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 UPS05244729Bushing · damagedENGINE NR 3 FWD MOUNT AFT O/B HOLE REPAIR BUSHING DAMAGED. BUSHING REPLACED IAW UPS EO B727-5440-11592-A.SDR UPS05244728Structure · corrodedENG NR 1 FWD MOUNT BOTH O/B HOLES HAVE PITTING CORROSION ON REPAIR BUSHINGS. BUSHINGS REPLACED IAW UPS EO B727-5440-11592-A.SDR 05FDEA01527Support Bracket · crackedFOUND ANGLE SUPPORT BRACKET FOR MAIN HYDRAULIC LINE CRACKED INBD SIDE OF PYLON AT RIB 20. REMOVED AND REPLACED ANGLE ON NR 2 PYLON IAW A310 SRM 51-40-21 AND 51-72-10.SDR AMTA200500507Shim · migratedSHIMS MIGRATING IN NR 1 ENGINE MID-SPAR BULKHEAD AT OB AFT LOWER ATTACH BOLT UPPER SURFACE. REPAIRED DAMAGE IAW ERA. (K)SDR USAA050706Stiffener · crackedCLT - FOUND STIFFENER AND CHANNEL CRACKED .5 INCHES, NR 2 ENGINE AFT STRUT STRUCTURE. FABRICATED AND INSTALLED NEW CHANNEL REMOVED AND REPLACED STIFFENER IAW SRM 51-10-01 AND DRAWING 313H1355. (M)SDR 05FDEA01496Stiffener · gougedCOMPLY WITH EA 8-7254-89506 ENGINE - TURBINE - TMF STRUT NR 1 STIFFENER GOUGE REPAIR. COMPLIED WITH EA 8-7254-89506.SDR QXEA200501050Diaphragm · crackedPDX - RIGHT NACELLE OUTBOARD SIDE, DIAPHRAGM CRACKED AT STATION 197.00 ABOVE NR 3 FLAP TRACK. REPAIRED IAW Q400 SRM 51-40-07.SDR QXEA200501049Diaphragm · crackedPDX - LEFT NACELLE, OUTBOARD SIDE, DIAPHRAGM CRACKED AT STATION 197.00. REPAIRED IAW RD 8/4-54-155 AND DHC-8-400 SRM 51-40-10 AND 51-42-05.SDR ABXA050132Web · crackedCRACK INSIDE PYLON UNDER PANEL 8206. REPAIRED CRACK IAW DC-9 SRM 54-01.SDR 05FDEA01255Shroud · crackedPYLON NR 1 SHROUD/PAN, UNDER THE ENGINE BLEED AIR DUCT, IS CRACKED. VIEWED THRU ACCESS PANEL 413EL. REMOVED CRACKED SHROUD, FAB NEW SHROUD ON TR T5/517007 301-25 .025SS BATCH 0000887337, INSTALLED SHROUD IAW SRM 51-4-21.SDR 05FDEA01249Gusset · corrodedNR 2 PYLON OUTBOARD SIDE RIBS 15A, 16A, AND 17A UPPER AREA OF PYLON HAVE CORROSION AROUND, IN FASTENER HOLES AND EXTENDING UNDER NUT PLATES AS MARKED. REMOVED AND REPLACED GUSSETS IAW A310-200 SRM 51-40-21 AND 51-72-10.SDR QXEA200500845Diaphragm · crackedPDX - LEFTHAND NACELLE TO WING DIAPHRAGM IS CRACKED, OUTBOARD AFT TRAILING EDGE. REPAIRED IAW DHC-8 400 SRM 51-42-05.SDR AMTA200500424Shim · migratedBULKHEAD/FIREWALL, NR 2 ENGINE STRUT MID BULKHEAD HAS MIGRATING SHIMS AT FWD IB AND OB LOWER MID SPAR BOLT ATTACH POINTS PP STA 174. COMPLIED WITH PART 1 OF ERA. (K)SDR AMTA200500423Shim · migratedBULKHEAD/FIREWALL, NR 1 ENGINE STRUT MID BULKHEAD HAS MIGRATING SHIMS AT FORWARD OUTBOARD LOWER MID SPAR BOLT ATTACH POINT PP STATION 174. COMPLIED WITH PART 2 OF ERA 757-54R-5870. (M)SDR USAA050589Stiffener · crackedCLT - FOUND STIFFENER CRACKED .4 INCH IN VERTICAL STIFFENER AT AFT SIDE OF PYLON LOWER SIDE OF WING. FABRICATED REPAIR PART AND INSTALLED SRM 51-10-02. (M)SDR 0500996745Web · crackedDURING H-CHECK, FOUND CRACK IN NR 3 PYLON OB AFT FRAME WEB. REPAIRED PER EA 67-165208.SDR QXEA200500700Structure · chafedPDX - LEFTHAND MAIN LANDING GEAR CHAFE ABOVE DRAG STRUT ASSEMBLY LEFT SIDE. REPAIRED IAW RD 8-54-2000 AND HORIZON AIR EA 2-54-227.SDR USAA050503Shim · migratedFOUND SHIM MIGRATION GREATER THAN .030 INCH, NR 1 PYLON MID BULKHEAD UPPER ATTACH AREA BETWEEN THREAD FITTING. REPLACED SHIMS PER EO 5402R022A SECT IV PART 2/6, EA 96212. (M)SDR QXEA200500822Beam · nickedYYC - RIGHT PYLON, HINGE BEAM HAS NICK 6" FORWARD OF PYLON TIE BAR NR 3 HINGE POSITION. REPAIRED IAW HORIZON AIR EA R-78-36 AND REO 670-78-34-260.SDR QXEA200500823Hinge · gougedYYC - RIGHT PYLON HINGE BEAM AT PYLON TIE BAR HAS GOUGES ON HINGE TOP AND LOWER LOCATIONS FROM TIE BAR BRACKETS RUBBING NR 3 HINGE POSITION. REPAIRED IAW REO 670-78-34-360 AND HORIZON AIR EA R-78-36.SDR USAA050474Link · out of roundCLT - FOUND UPPER LINK FITTING OUT OF ROUND, RT PYLON. REPAIRED OVERSIZED HOLE IN LINK, FABRICATED REPAIR BUSHING IAW EA 96400. (M)SDR AMTA200500336Bracket · chafedMAIN FRAME, NR 1 ENGINE PYLON WEB UPPER SURFACE CHAFED UNDER BRACKET AT NAC STATION 120. DAMAGE AT PYLON UPPER WEB NAC STATION 120 REPAIRED IAW ER/A NR 757-54R-5846 SEE PARTIAL WORK ABOVE AND M12A NR 747-54R-5846 FOR INDIVIDUAL WORK STEPS. (M)SDR 05FDEA00746Bracket · wornNR 2 ENGINE RT CORE COWL DOOR HOLD OPEN ROD SUPPORT BRACKET ON ENGINE IS WORN. REMOVED AND REPLACED BRACKET, INSTALLING IAW A310-200 AMM 20-21-12.SDR 05FDEA00745Bracket · crackedNR 1 PYLON AFT END AT APPROX RIB 18 1 BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW A310-200 SRM 51-72-10.SDR USAA050530Plate · corrodedBFM - FOUND PANEL FLANGE PLATE CORRODED 4 INCHES LONG BY 2.5 INCHES WIDE BY .05 INCH DEEP, NR 1 PYLON MID FAIRING PANEL FLANGE PLATE. INSTALLED REPAIR SPLICE PLATE PER SRM 54-50-70 AND BOEING DWG 313A1380. (M)SDR QXEA200500532Bracket · crackedPDX - NR 2 ENGINE SPINE COWL FORWARD RIGHT BRACKETS CRACKED. REPAIRED IAW RD 8/4-71-032 AND DHC-8-400 SRM 51-42-05.SDR QXEA200500535Stiffener · crackedPDX - AFT NACELLE, TOP DECK, OUTBOARD ANGLE/LONGITUDINAL STIFFENER CRACKED, 25 INCHES FORWARD FROM AFT END OF NACELLE. REPAIRED IAW SRM 51-42-05, PAGE 20D.SDR QXEA200500569Structure · scratchedYYC - RIGHTHAND NACELLE, AFT CORE COWL SCRATCHED ON OUTBOARD. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01.SDR QXEA200500539Diaphragm · crackedPDX - RIGHT OUTBOARD NACELLE DIAPHRAM CRACKED. REPAIRED IAW DHC-8-400 SRM 51-42-05, SRM 51-40-15 AND RD 8/4-31-155.SDR 2005FA0000403Bracket · crackedEJECTOR COWLING ALIGNMENT BRACKET CRACKED DUE TO VIBRATION. (K)SDR UIEA200500017Cap · chafedDURING SCHEDULED MAINTENANCE, CHAFING MARK WAS FOUND ON THE LEFT SIDE OF THE SKIN ASSEMBLY AT NACELLE STATION 270. AFFECTED FASTENERS WERE REMOVED AND FASTENER HOLES WERE HFEC INSPECTED TO ENSURE CRACK AND DAMAGE FREE CONDITION. THE CHAFING DAMAGE WAS REMOVESDR QXEA200500215Support Bracket · crackedPDX - RIGHTHAND DIAPHRAM SUPPORT BRACKET AT NACELLE TO OUTBOARD WING JUNCTION IS CRACKED. REPAIRED IAW DHC08 400 SRM 51-40-15, 51-42-05 AND 51-42-45.SDR QXEA200500214Support Bracket · crackedPDX - LT DIAPHRAM SUPPORT BRACKET AT NACELLE TO OUTBOARD WING JUNCTION IS CRACKED. REPAIRED IAW DHC-8 400 SRM 51-40-15.SDR QXEA200500403Web · crackedYYC - LEFTHAND NACELLE WEB IS CRACKED JUST ABOVE FLAP TRACK NR 3. REPAIRED IAW RD 8/4-54-155, ISSUE 1 AND Q400 SRM SUB TASK 51-42-05-330-001, 51-40-15-400-001.SDR QXEA200500368Ejector · crackedYYC - LEFTHAND NACELLE AFT EXHAUST EJECTOR AFT TIP CRACKED. REPAIRED IAW RD 8/4-54-016, ISSUE 3.SDR QXEA200500402Anchor Fitting · brokenYYC - RIGHTHAND NACELLE PANEL 424AR ATTACHMENT AREA HAS A BROKEN ANCHOR NUT AND THREE ANCHOR NUTS WITH BROKEN SCREWS STUCK INSIDE. REPAIRED IAW Q400 SRM 51-42-05-330-001, PARAGRAPH E.SDR QXEA200500079Structure · damagedPDX - COUPON CUTOUT ON NR 2 NACELLE. INSTALLED REPAIR DOUBLER IAW EA 2-54-213.SDR QXEA200500044Stiffener · wornYYC - LEFT HAND NACELLE AFT ACCESS PANEL 414AR INTERNAL STIFFENER IS WORN AWAY. REPAIRED IAW RD 8/4-54-218, ISSUE 1 AND HORIZON AIR EA 6-54-324.SDR QXEA200500043Stiffener · wornYYC - RIGHT HAND NACELLE AFT FAIRING PANEL 424AL INTERNAL STIFFENER IS WORN ON ONE END. REPAIRED IAW RD 8/4-54-218, ISSUE 1 AND HORIZON AIR EA 6-54-324.SDR QXEA200500042Stiffener · brokenYYC - LEFT HAND NACELLE AFT FAIRING PANEL 414AL INTERNAL STIFFENER IS BROKEN AT ONE END. REPAIRED IAW HORIZON AIR EA 6-54-324 AND RD 8/4-54-218, ISSUE 1.SDR SWAA043611Strap · crackedDURING SCHEDULED SERVICE CHECK, FOUND STRAP AT NAC STA 234, NR 2 ENGINE PYLON, CRACKED. REMOVED AND REPLACED STRAP PER SRM.SDR QXEA200400865Stiffener · crackedYYC - LEFT HAND NACELLE STATION XN269, ZN10, YN-3 SHEET METAL DECK BELOW EXHAUST DUCT HAS CRACKED STIFFENER. REPAIRED IAW Q400 SRM TASK 51-42-05-330-001.SDR QXEA200400866Intercostal · crackedYYC - LEFT HAND NACELLE UPPER AREA OF ZONE 413 FRAME XN210 OUTBOARD INTERCOSTAL IS CRACKED. REPAIRED IAW Q400 SRM 51-40-15 AND RD 8/4-54-155.SDR 04FDEA03183Adapter · crackedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND NR 2 PYLON JOINT PANEL INTERAL SIDE WITH CRACK. REPLACED ADAPTER RING: ATL7029-91, ATL7029-87, ATL7029-89.SDR QXEA200400806Support Beam · crackedPDX - RIGHT HAND ENGINE OUTBOARD PEC SUPPORT BEAM, FORWARD END, AFT SIDE OF HORSE COLLAR 90 DEGREE ANGLE IS CRACKED. REPAIRED IAW SRM SUBTASK 51-42-05-330-001, PAGE 206, PARAGRAPH E AND SUBTASK 51-40-800-801.SDR UIEA200400195Fairing · delaminatedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, DELAMINATION WAS FOUND ON NR 4 PYLON FAIRING ASSY. AT THE AFFECTED AREA, SKIN AND CORE WERE TRIMMED FROM BOTH IB AND OB SIDES WITH REPLACEMENT CORE, SKIN AND DOUBLERS BONDED IAW SRM 51-40-06. PERFORM DETAILEDSDR UIEA200400194Fairing · delaminatedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, DELAMINATION WAS FOUND ON NR 2 PYLON FAIRING ASSY. AT THE AFFECTED AREA, SKIN AND CORE WERE TRIMMED FROM THE OB SKIN SIDE AND REPLACEMENT CORE AND SKIN WERE SPLICED BY BONDING IAW SRM 51-40-06. IT WAS FURTHERSDR QXEA200400793Intercostal · crackedPDX - LEFT HAND NACELLE OUTBOARD SIDE OF ZONE 413 INTERCOSTAL ATTACHING TO UPPER SKIN IS CRACKED AT STATION XN210.0. REPAIRED IAW RD 8/4-54-155 AND SRM 51-42-05-800-801 AND SRM 51-40-15, PAGE 210.SDR QXEA200400795Intercostal · crackedPDX - RIGHT HAND NACELLE OUTBOARD SIDE, ZONE 623, INTERCOSTAL ATTACHING TO UPPER SKIN IS CRACKED AT STATION XN 210.0. REPAIRED IAW SRM 51-40-15, PAGE 201 AND Q400 SRM 51-25-05-370-801.SDR UIEA200400191Strap · crackedDURING SCHEDULED MAINTENANCE, FOUND CRACK NR 4 PYLON AT AFT MOUNT BULKHEAD FRAME STRAP. SUBJECT CRACK WAS LOCATED ALONG THE STRUT UPPER SKIN ASSY LOWER EDGE. CRACK AFT END WAS CONTAINED WITH A STOP HOLE IN THE STRAP. THE REPAIR AREA WAS NDT INSPECTED, INCLU
Back to JASC 5420