JASC 5420
Service difficulty reports · 3,948
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 FDEA2020060321114Trim Panel · crackedNUMBER 2 ENGINE PYLON INBD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD. REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING. REMOVED AND REPLACED EXTERIOR TRIM IAW SRM 51-40-21 AND DWG A54515187, ISSUE E.SDR FDEA2020060321110Plate · crackedNUMBER 1 PYLON INBD FISH PLATE CRACKED. REMOVED FISH PLATE ON NR 1 PYLON INBD SIDE IAW SRM 51-40-21. LOCATED AND DRILLED NEW FISH PLATE PO 962545.4 AND SHIM PO 972481.1 IAW SRM 51-40-44 AND DWG A54612371 ISSUE B, ASSEMBLED FISH PLATE AND SHIM IAW SRM 51-40-2SDR FDEA2020060111095Fitting · crackedRIGHT STRUT OB LOWER FWD END HAS A CRACKED CLIP. REMOVED AND REPLACED CLIP PART NR 313N3052-17 IAW DWG NR 313N3052 REV B AND SRM 51-40-02.SDR FDEA2020052651043Attach Bracket · crackedLOOSE FASTENERS ON STRUT NR 2 AFT SAILBOAT FAIRING DIRECTLY ABOVE DRAIN TUBES FAIRING REMOVED IAW SRM 51-40-02 WORN FASTENER HOLES FOUND IN FAIRING SKIN AND SUPPORT STRUCTURE, FAIRING ATTACH BRACKET FOUND TO BE CRACKED. REPLACED AFT FAIRING SKIN, SUPPORT CHANNSDR ABXA20200522119Angle · crackedNR 2 PYLON AFT FAIRING UPPER INBD AND OUTBD ANGLES CRACKED. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522118Angle · wornNR 2 OTBD FWD ZEE ANGLE WORN. THE AIRPLANE WAS GROUNDED.SDR SWAA2021081778650Bracket · cracked#1 ENG PYLON AFT STRUT FAIRING AFT OUTBD BRACKET CRACKED / RAR #1 ENG PYLON AFT STRUT FAIRING AFT FITTING (P/N 313A2752-1) IAW SRM 51-40-02 NO FURTHER DEFECTS NOTED. REF SA-M 326 A1126092SDR FDEA2020052660963Fitting · corrodedPITTING CORROSION AT NR 2 ENG FWD MOUNT PYRAMID FITTING O/B AFT HOLE UPPER FLANGE. ACCOMPLISHED EA 6-5450-T0353224 REPAIR. NACELLES / PYLON WING PYLON / STRUT. RIGHT HAND PYLON, FWD ENG MOUNT AFT OUTBD HOLE CORROSION REPAIR CAT "A" REPAIR MAJOR REPAIR.SDR FDEA2020052660962Fitting · corrodedNR 1 PYLON SPIGOT RECEPTACLE FITTING SPHERICAL BEARING/BUSHING CONTACT INSIDE SURFACE HAS RUST/CORROSION. ACCOMPLISHED REPAIR IAW EA 6-5410-T0353242. NACELLES / PYLONS - TAIL AUX NAC STRUCTURE - NR 1 PYLON SPIGOT RECEPTACLE CORROSION REPAIR, FITTING REPLACEMENSDR FDEA2020052260962Fitting · corroded#1 PYLON SPIGOT RECEPTACLE FITTING SPHERICAL BEARING/BUSHING CONTACT INSIDE SURFACE HAS RUST/CORROSION. ACCOMPLISHED REPAIR IAW EA # 6-5410-T0353242. MAJOR REPAIR CAT"A" REPAIRSDR FDEA2020051860963Fitting · corrodedPITTING CORROSION AT NO. 2 ENG FWD MOUNT PYRAMID FITTING O/B AFT HOLE UPPER FLANGE. ACCOMPLISHED EA # 6-5450-T0353224 REPAIR. CAT "A" REPAIR MAJOR REPAIRSDR FDEA2020051860962Fitting · corroded#1 PYLON SPIGOT RECEPTACLE FITTING SPHERICAL BEARING/BUSHING CONTACT INSIDE SURFACE HAS RUST/CORROSION. ACCOMPLISHED REPAIR IAW EA # 6-5410-T0353242. MAJOR REPAIR CAT"A" REPAIRSDR SWAA2020060889725Stiffener · damagedTWO STIFFENERS DAMAGED AT UPPER ATTACH POINTS COMMON TO I/B PYLON RIB & LEADING EDGE SKIN. REPLACED DAMAGED STIFFENERS PER SRM 51-40-02.SDR IPXA2020051855337Web · brokenINSPECTION TYPE:SEG#2 PYLON AFT LOWER AREA AT DRAIN TUBE ACCESSED BY 485AL IS CRACKED/BROKENREMOVED AND REPLACED WEB ASSY. IAW A300 SRM 51-40-21SDR FDEA2020052670910Fitting · corrodedNR 2 ENG PYLON SPIGOT FITTING RECEPTACLE HAS CORROSION. ACCOMPLISHED FINAL EA 6-5450-T0353280. NACELLES / PYLONS - WING PYLON / STRUT - RT WING TO PYLON SPIGOT RECEPTACLE CORROSION REPAIR, FITTING REPLACEMENT PER SB A300-54-6017 CAT "A" MAJOR REPAIR.SDR FDEA2020050870910Fitting · corroded#2 ENG PYLON SPIGOT FITTING RECEPTACLE HAS CORROSION. ACCOMPLISHED FINAL E.A. 6-5450-T0353280. CAT "A" MAJOR REPAIRSDR HYIA20200508003Fitting · corrodedWHILE PERFORMING LIGHTED BOROSCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R2 TO SATISFY AD2017-10-09, A SPOT OF CORROSION WAS IDENTIFIED ON THE RIGHT HAND OUTBOARD NACELLE FITTING (P/N: 5292029-24). THIS CORROSION IS LOCATED ON THE BOTTOM OF THE SDR IPXA2020061556637Structure · damagedINSPECTION TYPE:A300 NR 2 PYLON AFT FIXED FAIRING LT HAS ELONGATED HOLES. REMOVED AND REPLACED T CHORD IAW SRM 51-40-44.SDR IXXA20200519010Mount Bracket · gougedAIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-54-408-00-02 " GVI - EXTERNAL - NO. 2 NACELLE STRUT" LEFT AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 LEFT CORE COWL. REMOVED AND REPLACED LEFT AFT PRECOOLER MOUNT BRACKET IAW B767 SRM SDR HYIA20200508004Fitting · crackedWHILE PERFORMING LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R2 TO SATISFY AD2017-10-09, A CRACK WAS IDENTIFIED IN THE OUTBOARD RADIUS OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES .300 INCHES LONG AND IS CONSISTENTSDR SWAA2021081077600Support Bracket · cracked#2 PYLON REMOVABLE FAIRING HAS CRACK AT THE AFT END WHERE ROD SUPPORT IS ATTACHED. MARKED / REMOVED AND REPLACED AFT FAIRING SUPPORT BRACKET ASSY PER SRM 51-40-02. SEE WIPS AND TASKS FOR INDIVIDUAL SIGN OFFS.SDR 2020F00328Panel · corrodedNON-ROUTINE 2832N283, NR 1 ENG ZONE 433 NACELLE STRUT MID STRUCTURE O/B PANEL, LWR AFT CORNER; FOUND EXCESSIVE CORROSION. REPAIRED NR 1 ENGINE NACELLE STRUT MID STRUCTURE O/B PANEL, ACCOMPLISHED REPAIR ON ENGINEERING ORDER 20192, WITHOUT ANY DEVIATIONS.SDR SWAA2021082094360Support · cracked#1 ENGINE AFT STRUT SUPPRT STRUCTURE CRACKED BEHIND THE TRAILING EDGE ACCESS PANEL 434BL / C/W ECTC# 20-154-00404.SDR JR2R202004282298Panel · crackedPANEL 419NR IS CRACKED AROUND FASTENER HOLES.SDR IXXA20200519013Web · brokenAIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-105-00-01 "DET - FORWARD NACELLE STRUT FAIRING - NACELLE 2 (EZAP)" THE FOLLOWING FINDINGS WERE NOTED:
NUMBER 2 PYLON - WEB AND BRACKET WHICH THE NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARDSDR ABXR2020050600029Web · crackedNUMBER 2 PYLON - WEB AND BRACKET THAT NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD END OF PYLON AT PASS THRU ARE WORN/BROKEN.REPLACE WORE BRACKET IAW B767 SRM 51-40-02, NEW WEB REPLACEMENT DONE ON AMES REA 47404FAB01 ON #2 PYLON FWD END.SDR FDEA2020041730746Structure · damagedDURING BOAT TAIL INSTALLATION, AFT SLING ATTACHMENT TO SKIN FAIRING CAP IS DAMAGED. REPAIRED DAMAGED AREA REFERENCE SRM 54-00-01 FIG. 11 SHT.1 VOL. 1 AND SRM 54-00-01 FIG. 13 SHT. 1 VOL. 1.SDR SWAA2021082340839Tab · crackedLEFT ENGINE FAN COWL AT THE TRAILNG EDGE FLANGE AT 11 AND 1 O'CLOCK HAVE TABS THAT ARE CRACKED / R&R'D LEFT ENGINE FAN COWL TABS AT THE TRAILNG EDGE FLANGE AT 11 AND 1 O'CLOCK PER SRM 51-10-02.SDR FDEA2020041380734Web · dented#2 ENGINE AFT PYLON CENTER SECTION VERTICAL WEB R/H SIDE IS DENTED. FABRICATED/INSTALLED #2 ENG PYLON WEB USING DOUGLAS DRW AVB7318, AVB7023 & AVB7050 AS A REFERENCE.SDR MK1Y20200407001Hinge Fitting · chafedDURING MAINTENENCE AT IAI CHAFING DAMAGE FOUND ON LOWER SURFACE OF HINGE FITTING ASSY P/N 311U2523-5SDR AALA2020040659010Shim · migratedAIRCRAFT IN BASE MAINTENANCE: LEFT WING FRONT SPAR PYLON UPPER INBOARD LINK DRAG FITTING SHIM "C" MIGRATING OUTBOARD. REMOVED DRAG LINK FITTING REPLACED SHIM AND RE-INSTALLED DRAG FITTING PER EA 303618.SDR IPXA2020041754311Web · crackedINSPECTION TYPE:2C#1 PYLON AFT FAIRING WEB/RIB IS WORN AND CRACKED.REMOVED AND REPLACED WEB/RIB IAW SRM 54-05-41. (MINOR)SDR AALA2020040749001Web · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED WEB ON RIB 8A INNER SIDE ON LEFT HAND PYLON. REPAIRED WEB ON RIB 8A PER SRM 54-52-12-300-017.SDR IPXA2020041554233Bracket · crackedINSPECTION TYPE:A300#2 PYLON FWD OF PRE COOLER UPPER MIDDLE BRACKET OF PANELS 423AL AND 424AR BRACKET HAS 1 INCH CRACKREMOVED DAMAGED BRACKET UAW SRN 51-40-21 RECEIVED NEW BRACKET PN 15461198350000 BATCH# 3547345 INSTALLED IAW SRM 51-40-21SDR UIEA2020040200589Support Angle · cracked#3 PYLON AFT V-FAIRING I/B SIDE SUPPORT ANGLE FOUND CRACK(<P>#3 PYLON STRUT INBD SKATE ANGLE CRACK AREA (NEAR STA 456.36) REPAIRED IAW RI-54-56-13962 REV A</P>)SDR SWAA2021082304804Web · crackedRT ENGINE PYLON HAS CACK ON AFT FAIRING WEB CRACK MEASURES 1' PERFORMED INTERIM REPAIR PER EA REPAIR-54EA-07899 / REMOVED AND REPLACED AFT FAIRING TRAILING EDGE ASSY. REF: SRM 51-40-02 & DWG # 313A2752 REF SA-M 326: A1081286SDR SWAA2021082303718Bulkhead · cracked#2 ENG AFT STRUT FAIRING AFT BULKHEAD INBD SIDE HAS 1 1/2' CRACK THROUGH RADIUS / REMOVED AND INSTALLED NEW AFT STRUT FAIRING PER SRM 51-40-02 AND SRM 51-0-02 REF TSR 20200011503; SEE ATTACHMENT A1126086 FOR ALL MAINTENANCE PERFORMED.SDR DALA2020032702048Bushing · wornSHIP 5802 WEAR ON BUSHING (1 EA) IN LOWER ATTACH FITTING AT UPPER LINK STA NAC=160 RH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00574: BUSHING (2EA) IN LOWER ATTACH FITTING AT UPPER LINK RH PYLON WAS REMOVED, FABRICATED AND INSTALLED PER B757/300 SRM. (1537457)SDR SWAA2021081633406Web · crackedCUSTOMER REQUEST SWA REP LC: #2 ENGINE STRUT AFT FAIRING TRAILING EDGE ASSEMBLY PN 313A2752-2 WEB IS CRACKED AT NAC STA 352. / REMOVED AND REPLACED WITH A NEW #2 ENGINE STRUT AFT FAIRING TRAILING EDGE ASSEMBLY I/A/W B737 SRM 51-40-02-0G-0 AND BOEING DRAWING 31SDR IPXA2020041754282Plate · wornINSPECTION TYPE:C#2 PYLON PANEL 485AL HAS FWD R/H ADAPTER PLATE WITH WORN HOLESREMOVED DAMAGE ADAPTER PLATE IAW SRM 51-40-21 RECEIVED NEW ADAPTER PLATE PN 221-0081-326 BAT 3621403 AND INSTALLED NEW ADAPTER PLATE IAW SRM 51-40-21SDR IPXA2020041554200Plate · wornINSPECTION TYPE:A300#1 PYLON PANEL 475AL HAS FWD LH ADAPTER PLATE WITH WORN HOLESREMOVED DAMAGE ADAPTER PLATE IAW SRM 51-40-21 RECEIVED NEW ADAPTER PLATE PN 221-0081-325 BATCH#3608357 AND INSTALLED NEW IAW SRM 51-40-21SDR IPXA2020041554199Plate · wornINSPECTION TYPE:A300#2 PYLON PANEL 485AL HAS FWD LH ADAPTER PLATE WITH WORN HOLESREMOVED DAMAGED PLATE IAW SRM 51-40-21 RECEIVED AND INSTALLED NEW PLATE PN 221-0081-325 BATCH#3808349 INSTALLED IAW A300 SRM 51-40-21.SDR DALA2020032502038Bushing · wornSHIP 5802 WEAR ON BUSHINGS (2EA) IN LOWER ATTACH FITTING AT UPPER LINK STA NAC=160 LH PYLON. CORRECTIVE ACTION:SUMMARY: NRC.00502 BUSHINGS (2EA) WERE REPLACED IN LOWER ATTACH FITTING AT UPPER LINK STA NAC=160 LH PYLON. PER B-757-300 SRM. (1536649)SDR HNAA2020040700120Fitting · crackedLEFT HAND ENGINE PYLON FORWARD YOKE LOWER FORWARD FITTING CRACKED. REPAIRED IAW ETD2020-145-009605 AND EO1-54-20-0147.SDR T17A202003198010Support Angle · crackedLEFT PYLON SUPPORT ANGLES CRACKED, MX REPLACED LEFT PYLON CENTER SUPPORT ANGLES WITH FABRICATED UNITS. ANGLES FABRICATED FROM 2024-T3 .025 IAW BEECHCRAFT SRM 54-10-00 AND SRM 51-30-45, WITH THESE REPAIRS NO REINSPECT IS CALLED OUT IN THE SRM MANUALSDR DALA2020032301993Web · crackedNO.1 PYLON WIRE BUNDLE WEB CUTOUT AT NAC STA255 FOUND CRACK. C/W REPAIRED PER ERA585803-14 (LP 1533339)SDR DALA2020032301991Web · cracked#2 ENG PYLON STRUT UPPER WEB I/B WIRING CUT OUT FOUND CRACKED AT NAC STA223 TO NAC STA235. (LP 1533329)SDR SWAA2021081832079Stop · brokenBROKEN STRUT FAIRING RING STOP ON FWD COMPRESSION ROD AT ENGINE 2 (2 EA) / REPLACED STRUT FAIRING RING STOP ON FWD COMPRESSION ROD AT ENGINE 2 (2EA) IAW B737-700 SRM 51-10-02-0G-0 STEP 9SDR P5CA2020031900100Seal · brokenBROKEN SEAL ASSY, NO. 2 PYLON AFTER FAIRING SIDE PANEL (PNL NO. 446CR) LOWER EDGE.(<P>IAW AMM 71-00-02-004-002 REV. 129 REMOVED THE PANEL NO. 446CR. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 112. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 112 AND DWG NO. 311T25SDR ABXA2020062620097Structure · damagedNR 2 STRUT FWD RT CORNER HAS DAMAGED STRUCTURE. THE AIRPLANE WAS GROUNDED.
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