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 IPXA09557141Bracket · crackedINSPECTION TYPE:C1 CRACK IN BRACKET LOCATED BEHIND NR 1 PYLON ACCESS PANEL 435AR LWR FWD CORNER (MARKED). BRACKET WAS REPLACED PER SRM 51-40-02-0G.SDR IPXA09557140Attach Fitting · chafedINSPECTION TYPE:C1 NR 1 STRUT AFT ATTACH POINT FOR PANEL 434BL CHAFED. REMOVED AND REPLACED FILLER IAW SRM 54-51-71-141; SRM 51-40-02-0G; SRM 51-40-05-0G; DRW 313N3033.SDR UIEA201000163Insulation · damagedUPON REMOVAL OF THE NR 2 ENGINE FOR REPLACEMENT PURPOSES THE NR 2 STRUT LOWER WEB INSULATION BLANKET ("HEAT SHIELD") WAS FOUND DAMAGED WITH MISSING MATERIAL. "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR BY INSTALLING A REPAIR DOUBLER MADE FROM SS 301SDR UIEA201000177Fairing · crackedENG 3 OTBD CORE COWL UPPER AFT AREA FAIRING HAS A CRACK. ON THE AFT UPPER EDGE. DUE TO NO STOCK FOR THE PANEL, DISPOSITION WAS TO ACCOMPLISH A TIME LIMITED REPAIR BY WELDING THE CRACK IAW STANDARD PRACTICES AND REPLACEMENT OF FAIRING WITHIN THE NEXT 2A CHECK.SDR USAA2009091592540Fitting · corrodedSAL - Q6 - MAJOR REPAIR - CORROSION ON RIGHT SIDE OF NR 2 ENGINE PYLON OUTBOARD MID SPAR FITTING. REPAIRED RIGHT SIDE OF NR 2 ENGINE PYLON OUTBOARD MID SPAR FITTING IAW US AIRWAYS EA 132556.SDR IPXA09556938Channel · chafedINSPECTION TYPE:C 2 RT PYLON PANEL 495BL IS CHAFED ON THE FWD INTERIOR SURFACE. REMOVED AND REPLACED PYLON PANEL 445BL CHANNEL P/N 313N 3022-102 IAW SRM 51-30-01-0G.SDR IPXA09556936Channel · chafedINSPECTION TYPE:C-2 LEFT PYLON PANEL 435BL IS CHAFED ON THE INNER SURFACE. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02-0G, SRM 51-40-05, AND DWG 313N3022.SDR C2XA09TY202Flange · corrodedNR 1 ENG INLET ATTACH FLANGE HAS CORROSION AROUND BOLT HOLES. REAMED AND INSTALLED BUSHING IAW EC5420-01158.SDR IPXA09556916Support Angle · crackedINSPECTION TYPE:C113 NR 2 ENG AFT STRUT FAIRING AT STA 240 O/B SUPPORT FRAME LWR ANGLE SUPPORT IS CRACKED. REMOVED AND REPLACED LWR SUPPORT ANGLE AT BS 240 IAW SRM 51-40-02-0G, SRM 51-10-02-0G.SDR IPXA09556915Angle · chafedINSPECTION TYPE:C1 ENG NR 2 AFT STRUT FAIRING AT PNL 4451L STRUCTURE FRAME AFT STUP PLATE IS CHAFED. REMOVED AND REPLACED ANGLE AND RUBSTRIP PER SRM 51-40-02.SDR TAMF20090035SFlange · crackedDURING (SC3) CHECKS INSP WAS FOUND CRACKED FLANGE SECTION FROM FWD SEAL SUPPORTS (AIRDAM) ON MARTIN TRANSCOWLS, REPAIRED ACCOMPLISHED IAW EWO 767-54-064 MRA E-MAIL 07-23-09.SDR AALA20090731AFW01Bushing · migratedLEFT PYLON STRUT HAS MIGRATING BUSHING ON THE INBOARD LUG OF THE LEFT PYLON FORWARD UPPER SPAR FITTING. REPAIRED PER ENGINEER AUTHORIZATION.SDR C2XA09TY172Attach Fitting · corrodedNR 2 ENG INLET ATTACH FLANGE HAS CORROSION AROUND 9 NUT PLATE HOLES. REAMED TO REMOVE CORROSION AND INSTALLED BUSHINGS IAW EC5420-01158.SDR KCSA091068Drag Angle · chafedNR 1 PYLON DRAG STRUT HAS CHAFING ON FORWARD LOWER SIDE.SDR SWIA200922309Stiffener · crackedLEFT NACELLE FLAP WELL STIFFENER CRACKED. (C CHECK) REPLACED PER SRM.SDR UALA2009072002122Panel · wornNR 1 PYLON INBOARD PANEL 437ERX HAS 3 EACH WORN FASTENER HOLES. REPAIRED PANEL PER REO G12256, REV A. ACCOMPLISHED TAP TEST. TAP TEST GOOD. REPAIR IS NOW CONSIDERED PERMANENT.SDR UALA2009071702114Structure · damagedNR 1 PYLON HAS SUSTAINED DAMAGE. APPLYING UA-EVA 72783B TIME LIMITED REPAIR. RECEIVED LAST FASTENERS FOR THE DOUBLER REPAIR, INSTALLED & SOLD.SDR FDEA200907172648Fairing · crackedFOUND OLD REPAIR (PATCH) ON LT PYLON AFT FAIRING WITH SMALL DEVIATION (FASTENER PITCH) TO EXISTING OLD RECORDS AND A CLIP IS CRACKED. REPAIR PERFORMED BY REPLACEMENT OF CLIP AND IT IS ACCEPTACLE TO LEAVE THE REPAIR AS IT IS, APPROVED BY RAS ROHR/0998/2008 ANSDR C2XA09TY146Web · crackedNR 1 ENGINE FWD/LWR YOKE WEBBING CRACKED. REMOVED AND REPLACED NR 1 ENGINE FWD/LWR YOKE WEBBING. CLOSEDSDR IPXA09556731Bracket · wornINSPECTION TYPE: C2 NR 2 PYLON - NAC STA 161-35 BRACKET PN 312N3903-126 HOLE IS WORN. REMOVED AND REPLACED WITH FABRICATED REPLACEMENT PART SRM 51-40-02 AND SRM 51-40-05.SDR IPXA09556726Angle · crackedINSP TYPE: C2 ENG NR 1 NAC STRUT AT 12 O-CLOCK, STA 105.66 2 EA BRACKETS ARE CRACKED. REMOVED AND REPLACED BRACKETS IAW SRM 51-40-02.SDR IPXA09556724Bracket · crackedINSPECTION TYPE: C2 NR 1 STRUT BRACKET IS CRACKED, NAC. STA 200, INBD, LWR. REMOVED AND REPLACED BRACKET PER SRM 51-40-02SDR CA090702002Support Bracket · cracked(CAN) AFTER LANDING, CREW OBSERVED A LARGE SECTION OF INBD NR 1 ENG TRANSLATING SLEEVE MISSING. MX MEASURED DAMAGE AT 65 INCHES BY 13 INCHES. ACFT FERRIED BACK TO DEPARTURE WHERE MX OBSERVED INNER ACOUSTIC LINER SEGMENT AT 12 O`CLOCK POSITION, MISSING. SUPPSDR 2009F00051Structure · missingON 6/28/2009 ACFT WAS ENROUTE AT 23000 FEET WHEN THE PILOTS HEARD A LOUD BANG. THEY FOUND THE RT RAISBECK WING LOCKER MISSING. THE FLIGHT CONTINUED AND THEY ELECTED TO LAND. MX WAS INFORMED AND HAS CONTACTED MFG ENGINEERING WHO WILL BE IN ANC 6/30/09 TO TRY ANSDR ASAA0976038Support Bracket · crackedRT WING FIXED TRAILING EDGE FAIRING AFT OF NR 2 PYLON CENTER SUPPORT BRACKET IS CRACKED. REPLACED SUPPORT BRACKET PER AMM 20 50 11.SDR C2XA09TY129Mount · corrodedNR 1 AND NR 2 ENG INLET BOLT HOLES SCARED AND/OR HAVE CORROSION. REMOVED DAMAGE AND CORROSION FROM BOLT HOLES ON INLET MOUNT FLANGE IAW EC5420-01158B.SDR C2XA09TY126Yoke · crackedNR 1 ENGINE LOWER FWD YOKE WEBBING CRACKED. THE LOWER FWD YOKE WAS REMOVED AND REPLACED.SDR IPXA09556531Stand Off · crackedINSPECTION TYPE:C2 NR 2 ENGINE HYD LINE BRACKET CRACKED AT AFT ATTACH SCREW AT 3 O`CLOCK POSITION ON ENG. REMOVED AND REPLACED BRACKET PER RR SPM 70-51-00-400-000.SDR SWIA200922180Channel · crackedLEFT NACELLE CHANNEL CRACKED. (C CHECK) REPLACED CHANNEL PER SRM.SDR CA090618008Angle · broken(CAN) ON ARRIVAL, BLOW-OUT PANEL NR 3302L WAS FOUND OPEN. THIS PANEL PROVIDES ACCESS TO THE RAM AIR DUCT. INSP OF AREA FOUND ANGLE PN 65-49573-23 BROKEN. THIS ALLOWED RAM AIR TO LEAK INTO THE PANEL AREA AND CAUSE PANEL NR 3302L TO BLOW OPEN.SDR HALA2009061500249Retainer · crackedNR 2 ENGINE PYLON T/E FWD LOWER GAP SEAL RETAINER CRACKED. REPAIRED PER HAL M-105 FILE NR 486106.SDR FDEA200906152113Web · crackedN/R206- 5 IN CRACK ON UPPER WEB INBD SIDE NR 3 PYLON APPROX 12 IN. FROM AFT PYLON MOUNT. REMOVED UPPER WEB ATNR 3 PYLON REF SRM 51-00-01. FABRICATED NEW WEB REF DRAWING AUB7031. INSTALLED NEW WEB REF 51-00-01 VOL 1, E.O. 5-5410-7-4311 P2 AND EO 8-5410-7-4311 PSDR FDEA200906152104Fitting · corrodedFOUND CORROSION ON UPPER AND LOWER SPIGOT FITTING REPAIR PERFORMED BY REPLACEMENT OF PARTS IAW SB, APPROVED BY EA 6-5440-120195.SDR FDEA200906152103Fitting · corrodedFOUND CORROSION ON UPPER AND LOWER SPIGOT FITTING REPAIR PERFORMED BY REPLACEMENT OF PARTS IAW SB A300-54-6017, APPROVED BY EA 6-5440-120195.SDR SWIA200922628Beam · crackedLEFT NACELLE HYDRAULIC BAY DOOR CUTOUT OUTBOARD BEAM CRACKED. (C CHECK) REPLACED BEAM PER SRM.SDR IPXA09656264Support Bracket · crackedINSPECTION TYPE:6C NR 2 PYLON - INTERNAL VERTICAL STIFFENER UPPER ATT SUPPORT BRACKET CRACKED AT NAC STA 280 LT SIDE NR 2 PYLON. INTERNAL VERTICAL STIFFENER UPPER ATT SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44 JUST ASDR QXEA2009060100387Support · brokenPDX - C5 - GUSSET SUPPORT FOR RT OTBD NACELLE PANEL 423DR IS BROKEN IN HALF. REMOVED AND INSTALLED NEW BRACKET AND NUTPLATES IAW SRM REV 6 APR 05/2007 TASK 51-42-05-02-01.SDR C2XA09TY102Mount Flange · corrodedTYS - AIRCRAFT CURRENTLY IN A C-CHECK STATUS, INSPECTION FOUND CORROSION IN BOTH LEFT AND RIGHT INLET MOUNTING FLANGES. MAINTENANCE REAMED THE HOLES AND REPLACED BUSHINGS IAW EC 5420-01158. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHESDR ASAA0945732Angle · crackedRT WING NR 2 PYLON SUPPORT ANGLE IS CRACKED AT UPPER INBD SIDE OF AFT FRAME. REMOVED AND REPLACED.SDR SWIA200921943Channel · crackedCHANNEL ON RIGHT FORWARD NACELLE CRACKED. (C CHECK) REPLACED PER SRM.SDR ASAA0945714Support Angle · crackedNR 2 SUPPORT ANGLE CRACKED REMOVED AND REPLACED NR 2 SUPPORT ANGLE.SDR IPXA09555992Angle · chafedINSPECTION TYPE:C1 CHAFED AREA OF ATTACH ANGLE FOR NR 2 PYLON ACCESS PANEL NR 442AL LT SIDE 44.5 INCHES AFT OF FWD END. REPAIRED PER SRM 51-70-11-0G.SDR C2XA09TY092Mount Fitting · corrodedTYS - DURING C-CHECK SMALL PITS WERE FOUND AT 3 MOUNT POINT HOLES ON THE NR 2 ENGINE INTAKE. THE 3 HOLES WERE REPAIRED IAW EC 5420-01158. A/C STILL IN C-CHECK.SDR IPXA09556087Support Bracket · crackedINSPECTION TYPE:C3 WHILE WORKING CC NR 802125 FOUND CRACKED WIRING SUPPORT BRACKET ON NR 2 PYLON INBD. REMOVED, FABRICATED NEW BRACKET FROM 2024 T3 .050 ALUM. CLAD SHEET 876588 ALODINED, PRIMED AND INSTALLED NEW WIRE SUPPORT BRACKET ON THE NR 2 PYLON INBD SISDR C2XA09TY083Mount · corrodedNR 2 ENGINE AIR INTAKE CORRODED AROUND AND INSIDE MOUNTING FLANGE HOLES. REMOVED CORROSION AND ALODINED IAW EC5420-01158. AIRCRAFT IN C-CHECK.SDR UALA2009043001261Pan · damagedNR 1 PYLON LOWER PAN DAMAGE, OUT OF LIMITS. ACCMP'D RE-CHECK INSPECTION OF DENT ON THE BOTTOM OF NR 1 ENGINE PYLON. CHECKED OK TO FOR SERVICE.SDR C2XA09TY065Yoke · crackedTYS - DURING C-CHECK THE NR 1 ENGINE FWD LOWER YOKE WAS FOUND CRACKED AT THE FWD ATTACH POINT. A DYE PEN TEST WAS PERFORMED IAW EMB NDT PTO 1 AND PTO 2 AND THE CRACK WAS CONFIRMED. THE NR 1 ENG FWD LOWER YOKE INNER PIECE WAS REMOVED AND REPLACED IAW EMB 145 SDR C2XA09TY064Yoke · crackedTYS - DURING C-CHECK THE NR 1 ENGINE FWD LOWER YOKE WAS FOUND CRACKED AT THE FWD ATTACH POINT. A DYE PEN TEST WAS PERFORMED IAW EMB NDT PTO 1 AND PTO 2 AND THE CRACK WAS CONFIRMED. THE NR 1 ENG FWD LOWER YOKE INNER PIECE WAS REMOVED AND REPLACED IAW EMB 145 SDR IPXA09555600Swivel · looseINSPECTION TYPE:C4 NR 2 NACELLE STRUT PANEL NR 444AL HOLD OPEN ROD SWIVEL IS LOOSE AND WORN. REMOVED AND REPLACED BASE PER SRM 51-40-02.SDR IPXA09555688Web · chafedINSPECTION TYPE:C4 ENGINE NR 2 NACELLE STRUT FAIRING LOWER WEB IS CHAFED I/B LOWER SURFACE AT PPS 262. REMOVED DAMAGED AND FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-70-13-0G AND SRM 51-30-01-0G.
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