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 UPS07550703Skin · crackedINSPECTION TYPE:C NR 2 OUTBOARD NACELLE STRUT SKIN CRACKED ABOUT ONE INCH ALONG 443BR CUTOUT. COMPLIED WITH FINAL EA 757-5451-27-A1748 AND EO B757-5430-27710.SDR 07FDEA03675Skin · wornFOUND ON PYLON NR 1 AT RIB 8 INBOARD AND OUTBOARD SIDE THE HOLE FOR SUPPORT WORN DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.SDR 07FDEA03590Skin · crackedPYLON NR 1 EXT SKIN FOUND CRACK ON SKIN UPPER SIDE RT. 10-25-07 REPAIRED PYLON SKIN IAW SRM 51-00-01 VOL I FIG 100 & SRM 54-00-01 VOL I FIG 2B.SDR DU4R2007169Skin · damagedPERMANENT REPAIR TO NR 2 PYLON FWD SKIN REQUIRED. ACCOMPLISHED PERMANENT REPAIR IAW DELTA EA 06-074338-03 REV B DATED 01-30-2003 IAW DELTA ERA 362852-14 REV E DATED 9/5/07 APPROVED PER FAA FORM 8110-3 SIGNED BY DER NR SO-831 DATED 29 SEP 1997.
SDR 07FDEA03496Panel · wornFOUND WORN HOLES ON RIB 8 INBOARD AND OUTBOARD PANEL, PYLON NR 2 RHS. REPAIR PERFORMED IAW SRM 54-51-31/CONF 02/FIG 201.SDR 07FDEA03493Panel · wornFOUND WORN HOLES ON RIB 8 INBOARD AND OUTBOARD PANEL, PYLON NR 1 LHS. REPAIR PERFORMED IAW SRM 54-51-31/CONF 02/FIG 201.SDR DU4R2007171Skin · damagedNR 1 PYLON I/B SKIN HAS TEMPORARY REPAIR. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON O/B SKIN IAW DELTA EA 06-074338-03 REV B DATED 01/30/2003 IAW DELTA ERA 454288-14 REV ORIG AND B757 SRM 51-00-00D PG 1 APPROVED PER 14 CFR 121.379(B).SDR DU4R2007172Skin · damagedTEMPORARY REPAIR TO NR 1 PYLON O/B SKIN. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON O/B SKIN REPAIR IAW DELTA EA 06-074338-03 REV B DATED 01/30/2003 IAW DELTA ERA 454258-14 REV ORIG APPROVED PER 14 CFR 121.379(B).SDR DU4R2007170Skin · damagedFOUND TEMPORARY REPAIR NR 1 PYLON I/B SKIN. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON I/B SKIN IAW DELTA EA 06-074338-03 REV B DATED 01/30/2003 IAW DELTA ERA 093016-14 REV A AND B757 SRM 51-00-00D PG 1 APPROVED PER 14 CFR 121.379(B).
SDR DL76P071179Door · missingFOUND BY MTC ON DAILY RELIABILITY/WEEKLY CHECK NUMBER 2 ENGINE PYLON INBOARD STRUT DOOR MISSING. AOG PART 311T3065-127 INSTALLED NEW ACCESS PANEL PER MM.SDR 07FDEA03382Panel · crackedCRACKED HOLES (8 MM) FOUND ON PYLON NR 1, RIB 8 INBOARD SIDE. REPAIR PERFORMED IAW SRM 54-51-31/FIG 201.SDR 07FDEA03378Skin · crackedCRACKED HOLES (ABOUT 8 MM) ON PYLON NR 1, RIB 8 OUTBOARD SIDEWALL. REPAIR PERFORMED IAW SRM 54-51-31/FIG 201.SDR FDKA200709488Panel · damagedPANEL 412CL HAS AN ELONGATED HOLE THAT IS BEYOND LIMITS. INSTALLED A DIMPLED WASHER OVER THE DAMAGE.SDR 2007UALA03510Panel · damagedPANEL ON NR 2 PYLON IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER/FILLER REPAIR ON PANEL 424CR. INSTALLED PANEL ONTO NR 2 PYLON.SDR 07FDEA03232Skin · corrodedNR 2 STRUT, RIGHT SIDE SKIN AT APPROXIMATE PP STA 182 HAS CORROSION ON SKIN AND UNDER LOWER FRAME. CORROSION WAS REMOVED FROM SKIN, AND FOUND OUT OF LIMITS PER SRM 54-50-01. CONTACTED ENGINEERING AND WAS PRESENTED EA NR F-5450-110764A FOR CORRECTIVE ACTIONSDR EIA2007158Skin · chafedNUMBER ONE ENGINE PYLON RIGHT SIDE NACELLE STA 180 TO NACELLE STA 236YLON SKIRT CHAFED AND FASTENERS SHEARED. REMOVED EXISTING DAMAGE NR 1 PYLON, RT SKIRT REPAIR DOUBLER AND SHEARED FASTENERS, FABRICATED AND INSTALLED NEW REPAIR DOUBLER AND NEW FASTENERS ON NSDR 07FDEA03162Skin Panel · crackedCRACKED HOLE ON PYLON NR 2 AT RIB 8 UPPER SPAR. REPAIR PERFORMED IAW SRM 54-51-31/FIG 20. INSPECTION PROGRAM IAW EA 6-5451-103288.SDR USAA070677Skin · crackedPYLON ABOVE NR 2 ENGINE O/B SIDE OF LOAD FITTING PIN HAS CRACK. REMOVED REPAIR, CLEANED AREA, INSTALLED REPAIR WET WITH SEALANT PER TR 57-41-02, DEFECT SIZE: .5 INCH.SDR USAA070690Panel · crackedTOP OF RT ENGINE PYLON AT PANEL 5828R OPENING HAS CRACK. INSTALLED DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .75 INCH.SDR USAA070691Panel · crackedTOP OF PYLON 2 PANEL 5727L OPENING HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: .5.SDR 07FDEA02963Skin · corrodedNR 2 STRUT, RT SIDE, SIDE SKIN AT APPROXIMATELY NAC STA 144 INTERNAL, IS CORRODED ON SKIN AND UNDER LOWER FRAME/CHORD. REMOVED CORROSION FROM INTERNAL SKIN AS MARKED PER SRM 54-50-01. ORIGINAL SKIN THICKNESS (DOUBLER SIDE) .090", AFTER REWORK .075" AT LOWESDR 07FDEA02825Skin · corrodedNUMBER ONE STRUT/PYLON, LT SIDE SKIN, AT APPROXIMATE NAC STA 144, INTERNAL, IS CORRODED ON SKIN AND UNDER LOWER FRAME/CHORD. REMOVED CORROSION IAW SRM 54-50-01. ORIGINAL MATERIAL THICKNESS WAS .090", AFTER REWORK REMAINING MATERIAL THICKNESS WAS .079", OUT OSDR TAMF20070011SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 06-084-01-2) WAS FOUND WEAR ON STRUT SKIN STA 148.50. THE MINIMUM THICKNESS IS 0.047 INCH. CF6-80C2 ENGINE NR 2. DAMAGED AREA WAS REPAIRED IAW EWO 767 54-017 AND MFG SERVICE REQUEST 1-512263744. THIS REPAIR CONSTITUTESSDR KCSA071283Skin · chafedNR 4 PYLON AFT LOWER SPAR INBOARD SIDE SKIRT IS CHAFED AT NAC STA 180 TO 265.4.SDR USAA070604Skin · crackedPYLON NR 1 ENGINE UNER PANEL 5727 HAS CRACK. STOP DRILLED & INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: 1 INCH.SDR KCSA071281Skin · wornNR 2 PYLON OUTBOARD SIDE SKIN FILLER OF PREVIOUS REPAIR WORN AND SKIN WORN FORWARD OF EXISTING REPAIR AT NAC STA 180 TO 221.9, ABOVE MIDSPAR.SDR TAMF20070010SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 06-091-01-2) WAS FOUND CORE COWL P/N:224-2301-517, S/N: 0115 WITH ELONGATED HOLE AT FRAME STA NAC 294, ENGINE NR 2.DAMAGED AREA WAS REPAIRED IAW EWO 767 54-016 AND AUTHORIZATION CV07-1674-01.SDR 2007UALA02923Panel · gougedNR 1 PYLON AFT BULKHEAD UPPER CLOSE OUT PANEL HAS DEEP GOUGE. BLENDED GOUGE AND FABRICATED PANEL PER BOEING DWG 311N3150 AND INSTALLED REPAIR PER UA ENGINEERING SPECIFICATIONS.SDR KCSA071260Skin · wornNR 3 PYLON I/B SIDE LOWER SKIRT SKIN WORN AT NAC STA-200 TO 236.SDR KCSA071259Skin · wornNR 3 PYLON O/B SIDE LOWER SKIRT WORN IN SEVERAL AREAS AT NAC STA-180 TO 236.SDR KCSA071258Skin · chafedNR 4 PYLON STA 180-265 AFT LOWER SPAR O/B SKIRT CHAFED AT KNIFE EDGE.SDR NWAA072715503Skin · crackedDURING "M" CHECK, FOUND CRACK IN NR 2 PYLON SKIN PANEL AT NAC STATION 128. REPAIRED PER EA 55-194182.SDR USAA070563Skin · crackedAT ACCESS PANEL OPENING 5727 LEFT ENGINE PYLON HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: .5 INCH.SDR EIA2007140Skin Panel · gougedNR 3 PYLON OUT BOARD ACCESS DOOR NR 473AR THE DOOR RING HAS DEEP GOUGE AT INNER SIDE. REPAIRED NR 3 PYLON OUTBOARD ACCESS DOOR NR 473AR PER ECRA 488-54-019-2.SDR 2007UALA02614Panel · damagedNR 1 ENGINE FWD PYLON CANTILEVER PANEL IS DAMAGED. REPAIRED FAIRING.SDR UIEA200700267Skin · crackedNR 3 ENGINE LT CORE COWL NR 437, AFT LOWER CORNER LONGERON STRUCTURE AND OUTER COWL SKIN HAS A CRACK AND LOOSE RIVETS. PERMANENT REPAIR ACCOMPLISHED AS PER 747 SRM 54-31-03 FIG 3 AND ATLAS EO4771A026 AND FAA 8110-3 FORM (REF: FIG. 1 AND 2) AND ATLAS AIR XEO NSDR 07FDEA02617Panel · crackedPYLON NR 2, RIB 8 LT WITH CRACK AT UPPER AREA. IT WAS REPAIRED IN ACCORDANCE WITH SRM 54-51-31 FIG 201.SDR QXEA200701130Skin · crackedC4 PDX - NR 1 NACELLE HAS A CRACK IN THE NACELLE SKIN AT THE FORWARD OUTBOARD CUTOUT RADIUS FOR THE FORWARD GEAR DOOR. REPAIRED IAW RD8/4-54-873.SDR NWAA072425519Skin · crackedDURING SCHEDULED NR 2 ENGINE CHANGE FOUND CRACK IN PYLON SIDE SKIN AT NAC STA 128. REPAIRED PER EA 55-210070 SECTION I, SECTION II TO BE ACCOMPLISHED WITHIN 24 MONTHS OF SECTION I.SDR HALA0700281Skin · bentPER INBD CREW, F/A REPORTS METAL STICKING UP ON NR 2 ENGINE. FOUND OUTBD FAN COWL TOP FWD CORNER DAMAGE APPROX 1-1/2" BY 1/2" AND FWD OUTBD. ON PYLON EXTENSION LIFTED APPROX 4" (APPROX 1/2" LIFTED UP). ACCOMPLISHED HAL-M105 FILE #597063 AND 597064. CONDITISDR 07FDEA02350Panel · damagedOLD REPAIR ON PYLON NR 2 INBOARD SIDE, RIB 8 NOT CONFORM TO SRM DOUBLER REPAIR RENEWED IAW SRM 54-51-31 FIG 201. APPROVED BY EA 6-5451-1067447 REV A.SDR 07FDEA02349Panel · crackedCRACKED HOLE (ABOUT 8MM ) AT RIB 8A PYLON NR 1, INBOARD SIDE. REPAIR PERFORMED BY DOUBLER INSTALLATION IAW SRM 54-51-31 PB 200, APPROVED BY EA 6-5451-106447 A.SDR UPS07M50718Cover · crackedINSPECTION TYPE:C TAIL PYLON COVER BEHIND THE EXHAUST NOZZLE CRACKED (6 INCHES), STOPPED DRILLED, NUMEROUS RIVETS PULLED THRU IN LT AND RT SIDE, NEEDS REPLACEMENT. FPI C/O PER DAC NDTSPM R13 PT8 & MARKED OUT CRACK END. CRACK END STOP DRILLED PER EN 1438-07. SDR USAA070501Skin · crackedFOUND CRACK AT 2 PYLON AT PANEL NR 5827R. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TR 54-30-07, DEFECT SIZE: .200".SDR USAA070500Skin · crackedFOUND CRACK AT 2 PYLON PANEL NR 5828R BENEATH LONGERON. STOP DRILLED END OF CRACK AND INSTALLED REPAIR DOUBLER PER TR 54-30-07, DEFECT SIZE: .250".SDR FDKA200706315Panel · chafedLT COWLING PANEL 414, HAS CHAFE DAMAGE TO THE FRAMES FROM CONTACT WITH THE FORWARD AND AFT STAY RODS. REPAIRED DAMAGE.SDR UPS07650196Skin · gougedINSPECTION TYPE:2C LEFT ENGINE PYLON SKIN GOUGED. BLENDED BOTH GOUGES. BOTH BLENDS OUT OF LIMIT. HFEC INSPECTION BLENDED AREAS, NO CRACKS FOUND. DRILLED DOUBLER PER SRM 54-52-01-2. ALODINED & PRIMED DOUBLER & BLENDED AREAS. INSTALLED DOUBLER. INSTALLED SDR 2007UALA02209Access Panel · crackedNR 2 PYLON FWD OF ACCESS PNL NR 442BR WEB FWD OF FUEL FEED LINE IS CRACKED. INSTALLED DOUBLER REPAIR.SDR AMWA31034CSkin · damagedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE, DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW AIRCRAFT ENGINEERING INC REPORT NR 6732SDR HALA0700251Skin · crackedON NR 1 ENGINE CHANGE, LT PYLON APRON LOWER AFT LATCH CUTOUT HAS 2 CRACKS. REPAIRED NR 1 ENGINE LOWER AFT LATCH CRACKS PER HAL M105 B10192.
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