JASC 5414
Service difficulty reports · 4,360
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 C77A20140214004Panel · damagedLEFT PYLON PANEL 419UR HAS AN OVERSIZED FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WORK ORDER 746718-463 IAW ETD 2014-170-011172 & EA E170-54-020 REV IR WORK ORDER 1405981.SDR DALA14011240189Access Panel · crackedNR 2 PYLON ACCESS DOOR 426BR CUTOUT FOUND CRACK AND REPAIRED IAW SRM 54-53-01.SDR DALA14011230189Skin · damagedNR 2 PYLON INBD SIDE INNER SKIN AND DOUBLER CUTOUT BETWEEN NAC STA 180, ACCESS PANEL 442AL. REPAIRED IAW ER/A 521579-14, REV.SDR DALA14011190189Skin · crackedNR 2 PYLON INBD SIDE STRUT SKIN, AFT TRAPEZOIDAL ACCESS DOOR CUTOUT CRACKED. COMPLIED WITH ERA 090076-14.SDR FDEA201402060276Skin · corrodedNUMBER 2 PYLON INBD FWD SKIN IS CORRODED AT DOOR AT PPS 106.SDR FDEA201402030250Skin · corrodedNUMBER 2 PYLON INBD SKIN IS CORRODED AT LOWER SPAR FWD OF MID BULKHEAD FITTING. MINOR REPAIR.SDR SWIA201436449Repair · looseLEFT NACELLE OTBD AFT SKIN AT FRAME NR 10 REPAIR LOOSE. C CHECK PERFORMED PERMANENT REPAIR TO LT NACELLE OTBD AFT SKIN AT FRAME NR 10 IAW ETD.SDR C77A201401240012Panel · wornOVERSIZE FASTENER HOLE ON PYLON PANEL 429ML. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 738174-430 IAW ETD 2014-170-005780 & EA E175-54-163 REV IR WORK ORDER 1352237.SDR C77A201401240011Panel · wornOVERSIZE FASTENER HOLE ON PYLON PANEL 419KL. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 738174-424 IAW ETD 2014-170-005780 & EA E175-54-163 REV IR WORK ORDER 1352237.SDR C77A201401240010Panel · wornPYLON PANEL 429UR HAS THREE ELONGATED FASTENER HOLES. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 738174-408 IAW ETD 2014-170-005434 & EA E175-54-162 REV IR WORK ORDER 921972.SDR C77A20140124009Panel · wornPYLON PANEL 429TL HAS ELONGATED FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 738174-407 IAW ETD 2014-170-005434 & EA E175-54-162 REV IR WORK ORDER 921972.SDR C77A20140124008Panel · wornPYLON PANEL 419ML HAS ELONGATED FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 738174-406 IAW ETD 2014-170-005434 & EA E175-54-162 REV IR WORK ORDER 921972.SDR C77A20140121016Panel · wornPYLON PANEL 419YL HAS ELONGATED FASTENER HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 737209-412 IAW ETD 2014-170-004813 & EA E175-54-161 REV 1 WORK ORDER 915246.SDR C77A20140121019Panel · wornFASTENER HOLE ON LT ENG PYLON PANEL 419ML IS WORN OVERSIZE. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 737209-475 IAW ETD 2014-170-004813 & EA E175-54-161 REV 1 WORK ORDER 91524SDR C77A20140121018Panel · wornFASTENER HOLE ON RT ENG PANEL 429LR IS WORN OVERSIZE. REAMED FASTENER HOLE BACK TO ROUND & INSTALLED NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02 ON WORK ORDER 737209-474 IAW ETD 2014-170-004813 & EA E175-54-161 REV 1 WORK ORDER 915246.SDR C77A20140121015Panel · wornFASTENER HOLE ON RH ENGINE PANEL 429LR IS WORN OVERSIZE. REAMED FASTENER HOLE BACK TO ROUND AND INSTALL NAS 1169C REPAIR WASHER IAW STANDARD PROCEDURES IN SRM 51-40-02.SDR SWAA2014012024328Panel · crackedNR 2 ENG STRUT PANEL 5864R CRACKED AT FASTENER HOLE. R & R PANEL IAW SRM.SDR CALA2013123094020Skin · chafedNR 2 PYLON LT SIDE ACCESS PANEL 443CL CUTOUT SKIN AT NAC STATION 325 FOUND 4 LOCATION WITH CHAFING MARK. NR 2 PYLON LT SIDE ACCESS PANEL 443CL CUTOUT SKIN AT NAC STATION 325 AREA TRIPLER INTERIM REPAIRED IAW ECRA 5450- 02128 REV PART 1. HFEC INSPECTED NO CRSDR USAA2013123000018Skin Panel · crackedRIGHT WING PYLON SKIN CRACKED AT ACCESS PANEL 5827. REPAIRED IAW TYPICAL REPAIR 737-5430-10-0054.SDR SWAA2014010923921Access Panel · crackedRT PYLON ACCESS PANEL CRACKED AT BS 235. REPAIRED PANEL IAW SRM.SDR ASOA2014013109822Doubler · chafedRIGHT ENGINE LOWER CORE COWL, INNER SKIN DOUBLE REPAIR HAS CHAFE DAMAGE. REMOVED DOUBLER ON RT LOWER COWL DOOR IAW SRM 51-42-06-001-001. COMPLIED WITH REPAIR OF THE FWD CORE COWL IAW REO 670-54-23-959. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOPSDR SWAA2014012024255Access Panel · crackedLT NACELLE STRUT ACCESS PANEL 5764 CRACKED. REPAIRED PANEL IAW EO & EA.SDR CALA2013122393879Skin · crackedNR 2 ENG PYLON FWD TORQUE BOX UPPER SPAR SKIN CRACKED AT THE HYD LINE EXIT, ACCESS PANEL 442BL. FOUND WEB CRACKED AT CASE DRAIN CUTOUT JUST AFT OF NAC STATION 172.14. REMOVED EXISTING REPAIR DOUBLER ON THE INBD SIDE & FABRICATED A NEW REPAIR DOUBLER & FILLERSDR C77A20131223003Panel · worn419ML, PN 170-23401-423, HAS ONE EACH OVERSIZED SCREW HOLE. REAMED FASTENER HOLE BACK TO ROUND & INSTALL NAS 1169C REPAIR WASHER IAW SRM 51-40-02 ON WO 739450-480 IAW ETD 2013-170-069392 & EA E175-54-158 REV 1 WO 896887.SDR C77A20131223002Panel · crackedLT PYLON PANEL 419ML, PN 170-23401-423, HAS A 2 INCH CRACK LOCATED AT A FASTENER HOLE. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM II 51-41-00 ON WO 739450-479 IAW ETD 2013-170-069392 & EA E175-54-158 REV IR WO 896887.SDR C77A201312230001Skin · crackedLEFT PYLON PANEL 419ML HAS A TWO INCH CRACK. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM II 51-41-00.SDR SWIA201335783Skin · crackedRT NACELLE LOWER AFT OTBD CORNER SKIN IS CRACKED. C-CHECK STOP DRILLED CRACK & INSTALLED REPAIR DOUBLER IAW SRM.SDR FDEA201312092945Skin · corrodedENG NR 2 STRUT OTBD SIDEWALL, INTERNAL, SKIN HAS CORROSION LOC PPS 120.0 TO PPS 170.0.SDR HNAA2013120600604Skin · damagedINBD SIDE OF NR 2 NACELLE HAS SEVERAL RIVET HEADS WORN AT LOWER FWD CORNER OF SKIN. REMOVED RIVETS AND INSTALLED PATH ON INBD FORWARD SIDE SKIN OF NR 2 NACELLE IAW RD8-54-1045. COMPLIED WITH HFEC INSPECTION.SDR AALA20131204011Skin · crackedDURING ACCOMPLISHMENT OF THE AFT HINGE FITTING PREVENTATIVE MODIFICATION, ECO F1566, ON THE NR 1 PYLON ONE FASTENER HOLE THROUGH THE FITTING & STRUCTURE WAS OVERSIZED & HFEC INSPECTED. REMOVED CRACK BY ENLARGING HOLE, VERIFIED CRACK REMOVAL BY HFEC INSPECTIONSDR CA131125006Panel · detached(CAN) ACFT HAD PART OF ITS PYLON COMPOSITE PANEL DEPART THE ACFT IN FLIGHT. APPROXIMATELY 6" X 6" AREA.SDR AALA20131121003Skin · damagedLT HAND PYLON WAS FOUND TO AN OVERSIZED HOLE IN THE INBD SKIN, COMMON TO THE SIDE LOAD FITTING, NEAR A GSE FITTING. ACCOMPLISHED REPAIR IAW EA B767 54-032581 & ECO C3369. HFEC OPEN HOLE INSPECTED WITH NO CRACK INDICATION NOTED.SDR CALA2013112093139Skin · delaminatedLT ENGINE NACELLE DELAMINATING. AT 10:00 POSITION A 2.5 BY 11 INCH AREA OF SKIN HAS BECOME DISBONDED AT LE. TAPPED ENTIRE AREA & FOUND TO BE SOLID, INTERIM REPAIRED IAW ECRA 7111-01475.SDR FDEA201311162798Skin · damagedHIDDEN DAMAGE ON REMOVAL OF THE NR 2 OTBD CORE COWL RUBSTRIP, FOUND DAMAGE TO THE SKIN UNDERNEATH THE RUBSTRIP.SDR SWAA2013112722800Access Panel · crackedRT WING PYLON STRUT ACCESS PANEL 5851R CRACKED. REPAIRED PANEL IAW SRM.SDR DALA13061745640Doubler · crackedNR 2 PYLON HYDRAULIC DISCONNECT PANEL DOUBLER CRACKED AT LOWER END BELOW LOWER AFT HYDRAULIC FEED THRU HOLE. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02 PG 6 & 7SDR DALA13061511505Skin · crackedNR 1 PYLON O/B SKIN FOUND CRACKED AT PANEL 432AL CUTOUT. REPAIRED AS PER ERA 518683-14.SDR A6WA201310284327Skin · gougedLEFT LOWER CORE COWL HAS GOUGE FROM BLOCKER DOOR ON OUTER SKIN JUST AFT OF FWD LATCHES. COMPLIED WITH EA 15-2013-463 BY BLEND OUT DAMAGE AND INSTALL DOUBLER.SDR UIEA2013102500537Skin · delaminatedLEFT ENGINE INLET COWL DELAMINATION AT 06:00 POSITION, AT AFT EDGE. (PERFORMED TIME LIMITED REPAIR ON LT ENGINE INLET COWL IAW EO 6771A004.)SDR A6WA201310244328Skin · damagedRT LOWER CORE COWL ALIGNMENT HOLES ELONGATED. FABRICATED AND INSTALL 2 EA DOUBLER FOR RT LOWER CORE COWL ALIGNMENT HOLES.SDR CALA2013102192216Panel · erodedNR 4 PYLON, UPPER FAIRING LE IS ERODED ON INBD SIDE JUST AFT OF THE NOSE COWL. INTERIM REPAIR HAS BEEN ACCOMPLISHED. REMOVE PANELS, R & R TO SHOP. PANEL REPAIRED IN SHOP IAW R & R R92972. REINSTALLED PANEL.SDR SWAA2013111822472Access Panel · crackedNR 1 ENGINE FAIRING STRUT FAIRING ACCESS PANEL 5764L CRACKED. REPAIRED PANEL IAW EO & EA.SDR REXA2013101702144Skin · gougedLEFT PYLON SKIN PANEL 433BB GOUGED. FABRICATED & INSTALLED NEW SKIN PANEL IAW SRM 51-40-11, 51-24-21 & SRM 51-42-06.SDR REXA2013101702143Skin · gougedLEFT PYLON SKIN PANEL 433BT GOUGED. FABRICATED & INSTALLED NEW SKIN PANEL IAW SRM 51-40-11, SRM 51-24-21 & SRM 51-42-06.SDR REXA2013101702121Access Panel · crackedNR 2 PYLON ACCESS PANEL 443BB IS GOUGED ON AFT END. FABRICATED & INSTALLED NEW SKIN ON PANEL 443BB IAW SRM 51-42-11, SRM 51-24-21 & SRM 51-42-06.SDR REXA2013101702120Access Panel · crackedNR 2 PYLON ACCESS PANEL 443BT IS CRACKED. FABRICATED & INSTALLED NEW SKIN ON PANEL 443BT IAW SRM 51-40-11, SRM 51-24-21 & SRM 51-42-06.SDR REXA2013101702116Skin · chafedLEFT ENGINE AFT CORE COWL OUTER SKIN AT PYLON SEAL IS CHAFED. REPAIRED LEFT ENGINE AFT CORE COWL OUTER SKIN TO WITHIN LIMITS CONDITION IAW SRM 54-13-00.SDR KCSA201310170099Skin · chafedNR 2 PYLON APPROX. NAC STA 263 EXTERIOR SKIN CHAFED ON INSIDE OF SKIN.SDR KCSA201310170098Skin · crackedNR 3 PYLON INBD SIDE NAC STA 192 FWD LOWER ACCESS PANEL OPENING HAS CRACK ON EXTERNAL SKIN AT FWD LOWER CORNER.SDR REXA2013101102053Access Panel · damagedNR 2 ENGINE ACCESS PANEL 443BT CRACKED AND GOUGED. FABRICATED NEW ACCESS PANEL IAW SRM 51-24-21 AND SRM 51-40-11.
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