N424QX, cancelled Jan 17, 2013

Service difficulty reports · 374

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 = 'N424QX' AND deregistration_id = 'N424QX-2013-01-17'
  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 QXEA2012081100787Shuttle Valve · inoperativeSPONGY BRAKES. BRAKING IS EQUAL, NO PULLING LT OR RT. BLED ALL FOUR BRAKES WITH MAIN BRAKE SYSTEM IAW AMM TASK 32-42-00-870-801. DURING BLEED PROCESS, FOUND NR 2 FUSE /SHUTTLE VALVE APPEARED TO BE INOPERATIVE. REPLACED NR 2 BRAKE FUSE /SHUTTLE VALVE IAW AMAug 11, 2012 · N424QX · Bombdr DHC8402 · Landing Gear Brake SystemSDR QXEA2012072400740Transducer · malfunctionedBRAKES INEFFECTIVE ON LANDING ROLL OUT. ON POST FLIGHT FOUND NR 1 & 4 BRAKES COOL AND NR 2 & 3 HOT. R & R RT INBD WHEEL SPEED TRANSDUCER IAW AMM TASKS 32-46-11-000-801 AND 32-46-11-400-801. PERFORMED FUNCTION CHECKS IAW AMM TASK 32-46-00-720-801 AND 32-46-Jul 24, 2012 · N424QX · Bombdr DHC8401 · Landing Gear Brake SystemSDR QXEA2012071800712Light · unserviceableEMERGENCY FLOOR PATH LIGHTING STRIP AT THE CABIN ENTRY TO THE CENTER CABIN IS UNSERVICABLE. REPLACED THE FLOOR PATH LIGHTING AS REQUIRED.Jul 18, 2012 · N424QX · Bombdr DHC8401 · Emergency LightingSDR QXEA2012061700474Warning Light · false activationAP/YD DISENGAGED DURING CLIMB. AP/YD FAIL MESSAGE DISPLAYED ON BOTH PFD'S. COMPLIED WITH EMERGENCY ABNORMAL CHECKLIST. ALSO ON DESCENT "YD NOT CENTERED" MESSAGE DISPLAYED ON BOTH PFD'S. INTERROGATED CDS FCS PAGE NO ASSOCIATED FAULTS FOUND RESET CIRCUIT BREAKJun 17, 2012 · N424QX · Bombdr DHC8402 · Autopilot SystemSDR QXEA2012051600381Flap Track · wornNR 5 FLAP TRACK WAS WORN AREA IN INBD WEB. REMOVED LOOSE MATERIAL, POLISHED AND BROKE SHARP EDGES IAW RD 8/4-57-1238. REMAINING MATERIAL WITHIN LIMITS IAW RD 8/4-57-1238, COMPLIED WITH STEPS 1-6 OF RD 8/4-57-1238.May 16, 2012 · N424QX · Bombdr DHC8402 · Trailing Edge FlapsSDR QXEA2012051600382Flap Track · wornNR 4 LT FLAP TRACK HAS WORN AREA ON INBD WEB. REMOVED LOOSE MATERIAL, POLISHED AND BROKE SHARP EDGES IAW RD 8/4-57-1238. CONFIRMED CRACK FREE AREA REF 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-57-1238. COMay 16, 2012 · N424QX · Bombdr DHC8402 · Trailing Edge FlapsSDR QXEA2012010300003Bulb · inoperativeF/A EMERGENCY LIGHTING SWITCH IS BURNED OUT. RELAMPED FWD EMERGENCY SWITCH LIGHT SWITCH. LIGHTS CHECKS GOOD. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.Dec 27, 2011 · N424QX · Bombdr DHC8402 · Emergency LightingSDR QXEA2011092900917Filter · dirtyBAD "SOCK ODOR" WITH LOW POWER SETTING ON FINAL. (FROM BLEEDS). R & R RECIRCULATION FILTER IAW AMM TASK 21-22-22-000-801/400-801. NO SOCK ODOR NOTED. RETURNED TO SERVICE.Sep 24, 2011 · N424QX · Bombdr DHC8402 · Air Distribution SystemSDR QXEA2011070100475Axle · corrodedDURING THE REMOVAL OF THE NR2 BRAKE, FOUND THE NR1 AXLE TO BE CORRODED AND THE NR2 BRAKE AND WHEEL BEARING LAND. CORROSION WAS PEELING PAINT AND PITTING CORROSION. FERRIED TO REPAIR. R & R NR 1 MLG AXLE IAW 32-11-04-000-801 AND 32-11-04-400-801. RETURNED TO Jun 27, 2011 · N424QX · Bombdr DHC8402 · Main Landing Gear Strut/Axle/TruckSDR QXEA2011042500291Skin · corrodedFUSELAGE SKIN REPAIR DOUBLER, ANTENNA DOUBLER, AND ADAPTER PLATE AT LOWER TCAS ANTENNA HAVE SURFACE CORROSION. REMOVED CORROSION ON FUSELAGE SKIN REPAIR DOUBLER IAW SRM 51-21-00, FOUND TO BE IN LIMITS IAW RD8/4-53-505. DOUBLER CORROSION OUT OF LIMITS FABRICATApr 23, 2011 · N424QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2011042000287Skin · corrodedDURING REMOVAL OF AFT BAGGAGE DOOR CUTOUT SILL, FOUND CORROSION ON LOWER AFT BAGGAGE DOOR SURROUND SKIN UNDER SILL. REMOVED CORROSION IAW SRM 53-40-52-02-01, PERFORMED UT THICKNESS CHECK AND EDDY CURRENT INSP IAW NTM 51-00-02-250-801 AND 51-00-06. TREATED, Apr 17, 2011 · N424QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2011030200199Seal · obstructedRIGHT FORWARD EMERGENCY EXIT MAKING NOISE ON CLIMB AND DESCENT NOISE STOPPED ABOVE 10,000. RETURNED TO THE FIELD, LANDING UNEVENTFUL. FOUND DITCHING DAM LANYARD CAUGHT IN DOOR SEAL. CLEANED DOOR SEALS, REMOVED DEBRIS, AND PRESSURIZED A/C IAW Q400 AMM TASK 21-0Feb 26, 2011 · N424QX · Bombdr DHC8402 · Passenger/Crew DoorsSDR QXEA2011021100141Encoder · malfunctionedON TAXI OUT, BLEED OVER OCCURED WHEN FO TRANSMITTED ON COMM NR 2 130.725 AND CAPT WAS ON COMM NR 1 121.700. BLEEDOVER WAS VERY CLEAR AND LOUD WHICH CAUSED DIFFICULTY IN HEARING GROUND. WHEN SEL CALLING DISPATCH SHE REPORTED LOTS OF CLICKING & STATIC IN BACKFeb 7, 2011 · N424QX · Bombdr DHC8402 · HF Communications SystemSDR QXEA2011020400126Radio · failedENROUTE, HAD A FALURE OF THE COMM RADIO SYSTEMS. ACFT LANDED OK.Feb 1, 2011 · N424QX · Bombdr DHC8402 · HF Communications SystemSDR QXEA2010122100918Skin · corrodedC4 CHECK - LAV DRAIN MAST FOUND EXTERNAL DOUBLER HAS CORROSION. REMOVED LAV DRAIN MAST EXTERNAL DOUBLER IAW SRM 51-42-05. FABRICATED NEW EXTERNAL DOUBLER FROM 2024 T3 .063" IAW SRM 51-42-05. ALODINED AND PRIMED PART IAW SRM 51-21-10 AND 51-25-10. INSTALLEDDec 17, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2010122100917Skin · corrodedC5 CHECK - BELLY ANTENNA BETWEEN FR 236.000 AND 258.500 IS CORRODED. BLENDED CORROSION FROM SKIN REF SRM 51-21-00-00-01. MIN THICKNESS .05" REF NTM 51-00-02-250-801. CONFIRMED AREA IS CRACKFREE CONDITION. REMAINING THICKNESS FOUND TO BE OUT OF LIMITS IAW SDec 17, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2010122100915Doubler · corrodedC4 CHECK - LAV VENT AFT OF FR 19.400 BY STR 33 INTERNAL SKIN DOUBLER IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00. MIN THICKNESS REMAINING .024" REF NTM 51-00-02-250-801 FOUND OUT OF LIMITS. FABRICATED AND MATCH DRILLED NEW DOUBLER IAW SRM 51-40-07. ALODec 17, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2010122000919Frame · corrodedWHILE WORKING CORROSION ON FRAME 18.25 LOWER FLANGE, FOUND CORROSION ON THE VERTICAL WEB JUST OTBD OF STRINGER 31R. RECEIVED NEW FRAME SECTION AND INSTALLED IAW TASK CARD AND RD 8/4-53-3446.Dec 16, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010122000916Frame · corrodedC-CHECK, FRAME 196.000 LOWER FLANGE IS CORRODED BETWEEN STRINGERS 32L AND 33. REMOVED FOR ACCESS, THE RADIO ALTIMETER TRANSCEIVER. REMOVED RIVETS TO GAIN ACCESS. FLANGES ON FRAME BETWEEN 32L AND 33 FOUND TO BE OUT OF LIMITS. BLENDED CORROSION ON FRAME FLANGE 1Dec 16, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010122000901Skin · damagedC-CHECK, EXTERNAL FUSELAGE RT SIDE HAS EVIDENCE OF A LIGHTNING STRIKE. MELT MARKS ON THE SKIN TO RIVETS FROM STR 9R STA 30.000 TO 301.000. BLENDED BURN MARKS IAW SRM 51-14-00-02-03. FOUND TO BE WITHIN LIMITS. TREATED AND PRIMED REPAIRED AREAS. NDT CONFIRMDec 16, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2010122000898Stringer Clip · corrodedFRAME 49.500 TO STR 33, CLIP IS CORRODED. REMOVED CLIP FOR ACCESS TO AREA. REMOVED CORROSION IAW SRM 51-21-00, REV 7. REMOVED MATERIAL OUT OF LIMITS. FABRICATED FRAME 49.500 TO STR 33 CLIP OUT OF .040 7078-T6 IAW TASK CARD 6-53-960. NDT DETERMINED TO BE CRACDec 16, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Attach FittingsSDR QXEA2010122000895Threshold · corrodedC-CHECK. CARGO DOOR THRESHOLD HAS AREAS OF CORROSION. BLENDED CORROSION IAW SRM 51-21-00-02. REMAINING THICKNESS 0.52" OUTSIDE OF LIMITS. FABRICATED AND INSTALLED NEW DOOR THRESHOLD IAW T/C 6-53-958.Dec 16, 2010 · N424QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2010122000920Skin · dentedC-CHECK, RT HORIZONTAL STABILIZER UPPER SURFACE HAS 2 SMALL DENTS 12 INCHES LONG FROM THE T/E AND 3 FT OUT FROM THE VERTICAL STAB. REMOVED PAINT TO INSPECT AREA. FIRST DENT .017" AND SECOND DENT .005". FWD DENT FOUND TO BE CRACKED. REMOVED PANEL 342BB FOR FODec 15, 2010 · N424QX · Bombdr DHC8402 · Horizontal Stabilizer, Plate/SkinSDR QXEA2010122000910Frame · corrodedC-CHECK. FRAME 94.800 LOWER FLANGES BETWEEN STRINGERS 32L AND 31R ARE CORRODED. REMOVED MLS AND ELECTRONIC TRAYS FOR ACCESS. FABRICATED 3 FRAME REPAIR FLANGES OUT OF 2024-T3 TREATED AND PRIMED. NDT CONFIRMED CRACK FREE. INSTALLED REPAIR FLANGES AND STRINGERDec 15, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010122000902Skin · crackedC-CHECK. RT OTBD FLAP UPPER SURFACE BETWEEN TRACKS 4 AND 5 HAS 3 DENTS. NO CRACKS FOUND AND NO DISBOND FOUND. APPLIED YELLOW DOTS TO DENTS IAW GPM 10.11.4.Dec 15, 2010 · N424QX · Bombdr DHC8402 · Trailing Edge FlapsSDR QXEA2010122000900Frame Splice · corrodedC-CHECK, FRAME X94.800 SPLICE PLATE AT BL 0 CORRODED. FABRICATED NEW REPAIR FRAME SPLICE IAW STEP 7 OF MFG RD 8/4-53-3459. NDT CONFIRMED CRACK FREE. PRIMED AND PAINTED AND INSTALLED REPAIR TO THE ACFT.Dec 15, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010122000899Frame · corrodedC-CHECK, FRAME 49.500 LOWER FLANGES BETWEEN STRINGERS 33 AND 31R ARE CORRODED. REMOVED TRANSPONDER RECEIVERS TO GAIN ACCESS AND REMOVED BRACKET. REMOVED CORROSION FROM AREA IAW SRM 51-21-00, REV 7. REMOVED MATERIAL OUT OF LIMITS. CUT OFF LOWER DAMAGED FLANGDec 15, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010122000897Frame · corrodedC-CHECK. FRAME 49.500 TOP FLANGE IS CORRODED BY THE STANTION AT STR 31R. REMOVED TCAS PROCESSOR FOR ACCESS TO THE AREA. REMOVED STANTION FOR ACCESS. REMOVED CORROSION FROM TOP FLANGE AND STA MATING SURFACE OF FRAME IAW SRM 51-21-00-00-02 REV 7. REMOVED MATDec 15, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010122000896Frame · corrodedC-CHECK. FRAME 18.250 LOWER FLANGE BETWEEN STRINGERS 31L AND 32L IS CORRODED. REMOVED RIVETS TO GAIN ACCESS TO AREA. REMOVED CORROSION IAW SRM 51-21-00-00-02. CORROSION ALSO FOUND BETWEEN STRINGERS 32L AND 33 AND WAS REMOVED AS WELL IAW R/D 8/4-53-2344. MATEDec 15, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121600892Door Frame · corrodedC5 CHECK - CORROSION ON THE AFT DOOR FRAME AND FLANGE OF ACCESS DOOR 311AB. REMOVED CORROSION IAW SRM 51-21-00-00-02 AND RD 8/4-53-2344. CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801. COMPLIED WITH RD 8/4-55-592.Dec 14, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, StructureSDR QXEA2010121600861Frame · corrodedREMOVED CORROSION FROM FRAME 32.400 IAW SRM 51-21-00, MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-20-15. REMOVED FRAME PIECE STR 33-28R IAW SRM 51-42-05 AND 51-41-00. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-05. APPLIED PAINT AND CPC AS NEEDED IAW ADec 14, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121400891Floor Panel · corrodedC5 CHECK - AFT CARGO COMPARTMENT FLOOR PANEL 144GH IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02, MEASURED A NOMINAL THICKNESS OF .042" AND A MIN REMAINING THICKNESS OF .032" FOUND PANEL TO BE OUT OF LIMITS IAW SRM 51-14-00-00-01. MATCH DRILLED HOLESDec 14, 2010 · N424QX · Bombdr DHC8402 · Fuselage Floor PanelSDR QXEA2010121400890Floor Panel · corrodedC5 CHECK - AFT CARGO COMPARTMENT FLOOR PANEL 144HZ IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02, MEASURED A NOMINAL THICKNESS OF .042" AND A MIN REMAINING THICKNESS OF .036" FOUND PANEL TO BE OUT OF LIMITS IAW SRM 51-14-00-00-01. MATCH DRILLED HOLESDec 14, 2010 · N424QX · Bombdr DHC8402 · Fuselage Floor PanelSDR QXEA2010121300872Frame · corrodedC5 CHECK - FR 176.000 LOWER FLANGES ARE CORRODED BETWEEN STR 32L AND 31R. REMOVED CORROSION FR 176 LOWER FLANGE, FOUND OUT OF LIMITS, IAW RD 8/4-53-2344. TRIMMED LOWER FRAME FLANGES AT 32L-33 AND 32R-33 IAW RD 8/4-53-017. BLENDED LOWER FRAME FLANGE AT 31R IAWDec 13, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121300886Frame · corrodedC5 CHECK - UPON REMOVAL OF STA 49.500 STR 33 CLIP FOUND FRAME AT STA 49.500 STR 33-32R FWD SIDE TO BE CORRODED. REMOVED CORROSION IAW SRM 51-21-00. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3453. APPLIED ALODINE AND PRIMER IAW SRM 51-21-10 AND 51-25-10. APPDec 12, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121300885Frame · corrodedC5 CHECK - AFT SIDE OF FRAME AT STA 18.250 IS CORRODED AT STR SPLICE ATTACH POINT STR 31R. R & R FRAME.Dec 11, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121300884Web · corrodedC5 CHECK - WHILE WORKING CORROSION ON FR 18.25 LOWER FLANGE, FOUND CORROSION ON VERTICAL WEB JUST OTBD OF STR 31R. REMOVED CORROSION IAW SRM 51-14-00. FOUND TO BE WITHIN LIMITS IAW SRM 51-14-00 STEP 5C. ALODINE AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-Dec 11, 2010 · N424QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2010121300882Frame · corrodedC5 CHECK - FR 236.000 LOWER FLANGES FROM STR 32L TO 31R ARE CORRODED. REMOVED CORROSION SRM 51-21-00-00-02. MIN REMAINING THICKNESS .033" REF NTM 51-00-02-250-801, CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801. LOSS FOUND OUT OF LIMITS IAW RD 8/4-Dec 11, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121300881Frame · corrodedC5 CHECK - FR 18.250 UPPER FLANGE IS CORRODED FROM STR 33 TO 32R. REMOVED CORROSION IAW SRM 51-21-00-00-02, FOUND TO BE WITHIN LIMITS IAW SRM 51-14-00-02-03.Dec 11, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121300871Frame · corrodedC5 CHECK - FOUND CORROSION ON FR 156 LOWER FLANGE STR 33-32R. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. CONFIRMED REPAIR AREA IS CRACK FREE REF NTM 51-00-01-250-801. FABRICATED AND INSTALLED REPAIR IAW RD 8/4-53-017 AND SRM 51-21-10 AND 51-25-10. APPLIED Dec 11, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121300880Stringer · corrodedC5 CHECK - STR 32R IS CORRODED ON THE INBD SIDE APPROX 16" AFT OF THE PILOTS BULKHEAD. REMOVED CORROSION IAW SRM 51-21-00. CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801. MIN THICKNESS REMAINING .036" REF NTM 51-00-02-250-801. LOSS FOUND TO BE OUTDec 10, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Longeron/StringerSDR QXEA2010121300879Seat Track · corrodedC5 CHECK - SEAT TRACK 9 HAS CORROSION AROUND THE FASTENERS BY STA X747.602. REMOVED FASTENERS AND BLENDED CORROSION IAW SRM 51-40-15. COMPLIED WITH RD 8/4-53-884, RD 8/4-53-3439 AND SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-15-02-01.Dec 10, 2010 · N424QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010121300878Skin · corrodedC5 CHECK - FUSELAGE SKIN CORROSION UNDER FRAME NR3 BOTTOM STA X882.703. REMOVED LIGHT CORROSION IAW SRM 51-21-00. CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801. MIN REMAINING THICKNESS OF SKIN .060 REF NTM 51-00-02-250-801. MATERIAL LOSS FOUND WIDec 10, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2010121300877Stringer · corrodedC5 CHECK - STRINGER 31R IS CORRODED AT CROSSRACE ATTACH POINT AND AT STRINGER SPLICE AFT SIDE OF FRAME AT STA 18.250. REMOVED CORROSION IAW SRM 51-21-00-00-02, FOUND TO BE IN LIMITS IAW SRM 53-20-03. MIN MATERIAL THICKNESS .080 SRM NOMINAL .080 NO MATERIAL LDec 10, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Longeron/StringerSDR QXEA2010121300875Stringer · corrodedC5 CHECK -STR 32R IS CORRODED ON THE INBD SIDE APPROX 16" AFT OF THE PILOTS BULKHEAD. REMOVED CORROSION IAW SRM 51-21-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-03. COMPLIED WITH RD 8/4-53-3444, SRM 51-21-10-02-01 AND 51-25-10-02-01.Dec 10, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Longeron/StringerSDR QXEA2010121300874Fitting · corrodedC5 CHECK - AFT CABIN FLOOR FITTING AT X697 BETWEEN SEAT TRACKS 15 AND 23 ARE CORRODED. REMOVED CORROSION IAW SRM 51-21-00. FOUND TO BE OUT OF LIMITS. REMOVED FITTING IAW SRM 51-42-05-02-01, INSTALLED NEW FITTING IAW SRM 51-42-02-01.Dec 10, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Attach FittingsSDR QXEA2010121300873Sill · corrodedC5 CHECK - AFT BAGGAGE COMPARTMENT OUTER DOOR SILL HAS CORROSION IN MULTIPLE AREAS ON INBD SIDE. REMOVED CORRODED DOOR SILL IAW SRM 51-21-00-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-01. REMOVED DOOR SILL AND INSTALLED NEW SILL IAW SRM 51-42-05.Dec 10, 2010 · N424QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2010121300883Frame · corrodedC5 CHECK - STA 71.200 FRAME FLANGE CORRODED FROM STR 32R-31R. REMOVED CORROSION IAW SRM 51-21-00-00-02. FLANGE IS OUT OF LIMITS IAW RD 8/4-53-2344. CONFIRMED AREA CRACK FREE CONDITION. FABRICATED NEW FLANGE TREATED AND INSTALLED FLANGE IAW RD 8/4-53-017.Dec 9, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2010121300876Skin · corrodedC5 CHECK - UPON REMOVAL OF AFT BAGGAGE DOOR SILL FOUND CORROSION ON SKIN. REMOVED CORROSION IAW SRM 51-21-00. MIN REMAINING THICKNESS IN BLENDED AREA IS .206. CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801. COMPLIED WITH RD 8/4-53-3445 AND APPLIED Dec 9, 2010 · N424QX · Bombdr DHC8402 · Cargo/Baggage DoorsSDR QXEA2010121000868Frame · corrodedC5 CHECK - CORROSION ON FRAME IN TAIL COMPARTMENT JUST FWD OF DOOR 311AB. REMOVED FRAME NR3 BOTTOM AT X882.703 AND LT AND RT CAP SPLICE REF SRM 53-50-15, FIG 1, PG 14, BY DRILLING OUT RIVETS IAW SRM 51-42-05. LOCATED AND DRILLED FASTENER HOLES IN NEW NR3 BOTDec 9, 2010 · N424QX · Bombdr DHC8402 · Fuselage Main, Frame
Back to N424QX, cancelled Jan 17, 2013