JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 QXEA200500878Cowl Door · wornYYC - LEFT ENGINE LOWER FAN COWL DOOR INNER INBOARD SURFACE WORN BY ELECTRICAL HARNESS. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01 AND 51-25-01-001-001-A01.SDR QXEA200500877Cowl Door · wornYYC - LEFT ENGINE LOWER FAN COWL DOOR INNER INBOARD SURFACE WORN BY TRAILING EDGE FLEX CABLE. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001, 51-25-01-001-001-A01.SDR QXEA200500811Cowling · chafedYYC - LEFTHAND ENGINE TRANSLATING COWL IS CHAFING ON FORWARD COWL WHEN STOWED AT UPPER ANDL LOWER COWLS. REPAIRED IAW HORIZON AIR EA R-78-39, EA R-78-40 AND REO 670-78-33-363.SDR QXEA200500821Flange · chafedYYC - RIGHT ENGINE LOWER TRANSCOWL FORWARD FLANGE IS CHAFING ON THE TORQUE BOX AT APPROXIMATELY 7:00 POSITION. REPAIRED IAW HORIZON AIR EA R-78-38 AND REO 670-78-33-362.SDR QXEA200500817Beam · gougedYYC - LEFT PYLON HINGE BEAM AT PYLON TIE BAR HAS GOUGES ON HINGE, TOP AND LOWER LOCATION FROM TIE BAR BRACKETS RUBBING. REPAIRED IAW CRJ700 MM 78-36-05-000-801-A01, PAGE 402, PARAGRAPH C, STEPS 1-4, REO 670-78-34-360 AND CRJ700 SRM 51-25-06-001-001-A01.SDR QXEA200500828Door · wornYYC - RIGHT ENGINE TRANS COWL LATCH DOOR ASSEMBLY AREA, DOOR LATCH CONTACT POINT WORN. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01.SDR 05FDEA00797Door · corrodedNR 1 PYLON PANEL 416AR HAS AREA AROUND SCOOP AND EXTENDING UNDER SCOOP WITH CORROSION. REMOVED AND REPLACED DOOR ASSY PER A310-200 AMM 54-50-00-4, DUE TO CORROSION OUT OF LIMITS PER A310-200 SRM 54-50-00 TABLE 102, SHEET 2.SDR DHL2005740557Structure · dentedDENT LT SIDE FUSELAGE STA 1374, NR 2 ENGINE SUPPORT STRUCTURE. REMOVED FASTENERS AT LT SIDE FUSELAGE SKIN STA 1374 NR 2 ENGINE SUPPORT STRUCTURE IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .050 PO NR 9002093 SIZE 5 1/4" BY 5 1/4" IASDR 05FDEA00740Gusset · corrodedNR 1 PYLON OUTBD SIDE AT RIB 15 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310200 SRM 51-72-10.SDR 05FDEA00739Gusset · corrodedNR 1 PYLON OUTBD SIDE AT RIB 16 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310-200 SRM 51-72-10.SDR 05FDEA00738Gusset · corrodedNR 1 PYLON OUTBD SIDE AT RIB 17 ANGLE HAS CORROSION AROUND 4 HOLES. REMOVED AND REPLACED GUSSET IAW A310-200 SRM 51-72-10.SDR ABXA050083Splice · crackedINBOARD FRAME FOOT ON AFT SIDE OF LEFT PYLON BULKHEAD WAS CRACKED. REPLACED CRACKED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR 05FDEA00568Rib · corrodedNR 2 PYLON OTBD SIDE RIB 16A UPPER AREA BRACKET LWR AREA HAS AN AREA OF CORROSION EXTENDING UNDER FASTENERS. REMOVED AND REPLACED BRACKET IAW A310-200 SRM 51-72-10. REINSTALLED 3 NUTPLATES IAW A310 SRM 51-40-21. (SEE JPF)SDR DHL2005782535Skin · dentedNR 3 ENG NOSE COWL, EXTERIOR SKIN AT 3 O'CLOCK AFT SKIN SURFACE EDGE IS DENTED, ERODED AND SEPARATING. DAMAGE ON NR 3 ENG NOSE COWL EXTERIOR SKIN 3 O'CLOCK AFT SKIN FOUND TO BE OUT OF LIMITS IAW 727 SRM 54-30-1 FIG 1. CUT OUT DAMAGED AREA, FABBED FILLER FROMSDR DHL2005782533Nose Cowl · dentedNR 3 ENGINE NOSE COWL, EXTERIOR SKIN AT 9 O'CLOCK FWD OF LOWER LATCH HANDLE, SKIN IS DENTED. DAMAGE ON NR 3 ENGINE NOSE COWL EXTERIOR SKIN AT 9 O'CLOCK FWD OF LOWER LATCH HANDLE OUT OF LIMITS IAW 727 SRM 54-30-1 FIG 1. CUTOUT DAMAGED AREA DIM 1 INCH BY 3/4 ISDR 05FDEA00469Bracket · corrodedNR 1 PYLON OTBD SIDE UPPER AREA RIB 15A BRACKET ON LWR AREA HAS CORROSION EXTENDING UNDER FASTENERS FOR NUT PLATE. CORROSION REMOVED IAW A310 SRM 51-74-10, NDT MATERIAL THICKNESS AFTER THICKNESS IS OUT OF LIMITS. REMOVED AND REPLACED BRACKET AND 3EA NUTPLASDR 05FDEA00398Rib · crackedNR 1 PYLON 1 INCH AFT OF RIB 19 I/B SIDE WEB ATTACH POINT HAS A .5 INCH CRACK REF N00647. REMOVED AND REPLACED WEB AT RIB 19 IAW SRM 51-40-21 & 51-72-10.SDR 05FDEA00397Support Angle · crackedNR 1 PYLON - ACCESS 475AL- RT UPPER INTERIOR ANGLE SUPPORT CRACKED IN T-SHAPED LENGTH EA WAY 1.0 INCH REF N00449. REMOVED AND REPLACED ANGLE SUPPORT IAW SRM 54-55-51.SDR 05FDEA00328Longeron · chafedNUMBER 3 ENGINE INBOARD CORE CORE COWL UPPER SEAL IS CHAFFED. FOUND CORE COWL LONGERON CHAFED WHILE REMOVING CHAFE STRIP. REPAIRED LONGERON IAW FEDEX EA 8- 5410-83991, NACELLES/PYLON- NUMBER 3 ENGINE INBOARD CORE COWL UPPER LONGERON. REPAIR, REMOVED AND REPSDR QXEA200500475Access Panel · corrodedYYC - LEFT HAND COWL LATCH ACCESS PANEL 433AL HAS FRETTING CORROSION AT INTERNAL EDGE. REPAIRED IAW CRJ700 SRM 54-21-00-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-06-001-001-A01.SDR QXEA200500514Arm · gougedYYC - LEFT HAND NACELLE LATCH DOOR HINGE ARMS ARE GOUGED. REPAIRED IAW CRJ700 SRM 51-25-00*-001-001-A01, SRM51-12-00-001-001-A01, AND SRM 54-21-00-101-001-A01.SDR QXEA200500356Support · crackedPDX - NR 2 ENGINE LOWER COWL, BYPASS DUCT CENTER SUPPORT FRAME IS CRACKED ON UPPER FLANGE. REPAIRED IAW RD 8/4-71-016.SDR QXEA200500321Bracket · crackedPDX - LEFTHAND NACELLE LOWER COWL, CHANNEL AND BRACKET ARE CRACKED ALONG OUTBOARD EDGE OF BYPASS DOOR. REPAIRED IAW DHC-8400 SRM 51-42-05.SDR 252TR0035Panel · crackedLEFT ENGINE O/B COWL EXHAUST LOUVER PANEL CRACKED. WELDED PER BAC SPEC 5975.SDR 252TR0034Panel · crackedRIGHT ENGINE I/B COWLING EXHAUST LOUVER PANEL CRACKED. WELDED PER BAC SPEC 5975.SDR HYI2005F00003Beam · crackedDURING ENGINE NACELLE INSPECTION, FOUND 1.5 INCH CRACK ON TOP REAR RADIUS OF CROSSOVER BEAM. REMOVED BEAN AND INSTALLED NEW BEAM IAW MFG MM. (NE01200502852) (K)SDR UPS05443931Web · crackedINSPECTION TYPE: C, NR 2 PYLON REAR LOWER WEB AT NAC STN 212 I/B EDGE UPPER SURFACE RIVETS HOLES FOUND CRACKED. NAC STN 212 REAR LOWER WEB REPAIRED PER SRM 54-10-03 FIG 2.SDR UPS05543860Pylon · crackedNR 2 ENGINE PYLON CRACKED. RT ENGINE FIRESHIELD ABOVE AND AFT OF REAR ENG MOUNT IS CRACKED. REMOVED DAMAGED FIRESHIELD AND DRILLED NEW SHIELD AND INSTALLED LOCK FASTENERS IN UPPER LEG AS PER DWG 311N3570. FINISHED INSTALLATION OF RT ENGINE FIRE SHIELD IAW DWSDR 05FDEA00253Support Fitting · gougedNR 1 PYLON, STATION YN256, MOUNT BRACKET FOR LEFT AND RIGHT THRUST REVERSER ACTUATORS, OPEN/CLOSE BEARING WORN AND GOUGED. COMPLIED WITH FEDEX EA 8-5450-83973, NACELLES/PYLON - NR 1 PYLON FAN REVERSER JACK SCREW SUPPORT FITTING GOUGED - REPAIR, REMOVED AND RESDR QXEA200500366Boot · damagedYYC - LEFTHAND BOOT TAIL PANEL 414BB MOUNTING AREA HAS SEVERAL DRILLED OFF SCREWS STUCK IN THE ANCHOR NUTS. REPLACED ANCHOR NUTS IAW TASK 51-42-35-330-801.SDR ABXA050032Angle · crackedCRACK INDICATION ON ANGLE, UPPER INTERIOR SURFACE OF PYLON, 3RD FROM FRONT SPAR. REMOVED ANGLE, FABRICATED NEW ANGLE, REINSTALLED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA050027Attach Angle · crackedLOWER LEFT PYLON ATTACH ANGLE WAS CRACKED INBOARD OF PYLON ACCESS PANEL 8101. REPAIRED AREA IAW DC-9 SRM 54-04.SDR MALA050140Inlet · chafedDURING 6Y/4Y INSPECTION IN YYC, LT NACELLE, INLET PROTECTION DEVICE P/N NF24668-057 IS CHAFED COMPLETELY THROUGH AND IS BEING REPLACED. AIRCRAFT RETURNED TO SERVICE 01/18/2005.SDR 05FDEA00034Fairing · crackedNR 2 PYLON, AFTER FIXED FAIRING WITH CRACK AT LT. REMOVED IAW AMM 54-55-00. REPAIRED IAW FEDEX EA 6-5480-81822. INSTALED IAW AMM 54-55-00.SDR UPS05443630Stringer · crackedINSPECTION TYPE:N/A FOUND CRACK ON NR 3 PYLON STRINGER, LT JUST FWD OF NAC STA 221, AREA MARKED IN RED. STRINGER IS CRACKED FROM TOP TO BOTTOM. STARTED DRILLING OUT FASTENERS IN STIFFENER & STRINGER REMOVED STIFFENER AND RIB FABRICATED REPAIR PARTS. ALODINESDR UPS05M43955Fitting · corrodedINSPECTION TYPE:C NR 2 ENG BELL MOUTH AFT LWR BRACE LINK SUPPORT AT 6 O'CLOCK POSN FOUND WITH SURFACE CORROSION AS MARKED. CORROSION REMOVED & SURFACE REPROTECTED AS PER SRM 51-21-01, ORIG THK 0.2 5 INCH & MAT REMOVED 0.043 INCH, FOUND EXCEEDED LIMIT AS SRM 5SDR 04FDEA03376Fairing · damagedACCOMPLISH MAINTENANCE "C" CHECK, 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. PYLON NR 2, LOWER AFTER FAIRING WITH INTERIM REPAIR ONSDR DL76S041080Door · missingON ARRIVAL FOUND MISSING BLOW OUT PANEL ON NR 2 ENGINE INBOARD PYLON. PANEL SIZE APPROX 9 INCHS DIAMETER. INSTALLED NEW ACCESS DOOR NR 2 PYLON INBOARD.SDR 04FDEA03325Bushing · wornDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ON PYLON NR 3 BUSHING AFT WITH WEAR. REPLACE BUSHING PER MM 54-00-02-4, P/N AUB 7281-1. SPHERICAL BEARING PER MM 54-40-02. PERFORM DIMENSIONAL CHECK OF HOLE TO DETERTMINE WHICH O/S BEARING TO ORDERED.SDR 04FDEA03202Liner · damagedPOST FLIGHT WALK AROUND FOUND SEVERAL AFT LINER SEGMENTS WITH UPPER SKIN GONE AND HONEYCOMB MATERIAL DAMAGED. ALMOST EVERY SEGMENT DAMAGED ON NR 1 ENGINE. NR 3 ENGINE FOUND AFT LINER SEGMENT OUTER SKIN DELAMINATED AND HONEYCOMB MATERIAL DAMAGED ALMOST COMPSDR 2004000015Cowling · departedAT CLIMB-OUT, NR 3 ENG LOST ENGINE COWLING DUMPED FUEL RETURNED TO EDDF.SDR 04FDEA03141Longeron · wornNR 1 ENGINE INBOARD CORE COWL UPPER LONGERON IS CRACKED AFT OF CENTER HINGE. REPAIRED IAW FEDEX EA 8-5410-81514, NACELLES/PYLON, NR 1 ENGINE RIGHT HAND CORE COWL UPPER LONGERON, REPAIR. REFERENCE NON-ROUTINE N00166.SDR 04FDEA03139Longeron · wornNR 3 ENGINE OUTBOARD CORE COWL UPPER LONGERON WORN AFT OF CENTER HINGE. REMOVED DAMAGED AREA IAW FEDEX EA 8-5410-81518, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX EA 8-5410-81518, NACELLES/PYLON, NR 3 ENGINE RIGHT HAND CORE COWL UPPER LONGERON REPAIR. SDR 04FDEA03138Longeron · wornNR 1 ENGINE RIGHT HAND CORE COWL UPPER LONGERON HAS 2 EACH GOUGES UNDER AFT HINGE. REMOVED AFT FITTING IAW DC10 SRM 51-31-01 VOL II. CUT OUT DAMAGED AREA IAW FEDEX EA 8-5410- 81531, NACELLES/PYLON, NR 1 ENGINE RIGHT HAND CORE COWL UPPER LONGERON, REPAIR. RESDR 04FDEA03020Longeron · chafedFOUND LONGERON FLANGE CHAFED BEYOND LIMITS, AREA 2.5 INCHED LONG BY 0.250 INCHES WIDE, COMPLETELY THROUGH .063 INCH FLANGE, NR 2 RIGHT HAND COWL, JUST AFT OF CENTER HINGE POINT. FABRICATED REPAIR AND INSTALLED REPAIR IAW FEDEX EA 8-5410-81503.SDR 04FDEA03019Longeron · wornREMOVED UPPER COWL CHAFE STRIPS AND FOUND LONGERON FLANGE CHAFED AREA 2.5 INCHES LONG BY 1.5 INCHES WIDE JUST AFT OF CENTER LINE, NR 1 ENGINE RIGHT HAND COWL. REPAIRED DAMAGED LONGERON IAW FEDEX EA 8-5410-81504.SDR ASOA04868Structure · crackedDURING A C-CHECK, THE LT AND RT UPPER EDGING ON THE LT LOWER NACELLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT UPPER EDGING ON THE LOWER NACELLE IAW SRM 51-25-03.SDR 04FDEA02951Panel · misalignedNR 1 PYLON PRECOOLER VENTILATOR PANEL ASSY PN AUB7054-501 FASTENER HOLES DO NOT ALIGN TO PYLON STRUCTURE. COMPLIED WITH EA 8-5480-81485 REV. A, NR 1 ENGINE VENTILATOR PANEL REPAIR.SDR CA041015003Cap · worn(CAN) FRESH AIR DUCT PN 6515317-12 FRETTED ON THE OUTBOARD FLANGE OF THE TEE SECTION CAP.SDR 04FDEA02913Longeron · wornNR 1 ENGINE LEFT HAND CORE COWL UPPER CHAFE STRIP WORN. FABRICATED DOUBLER, FILLERS, AND STRAP FOR LONGERON REPAIR IAW FEDEX EA8-7110-81487. INSTALLED LONGERON REPAIR IAW DC10 SRM 51-35-01 VOLUME II. FABRICATED RUB STRIP IAW DAC DWG NSL6016. INSTALLED RUB
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