESET.
- [SDR CA180723012](https://openairdocs.org/sdr/CA180723012.md): Condenser · cracked · Jun 18, 2018 · Dhav DHC8102 · Air Distribution System
  > (CAN) DURING FLIGHT, FLIGHT CREW REPORTED AN INTERMITTENT AIR COND PACK HOT AMBER CAUTION LIGHT. DURING TROUBLESHOOTING, THE CONDENSER MIXER WAS FOUND CRACKED AT THE HEAT EXCHANGER INLET PORT. THE CONDENSER MIXER WAS REPLACED AND THE SYSTEM TESTED SERVICEABL
- [SDR CA180404019](https://openairdocs.org/sdr/CA180404019.md): Oil Cooler · leaking · Apr 1, 2018 · Dhav DHC8102 · Engine Oil Cooler
  > (CAN) ON APPROACH THE NR 1 ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 40PSI WITH ASSOCIATED NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. WHILE TAXIING TO THE GATE THE OIL PRESSURE DROPPED TO ZERO AND FLUCTUATED. THE CREW THEN PERFORMED AN ENGINE SHU
- [SDR CA180103007](https://openairdocs.org/sdr/CA180103007.md): Pump · failed · Dec 30, 2017 · Dhav DHC8102 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) SHORTLY AFTER TAKE-OFF THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED. THE CREW TURNED BACK TO BASE AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. P/N: 570347 S/N: MX-494399CD TSN HOURS: 29470, CYCLES: 33246 TSR HOURS: 115, CYCLES: 98 A/C HOURS
- [SDR HNAA2017103000364](https://openairdocs.org/sdr/HNAA2017103000364.md): Light · inoperative · Oct 29, 2017 · N806EX · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY LIGHTS AT ROW 17DF DIM. REMOVE AND REPLACED THE EMERGENCY LIGHT ASSEMBLIES AT ROW 7DF.
- [SDR HNAA2017103000361](https://openairdocs.org/sdr/HNAA2017103000361.md): Indicator · malfunctioned · Oct 29, 2017 · N806EX · Dhav DHC8102 · Engine Temperature Indicating System
  > ON TAKEOFF, NR 2 ITT INDICATOR STUCK AT 1050. ALL OTHER ENGINE PARAMETERS AND INDICATIONS WERE NORMAL. POWERED AIRCRAFT DOWN AND REAPPLIED POWER. TESTED NR 2 ITT INDICATOR. OPERATED NORMAL. GROUND RAN THE AIRCRAFT. ALL INDICATIONS OPERATE NORMAL AT THIS TI
- [SDR HNAA2017101000347](https://openairdocs.org/sdr/HNAA2017101000347.md): Light · inoperative · Oct 8, 2017 · N809EX · Dhav DHC8102 · Emergency Lighting
  > FLOOR EMERGENCY LIGHT AT SEAT 7DF INOPERATIVE. R & R THE EMERGENCY LIGHT.
- [SDR HNAA2017101000346](https://openairdocs.org/sdr/HNAA2017101000346.md): Bulb · burned out · Oct 6, 2017 · N805EX · Dhav DHC8102 · Emergency Lighting
  > CABIN FLOOR EMERGENCY LIGHT THIRD RED LIGHT BULB INOPERATIVE AT SEAT 1DF. REMOVED & REPLACED THE BULB.
- [SDR HNAA2017092900336](https://openairdocs.org/sdr/HNAA2017092900336.md): Switch · inoperative · Sep 27, 2017 · N975HA · Dhav DHC8102 · Emergency Lighting
  > FLOOR EMERGENCY LIGHTS WILL NOT TURN OFF USING F/A SWITCH. SIDE WALL LIGHTS WILL NOT RESPOND TO THE SWITCH. R & R THE F/A LIGHTS CONTROL PANEL IAW 33-20-00, AND 33-51-00. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2017092900339](https://openairdocs.org/sdr/HNAA2017092900339.md): Unknown · odor · Sep 26, 2017 · N805EX · Dhav DHC8102 · Air Distribution System
  > CREW REPORTED AN ODD ODOR IN THE ACFT AROUND SEAT 5AC. DROPPED LT PSU AND CENTER AISLE PANEL INSPECTED, NO FAULTS FOUND. REINSTALLED PSU AND CENTER PANEL. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HNAA2017091801](https://openairdocs.org/sdr/HNAA2017091801.md): Power Supply · burned · Sep 16, 2017 · N975HA · Dhav DHC8102 · Emergency Lighting
  > DURING TROUBLESHOOTING OF SEQ 3, FOUND THE POWER SUPPLY BASE AT 3351-P4 HAS A BURNED ODOR AND APPEARS TO HAVE A BURNED RESISTOR. R & R THE EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-00.
- [SDR HNAA20170918317](https://openairdocs.org/sdr/HNAA20170918317.md): Battery Pack · inoperative · Sep 16, 2017 · N975HA · Dhav DHC8102 · Emergency Lighting
  > LEFT FUSELAGE MOUNTED EMERGENCY LIGHTS INOPERATIVE. R & R THE POWER SUPPLY AND BATTERY AT 3351-PS3 IAW AMM 33-51-00.
- [SDR HNAA20170918316](https://openairdocs.org/sdr/HNAA20170918316.md): Warning Light · unknown · Sep 16, 2017 · N805EX · Dhav DHC8102 · AC Generator-Alternator
  > RIGHT AC BUSS CAUTION LIGHT ILLUMINATED DURING CLIMB OUT, WITH ASSOCIATED CAUTION LIGHTS. REMOVED AND REINSTALLED THE LT AC GCU FOR TROUBLESHOOTING. REPLACED RT GCU. OPS CHECK GOOD.
- [SDR HNAA2017091400304](https://openairdocs.org/sdr/HNAA2017091400304.md): Switch · lack of lube · Sep 9, 2017 · N837EN · Dhav DHC8102 · Propeller Controlling System
  > REJECTED TAKE OFF DUE TO AT 60 PERCENT TORQUE AUTOFEATHER ARM LIGHT ILLUMINATED WITH TAKEOFF WARNING HORN. CLEANED AND LUBRICATED THE SWITCHES. R & R FLAP POSITION INDICATOR. OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR HNAA2017090500299](https://openairdocs.org/sdr/HNAA2017090500299.md): Light · inoperative · Sep 3, 2017 · N941HA · Dhav DHC8102 · Emergency Lighting
  > MIDDLE CEILING EMERGENCY LIGHT INOP.
- [SDR HNAA2017082500288](https://openairdocs.org/sdr/HNAA2017082500288.md): Contactor · inoperative · Aug 24, 2017 · N941HA · Dhav DHC8102 · Landing Gear Position and Warning
  > LEFT MAIN GEAR INDICATION FAILED IN THE DIM AND BRIGHT MODE. GREEN DOWNLOCK INDICATION. INSPECTION FOUND CONTACTS NOT CONNECTING TO BULBS.
- [SDR HNAA2017082500286](https://openairdocs.org/sdr/HNAA2017082500286.md): Autofeather Sys · malfunctioned · Aug 24, 2017 · N336EN · Dhav DHC8102 · Propeller Feathering/Reversing
  > REJECTED TAKEOFF DUE TO AUTOFEATHER NOT ARMING UP TO 90% TORQUE. R & R THE NR 1 TSEU. GROUND RAN ACFT. AUTO-FEATHER SYSTEM OPS NORMAL IAW RUNUP MANUAL,. OK FOR SERVICE AT THIS TIME.
- [SDR HNAA2017080200259](https://openairdocs.org/sdr/HNAA2017080200259.md): Sign · inoperative · Aug 2, 2017 · N806EX · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE ON FWD RT FUSELAGE, FWD AISLE OVERHEAD EMERGENCY EXIT SIGN.
- [SDR HNAA2017073100253](https://openairdocs.org/sdr/HNAA2017073100253.md): Light · inoperative · Jul 30, 2017 · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY AISLE LIGHT INOPERATIVE AT ROW 7
- [SDR HNAA2017073100254](https://openairdocs.org/sdr/HNAA2017073100254.md): Light · inoperative · Jul 29, 2017 · N937HA · Dhav DHC8102 · Emergency Lighting
  > THE THIRD RED AFT EMERGENCY AISLE LIGHT IS INOPERATIVE.
- [SDR HNAA2017073100251](https://openairdocs.org/sdr/HNAA2017073100251.md): Light · inoperative · Jul 25, 2017 · N941HA · Dhav DHC8102 · Emergency Lighting
  > THIRD RED FLOOR EMERGENCY LIGHT INOPERATIVE.
- [SDR HNAA2017072500247](https://openairdocs.org/sdr/HNAA2017072500247.md): Battery · discharged · Jul 21, 2017 · N805EX · Dhav DHC8102 · Emergency Lighting
  > FWD RT EXTERNAL EMERGENCY LIGHT INOPERATIVE, GALLEY CEILING, RT FWD EMERGENCY EXIT TOP, NOT WORKING. CHANGED THE BATTERY AT 3351 PS2 LOCATION IAW AMM 33-51-00, OPS CHECKED GOOD.
- [SDR HNAA2017071200238](https://openairdocs.org/sdr/HNAA2017071200238.md): Connector · dirty · Jul 11, 2017 · N942HA · Dhav DHC8102 · Engine Indicating System Wiring
  > NR 2 ITT AND TORQUE GAUGES CIRCUIT BREAKERS TRIPPED INFLT. REMOVED AND CLEANED THE ENGINE SPIDER HARNESS CONNECTOR AT THE FIRE WALL. RESET CIRCUIT BREAKERS AND OPS CHECKED GOOD.

Next page: https://openairdocs.org/model/boeing-dhc-8-102/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 aircraft_model_key = 'DHC8102'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-dhc-8-102/reports

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