JASC 5420
Service difficulty reports · 3,949
Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, 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 = '5420' 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 = '5420' 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 UALA2013050203053Fastener · missingON ARRIVAL, NR 2 ENGINE PYLON PANEL 482A MISSING ONE FASTENER FROM LOWER FWD EDGE. REPLACED FASTENER AND SECURED ADJACENT FASTENERS.SDR SWAA2013052016251Structure · crackedNR 1 ENGINE PYLON /APRON SMALL CRACKED ON UPPER LONGERON AT AFT HINGE CUTOUT. REPAIR DOUBLER IAW SRM.SDR AALA20130424008Bracket · damagedRIGHT ENGINE FIRE BARRIER BRACKET INBOARD SIDE IS DAMAGED JUST BELOW PYLON TORQUE BOX, 8 INCHES AFT OF EXHAUST NOZZLE SEPARATION FLANGE. REPLACED FIRE BARRIER BRACKET PER SRM 51-40-02-0G.SDR REXA2013041900526Panel · brokenLEFT ENGINE UPPER AFT HINGE PANEL BROKE. REMOVED AND REPLACED LEFT ENGINE UPPER AFT HINGE LINE FAIRING IAW CRJ 900 AMM 54-12-01.SDR UALA2013041802685Liner · missingACOUSTIC INSULATION AT 2 O'CLOCK IS MISSING A PIECE ON RIGHT ENGINE 1.5 INCHES DIAMETER PIECE MISSING IN RIGHT ENGINE FRONT FAN CASE RUB STRIP. REPAIRED RUB STRIP PER MM.SDR UIEA2013041300197Block · unsecureCLAMP BLOCK FOR HYD LINES FOUND IN BOTTOM OF NR 2 PYLON. INSTALLED CLAMP BLOCK OF HYDRAULIC LINES.SDR UALA2013041502543Seal · missingA SIX INCH RUBBER SEAL MISSING FROM RIGHT ENGINE INBD PYLON WING ROOT. REPLACED SEAL.SDR V0XR2013041000002Structure · crackedRIGHT HORSE COLLAR CRACKED ON TOP AFT FLANGE IN RADIUS. REPAIRED CRACK ON RIGHT NACELLE HORSE COLLAR TOP ANGLE BY REMOVING DAMAGE, CRACK DETECT USING EDDY CURRENT METHOD PER PSM 1-8-7A, AND INSTALLING 0.063 TITANIUM REPAIR PACKERS AND ANGLE, 0.040 TITANIUM COSDR V0XR2013041000001Structure · crackedLEFT HORSE COLLAR CRACKED TWO PLACES ON TOP AFT FLANGE IN RADIUS. REPAIRED TWO EACH CRACKS ON LEFT NACELLE HORSE COLLAR TOP ANGLE BY REMOVING DAMAGE, CRACK DETECT USING EDDY CURRENT METHOD PER NDT MANUAL PSM 1-8-7A, AND INSTALLING REPAIR ANGLE AND PACKERS OF SDR SWAA2013042415090Angle · crackedNR 1 ENGINE STRUT FAIRING ANGLE CRACKED AT STA 363.65. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.SDR FDEA201304090751Shim · migratedNR 1 PYLON UPPER ANGLE INNER WALL AT PPSTA 136.60 HAS SHIM MIGRATION. THIS IS CLASSIFIED AS CATEGORY B REPAIR.SDR FDEA201304090749Shim · migratedNR 1 PYLON LT CUTOUT LOWER RIB MOUNT AT PPSTA 174.30 HAS SHIM MIGRATION. EVALUATED MIGRATED SHIM MAXIMUM MIGRATION IS 0.200, FOUND TO BE WITHIN LIMITS IAW SRM54-50-90 REPAIR 7. CLASSIFIED CATEGORY B REPAIR .SDR FDEA201304090748Shim · migratedNR 1 PYLON LT CUTOUT LOWER RIB MOUNT AT PPSTA 174.30 HAS SHIM MIGRATION. EVALUATED MIGRATED SHIM MAXIMUM MIGRATION IS 0.200, FOUND TO BE WITHIN LIMITS IAW SRM 54-50-90 REPAIR 7.SDR SWAA2013050615568Pan · crackedCRACK ON PAN LOCATED OUTBOARD SIDE ASSY AFT STRUT FAIRING ENGINE NR 1. REPAIRED PAN IAW EA.SDR UALA2013040902371Nut Plate · defectiveSCREW STICKING OUT ON NR 1 PYLON OUTBOARD SIDE. MAINT TEXT: FWD FAIRING, AFT SECTION, LOWER OUTBD CORNER HAS 1 SCREW STICKING OUT, SEE FIG 1, AMM 54-52-00 PAGE 2. NEEDS NUT PLATE REPLACED. SCREW IS ON TRAILING EDGE 1 SCREW UP FROM CORNER. CF FOR REPAIR RESDR SWAA2013050715751Angle · crackedNR 1 ENGINE STRUT TORQUE BOX ACCESS NR 5757L ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.SDR SWAA2013041214796Rub Strip · missingRUB STRIPS MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5831R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.SDR SWAA2013041214795Rub Strip · missingRUB STRIP MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5828R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.SDR SWAA2013041214793Rub Strip · missingRUB STRIPS MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5827R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.SDR SWAA2013041214792Rub Strip · missingRUB STRIP MISSING AT INTERNAL AREA OF CUT OUT OF PYLON ACCESS PANEL 5724L NR 1 ENGINE. INSTALLED RUB STRIP IAW DWG.SDR SWAA2013042415084Stiffener · crackedSTIFFENER CRACKED LOCATED AFT STRUT FAIRING LOWER SURFACE OF ENGINE NR 1. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.SDR SWAA2013041814968Stiffener · crackedNR 6 INBD SIDE RT PYLON STIFFENER CRACKED AT ON FLAP TRACK FAIRING. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.SDR C77A20130406009Fairing · chafedLEFT AFT PYLON FAIRING HAS CHAFING ON FWD LEADING EDGE ON LT AND RT SIDES. BLENDED CHAFED AREA, TREATED AND PRIMED IAW SRM 51-10-03 & 51-12-01.SDR UALA2013040402245Panel · warpedRT PYLON PANEL 482AR WARPED. REPLACED PYLON FAIRING PANEL. PCN 110-1627SDR SWAA2013050715777Structure · crackedLEFT WING LEFT APRON CRACKED AT AFT UPPER COWLING LATCH HINGE CUTOUT. REPAIRED CUTOUT PER SRM.SDR REXA2013033100487Panel · crackedRIGHT PYLON UPPER AFT HINGE PANEL CRACKED AT THE AFT FASTENER. REPAIRED HINGE FAIRING PANEL IAW CRJ 900 SRM 51-40-11.SDR UALA2013040202150Block · wornDURING RIGHT ENGINE PLUMBING INSPECTION EQ7592, SEVERAL BLOCKS FOUND WORN. REPLACED RUBBER BLOCKS ON HYD LINE BETWEEN NAC STA 180.8 AND 149.5.SDR UALA2013040202126Fairing · out of toleranceREF CF0606 NEED TO REMOVE STRUT BIFURICATION PANEL AT THE 12 O'CLOCK POSITION ON THE NR 2 ENGINE. REPLACED OUTBOARD BIFURICATION FAIRING AT THE 12 O'CLOCK POSITION.SDR UALA2013040102109Structure · dentedON POSTFLIGHT IN MCO NOTICED 2 SHALLOW DENTS BELOW OIL SERVICE DOOR ON ENGINE 1. FILLED DENT, SMOOTHED SURFACE AND RE-APPLIED FINISH.SDR SWAA2013050615566Pan · crackedCRACK ON LOWER PAN LOCATED ASSY AFT STRUT FAIRING OUTBOARD SIDE ENGINE NR 1. REPAIRED PAN IAW EA.SDR SWAA2013042415085Fitting · crackedLEFT PYLON NACELLE TO FLAP TRACK FAIRING INTERFACE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM AND DWG.SDR SWAA2013040114318Pan · crackedLEFT PYLON HEAT SHIELD STRUT FAIRING PAN CRACKED. REPAIRED PAN IAW EA.SDR REXA2013033000418Riser · corrodedLEFT PYLON THRUST FITTING PRODUCTION RISER FRETTED. REPAIRED IAW BOMBARDIER REO 601R-54-50-036.SDR REXA2013033000417Riser · corrodedRIGHT PYLON THRUST FITTING PRODUCTION RISER FRETTED. REPAIRED IAW BOMBARDIER REO 601R-54-50-036.SDR SWAA2013040114317Fitting · crackedLEFT PYLON NACELLE TO FLAP TRACK FAIRING INTERFACE FITTING CRACKED. REPAIRED FITTING IAW EA.SDR SWAA2013040114304Rub Strip · crackedNR 1 ENGINE NACELLE STRUT ACCESS PANEL 57700L RUB STRIP CRACKED. REMOVED AND REPLACED RUB STRIP IAW SRM AND DWG.SDR SWAA2013040114303Rub Strip · crackedNR 1 ENGINE NACELLE STRUT ACCESS PANEL 5747L RUB STRIP CRACKED. REMOVED AND REPLACED RUB STRIP IAW SRM AND DWG.SDR HNAA2013032600180Strip · corrodedRIGHT NACELLE REAR CONE, TOP ALUMINUM STRIP IS CORRODED. R & R WITH FABRICATED PART IAW SRM 51-40-00.SDR HNAA2013032500160Angle · crackedCRACKED ANGLE FOUND AT INTERSECTION OF LANDING PLATE ON LT NACELLE. R & R ANGLE AT INTERSECTION OF LANDING PLATE IAW DWG 85410245.SDR HNAA2013032200156Structure · crackedLT FINGERNAIL INBD RIBLET IS CRACKED. R & R RIBNET IAW SRM 51-42-05.SDR HNAA2013032200155Plate · crackedLEFT LANDING PLATE OF PANEL 412DT, AFT SIDE IS CRACKED. R & R PLATE IN LT NACELLE IAW SRM 51-42-05 AND SRM 51-40-00.SDR HNAA2013032200154Angle · crackedFORWARD INBD ANGLE IS CRACKED ON LT FINGERNAIL. R & R LT ANGLE IAW SRM 51-42-05 AND SRM 51-40-00.SDR HNAA2013032200148Structure · crackedLEFT FINGERNAIL OTBD RIBLET IS CRACKED. R & R FINGERNAIL RIBLET IAW SRM 51-42-05.SDR HNAA2013032200146Angle · crackedLT NACELLE ANGLE FOUND CRACKED ON OTBD SIDE AT INTERSECTION OF LANDING PLATE AND OTBD SIDE WEB. R & R ANGLE IAW SRM 51-42-05.SDR HNAA2013032100139Heat Shield · crackedINBD AND OTBD STRINGER FOUND CRACKED UNDER LT NACELLE HEAT SHIELD, AFT END. R & R WITH MADE REPAIRED PARTS. INSTALLED IAW STRUCTURAL REPAIR MANUAL 51-42-42205SDR DALA1307980184Stiffener · damagedELONGATED FASTENER HOLES ON STIFFENER AT UPPER SPAR WEB LT SIDE. REPAIRED IAW PRI 511842-14AD REV 1 AND ER/A 511842-14AD, REV ORIG.SDR SWAA2013041514844Nut Plate · crackedCRACK ON NUT STRIP LOCATED UNDER ACCESS PANEL 58710R UPPER PYLON AREA ENGINE 2. REMOVED AND REPLACED NUT STRIP IAW SRM AND DRAWING.SDR SWAA2013040114334Rub Strip · crackedRUB STRIP LOCATED ON INTERNAL STRUCTURE OF ACCESS PANEL 5847R FWD STRUT FAIRING AREA ENGINE NR 2 CRACKED. REMOVED AND REPLACED RUB STRIP IAW SRM AND DRAWING.SDR SWAA2013032814223Support Angle · crackedRIGHT WING NR 2 PYLON O/B UPPER T/E SUPPORT ANGLE CRACKED AT AFT END. REMOVED AND REPLACED ANGLE IAW SRM.SDR SWAA2013041514843Nut Plate · crackedCRACK ON NUT STRIPS LOCATED INTERNAL AREA OF ACCESS PANEL 57710L ENGINE NR 1. REMOVED AND REPLACED NUT STRIPS IAW SRM AND DWG.
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