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 ZW0A0209403Skin · crackedDURING CHECK-C MAINT ON NUMBER 2 PYLON 1.5 INCH CRACKS GOING AFT WERE FOUND INBD AND OTBD FORWARD ACCESS HOLE AT NACELLE STA 120 BETWEEN STA 116.05 AND 128. ACCOMPLISHED EMLR 73249.SDR ZW0A0209302Skin · crackedDURING CHECK-C MAINT THE NR 2 ENGINE PYLON, FWD ACCESS HOLE TO INTERIOR OF THE PYLON, APPROXIMATE NACELLE STA 162, THE OTBD SIDE HAD A CRACK 1.625 INCHES LONG. THE CRACK WAS LOCATED TOP FWD SECTION, AND VISIBLE ON OTBD TO INBD OF THE SKIN. ACCOMPLISHED BOEINSDR AWXA200200925Doubler · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 1/8" CRACK WAS FOUND ON FLANGE OF #1 NACELLE ACCESS PANEL 5727L. MAINTENANCE STOP DRILLED HOLES AND PERFORMED A HFEC INSPECTION TO VERIFY CRACKS WERE CONTAINED; REMOVED NECESSARY FASTENERS; FABRICATED A REPAIR DOUBLERSDR UIEA200200040Skin · crackedDURING CURRENT C-CHECK AT SIAEC, FOUND NR 2 PYLON TOP CAP SKIN CRACKED AT NAC STATION 264 INBOARD SIDE. CUTOUT CRACKED SKIN AND DOUBLER. SURFACE CORROSION LEVEL 1 REVEALED TO SANDWICHED STIFFENER. REMOVED AFT SECTION OF STIFFENER FOR CORROSION BLEND REPAIRSSDR AWXA200200961Skin Panel · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1/4" CRACK WAS FOUND ON THE # 1 ENGINE PYLON TOP FAIRING FORWARD OUTBOARD PANEL CUTOUT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED., FABRICATED A DOUBLER, AND INSTALSDR AWXA200200969Skin · corrodedYVR - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON SKIN OF THE # 1 ENGINE PYLON UPPER FAIRING JUST FORWARD OF THE UPPER ATTACH POINT, SKIN BULGED BETWEEN SKIN JOINTS AS VIEW FROM UPPER SURFACE. MAINTENANCE REMOVED FASTENERS AND LIFTED SKIN ; CLEANEDSDR USAA020330Skin · crackedPIT - FOUND PYLON SKIN CRACKED 1 INCH, RIGHT ENGINE PYLON ACCESS PANEL 5828R, STATION 196.700. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M)SDR CALA0200448Skin · crackedINSPECTION FOUND A 1" CRACK IN UPPER SURFACE OF #1 ENGINE PYLON PANEL 5727L CUTOUT. REPAIRED CRACK IAW ECRA 5430-01230, REV B.SDR QXEA0201324Skin · chafedPDX - NR 2 NACELLE EXHAUST DECK/SKIN IS CHAFED ON UNDERSIDE BY OIL DRAIN LINE. REPAIRED IAW RD 8-54-097.SDR F3LA200200228Skin · delaminatedDURING C-7 CHECK, INSPECTION REPORTED NO. 2 ENGINE PYLON TOP FWD SKIN DELAMINATED AT FWD INBD CORNER. REPAIRED AND REFINISHED PER SRM 51-70-17.SDR UPS02439278Panel · wornINSPECTION TYPE:C NR 3 PYLON - O/B AFT UPPER MOUNT HALF MOON PANEL CUTOUT WORN AT FWD PORTION. NR 3 PYLON O/B AFT UPPER MOUNT HALF MOON PANEL CUTOUT REPAIRED AS PER SRM 54-30-03 FIG 35 AND FIG 36.SDR UPS02839134Skin · crackedINSPECTION TYPE:C1 NR 1 PYLON O/B SIDE AT PNL 199A UPPER SKIN IS CRACKED. FABBED DOUBLER IAW DC8 SRM 54-2-0, INSTALLED DOUBLER IAW DC8 SRM 51-1-20D.SDR QXEA0201181Skin · scratchedPDX- NR 1 NACELLE FORWARD ALUMINUM LANDING FOR PANEL 412DT HAS SCRATCHES ALONG FORWARD SKIN EDGE. REPAIRED IAW DHC8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-36.SDR QXEA0201179Skin · gougedPDX- NR 1 NACELLE AFT ALUMINUM LANDING FOR PANEL 412DT HAS A GOUGE IN THE CENTER OF LANDING. REPAIRED IAW DHC8 SRM 51-20-11, PAGE 7, SRM 51-20-16 AND SRM 51-20-36.SDR UPS02439098Skin · damagedINSPECTION TYPE:C NR 2 PYLON I/B REAR MOUNT PYLON SKIN LOWER EDGE DOUBLER NONSTANDARD REPAIR IS FOUND AS MARKED. NR 2 PYLON I/B LOWER EDGE SKIN REPAIRED AS PER SRM 54-34-03 FIG 24 AND SRM 54-34-03 FIG 25.SDR UPS02439099Skin · deformedINSPECTION TYPE:C NR 1 PYLON RT LOWER EDGE AREA FROM NAC STA 180- REAR DRAG FIXED FAIRING INTERIOR METAL SKIN DEFORMED AS MARK. NR 1 PYLON RT LOWER EDGE AREA FROM NAC STA 180- REAR DRAG FIXED FAIRING INTERIOR METAL SKIN REPLACED AS PER SRM 54-34-03 FIG 25.SDR GTIA020860Skin · damagedDTW - NR 2 ENGINE INLET COWL WIRE MESH LINER TORN. REPAIRED TORN LINER WIRE MESH NR 2 ENGINE INLET COWL. (M)SDR UPS02239018Panel · delaminatedINSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED, INNER SURFACE FWD END. REPAIRED IAW SRM 51-40-5.SDR UPS02239017Panel · delaminatedINSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER, SURFACE FWD END. REPAIRED IAW SRM 51-40-5.SDR CALA0200425Panel · crackedINSPECTION FOUND A 1 INCH CRACK AT EDGE OF ACCESS HOLE IN NR 1 ENGINE PYLON PANEL 5724L. INSTALLED REPAIR DOUBLER IAW ECRA 5430-01204.SDR COMA0260491SkinFASTENER HOLE ON PNL 422EB IS DAMAGED.REAMED HOLE TO .4045" AND INSTALLED A FREEZE PLUG FABRICATED FROM AMS 5659 PO #23283/1 AND REPLACED PROTECTIVE FINISH. WORK WAS PERFORMED I/A/W WVAC 601R-54-3374B APPROVED BY 8110-3 DATED 07/19/02. REF COMAIR W/O 29767 MAISDR COMA0260444ChannelWEB AND CHANNEL IN THE R/H MLG BAY @ F.S. 50.45 WERE INADVERTANTLY DAMAGED DURING GEAR RETRACTION.TRIMMED OUT DAMAGED WEB SKIN AND REPROFILED THE CHANNEL LIP. EDDY CURRENT INSPECTION WAS PERFORMED TO ENSURE CHANNEL INTEGRITY, FILLER AND REPAIR DOUBLER WERE FABSDR SIMA200220501Skin · crackedFOUND RT NACELLE OUTBOARD FORWARD SKIN HAS POSSIBLE CRACK AT RIVET. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND INDICATION OF A CRACK. PERFORMED CUT TO INNER SKIN TO GAIN ACCESS TO DAMAGE AREA. REMOVED DAMAGED SKIN BY CUTOUT AND PERFORMED AN NDT INSPESDR UIEA200200025Skin · wornDURING CURRENT (C) CHECK, INSPECTION OF NR 3 PYLON ACCESS PLATE (473AR) CUTOUT, FOUND HEAVY WEAR AT ONE OF THE LATCH POSITIONS. WEAR AREA TRIMMED AWAY FROM SKIN AND DOUBLER. DOOR ACCESS SIZE INCREASED ON RETAINING LIP. FABRICATED REPAIR DOUBLER AND FILLERS.SDR SIMA200220001Skin · damagedFOUND RT NACELLE INBOARD FORWARD SKIN HAS THREE RIVETS RECESSED THROUGH SKIN. PERFORMED CUT TO INNER SKIN TO GAIN ACCESS TO DAMAGED AREA. FABRICATED AN INNER SKIN SPLICE DOUBLER. REPAIR DONE IAW SRM PRACTICES.SDR QXEA0201035Skin · dentedPDX - DENT IN NACELLE SKIN, INBOARD SIDE OF NACELLE, AT APPROXIMATELY STATION XN121.2, ZN20.25, JUST FORWARD OF DRAIN MAST. REPAIRED IAW HORIZON AIR EA 2-54-146.SDR MALA020421Skin · damagedDURING 4K-CHECK IN CWA, LT INBOARD COWL AFT UPPER CORNER FOUND DENT AND A PIECE OF SKIN MISSING. MAINTENANCE REPAIRED DAMAGE IAW SAAB STATEMENT 340SDS004112 AND EO S54059. REFER TO 409 109730. RELEASE DATE 7/17/02SDR GTIA020785Cowling · peelingDTW - NR 2 ENGINE NOSE COWL, INLET LINER, METAL MESH PEELING AT 12 O'CLOCK POSITION. REPAIRED WIRE MESH ON NR 2 ENGINE, INLET COWL IAW MD80 SRM 54-04. (M)SDR HMG2002F00002Door · departedLT INBOARD NACELLE DOOR DEPARTED AIRCRAFT IN FLIGHT AND PUNCTURED THE FUSELAGE.SDR QXEA0200989Skin · corrodedPDX - FRETTING CORROSION ON AFT ALUMINUM LAND UNDER PANEL 422DT NEAR CENTER NUT PLATE. REPAIRED IAW DHC-8-202 SRM 54-00-16, TABLE 1 ON PAGE 2.SDR QXEA0200988Skin · corrodedPDX - FRETTING CORROSION ON AFT ALUMINUM LAND UNDER PANEL 422DT NEAR CENTER NUT PLATE. REPAIRED IAW DHC-8-200 SRM 51-00-26, TABLE 2 ON PAGE 2.SDR KBMA117644Latch · wornRIGHT REAR ENGINE COWLING LATCH IS WORN. REPLACE WITH SERVICEABLE LATCH.SDR CALA0200376Skin · crackedINSPECTION FOUND 1/2 INCH CRACK IN NR 1 PYLON ACCESS PANEL CUTOUT FOR PANEL 5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR ZW0A0206903Skin · crackedDURING CHECK-C MAINT ON THE RT PYLON THE FWD INBD SIDE LIGHTNING HOLE ON NUMBER 2 PYLON WAS CRACKED 1/2 INCH LONG. CONFIRMED BY NDT. REPAIRED PER SERVICE BULLETIN 757-54-0037, AND EMLR 73125. --CLOSED--SDR ZW0A0206901Skin · crackedDURING CHECK-C MAINT ON NUMBER 1 PYLON FOUND A 1 7/8 INCH CRACK EXTENDING FROM UPPER FORWARD CORNER OF FORWARD LIGHTNING HOLE IN LT SIDE SKIN OF PYLON. CONFIRMED BY EDDY CURRENT. INSTALLED FORWARD DOUBLER ON OTBD SIDE PER SERVICE BULLETIN 757-54-0037 AND EMLSDR UPS02838712Skin · crackedINSPECTION TYPE:C2, NR 1 PYLON OUTBOARD SIDE SKIN IS CRACKED AT YN 343. NDT VERIFIED CRACK TERMINATES AT END OF PART. FABRICATED AND INSTALLED DOUBLER IAW DC8 70 SERIES SRM 54-2-0 FIG 6.SDR AWXA200200543Skin · crackedLCQ - MAJOR REPAIR - DURING C-8 INSPECTION A CRACK WAS FOUND ON THE NR 1 ENGINE PYLON FRAME AT THE LOWER FORWARD CORNER OF ACCESS APNEL 433AL CUTOUT. MAINTENANCE STOP DRILLED CRACK IAW B757 SRM 51-10-02 PAGE 17. FABRICATED REPAIR DOUBLER .125 STELL 15 SPH, HEASDR 02FDEA00392Skin · chafedSKIN CHAFED AT BS 1352 AT NR 2 ENG RT RAIN GUTTER 15 INCHES BELOW NR 3 PYLON T/E AND RAIN GUTTER. REMOVED AND REPLACED PER EA 7-5410-64955 & SRM 54-30-3.SDR GTIA020576Skin · delaminatedDTW - FOUND ON DAILY INSPECTION, FOUND NR 2 ENGINE UPPER COWL DELAMINATED MIDWAY ALONG LENGTH. SUSPECT BLEED DUCT LEAKAGE. INTERIM EXTERNAL DOUBLER REPAIR INSTALLED ON RIGHT UPPER COWL DOOR EXTERNAL SURFACE PER SPIRIT AIRLINES EA 7110-0202 ON C/O 28664-2. (SDR UPS02438357Skin · crackedINSPECTION TYPE:N/A NR 3 ENG SLOT SEAL AREA PYLON SKIN CRACK I/B SIDE REF D238005 AND REF LP702147. NR 3 ENG SLOT SEAL AREA PYLON SKIN REPAIRED AS PER HAECO RS R-54-51-34 826 & UPS EO 747-54-20019.SDR CA020527004Access Panel · departed(CAN) ON ARRIVAL AT DESTINATION, FOUND INBOARD OF NR 1 ENGINE, INSPECTION PANEL (BLOW OUT), MISSING ( BROKEN AT HINGE LEVEL, REFERENCE IPC 57-33-10,ITEM 272). MAINTENANCE INSPECTED THE LT LOWER WING LEADING EDGE ACCESS AND NO DAMAGE FOUND. A LEAK CHECK WAS CASDR UPS02438688Access Panel · crackedINSPECTION TYPE:C NR 1 PYLON ACCESS PANEL NR 452 BL CUTOUT ARE CRACKED AT 2 LOCATIONS AS MARKED. CUTOUT NR 1 PYLON ACCESS PANEL NR 452 BL REAR CUTOUT TWO LOCATIONS REPAIRED IAW RS R54-51-34816.SDR CALA0200254Skin · crackedINSPECTION FOUND A 1/2" CRACK IN #2 ENGINE UPPER PYLON SKIN AT ACCESS PANEL 5827R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR SIMA200210206Fairing · chafedDURING INSPECTION OF AIRCRAFT, FOUND RIGHT INBOARD NACELLE FILLET FAIRING CHAFED. BLENDED OUT CHAFE. FABRICATED AND INSTALLED DOUBLER IAW SAAB 340 SRM 54-10-10 AND STANDARD SRM PRACTICES. (M)SDR CALA0200190Skin · crackedINSPECTION FOUND A 1/4" CRACK IN UPPER PYLON SKIN PANEL #5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV. B.SDR USAA020131Skin · crackedPHL - FOUND ON WALKAROUND, SKIN CRACKED AND MISDRILLED FASTENR HOLE .375 INCH, CRACK BEYOND RIVET RIGHT ENGINE PYLON OUTBOARD. REPAIRED PER TYPICAL REPAIR 54-50-07. (M)SDR 81TJ41902Skin · chafedLEADING EDGE SKIN PANEL OF RIGHT PYLON HAS CHAFED HOLE FROM CONTACT WITH COWLING.SDR 81TJ41802Skin · crackedRIGHT UPPER MIDDLE ENGINE PYLON SKIN DUE TO CRACKING AT LOCATION OF PRE-EXISTING REPAIR OF HOLE AND CRACK IN SKIN.SDR F3LA200200122Fairing · delaminatedDURING C-2 CHECK, INSPECTION REPORTED DELAMINATION ON TOP INSIDE DUCT OF NR 1 ENGINE INBOARD THRUST REVERSER MID STREAM FAIRING AND METAL MISSING. REMOVED DAMAGE, FABRICATED DOUBLER AND INSTALLED REPAIR PER EA 54-737-041 AND SRM 51-10-02.SDR GAIA02011OPSkin · crackedDURING B-CHECK INSPECTION MAINTENANCE, FOUND A 2.5 INCH CRACK TO THE NR 3 ENGINE NOSE COWL SKIN LOCATED AT NAC STATION 77.5. MAINTENANCE REMOVED AND REPLACED THE NR 3 ENGINE NOSE COWL. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)
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