# Service difficulty reports: Dehavilland DHC-2 MK.I A list on [Dehavilland DHC-2 MK.I](https://openairdocs.org/model/dehavilland-dhc-2-mk-i.md). Newest first. General aviation reporting is voluntary. Page 1 of 5 · 206 reports - [SDR 2024F00194](https://openairdocs.org/sdr/2024F00194.md): Exhaust Valve · none · Aug 2, 2024 · N4444Z · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > PILOT REPORTED: NORMAL: WEIGHT AND BALANCE CHECK, PREFLIGHT, FUELING (35 FRNT 35 CTR 05 REAR) PAX LOADING/BRIEFING, TAXI FOR SE DEPART, AND RUN UP. PREFLIGHT CHECKLIST: FUEL SELECTOR CTR TANK, FLAPS AND TRIM SET TO TAKEOFF, WATER RUDDERS RETRACTED, CARB HEAT - [SDR ERHA20190805144](https://openairdocs.org/sdr/ERHA20190805144.md): Mount Bracket · deformed · Jul 24, 2019 · N2740X · Dhav DHC2MKI · Main Landing Gear > MOUNT BRACKET HAS ELONGATION OF ALL ATTACHMENT HOLES. AND EXHIBITS CORROSION. - [SDR CA160308007](https://openairdocs.org/sdr/CA160308007.md): Fitting · corroded · Mar 4, 2016 · Dhav DHC2MKI · Wheel/Ski/Float > (CAN) LEFT UPPER FLOAT FITTING FOUND CORRODED. NEW PART FITTED TO AIRCRAFT. - [SDR CA160219011](https://openairdocs.org/sdr/CA160219011.md): Block · loose · Feb 16, 2016 · Dhav DHC2MKI · Electrical Power System Wiring > (CAN) ALTERNATOR FAIL DISCOVERED IN FLIGHT, UPON FURTHER INVESTIGATION OF THE PART, THE ALTERNATOR TERMINAL BLOCK WAS FOUND LOOSE CAUSING A SHORT INTERNALLY. - [SDR CA160219010](https://openairdocs.org/sdr/CA160219010.md): Wire · chafed · Feb 13, 2016 · Dhav DHC2MKI · Electrical Power System Wiring > (CAN) WIRING COMING OUT OF CASING TO ALTERNATOR TERMINAL BLOCK CHAFFED, CAUSING A SHORT. - [SDR CA160119020](https://openairdocs.org/sdr/CA160119020.md): Torque Tube · cracked · Jan 8, 2016 · Dhav DHC2MKI · Rudder Control System > (CAN) AFTER WATER LANDING PILOT EXPERIENCED LOSS OF WATER RUDDER STEERING CONTROL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE TORQUE TUBE WHICH CONTROLS THE WATER RUDDER/TAIL WHEEL STEERING HAD SUFFERED A TORSIONAL SHEAR ACROSS THE TUBES DIAMETER AT ITS - [SDR CA151217008](https://openairdocs.org/sdr/CA151217008.md): Frame · failed · Dec 15, 2015 · Dhav DHC2MKI · Fuselage Internal Mounting Structure > (CAN) THE "BIRD CAGE" TUBING WAS ULTRASONICALLY TESTED. FAILURE IN 7 AREAS. - [SDR CA151013014](https://openairdocs.org/sdr/CA151013014.md): Main Bearing · failed · Oct 8, 2015 · Dhav DHC2MKI · Reciprocating Engine Power Section > (CAN) UNKNOWN TYPE OF METAL FOUND IN THE OIL FILTER SCREEN. ENGINE SENT FOR OVERHAUL. REAR MAIN BEARING FAILED. - [SDR CA151030020](https://openairdocs.org/sdr/CA151030020.md): Cylinder · failed · Oct 1, 2015 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) DURING INSPECTION FOUND FOUR FAILED STUDS ON NR 3 CYLINDER ASSEMBLY. ALSO CRACK WAS SEEN ON FRONT CRANK CASE ADJACENT TO THE CYLINDER. - [SDR CA150826006](https://openairdocs.org/sdr/CA150826006.md): Retainer · damaged · Aug 12, 2015 · Dhav DHC2MKI · Fuel Storage > (CAN) DURING MAINTENANCE THERE WAS EVIDENCE THE UPPER TANK COVER GASKETS P/N C2PT529-27 WERE LEAKING. THIS AIRCRAFT HAS MOD 2/1376 INSTALLED TO INTRODUCE RUBBER FUEL TANK LINERS. THE GASKETS WERE REPLACED AND THE TANK FILLED WITH FUEL. THE TANK STILL LEAKED BE - [SDR 2015FA0000363](https://openairdocs.org/sdr/2015FA0000363.md): Cylinder · split · Aug 4, 2015 · N6LU · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > ON AN EMPTY FLIGHT RETURNING TO BASE, APPROXIMATELY 20 MINUTES OUT OF DESTINATION AT 1500' THE ENGINE SUDDENLY BEGAN RUNNING ROUGH. THE PILOT AFTER CHECKING FUEL, MAGS & CARB HEAT CLIMBED TO 3000' & CONTINUED TOWARDS DESTINATION. THE PILOT CONTACTED THE OFFI - [SDR CA150626008](https://openairdocs.org/sdr/CA150626008.md): Skin · cracked · Jun 26, 2015 · Dhav DHC2MKI · Elevator, Plate/Skin > (CAN) CRACK OF 7 INCHES FOUND ON THE OUTBOARD TIP AREA OF THE RIGHT ELEVATOR DURING THE PILOTS PREFLIGHT INSPECTION BEFORE THE FIRST FLIGHT OF THE DAY. ELEVATOR ASSEMBLY REPLACED. - [SDR CA150520011](https://openairdocs.org/sdr/CA150520011.md): Drive Gear · failed · May 15, 2015 · Dhav DHC2MKI · Magneto/Distributor > (CAN) DURING THE SECOND GROUND RUN ON AN O/H ENGINE, THE ENGINEER SELECTED RT MAGNETO, THE ENGINE RPM DECAYED, AND WAS FOLLOWED BY A LOUD BACKFIRE. THE ENGINEER SELECTED BOTH MAGNETOS AND THEN SHUT ENGINE DOWN. AFTER AN INSPECTION, THE RT INTERNAL DRIVE GEAR - [SDR CA150520012](https://openairdocs.org/sdr/CA150520012.md): Cylinder Head · cracked · May 5, 2015 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) CYLINDER HEAD CRACK AND SUBSEQUENT PARTIAL SEPARATION. - [SDR CA150526009](https://openairdocs.org/sdr/CA150526009.md): Shaft · cracked · Apr 29, 2015 · Dhav DHC2MKI · Power Lever > (CAN) THE THROTTLE LAY SHAFT ASSEMBLY MUST HAVE CORRECTED FROM THE INSIDE OUT & CAUSED STRESS CRACKS TO APPEAR IN THE SHAFT. IF THIS HAD CONTINUED UNATTENDED IT COULD HAVE BROKEN & CAUSED THE THROTTLE TO GET STUCK ON THAT POWER SETTING. - [SDR CA150408034](https://openairdocs.org/sdr/CA150408034.md): Balance Weight · loose · Apr 3, 2015 · Dhav DHC2MKI · Reciprocating Engine Power Section > (CAN) DURING A REGULARLY SCHEDULED INSPECTION TO REMOVE A CYLINDER & INSPECT THE POWER SECTION, IT WAS NOTICED THAT THE DYNAMIC BALANCE WEIGHTS HAD AN ALMOST.025 GAP WHICH WAS ABLE TO BE PRIED OPEN TO.060. THE LEADING BOLT COULD BE SPUN INDEPENDENTLY OF THE - [SDR CA150327018](https://openairdocs.org/sdr/CA150327018.md): Bracket · cracked · Mar 27, 2015 · Dhav DHC2MKI · Elevator Structure > (CAN) THE FORWARD MOST ELEVATOR STOP BRACKET IS INSTALLED ON THE LEFT, LOWER, LONGITUDINAL RUNNING TUBE OF THE FORWARD FUSELAGE FRAME STRUCTURE. UPON REMOVING CORROSION AND INSPECTION OF THE ENTIRE FRAME STRUCTURE, THE BRACKET WAS FOUND CRACKED AT THE BASE OF - [SDR CA150211008](https://openairdocs.org/sdr/CA150211008.md): Guide · broken · Feb 10, 2015 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) DURING AN INSPECTION FOR METAL CONTAMINATION FOUND AT A SCHEDULED INSPECTION, THE NR 8 CYLINDER EXHAUST VALVE GUIDE WAS FOUND TO HAVE COME LOOSE AND WAS BEING STRUCK BY THE EXHAUST VALVE. THE CYLINDER PN 399353, SN AR1476 WAS REMOVED WITH 1104.0 TSO, AN - [SDR CA141205009](https://openairdocs.org/sdr/CA141205009.md): Fuel Tank · cracked · Dec 2, 2014 · Dhav DHC2MKI · Fuel Storage > (CAN) DURING ROUTINE MAINTENANCE, A FUEL LEAK WAS NOTICED FROM THE FORWARD FUEL BAY AREA. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT AT SOME POINT A FIRE HAD OCCURRED IN THE FORWARD FUEL BAY. NO FIRE WAS REPORTED AND THE OPERATOR WAS UNAWARE OF ANY INCIDENT - [SDR CA141120011](https://openairdocs.org/sdr/CA141120011.md): Bolt · broken · Oct 27, 2014 · Dhav DHC2MKI · Vertical Stabilizer > (CAN) FIN SPAR RT MAIN ATTACH BOLT WAS FOUND TO BE BROKEN OFF. HEAD OF BOLT WAS STILL IN ATTACH FITTING NUT AND LOWER PORTION OF BOLT WERE MISSING, BOTH BOLTS REPLACED. - [SDR CA140930004](https://openairdocs.org/sdr/CA140930004.md): Volt Regulator · overheated · Sep 26, 2014 · Dhav DHC2MKI · DC Regulator > (CAN) IMMEDIATELY AFTER DEPARTING A STRONG BURNING ODOR WAS NOTICED IN THE AIRCRAFT. AIRCRAFT RETURNED TO BASE, WHERE MAINTENANCE DETERMINED THAT A RESISTER WITHIN THE VOLTAGE REGULATOR OVERHEATED AND WAS THE CAUSE OF THE ODOR. - [SDR CA140918016](https://openairdocs.org/sdr/CA140918016.md): Lift Strut · cracked · Sep 15, 2014 · Dhav DHC2MKI · Wing Main, Frame Structure > (CAN) DURING A SCHEDULED 100 HOUR INSPECTION, THE RT WING STRUT LOWER FITTING WAS FOUND CRACKED. THE LIFT STRUT WAS REPLACED WITH A SERVICEABLE STRUT TO RECTIFY THE DEFECTS. THE LIFT STRUT TSN: 16004.8. TIME SINCE EDDY CURRENT 833.3 HRS, 18 MONTHS PRIOR. (TC# - [SDR CA140916005](https://openairdocs.org/sdr/CA140916005.md): Shaft · corroded · Aug 24, 2014 · Dhav DHC2MKI · Engine Controls > (CAN) STEEL LAY SHAFT CORRODED FROM INSIDE OUT AND TORSION OF THROTTLE CONTROL ARMS CRACKED SHAFT. - [SDR CA141001001](https://openairdocs.org/sdr/CA141001001.md): Connecting Rod · failed · Aug 12, 2014 · Dhav DHC2MKI · Reciprocating Engine Power Section > (CAN) DURING CRUISE, THE ENGINE HAD HIGH VIBRATIONS FOR COUPLE OF SECONDS AND THEN THE ENGINE STOPS SUDDENLY. THE PILOT DID AN EMERGENCY LANDING. THE AME`S FOUND THE CYLINDER NR 5 BEEN PUNCTURED BY CONNECTING ROD. ENGINE OVERHAUL SHOP ACKNOWLEDGED THE PROBA - [SDR CA140724002](https://openairdocs.org/sdr/CA140724002.md): Cylinder · cracked · Jul 23, 2014 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) DURING SCHEDULED 100 HR INSPECTION, BROKEN OFF A PIECE OF CYLINDER NR 9 FOUND RESTING IN LOWER COWLING, FURTHER INVESTIGATION FOUND THE UPPER COWLING MOUNT BRACKET C/W REMAINING/BROKEN PIECE OF CYLINDER STILL ATTACHED IN COWL. CYLINDER NR 9 PUSH ROD HOU - [SDR CA140303021](https://openairdocs.org/sdr/CA140303021.md): Rib · cracked · Mar 3, 2014 · Dhav DHC2MKI · Wing, Rib/Bulkhead > (CAN) DURING DISASSEMBLY TO REPAIR A WING DUE TO EARLIER DAMAGE, THE RIB AT 136.5 WAS FOUND CRACKED AT THE TOP FLANGE. THE RIB WAS CRACKED IN AN AREA OF THE WING THAT WAS NOT DISTURBED BY THE PREVIOUS DAMAGE. THE RIB WAS REPLACED WITH A SERVICEABLE RIB TO REC - [SDR CA141030008](https://openairdocs.org/sdr/CA141030008.md): Frame · corroded · Feb 25, 2014 · Dhav DHC2MKI · Fuselage Main, Frame > (CAN) DURING MODIFICATION TO THE FWD FUSELAGE FRAME "BIRDCAGE" IAW STC SA97-88, A LOT OF CORROSION HAS BEEN VISUALLY DISCOVERED ON THE LOWER TUBES. IT HAS BEEN DETERMINED THAT IT WOULD BE CHEAPER AND FASTER TO CHANGE THE BIRDCAGE RATHER THAN REPAIR IT. THIS - [SDR CA140211013](https://openairdocs.org/sdr/CA140211013.md): Cotter Pin · failed · Feb 7, 2014 · Dhav DHC2MKI · AC Inverter > (CAN) COTTER PIN HOLDING NUT ON TO GEAR DRIVE FAILED. - [SDR CA140115007](https://openairdocs.org/sdr/CA140115007.md): Cylinder Head · separated · Jan 12, 2014 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) DURING CRUISE, THERE WAS A LOUD BANG FROM THE ENGINE AND THE ACFT LOST POWER. PILOT EXECUTED A FORCED LANDING. UPON INSPECTION, MAINTENANCE FOUND THAT THE HEAD WAS CRACKED ON THE NR 9 CYLINDER. ENGINE TSO AT TIME OF INCIDENT WAS 275.9. - [SDR CA140113013](https://openairdocs.org/sdr/CA140113013.md): Tube · cracked · Jan 10, 2014 · Dhav DHC2MKI · Fuselage Main, Structure > (CAN) DURING A SCHEDULED 100 HR INSPECTION, THE FORWARD LT DIAGONAL TUBE OF THE FWD TUBULAR STRUCTURE WAS FOUND CRACKED DUE TO INTERNAL CORROSION. THE DAMAGED TUBE WAS CUT OUT AND THE STRUCTURE WAS REPAIRED TO RECTIFY THE DEFECT. THE REPAIRED AREA WAS PREPPE - [SDR CA131016001](https://openairdocs.org/sdr/CA131016001.md): Seat · worn · Oct 10, 2013 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) EXCESSIVE WEAR OF EXHAUST SEAT WAS NOTED IN 109 HRS OF TOTAL OPERATION. THE VALVE WAS ADJUSTED TWICE IN THE SPAN OF OPERATION BEFORE THE CYLINDER ASSY WAS REMOVED FROM SERVICE. EXHAUST VALVE SEAT WEAR IS APPROXIMATELY.175. ALL REMAINING CYLINDERS ON T - [SDR CA131004002](https://openairdocs.org/sdr/CA131004002.md): Control Cable · separated · Sep 26, 2013 · Dhav DHC2MKI · Rudder Tab Control System > (CAN) CURSORY/ROUTINE INSP IN THE AFT FUSELAGE REVEALED A NON-STANDARD, RUDDER TRIM CABLE. AFT RUDDER TRIM CABLE WAS FOUND, SPLICED WITH NICOPRESS SLEEVES AND THIMBLES. HAND MOVEMENT OF THE CABLE CAUSED THE.0625 CABLE TO SLIDE OUT OF THE INCORRECTLY SWAGED N - [SDR CA130916002](https://openairdocs.org/sdr/CA130916002.md): Cylinder Head · cracked · Sep 13, 2013 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) CYLINDER HEAD FOUND CRACKED 1.5" ABOVE THE HEAD AND BARREL JOINING POINT. - [SDR CA130821002](https://openairdocs.org/sdr/CA130821002.md): Bracket · cracked · Aug 19, 2013 · Dhav DHC2MKI · Fuselage Miscellaneous Structure > (CAN) PILOT NOTICED WINDSHIELD MOVING, CONTACTED MAINTENANCE AND AFTER INSPECTION FOUND WINDSHIELD BRACKET CRACKED. - [SDR CA130820008](https://openairdocs.org/sdr/CA130820008.md): Exhaust Valve · leaking · Aug 15, 2013 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) DURING A SCHEDULED INSPECTION, THE CYLINDER LEAK CHECK SHOWED 0/80 ON CYLINDER NR 3. INVESTIGATION FOUND THAT THE EXHAUST VALVE WAS BEING HELD OPEN. FURTHER INVESTIGATION SHOWED THAT THE EXHAUST VALVE SEAT WAS EXCESSIVELY WORN. THE CYLINDER WAS REPLAC - [SDR CA130815015](https://openairdocs.org/sdr/CA130815015.md): Fitting · cracked · Aug 15, 2013 · Dhav DHC2MKI · Wheel/Ski/Float > (CAN) DURING A SCHEDULED 100 HR INSPECTION, THE RT FWD FLOAT FITTING, PN 58S926R WAS FOUND BADLY CORRODED AND CRACKED AT BOTH LOWER ATTACHMENT HOLES. THE FLOAT FITTING WAS REPLACED WITH A NEW FITTING TO RECTIFY THE DEFECT. - [SDR CA130815002](https://openairdocs.org/sdr/CA130815002.md): Link · failed · Aug 15, 2013 · Dhav DHC2MKI · Elevator Tab Control System > (CAN) DURING PRE-FLIGHT/COCKPIT CHECK, PILOT NOTICE THAT THE CONTROL COLUMN WAS NOT AS FAVOR TO TRAVEL AS IS NORMAL. MAINTENANCE CALLED TO INVESTIGATE INSPECTION OF ELEVATOR CONTROL SYS. FOUND ELEVATOR/TRIM LINKAGE DRY/TIGHT. IPC FIG 10, ITEM 37, 38, 43. BO - [SDR CA130718003](https://openairdocs.org/sdr/CA130718003.md): G Switch · failed · Jul 9, 2013 · Dhav DHC2MKI · Emergency Locator Beacon > (CAN) ELT G-SWITCH FAILED TO OPERATE DURING FUNCTION CHECK. G-SWITCH REPLACED. - [SDR CA130717007](https://openairdocs.org/sdr/CA130717007.md): Rod · broken · Jul 8, 2013 · Dhav DHC2MKI · Elevator Tab Control System > (CAN) PILOT REPORTED HEARING A POP WHEN SETTING HIS ELEVATOR TRIM FOR CRUISE AND THEN CONTROL COLUMN VIBRATING. THE PILOT THEN CONTACT MAINTENANCE OF THE SITUATION THAT HE WAS FOUR MINUTES OUT AND THAT HE STILL HAD FULL CONTROL OF THE AIRCRAFT. THE PILOT LANDE - [SDR CA140916006](https://openairdocs.org/sdr/CA140916006.md): Battery · discharged · Jul 5, 2013 · Dhav DHC2MKI · Emergency Locator Beacon > (CAN) BATTERY REPLACED AFTER YEAR 1, (SUPPOSED TO BE A 5 YEAR LITHIUM BATTERY) G SWITCH FAILURE 3 TIMES IN 4 YEARS. UNIT HAS BEEN REPLACED WITH ACK 406MHZ ELT. (TC# 20140916006) - [SDR CA130626011](https://openairdocs.org/sdr/CA130626011.md): Crankshaft · sheared · Jun 24, 2013 · Dhav DHC2MKI · Reciprocating Engine Power Section > (CAN) WHILE ON A RETURN FLIGHT FROM TOBA INLET AND DESCENDING THROUGH 2000 FEET THE ENGINE STARTED TO SHAKE VIOLENTLY. THE VIBRATION WAS TO THE POINT WHERE THE PILOT HAD TO MAKE AN EMERGENCY LANDING IN HALF MOON BAY. THE POWER SETTING WAS PULLED BACK TO IDLE A - [SDR CA130606009](https://openairdocs.org/sdr/CA130606009.md): Plug · unsecure · Jun 4, 2013 · Dhav DHC2MKI · Turbine Engine Oil System > (CAN) ENGINE OIL PLUG NOT TIGHTENED, OIL LEAKED FROM SUMP CAUSING ENGINE DAMAGE AND UNSCHEDULED LANDING. - [SDR CA130604004](https://openairdocs.org/sdr/CA130604004.md): Cylinder Head · leaking · Jun 3, 2013 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) LEAKAGE/SEEPING OBSERVED ON CYLINDER NR 6 AT CYLINDER HEAD TO BARREL JOINT. - ENGINE PERFORMANCE/OPERATION OTHERWISW NORMAL. - CYLINDER ASSY REPLACED AS A PRECAUTION. - [SDR CA130603013](https://openairdocs.org/sdr/CA130603013.md): Gear · failed · Jun 1, 2013 · Dhav DHC2MKI · Magneto/Distributor > (CAN) PHENOLIC INTERNAL GEAR STRIPPED INSIDE MAGNETO. - [SDR CA130422008](https://openairdocs.org/sdr/CA130422008.md): Bolt · broken · Apr 22, 2013 · Dhav DHC2MKI · Fuselage Main, Attach Fittings > (CAN) HORIZONTAL STABILIZER ATTACHMENT BRACKETS, PN C2-TP-160, DURING A ROUTINE 100 HR INSPECTION, IT WAS FOUND THAT THE RT STABILIZER ATTACHMENT BRACKET C2-TP-160 HAD 2 OF THE 3 ATTACHMENT BOLTS, PN NAS144-14, NUTS MS21042 WERE SPLIT IN HALF AND RESTED BELOW - [SDR CA130418004](https://openairdocs.org/sdr/CA130418004.md): Bolt · loose · Apr 12, 2013 · Dhav DHC2MKI · Fuel Control/Reciprocating Engines > (CAN) ENGINE BEGAN TO RUN ROUGH APPROXIMATELY 15 NM SOUTH OF CAM9 AT ALTITUDE OF 500 FT. ENGINE WAS BACKFIRING, ALL ENGINE INSTRUMENTS SHOWED THE PARAMETERS WERE IN THE GREEN, NORMAL, EXCEPT THE CARBUREATOR TEMPERATURE GUAGE WHICH INDICATED A LARGE SPIKE FOLL - [SDR CA130328012](https://openairdocs.org/sdr/CA130328012.md): Cylinder Head · separated · Mar 26, 2013 · Dhav DHC2MKI · Reciprocating Engine Cylinder Section > (CAN) DURING TAKEOFF, THE PILOT HEARD A BANG FROM THE ENGINE COMPARTMENT FOLLOWED BY AN ENGINE VIBRATION. THE PILOT ABORTED THE TAKE OFF AND TAXIED BACK TO THE FLOAT PLANE DOCK FOR INVESTIGATION. DURING INSPECTION, MAINTENANCE PERSONNEL FOUND NR 9 CYLINDER HE - [SDR CA130318025](https://openairdocs.org/sdr/CA130318025.md): Frame · misrepaired · Mar 15, 2013 · Dhav DHC2MKI · Fuselage Main, Frame > (CAN) DURING AN UNSCHEDULED FWD TUBULAR FRAME, BIRDCAGE REPLACEMENT, THE RUDDER STOPS ON THE RECEIVED REPAIRED TUBULAR STRUCTURE WERE FOUND TO HAVE BEEN WELDED.5" FWD OF THE DWG LOCATION. IT WAS ALSO NOTED THAT THE FUEL SELECTOR CABLE GUARD WAS FOUND WELDED - [SDR CA130312008](https://openairdocs.org/sdr/CA130312008.md): Bracket · cracked · Mar 11, 2013 · Dhav DHC2MKI · Mixture Control > (CAN) DURING INSPECTION, THE MIXTURE CONTROL BRACKET ATTACHED TO THE FIREWALL, PN C2C2927, WAS FOUND TO HAVE A.2500" CRACK IN THE BEND RADIUS. THE MIXTURE BRACKET WAS REPLACED WITH A SERVICEABLE BRACKET TO RECTIFY THE DEFECT. - [SDR CA130307003](https://openairdocs.org/sdr/CA130307003.md): Spar · cracked · Mar 6, 2013 · Dhav DHC2MKI · Wing Spar > (CAN) DURING INSTALLATION OF THE WIPAIRE UP GROSS KIT, A CRACK WAS FOUND IN A SECTION OF THE REAR SPAR AT WS 123.5 BEHIND THE OTBD FLAP HANGER. THE REAR SPAR SECTION, PN C2W1107 WAS R & R WITH A NEW SECTION, PN CSW1007 TO RECTIFY THE DEFECT. Next page: https://openairdocs.org/model/dehavilland-dhc-2-mk-i/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 = 'DHC2MKI' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/dehavilland-dhc-2-mk-i/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.