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 NOCA03911Angle · crackedA FRAME SUPPORT CRACKED NR 2 PYLON SAIL BOAT FAIRING FWD FRAME AFT SIDE. REMOVED DAMAGED PARTS DRILLED AND INSTALLED NEW ANGLE AS PER SRM 54-52-70.SDR NOCA03811Angle · crackedA FRAME SUPPORT CRACKED SAIL-BOAT FAIRING FED INBD ANGLE AND LOWER AFT SIDE. REMOVED DAMAGED PARTS DRILLED AND INSTALLED NEW ANGLES PER SRM 54-52-70.SDR AALA20110406AFW01Web · crackedCRACKS AROUND THE LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. ACCOMPLISHED REPAIRS PER EA B767-54-015990.SDR FDEA201104051328Support · crackedNR 2 PYLON FWD UNDER WING FAIRING SUPPORT FOUND CRACKED. NR 2 PYLON FWD UNDER WING FAIRING SUPPORT REPLACED BY FABRICATION IAW DWG 313N5004, SHT 1, REV D AND INSTALLED IAW SRM 51-40-02, REV 102. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR AALA20110405AFW01Web · crackedCRACKS AROUND THE RIGHT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. ACCOMPLISHED DOUBLER REPAIR PER EA B767-54-015989.SDR IPXA11566110Angle · crackedINSPECTION TYPE: MOD LT AFT FAIRING STRUCTURE, UPPER INBD AFT WIRE SUPPORT ANGLE IS CRACKED AND BROKEN, PN 287N1112-12. REPLACED IAW SRM 51-40-02-0G.SDR IPXA11566084Angle · gougedINSPECTION TYPE: MOD, RT AFT FAIRING STRUCTURE FWD RT VERTICAL ANGLE IS GOUGED IN RADIUS. REMOVE, FABRICATED AND INSTALL IAW DWG 313N5033 AND SRM 51-40-02.SDR UALA2011040401617Acoustic Panel · damagedON ARRIVAL INNER ACOUSTIC PANEL DAMAGED BETWEEN 3 AND 4 O'CLOCK POSITION 4"X 2"X .25" DENT-PUNCTURE. AREA REPAIRED PER MM 54-00-01 REPAIR 2 AND AREA TAPED.SDR ASAA1149513Structure · chafedNR 1 ENGINE OUTBOARD UPPER FORWARD PYLON CHORD CHAFED LOWER SURFACE. ACCOMPLISHED BLEND REPAIR IAW ASA EA 400 54EA O5296 REV NEW DATED 21 APR 2011.SDR ASAA1149512Structure · chafedNR 1 ENGINE INBOARD FORWARD UPPER PYLON CHORD CHAFED SEVERAL AREAS LOWER SURFACE. ACCOMPLISHED BLEND REPAIR IAW ASA EA 400 54EA O5296 REV NEW DATED 21 APR 2011.SDR ASAA1149511Structure · chafedNR 2 ENGINE PYLON UPPER FORWARD CHORD CHAFED SEVERAL AREAS INBOARD LOWER SURFACE. ACCOMPLISHED BLEND REPAIR IAW ASA EA 400 54EA O5297 REV NEW DATED 21 APR 2011.SDR ASAA1149510Structure · chafedNR 2 ENGINE PYLON UPPER FORWARD CHORD CHAFED SEVERAL AREAS OUTBOARD LOWER SURFACE. ACCOMPLISHED BLEND REPAIR IAW ASA EA 400 54EA O5297 REV NEW DATED 21 APR 2011.SDR DALA1123919871Panel · chafedNR 1 ENGINE PYLON L/E PANEL INNER SURFACE AT UPPER AND LOWER O/B EDGE CHAFED PARTS RACK DL198. BLENDED CHAFED AREA IAW DC9 SRM 54-01 FIG ORIG MAT .070 TITANIUM DMS1536 IAW DC9 SRM 54-30-0 FIG 1. MAT REMOVED .030 MAT REMAINS .040 FOUND OUT OF LIMITS IAW DC9 SSDR UALA2011033101551Angle · crackedNR 2 PYLON CLOSEOUT ANGLE IS CRACKED AT O/B MIDSPAR FTG I/B FASTENER HOLE. REMOVED O/B FITTING I/B BOLT. POLISHED AND CLEANED O/B FTG I/B HOLE. ACP HFEC OF O/B MID SPAR FTG I/B HOLE PER MM. NO CRACK FOUND. ACP HFEC OF O/B MIDSPAR FTG CLOSEOUT ANGLE I/B BOSDR UALA2011033101552Angle · crackedNR 2 ENG PYL OTBD MIDSPAR FTG CLOSEOUT ANGLE INBD BOLT HOLE CRACKED. ACP SMC 017 ACP PER EVA 80724. ON WU E9784H. VERIFIED WITH HFEC CRACK CONTAINED BY STOP DRILL. ACP PER AMT. FASTENERS REMOVED AND OPEN HOLE INSPECTION ACCOMPLISHED. NO CRACKS FOUND.SDR SIMA201108302Linkage · crackedDURING MAINTENANCE BASE VISIT FOUND THE RIGHT ENGINE FORWARD LOWER YOKE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE RIGHT ENGINE LOWER YOKE IAW EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR KCSA111081Fireshield · chafedNR 1 PYLON FIRESHIELD CHAFED NAC STA 221 INBOARD.SDR KCSA111080Fireshield · chafedNR 2 PYLON FIRESHIELD CHAFED NAC STA 221 INBOARD.SDR KCSA111079Fireseal · crackedNR 2 PYLON FIRESEAL CRACKED NAC STA 221.SDR AALA20110321AFW02Pylon · crackedCRACK WAS FOUND FROM THE FORWARD INBOARD RADII OF THE POWER FEEDER CABLE PASS THROUGH HOLE JUST AFT OF RIGHT PYLON STATION 221.25. ACCOMPLISHED DOUBLER REPAIR PER EA 015770.SDR AALA20110321AFW01Pylon · crackedCRACK WAS FOUND FROM THE FORWARD INBOARD RADII OF THE POWER FEEDER CABLE PASS THROUGH HOLE JUST AFT OF LEFT PYLON STATION 221.25. ACCOMPLISHED DOUBLER REPAIR PER EA 015771.SDR A6WA201140202Angle · crackedLT PYLON PANEL 410BT ANGLE CRACKED. R & R LT PYLON PANEL 410BT ANGLE IAW SRM 51-42-06.SDR AALA20110314AFW01Web · crackedCRACKS AROUND THE LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. ACCOMPLISHED DOUBLER REPAIR PER EA B767-54-015644.SDR AALA20110316DWH03Skate Angle · crackedIN LINE CRACK IN THE LEFT OUTBOARD NACELLE SKATE ANGLE FOR THE AFT FAIRING. ACCOMPLISHED REPAIR PER EA B767-64-005449.SDR UALA2011031001158Bracket · damagedNR 1 ENG AFT RT CORE COWL AFT HOP TIE SUPPORT DAMAGED. REMOVED BRACKET ASSY. INSTALLED BRACKET ASSY.SDR A6WA201140240Track · chafedRT UPPER AND LOWER PYLON TRACK CHAFED. BLENDED OUT CHAFED DAMAGE ON RT UPPER AND LOWER PYLON TRACK FOUND REMAINING MATERIAL TO BE WITHIN LIMITS, IAW B/A REO 601R-78-34-3479 UPPER TRACK REMAINING THICKNESS .117 LOWER TRACK REMAINING THICKNESS .120. REQUIRED RSDR UALA2011030301050Panel · missingNR 4 ENGINE INTERMEDIATE CASE STRUT FAIRING AT APPROX 7 O'CLOCK POSITION, INNER PANEL MISSING. INSTALLED AND SECURED PANEL TO NR 4 ENG STRUT FAIRING.SDR DALA1115249877Angle · crackedCRACK ON SUPPORT ANGLE AT PYLON 2 WEB BEHIND PNEUMATIC DUCTS /FIRE SHIELD ACCESS THRU DOOR 8206A. DRILLED .025 STOP HOLE AT END OF THE CRACK IAW DC-9 SRM 54-01 FIG 2 SHT 3 HFEC INSPECTION STOP DRILL AND NO PROG NOTED FABBED NEW REPAIR ANGLES 2 EA. HFEC SURFASDR DALA1114426315Fitting · corrodedCORROSION WAS FOUND ON O/B SIDE STRUT AFT BULKHEAD FITTING BEARING OF NO 3 STRUT TO WING. DSB BEARING CORRECTED PER CARD 5441-01068-03C.SDR USAA2011031891145Hinge Fitting · excess playSAL - S5 - MAJOR REPAIR - MIGRATED BEARINGS ON NR 1 ENGINE T/R HINGE FITTINGS ON OUTBOARD SIDE AT AFT & MIDDLE POSITIONS AT PYLON STA 5930/RIB 1 & 6174/ RIB 2. REPLACED NR 1 ENGINE T/R HINGE FITTINGS ON OUTBOARD SIDE AT AFT & MIDDLE POSITIONS AT PYLON STA 593SDR DALA1117259870Stiffener · crackedNR 1 ENGINE PYLON UNDER PANEL 8101A FWD STIFFENER CRACKED AT I/B END. REMOVED CRACKED STIFFENER ON NR 1 ENGINE PYLON UNDER PNL 8101A IAW DC-9 SRM 51-30-5, 51-30-2. FABBED, FORMED, DRILLED, COUNTERSUNK NEW STIFFENER FROM .040 2024-T3 IAW DC-9 SRM 54-10-0 FIG SDR V0XR20110226002Diaphragm · cracked(V0XR) DIAPHRAGM AND CHANNEL ON RT THUMBNAIL REQUIRES REPLACEMENT DUE TO CRACKS. REPLACED DIAPHRAGM P/N A23837-1 AND CHANNEL P/N A23840-1 ON RT THUMBNAIL IAW DHC8-100 SRM 51-10-00, 51-40-11.SDR V0XR20110226001Stiffener · cracked(V0XR) STIFFENER AT O/B YN 3.75 AND XN 169-244 HAS CRACKED OUT HOLES. FABRICATED STIFFENER AND INSTALLED AT YN 3.75 AND XN 169-244, LT NACELLE IAW DHC8-100 SRM 51-40-205, 51-40-07, 51-20-36 AND DRAWING 85410739.SDR UALA2011022800986Retainer · looseNR 2 NACELLE AFT STRUT FAIRING LOWER HEAT SHIELD SEAL RETAINER HAS 6 LOOSE ATTACHMENT FASTENER. ACCOMPLISHED INTERIM REPAIR REF MT 54-UA1. RE-INSPECT EVERY 3 SERVICE AND PERMANENT REPAIR AT C CHECK. OK TO CF9 PER OPBLM.INTERIM FASTENERS ARE 3,5, 9,11,15, AND SDR V0XR20110225002Angle · cracked(V0XR) RT THUMBNAIL O/B FWD RT ANGLE CRACKED. REPLACED O/B FWD RT ANGLE ON RT THUMBNAIL IAW DASH8-100 SRM 51-40-11 AND 51-10-00.SDR USAA2011031791087Sleeve · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON RIGHT PYLON SPIGOT SLEEVE AT WS 3758, RIB 7. REPLACED RIGHT PYLON SPIGOT SLEEVE AT WS 3758, RIB 7 IAW A320 AMM 57-26-00.SDR IPXA1565043Bracket · crackedINSPECTION TYPE:MOD, NR1 PYLON UPPER AFT INBD BRACKET ASSY IS CRACKED IN RADIUS, PPS 187, RBL 10, PN 312N5817-36. REPLACED BRACKET IAW SRM 51-40-02-0G.SDR USAA2011031791089Spherical Bearin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON LEFT PYLON SPIGOT SPHERICAL BEARING AT WS 3758, RIB 7. REPLACED LEFT PYLON SPIGOT SPHERICAL BEARING AT WS 3758, RIB 7 IAW A320 AMM 54-51-41.SDR MU1Z2011020200002Angle · crackedDURING HFEC INSPECTION CLOSE OUT ANGLE OF THE RT PYLON WAS FOUND CRACKED.SDR CALA2011022300106Attach Angle · corrodedSUPPORT TASK: NR 1 SAILBOAT AFT HEAT SHIELD ATTACH ANGLES AND WEB CORRODED. REPAIRED PER ECRA 5450-01862. ACCOMPLISH A PERMANENT REPAIR WITHIN 30 MONTHS FROM 21-FEB-2011. INTERIM REPAIR ACCOMPLISHED ON NR 1 PYLON, AFT FAIRING LWR CHORD AS PER ECRA 5450-01862SDR CALA2011022300105Attach Angle · corrodedSUPPORT TASK: NR 2 ENG SAILBOAT AFT HEAT SHIELD ATTACH ANGLE AND WEN CORRODED. REPAIRED PER ECRA 5450-01863.SDR FDEA201102210659Pan · gougedNR 2 STRUT AFT FAIRING LOWER EXTERNAL SURFACE INBD SIDE HAS PUNCTURE AT PP STA 260.48. PUNCTURE ON NR 2 STRUT AFT FAIRING REPAIRED IAW EA F-5480-146403 (RT PYLON AFT FAIRING PAN GOUGE REPAIR). REPAIR IS CLASSIFIED AS MINOR.SDR FDEA201102210658Pan · damagedNR 1 STRUT AFT FAIRING LOWER SURFACE INBD SIDE HAS PUNCTURE AT PP STA 260.48. PUNCTURED SKIN ON NR 1 STRUT AFT FAIRING REPAIRED IAW EA F-5480-146402 (LT PYLON AFT FAIRING PAN GOUGE REPAIR). REPAIR IS CLASSIFIED AS MINOR.SDR DALA1112619881Angle · crackedMONITOR BLIND FASTENER-LEFT ENGINE PYLON STA 1151 UPPER PYLON TO FUSELAGE ANGLE CRACKED APPROX 1 INCH CUT OUT DAMAGED AREA 2.5 INCH BY 1 INCH. NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABBED AND INSTALLED 1 FILLER AND SPLICES. HEAT TREATED TO STA SDR DALA1118800136Strap · cracked767 SIP MOD (GE ENGINE)-RT WING (01EA) FASTENER HOLE ON NR 2 STRUT STRAP ,CHORD P/N :311T3156-1 FOUND GOUGED WHEN ACCOMPLISHING SB 767-54-0081 FIG 7 OPEN HOLE. HFEC INSPECTION, DAMAGED FASTENER HOLE 01 EA AT NR 2 PYLON I/B FWD MOST HOLE COMMON TO MID SPAR FSDR AALA20110217TUL06Isolator · damagedRIGHT ENGINE PYLON ISOLATOR GRAY RUBBER O-RING SEALANT LOOSE. NEW ISOLATOR INSTALLED PER MM 71-20-00-04.SDR ZZDA2011170Structure · crackedLEFT PYLON APRON UPPER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED AFT HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.SDR IPXA11564862Angle · crackedINSPECTION TYPE:C3, NR 1 PYLON AFT FAIRING STRUCTURE LOWER BRACKET FOR SUPPORT BETWEEN PANELS 435AR AND 435BR IS CRACKED. R & R BRACKET IAW SRM 51-40-02.SDR IPXA11564861Bracket · brokenINSPECTION TYPE:C3, NR 1 PYLON AFT FAIRING STRUCTURE LOWER BRACKET FOR SUPPORT AT FWD END OF PANEL 435AR IS BROKEN. R & R SPRING CLIP IAW SRM 51-40-02.SDR JR2R2011021100010Plate · corroded2 PYLON UPPER SURFACE HAS CORROSION 8 INCHES FR T/E 23 INCHES AND 10 INCHES O/B OF FUSELAGE. REPAIRED 2 PYLON UPPER SURFACE IAW CRJ 200 SRM 51-22-00 AND SRM 51-42-10, NOTE THE CORRODED PART ON PYLON IS A BONDING PLATE.
Back to JASC 5420