JASC 5420
Service difficulty reports · 3,949
Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, 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 jasc_code = '5420' 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.
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 jasc_code = '5420' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA060711Support Beam · chafedNR 1 PYLON STRUT FAIRING BEAM AT O/B FWD END CHAFED. FABRICATED SUPPORT BEAM, UPPER SPLICE, LOWER SPLICE PER SRM 51-70-11, 51-40-05, 51-20-1, 5-40-02, DEFECT SIZE: 1"L X 1"W X .050"D.SDR USAA060710Support Beam · chafedNR 1 PYLON STRUT FAIRING BEAM AT I/B FWD END CHAFED. FABRICATED SUPPORT BEAM, UPPER & LOWER SPLICE & REPLACED FITTING PER SRM 54-62-71, 51-40-02, 51-70-1, DEFECT SIZE: 1"L X 1"W X .080"D.SDR DU4R2006445Fitting · wornNR 2 PYLON FOUND LWR FWD OUTBOARD LUG TO BE 2.008, OVERSIZED SHOULD BE > 2.009. REPAIRED BY FABRICATING AND INSTALLING BUSHING 1.748 ID FROM 15-5 PH IAW DELTA ERA 455545-14AD REV ORIGINAL DATED 5-12-06 APPROVED BY FAA FORM 8100-9.SDR QXEA200601318Structure · crackedYYC - C4 RIGHT NACELLE FINGER NAIL UPPER RIGHT SIDE AT STATION XN 270 CRACKED AT FASTENERS. REPAIRED IAW RD8-54-2184 AND EA 2-54-279.SDR UPS06446965Stiffener · crackedINSPECTION TYPE:C NR 3 PYLON REAR MOUNT B/H UPPER T-CHORD RT END 2EA HOLE FOUND CRACKED. CRACK LENGTH .5 INCH. NR 3 PYLON REAR MOUNT B/H UPPER T-CHORD REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR THMN4113SQ120Cowling · crackedRT UPPER ENGINE COWL AFT IB BRACKET CRACKED AT CORNER. MADE AIRWORTHY REPAIR IAW SRM 54-20-43 AND SRM 51-10-22.SDR THMN4113SQ121Cowling · crackedR/H UPPER ENGINE COWL CRACKED IN BRACKET UNDER SEAL IN CENTER SECTION. MADE AIRWORTHY REPAIR IAW FALCON 20 SRM 54-20-43.SDR QXEA200601592Diaphragm · crackedYYC - C3 RT NACELLE OUTER UPPER DIAPHRAGM AT XN197 CRACKED BY WING TRAILING EDGE. REPAIRED IAW RD 8/4-54-155, ISSUE 1.SDR QXEA200601591Diaphragm · crackedYYC - C3 LEFT NACELLE OUTER SUPPER DIAPHRAGM XN197 CRACKED BY WING TRAILING EDGE. REPAIRED IAW RD 8/4-54-155, ISSUE 1.SDR QXEA200601629Shield · damagedYYC - C3 RIGHT NACELLE, AFT LEFT DISHED HET SHIELD HAS A HOLE WORN THROUGH IT. REPAIRED IAW RD 8/4-54-336, ISSUE 2 AND EA 6-54-403.SDR UPS06146816Angle · crackedNR 2 ENG PYLON INBD MEMBER SECTION ANGLE AT RIB 18 IS CRACKED. REMOVED AND REPLACED NR 2 PYLON INBD MEMBER SECTION ANGLE PER SRM 51-40-21.SDR UPS06146815Angle · crackedNR 2 ENG PYLON OTBD MEMBER SECTION ANGLE AT RIB 18 IS CRACKED. REMOVED AND REPLACED NR 2 PYLON OTBD MEMBER SECTION ANGLE PER SRM 51-40-21.SDR CALA0600135Support Angle · crackedNR 2 PYLON AFT FAIRING O/B SUPPORT ANGLE CRACKED AT STA 418. REPLACE SUPPORT ANGLE PER SRM 51-10-02 & 51-40-02.SDR AWXA200600695Spar · crackedSAL - DURING C5 CHECK DISCOVERED CRACK ON RIGHT PYLON STRUCTURE, UPPER OUTBOARD SIDE, 1.5 INCHES, AFT RIB 6. MAINTENANCE REPAIRED THE RIGHT PYLON STRUCTURE UPPER OUTBOARD SIDE AFT RIB 6 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 26-5452-06108-SS6. ER WAS CSDR UPS06547208Fitting · chafedINSPECTION TYPE:C NR 2 PYLON - O/B LWR CORNER OF MIDSPAR FITTING IS CHAFFED. COMPLIED WITH EO 757-5453-27-A1915 REV DATED 4-19-06.SDR UPS06547206Fitting · chafedINSPECTION TYPE:C NR 2 PYLON, I/B LOWER CORNER OF MIDSPAR FITTING IS CHAFED. COMPLIED WITH EA 757-5453-27-A1415 REV DATED 04-19-06.SDR 061134Stiffener · crackedNR 4 PYLON MID SPAR WEB LOWER SIDE STIFFENER CRACKED AT O/B END IN RADIUS AT NAC STA 231.SDR QXEA200601032Angle · crackedYYC - C4 LEFT NACELLE, INBOARD DRAG ANGLE IS CRACKED AT LAST RIVET, AFT ON WING SIDE. REPARIED IAW RD 8-57-1053, ISSUE 2.SDR QXEA200601162Cowling · crackedPDX: LH NACELLE OTBD SIDE DIAPHRAM CRACKED (WING TO NACELLE FLAP COVE AREA). MAINTENANCE REPAIRED IAW Q400 SRM 51-40-15, SRM 51-42-15, SRM 51-40-07, SRM 51-42-05, SRM 51-23-00 AND RD 8/4-54-155.SDR SWIA200616898Web · crackedLOWER ENG SUPPORT WEB CRACKED AT LBL36.00 AT EDGE OF ACCESS COVER HOLE. INSTALLED REPAIR DOUBLER TO LOWER ENGINE SUPPORT WEB AT LBL 36 IAW CRJ200 SRM 51-42-06 PG 11; 51-42-20 STEP 9C.SDR AWXA200600648Shim · migratedGYR - DURING C12 CHECK DISCOVERED NR 1 PYLON DIAGONAL BRACE FITTING SHIMS MIGRATING LEFT SHIM HORIZONTAL MOVEMENT 0.400 INCHES AND VERTICAL MOVEMENT 0.900 INCHES. MAINTENANCE REPAIRED PER AWA ER 19-5453-06060-BA1 AND BOEING SB 757-54-0035 FIG. 21, STEPS 8, 12SDR QXEA200600889Diaphragm · crackedPDX: LT NACELLE DIAPHRAGM ON UPPER OUTBOARD SIDE AT APPROX STA XN197.0 CRACKED. MAINTENANCE REPAIRED IAW RD 8/4-54-155.SDR MALA060166Duct · chafedRIGHT NACELLE, LOWER INLET DECK IS CHAFED OUT OF LIMITS. REPAIRED IAW MESABA EOS54095.SDR QXEA200600713Structure · gougedYYC - C4 RIGHT HAND NACELLE STATION XN176.50, STRUCTURE AT AFT HINGE POINT FOR FORWARD GEAR DOOR IS GOUGED DUE TO BOLT FOR BONDING WIRE BEING INSTALLED BACKWARDS. REPAIRED IAW DHC-8-200 SRM 51-40-11.SDR 2006UALA00469Angle · crackedCLOSEOUT ANGLE BELOW MID SPAR FITTINGS OF NR 2 PYLON HAS CRACKS FROM INBOARD AND OUTBOARD ENDS. INBD AND OUTBD ENDS ON CLOSEOUT ANGLE BELOW MID SPAR FITTINGS OF NR 2 PYLON WERE FOUND CRACKED. THE CLOSEOUT ANGLE WAS REPLACED USING 767-300 SRM 51-40-02.SDR QXEA200600776Bracket · crackedPDX C4, CRACK AT APPROXIMATELY STATION XN125.5 AND ZN7.0 ABOVE FIRE LOOP BRACKET. REPAIRED IAW DHC-8 RD 8-54-611.SDR QXEA200600702Stiffener · crackedYYC C4 , RIGHT HAND NACELLE FINGER NAIL DECK HAS CRACKED STIFFENER AT XN250 TOP SURFACE. REPAIRED IAW HORIZON AIR EA 2-54-255 AND DHC-8-200 SRM 51-40-11, PAGES 1-4.SDR QXEA200600711Attach Angle · damagedYYC - C4 RIGHT HAND NACELLE MISSING RIVETS ON LEFT HAND INSIDE AT ANGLE ATTACH TO SEAL FRAME, FORWARD SIDE XN214.00. REPAIRED IAW DHC-8-200 SRM 51-10-21, 51-40-11.SDR QXEA200600709Strap · corrodedYYC C4, LEFT HAND NACELLE FINGER NAIL DECK OUTBOARD SIDE ATTACH STRAP WORN AND CORRODED AROUND ANCHOR NUTS AT AFT END. REPAIRED IAW RD 8-54-163, ISSUE 2, PAGES 1-6.SDR QXEA200600705Strap · wornYYC C4 , RIGHT HAND NACELLE FINGER NAIL, INBOARD ATTACH STRAP END WORN AT ANCHOR NUT APPROXIMATELY XN270. REPAIRED IAW RD 8-54-163, ISSUE 2.SDR QXEA200600710Strap · wornYYC - C4 LEFT HAND NACELLE FINGER NAIL DECK, INBOARD SIDE ATTACH STRAP WORN AND CORRODED AROUND ANCHOR NUTS AFT END. REPAIRED IAW RD 8-54-163, ISSUE.SDR QXEA200600708Strap · gougedYYC C4, LEFT HAND NACELLE FINGER NAIL DECK, AFT ATTACH STRAP FOR TAIL CONE WORN AND GOUGED. REPAIRED IAW RD 8-54-163, ISSUE 2, PAGES 1-3.SDR QXEA200600707Stiffener · crackedYYC C4, LEFT HAND NACELLE FINGER NAIL DECK HAS CRACKED STIFFENER APPROXIMATELY XN270 TOP SURFACE. REPAIRED IAW RD 8-54-1153, ISSUE 3.SDR QXEA200600706Strap · wornYYC C4, RIGHT HAND NACELLE FINGER NAIL DECK, AFT ATTACH STRAP FOR TAIL CONE WORN AT ANCHOR NUTS. REPAIRED IAW RD 8-54-163, ISSUE 1, PAGE 3, PARAGRAPH 1, AND RD 8-54-163, PAGE 3, PARAGRAPH 4 AND PAGES 1-2, ISSUE 2.SDR QXEA200600703Structure · gougedYYC C4, RIGHT HAND NACELLE FINGER NAIL DECK, HAS TWO DEEP GOUGES FROM SCREWS AFT END, BY TAIL CONE ATTACH STRAP, APPROXIMATELY XN278. REPAIRED IAW RD 8-54-097.SDR QXEA200600704Stiffener · crackedYYC C4, RIGHT HAND NACELLE FINGER NAIL DECK HAS CRACKED STIFFENER AFT, XN270 TOP SURFACE. REPAIRED IAW RD 8-54-1153 AND DHC-8-200 SRM 51-40-11, PAGES 1-4.SDR UPS06146450Fairing · crackedNR 1 ENG LOWER PYLON, AFT LOWER SECTION HAS CRACK. REPAIRED AFT LOWER SKIN PANEL PER A300 SRM 51-40-00, SAA EA 300-5455-01-A0103 AND UPS RAA A300-54-20053.SDR PIDA06025Structure · crackedLEFT ENGINE PYLON PANEL 5724 LT HAS A SMALL CRACK AT THE EDGE OF THE CUTOUT. REPAIRED CRACK IN THE UPPER FORWARD CORNER OF THE CUTOUT PER BOEING SB 737-54-1032.SDR PIDA06024Structure · crackedNR 2 PYLON OUTBOARD MID ACCESS CUTOUT FOR PANEL 5824R IS CRACKED AT THE UPPER FORWARD AND LOWER AFT CORNERS. REPAIRED PER BOEING SB 737-54-1032.SDR QXEA200600490Structure · wornPDX: RT LOWER COWL STEP WEAR BETWEEN INBOARD HINGE ARM AND AIRCRAFT CLEVIS HINGE STRUCTURE. MAINTENANCE REPAIRED IAW HORIZON EA 6-54-382 NDTM PART 6, 51-00-02, SRM 54-20-05 AND SRM 54-10-06.SDR QXEA200600591Diaphragm · crackedLT NACELLE TOP FAIRING OUTBOARD SUPPORT DIAPHRAGM CRACKED AT STA XN 245.5. MAINTENANCE REPAIRED IAW Q400 SRM 51-42-05 AND 51-40-15.SDR P5CA0601440Structure · crackedNR 2 PYLON - PRECOOLER ACCESS CUTOUT CRACKED, AFT BOTTOM RIGHT SIDE. REPAIRED PER BOEING 8100-9 DATED 01FEB2006 PER EO-4754A184.SDR P5CA0601439Structure · crackedNR 3 PYLON PRECOOLER CUTOUT CRACK AT FASTENER HOLE, LOWER AFT CORNER. REPAIRED PER BOEING 8100-9 DATED 01FEB2006, PER EO-4754A184.SDR P5CA0601437Structure · crackedNR 4 PYLON PRECOOLER CUTOUT CRACKED AT LOWER AFT CORNER BY FASTENER HOLE. REPAIRED PER BOEING 8100-9 DATED 01FEB2006, PER EO-4754A184.SDR UPS06146234Support Angle · crackedINSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT OTBD SUPPORT ANGLE CRACKED AT JOGGLE INTERIOR SIDE. REMOVED AND REPLACED SUPPORT ANGLE PER A300 SRM 51-40-21.SDR UPS06146233Support Angle · crackedINSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT INBD SUPPORT ANGLE CRACKED AT JOGGLE INTERIOR SIDE. REMOVED AND REPLACED SUPPORT ANGLE PER A300 SRM 51-40-21.SDR UPS06146231Support · crackedINSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT END SUPPORT MEMBER CRACKED AT INBD SIDE JUST ABOVE GANG DRAIN EXIT OF PYLON. REMOVED AND REPLACED MEMBER PER A300 SRM 51-40-21 AND 51-40-00.SDR PIDA06016Channel · crackedU-CHANNEL CRACKED BEHIND PANEL 5843R ON THE RIGHT ENGINE PYLON. REPLACED CHANNEL PER BOEING DWG 313A1355.SDR DL76L060091Tee Fitting · crackedTHE NR 1 ENGINE PYLON MID SPAR FITTING CLOSEOUT TEE WAS FOUND CRACKED. REPLACED THE CRACKED CLOSEOUT TEE. REF AD 2005-19-23.SDR 06FDEA0365Bearing · unknownCOMPLY WITH EA 6-5720-92381 INSPECTION/CHECK OF PYLON AFT ATTACH FITTING UPPER BEARINGS ENT BY: 501863 RPT BY: 501863 FACT 20JAN06 07:25 BFM R COMPLIED WITH EA 6-5720-92381 INSPECTION CHECK OF PYLON AFT ATTACH FITTING UPPER BEARINGS RII:573074 ENT BY: 57
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