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 07FDEA00737Panel · crackedNR 1 PYLON, RT SIDE PANEL AT RIB 8 FOUND CRACKED REPAIRED IAW SRM 54-51-31 FIG 201 SHT 1 AND 2.SDR 07FDEA00711Skin · crackedNR 2 PYLON PRECOOLER HOUSING RT SIDE SKIN SURFACE FOUND CRACKED AT RIB 5A UPPER AREA INSTALLED NEW WALL P/N A5461139320300 PER SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".SDR COEA0706908Panel · damagedFRETTING DAMAGE FOUND ON RT NACELLE REBATE FLANGE COMMON TO PANEL 486AL AND 486AR. REPLACED FABRICATED REBATE PANELS IAW ATR SRM. (M)SDR COEA0717908Panel · damagedFRETTING DAMAGE ON LT NACELLE REBATE FLANGE COMMON TO PANEL 475AL. REBATE PANEL REMOVED. FABRICATED AND INSTALLED NEW REBATE PANEL IAW ATR42 SRM. (M)SDR 2007UALA00698Skin · crackedNR 2 PYLON INBOARD SIDE SKIN CRACKED AT FWD HOLE. MAJOR REPAIR ACCOMPLISHED: REPAIRED SIDE SKIN WITH 3 EACH REPAIR DOUBLERS.SDR UIEA200700111Skin · crackedNR 4 PYLON PRECOOLER EXHAUST CUT-OUT SKIN ASSEMBLY AND DOUBLERS CRACKED. PYLON REPAIRED AS PER BOEING MESSAGE 1-289015678-8.SDR UIEA200700110Skin · crackedNR 1 PYLON PRECOOLER EXHAUST CUT-OUT SKIN ASSEMBLY AND DOUBLER FOUND CRACKED. SKIN ASSEMBLY TRIMMED OFF FILLER FABRICATED AND INSTALLED AS PER BOEING MESSAGE 1-289015678-4 AND REMOVED FASTENERS INSTALLED AS PER BOEING MESSAGE 1-289015678-8 AND FAA FORM 8100-9SDR 2007UALA00687Skin · crackedNR 2 PYLON OUTBOARD SKIN IS CRACKED AT FWD HOLE. [SUP 4-24-07] MAJOR REPAIR ACCOMPLISHED. HFEC INSP AT END OF CRACK. INSTALLLED 301 HALF 0.050" DOUBLERS AS A UA APPROVED REPAIR.SDR UIEA200700122Skin · crackedNR 4 PYLON CUT-OUT FOR PRE-COOLER EXHAUST AIR, RT SIDE OF PYLON AT NACELLE STATION 248.0 HAS A 2.625 INCH CRACK AT AFT, LOWER CORNER. ACCOMPLISHED INTERIM REPAIR, LOCATED CRACK AS PER NDT 747 MANUAL 51-00-00 PAR 6 AND STOP DRILLED BY REAMING EXISTING HI-LOCK SDR UIEA200700118Skin · crackedNR 3 PYLON TOP SKIN, AFT EDGE, ABOVE LINK FITTING HAS A 0.375 INCH CRACK. TRIMMED OUT SKIN TO REMOVE CRACK AS PER 747 SRM 51-10-01. ACCOMPLISHED HFEC INSPECTION TO VERIFY REMOVAL OF CRACK AS PER 747 NDT MANUAL PAR 6 SECTION 51-00-00 FIG 4. ALSO, REFERENCE ASDR UIEA200700100Skin · crackedNR 3 ENGINE LT CORE COWL SKIN BOND DOUBLER CRACKED AT AIR EXHAUST DUCT AFT LOWER PORTION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286833874-1 THRU -6, DWG 65B94280 AND FAA FORM 8100-9.SDR DL76L070177Panel · missingON WAC FOUND RIGHT ENG INBD PYLON TRAPEZOID PANEL MISSING. FWD TO MCO AS PER CDL 54-53-02 CHECKED TIGHTENING BOLTS ON ALL OTHER PYLON ACCESS PANEL ON BOTH ENGINE. INSTALLED RT ENG PYLON OTBD TRAPEZOID PANEL MCO AND PLAC REMOVED.SDR HALA0700070Access Door · missingNR 1 ENG PYLON NACELLE STRUT ACCESS DOOR MISSING (I/B). INSTALLED ACCESS DOOR IN NR 1 ENG PYLON NACELLE STRUT SEC, CK OK.SDR USAA070134Skin · crackedAT PANEL (5827) OPENING FLANGE ON TOP OF RT PYLON INBOARD SIDE, STA 212.84 HAS CRACK. STOP DRILL CRACK, FAB'D SKIN DOUBLER & INSTALLED PER TYP REPAIR 54-30-07, DEFECT SIZE: .025 INCH.SDR USAA070122Skin · crackedRT PYLON TOP OUTBOARD SIDE, PANEL 5828 OPENING, PYLON STA 220.84 FLANGE CRACKED. STOP DRILL CRACK, FAB'D DOUBLER & INSTALLED PER TYP REP 54-30-07, DEFECT SIZE: .75 INCH.SDR 2007UALA00562Skin · crackedNR 2 NACELLE STRUT SIDE SKIN OUTBOARD FORWARD ACCESS DOOR CUT-OUT HAS A CRACK INDICATION, INSIDE OF CUT-OUT, CRACK ENDS MARKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED 3 EACH DOUBLERS.SDR F3LA200700027Pin · corrodedDURING C-2 CHECK, INSPECTION REPORTED RT PYLON PANEL 483BL ONE ALIGNMENT PIN CORRODED. REPLACED PIN IAW AMM 51-42-11.SDR AWXA200700347Skin · crackedMCN - NR 2 PYLON STRUT SKIN CRACKED, EXTENDS BEYOND STOP DRILL HOLE, AT PANEL NR 5828R, NAC STATION 196.70 -NAC STATION 254.525. REPAIRED NR 2 PYLON STRUT SKIN, NAC STATION 196.70 -NAC STATION 254.525 PER AWA ER 03-5400-07065-SS3.SDR WRNA200700033Skin · damagedDURING C-CHECK, THE O/B SKIN OF NR 3 PYLON WAS FOUND DAMAGED AT APPROX STA 221.9 JUST BELOW MID SPAN. REMOVED DAMAGE IAW SRM 54034-03, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 54-34-03 FIG 25, SRM 51-10-02 AND SOPM 20-42-02.SDR WRNA200700017Skin · damagedDURING C-CHECK, NR 3 PYLON INBOARD SKIN DOUBLER WAS FOUND WORN UNDER FORESHIELD NEAR NAC STA 221. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 01-07019.SDR USAA070094Skin · crackedLT ENG PYLON PANEL OPENING 5727L AT O/B AFT CORNER OF OPENING. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .5".SDR 07FDEA00460Panel · crackedFOUND CRACK AT PYLON NR 2 RT ON AREA AT LOWER SIDE PANEL AT RIB 18 INBOARD. REPAIR WAS PERFORMED IAW RAS 048245/005/2006 ISSUE: A AND EA 6-5451-103394.SDR WRLA2007033Skin Panel · crackedFOUND NR 1 PYLON PRECOOLER TORQUE BOX SKIN PANEL GOUGE. PERFORM NR 1 PYLON PRECOOLER TORQUE BOX SIDE SKIN PANEL GOUGE AREA DOUBLER INSTALL REPAIR PER MD-11 SRM VOL 1, 54-00-01 FIG 3 REV:38.SDR NWAA070595523Skin · crackedDURING SCHEDULED ENGINE CHANGE INSPECTION REVEALED CRACK IN NR 2 PYLON RIGHT SIDE SKIN. REPAIRED PER EA 55-208923 SECTION I, SECTION II REPAIR TO BE ACCOMPLISHED WITHIN 24 MONTHS.SDR USAA070085Skin · crackedLEFT ENGINE PYLON PANEL OPENING 572L AT O/B AFT CORNER OF OPENING CRACKED. STOP DRILLED CRACK & INSTALLED REPAIR DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .5 INCH.SDR DHL2007802529Skin · crackedRT NR 3 ENGINE NACELLE INLET COWL SHOWS CRACK 0.500" ON SKIN STA YN 138.000 AT 3 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-54-105 REV IR DATED 01-19-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D.SDR UIEA200700047Skin · crackedNR 2 PYLON PRECOOLER EXHAUST CUT-OUT CRACKED AT LOWER AFT CORNER AT NAC 248. THE SKIN ASSEMBLY CRACKS WERE REMOVED BY TRIMMING. THE NR 3 STIFFENER WAS REINFORCED WITH A SUPPLEMENTARY STEEL LOWER ANGLE FROM NAC STATION 235 TO 254. THE RIB INSTALLATION AT NACSDR UIEA200700048Skin · crackedNR 3 PYLON PRECOOLER EXHAUST CUT-OUT CRACKED AT LOWER AFT SIDE. THE SKIN ASSEMBLY CRACKS WERE REMOVED BY TRIMMING. THE NR 3 STIFFENER WAS REINFORCED WITH A SUPPLEMENTARY STEEL LOWER ANGLE FROM NAC STATION 235 TO 254. THE RIB INSTALLATION AT NAC STATION 248 SDR UIEA200700046Skin · crackedNR 1 PYLON PRECOOLER EXHAUST CUT-OUT CRACKED AT AFT CORNER STATION 248. THE SKIN ASSEMBLY AND WINDOW STRAPS WERE TRIMMED TO REMOVE CRACKS. NET FIT ALUMINUM FILLERS WERE INSTALLED AT ALL TRIMMED AREAS. REPAIR WAS NDT INSPECTED. THE NR 3 STIFFENER WAS REINFOSDR UIEA200700049Skin · crackedNR 4 PYLON PRECOOLER EXHAUST CUT-OUT CRACKED AT LOWER AFT SIDE. THE SKIN ASSEMBLY AND WINDOW STRAP WERE TRIMMED TO REMOVE CRACKS. NET FIT ALUMINUM FILLERS WERE INSTALLED AT ALL THE SUBJECT TRIMMED AREAS TO FACILITATE ALL REPAIR PARTS AND FASTENER INSTALLATIOSDR NWAA070966305Skin · crackedDURING "M" CHECK, FOUND CRACK IN NR 4 PYLON LT INBOARD SKIN NAC STA 276, NWL 170, PANEL 482EL CUTOUT. REPAIRED PER EA 63-208898.SDR UIEA200700034Skin · chafedNR 3 PYLON RT ACCESS PANEL 473AR CUTOUT AT NAC STA 286 TO STA 300 FOUND CHAFING. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272049267 AND FAA FORM 8110-9.SDR AWXA200700277Skin · crackedMCN - FOUND LEFT PYLON ACCESS PANEL NR 5727L, CUT OUT LAND CRACKED, NAC STATION 254. REPAIRED LEFT PYLON ACCESS PANEL NR 5727L, CUT OUT LAND, NAC STATION 254 IAW AWA ER 03-5433-00340-DL1 AND SB 737-54-1035.SDR UIEA200700020Skin · debondedNR 1 ENGINE RT T/REV TRANSLATING COWL UPPER EDGE SKIN FOUND DEBOND. REPAIR ACCOMPLISHED AS PER EO NR 4778A088 AND FAA FORM 8110-3.SDR UIEA20070063Skin · wornNR 3 PYLON ACCESS PANEL CUT-OUT SKIN FOUND WORN AT PANEL 472AR. REPAIR: THE EFFECTED INNER DOUBLER WAS TRIMMED. THE TRIMMED EDGE WAS NDT INSPECTED. REPAIR SKIN WAS INSTALLED WITH HILOCK FASTENERS TO RESTORE THE TRIMMED OUT AREA. A MODIFIED STEEL WEAR PLATE SDR 2007UALA00173Fairing · crackedCRACK IS FOUND ON RIGHT NACELLE AFT FAIRING, LWR LEFT CHORD, SAF STA 16.152. REMOVED AND REPLACED DAMAGED CHORD. AIRCRAFT RETURNED TO SERVICE.SUSPECT COMBINATION OF VIBRATION & FATIGUE.SDR USAA070064Skin · crackedPYLON SKIN, LT PYLON PANEL CUTOUT NR 5728L HAS CRACK. INSTALLED DOUBLER & REPAIR PARTS PER T/R 54-30-07, DEFECT SIZE: .25 INCH.SDR USAA200701005Skin · crackedA .5 INCH CRACK FOUND ON PYLON SKIN AT RIGHT ENGINE PYLON OPENING FOR PANEL 5827R.SDR 2007UALA00169Skin · crackedRIGHT NACELLE STRUT O/B SKIN CRACKED AT STA 110 FWD UPPER QUADRANT. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER ENGINEERING AUTHORIZATION AND MAINTENANCE SPECIFICATION.SDR 07FDEA00141Panel · dentedA DENT EXIST AT NR 1 ENG PYLON UPPER FWD FIXED L/E PNL MEASURING 6 INCH BY 4 INCH BY 0.350 INCH REMOVED AND REINSTALLED FIXED PANEL IAW A310 SRM 51-40-21. REWORKED DENT IAW A310 SRM 54-50-00 FIG 201 AND EA 6-5480-106313 PT1.SDR 0700416740Skin · crackedDURING "M" CHECK, FOUND CRACK IN NR 3 PYLON CAP SKIN AT FRONT SPAR CHORD AND REAR ENGINE MOUNT BULKHEAD UPPER FORWARD FRAME. REPAIRED PER EA 67-208615.SDR UIEA200700018Panel · missingON WALK AROUND, FOUND PANEL MISSING ON NR 1 PYLON RIGHT HAND SIDE, PANEL 452 CR. INSTALLED NEW PANEL IAW MM 54-62-00.SDR NWAA70065513Skin · crackedDURING "M" CHECK, FOUND CRACK IN NR 2 PYLON OUTBOARD SKIN AT NAC STA 144. REPAIRED PER EA 55-208680.SDR 2006UALA02401Skin · damagedNR 1 ENG PYLON IS TWISTED AND LIFTED AT FWD INBOARD END AND INBOARD SKIN ATTACH PLATE AND FRNG ARE BUCKLING. NR 1 PYLON FORWARD SECONDARY STRUCTURE "CANTILEVER" SECTION REPLACED BY AIRBUS IN ACCORDANCE WITH REPORT NUMBER M-300989-EMBOD.SDR QXEA200603210Skin · tornC4 PDX - NR 1 ENGINE, SMALL SECTION OF SHEETMETAL TORN AWAY JUST FORWARD OF AFT RIGHT ATTACH PIN HOLE FOR THE LOWER COWL. REPAIRED IAW RD8-54-063 AND SRM 51-20-16.SDR TRAX200601130Panel · missingON POST FLIGHT INSPECTION FOUND THE RIGHT HAND UPPER FIXED COWL MISSING.SDR QXEA200603184Skin · crackedC4 PDX - LEFT NACELLE SKIN IS CRACKED AT FORWARD INBOARD CORNER OF GEAR WELL OPENING. REPAIRED IAW RD8-54-873.SDR DJFA2006361Skin · crackedDURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE DISCOVERED CRACKS ON THE TOP SKIN OF THE PYLON. THE CRACKS WERE LOCATED NEAR THE INBOARD TRAILING EDGE; THE FORWARD CRACK WAS .9" LONG 17.25" FROM THE TRAILING EDGE. THE SECOND CRACK WAS .2" LONG 16.125" FROM TSDR QXEA200603095Skin · dentedC3 YYC - RIGHT ENGINE LOWER FAN COWL OUTBOARD SIDE HAS 2 DENTS. REPAIRED IAW SRM 54-44-00.SDR IXXA06SMN400SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 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.
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