# Service difficulty reports: Bombardier DHC-8-202

A list on [Bombardier DHC-8-202](https://openairdocs.org/model/bombardier-dhc-8-202.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 165 · 8,233 reports

- [SDR BIGA20260824001](https://openairdocs.org/sdr/BIGA20260824001.md): Air Duct · detached · Aug 24, 2026 · N993BH · Dhav DHC8202 · Air Distribution System
  > AIRCRAFT WAS ENROUTE TO RESPOND TO A FIRE MISSION. WHILE ENROUTE THE SMOKE-JUMPER CREW SAW WHAT APPEARED TO BE SMOKE COMING FROM RIGHT AFT CABIN FLOORBOARDS. THE AIRCRAFT MADE AN UN-SCHEDULED LANDING AT GPI WITH NO INCIDENT. ONCE ON THE GROUND THE AIRCRAFT
- [SDR 2023FA0000702](https://openairdocs.org/sdr/2023FA0000702.md): Engine · power loss · Oct 5, 2023 · N805MR · Dhav DHC8202 · Engine (Turbine/Turboprop)
  > 10/5/2023 AT AROUND 4:25 PM CST, D8-200 N805MR WAS DEPARTING MIAMI EXECUTIVE AIRPORT. AIRCRAFT WAS SET UP FOR CRUISE CLIMB WITH AUTOPILOT ENGAGED. PROP RPM 1064 AND 1058. TORQUES AT 95.5 AND 95.5%. BETWEEN 3000-4000 FEET, #2 ENGINE SPIKED TO 112.75 AND # 1 WE
- [SDR 2022FA0000214](https://openairdocs.org/sdr/2022FA0000214.md): None · none · Apr 15, 2022 · N991HA · Dhav DHC8202 · Fuel Storage
  > UNDETECTED, STANDING FUEL IN A WING DRY BAY WITH A BLEED AIR TUBE HAS PROMPTED THIS REPORT. THE AIRCRAFT HAS BEEN MODIFIED WITH STC ST03382NY, WHICH CONVERTS A DRY BAY IN EACH WING TO AN EXTENDED RANGE AUXILIARY FUEL TANK. AT HEAVY CHECK, ON OPENING THE ACCESS
- [SDR HKGA20220314004](https://openairdocs.org/sdr/HKGA20220314004.md): Spacer · cracked · Mar 13, 2022 · N449YV · Dhav DHC8202 · Air Conditioning System
  > BLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER.
- [SDR HKGA20220314003](https://openairdocs.org/sdr/HKGA20220314003.md): Spacer · cracked · Mar 13, 2022 · N437YV · Dhav DHC8202 · Air Conditioning System
  > BLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER.
- [SDR HKGA20220314002](https://openairdocs.org/sdr/HKGA20220314002.md): Spacer · cracked · Mar 13, 2022 · N541AV · Dhav DHC8202 · Air Conditioning System
  > BLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER.
- [SDR HKGA20190821742](https://openairdocs.org/sdr/HKGA20190821742.md): Trim Tab · cracked · Aug 16, 2019 · N989HA · Dhav DHC8202 · Elevator Tab Control System
  > RH ELEVATOR SPRING TAB CRACKED @ TRAILING EDGE. REMOVED AND REPLACED RH ELEVATOR SPRING TAB IAW DHC-8 MM 27-34-11.
- [SDR HKGA201908217041](https://openairdocs.org/sdr/HKGA201908217041.md): Trim Tab · damaged · Aug 16, 2019 · N989HA · Dhav DHC8202 · Elevator Tab Control System
  > DURING INSPECTION IT WAS FOUND THAT THE LH ELEVATOR SPRING TAB HAS A BULLET HOLE @ TRAILING EDGE. REMOVED AND REPLACED LH ELEVATOR SPRING TAB IAW DHC-8 MM 27-34-11.
- [SDR CA190628008](https://openairdocs.org/sdr/CA190628008.md): Switch · broken · Jun 21, 2019 · Dhav DHC8202 · Engine Controls
  > (CAN) WE HAD AN ENGINE IFSD ON MSN 522 DUE TO THE RH ENGINE SURGE BETWEEN 80% AND 120% ON FRIDAY 21/JUNE/19. PRECAUTION ENGINE SHUT DOWN WAS PERFORMED AND THE AIRCRAFT WAS SAFELY LANDED WITHOUT ANY INCIDENT: PILOT REPORT: THE ENGINE STARTED SURGING IMMEDIATELY
- [SDR CA190605008](https://openairdocs.org/sdr/CA190605008.md): Elevator System · malfunctioned · May 30, 2019 · Dhav DHC8202 · Elevator Control System
  > (CAN) WHEN THE CREW ROTATED THE AIRCRAFT, THERE WERE NO RESPONSE TO PITCH CONTROL INPUT AND THE CREW ELECTED TO EXECUTE A REJECTED TAKEOFF. THE AIRCRAFT IS CONFIGURED IN A Y29 COMBI VERSION (HUNTING CARGO/COMBI 8/2822) WITH 28 ADULT AND ON CHILD + 412 KGS BAGS
- [SDR CA190507007](https://openairdocs.org/sdr/CA190507007.md): Tab · dented · May 2, 2019 · Dhav DHC8202 · Elevator, Tab Structure
  > (CAN) DURING TAXI, WHILE PREFORMING THE BEFORE TAKEOFF CHECKS PRIOR TO FLIGHT, THE CREW REPORTED THE PITCH CONTROL WAS JAMMED AND THE FLIGHT WAS CANCELLED. AFTER INSPECTION OF THE FLIGHT CONTROL SURFACES, DENT DAMAGE WAS FOUND ON THE L/H ELEVATOR SPRING TAB
- [SDR CA190503014](https://openairdocs.org/sdr/CA190503014.md): Check Valve · cracked · Apr 30, 2019 · Dhav DHC8202 · Hydraulic System, Main
  > (CAN) DIVERSION CARRIED OUT DUE TO #2 HYDRAULIC FLUID LOSS. MAINTENANCE REPLACED BROKEN HYDRAULIC CHECK VALVE P/N: 3-1582-2-3 LOCATED IN THE TAIL SECTION AND RETURNED THE AIRCRAFT TO SERVICE. (TC# 20190503014)
- [SDR CA190415014](https://openairdocs.org/sdr/CA190415014.md): Starter Gen · malfunctioned · Apr 15, 2019 · Dhav DHC8202 · Starter-Generator
  > (CAN) UNIT SLOW TO START. LH STARTER GENERATOR VENT HAD INDICATIONS OF SMOKE OR OIL ON COWL. FOUND DRIVE SHAFT LOOSE AND UNIT WAS MAKING SMOKE. TEAR DOWN REPORT SHOWS: ENCLOSURE BROKEN/US. D.E. BEARING FAILURE. MISSING SECTIONS OF END BELL SCREEN. C.E. BEARING
- [SDR CA190411016](https://openairdocs.org/sdr/CA190411016.md): Bolt · loose · Apr 10, 2019 · Dhav DHC8202 · Elevator Control System
  > (CAN) DURING PILOT PRE TAKE OFF FLIGHT CONTROL CHECK, WITH CONTROL LOCK DISENGAGED, ELEVATOR MOVEMENT RESTRICTED, UNABLE TO MOVE AFT OF NEUTRAL POSITION. AIRCRAFT RETURNED TO BAY FOR MAINTENANCE ACTION. MAINTENANCE TROUBLESHOOTING CARRIED OUT. FARING ON RH EL
- [SDR A8ZR20181113003](https://openairdocs.org/sdr/A8ZR20181113003.md): Firewall · cracked · Nov 12, 2018 · N360PH · Dhav DHC8202 · Nacelle/Pylon, Bulkhead/Firewall
  > ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF #1 NACELLE RH IB SIDE AT XN 127.00 REF BOMBARDIER DEHAVILLAND RD 8-54-1565 ISSUE 3 DTD 18 FEB 04
- [SDR A8ZR20181113002](https://openairdocs.org/sdr/A8ZR20181113002.md): Structure · cracked · Nov 12, 2018 · N360PH · Dhav DHC8202 · Nacelle/Pylon, Bulkhead/Firewall
  > ACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 1 NACELLE RT IB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001.
- [SDR A8ZR20181113001](https://openairdocs.org/sdr/A8ZR20181113001.md): Firewall · cracked · Nov 12, 2018 · N360PH · Dhav DHC8202 · Nacelle/Pylon, Bulkhead/Firewall
  > ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NO 1 NACELLE RT IB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017.
- [SDR A8ZR20181106001](https://openairdocs.org/sdr/A8ZR20181106001.md): Firewall · cracked · Nov 5, 2018 · N360PH · Dhav DHC8202 · Nacelle/Pylon, Bulkhead/Firewall
  > ACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NR 2 NACELLE RT OB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017.
- [SDR A8ZR20181106002](https://openairdocs.org/sdr/A8ZR20181106002.md): Structure · cracked · Nov 5, 2018 · N360PH · Dhav DHC8202 · Nacelle/Pylon, Bulkhead/Firewall
  > ACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 2 NACELLE RT OB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001.
- [SDR 2018FA0000393](https://openairdocs.org/sdr/2018FA0000393.md): Hydraulic Line · leaking · Sep 20, 2018 · Dhav DHC8202 · Hydraulic System, Main
  > DURING CLIMB IN VVI-SRE LEG, THE AIRCRAFT SUFFERED TOTAL LOOS OF SYSTEM NR.2 HYDRAULIC FLUID, QRF TO DEPARTURE STATION. CORRECTIVE ACTION: HYDRAULIC FLUID LOOS WAS CAUSED BY A DEFECTIVE FLEXIBLE LINE LOCATED IN NLG BAY. THE DEFECTIVE HYDRAULIC FLEXIBLE LINE WA
- [SDR 2019F00058](https://openairdocs.org/sdr/2019F00058.md): Signal Cond Unit · failed · Aug 12, 2018 · Dhav DHC8202 · Propeller Indication System
  > PROPELLER OVERSPEED INDICATION ENG#1. AIRCRAFT TURN BACK TO AIRPORT AFTER SHUTTING DOWN AFFECTED ENGINE ACCORDING TO PROCEDURE. CORRECTIVE ACTION: SIGNAL CONDITIONER UNITS SWAPPED BETWEEN ENG#1 AND ENG #2. CLEANED OVERSPEED GOVERNOR SOLENOID VALVE CONNECTOR. E
- [SDR A8ZR20180817001](https://openairdocs.org/sdr/A8ZR20180817001.md): Skin · dented · Aug 11, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > DENT FOUND AT BS331, STRINGER 31L. REFORMED THE DENT AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-061, REV. A.
- [SDR A8ZR20180921001](https://openairdocs.org/sdr/A8ZR20180921001.md): Light · defective · Aug 10, 2018 · N375PH · Dhav DHC8202 · Emergency Lighting
  > RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.
- [SDR A8ZR201809121005](https://openairdocs.org/sdr/A8ZR201809121005.md): Skin · gouged · Jul 19, 2018 · N367PH · Dhav DHC8202 · Cargo/Baggage Doors
  > ACCOMPLISHED RE-SKIN ON AFT BAGGAGE DOOR UPPER SECTION THAT MEASURES 5.7" X 49.70" FOR GOUGES IN SKIN REF RD 8-52-029 ISSUE 2 DATED 2014-06-05.
- [SDR A8ZR20180924003](https://openairdocs.org/sdr/A8ZR20180924003.md): Light · defective · Jul 18, 2018 · N379PH · Dhav DHC8202 · Emergency Lighting
  > RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.
- [SDR A8ZR20180924002](https://openairdocs.org/sdr/A8ZR20180924002.md): Light · defective · Jul 18, 2018 · N363PH · Dhav DHC8202 · Emergency Lighting
  > RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N DSC543-1 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.
- [SDR A8ZR20180921003](https://openairdocs.org/sdr/A8ZR20180921003.md): Light · defective · Jul 17, 2018 · N361PH · Dhav DHC8202 · Emergency Lighting
  > RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.
- [SDR A8ZR20180921002](https://openairdocs.org/sdr/A8ZR20180921002.md): Light · defective · Jul 12, 2018 · N360PH · Dhav DHC8202 · Emergency Lighting
  > RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.
- [SDR A8ZR20180920001](https://openairdocs.org/sdr/A8ZR20180920001.md): Light · defective · Jul 10, 2018 · N359PH · Dhav DHC8202 · Emergency Lighting
  > RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.
- [SDR A8ZR20180831001](https://openairdocs.org/sdr/A8ZR20180831001.md): Light · defective · Jul 5, 2018 · N366PH · Dhav DHC8202 · Emergency Lighting
  > AFT RT EMERGENCY BETA LAMP FAILED BRIGHTNESS TEST. BETA LAMP ASSY REMOVED AND REPLACED REF AMM 33-51-00 REV 38 DATED MAY 15/17.
- [SDR A8ZR20180911002](https://openairdocs.org/sdr/A8ZR20180911002.md): Structure · dented · Jul 2, 2018 · N367PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > ACCOMPLISHED DOUBLER REPAIR AT STA 315.80 & BETWEEN S30S AND S31S FOR DENT WITH CREASE REF EA 45-2018-080 REV ORIGINAL ISSUE DATED 06/20/2018.
- [SDR A8ZR20180823007](https://openairdocs.org/sdr/A8ZR20180823007.md): Striker · out of limits · Jun 27, 2018 · N358PH · Dhav DHC8202 · Nacelle/Pylon, Main Frame
  > ACCOMPLISHED RE-CONTOUR OF NR 2 ENGINE I/B COWL DOOR NACELLE STRIP-STRIKER FOR THE UPPER EDGE OF THE DOOR IAW EA 43-2018-083, REV A.
- [SDR A8ZR20180911004](https://openairdocs.org/sdr/A8ZR20180911004.md): Structure · dented · Jun 20, 2018 · N367PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > ACCOMPLISHED DOUBLER REPAIR AT STA 213.8 & BETWEEN S16S AND S17S FOR DENT REF EA 48-2018-042 REV ORIGINAL ISSUE DATED 06/20/2018.
- [SDR A8ZR20180830004](https://openairdocs.org/sdr/A8ZR20180830004.md): Structure · cracked · Jun 15, 2018 · N366PH · Dhav DHC8202 · Passenger/Crew Doors
  > ACCOMPLISHED REPLACEMENT ON MAIN AIRSTAIR DOOR AFT EDGE MEMBER UPPER SECTION FOR CRACKS, REF STS EA 32-2018-078 REV IR DATED 06/15/2018.
- [SDR A8ZR20180830003](https://openairdocs.org/sdr/A8ZR20180830003.md): Skin · dented · Jun 15, 2018 · N366PH · Dhav DHC8202 · Entrance Stairs
  > ACCOMPLISHED REPLACEMENT OF DOUBLER TO UPPER SKIN ON AIRSTAIR DOOR FOR DENT, REF BOMBARDIER RD 8-52-040 ISSUE 4 DATED 2014-06-05.
- [SDR A8ZR20180924001](https://openairdocs.org/sdr/A8ZR20180924001.md): Light · defective · Jun 11, 2018 · N369PH · Dhav DHC8202 · Emergency Lighting
  > RT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N DSC543-1 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.
- [SDR A8ZR20180829007](https://openairdocs.org/sdr/A8ZR20180829007.md): Skin · dented · Jun 7, 2018 · N366PH · Dhav DHC8202 · Horizontal Stabilizer, Plate/Skin
  > LEFT LOWER SURFACE OF THE HORIZONTAL STABILIZER 15.5 INCHES INBD FROM OTBD EDGE AND 6.5 INCHES FWD OF AFT EDGE WAS DENTED. ACCOMPLISHED DOUBLER REPAIR IAW EA 45-2018-074, REV IR.
- [SDR A8ZR20180828002](https://openairdocs.org/sdr/A8ZR20180828002.md): Skin · dented · Jun 7, 2018 · N366PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AT BS 240.5 BETWEEN STRINGERS 29P & 30P WAS DENTED. REPAIRED IAW EA 42-2018-040, REV A-P2.
- [SDR A8ZR20180911001](https://openairdocs.org/sdr/A8ZR20180911001.md): Tail Cone · delaminated · Jun 6, 2018 · N367PH · Dhav DHC8202 · Aerodynamic Fairings
  > ACCOMPLISHED COMPOSITE REPAIR ON LWR TAILCONE FWD AT TAIL BUMPER FOR DELAMINATION STA X806 & Z130.43 REF SRM 53-70-28 REV 6 DATED SEP 17, 2017.
- [SDR A8ZR20180829004](https://openairdocs.org/sdr/A8ZR20180829004.md): Skin · dented · Jun 6, 2018 · N366PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > BS 293 TO 321.85, STRINGER 24S WAS DENTED. ACCOMPLISHED A DOUBLER AND TRIPLER REPAIR IAW EA 42-2018-041, REV B.
- [SDR 2018FA0000170](https://openairdocs.org/sdr/2018FA0000170.md): Generator · failed · May 30, 2018 · N646CC · Dhav DHC8202 · DC Generating System
  > NR 1 GENERATOR FAILURE, CYCLING ON AND OFF. CAUSED MULTIPLE SYSTEM FAILURES, TO INCLUDE AUTO PRESSURIZATION SYSTEM FAILURE. THE NR 1 DC GENERATOR LIGHT ILLUMINATED WITH AUX INVERTER LIGHT. LEFT STALL WARNING LIGHT ILLUMINATED INTERMITTENTLY. AUTOPILOT DISCON
- [SDR A8ZR20180829006](https://openairdocs.org/sdr/A8ZR20180829006.md): Skin · dented · May 29, 2018 · N366PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > SKIN DENTED AT BS 321.6, STRINGER 24S-3.5, SUCCESSFULLY REFORMED BACK TO ORIGINAL CONTOUR WITH NO INDICATIONS FOR CRACKS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-041, REV B.
- [SDR A8ZR20180829005](https://openairdocs.org/sdr/A8ZR20180829005.md): Skin · dented · May 29, 2018 · N366PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > SKIN DENTED AT BS 307.5, STRINGER 26S+1.60/ SUCCESSFULLY REFORMED BACK TO ORIGINAL CONTOUR WITH NO INDICATIONS FOR CRACKS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-041, REV B.
- [SDR A8ZR20180829009](https://openairdocs.org/sdr/A8ZR20180829009.md): Skin · dented · May 25, 2018 · N366PH · Dhav DHC8202 · Aileron Tabs
  > SKIN PANEL DENTED ON THE RT AILERON TRIM TAB. REPAIRED IAW SRM 51-42-45.
- [SDR A8ZR20180829008](https://openairdocs.org/sdr/A8ZR20180829008.md): Skin · dented · May 22, 2018 · N366PH · Dhav DHC8202 · Elevator, Plate/Skin
  > ACCOMPLISHED A SKIN REPLACEMENT AND SPLICE 10.8 INCH X 1.70 INCH ON THE RT ELEVATOR SPRING TAB UPPER SURFACE, 2.5 INCHES INBD OF HINGE NR 2, 2.8 INCHES FWD OF THE T/E IAW RD 8-55-037, ISSUE 6.
- [SDR A8ZR20180827002](https://openairdocs.org/sdr/A8ZR20180827002.md): Skin · dented · May 21, 2018 · N366PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > THREE DENTS ON THE FUSELAGE AT BS 111.5 & 121.8 AND STRINGERS 21P & 22P. REFORMED TO ORIGINAL CONTOUR, CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 43-2018-066, REV IR.
- [SDR JJBA2018061910007](https://openairdocs.org/sdr/JJBA2018061910007.md): Wire · out of position · May 10, 2018 · N365PH · Dhav DHC8202 · Light System Wiring
  > LEFT EMERGENCY EXIT FORWARD EMERGENCY LIGHT WAS UNSERVICEABLE. TROUBLESHOT AND FOUND WIRES IN CONNECTORS J12 ON SIDEWALL PANEL SWAPPED. SWAPPED WIRES BACK. OPS CHECKED SATISFACTORY.
- [SDR A8ZR201808290010](https://openairdocs.org/sdr/A8ZR201808290010.md): Skin · dented · May 9, 2018 · N366PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT BS 295, STRINGER 31S+2.8 INCHES DENTED. REPAIRED IAW EA 45-2018-067, REV ORIGINAL.
- [SDR A8ZR20180830002](https://openairdocs.org/sdr/A8ZR20180830002.md): Skin · dented · May 7, 2018 · N366PH · Dhav DHC8202 · Ailerons
  > ACCOMPLISHED DOUBLER REPAIR ON L/H AILERON UPPER SURFACE AT YW 474 & 4.7" FWD OF TRIM TAB AND YW 476 & 1" TO 6" FWD OF TRIM TAB FOR MULTIPLE DENTS REF DEHAVILLAND SRM 57-60-21 REV 6 DATED SEPTEMBER 15, 2017
- [SDR A8ZR20180821002](https://openairdocs.org/sdr/A8ZR20180821002.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE AT STA 328.5 & S13P+6" THAT MEASURES.50"L X.9"W X.006"D SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR WITH NO OFFSETS TO MATERIAL THICKNESS. CONSIDRERED ACCEPTABLE REF STS EA 42-2018-055 REV B DATED 04/19/2018.

Next page: https://openairdocs.org/model/bombardier-dhc-8-202/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 = 'DHC8202'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bombardier-dhc-8-202/reports

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