# Service difficulty reports: Bombardier DHC-8-201

A list on [Bombardier DHC-8-201](https://openairdocs.org/model/bombardier-dhc-8-201.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 299 reports

- [SDR 2026FA0000665](https://openairdocs.org/sdr/2026FA0000665.md): Fuel Sys · abnormal · Aug 25, 2026 · N541AV · Dhav DHC8201 · Fuel Storage
  > THE AIRCRAFT HAS BEEN MODIFIED WITH STC ST03382NY, WHICH CONVERTS A DRY BAY IN EACH WING TO AN EXTENDED RANGE AUXILIARY FUEL TANK. STANDING FUEL WAS NOTED IN THE DRY BAY ADJACENT TO THE BAY MODIFIED INTO AN AUX FUEL TANK. THE FUEL WAS TRAPPED BY STRINGERS AND
- [SDR HKGA20220314001](https://openairdocs.org/sdr/HKGA20220314001.md): Spacer · cracked · Mar 12, 2022 · N406AV · Dhav DHC8201 · Air Conditioning System
  > BLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED DURING ROUTINE MAINTENANCE. REMOVED AND REPLACED SPACER ASSEMBLY.
- [SDR CA190709011](https://openairdocs.org/sdr/CA190709011.md): Capacitor · damaged · Jul 5, 2019 · Dhav DHC8201 · Electrical Power System Wiring
  > (CAN) THE OCCURRENCE HAPPENED ON GROUND DURING MAINTENANCE WITH NO PASSENGERS OR FLIGHT CREW ON BOARD. DESCRIPTION: DURING MAINTENANCE, IT WAS DISCOVERED SMOKE FROM AVIONIC SHELF. CIRCUIT BREAKERS 115/26 VAC XFMR LT AND CIRCUIT BREAKER RNAV 2 (J2) WAS FOUND P
- [SDR CA190610009](https://openairdocs.org/sdr/CA190610009.md): Outflow Valve · malfunctioned · Jun 3, 2019 · Dhav DHC8201 · Pressure Regulator/Outflow Valve
  > (CAN) CREW OBSERVED CABIN ALT FLUCTUATION (BOTH INCREASING AND DECREASING) WITH CAB RATE OF CLIMB 2000 FPM. THE AIRCRAFT DESCEND TO A/C ALT 7000 FT (WITH CAB ALT 6000 FT). AIR TURN BACK PERFORMED. CREW REPORTED EAR ACHE AND A KIND OF WHITE SMOKE MOMENTARILY.
- [SDR HNAA2017042500146](https://openairdocs.org/sdr/HNAA2017042500146.md): Bulb · inoperative · May 2, 2017 · N937HA · Dhav DHC8201 · Emergency Lighting
  > GREEN LIGHT ON EMERGENCY LIGHT SWITCH AT FLIGHT ATTENDANT PANEL INOPERATIVE. R & R THE BULB.
- [SDR HNAA2017042500145](https://openairdocs.org/sdr/HNAA2017042500145.md): Bulb · inoperative · May 2, 2017 · N942HA · Dhav DHC8201 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. R & R THE BULBS.
- [SDR HNAA2017042500139](https://openairdocs.org/sdr/HNAA2017042500139.md): Power Supply · inoperative · Apr 28, 2017 · N930HA · Dhav DHC8201 · Emergency Lighting
  > GROUND EMERGENCY LIGHT BY FWD EMERGENCY EXIT DIMS AND GOES OUT AFTER A FEW SECONDS R & R THE POWER SUPPLY AT SEAT 7AC IAW AMM 33-50-00.
- [SDR HNAA2017042500138](https://openairdocs.org/sdr/HNAA2017042500138.md): Bulb · inoperative · Apr 27, 2017 · N943HA · Dhav DHC8201 · Emergency Lighting
  > F/A PANEL EMERGENCY LIGHT SWITCH NORM INDICATING BULB INOPERATIVE. R & R THE BULB.
- [SDR HNAA2017021500052](https://openairdocs.org/sdr/HNAA2017021500052.md): Control Panel · malfunctioned · Feb 11, 2017 · N938HA · Dhav DHC8201 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, THE F/O SELECTED GEAR UP. THREE RED UNSAFE LIGHTS AND THREE GREEN ILLUMINATED ON THE MLG PANEL ALONG WITH BOTH HANDLE LIGHTS. CREW FOLLOWED CHECKLIST AND THE LIGHTS CLEARED WHEN GEAR SELECTED DWN. OK AFTER THAT. R & R THE LANDING GEAR SELECTOR
- [SDR JJBA20160109007](https://openairdocs.org/sdr/JJBA20160109007.md): Battery · discharged · Jan 9, 2016 · N857CA · Dhav DHC8201 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R 6 EMER LIGHT BATTERIES. PERFORMED OPERATIONS CHECK. THE RESULTS OF THE OPERATIONS CHECK WAS SATISFACTORY.
- [SDR JJBA20160108008](https://openairdocs.org/sdr/JJBA20160108008.md): Fuel Control · malfunctioned · Jan 8, 2016 · N374PH · Dhav DHC8201 · Fuel Control/Turbine Engines
  > ON CLIMB OUT, NR 2 TORQUE LAGGED BEHIND NR 1 TORQUE GAUGE, WHICH EVENTUALLY DROPPED TO 20% & CREW SHUTDOWN THE ENG. FUEL FLOW WAS 100 LBS LESS. R & R FUEL CONTROL, ECU & PERFORMED OPERATIONS TEST, RESULTS OF OPERATIONS TEST WAS SATISFACTORY.
- [SDR JJBA20160108006](https://openairdocs.org/sdr/JJBA20160108006.md): Smoke Detector · faulty · Jan 8, 2016 · N366PH · Dhav DHC8201 · Smoke Detection
  > LAVATORY SMOKE DETECTOR ALARM SOUNDED DURING TAXI. R & R SMOKE DETECTOR & OPERATIONS CHECK DONE. OPERATIONS CHECK WAS SATISFACTORY.
- [SDR JJBA20160107005](https://openairdocs.org/sdr/JJBA20160107005.md): Ditching Dam · low pressure · Jan 7, 2016 · N839CA · Dhav DHC8201 · Emergency Equipment
  > RIGHT SIDE DITCHING DAM PRESS INDICATES 1000 PSI. SERVICED DITCHING DAM TO PROPER PSI.
- [SDR JJBA20160103003](https://openairdocs.org/sdr/JJBA20160103003.md): Switch · out of adjust · Jan 3, 2016 · N366PH · Dhav DHC8201 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH IS NOT ILLUMINATING GREEN. ADJUSTED EMER LIGHT SWITCH. PERFORMED OPERATIONS CHECK OF SYS, SYS TESTED SATISFACTORY.
- [SDR JJBA20160102004](https://openairdocs.org/sdr/JJBA20160102004.md): Indicator · defective · Jan 2, 2016 · N379PH · Dhav DHC8201 · Airspeed/Mach Indicator
  > TAKEOFF AIRSPEED DIFFERENCE OF 30 KNOTS, BETWEEN THE AIRSPEED INDICATORS, FIRST OFFICERS SIDE. R & R FIRST OFFICERS AIRSPEED INDICATOR, PERFORMED OPERATIONS CHECK, CHECKED SATISFACTORY.
- [SDR JJBA20151226010](https://openairdocs.org/sdr/JJBA20151226010.md): Battery Pack · discharged · Dec 26, 2015 · N366PH · Dhav DHC8201 · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT WORK WHEN TESTED. R & R LIGHT BATTERY PACKS.
- [SDR JJBA20151210007](https://openairdocs.org/sdr/JJBA20151210007.md): Warning System · false activation · Nov 14, 2015 · N876CA · Dhav DHC8201 · Cabin Pressure Control System
  > CABIN PRESS LIGHT ILLUMINATED IN FLIGHT. PERFORMED CABIN PRESS OPERATIONS CHECK. OPERATIONS CHECK WAS SATISFACTORY.
- [SDR JJBA20151113003](https://openairdocs.org/sdr/JJBA20151113003.md): Warning System · false activation · Nov 13, 2015 · N369PH · Dhav DHC8201 · Door Warning System
  > PASSENGER DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. INSPECTED DOOR CLOSED SENSOR & OVER CENTER PROXIMITY SENSOR WIRING & CONNECTIONS. PERFORMED DETAILED VISUAL INSPECTION & OPERATION CHECKED DOOR, PRESSURIZED ACFT TO 3 PSI WITH NO LEAKS OR WARNING.
- [SDR JJBA20151104002](https://openairdocs.org/sdr/JJBA20151104002.md): Battery Pack · discharged · Nov 4, 2015 · N379PH · Dhav DHC8201 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE CABIN DOOR INOPERATIVE. R & R BATTERY PACK.
- [SDR JJBA20151104001](https://openairdocs.org/sdr/JJBA20151104001.md): Battery · discharged · Nov 4, 2015 · N368PH · Dhav DHC8201 · Emergency Lighting
  > THREE CABIN EMER EXIT LIGHTS INOPERATIVE. R & R PS-1 & PS-2 EMER BATTERIES.
- [SDR JJBA20151029010](https://openairdocs.org/sdr/JJBA20151029010.md): Warning System · activated · Oct 29, 2015 · N360PH · Dhav DHC8201 · Landing Gear Position and Warning
  > WITH LG DOWN & LOCKED, RECEIVED GEAR UNSAFE HORN AS WELL AS BOTH AMBER & RED GEAR UNSAFE LIGHTS, WHICH WERE ILLUMINATED. GEAR UNSAFE LIGHTS CYCLED 6 TIMES FROM AMBER TO RED WHILE PROCEEDING TO GO AROUND IN LEVEL FLIGHT. ALTERNATE EXTENSION PROCEDURES WERE EX
- [SDR JJBA20151029009](https://openairdocs.org/sdr/JJBA20151029009.md): Trim Panel · out of adjust · Oct 29, 2015 · N366PH · Dhav DHC8201 · Emergency Exits
  > TYPE NR 2 EMER EXIT DOOR HITTING THE OVERHEAD BIN WHEN REMOVING. ADJUSTED TYPE NR 2 EMER EXIT DOOR TRIM.
- [SDR JJBA20151029008](https://openairdocs.org/sdr/JJBA20151029008.md): Handle · detached · Oct 29, 2015 · N362PH · Dhav DHC8201 · Emergency Exits
  > TYPE NR 2 EMER EXIT DOOR HANDLE NOT ATTACHED. SECURED TYPE NR 2 EMER EXIT DOOR HANDLE TO DOOR.
- [SDR JJBA20151028007](https://openairdocs.org/sdr/JJBA20151028007.md): Vsi · defective · Oct 28, 2015 · N837CA · Dhav DHC8201 · Rate of Climb Indicator
  > CAPTAINS INERTIAL VERTICAL SPEED INDICATOR SCREEN WENT BLANK, THEN THE SMELL OF SMOKE WAS IN THE COCKPIT. INSPECTED SYS & FOUND NR 1 INERTIAL VERTICAL SPEED INDICATOR DEFECTIVE.
- [SDR CA151117011](https://openairdocs.org/sdr/CA151117011.md): Strut · cracked · Oct 21, 2015 · Dhav DHC8201 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) CRACKS HAVE BEEN REPORTED ON NLG OUTER CYLINDERS. REPORTED CYCLES SINCE NEW RANGE BETWEEN 18,995 CYCLES TO 49,039 CYCLES. REPORTED CYCLES SINCE O/H HAVE RANGED BETWEEN 2034 CYCLES AND 18,888 CYCLES. ALL CRACKING WERE LOCATED ON THE STARBOARD AFT FACE,
- [SDR JJBA20151019005](https://openairdocs.org/sdr/JJBA20151019005.md): Hydraulic Line · broken · Oct 19, 2015 · N369PH · Dhav DHC8201 · Hydraulic System, Main
  > LOSS OF ALL HYD FLUID ON THE NR 2 ENG. FOUND CASE DRAIN LINE BROKEN. REPLACED BROKEN LINE WITH FLEXIBLE LINE.
- [SDR JJBA20151018006](https://openairdocs.org/sdr/JJBA20151018006.md): Stud · loose · Oct 18, 2015 · N366PH · Dhav DHC8201 · Aileron Tab Control System
  > WHILE AUTOPILOT WAS OFF, VERY BUFFET IN THE CONTROL COLUMN APPEAR TO BE WORSE AT HIGH SPEEDS, BUFFET WENT AWAY WITH AUTOPILOT ON. PERFORMED GENERAL VISUAL INSPECTION OF ALL FLIGHT CONTROLS, INSPECTED UNDER FLOOR CONTROLS, PILOTS YOKE & COPILOTS YOKE. FOUND L
- [SDR JJBA20151018004](https://openairdocs.org/sdr/JJBA20151018004.md): Connector · dirty · Oct 18, 2015 · N839CA · Dhav DHC8201 · Fire Protection System Wiring
  > BAGGAGE SMOKE WARNING TEST 2 WON'T TEST. CLEANED & RE-SEATED CONNECTOR.
- [SDR JJBA20151009002](https://openairdocs.org/sdr/JJBA20151009002.md): Light · inoperative · Oct 9, 2015 · N839CA · Dhav DHC8201 · Emergency Lighting
  > LAST 2 EMER CEILING LIGHT INOPERATIVE. PERFORMED OPERATIONS CHECK OF THE EMER LIGHT SYS.
- [SDR JJBA20151007001](https://openairdocs.org/sdr/JJBA20151007001.md): Battery · not seated · Oct 7, 2015 · N839CA · Dhav DHC8201 · Emergency Lighting
  > EMERGENCY THRESHOLD LIGHT INOPERATIVE. RE-SEATED BATTERY.
- [SDR JJBA20150925006](https://openairdocs.org/sdr/JJBA20150925006.md): Smoke Detector · false activation · Sep 25, 2015 · N366PH · Dhav DHC8201 · Smoke Detection
  > SMOKE WARNING ILLUMINATED IN FLIGHT. R & R FWD & AFT SMOKE DETECTORS.
- [SDR JJBA20150920005](https://openairdocs.org/sdr/JJBA20150920005.md): Battery · discharged · Sep 20, 2015 · N361PH · Dhav DHC8201 · Emergency Lighting
  > FLIGHT ATTENDANT EMER LIGHTS WILL NOT TEST. R & R 6 EACH EMER LIGHT BATTERIES, PS 1 - PS 6.
- [SDR JJBA20150908002](https://openairdocs.org/sdr/JJBA20150908002.md): Battery · discharged · Sep 8, 2015 · N360PH · Dhav DHC8201 · Emergency Lighting
  > EMERGENCY LIGHTS FLICKER ON WHEN SELECTED, THEN GO OUT. R & R EMER BATTERY PS-2.
- [SDR CA150717002](https://openairdocs.org/sdr/CA150717002.md): Pitot Tube · malfunctioned · Jun 20, 2015 · Dhav DHC8201 · Pitot/Static Anti-Ice System
  > (CAN) AIRCRAFT ENTERED ICING CONDITIONS. CREW REPORTED PITOT HEAT 1 AND 2 CAUTION ILLUMINATED WITH THEIR ASSOCIATED CB TRIPPING. QUICK DESCENT WAS INITIATED. REPORTS OF SMOKE SEEN COMING OUT OF THE AIR-CONDITION VENTS, HOWEVER THERE WAS NO SMELL OF SMOKE. EMER
- [SDR CA150410008](https://openairdocs.org/sdr/CA150410008.md): Unknown · odor · Apr 7, 2015 · Dhav DHC8201 · Air Distribution System
  > (CAN) SURVEILLANCE FLIGHT PERFORMED AN AIR RETURN SHORTLY AFTER TAKEOFF FOR MINOR OIL SMELL IN CABIN. ACFT LANDED UNEVENTFULLY. TROUBLESHOOTING IS ONGOING.
- [SDR CA141006014](https://openairdocs.org/sdr/CA141006014.md): Propeller · overspeed · Sep 15, 2014 · Dhav DHC8201 · Propeller System
  > (CAN) DURING CLIMB, THE PROPELLER HAD AN OVERSPEED AND THE PILOT SHUTDOWN THE ENGINE. ELECTED TO RETURN TO ORIGIN WHERE AN UNEVENTFULLY LANDING WAS PERFORMED. ALSO DURING CLIMB, THE PILOT SHUTDOWN THE ENGINE AFTER TORQUE FLUCTUATION OCCURRED. AT THIS TIME T
- [SDR CA140522014](https://openairdocs.org/sdr/CA140522014.md): Starter Gen · failed · Apr 13, 2014 · Dhav DHC8201 · Starter-Generator
  > (CAN) PILOT REPORT, AFTER ACFT BOARDED AND AN ATTEMPTED APU START MADE A CHECK FIRE DETECT WARNING WAS OBSERVED ALONG WITH A GEN OVERHEAT ADVISORY LIGHT. FUMES AND SMOKE FROM THE APU AREA WERE CONFIRMED. NO APU FIRE ADVISORY WAS PRESENT. ACFT WAS DE-POWERED
- [SDR CA140604002](https://openairdocs.org/sdr/CA140604002.md): Control Unit · faulted · Mar 27, 2014 · Dhav DHC8201 · Fire Detection
  > (CAN) DURING CRUISE ENGINE FIRE MASTER WARNING LIGHT, FIRE BELLS AND MASTER WARNING CHECK FIRE DETECTION LIGHTS CAME ON WITH NO OTHER INDICATIONS. FIRE BELLS AND LIGHT COULD NOT BE CANCELLED OR SILENCED FOR APPROXIMATELY 90 SEC. AFTER THAT FAULT DID NOT RETUR
- [SDR CA140311008](https://openairdocs.org/sdr/CA140311008.md): Connector · damaged · Mar 1, 2014 · Dhav DHC8201 · Air Conditioning System Wiring
  > (CAN) CREW REPORTED THAT THE GROUND FAN WAS INOPERATIVE. DURING TROUBLESHOOTING WAS FOUND THAT THE CONNECTOR OF THE GROUND FAN WAS BURNED DUE TO A SHORT CIRCUIT. THE UNIT WILL BE SENT TO THE VENDOR FOR INVESTIGATION TO FIND THE ROOT CAUSE.
- [SDR CA140522011](https://openairdocs.org/sdr/CA140522011.md): Line · burst · Jan 16, 2014 · Dhav DHC8201 · Turbine Engine Oil System
  > (CAN) NR 1 ENGINE HAD IN-FLIGHT SHUTDOWN DUE TO ENGINE LOW OIL PRESSURE CAUTION LIGHT ILLUMINATED. MAINTENANCE ACTION C/O: ERG DONE TO CHECK FOR OIL LEAKS. FOUND OIL LEAK DUE TO MAIN OIL SUPPLY LINE BURST. NR 1 ENGINE OIL HOSE, PN DSC391-2, FOUND CRACKED A
- [SDR CA140119008](https://openairdocs.org/sdr/CA140119008.md): Warning Light · activated · Jan 15, 2014 · Dhav DHC8201 · Engine (Turbine/Turboprop)
  > (CAN) REPORTED THAT THE NR 1 ENGINE HAD A PILOT-INDUCED IFSD DUE TO A LOW OIL PRESSURE CAUTION LIGHT. PRELIMINARY INSPECTION POINTING TOWARDS AN EXTERNAL OIL LEAK.
- [SDR CA130910001](https://openairdocs.org/sdr/CA130910001.md): Spu · leaking · Sep 10, 2013 · Dhav DHC8201 · Hydraulic System, Main
  > (CAN) AN ACFT EXPERIENCED PROBLEM ON NR 2 HYDRAULIC SYS DURING APPROACH. THE CREW DECLEARED AN EMERGENCY, PERFORMED ALTERNATE LG EXTENSION AND LANDED. HYDRAULIC LEAKAGE WAS CONFIRMED FROM NR 2 SPU, PN 731840, 2 MECHANICS AND 1 QA INSPECTOR WERE DISPATCHED ON
- [SDR CA130314013](https://openairdocs.org/sdr/CA130314013.md): Acm · seized · Mar 4, 2013 · Dhav DHC8201 · Cabin Cooling System
  > (CAN) DURING CRUISE AT 13,000 FT, CABIN DUCT TEMPERATURE STARTED TO RISE. QRH FOLLOWED, ACFT DESCENDED TO 10,000 FT. MAINTENANCE HAS CONFIRMED THE ACM HAD SEIZED. ACM REPLACED.
- [SDR CA120920001](https://openairdocs.org/sdr/CA120920001.md): Windshield · sparks · Sep 17, 2012 · Dhav DHC8201 · Window System Wiring
  > (CAN) CREW OBSERVED AN ELECTRICAL FLASH ACCOMPANIED WITH A SMOKE PLUME FROM THE CAPTAINS WINDSHIELD AREA FOR APPROXIMATELY 2 SECONDS. CREW CONDUCTED THE COMPANY SMOKE RECALL. CREW DECLARED A PAN CALL AS A PRECAUTION & CONDUCTED ALL RELEVANT CHECKLISTS AFTER WH
- [SDR CA120522008](https://openairdocs.org/sdr/CA120522008.md): Blade · damaged · Apr 9, 2012 · Dhav DHC8201 · Propeller Blade Section
  > (CAN) DURING APPROACH AT APPROXIMATELY 1500 FT A LOUD TAP NOISE WAS HEARD. THIS NOISE SOUNDED UNLIKE THE TYPICAL THUD THAT A BIRD MAY MAKE UPON IMPACT. CREW FOUND DURING WALK AROUND TO CHECK THE ACFT FOR DAMAGE AND SUBSEQUENTLY DISCOVERED A LARGE IMPACT MARK
- [SDR CA111030006](https://openairdocs.org/sdr/CA111030006.md): Oil System · low · Oct 19, 2011 · Dhav DHC8201 · Engine (Turbine/Turboprop)
  > (CAN) DURING DESCENT, THE PILOT REPORTED OIL PRESSURE FLUCTUATIONS AND LOW OIL PRESSURE WARNING. THE ENGINE WAS SHUTDOWN AND UNEVENTFUL SINGLE ENGINE LANDING CARRIED OUT AT DESTINATION. POST FLIGHT INSPECTION FOUND THE OIL LEVEL 8 QUARTS LOW AND AN OIL LEAK
- [SDR CA110331008](https://openairdocs.org/sdr/CA110331008.md): Indicator · inaccurate · Mar 20, 2011 · Dhav DHC8201 · Engine Oil Pressure
  > (CAN) OIL PRESSURE LOSS DURING FLIGHT, THE OIL PRESSURE STARTED TO OSCILLATE AND THEN STARTED TO DECREASE. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. TROUBLESHOOTING IS ON-GOING AND FOCUSING ON AN INDICATION PROBLEM.
- [SDR CA110209009](https://openairdocs.org/sdr/CA110209009.md): Flt Controls · multiple fail · Feb 6, 2011 · Dhav DHC8201 · Flight Control System
  > WHILE CLIMBING TO FLIGHT LEVEL 19000. AT APPROX 10000 FT AND IN THE CLIMB, 130 KIAS, PILOTS NOTICED AN INCREASINGLY EXCESSIVE FORCE WAS REQUIRED ON ALL PITCH AND ROLL INPUTS. LEVELING AT FL190 BOTH HANDS WERE NEEDED TO LEVEL THE ACFT DUE TO EXTREMELY EXCESSIVE
- [SDR CA101229003](https://openairdocs.org/sdr/CA101229003.md): Shaft · cracked · Dec 18, 2010 · Dhav DHC8201 · Propeller Assembly
  > (CAN) OIL LEAK DURING FLIGHT, THE CREW REPORTED HIGH VIBRATIONS WHICH WAS FOLLOWED DURING APPROACH BY OIL PRESSURE FLUCTUATIONS. DURING TAXI AFTER LANDING, THE LOW OIL PRESSURE WARNING LIGHT FLICKERED ON AND OFF. POST FLIGHT INSPECTION FOUND A SEVERE OIL LEAK
- [SDR CA101210004](https://openairdocs.org/sdr/CA101210004.md): Wheel · damaged · Dec 7, 2010 · Dhav DHC8201 · Wheel/Ski/Float
  > (CAN) AFTER LANDING MAINTENANCE NOTED THAT THE NR 2 MAIN WHEEL WAS FLAT. IT WAS ALSO NOTED THAT 30 TO 40 PERCENT OF THE BEADSEAT AREA ON THE INBOARD WHEEL HALF WAS MISSING.

Next page: https://openairdocs.org/model/bombardier-dhc-8-201/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 = 'DHC8201'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bombardier-dhc-8-201/reports

---
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.