JASC 5414
Service difficulty reports · 4,361
Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 = '5414' 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 = '5414' 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 IXXA06SMN399SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 2 PYLON RIGHT UPPER SKIN CRACKED AT STATION YN210.000. REMOVED LEFT SKIN. REMOVED RIGHT SIDE STRAP AND HINGE HALVES FROM RIGHT SIDE AND ATTACHING PARTS FROM PYLON STRUCTURE AS NEEDED. FABRICATED REPAIR PARTS. SDR IXXA06SMN386SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NR 4 PYLON LEFT UPPER SKIN CRACKED AT STATION YN225.000. REMOVED LEFT PANEL. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SERVICE BULLETIN NUMBER 54-70 DSDR IXXA06SMN385SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 4 PYLON RIGHT UPPER SKIN CRACKED AT STATION YN225.000. REMOVED LEFT SKIN. REMOVED RIGHT SIDE STRAP AND HINGE HALVES FROM RIGHT SIDE AND ATTACHING PARTS FROM PYLON STRUCTURE AS NEEDED. FABRICATED REPAIR PARTS. SDR 2006UALA02151Skin · crackedNR 4 PYLON SIDE SKIN CRACKED AT ACCESS PANEL 482ER CUT-OUT. INSTALLED REPAIR DOUBLER REF SRM 54-50-01 RPR 2.SDR 0602456623Skin · crackedDURING "L" CHECK, FOUND NR 3 PYLON DOUBLER SKIN CRACKED AT BS 180 BULKHEAD CUTOUT. REPAIRED PER EA 66-208301.SDR 2006UALA02159Skin · crackedNR 2 ENG STRUT SIDE SKIN PANEL AT FWD TORQUE BOX ACCESS HOLE CRACKED THRU EXISTING FASTENER, AND VERIFIED AND END MARKED BY HFEC INSPECTION. REQ STRUCTURAL REPAIR MANUAL REPAIR. STOP DRILLED HOLE, NR 2 ENG PYLON OTBD WEB RPR. DRILLING OUT FASTNERS, HAVE MSDR QXEA200602905Skin · bentC3 YYC - RIGHT PYLON UPPER SKIN REBATE FOR PANEL 422OT IS BENT. REPAIRED IAW REO670-54-51-010.SDR USAA061254Skin · crackedLEFT ENGINE PYLON SKIN AT ACESS PANEL 57271 CRACKED. MAJOR REPAIR IAW SRM 54-30-08, DEFECT SIZE: .50 INCH.SDR KCSA061439Skin · crackedNR 3 PYLON I/B SKIN CRACKED AT NAC STA 193 JUST FWD OF PANEL 473CL.SDR HALA0600804Skin · lightning strikeLIGHTNING STRIKE NR 1 ENG O/B FAN INLET COWL 5 O'CLOCK POS 2 FEET AFT OF L/E 2. LIGHTNING STRIKE NR 1 ENG O/B T/R COWL AFT EDGE 5 O'CLOCK POSITION. C/W EXAMINE FCR LIGHTNING STRIKE DAMAGES INSPECTION. REF ITEM 74,75,76,77 AND 80 FOR DAMAGE LOCATIONS. NO OTSDR HALA0600837Skin · brokenNR 2 PYLON SUPPORT FLANGE AND STAINLESS RUB RING FOR TOP SIDE OF ACCESS PANEL 446BR ARE BROKEN. REPAIRED NR 2 PYLON SUPPORT FLANGE AND STAINLESS RUB RING ON TOP SIDE OF ACCESS PANEL 446 BR PER HAL M-105 NR 585O63.SDR 2006UALA01898Skin · dentedUPPER PYLON SKIN AT NR 1 ENG BETWEEN RIB 04 AND 06 JUST FWD OF STA 495 HAS DENTS IN SKIN. AIRBUS TEAM REPLACED CANTILEVER BEAM IN ACCORDANCE WITH REPORT M-300903-EMBOD. "DAMAGE ON THE LT PYLON CANTILEVER WAS FOUND DUE TO EQUIPMENT FAILURE DURING ENGINE CHSDR 06FDEA03462Access Panel · unknownNR 3 PYLON INBD SKIN ACCESS COVER PANEL488BL (PANEL P/N AUB7595-1)(ER/A381467-14) SNRM N00367: NEW PANEL MACHINED AND REPLACED AS PER DRAWING AUB7595.SDR HALA0600794Skin · damagedNR 2 PYLON IB LE TO PYLON GAP COVER PANEL HAS DAMAGE TO EXTERIOR SKIN. REPAIRED NR 2 PYLON I/B LE TO PYLON GAP COVER PANEL, DAMAGE TO EXTERIOR SKIN IAW BOEING DWG 313T1200 REV A AND REV AV, SRM 51-70-17-0G.SDR ANCF200600034Access Panel · loosePILOT REPORT: RT ENG COVER UPPER SIDE SEPARATE DURING TAKE OFF. RT ENG INSPECTED. NO VISIBLE DAMAGE FOUND INTERNAL WING, EMPENNAGE AND FUSELAGE SKIN WERE INSPECTED NO FINDINGS, IAW AMM 05-51-18 PAG 204. THE PANEL 442AL WAS INSTALLED IAW AMM 54-52-01 PAG 401.SDR IXXA06SMN313SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND A NON STANDARD REPAIR ON NUMBER 2 PYLON AT STATION XAR0.000. REMOVED EXISTING NON STANDARD REPAIR FROM STATION XAR0.000 TO STATION XE60.000. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. BONDED PARTS WITH HYSOL. SDR 0602186730Skin · crackedDURING M-CHECK FOUND CRACK IN NR 3 PYLON CAP SKIN FASTENER HOLE NR 43. REPAIRED PER EA 67-207301.SDR DL757060766Fitting · damagedNR 2 PYLON STRUT FITTINGS HAVE ELONGATED HOLES. ACCOMPLISHED PERMANENT REPAIR PER ACTS PRODUCTION PERMIT B757-54-25720. REFERENCE ERA 456938-14.SDR UPS06448239Frame · crackedINSPECTION TYPE:C NR 3 PYLON REAR UPPER ENG MT BULKHEAD O/B FWD FRAME FOUND CRACK AT UPPER PORTION, CRACK LENGTH 1.5". NR 3 PYLON REAR BULKHEAD O/B FWD FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR 0602196730Skin · crackedDURING M-CHECK FOUND CRACKS IN NR 2 PYLON SKIN FASTENER HOLES IN THE FOLLOWING HOLE LOCATIONS 17, 24, 43, 52, 54, 58 AND 67. REPAIRED PER EA 67-207300.SDR UPS06848059Skin · crackedINSPECTION TYPE:C3 NR 1 PYLON INBD SIDE FOUND CRACK AT APPROX STA YN 321. STOP DRILLED CRACK. CRACK TERMINATES AT STOP DRILL EO DC8-5740-0716.SDR QXEA200602551Cowl Door · damagedC4 YYC - RIGHT ENGINE COWL SIDE DOOR 424AR INTERNAL STIFFENER EDGE IS BROKEN OFF AND JAGGED. REPAIRED IAW RD8-71-0528.SDR QXEA200602544Skin · crackedC4 YYC - LEFT ENGINE SIDE COWL DOOR 414AR INTERNAL STIFFENER HAS A CRACKED AND BROKEN EDGE. REPAIRED IAW RD8-71-0528.SDR QXEA200602514Skin · looseC4 YYC - RIGHT NACELLE OUTBOARD SKIN HAS LOOSE AND BROKEN FASTENERS AT STATION XN 1255. REPAIRED IAW RD8-54-1193 AND SRM 51-40-11.SDR EIA2006252Skin · damagedNR 4 PYLON NACELLE STA 180-240 R INTERIOR FOUND SKIN ABRASIVE. SKIN REPAIRED IAW EA 54-0242.SDR 06FDEA03141Skin · crackedNR 2 ENGINE INLET INTERIOR SKIN IS CRACKED AT TE 12 O`CLOCK. REPARIED NR 2 ENGINE INLET SKIN PER SRM 54-10-3.SDR 2006UALA01688Skin · crackedNR 1 ENG PYLON INBOARD SIDE 2 INCH CRACK OUTER SKIN OUT OF INSPECTION PANEL CUTOUT.SDR KCSA061268Skin · damagedNR 4 PYLON DAMAGED ON O/B SIDE LOWER SKIN EDGE APPROX NAC STA 233 ON PREVIOUS REPAIR.SDR KCSA061266Skin Panel · wornNR 4 PYLON INBOARD SIDE LOWER SKIN IS WORN THROUGH SKIRT AREA AT NAC STA 236.SDR AALA20060818Skin · damagedAFW - LEFT HAND PYLON INBOARD AND OUTBOARD SKIN AT STATION 250 HAS GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. AREA OF DISCREPANCY FOR INBOARD IS THREE INCHES BY 0.9 INCH WITH A DEPTH OF 0.055 INCH. AREA OF DISCREPANCY FOR OUTBOARD IS 2.5 INCHES BY 1 INCSDR HALA0600605Panel · crackedLEFT PYLON INBOARD SIDE PANEL NR 437AR CRACKED AND PIECE MISSING. REMOVED AND REPLACED PANEL NR 437AR. CONDITION AND SECURITY CHECK OKAY.SDR AALA20060815Skin · damagedAFW - LEFT AND RIGHT HAND PYLON OUTBOARD SKIN AT STATION 250 HAS GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. BLENDED GROOVE PER MRB 767 2859 AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS. NO CRACKS FOUND. SYSTEM GROUND CHECKED NORMAL OSDR UIEA200600218Skin · crackedPYLON NR 2 ACCESS PANEL 462AL CUTOUT FOUND A CRACK NAC STA 220 0.75 INCH LONG. CARRIED OUT HFEC INSPECTION AS PER NTM PT 6 51-00-00 FIG 23 & 16. NIL CRACK INDICATION. CRACK ON SKIN WAS TRIMMED OUT & HFEC INSPECTED & REPAIR AS PER FAA FORM 8100-9.SDR UPS06448125Skin · crackedINSPECTION TYPE:C NR 4 PYLON CAP SKIN SUSPECT CRACK AT SHEARED RIVET AREA, CRACK LENGTH 1/4". NR 4 PYLON CAP SKIN REPAIRED AS PER HX TOWS NO T-747-54-0224 AND RS R54-51-35569 AND UPS ENGINEERING FILE NUMBER 747-54-20055.SDR QXEA200602073Skin · crackedPDX C4 CRACK AT RIGHT HAND NACELLE FORWARD OUTBOARD SKIN CUTOUT CORNER FOR RIGHT HAND MAIN LANDING GEAR. REPAIRED IAW RD 8-54-873.SDR QXEA200602003Skin · dentedPDX C4 OUT DENT AT APPROXIMATELY X287.400, 3' BELOW RIGHT HAND LOWER STRAP. REPAIRED IAW DHC-8-200 RD 8-53-2181.SDR UPS06547459Skin · chafedNR 1 ENGINE PYLON UPPER SKIN CHAFED AT NS-120 LT SIDE HYD PRESSURE LINE BRACKET. REPAIRED NR 1 ENGINE PYLON SKIN IAW GOODRICH ER NR 06-2698, UPS EO B757-5430-24781-A DTD 27JUL06.SDR KCSA061240Doubler · crackedNR 4 PYLON I/B SKIN DOUBLER AT NAC STA 180 CRACKED.SDR ASAA0640809Skin · chafedRT PYLON IB SKIN CHAFED AT LE. REPAIRED PER EA 5430 01150.SDR UPS06447398Skin · wornNR 4 PYLON INNER VERT WEB O/B SIDE SKIN WORN THROUGH GREATER THAN 50% OF THICKNESS ALONG THE ENTIRE LENGTH DUE TO CONTACT WITH THE CORE COWL. FABRICATED REPAIR DOUBLER FROM .125 2025-T3, DRILLED AND COUNTERSUNK PER B747 SRM 54-30-03 FIG 35 AND 36. INSTALLED SDR UPS06447397Skin · wornNR 4 PYLON INSIDE VERT WEB INBD SKIN WORN THROUGH AT AFT END PEELING AND MISSING AT FWD END. DRILLED OFF INNER STAINLESS AND TRIMMED OUT DAMAGE SKIN 1" BY 9.5". DAMAGE REGLUED. TRIMMED OUT ADDITIONAL DAMAGE. FABRICATED AND DRILLED DOUBLER AND FIRE SHIELD PSDR QXEA200601979Panel · damagedPDX C3 LEFT HAND NACELLE PANELS 413AT AND 414AT HAVE SEVERAL AREAS OF CHIPPED PAINT. PAINTED IAW DHC-8-400 SRM 51-25-05-370-801.SDR UIEA200600181Skin · crackedPYLON NR 4 ACCESS SKIN CUTOUT AT NAC STA. 273.09, PANEL 483AL, HAS A 0.750 INCH LONG CRACK AT UPPER FORWARD CORNER. ACCOMPLISHED SKIN PERMANENT REPAIR IAW SRM 54-31-03 FIG. 6.ALSO, REFERENCE EO 4754A231.SDR UIEA200600180Skin · crackedPYLON NR 4 ACCESS SKIN CUTOUT AT NAC STA 281.34, PANEL 483AL, HAS A 1.0 INCH LONG CRACK AT LOWER AFT CORNER. ACCOMPLISHED SKIN AND INNER DOUBLER PERMANENT REPAIR SRM 54-31-03 FIG. 6.ALSO, REFERENCE EO 4754A231.SDR AWXA200601338Skin · scratchedSCRATCH ON L2 DOOR EXTERNAL SKIN 20 IN UP FROM LOWER EDGE AND 21" AFT FROM FWD EDGE. REPAIR ON L2 DOOR EXTERNAL SKIN 20 IN UP FROM LOWER EDGE AND 21 IN AFT FROM FWD EDGE IAW SRM A320 52-10-00 FIG 206 AND PROTECTIVE TREATMENT APPLIED IAW SRM A320 51-21-11 AND SDR DL76S060584Fitting · crackedTHE FORWARD UPPER SPAR FITTINGS ARE CRACKED AT A FASTENER HOLE. THE HOLES WERE OVERSIZED TO REMOVE THE CRACK AND BUSHINGS WERE INSTALLED.SDR QXEA200601856Skin Panel · crackedPDX C4 - CRACK IN OUT SKIN PANEL OF THE RIGHT HAND ENGINE COWLING. REPAIRED IAW HORIZON AIR EA 2-71-317.SDR AALA20060808Skin · damagedAFW - LEFT AND RIGHT HAND PYLON SKINS AT STATION 250 HAD GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. GROOVE WAS BLENDED AND HIGH FREQUENCY EDDY CURRENT INSPECTION PERFORMED. NO CRACKS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR UIEA200600170Skin · crackedPYLON NR 2 FORWARD ACCESS PANEL CUTOUT SKIN AND DOUBLER HAS A 1 1/16 INCH CRACK AT LOWER AFT CORNER. ACCOMPLISHED SKIN AND INNER DOUBLER REPAIR AS PER 747 SRM 54-31-03 FIG 6 AND REFERENCE ATLAS AIR XEO NR 54-070806-2.SDR CALA0600283Skin · crackedINSPECTION FOUND NR 2 PYLON I/B MID-SPAR AREA ONE EACH FASTENER HOLE HAD A 0.06" CRACK IN SKIN AT STA 285. THE SKIN WAS REPAIRED IAW ECRA 5430-01784.
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