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 DALA2020011300223Panel · worn(AIRCRAFT 670, L/P 1438903) #1 PYLON BULLNOSE PANEL WORN THROUGH AT PREVIOUS REPAIR. CORRECTIVE ACTION: REPAIRED PER ERA 450692-14AD.SDR DALA2020010900168Bushing · corrodedCORROSION LEVEL: 2 NO.1 PYLON UPPER LINK I/B BUSHING ON PYLON SIDE SHOWS SIGNS OF PITTING. REPLACED BUSHING. (LP 1436667)SDR SWIA2020030348975Splice Plate · corroded*LH ENGINE AFT PYLON UPPER AND LOWER SPLICE PLATES ARE CORRODED AS MARKED (C-CHECK) RO 2/28/2020 REPAIRED LH ENGINE AFT PYLON UPPER AND LOWER SPLICE PLATES THAT ARE CORRODED AS MARKED BY INSTALLING (4EACH) NEW REPLACEMENT BONDING PLATES PER BOMBARDIER RIL.SDR SWIA2020030348976Plate · corroded* RIGHT PYLON TRAILING EDGE UPPER BONDING PLATES ARE CORRODED. (C-CHECK) RO 2/28/2020 COMPLIED WITH BOMBARDIER RIL# 1166, REV. C, DATED 17-JUL-2007. REMOVED DAMAGED RH PYLON T/E UPPER BONDING PLATES 2EA, CLEANED AND INSTALLED BONDING PLATES 601-37012-33 (SDR IPXA2020012251217Bracket · brokenINSPECTION TYPE:3C, NR 3 ENG. PYLON O/B SIDE OF ENGINE MOUNT FRAME SUPPORT BRACKET IS BROKEN.REMOVED AND REPLACED BROKEN #3 ENG. O/B SIDE OF ENGINE MOUNT FRAME SUPPORT BRACKET IAW MD-11 SRM 54-05-41. (MINOR)SDR DALA2020010600062Structure · crackedTWO CRACKS AT AFT HOLES AT NSTA221.25 AT NO.1 NACELLE , ONE CRACK AT 3 O'CLOCK OF RH , THE OTHER CRACK AT 9 O'CLOCK OF LH , TWO CRACK HOLES REPAIRED AS PER PRI 583850-14AD REV O AND REV 1. PRI 583850-14AD REV0 AND REV1 COMPARED AND COMPLIED WITH ER/A 583850-14SDR DALA2020010300033Web · crackedNO.1 PYLON UPPER WEB WIRE CUTOUT FOUND CRACK (02EA) AT NAC STA 230. C/A NO.1 PYLON UPPER WEB , NAC STA 221.25 - 237.5 POWER FEEDER CABLE CUTOUT CRACK (02EA) REPAIRED AS PER PRI 583788-14 REV 0. PRI 583788-14 REV 0 COMPARED AND COMPLIED WITH ER/A 583788-14AD SESDR DALA2020010200006Web · crackedFOUND NO.2 PYLON UPPER WEB SKIN CRACK AT NAC STA 230 WIRE CUTOUT. C/A W NO.2 PYLON UPPER WEB SKIN , NAC STA 221.25 - 237.5 POWER FEEDER CABLE CUTOUT REPAIRED AS PER PRI 583724-14 REV 0. PRI 583724-14 REV 0 COMPARED AND COMPLIED WITH ER/A 583724-14AD REV ORIGINSDR ABXR2019123000343Stiffener · crackedNR 1 PYLON LOWER SKIRT FAIRING STIFFENER CRACKEDSDR ABXR2019123000342Beam · corrodedHYD BAY LOWER FRAME BEAM CRACKEDSDR DALA2020010407692Bushing · corrodedCORROSION LEVEL: 2 NO 1 PYLON UPPER LINK, O/B BUSHING ON UPPER MOUNT ON WING SIDE SHOW SIGNS OF PITTING. REPLACED BUSHING ON CWO 115958-0003. (LP 1420528)SDR DALA2020010407691Bushing · corrodedCORROSION LEVEL: 2 NO 1 PYLON, UPPER LINK I/B BUSHING ON WING SIDE SHOWS SIGNS OF PITTING. REPLACE BUSHINGS ON CWO 115958-0003. (LP1420523)SDR DALA2020010407690Bushing · corrodedCORROSION LEVEL: 2 NO.1 PYLON UPPER LINK O/B BUSHING ON PYLON SIDE SHOWS SIGNS OF PITTING REMOVED AND REPLACED BUSHING ON CWO 115959-0005. (LP 1420526)SDR DALA2020010407679Bushing · corrodedCORROSION LEVEL: 2 NO.1 PYLON FWD BUSHING ON UPPER LINK SHOWS SIGNS OF PITTING. REPLACED (LP1418700)SDR SWIA2019122647101Fairing · chafedL/H ENGINE AFT PYLON FAIRING- FRAME 1 CHAFED ON BOTH INBD SIDES. REMOVED AND REPLACED LT ENGINE AFT PYLON FAIRING IAW SRM.SDR SWAA2022032540479Fitting · crackedLEFT ENGINE TE AFT LOWER PYLON FAIRING EDGE FITTING ASSY IS CRACKED IN THE RADIUS. / R & R $1 ENGINE AFT LOWER PYLON FAIRING AFT WEDGE FITTING. REF AMM 51-40-02. NO DEFECTS NOTED AT THIS TIME. SEE SA=M 326 #A948339 ATTACHEDSDR SWIA2020020348140Plate · corroded*RH ENGINE PYLON TRAILING EDGE BOTTOM INBD REINFORCEMENT TAB CORRODED (MARKED) (C-CHECK) RO:1/29/2020REMOVED AND REPLACED WITH NEW BONDING PLATE ( 1 ) ONE PN # 601-37012-33, COMPLIED WITH ALL STEPS 1 THRU 7 AND BOMBARDIER RIL.SDR FDEA2019120653185Bracket · chafed#2 PYLON IB BRACKET AT RIB 20 IS CHAFED THROUGH MATERIAL ACCOMPLISHED REPAIR AT #2 PYLON INBOARD AFT UPPER SPAR WEB IAW FEDEX EA: 6-5450- T0350874 T0350874-P1. TITLED: NACELLES/PYLON - WING PYLON/STRUT - NO. 2 PYLON INBOARD AFT UPPER SPAR WEB.SDR SWAA2022041100025Panel · delaminatedRIGHT # 2 ENGINE PYLON PANEL 444BR CORNER DELAMINATED / REMOVED AND REPLACED PANEL IN REF TO SOPM 20-50-01SDR S9BA20191203002Angle · crackedCRACK AT R/H NACELLE ANGLE NS 197SDR SWAA2022032551788Bracket · crackedUPON REMOVAL OF ACCESS PANEL 443BT FOUND CENTER NUT PLATE AND BRACKET CRACKED / REMOVED AND REPLACED ACCESS PANEL 443BT REF AMM 54-53-01. INSPECTOR H53SDR SWAA2022032499419Panel · crackedCRACK BLADE ACCESS PANEL 431AL AT LT PYLON (1 EA) / REPLACED BLADE ACCESS PANEL 431AL AT LT PYLON (1EA) IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 (U078)SDR SWAA2022032452645Door · cracked#2 ENGINE; VERIFY CRACK FREE CONDITION OF OIL ACCESS DOOR AT UPPER FWD CORNER OF UPPER LATCH CUTOUT / REMOVED #2 ENGINE OIL ACCESS DOOR IAW AMM 71-11-05-000-801-F00 STEP 2. INSTALLED SERVICEABLE #2 ENGINE OIL ACCESS DOOR IAW AMM 71-11-05-400-801-F00 STEP 3. RESDR ABXA201912104194Angle · corrodedCORROSION IN THE LEFT PYLON FAIRING PANEL 437BL BONDING WIRE ATTACH POINT (ANGLE). THE ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104193Stiffener · crackedCRACK IN THE LEFT PYLON FAIRING INBOARD STIFFENER. THE STIFFENER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104192Retainer · crackedCRACK IN THE LEFT PYLON PANEL 437BR AFT SEAL RETAINER. THE SEAL RETAINER WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104191Angle · corrodedCORROSION IN THE LEFT PYLON PANEL 437BR CUT-OUT, INNER AFT SUPPORT ANGLE. THE SUPPORT ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104190Frame · corrodedCORROSION IN THE LEFT PYLON FAIRING, INBOARD FRAME, AT PYLON STATION 376. THE FRAME WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104189Stiffener · crackedCRACK IN THE LEFT PYLON, INBOARD AFT FAIRING, INBOARD STIFFENER. THE STIFFENER WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104188Web · crackedCRACK IN THE RIGHT PYLON, UNDER PANEL 437BR, AFT SUPPORT WEB. THE WEB WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104187Angle · crackedCRACK IN THE RIGHT PYLON INBOARD AFT FAIRING SUPPORT ANGLE. THE FAIRING SUPPORT ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104182Plate · corrodedCORROSION IN THE RIGHT PYLON, UNDER PANEL 437BR, AFT SIDE UPPER CUT-OUT INNER SUPPORT PLATE. THE SUPPORT PLATE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104181Angle · crackedCRACK IN THE RIGHT PYLON PANEL 437BR CUT-OUT, INNER AFT SUPPORT ANGLE. THE SUPPORT ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104180Retainer · crackedCRACK IN THE LEFT PYLON HYDRAULIC BAY CUT OUT LOWER ZEE ANGLE SEAL RETAINER. THE ZEE ANGLE SEAL RETAINER WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR SWAA2022032434323Web · cracked#1 ENGINE INBOARD FAN COWL VERTICAL WEB AFT OF OIL SERVICE DOOR IS CRACKED AT UPPER END / REMOVED WEB SHEILD AT #1 ENG I/B FAN COWL VERTICAL WEB AFT OF OIL SERVICE DOOR I.A.W SRM 51-40-02-0G-0. DRILLED NEW WEB SHIELD I.A.W SRM 51-40-05-0G-0 AND CMM 71-13-30. ISDR FDEA201901300240Bracket · worn#1 ENGINE: RIGHT SIDE OF PYLON INSIDE ACCESS PANEL 438DR, PNEUMATIC DUCT SUPPORT. LOWER BRACKET HAS LOOSE ATTACH SCREWS/ELONGATED HOLES BRACKET REPAIR COMPLIED WITH I.A.W. E.A. 1-5450-T0351554 PT, REF JPF STEP ITEM 12. TITLE: NACELLES/PYLON - WING PYLON/STSDR DALA2019111806737Stiffener · crackedNUM 2 ENG NOSE COWL EXTERNAL AFT STIFFENER CRACKED AT 07:00 MKD INTERNAL FWD BULHHEAD STIFFENER CRACKED 206:00 MKD INTERNAL STIFFENER FASTENERS LOOSE AT 07:00 MKD. NUM 2 ENG NOSE COWL REPL AND INST ON AMDS CARD 7100-4682-RH COWL, NOSE, LT OFF 88-7110-9-0001 S/SDR IPXA2019111859042Angle · crackedINSPECTION TYPE:A300#2 PYLON AFT FAIRING FWD END RH SIDE FWD CORNER ANGLE PLATE CRACKEDREMOVED AND REPLACED IAW SRM 51-40-02SDR FDEA202001030006Support Bracket · worn#1 PYLON UPR PNL SUPPORT BRACKET BETWEEN PNLS 437CL AND 437DL WORN FROM PNL CHAFING. REPLACED BRACKET PER DWG AUB7564-29 AND SRM 51-31-01-0G.SDR DALA2019111296582Angle · crackedCLOSE OUT ANGLE CRACKED AT INBD UPPER AREA IN PYLON AS SEEN THROUGH PANEL 436AL. REPLACED PYLON CLOSE OUT ANGLE (LP 1351374)SDR IPXA2019111549013Angle · crackedINSPECTION TYPE:C1#1 PYLON AFT FAIRING FWD END RH SIDE HAVE CRACKED ANGLEREMOVED AND REPLACED IAW SRM 51-40-2SDR SWAA2022040666395Fitting · corrodedRH ENGINE STRUT AFT FAIRING (PN 313-2060-928; SN 889301001) FRAME LATERAL RESTRAINT FITTING INSTALLATION IS CORRODED AT NAC STA 283; NAC LBL 4; NAC WL 122. / REMOVED CORROSION ON R/H ENGINE STRUT AFT FAIRING FRAME INTERNAL RESTRAINT FITTING IAW B 737 SRM 51-10SDR SWAA2022040566393Panel · corrodedRIGHT PYLON PANEL 441EL LOWER INTERNAL MATING SURFACE HAS AREA OF CORROSION / REMOVED CORROSION FROM RT PYLON PANEL 441EL IAW SRM 51-10-02-0G-0. ORIGINAL 'T' .110' AND .170'; REMAINING 'T' .107' AND .152' LOSS OF .003' AND .018'. REPAIRED PANEL IAW EA 190911 RSDR IPXA2019112049204Bracket · crackedINSPECTION TYPE:2C#3 PYLON WIRE BRIDGE WEB "L" ANGLE IS CRACKED AT TOP, FWD. OF PRECOOLER.REMOVED AND REPLACED BRACKET IAW SRM 54-01-42. (MINOR)SDR CALA2019110501920Seal · crackedPDA 2 RIGHT ENG INBD T-R TO PYLON FLEX SEAL (SECOND FROM AFT) IS CRACKED AND MISSING SEGMENT. PARTS UPDATE IPC 54-57-22-07A REMOVED AND REPLACED FLEX SEAL - REF ECRA 5450-02357 REV-B.SDR HNAA2019110600347Yoke · crackedRH PYLON FWD LWR YOKE FIXTURE HAS POSSIBLE CRACK....FIX: REMOVED AND REPLACED RH PYLON FWD LWR YOKE IAW PIEDMONT EO1-54-19-0495. NOTE: A/C IN ABI HVY CHECKSDR ABXA2019103126164Web · corrodedCORROSION ON THE UPPER SURFACE OF THE LEFT PYLON FORWARD UPPER SPAR WEB APPROXIMATELY AT NACELLE STATION 227. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR IPXA2019110848768Web · crackedINSPECTION TYPE:12YR#1 PYLON RIB 8 WEB LT SIDE IS CRACKED.REPAIRED CRACKED #1 PYLON RIB 8 WEB AT LT SIDE IAW UPS EO A300-5450-51643-A. (MINOR)SDR IPXA2019110848772Web · crackedINSPECTION TYPE:12YR#2 PYLON RIB 8A WEB IS CRACKED AT R/H CORNER.REPAIRED CRACKED #2 PYLON RIB 8A WEB AT R/H CORNER IAW UPS EO A300-5450-51643-A. (MINOR)SDR SWAA2022032358559Panel · cracked#1 ENGINE O/B T/R LOWER PANEL AROUND LATCHES IS BROKEN AT FWD LATCH AT SCREW HOLE / REMOVED AND REPLACED #1 O/B T/R LATCH BEAM FAIRING REF CMM 78-31-37; AND SRM 51-40-02. PREPARED AND PAINTED REF AMM 51-21-99.
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