JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon 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 = '5400' 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 = '5400' 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 DLM88952024Angle · crackedFOUND DURING F-1 LETTER CHECK, NBR 1 ENG UPPER PYLON ATTACH ANGLE CRACKED 1.5 INCHES APPROX 10 INCHES FROM AFT END REPAIRED PER SRM 54-04A FIG 4.SDR ABXA9500405Angle · crackedDURING D-CHECK, FOUND THE NR 1 PYLON LEADING EDGE INTERIOR CRACKED AT STA 237. REPAIRED IAW ABX REA D854-11007.SDR ABXA9500398Spar · crackedDURING D-CHECK, FOUND NR 2 AND NR 3 PYLONS WITH CRACKS ON THE UPPER SPAR CAP. REPAIRED IAW ABX REA D854-11147.SDR AWXA9500280Angle · crackedPHX - DURING C11 INSPECTION, FOUND NR 1 ENGINE PYLON TRAILING EDGE SUPPORT ANGLE CRACKED IN UPPER INBOARD CORNER. REPAIRED PER SRM 51-40-02 AND SRM 51-10-02. NEW ANGLE FABRICATED AND INSTALLED. (W)SDR ABXA9500389Spar Cap · crackedDURING D-CHECK, FOUND THE NR 4 PYLON INBOARD SPAR CAP CRACKED IN TWO PLACES. REPAIRED CRACKED SPAR CAP IAW REA D854-11009MR.SDR C2XA95IA068Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIBS AT LEFT MLG OUTBOARD AFT GEAR DOOR ATTACH POINTS CRACKED. MAINTENANCE STOP DRILLED CRACKS AND INSTALLED DOUBLERS ON AFFECTED RIBS, AND AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (EMB-120 SRM 54-20-04). AIRCRAFT SDR 9507761158Fasteners · brokenDURING PERIODIC CHECK, FOUND BROKEN FASTENERS COMMON TO THE NR 4 BANJO FITTING AFT FLANGE AND THE PYLON CARRY THROUGH CAP. INSTALLED BUSHINGS AND REPAIRED CHANNELS PER EA 11-098170. MFG PART NUMBER AJC7054-1.SDR DLL10951835Splice · crackedBLKD SPLICE TEE CRACKED LT FS 1705 WL 405 VIEWED THROUGH PANEL 313A-1 AND 311UL.SDR DL757951810Lightning Hole · crackedNR 1 PYLON OUTBD LIGHTNING HOLE SHOWS CRACK INDICATION BY E/C ON UPPER AFT CORNER. FOUND AT HMV, REPAIRS ACCOMPLISHED PER DL ERA 270637-14.SDR UPS402981D-Beam · crackedWHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK IN D-BEAM, FRONT SIDE, NR 3 PYLON. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-02.SDR HAL95056Fairing · corrodedSBA - DURING D-CHECK, FOUND RT PYLON AFT FAIRING HAS LEVEL 2 CORROSION AT FUSELAGE ATTACH HOLES AND IN BETWEEN SKIN LAYERS. CUT OUT CORRODED AREA AND INSTALLED DOUBLER REPAIR PER SRM 54-01 FIG 4. (Z)SDR USAA950587Angle · crackedDURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .75 INCH CRACK TOP PYLON TO FUSELAGE ATTACH ANGLE STATION 1019 LEFT PYLON. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 10. (M)SDR 95ZZZW737Angle · crackedSTL - DURING C-CHECK, FOUND .375 INCH CRACK AT TOP PYLON ATTACH ANGLE, STATION 978, LEFT PYLON. REPAIRED PER SRM 54-04, FIGURE 10, SHEET 2.SDR DL72L951702Stiffener · crackedFOUND ON CV2 CHECK, CRACK IN STIFFENER STA 1400 OVERHEAD OF NR 2 ENGINE COMPARTMENT SECTION. REPAIRED PER SRM 54-10-3 AND IDENTIFIED PER PS 900-5-1 FIG 4.SDR 95ZZZW593Fuse Pin · crackedON C-CHECK INSPECTION IAW SB 757-54-0020 EDDY CURRENT INSPECTION REVEALED CRACKED MIDSPAR STRAIGHT FUSE PIN ON LEFT STRUT. REMOVED AND REPLACED CRACKED FUSE PIN.SDR DLL15951397Pan · crackedCRACK IN NR 3 ENG PYLON BOX PAN FWD OF HYD SUPPLY LINE. REF SRM 54-11-00 ITEM 37. CRACK IS TO BE WELDED PER SRM 54-11-00 PG 812.SDR 95ZZZX2034Gasket · brokenINSPECTION FOUND HOT AIR GASKET ON PYLON BROKEN IN TWO PIECES. POSSIBLE FIRE HAZARD DUE TO HYDRAULIC LINES NEAR LEAKS INSIDE PYLON. SUBMITTER SUGGESTS THERE IS NO TIME CHANGE ON GASKETS. AIRFRAME TOTAL TIME, 2992.9. AIRFRAME TOTAL LANDINGS, 2961.SDR 95ZZZW552Foot Stool · crackedDURING AD 93-21-08 PYLON FOOT STOOL FITTING INSPECTION, NR 2 POSITION WAS FOUND TO BE CRACKED APPROX .45 INCHES. STOP DRILLED PER DOUGLAS TELEX REINSPECTION WEEKLY PER SB 57-99.SDR WTAA950142Nacelle · bird strikeSFO - BIRD STRIKE REPORTED AT RIGHT ENGINE NACELLE. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. FOUND SMALL DENT IN INBOARD RT ENGINE INLET COWL ACCESS PANEL. REMOVED DENT FROM PANEL. NO OTHER DAMAGE NOTED TO AIRCRAFT. RETURNED AIRCRAFT TO SERVICE. SDR ABXA9500315Angle · crackedDURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 2 ENGINE LOWER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.SDR ABXA9500314Angle · crackedDURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 2 ENGINE UPPER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-112080-MR.SDR ABXA9500313Angle · crackedDURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 1 ENGINE LOWER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.SDR ABXA9500312Angle · crackedDURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND NR 1 ENGINE UPPER PYLON TO FUSELAGE ATTACH ANGLE TO BE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.SDR 9506146601Spar Web · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE MID SPAR WEB OF THE NR 3 ENGINE STRUT STARTING AT A FASTENER NEXT TO THE INBOARD MID SPAR FITTING RUNNING FORWARD AND UNDER THE FITTING. MADE REPAIR PER EA 66-97901.SDR 95ZZZX2002Angle · crackedMSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANCIS FOUND RT NACELLE UPPER INBOARD WING SKIN TO NACELLE ATTACH ANGLE CRACKED. REPAIR COMPLETED BY FABRICATING NEW ANGLE USING SAME MATERIAL AS ORIGINAL AND INSTALLING.SDR DLL17951537Angle · crackedAT HMV, FOUND NR 2 ENGINE INLET STRUCTURE CRACKED INSIDE PANEL 311UL AND 311UR AT FS 1705 JUST AFT OF NR 2 INLET L/E LIP. REPAIRED PER SRM 54-12-00 FIG 803.SDR DLL17951382Bushing · gougedAT HMV, FOUND BEARING GOUGED, NR 3 PYLON MAIN ATTACH CENTER BEARING. REMOVED BUSHING AND CLEANED BORE. INSTALLED NEW BUSHING PER SRM 54-11-00. HONED BUSHING TO 2.5005, SIZE OK.SDR DLL17951376Bushing · wornAT HMV, FOUND BUSHING WORN ON NR 3 PYLON O/B WING. REMOVED BUSHING AND CLEANED BORE. INSTALLED NEW BUSHING PER SRM 54-11-00 HONED BUSHING TO 2.5005, SIZE OK.SDR UPS802655Stiffener · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON NR 1 PYLON HORIZONTAL STIFFENER AT STA 364-942. REPAIRED PER UPS EO FILE NR DC8-54-0029.SDR DL72S951050Skin · crackedFOUND DURING F-1 LETTER CHECK, CENTER ENG INLET DUCT OUTER SKIN CRACKED .25 INCH RT SIDE FWD OF PNL 9501. REPAIRED PER M/M 54-30-0 FIG 801.SDR ARWA031356Bracket · crackedDURING C-CHECK, FOUND NR 1 PYLON LEFT SIDE CENTER COWL SUPPORT FITTING SUPPORT BRACKETS ARE CRACKED. REMOVED AND REPLACED SUPPORT BRACKETS AS PER SRM 54-2-1. (M)SDR MWEA95148Angle · crackedDURING ROUTINE INSPECTION, THE LEFT PYLON UPPER SURFACE TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED APPROX .25 INCH IN LENGTH. REPAIRED ATTACH ANGLE IAW SRM 54-05 FIG 10. RETURNED A/C TO SERVICE.SDR MWEA95146Angle · crackedDURING ROUTINE INSP, THE ANGLE WHICH SUPPORTS SERVICE PANEL 8105 ON RT PYLON LOWER SURFACE WAS CRACKED APPROX 1.5 INCHES. REPAIRED ANGLE IAW 54-01 FIG 2. RETURNED A/C TO SERVICE.SDR 95ZZZX1762Angle · crackRIGHT PYLON ANGLE RIB HAS 1 INCH LONG CRACK UNDER PANEL NR 8206. REPLACED ANGLE RIB PER SRM 51-30-02. AIRCRAFT TT. 54,495 HRS.SDR 95ZZZX1759Angle · crackRIGHT PYLON ANGLE RIB HAS A .75 INCH CRACK UNDER PANEL NR 8204. REPAIRED ANGLE PER SRM 54-01, FIGURE 2. AIRCRAFT TT, 54,495 HRS.SDR RAAAB295009Cowl · chafedDURING SCHEDULED 6C CHECK, FOUND NR 3 ENGINE UPPER COWL CHAFED BETWEEN 3RD AND 4TH CIRCUMFERENTIAL. REPAIRED PER SRM 54-10-3. (X)SDR 96ZZZM532S-Duct · corrodedDURING C-CHECK, NR 2 ENGINE S-DUCT INTERIOR AT STATION 1203, SKIN IS BULGING AT SPLICE JUST FWD OF PREVIOUS REPAIR. REMOVED CORROSION PER SRM 51-10-6. CUT OUT DAMAGE AREA PER SRM 51-10-3 AND INSTALLED REPAIR AS PER SRM 54-10-3 AND SRM 51-30-2 12 INCH BY 3 INSDR USAA950318Angle · crackedPIT - DURING Q-4 CHECK INSPECTION, FOUND ONE .5 INCH CRACK IN STATION 980 TOP PYLON TO FUSELAGE ATTACH ANGLE RT. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (W)SDR AWXA9500096Former · crackedPHX - FLT 1530 - DURING C7 INSPECTION, FOUND NR 2 ENGINE PYLON FAIRING FORMER CRACKED AT UPPER END IN RADIUS. REMOVED AND REPLACED CRACKED FORMER PER SRM 51-10-02 AND SRM 51-40-02. (Z)SDR DLM88950653Angle · crackedDURING LETTER CHECK, FOUND NR 2 PYLON WEDGE, UPPER SURFACE TO FUSELAGE ATTACH ANGLE CRACKED, REPAIRED PER SRM 54-04 FIG 4.SDR UPS802380Angle · crackDURING 'C' CHECK MAINTENANCE FOUND NR 1 PYLON OUTBOARD ATTACHMENT ANGLE CRACKED. INSTALLED REPAIR IAW SRM 51-1-20D.SDR DLL16950840Angle · crackedDURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS, APPROX 2 INCHES INSIDE ACCESS PANEL 311UL OF NR 2 ENGINE INTAKE (LEFT SIDE OF S DUCT LOOKING UP AND AFT). REPAIRED PER SRM 54-12-00 FIG 803.SDR DLL16950839Angle · crackedDURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS 2 INCHES. CRACK LOCATED INSIDE ACCESS PANEL 311UR, AT NR 2 ENGINE INTAKE. REPAIRED PER SRM 54-12-00 PG 808.SDR IXXA9538Drag Angle · crackedDURING ROUTINE C-CHECK INSPECTION, A 2.200 INCH CRACK WAS FOUND IN THE NR 2 PYLON, INBOARD DRAG ANGLE. AFTER EVALUATION BY DOUGLAS AND FAA DER APPROVAL, THE AIRCRAFT WAS RETURNED TO SERVICE WITH FOLLOW-UP INSPECTIONS REQUIRED AT C-CHECK AND REPLACEMENT REQUIRSDR ARWA0927954Stress Plank · damagedDURING INCIDENT, INSPECTION FOUND NR 4 PYLON INBAORD STRESS PANEL (STATIONARY PLANK) BENT. REMOVED AND REPLACED NR 4 PYLON INBOARD STATIONARY STRESS PLANK PER DAC DRAWINGS NR 5753010 AND 5753000. (M)SDR USAA950292Angle · crackedPIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK RIGHT UPPER PYLON ATTACH ANGLE STATION 1019. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (W)SDR 95ZZZX1522Angle · crackedDURING AN INSPECTION OF THE LEFT PYLON, A .50 INCH CRACK WAS DISCOVERED IN THE PYLON LEADING EDGE ATTACHMENT ANGLE (PN 1159 B21901-20). THE ANGLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ABXA9500174Rib Cap · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK ON THE NR 2 ENGINE PYLON RIB CAP AT STATION YN 170. REPAIRED RIB CAP IAW ABX REA D954-10691-MR.SDR DL757950404Hi-Lock · failed3 FASTENERS LOOSE, 1 FASTENER HAS SHEARED HEAD IN NR 2 PYLON STRUCTURE STA 107.7 AT WL 139.909 (REF DWG 311N3110 SH 1 B-9).SDR DL757950293Structure · crackedDURING L/O, NR 2 ENG WAS REMOVED FOR SCHEDULED MAINTENANCE, FOUND A 1.5 INCH CRACK IN THE INBOARD WEB OF PYLON STRUCTURE AT THE FWD INSPECTION HOLE. REPAIRED PER SRM 54-51-01 FIG 203.
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