N358PH, cancelled Jan 28, 2019

Service difficulty reports · 429

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N358PH' AND deregistration_id = 'N358PH-2019-01-28'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR A8ZR20180817001Skin · dentedDENT FOUND AT BS331, STRINGER 31L. REFORMED THE DENT AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-061, REV. A.Aug 11, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180823007Striker · out of limitsACCOMPLISHED 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.Jun 27, 2018 · N358PH · Dhav DHC8202 · Nacelle/Pylon, Main FrameSDR A8ZR20180821002Skin · dentedDENT 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.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180821005Skin · dentedDENT ON FUSELAGE AT BS 330 & S13P+3. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055 REV B.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180821003Skin · dentedDENT ON FUSELAGE AT STA 327.5 & S13P+8.5" THAT MEASURES .90"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.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180821004Skin · dentedDENT ON FUSELAGE AT BS 332 & S11P+6.25. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055 REV B.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820012Skin · dentedSKIN DENTED AT BS 331.5, STRINGER 16P. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055, REV B.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820009Skin · dentedFUSELAGE SKIN DENTED AT BS 330.5, STRINGER 11P. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW 42-2018-055, REV B.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820008Skin · dentedFUSELAGE SKIN DENTED, BS 328, STRINGER 11P. REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055, REV B.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180809001Skin · dentedFUSELAGE SKIN AT BS 328, STRINGER 11L WAS FOUND DENTED. COLD WORKED TO ORIGINAL CONTOUR AND ACCOMPLISHED NDT WITH NO CRACKS NOTED IAW EA 42-2018-055, REV B.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820010Skin · dentedSKIN DENTED AT BS 332, STRINGER 11P. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055 REV B.May 4, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820011Skin · dentedFUSELAGE SKIN DENTED AT BS 329, STRINGER 16P. ACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER IAW EA 42-2018-055 REV B.May 3, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180822004Skin · dentedDENT AT BS 313.5, STRINGER 25S-1.15" THAT MEASURES 1.0"L X .85"W X .011"D REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING AND CONSIDERED ACCEPTABLE IAW EA 41-2018-045 REV B.May 2, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180822001Skin · dentedDENT FOUND AT BS 310, STRINGER 25S -1.5, MEASURES .70 L X .65 W X .004 D. REFORMED TO OROGONAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING CONSIDERED ACCEPTABLE IAW EA 42-2018-045, REV B.May 2, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180822003Skin · dentedDENT AT BS 311.25, STRINGERS 24R & 25R. REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING AND CONSIDERED ACCEPTABLEREF STS EA 41-2018-045 REV B.May 2, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180821006Skin · damagedACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER ON MAIN CABIN DOOR UPPER SECTION FOR DENTS 4.75" BELOW UPPER EDGE AND 5.75" FWD OF AFT EDGE AND MAIN CABIN DOOR FWD EDGE & 11.5" BELOW UPPER EDGE REF STS EA 42-2018-056 REV A DATED 04/30/2018.May 2, 2018 · N358PH · Dhav DHC8202 · Passenger/Crew DoorsSDR A8ZR20180827001Skin · dentedFUSELAGE SKIN DENTED AT BS 102.2, STRINGER 24P. REFORMED AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-044, REV A.Apr 25, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820007Skin · dentedDENT FOUND ON THE CROWN SKIN, BS 325, 2L+4. REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020, REV A.Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820006Skin · dentedDENT FOUND ON THE CROWN SKIN AT BS 317.50, STRINGER 2P+5.25. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020 REV A DATED 04/19/2018.Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820003Skin · dentedFUSELAGE SKIN DENTED AT BS 301.5, S2P+7. ACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER IAW EA 42-2018-053.Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820005Skin · dentedDENT FOUND ON THE CROWN FUSELAGE SKIN AT BS 311.75, STRINGER 3L +1.35. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020, REV A.Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820004Skin · dentedFUSELAGE SKIN CROWN DENTED AT BS 307.5, STRINGER 2+3.5. REFORMED TO ORIGINAL CONTOUR IAW 42-2018-053, REV A.Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180820002Skin · dentedDENT ON THE CROWN FUSELAGE SKIN AT BS 318.25, STRINGER 2L -4" REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-053 REV A.Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180821007Skin · dentedDENT ON FUSELAGE AT BS 215.5 & S11P THAT MEASURES 4.50"L X 3.30"W X .009"D SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR WITH REMAINING MATERIAL THICKNESS OF 030" AND .031" CONSIDERED ACCEPTABLE REF EA 42-2018-059 REV A .Apr 20, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180823003Skin · dentedDENT FOUND ON THE RT WING LOWER SURFACE AT YW 88.600 & 2 INCHES AFT OF REAR SPAR THAT MEASURES 1.625"L X 1.25"W X .056"D. REFORMED TO NEW MEASUREMENT OF 1.60"L X 1.25"W X .045"D CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-052, REV ORIGINAL.Apr 19, 2018 · N358PH · Dhav DHC8202 · Wing, Plate/SkinSDR A8ZR20180820001Skin · dentedDENT WAS FOUND AT BS 418.25, STRINGER 31L. REFORMED TO ORIGINAL CONTOUR IAW EA 32-2018-050, REV B.Apr 19, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180817005Skin · dentedDENT FOUND AT BS 414.5, STRINGER 31L-3. REFORMED TO ORIGINAL CONTOUR IAW EA 32-2018-050, REV B.Apr 19, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180817004Skin · dentedFUSELAGE SKIN DENTED AT BS 408.5, STRINGER 31P. ACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER IAW EA 32-2018-050, REV B.Apr 19, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180823002Skin · dentedFUSELAGE SKIN DENTED AT BS 753.9, BETWEEN STRINGERS 12P AND 13P. REPAIRED IAW EA 42-2018-063, REV ORIGINAL.Apr 17, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180823005Skin · dentedA DENT WAS FOUND ON THE NR 2 LOWER NACELLE SKIN AT XN 177.0 JUST ABOVE THE SKIN DOUBLER REPAIR THAT MEASURES 1.5"L X .75"W X .050"D. REFORMED TO NEW MEASUREMENT OF 1.7"L X 1.7"W X .011"D WITH NO CRACKS NOTED AND MATERIAL OFFSET TO COMPLY WITH SRM 54-00-16, ALApr 13, 2018 · N358PH · Dhav DHC8202 · Nacelle/Pylon, Plate/SkinSDR A8ZR20180823008Panel · tornACCOMPLISHED INSTALLATION OF INTERNAL DOUBLER AND FILLER, OF TORN METAL ON FUSELAGE AT PANEL 112BR CUTOUT THAT MEASURES 1.32"L X .56"W, IAW EA 45-2018-034 REV ORIGINAL.Apr 9, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, StructureSDR A8ZR20180823001Skin · dentedDENT AT BS 413, STRINGER 15P-3 THAT MEASURES 8.4"L X 3.0"W X .013"D REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING AND CONSIDERED ACCEPTABLE IAW EA 30-2018-048 REV A.Apr 9, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180817002Skin · dentedDENT FOUND AT BS 340 & STRINGER 31L. REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-061, REV A.Apr 4, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR A8ZR20180823004Shroud · damagedRIGHT UPPER SHROUD PANEL T/E AT APPROX. YW377 WAS DAMAGED. TRIMMED OUT DAMAGE AND PERFORMED TAP TEST WITH NO DEFECTS NOTED.Mar 27, 2018 · N358PH · Dhav DHC8202 · Wing Miscellaneous StructureSDR A8ZR20180823006Inlet · chafedNR 2 ENGINE, LT FRONT INLET CASE HAD CHAFE DAMAGE OF .053 INCH IN DEPTH. HAS BEEN DETERMINED THAT THE ENGINE CONTINUES TO COMPLY WITH ITS CERTIFICATION BASIS AND IS IN A SERVICEABLE CONDITION FOR CONTINUED OPERATION SUBJECT TO PERFORM MAINTENANCE NECESSARY TOMar 8, 2018 · N358PH · Dhav DHC8202 · Turbine Engine Air Inlet SectionSDR JJBA20170607006Connector · unsecureFWD CEILING EMERGENCY LIGHT OVER AISLE INOPERATIVE. SECURED FWD OVERHEAD EMERGENCY EXIT SIGN LIGHT CONNECTOR PLUG 9811-P181. OPS CHECKED GOOD.Jun 7, 2017 · N358PH · Dhav DHC8202 · Light System WiringSDR JJBA20170503003Cover · unsecureEMERGENCY EXIT HANDLE COVER AT SEAT 18A LOOSE. SECURED THE EMERGENCY EXIT HANDLE COVER AS REQUIRED.May 3, 2017 · N358PH · Dhav DHC8202 · Emergency ExitsSDR JJBA20170404004Light · unknownFRONT SERVICE DOOR EMERGENCY LIGHTS FLICKERED. PERFORMED EXTENSIVE OPS CHECK OF EMERGENCY LIGHTS, OPS TEST GOOD. NO DEFECTS NOTED AT THIS TIME.Apr 4, 2017 · N358PH · Dhav DHC8202 · Emergency LightingSDR JJBA20170302003Bushing · wornFORE RUDDER HAS DROPPED, RUDDER HINGES AND VERTICAL STABILIZER REAR SPAR HINGES FITS AND CLEARANCE GAPS NOT WITHIN ALLOWABLE ACCEPTABLE LIMITATIONS OUTLINED IN AMM 55-40-11. TOP AND BOTTOM FORE RUDDER FAILSAFE HINGES ZERO GAP. HINGE PIVOTING ON HINGE, METAL Feb 25, 2017 · N358PH · Dhav DHC8202 · Rudder StructureSDR JJBA20170302002Support Bracket · crackedCARGO DOOR FWD TRACK LOWER SUPPORT BRACKET CRACKED. THE SUPPORT BRACKET WAS REPLACED.Feb 25, 2017 · N358PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR JJBA20170302001Bracket · chafedFORE RUDDER TOP HINGE BRACKET HAS WEAR CHAFE DAMAGE ON TOP OF BRACKET UNDER BOLT HEAD ATTACHMENT. REPAIRED IAW RD 8-55-1128.Feb 24, 2017 · N358PH · Dhav DHC8202 · Rudder StructureSDR JJBA20161115018Connector · dirtyFWD EMERGENCY LOWER HORIZONTAL LIGHT FLICKERS IN FLIGHT. CLEANED CONNECTION OPS CHECKED GOOD ON GROUND, NO DEFECTS NOTED.Nov 15, 2016 · N358PH · Dhav DHC8202 · Light System WiringSDR JJBA20160809007Wire · disconnectedSPOILER NR 1, NR 2 ILLUMINATED ON TAKEOFF. INSP FOUND WIRES IN THE MICROSWITCH DISCONNECTED. RECONNECTED AND SPLICED WIRES. OPS CK SAT NO DEFECTS NOTED AT THIS TIME.Aug 9, 2016 · N358PH · Dhav DHC8202 · Flight Control System WiringSDR JJBA20160720004Hydraulic System · lowPOSSIBLE HYD LEAK NR 1 HYD SYS. QTY DROPPED FROM 1.9 TO 0.9 IN FLIGHT. SERVICED NR 1 HYD SYSTEM TO 2 QUARTS. PERFORMED ENGINE RUNS IAW 71-00-00 PERFORMED CYCLING TEST OF HYDRAULIC SYSTEM NO LEAKS NOTED. OPS CHECK SAT.Jul 20, 2016 · N358PH · Dhav DHC8202 · Hydraulic System, MainSDR JJBA20160712003Tscu · inoperativeNR 2 ENGINE FEATHERED UNCOMMANDED. POWER UPTRIM ILLUMINATED. WHEN THE POWER WAS RETARDED THE PROP UNFEATHERED. WITH THE SYS DESELECTED, OFF AND POWER APPLIED THE ENGINE/PROP OPERATE NORMALLY. DEFERRED IAW MEL. R&R TSCU. OPS CHECK SAT. MEL CLOSED.Jul 12, 2016 · N358PH · Dhav DHC8202 · Engine BMEP/Torque IndicatingSDR JJBA20160622010Seal · out of positionINNER WINDOW SEAL POPPED OUT AT 4AB INFLIGHT. SECURED WINDOW PANE, NO OTHER DEFECTS.Jun 22, 2016 · N358PH · Dhav DHC8202 · Passenger Compartment WindowsSDR JJBA20160304002Sign · inoperativeEMERGENCY EXIT SIGN BY FLIGHT ATTENDANT JUMP SEAT WILL NOT ILLUMINATE. R & R EMER EXIT SIGN, PN 2LA007344-80.Mar 4, 2016 · N358PH · Dhav DHC8202 · Emergency LightingSDR JJBA20151104004Seat Track · corrodedMULTIPLE SPOTS OF CORROSION ON THE RT SEAT RAIL & DRIP TRAY FROM FS 180-234.5. REPLACED RT SEAT RAIL IAW RD 8-53-3074.Nov 4, 2015 · N358PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR JJBA20151104003Seat Track · corrodedMULTIPLE SPOTS OF CORROSION ON THE LT SEAT RAIL & DRIP TRAY FROM FS 180-234.5. REPLACED LT SEAT RAIL IAW RD 8-53-3074.Nov 4, 2015 · N358PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR JJBA20150425011Smoke Detector · faultyCARGO SMOKE WARNING LIGHT FLASHED. R & R FWD & AFT BAGGAGE SMOKE DETECTORS.Apr 25, 2015 · N358PH · Dhav DHC8202 · Smoke Detection
Back to N358PH, cancelled Jan 28, 2019