JASC 5420
Service difficulty reports · 3,948
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 2015FA0000153Angle · crackedDURING ENGINE REMOVAL FOR HSI AN INSPECTION OF THE NACELLE AREA WAS CONDUCTED PER THE OEM, WE NOTICED BOTH LEFT AND RIGHT ENGINE FRONT NACELLE HORSE COLLAR LOWER LEFT AND RIGHT ANGEL 20MM AND 22MM CRACKED AT THE BEND RADIUS HORIZONTALITY, THE REPAIR WAS MADE SDR ASOA20150312068Fitting · crackedDURING C-CK. NR 2 ENGINE FWD LOWER YOKE CRACKED. R & R NR 2 ENG FWD LOWER YOKE IAW EC5450-01070. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2015FA0000152Angle · crackedDURING ENGINE CHANGE AND INSPECTION OF THE NACELLE AREA NOTICED A ONE INCH CRACK ON THE HORSE COLLAR BOTTOM LEFT SIDE AT THE OUTER ANGEL OF THE ENGINE NACELLE HORSE COLLAR ASSY THE CRACK RAN AT THE ANGLE BEND HORIZONTALITY, THE REPAIR WAS MADE IAW DRAWING RIGHSDR SWAA2015101244833Panel · crackedRIGHT WING PYLON, UPPER PANEL JUST AFT OF NR 58710R, CRACKED AT AFT INBD SIDE CUT OUT. REPAIRED PYLON IAW EA.SDR REXA2015022200263Structure · damagedNUMBER 2 ENG HINGE LINE FAIRING 443BB CHAFED & CRACKED AROUND FASTENER HOLE. LOCATED, DRILLED & INSTALLED PARTS ON NEW FAIRING IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-40-11-001-001-A01. RESTORED TOPCOAT IAW SRM 51-25-16-001-001-A01.SDR DALA2015022101632Web · corrodedDURING INSPECTION, FOUND CORROSION ON VERTICAL WEB OF RT MOVABLE FAIRING. REPLACED VERTICAL WEB ON RT MOVABLE FAIRING IAW SRM 51-72-11 AND 51-42-11 AND DWG D545-30391.SDR DALA2015022101631Web · corrodedDURING INSPECTION, FOUND CORROSION ON VERTICAL WEB OF THE LT MOVABLE FAIRING. REPLACED VERTICAL WEB OF THE LT MOVABLE FAIRING IAW SRM 51-72-11 AND 51-42-11 AND DWG D545-30391.SDR UIEA2015021900136Panel · wornPYLON 4 482EL PANEL BOLT HOLE WORN. ACCOMPLISHED EI NO T2015A54B-230 REV O. JOB COMPLETED & CONDITION CHECKED NORMAL.SDR UIEA2015021900135Panel · wornPYLON 2 462EL PANEL BOLT HOLE WORN. ACCOMPLISHED T2015A54B-233 REV O. JOB COMPLETED & CONDITION CHECKED NORMAL .SDR AALA20150210006Stiffener · crackedFOUND DIAGONAL STIFFENER CRACKED ON THE NR 2 PYLON JUST FWD OF THE MID SPAR BULKHEAD. R & R STIFFENER IAW AARD 51-00-05-1 & DWG 311T2400.SDR DALA2015020901093Angle · crackedCRACK ON ACCESS PANEL ANGLE. ANGLE WAS REPLACED IAW DWG 9935747, REV SRM 51-10-3, PAR 21-14, SRM 51-30-2.SDR REXA2015020700222Bracket · brokenTASK CARD 192 RT ENG CORE COWL CHAFED AT OVERLAP, ALIGNMENT BRACKET BROKEN. REPAIRED RT ENG CORE COWL CHAFE IAW SRM 54-13-00-201-005-A01. REPAIRED ALIGNMENT BLOCK IAW SRM 54-13-00-201-002-A01.SDR REXA2015020700221Block · chafedTASK CARD 192 LT ENG CORE COWL ALIGNMENT BLOCK WORN, CHAFED AT 3 O' CLOCK. REPAIRED LT ENG CORE COWL ALIGNMENT BLOCK IAW SRM 54-13-00-201-002-A01. REPAIRED CHAFE AT 3 O'CLOCK POSITION IAW SRM 54-13-00-201-005-A01.SDR UIEA2015020800092Structure · wornNUMBER 1 PYLON 452EL ONE EACH INDICATOR HOLE FOUND WORN. REPAIRED IAW R1-54-00- 10805 REV A.SDR UIEA2015020800093Structure · wornNUMBER 3 PYLON 472ER TWO EACH INDICATOR HOLE FOUND WORN. REPAIRED IAW R1-54-00-10805 REV A.SDR UIEA2015020800094Structure · wornNUMBER 4 PYLON 482EL TWO EACH INDICATOR HOLE FOUND WORN. REPAIRED IAW R1-54-00-10805 REV A.SDR UIEA2015020900104Structure · damagedNUMBER 3 ENG RT CORE COWL UPPER AFT EDGE DEFORMED. REPAIRED IAW SRM 54-45-0-2R-7.SDR REXA2015020500212Stiffener · chafedTASK CARD 900-54-440-300 HINGE LINE FAIRING 433BB HAS CHAFE ON END & POSSIBLE CRACK AT LAST HOLE. HINGE LINE FAIRING PNL 433BB DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 54-12-01-101-001-A01. MATCH DRILLED & INSTALLED STIFFENER & ATTACH POINTS IAW 51-42-06-001SDR QXEA2015021100067Stiffener · crackedFOUND CRACKED STIFFENER ON LT COWL PANEL 414AR. R & R THE STIFFENER IAW SRM 51-42-05, REPAIR-01.SDR FDEA201502050444Support Beam · chafedNUMBER 2 PYLON FAN COWL SUPPORT BEAM OTBD RAIL AT NACELLE STATION 75 LOWER SURFACE FOUND CHAFED. REPAIRED IAW EA F-5450-T0315243 PT 1. RAIL GOUGE BLENDED OUT REPAIR. REPAIR CLASSIFIED AS MINOR.SDR REXA2015020400210Rub Strip · wornTASK CARD 900-54-440-301 RT ENG FWD CORE COWL, UPPER & LOWER AFT RUB STRIPS WORN. REPLACED RT ENG CORE COWL LOWER WORN RUB STRIP SECTION IAW SRM 54-23-00-201-007-A01. UPPER RUB STRIP FOUND TO BE WITHIN LIMITS IAW SRM 54-23-00-101-001-A01, THICKNESS STILL REMASDR REXA2015020400207Rub Strip · wornTASK CARD 900-54-430-301 LT ENG UPPER & LOWER FWD CORE COWLS AFT RUB STRIPS WORN. REPLACED LT ENG UPPER & LOWER WORN SECTION OF AFT RUB STRIPS IAW SRM 54-23-00-201-007-A01.SDR DALA2015020100808Retainer · crackedCRACKED PYLON T/E RT RETAINER. THE RETAINER WAS REPLACED IAW SRM 54-31-0, FIG 2B AND 51-30-1.SDR SWAA2015021036434Support Angle · crackedRIGHT PYLON SUPPORT ANGLE CRACKED AT WBL 198.6. R & R ANGLE IAW SRM & DWG.SDR CALA2015013093035Structure · crackedNUMBER 1 PYLON CUT OUT 452ER CRACKED AT LOWER AFT CORNER. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5450-02294.SDR R61A201501280070Stiffener · crackedDURING HEAVY CHECK, LT PYLON BEHIND FRAME 1 IS CRACKED. MX R & R LT PYLON BEHIND FRAME 1 STIFFENER.SDR DALA2015012700660Angle · wornNR 1 PYLON AFT END, AFT OF MOUNT LUGS ANGLE HAS WORN. REMOVED DAMAGE AND LOCATED AND DRILLED NEW ANGLE AND INSTALLED IAW DWG 3313N3052 AND SRM.SDR HYIA20150126001Beam · crackedDURING SCHEDULED INSPECTION EVENT, THE RT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED AT AREA EXTENDING FWD & LWR OF OTBD PORTION OF AFT MOUNT BEAM OVERLAYS. A SUPPLEMENT TO THIS SDR WILL BE SUBMITTED TO ILLUSTRATE DAMAGE POINT. CORRECTIVE ACTION WILL BE CSDR SWAA2015022536896Support Angle · crackedRIGHT PYLON OTBD STRUT FAIRING SUPPORT ANGLE CRACKED AT STATION 278. R & R ANGLE IAW SRM & DWG.SDR REXA2015012300092Mount Bracket · brokenTASK CARD CRJ900-C1 PYLON PANEL 443BT 2ND FROM AFT MOUNTING BRACKET BROKE. R & R BROKEN MOUNTING BRACKET IAW SRM 51-42-06-001-001-A01.SDR REXA2015012300091Panel · crackedTASK CARD CRJ900-C1 PYLON PANEL 433BB PANEL CRACKED AT FASTENER HOLE. R & R PANEL 433BB IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01 & 51-25-01-001-001-A01 STEP 7 E.SDR REXA2015012200087Retainer · damagedTASK CARD CRJ900-C1 PYLON PANEL 433BT POSSIBLE CRACK AT FASTENER HOLE, GOUGED & CHAFING ON SEAL RETAINER. RECEIVED NEW PANEL 433BT FROM STOCK, PREPARED HOLES & TRANSFERRED PARTS IAW SRM 51-42-06-001-001-A01 & SRM 51-40-11-001-001-A01. APPLIED PAINT TO PANEL SDR AALA20150120012Stiffener · crackedLEFT PYLON OTBD VERTICAL STIFFENER & UPPER ATTACH ANGLE CRACKED FWD OF OTBD MIDSPAR FITTING. INSTALLED NEW LT PYLON OTBD STIFFENER & UPPER ANGLE IAW SRM 51-10-02 & AARD 51-00-05.SDR AALA20150119012Stiffener · crackedLEFT PYLON OTBD HORIZONTAL STIFFENER CRACKED. R & R STIFFENER IAW SRM 51-10-02-0G & DWG 311T2400.SDR QXEA2015010901140Stiffener · chafedOTBD AFT UPPER COWL 424AR WITH WORN AND CHAFED THRU ON AFT RIB. REMOVED AND REPLACED IAW SRM 51-42-05, AND SRM 51-42-05.SDR KCSA201412311098Intercostal · damagedNR 4 PYLON LOWER WEB INTERCOSTAL AT NAC STA 216 IS DAMAGED.SDR DALA2014122006941Vapor Barrier · damagedLT STRUT VAPOR BARRIER WEB FOUND NINE .2187" OVERSIZED TO .2500" HOLES. REPAIRED IAW ERA 53065-14AD.SDR REXA2014121901223Pan · chafedLT ENGINE VENT PAN IS CHAFED LOWER COWL. MECH REPAIRED LT ENGINE VENT PAN IAW EO R54090.SDR FDEA201412170408Attach Fitting · gougedRIGHT PYLON TO ENG FWD ATTACH FITTING, INBD LOWER ARM, LOWER CORNER HAS GOUGE, JUST BELOW FEEDER LINES. ACCOMPLISHED FINAL EA 6-5440-T0315003 REV NR PS P1 CLASSIFIED AS MAJOR REPAIR. REPAIR LIFE LIMITATION 6 MONTHS IAW RDAS 80018687 003 2015 ISSUE A.SDR REXA2014121701217Pan · damagedNR 2 ENGINE AFT CORE COWL INSULATING PAD CRACKED AND STANDOFF BLOCK ALIGNMENT TAB DAMAGED AT 9 O'CLOCK POSITION. MECH R & R STAND OFF BLOCK AND INSULATING PAD AT NR 2 ENG AFT CORE COWL AT 9 O'CLOCK POSITION IAW SRM 54-13-00-201-002-A01.SDR CA141216003Support · mismanufactured(CAN) A STRUCTURES TECH WAS REPLACING DAMAGED PART WITH A NEW BELL SUPPLIED PART ND NOTICED THE PART IS SMALLER THAN THE ORIGINAL FOUND INSTALLED AND DID NOT HAVE SUFFICIENT EDGE DISTANCE FOR FASTENERS.SDR LR7A2014121600505Plenum · crackedDURING SCHEDULED B-3 CHECK, UNDER JOB CARD HB5701, FOUND NR4 ENGINE'S LOWER AFT NACELLE PLENUM HAD CRACKED ON THE INBD SIDE; FS536, PPWL0 TO PPWL-6, PPBL8.4L TO PPBL12.5L. REPAIRED IAW MEA 382-54-14-042.SDR SWAA2015011235641Support Angle · crackedLEFT PYLON NACELLE SUPPORT ANGLE CRACKED ON NACELLE STRUT INBD SIDE AT STATION 277.24. R & R ANGLE IAW SRM & DWG.SDR QXEA2014121001019Stiffener · crackedINBD COWL PANEL 414AR HAS A CRACKED STIFFENER AT BS 273.5. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-05, STEP 4.E AND SRM 51-42-05, PG.204-205, PROCEDURE D, STEPS 1-10.SDR REXA2014120701171Bracket · brokenTASK CARD C1 NR 2 ENG UPPER HINGE LINE FAIRING BRACKET ON PYLON TIE BAR IS BROKEN.
REMOVED BRACKET IAW SRM 51-42-21-001-001-A01. FABRICATED NEW BRACKET IAW SRM 51-24-21-001-001-A01. INSTALLED NEW BRACKET IAW SRM 51-42-21-001-001-A01.SDR ASOA2014122311948Bushing · unknownCONNECTOR, PN CN622-008-007, FAN COWL FWD K BAR FOR N146PQ, LT ENGINE, RV 161789. LT CONNECTOR APPROVED. R & R BUSHINGS IN LT ENGINE K-BAR IAW REO 670-54-22-002. C/W EC/TC FOR INSTALLATION OF BUSHINGS IN ENGINE K-BAR IAW REO 670-54-22-002. THIS REPAIR IS CSDR FDEA201412034045Doubler · chafedEXISTING REPAIR FINDINGS, THERE ARE CHAFING MARKS ON THE EXISTING REPAIR DOUBLER AT NR 2 PYLON OTBD SIDE, RT OF THE FAN COWL SUPPORT WEB AFT SIDE AT NAC STATION 102. DAMAGED REPAIR DOUBLER REMOVED & NEW REPAIR CARRIED OUT IAW SRM 54-51-02 FIG 201 REPAIR 1 REVSDR FDEA201411273916Web · chafedCHAFES ON THE REPAIR DOUBLER AT NR 1 PYLON INBD SIDE, RT OF THE FAN COWL SUPPORT WEB, AFT SIDE AT NAC STATION 102. REPAIRED IAW SRM 54-51- 02 FIG 201 REPAIR 1 REV 113. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201411273915Web · chafedTHERE ARE CHAFING MARKS ON THE EXISTING REPAIR DOUBLER AT NR 2 PYLON INBD SIDE, LEFT OF THE FAN COWL SUPPORT WEB AFT SIDE AT NAC STATION 102. REPAIRED IAW EA F-5450-T0314118 P 1. TITLE, NACELLES & PYLON, WING PYLON & STRUT, RT STRUT FAN COWL SUPPORT BEAM ASSSDR FDEA201411273914Skate Angle · crackedNUMBER 2 PYLON AFT FAIRING OTBD AFT SKATE ANGLE, WING SIDE, TE CRACKED. REPLACED BY FABRICATION & INSTALLATION IAW DWG 112N4601 SHT 02 REV C EA F-5400-T0315070 PT 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
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