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 DL72S000323Skin · crackedFOUND ON F2 LETTER CK, .75 INCH CRACK S-DUCT HOUSING SKIN AT PANEL 9524 RT. REPAIRED PER MM 54-30-0.SDR MALA000150Skin · chafedDURING C-CHECK, FOUND CHAFED LT AND RT NACELLE SKINS CAUSED BY THE WING LEADING EDGE SEAL. MAINTENANCE REPAIRED IAW EO NR S54025.SDR SIMA04515Skin · crackedSBP - DURING MBV, FOUND LEFT NACELLE INBOARD SIDE HAS CRACK BEYOND LIMITS. INSTALLED FABRICATED DOUBLER IAW SAAB STATEMENT 340SDS00870. (M)SDR USAA000165Doubler · crackedCLT - FOUND CRACKED DOUBLER .5 INCHES, LOWER FORWARD CORNER CUTOUT PANEL 433GR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA66547. (M)SDR USAA000164Doubler · crackedCLT - FOUND DOUBLER CRACKED AT CUTOUT PANEL 433AL AT LOWER FORWARD CORNER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA66547. (M)SDR TWAA0002402Fastener · looseDURING OP 16 MAINT CHECK FOUND NUMBER 1 PYLON TOP AFT SKIN HAD 4 ROWS OF BLIND FASTENERS LOOSE AND WORKING. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 9957742, 9915500, 9915501, 9915502, AND 9915503.SDR TWAA0002316Fastener · misinstalledDURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, TOP OF PYLON SKIN INBD OF AFT ENGINE MOUNT HAD ROW OF SCREWS WITH SKIN WASHERS LOOSE AND IMPROPERLY INSTALLED. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 9957742, 9915500, 9915501, 9915502 AND 9915503.SDR DHL200080385CPanel · crackedAT C-CHECK, NR 614 ACCESS DOOR CRACKED 1 INCH AND 8 LOOSE RIVETS ON RT - LT UPPER AND LOWER EDGE. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21A PG 4 & SRM 51-1-21 PG 7. N/R 4291SDR 2000UALA00032Access Panel · crackedFOUND ON WALKAROUND NR 1 AND NR 2 AFT STRUT MOUNT BOLT ACCESS PANELS INBOARD SIDE SEVERLY CRACKED WITH 2 PULLED SCREWS EACH PANEL. PANEL P/N 313T3200-351 AND 352- M615100 F. CRACKS ON NR 1: 3 IN AND 4 IN; NR 2 ONE CRACK 2 IN. SIMILAR CONDITION NOTED ON OTHESDR 2000UALA00026Skin · damagedON CREW WALKAROUND FOUND NUMBER 2 ENGINE AFT FAIRING TRAILING EDGE DAMAGED. *S/D* THE NR 2 ENGINE AFT FAIRING TRAILING EDGE WAS FOUND DAMAGED. CAUSED BY CRACKING OF THE SUPPORT CHANNEL AVB7021-29 AND TRAILING EDGE AVB7021-503. THE SUPPORT CHANNEL AND TRAILSDR DHL200071757DAccess Panel · damagedAT D CK, NR 1 ENG PYLON UPPER SURFACE AFT ACCESS PANEL HAS A HOLE IN S/M. INSTALLED FIBERGLASS OVERLAY REPAIR PER B727 SRM 51-40-8 FIG 1. REF: N/R 6512.SDR CALA9901734Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN UPPER FORWARD CORNER SKIN OF LT AFT NR 2 ENGINE COWL. THE CRACKED AREA WAS CUT OUT, A DOUBLER AND FILLER WERE INSTALLED IAW SRM 54-30-3, 51-10-2, AND 51-30-2.SDR CA000209036Panel · delaminated(CAN) PANEL NEAR LEADING EDGE OF NR 4 PYLON FOUND DELAMINATED. PANEL REPLACED.SDR QXEA9902701Skin · crackedPDX - RIGHT NACELLE EXTERIOR OUTBOARD SKIN HAS .250 CRACK FROM RIVET HOLE TO SKIN PANEL EDGE AT STATION XN122.00 AND YW171.200, ALSO HAS LOOSE WORKING RIVET IN SAME AREA JUST AFT OF PANEL 426AR. REPAIRED IAW HORIZON AIR EA 9-54-239.SDR QXEA9902696Guard · wornPDX - INBOARD MIDDLE GRAVEL GUARD ATTACH POINT WORN EXCESSIVELY THIN. REPAIRED IAW RD8-54-41.SDR CALA9901655Skin · dentedINSPECTION FOUND BOTTOM OF NR 3 ENGINE COWL SKIN DENTED AND SCRATCHED BETWEEN STIFFENERS 9 & 10. THE DAMAGED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 54-30-3.SDR QXEA9902700Skin · crackedPDX - RIGHT NACELLE EXTERIOR INBOARD SKIN HAS 1.5 CRACK AT STATION XN127.5 AND YW139.200, JUST AFT OF PANEL 425AL TOP EDGE. REPAIRED IAW DHC-8 SRM 51-40-11.SDR USAA991379Skin · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK TOP FORWARD CORNER OF ACCESS DOOR 5724L CUTOUT SKIN. INSTALLED DOUBLER PER TR 54-50-040. (M)SDR QXEA9902637Skin · damagedYXX - LEFT FORWARD LOWER NACELLE STRUCTURE ADJACENT TO LOWER COWL HINGE POINTS DAMAGED. REPAIRED IAW RD8-54-063.SDR DLM90992757Panel · separatedON ARRIVAL DFW FOUND NR 2 ENGINE C-DUCT ACCESS PANEL BLOWOUT DOOR MISSING. UPPER C-DUCT COWL DAMAGED BY DOOR. REPLACED UPPER REVERSER HALF AND RIGGED PER MM 78-32-00. REPLACED AND ADJUSTED BLOWOUT DOOR.SDR MALA976648Skin · chafedDURING HEAVY CHECK INSPECTION FOUND RIGHT INBOARD NACELLE SKIN CHAFED. MAINTENANCE PERFORMED PERMENANT REPAIR IAW EO NR S54022.SDR MALA976647Skin · chafedDURING HEAVY CHECK INSPECTION FOUND CHAFED SKIN ON LEFT INBOARD NACELLE SKIN. MAINTENANCE PERFORMED PERMANENT REPAIR IAW EO NR S54021.SDR AT9900868Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION AROUND SCREW HOLES ON NR 1 ENGINE PYLON L/E PANEL, MATERIAL LOSS WAS MORE THAN 20 PERCENT, THIS IS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 54-30 FIG 1, 51-10-04SDR USAA991211Skin · crackedCLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON NR 2 ENGINE PYLON AT ACCESS PANEL NR 5824R UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER PER EA 65982 AND TR 54-50-04D. (M)SDR CALA9901465Panel · gougedINSPECTION FOUND NR 1 ENGINE PYLON ACCESS PANEL NR 5727L CUTOUT GOUGED IN TWO PLACES. REPAIRED IAW ECRA 5430-01581.SDR CALA9901451Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON PRE-COOLER CUTOUT AT RT SIDE. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH A REPAIR ANGLE IAW ECRA 5450-01283.SDR USAA991137Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT ACCESS PANEL OUTBOARD EDGE CUTOUT PYLON SKIN. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR QXEA9902255Skin · dentedPDX - DENT ON INBOARD SIDE OF LEFT NACELLE AT APPROXIMATELY XN 155.30 AND ZN 24.25. REPAIRED IAW SRM 54.30.21, PAGE 2, FIGURE 2.SDR 9904569618Skin · wornDURING INSPECTION, FOUND NUMBEROUS LOOSE FASTENERS ON NR 1 PYLON. REPAIRED PER EA 99-097710.SDR 2000ZZZX703Skin · crackedAFT LEFT COWL DOOR HAS 3 INCH CRACK OUTSIDE SKIN AT INLET SCOOP NR 3 ENGINE. STOP DRILLED, NDT CONFIRMED CRACK HAS BEEN STOPPED. WELDED CRACK AND NDT NO FLAWS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-8-99. REF: ZANSDR QXEA9902253Skin · chafedPDX - RIGHT NACELLE EXHAUST FINGERNAIL DECK HAS 1 .5 BY .75 HOLE CHAFED THROUGH AT STATION XN 224.76. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 THROUGH 4.SDR QXEA9902252Skin · chafedPDX - RIGHT NACELLE EXHAUST FINGERNAIL DECK HAS DEEP CHAFE MARKS AT STATION XN 224.76. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 THROUGH 4.SDR QXEA9902251Skin · chafedPDX - RIGHT NACELLE UPPER DECK FOR EXHAUST FINGERNAIL IS CORRODED AND HAS SEVERAL AREAS WITH DEEP CHAFE MARKS. REPAIRED IAW DHC-8 SRM 51-40-11.SDR CALA9901427Skin · crackedINSPECTION FOUND A 1/4 CRACK IN #1 ENGINE PYLON SKIN UPPER SURFACE AT PANEL 5727 CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR USAA991091Skin · crackCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LOWER AFT CORNER OF PANEL NR 5727L CUTOUT LEFT PYLON SKIN. INSTALLED DOUBLER PER EA 65815 AND TR 54-30-07. (M)SDR ASOA99115Panel · corrodedDURING C-CHECK, FOUND THE PANELS 121 DB AND 131 BB ARE CORRODED. MAINTENANCE REMOVED AND REPLACED PANELS 121 DB AND 131 BB IAW EMB 120 MM 34-42-02. LEAK CHECK GOOD. OPERATIONAL CHECK GOOD. (M)SDR QXEA9902257Skin · chafedPDX - FINGERNAIL DECK HAS A CHAFE ON UPPER SURFACE AT CENTERLINE OF NACELLE AT STATION XN 240. REPAIRED IAW DHC-8-100 SRM 51-40-11.SDR CALA9901308Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON SKIN UPPER SURFACE. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR UF6A990934Panel · crackedSBN - THE RIGHT OUTBOARD IGNITER PANEL IS CRACKED. MAINTENANCE REPAIRED PANEL. ALL WORK WAS DONE IAW ENGINEERING ORDER 98-210. (M)SDR CALA9901304Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON SKIN UPPER SURFACE AT NAC STA 208. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR QXEA9901994Skin · chafedYXX - CHAFE ON LEFT-HAND AFT NACELLE UPPER DECK UNDER FINGERNAIL. REPAIRED IAW RD 8-54-866 AND DHC -8 SRM 51-20-36.SDR UPS99430619Panel · crackedINSPECTION TYPE:N/A, NR 4 PYLON PANEL CRACKED. REPAIRED PANEL IAW B747-5430-11517.SDR 99ZZZM686Skin · crackedNR 3 ENGINE PYLON APRON UPPER SURFACE HAS SEVERAL CRACKS. DAMAGED AREAS REMOVED IAW SRM 51-40-2. FABRICATED REPAIRS IAW SRM 51-40-2. INSTALLED REPAIRS IAW SRM 51-40-2. (M)SDR UPS99430614Panel · crackedINSPECTION TYPE:N/A, APPROX 11 INCH CRACK ON NR 3 PYLON I/B SIDE FWD OF LOWER ACCESS PANEL. PERFORM CONDUCTIVITY TEST AND VISUAL INSPECTION PER BOEING LETTER 99-00318H. *S/D* COMPLISHED CONDUCTIVITY TEST AND VISUAL INSPECTION PER BOEING REQUEST LETTER 99-00SDR UPS99830841Skin · crackedINSPECTION TYPE:C123 NR 4 PYLON INBD SKIN AT STA YN 278 IS CRACKED THROUGH A SCREW HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK718-147.SDR CALA9901111Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT O/B FORWARD CORNER OF NR 1 ENGINE PYLON ACCESS PANEL 5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5340-01230.SDR RRXA991493Panel · missingDURING A MAINTENANCE VISIT FOUND ROBBED PYLON PANEL ASSY FOR A/C N8085U NR 3 PYLON (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW FAA APPROVED TENNESSEE TECHNICAL SERVICESSDR MALA976545Skin · chafedLEFT ENGINE NACELLE INBOARD SIDE CHAFED AFTER REMOVAL OF THE SB DOUBLER. THIS DISCREPANCY WAS DISCOVERED DURING THE AIRCRAFT'S SCHEDULED HEAVY CHECK. MAINTENANCE REPAIRED IAW PER EO S54019.SDR CALA9900982Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON SKIN AT UPPER SURFACE OF FORWARD PYLON. A REPAIR WAS INSTALLED IAW ECRA 5431-01006.SDR USAA990722Skin · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT NR 1 ENGINE PYLON SKIN AT ACCESS PANEL NR 5727 CUTOUT LOWER AFT CORNER. INSTALLED DOUBLER PER TR 54-30-07. (M)
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