N429QX

Service difficulty reports · 217

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 = 'N429QX' AND registry_match = 'registration'
  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 QXEA2011092600889Skin · damagedRT WING UPPER T/E SHROUD SKIN HAS WORKING RIVETS AROUND OTBD SPOILER CENTER HINGE CUTOUT. DRILLED OFF WEB IAW SRM 51-42-45-02-01. REMOVED 6 RIVETS ON UPPER RT WING AROUND OTBD SPOILER CENTER HINGE CUTOUT IAW SRM 51-42-05-02-01. INSTALLED (6) RIVETS ON UPPER Sep 23, 2011 · N429QX · Bombdr DHC8402 · Wing, Plate/SkinSDR QXEA2011092600888Frame · corrodedFRAME 236, FLANGES STR 30P TO 32P ARE CORRODED. REMOVED SURFACE CORROSION AND BLENDED IAW RD 8/4-53-2344. CONFIRMED AREA CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS WITHIN LIMITS OF RD 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53Sep 23, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600887Frame · corrodedFRAME 94.8 FLANGES STR 30P TO 32P ARE CORRODED. REMOVED CORROSION AND BLENDED IAW RD 8/4-53-2344. CONFIRMED AREA CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS WITHIN LIMITS OF RD 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 23, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600886Frame · corrodedFRAME 116, FLANGES STR 30P TO 32P ARE CORRODED. REMOVED CORROSION AND BLENDED IAW SRM 51-21-00-00-02. MATERIAL LOSS WITHIN LIMITS OF RD 8/4-53-2344. COMPLETED REPAIR RD 8/4-53-2344.Sep 23, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092900916Frame · corrodedFRAME 38.4, UPPER TIE TO INTERCOSTAL 28P IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND OUT OF LIMITS. FABRICATED NEW PART IAW TASK CARD 6-53-1014. COMPLIED WITH TASK CARD 6-53-1014. PRIMED AND PAINTED IAW SRM 51-25-10-02-01 ANSep 22, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092700907Stringer Splice · corrodedSTRINGER 31P SPLICE BETWEEN FR 32.4 AND 47 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-01.MINIMUM REMAINING THICKNESS .081". CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. WITHIN LIMITS OF SRM 53-20-43-00-01. ALODINED, PRIMED SRSep 22, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, Longeron/StringerSDR QXEA2011092600891Stringer · corrodedSTRINGER 24P IS CORRODED FR 258.5 TO 301. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AREA CRACK FREE REF NTM RD 8/4-53-3953. MATERIAL LOSS WITHIN LIMITS OF RD 8/4-53-3953. ALODINED AND PRIMED REPAIR IAW RD 8/4-53-3953. COMPLIED WITH TASK CARD RD Sep 22, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, Longeron/StringerSDR QXEA2011092600890Frame · corrodedFRAME 216, FLANGES STR 29P TO 32P ARE CORRODED. BLENDED TO REMOVE CORROSION IAW RD 8/4-53-2344. CONFIRMED AREA CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS WITHIN LIMITS OF RD 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 22, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600873Bulkhead · corrodedUNDER FLOOR WEB FOR THE FWD DRAFT BULKHEAD IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. ANGLE SUPPORT FOUND TO BE OUT OF LIMITS. REMOVED AND FABRICATED NEW PART IAW TASK CARD 6-53-1019. ALODINED AND PRIMED PART IAW TASK CARD 6-53-1019. INSTALLED Sep 22, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, BulkheadSDR QXEA2011092600871Frame · corrodedSTATION AT FR 18.25 IS CORRODED BY STR 31P. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND BLEND TO BE WITHIN LIMITS IAW RD 8/4-53-3950. APPLIED ALODINE, PRIMER, PAINT AND CPC IAW RD 8/4-53-3950. COMPLIED WITH TASK CARD RD 8/4-53-3950.Sep 22, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600885Skin · corrodedLONGITUDINAL SKIN STRAP OTBD OF STR 32P, FR 547 TO 564.5 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND WITHIN LIMITS OF RD 8/4-53-3962. COMPLETED REPAIR IAW RD 8/4-53-3962.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2011092600884Frame · corrodedFRAME 258.5, FLANGE STR 31P TO 32P IS CORRODED. CLEANED AND REMOVED CORROSION IAW RD 8/4-53-2344. FOUND WITHIN LIMITS OF RD 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600883Stringer · corrodedSTRINGER 26P HAS AN AREA OF CORROSION AFT OF FR 258.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND WITHIN LIMITS OF RD 8/4-53-3954. COMPLETED REPAIR IAW RD 8/4-53-3954.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, Longeron/StringerSDR QXEA2011092600882Frame · corrodedFRAME 196, FLANGE STR 32S TO 31S IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND WITHIN LIMITS OF RD 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600881Frame · corrodedFRAME 196, FLANGES STR 28P TO 31P ARE CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND WITHIN LIMITS OF RD 8/4-53-2344. COMPLETED RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600880Frame · corrodedFRAME 136, FLANGES STR 30P TO 32S ARE CORRODED. BLENDED AND REPAIRED IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600879Frame · corrodedFRAME 49.5, FLANGE STR 29P TO 30P IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02 AND RD 8/4-53-2344. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600878Frame · corrodedFRAME 47, FLANGES STR 26P TO 28P ARE CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600877Frame · corrodedFRAME 4.5 FLANGES STR 31P TO 31S ARE CORRODED. BLENDED CORROSION IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS OF 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600876Frame · corrodedFR 38.4 FLANGES ARE CORRODED STR 26P TO 28P. REMOVED CORROSION AND REPAIRED IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600875Frame · corrodedFRAME 19.4 FLANGES ARE CORRODED STR 30S TO 33. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600874Frame · corrodedFRAME 19.4 FLANGES ARE CORRODED STR 30P TO 32P. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092600872Frame · corrodedFRAME X28.000 LOWER FLANGE HAS CORROSION ABOVE STRINGER 25P JUST BELOW FWD LT PAX DOOR THRESHOLD. BLENDED CORROSION IAW RD 8/4-53-2344. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092300869Frame · corrodedFRAME 664.5 FLANGE IS CORRODED STR 31P TO 32P. REMOVED CORROSION IAW RD 8/4-53-2344, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CIC IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092300868Angle · corrodedAFT CARGO DOOR LOWER DOOR SILL OUTER ANGLE HAS CORROSION ON THE INNER SURFACE AFT OF FR 763. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3948. APPLIED ALODINE, PRIMER, TOP COAT AND CPC IAW RD 8/4-53-3948. Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011092300867Web · corrodedAFT CARGO FLOOR LEVEL WEB HAS CORROSION OTBD OF SEAT TRACK 9 FR 763 TO 783. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3942. APPLIED ALODINE, PRIMER AND CPC IAW RD 8/4-53-3942. COMPLIED WITH RD 8/4-53-39Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011092300866Angle · corrodedAFT CARGO FLOOR WEB LT ANGLE AT FR 783 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3947. APPLIED ALODINE, PRIMER, TOP COAT AND CPC IAW RD 8/4-53-3947. COMPLIED WITH RD 8/4-53-3947 AND TASK CARSep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011092300865Seat Track · corrodedSEAT TRACK 16 IS CORRODED FORWARD OF FR 783. REMOVED CORROSION IAW RD 8/4-53-2362. SEAT TRACK FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3938. ALODINE APPLIED IAW RD 8/4-53-3938. COMPLIED WITH RD 8/4-53-3938 AND TASK CARD RD 8/4-53-3938.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2011092300864Floor Panel · corrodedFLOOR WEB ON SEAT TRACK 5 IS CORRODED BY FR 1.00. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND BLEND TO BE WITHIN LIMITS IAW RD 8/4-53-3941. ALODINED BLENDED ARE IAW SRM 51-21-10-02-01 AND PRIMED IAW SRM 51-25-10-02-01.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Floor PanelSDR QXEA2011092300863Frame · corrodedFRAME 1.00 FLANGE IS CORRODED 32P TO 31P. BLENDED OUT CORROSION IAW RD 8/4-53-2344, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED, PAINTED AND APPLIED CIC FLANGE IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092300862Frame · corrodedFRAME 1.00 FLANGE IS CORRODED 33 TO 32S. BLENDED CORROSION IAW SRM 51-21-00-00-02, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CIC IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092300861Angle · corrodedANGLE COMMON TO FR19.4 AND INTERCOSTAL 25P IS CORRODED. REMOVED ANGLE IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02, MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-20-15-00-01. INSTALLED NEW ANGLE IAW SRM 51-42-05-0Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011092300860Frame · corrodedFRAME 547, FLANGES STR 31P TO 33 ARE CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED, PAINTED AND APPLIED CIC IAW RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092300858Stringer · corrodedSTRINGER 27P IS CORRODED FR 94.8 TO FR 116. REMOVED CORROSION IAW 51-21-00-00-02, MATERIAL LOSS FOUND TO BE WITHIN LIMITS OF RD 8/4-53-3952. TREATED, PRIMED, PAINTED AND APPLIED CIC FLANGE IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, Longeron/StringerSDR QXEA2011092300859Threshold · corrodedAFT CARGO DOOR THRESHOLD STRAP HAS AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3951. APPLIED ALODINE, PRIMED, PAINTED AND APPLIED CIC IAW RD 8/4-53-3951.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011092300857Frame · corrodedFRAME 644.5 FLANGES STR 30S TO 32S ARE CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED, PAINTED AND APPLIED CIC FLANGE IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092300856Floor Support · corrodedFLOORBOARD SUPPORT BRACKET AT FR 19.4 IS CORRODED ON THE UPPER SURFACE AND LOWER AFT SIDE BY STR 25P. REMOVED CORROSION FROM FLOORBOARD SUPPORT BRACKET IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE WITHIN LIMITS OF RD 8/4-53-3931. TREATED, PRIMED, TOP CSep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011092300855Frame · corrodedFRAME 644.5 FLANGES STR 30P TO 32P ARE CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED, PAINTED AND APPLIED CIC FLANGE IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092300854Frame · corrodedFRAME 624.5 FLANGE STR 31P TO 32P IS CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED, PAINTED AND APPLIED CIC FLANGE IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND RD 8/4-53-2344.Sep 21, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011092900915Nut Plate · corrodedWHILE REMOVING LT SIDE ICE SHIELD, FOUND 6 EA NUT PLATES CORRODED FROM STA X290.000 TO 327.000. REMOVED BRACKETS WITH NUT PLATES, REMOVED NUT PLATES AND INSTALLED NEW NUT PLATES AND BRACKET IAW SRM 51-42-05-02-01.Sep 20, 2011 · N429QX · Bombdr DHC8402 · Fuselage, Door HingeSDR QXEA2011092100853Stringer · corrodedSTRINGER 27P IS CORRODED FR 176 TO 196. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING THICKNESS .058", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-3934. TREATED PRIMED AND PAINTED IAW RD Sep 20, 2011 · N429QX · Bombdr DHC8402 · Fuselage Main, Longeron/StringerSDR QXEA2011092100851Angle · corrodedFR 19.4 ANGLE BY PAX DOOR IS CORRODED BY STR 25P. REMOVED ANGLE IAW SRM 51-40-15-02-01 AND 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING MATERIAL THICKNESS OUT OF LIMITS IAW SRM 53-00-00-02-09. MATCH DRILLED NEW ANGLE IAW SRM 51-40-07Sep 19, 2011 · N429QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011092100850Seat Track · corrodedLT OTBD SEAT TRACK IS CORRODED AFT OF FR 701. BLENDED CORROSION IAW RD 8/4-53-2362. BLENDED AREA IS WITHIN LIMITS IAW RD 8/4-53-2362. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. APPLIED ALODINE AND FASTWELD IAW SRM 51-21-10-02-01 AND 51-22-35-02-01.Sep 19, 2011 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2011092100852Seat Track · corrodedSEAT TRACK 9 HAS AREAS OF CORROSION FR 701 TO 783. REMOVED CORROSION IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01, 51-41-05-00-01 AND 51-40-15-02-01. MATCH DRILLED NEW SEAT TRACK IAW SRM 51-40-07-02-01. INSTALLED SEAT TRACK IAW SRM 51-41-05-Sep 18, 2011 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2011091900849Seat Track · corrodedSEAT TRACK 5 IS CORRODED FROM FR 32.4 TO AFT FR 47. REMOVED CORROSION AND FOUND CORROSION TO BE OUT OF LIMITS IAW RD 8/4-53-884. REPAIRED IAW TASK CARD RD8/4-53-3937. SEAT TRACK FOUND TO BE WITHIN LIMITS IAW TASK CARD RD 8/4-53-3937.Sep 18, 2011 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2011091900848Seat Track · corrodedSEAT TRACK 10 IS CORRODED. FOUND CORROSION TO BE OUT OF LIMITS IAW RD 8/4-53-2358. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-00-00-01. DRILLED AND INSTALLED NEW SEAT TRACK NR10 IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01.Sep 18, 2011 · N429QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2011092900918Access Panel · damagedFUEL ACCESS PANEL 622AT HAS 2 SPINNING SCREWS BAD NUT PLATES. REMOVED GANG CHANNEL IAW SRM 51-42-05-00-01. INSTALLED DOME NUTS ON GANG CHANNEL IAW SRM 51-42-75-02-01. INSTALLED GANG CHANNEL TO FWD SIDE OF PANEL IAW SRM 51-42-75-02-01.Sep 17, 2011 · N429QX · Bombdr DHC8402 · Wing, Plate/SkinSDR QXEA2011091900847Access Panel · corrodedPANEL 624AT HAS CORROSION. BLENDED AWAY CORROSION IAW RD 8/4-57-442. FOUND TO BE WITHIN LIMITS OF RD 8/4-57-442. CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801. TREATED, PRIMED AND INSTALLED SEALS IAW RD 8/4-57-442.Sep 17, 2011 · N429QX · Bombdr DHC8402 · Wing, Plate/SkinSDR QXEA2011091900846Access Panel · corrodedRT WING PANEL 624FT ACCESS LANDING HAS CORROSION. BLENDED TO REMOVE CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS OF RD 8/4-57-445. CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801 AND COMPLETED REPAIR IAW RD 8/4-57-445.Sep 17, 2011 · N429QX · Bombdr DHC8402 · Wing, Plate/SkinSDR QXEA2011091900845Access Panel · corrodedRT WING PANEL 624ET ACCESS LANDING HAS CORROSION. BLENDED TO REMOVE CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS OF RD 8/4-57-445. CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801 AND COMPLETED REPAIR IAW RD 8/4-57-445.Sep 17, 2011 · N429QX · Bombdr DHC8402 · Wing, Plate/Skin
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