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 AALA20120112AFW01Torque Box · gougedRIGHT PYLON STRUT TORQUE BOX OUTBOARD SIDE STATIONS 238 TO 248 DAMAGED. ACCOMPLISHED DOUBLER REPAIR PER SRM 54-52-01-2R FIGURE 201.SDR UALA2012010900212Fastener · looseCRACK ON INBOARD ENG 1 COWL. MAINT TEXT: REV SLEEVE HAS A PANEL SEPARATION, WITH A RIVET HEAD STICKING OUT 1-8". ANEL SEPARATION IS BETWEEN TS5,TS8,TS10. SEPARATION MEASURES 2 & 12-32"LONG. LOCATION IS 9 AND 34" DOWN FROM PYLON AND 19 AND 3-8" FWD OF THE AFSDR HNAA2012010900464Heat Shield · crackedCRACKS FOUND ON DIMPLED HOLES OF LT NACELLE AFT HEAT SHIELD AFT END. REPAIRED AFT SECTION HEAT SHIELD IAW RD 8-54-020. COMPLIED WITH HFEC INSP ON CUTOUT. NO DEFECTS NOTED.SDR HNAA2012010900461Heat Shield · damagedCRACKS FOUND ON DIMPLE HOLES OF LT NACELLE AFT HEAT SHIELD END. REPAIRED HEAT SHIELD AFT SECTION IAW RD8-54-020. HFEC INSP WAS CARRIED OUT ON CUTOUT IAW RD8-54-020. NO CRACKS INDICATION FOUND.SDR HNAA2012011090045Web · corrodedTAILCONE WEB CORRODED ON LT NACELLE. TAILCONE JOINT STRAP REPLACED WITH A MADE REPAIRED PART AND INSTALLED WITH SOILID RIVETS IAW SRM 51-42-05.SDR 2012FA0000058Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR 2012FA0000057Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR 2012FA0000056Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR 2012FA0000053Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR 2012FA0000052Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR 2012FA0000051Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR 2012FA0000050Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR 2012FA0000049Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR 2012FA0000048Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A SDR DALA1517929236Support Fitting · not reportedPYLON AFT SUPPORT FITTING UPPER FASTENERS REPAIRED IAW AA5440-01069.SDR ASOA201200161Seal · tornLEFT AFT CORE COWL FWD SEAL TORN. REMOVED TORN LT AFT CORE COWL SEAL IAW SRM 51-42-06-001-001-A01. DRILLED UP, TRIMMED TO FIT & DEBURRED IAW SRM 51-40-11-001-001-A01. INSTALL SERVICEABLE SEAL, NG161765 1/12/12. INSTALLED FWD SEAL ON AFT LT CORE COWL IAW SRSDR UALA2012010400075Heat Shield · damagedNR 2 ENGINE AFT PYLON HEAT SHIELD IS DAMAGED. REMOVED AND REPAIRED HEAT SHIELD.SDR UALA2012010400074Heat Shield · wornNR 1 ENGINE AFT PYLON HEAT SHIELD WORN. REMOVED AND REPAIRED HEAT SHIELD IAW CMM 54-52-17,ITEM 7C.SDR UALA2012010400073Strip · wornNR 2 ENGINE PYLON HEAT SHIELD SEGMENT AFT GAP STRIP WORN BEYOND LIMITS. INSTALLED NEW GAP STRIP IAW MT 54-UA2 .SDR UALA2012010400072Strip · wornNR 1 ENGINE AFT PYLON HEAT SHIELD SEGMENT GAP STRIP WORN BEYOND LIMITS. REPLACED NR 1 ENGINE AFT PYLON HEAT SHEILD GAP STRIP IAW IPC 54-54-02-007 AND 777 MT54-UA2.SDR REXA201100949Riser · corrodedRT PYLON PRODUCTION RISER HAS AREAS OF FRETTING ON FORWARD SIDE FROM 10 O’CLOCK TO 6 O’CLOCK POSITION APPROX .004 DEEP. REPAIRED IAW BOMBARDIER REO 601R-54-50-036.SDR UALA2011122707106Strip · wornNR 1 ENG PYLON AFT FAIRING HEAT SHIELD GAP COVER STRIPS NR 2, 3 AND 4 FOUND TO BE WORN AND CREATING A GOUGE IN HEAT SHIELDS NR 3, 4 AND 5.SDR UALA2011122107031Seal · deterioratedNR 4 ENG SAIL TAIL INBRD DOOR, LOWER FWD CORNER 2 EA SEALS DETERIORATED. REPLACED NR 4 SAIL TAIL INBRD DOOR FWD LOWER HORIZONTAL SEAL. VERTICLE SEAL INSTALLED BUT NEEDS TO BE REPLACED. REPLACED SEAL.SDR FDEA201112215399Shim · damagedNR 1 PYLON MID BULKHEAD, LOWER FLANGE, INBD FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS FRAYED AND MIGRATED.SDR FDEA201112215398Shim · damagedNR 1 PYLON MID BULKHEAD, LOWER FLANGE OTBD FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS FRAYED AND MIGRATED.SDR UALA2011122107012Structure · crackedINBD AND OTBD DRAIN HOLES CRACKED NR 2 PYLON AT NAC STA 156 AREA HAS BEEN PREVIOUSLY REPAIRED PER SRM ON PEMCO NR 3363N00937. ACP INSP AND PART MARKED PREV. RPR'D AREA PER PEMCO EA PD67-54-008 AND ECRA 5450-01910 ON NR 3363N00937. THIS IS AN APPROVED CAT B SDR UALA2011122107011Structure · crackedOTBD DRAIN HOLES CRACKED NAC STA 156. AREA HAS BEEN PREVIOUSLY REPAIRED PER SRM. SAMC TEXT: THIS ITEM IS REFERRING TO THE NR 1 PLYON. ACP INSP AND PART MARKED PREV. RPR'D AREA PER EA PD67-54-010 AND ECRA 5450-01901 ON NR 3363N00936. THIS IS APPROVED CAT SDR FDEA201112195364Bracket · chafedCASE DRAIN LINE LOOSE AND CHAFING AT NR 2 PYLON AFT END AT LOWER WING SKIN FEED THRU HOLE (AFT WING JACK PAD POINT). REPAIR ACCOMPLISHED IAW EA 6-5410-155854. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR NSVA2011335Structure · chafedCONTROL # 202-50: RT ENGINE INLET COMPARTMENT CHAFED IN CENTER DECK AREA. COMPLETED REPAIR IAW TD 340-54-11-02.SDR QXEA2011121901405Stiffener · crackedDURING C-CHECK, FOUND LEFT AFT FINGERNAIL COVER PANELS 414AL AND 414AR BOTH HAVE CRACKED AFT STIFFENERS. REMOVED DAMAGED STIFFENERS AND INSTALLED NEW STIFFENERS ON FINGERNAIL COVER PANELS 414AL AND 414 AR IAW SRM 51-42-05-02-01. PREPPED AND PRIMED PANELS IAWSDR UALA2011121506882Cover · erodedNR 1 ENG AFT PYLON HEAT SHIELD 3RD GAP STRIP COVER ERODED. REMOVED DAMAGE & CLEANED REF 777MT54-UA2. 22-32 LONG BY 3-32 DEEP.SDR UALA2011121406872Heat Shield · crackedNR 2 ENG AFT PYLON GAP STRIP NR 2 IS CRACKED. DRESSED OUT PER MT 54-UA2 1.25 INCHES LONG AND .21875 INCH DEEP. DRESSED OUT PER MT 54-UA2 1.25 INCHES LONG AND .21875 INCH DEEP. REPLACED NR 2 HEAT SHIELDS.SDR UALA2011121406871Strip · crackedNR 2 ENG AFT PYLON GAP STRIP NR 3 IS CRACKED. DRESSED OUT PER MT 54-UA2 2.65625 INCHES LONG AND .1875 INCH DEEP.SDR QXEA2011121601368Support Bracket · crackedRIGHT AFT LOWER NACELLE REFUEL/DEFUEL TUBE CRACKED SUPPORT BRACKET WHICH ATTACHES FUEL LINE TO UPPER HORIZONTAL WEB. REMOVED CRACKED FUEL LINE BRACKET IAW SRM 51-42--05-02-01. INSTALLED NEW BRACKET IAW SRM 51-42-05-02-01.SDR QXEA2011121601372Intercostal · crackedLEFT LOWER AFT NACELLE AFT EXHAUST FINGERNAIL SUPPORT INTERCOSTAL IS CRACKED. REMOVED CRACKED LT AFT EXHAUST FINGERNAIL SUPPORT INTERCOSTAL IAW SRM 51-42-05-02-01. MATCH DRILLED NEW EXHAUST CHANNEL TO ACFT IAW SRM 51-40-07-02-01. INSTALLED NEW EXHAUST CHANNSDR DALA1203001501Structure · unknownPYLON REWORKED IAW ERA 389665-14.SDR DALA1169941503Structure · damagedPYLON REWORK IAW ERA 389666-14.SDR UALA2011120606690Liner · delaminatedNR 2 ENGINE EXIT LINER SEGMENT AT 7 O'CLOCK POSITION HAS WIRE MESH DELAMINATED FROM THE LEADING EDGE IN 2 LOCATIONS. REMOVED EXIT LINER AT 7 O'CLOCK POSITION PER MM. INSTALLED NEW SECTION OF LINER AND APPLIED SEALANT.SDR UALA2011120606697Heat Shield · damagedNR 2 NACELLE AFT HEAT SHIELD DAMAGED FROM GAP STRIP. REMOVED HEAT SHIELD. HEAT SHIELD REPAIRED, REINSTALLED HEAT SHIELD IAW AMM.SDR UALA2011120506682Casting · damagedDAMAGED NR 2 PYLON PAN CASTINGS.SDR AALA20111203AFW08Bushing · migratedRIGHT PYLON MIDSPAR OUTBOARD LUG INBOARD BUSHING MIGRATED. REPLACED BUSHING PER EA B767-54-020452SDR A6WA201240083Seal · chafedLEFT LOWER COLW T/E SEAL CHAFED. REPAIRED LT LOWER NOSE COWL T/E SEAL IAW CMM 71-14-01, SUBTASK 71-14-01-110-013-A01.SDR UALA2011120206638Heat Shield · damagedHEATSHIELD DAMAGE AT NR 2 ENG. DEACTIVATED LEADING EDGE SLATS, IAW REF AMM27-81-00 PG 201. ACCOMPLISHED REACTIVATION.SDR AALA20111215TUL15Bushing · migratedRIGHT PYLON MIDSPAR OUTBOARD LUG OUTBOARD BUSHING MIGRATED. REPLACED BUSHING PER EA B767-54-020452.SDR AALA20111215TUL14Bushing · migratedLEFT PYLON INBOARD ATTACHMENT FITTING OUTBOARD LUG BUSHING MIGRATED. REPLACED BUSHING PER EA B767-54-020452.SDR AALA20111206AFW01Bushing · migratedLEFT PYLON INBOARD ATTACHMENT FITTING INBOARD LUG BUSHING MIGRATED. REPLACED BUSHING PER EA B767-54-020452.SDR AALA20111207AFW04Torque Box · crackedLEFT PYLON UPPER TORQUE BOX SKIN CRACKED OUTBOARD AFT SIDE WHERE INTEGRATED DRIVE GENERATOR FEEDER CABLES RUN THRU. INSTALLED REPAIR DOUBLER PER EA B767-54-020372.SDR A6WA201240035Angle · crackedRT PYLON PANEL 422BT AFT ANGLE CRACKED. REMOVED UNSERVICEABLE RT PYLON PANEL: 422BT AFT ANGLE AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06.SDR USAA2011113000002Rod · brokenFLIGHT 1465 - PHL-ATL - THE ENGINE PYLON FAIRING DID NOT STOW PROPERLY AFTER TAKEOFF. FLIGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BROKEN PYLON FAIRING ATTACH ROD. OPERATIONAL CHECK IS GOOD PER AMM 54-50-23. ALSO REMSDR NSVA2011313Attach Fitting · crackedRIGHT NACELLE PANEL 462BR ATTACH FRAME CRACKED. COMPLETED REPAIR IAW SAAB STATEMENT 340SDS023433 AND TD 340-54-11-36.
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