JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon 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 = '5400' 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 = '5400' 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 HNAA2022040400146None · noneE907563 - LH FWD ENGINE PYLON UPPER AFT JO-BOLT HOLE HAS INTERNAL DAMAGE....COMPLETE: REAMED LH FWD ENGINE PYLON UPPER
AFT JO-BOLT HOLE TO 1ST OVERSIZE TO REMOVE DAMAGE AND INSTALLED REPAIR BUSHINGS IAW EMBRAER SB-145-54-0008 FIGURE 2 AND PIEDMONT EO1-54-22-0SDR UIEA2022022600171Bracket · brokenENG #1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 9 HOURS(<P>THE CLAMP SUPPORT ROOD OF THE ACCESS 447BR PANEL WAS REPLACED</P>)SDR UIEA2022022600173Clamp · brokenRH. HYDRAULIC BAY, CLAMP TO STORE SUPPORT ROD OF THE ACCESS PANEL447BR IS BROKE.(<P>THE CLAMP OF THE SUPPORT OF ACCESS PANEL 447BR WAS REPLACED</P>)SDR IXXA2022030304Bracket · crackedCRACKED SEAL BRACKETSDR IXXA2022030303Fairing · crackedSKIRT FAIRING CRACKEDSDR IXXA2022030206Strip · crackedSTRIP CRACKEDSDR IXXA2022030205Channel · crackedPYLON PANEL 447DB HAS CRACKED CHANNELSDR IXXA2022030204Access Panel · tornPANEL 446CL SKIN IS TORNSDR UIEA2022022300165Access Panel · elongated#2 PYLON VALVE ACCESS PNL #462EL 1EA BOLT HOLE ELONGATED(<P>#2 PYLON VALVE ACCESS PNL #462EL 1EA ELONGATED BOLT HOLE AREA DOUBLER REPAIRED AS PER RI-54-50-15404 REV.A</P>)SDR UIEA2022022300166Access Panel · elongated#3 PYLON VALVE ACCESS PNL #472EL 2EA BOLT HOLES ELONGATED(<P>#3 PYLON VALVE ACCESS PNL #472EL 2EA ELONGATED BOLT HOLES AREA DOUBLER REPAIRED AS PER RI-54-50-15403 REV.A</P>)SDR UIEA2022022300167Access Panel · elongated#1 PYLON VALVE ACCESS PNL #452EL 1EA BOLT HOLE ELONGATED(<P>#1 PYLON VALVE ACCESS PNL #452EL 1EA ELONGATED BOLT HOLE AREA DOUBLER REPAIRED AS PER RI-54-50-15405 REV.A </P>)SDR CALA2022030100543Screw · missingPDA 3 ONE SCREW MISSING LH INBOARD PYLON PANEL 414AR, SCREW WAS REPLACED REPLACED MISSING SCREW.SDR FDEA202202280376Frame Angle · cracked#1 PYLON UPPER PANEL ATTACH ANGLE R/H APPROX NAC STA 150 IS CRACKED REMOVED AND REPLACED PER BOEING DWG #313N3100 REV DSDR IPXA2022040380793None · corrodedINSPECTION TYPE:C#2 PYLON IB SKIN INSIDE BETWEEN PNLS 443HL AND 443JL HAS CORROSIONREPAIRED SKIN PER UPS EO# B757-5430-83067-ASDR IXXA2022022601Mount Bracket · crackedPYLON PANEL HANGER CRACKEDSDR IXXA2022022504Web · damagedPYLON STIFFENER DAMAGED.SDR IXXA2022022502Attach Angle · crackedCORE COWL ATTACH ANGLE BROKENSDR IXXA2022022501Web · crackedPYLON PANEL CRACKED V-WEB.SDR IXXA2022022401Access Panel · damagedPYLON PANEL 441AT DAMAGEDSDR REXA2022032200446Stringer · corrodedSTRINGER 25R IS CORRODED BETWEEN FS280 AND FS 338. - REPAIRED STRINGER IAW ENDEAVOR AIR EA CRJ953-12914.SDR SWAA2022022876570Fitting · cracked#1 ENGINE. AFT STRUT FITTING LEFT SIDE IS CRACKED. / [01] R & R #1 ENG LH AFT STRUT FITTING PER SRM 51-40-02SDR FDEA202202230362Barrier · cracked#1 ENG PYLON TORQUE BOX OTBD SIDE AFT CLOSEOUT PANEL IS CRACKED. REPAIRED #1 ENGINE TORQUE BOX OUTBOARD SIDE AFT CLOSEOUT PANEL CRACKS IAW FED EX EA F-5450-T0367060: TITLE NACELLES/PYLON-WING PYLON/STRUT-#1 (LH) PYLON OUTB FLUID BARRIER STIFFENER CRACK REPSDR 9WGA2022022141201Tail Cone · departedCLIMBING THROUGH 4000 FEET AIRCRAFT HAD AN AIRFRAME VIBRATION. ENGINE PARAMETERS WERE INDICATING NORMAL. AT ARRIVAL MAINTENANCE REPS IDENTIFIED #2 ENGINE MAINTENANCE PLATFORM DOORS DAMAGED. REMOVED TAIL CONE REFERENCE MD-11 AMM 53-52-00. REPLACED DAMAGED TAILSDR FDEA202202210346Rub Strip · cracked#2 PYLON HYDRO BAY DOOR OPENING AFT STRIKER PLATE IS CRACKED REMOVED AND REPLACED PER BAC DWG # 313N3053 REV ESDR MASA20220218111None · noneTHE L/H WING LEADING EDGE SLAT NO. 3 TRAILING EDGE WEDGE WAS FOUND WITH WEAR DAMAGE AT SS407.75. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-13-02 TABLE 1SDR FDEA202202160305None · cracked#2 PYLON, AFT FAIRING ASSY, NAC STA 377 FRAME, OUTBD ATTACH CLIP IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 313T1380, SHEET 3, REVISION CSDR ASAA2022021537741Fitting · crackedWHILE ACCOMPLISHING TC 545400-01-1-VAM LH UPPER SPAR.C001, FOUND OUTBD CORNER FITTING CRACKED AREA 6. GROUNDED - YES. REMOVED AND REPLACED OUTBD CORNER FITTING ON LH PYLON AFT FIXED FAIRING UPPER SPAR RIB 15. ALL WORK ACCOMPLISHED PER TC 545400-01-1-VAM. LH RESDR ASAA2022021537740Fitting · crackedDURING TC 545400-01-1-VAM RH UPPER SPAR FOUND 3 CRACKS IN AREA 4 AND 1 CRACK IN AREA 6 OUTBOARD CORNER FITTING REF STEP 20 & 21 GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON RH PYLON AFT FIXED UPPER SPAR BETWEEN RIB 14-15 PER TC 545400-01-1-VAM RH REPAIRS.SDR SWAA2022032171942Plate · broken#1 ENGINE I/B STRUT THUMBNAIL PANEL 431AR SEAL PLATE BROKEN. (18-032) / [01] REMOVED AND REPLACED SEAL PLATE ON #1 ENGINE I/B STRUT THUMBNAIL PANEL 431AR I.A.W. B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR SWAA2022032171943None · broken#1 ENGINE O/B STRUT THUMBNAIL 431AL PANEL SEAL PLATE BROKEN. (18-031) / [01] REMOVED AND REPLACED SEAL PLATE ON #1 ENGINE O/B STRUT THUMBNAIL 431AL PANEL I.A.W SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR IXXA2022021105Shim · faultySHIM FABRICATIONSDR IXXA2022021104Bracket · crackedBRACKET CRACKEDSDR IXXA2022021102Beam · crackedBEAM CRACKEDSDR FDEA202202100998Stiffener · crackedNO.2 ENGINE PYLON, CRACK ON WEB SUPPORT ANGLE AT FWD END OF LOWER BOAT TAIL SEGMENT. (MARKED #5) REF JPF ITEMS 1 TO 11, REMOVED AND REPLACED BROKEN 1378M76P161A STIFFENER, REF SRM 54-51-71-01, AND GMM 07-0-1001 SEC. 7 (A) 2.CSDR IXXA2022021001Bracket · crackedPYLON BRACKET CRACKEDSDR SWAA2022032170842Seal Plate · cracked#2 ENGINE I/B THUMBNAIL PANEL 441AL SEAL PLATE CRACKED. (18-026) / [01] REMOVED AND REPLACED SEAL PLATE ON #2 ENGINE I/B THUMBNAIL PANEL 441AL I.A.W. B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR SWAA2022032170843Seal Plate · cracked#2 ENGINE O/B THUMBNAIL PANEL 441AR SEAL PLATE CRACKED. (18-025) / [01] REMOVED AND REPLACED #2ENGINE O/B THUMBNAIL PANEL 441 AR SEAL PLATE.;[02] CORRECTION STEP 1: REMOVED AND REPLACED SEAL PLATE #2 ENGINE O/B THUMBNAIL PANEL 441 AR I.A.W. B 737-700 SRM 51-40SDR IXXA2022030404None · crackedPANEL 446CR HAS LOWER CORNER OF PANEL BROKEN OFFSDR IXXA2022022403Rod · cracked#2 PYLON HYD BAY DOOR O/B HOLD OPEN ROD FOUND BROKENSDR IXXA2022022402Panel · chafed# 1 PYLON PANEL 437AL CHAFEDSDR FDEA202202050756Support Bracket · gougedNO.1 ENG PYLON, PYLON BRACKET LAND FOR PNLS 437EL AND 437AR HAS NUMEROUS AREAS OF DEEP GOUGES/GALLING ON TOP ARCH OF BRACKET. REMOVED WORN SUPPORT BRACKET AND REPLACED WITH FABRICATED BRACKET IAW DAC DWG AUB7564 AND REF SRM 51-31-01-0G.SDR DALA2022020700765None · noneSHIP 3267 ELONGATED HOLE FITTING (1 E/A) AND SHEETMETAL (LATERAL PLATE 1E/ A) MOVABLE FAIRING ON RH PYLON. CORRECTIVE ACTION: REPLACED FITTING (1 E/A) AND SHEETMETAL (LATERAL PLATE 1E/A) ON MOVABLE FAIRING RH PYLON AS PER A320 SRM 51-72-11. (2111769)SDR UIEA2022020200085None · noneCRACK ON LH STRUT OUTBD SKIN PANEL P/N 311T2450-23 BETWEEN NAC STA 221.25 / NAC STA 237.5 (CUTOUT FOR ACCESS PANEL 432AL)(<P ><SPAN>LH STRUT OUTBD SKIN PANEL P/N 311T2450-23 WAS REPAIRED PER BOEING SR 4-5340563504</SPAN></P> / <P> </P>)SDR FDEA202202030211None · cracked#1 PYLON, AFT FAIRING ASSY, NAC STA 377 FRAME HAS 2EA CRACKED BRACKETS REMOVED & REPLACED SUPPORT BRACKETS IAW B767 SRM 51-40-02, ALL PARTS VERIFIED PER AIPC 54-53-02-20ASDR FDEA202202030209Fairing · cracked#1 PYLON AFT LOWER HEAT SHIELD IS CRACKED REPAIRED PER FEDEX EA # F-5480-T0366361 P1.SDR FDEA202202030207Angle · cracked#1 PYLON AFT O/B LOWER PAN ATTACH ANGLE IS CRACKED REMOVED AND REPLACED PER BAC DWG # 313N5042 REV FSDR A6WA202202168104Bracket · noneNUMBER 1 ENGINE (ESN801422) NOSE COWL SUPPORT BRACKET IS LOOSE INBOARD SIDE OF ENGINE. ***AIRCRAFT REMOVED FROM SERVICE*** INTERIM REPAIR - VERIFIED NUMBER 1 ENGINE NOSE COWL SUPPORT BRACKET P/N 228-50082-145 HAS NOT CAUSED DAMAGE TO SURROUNDING STRUCTURE. SDR P5CA2022012600020None · none#4 PYLON VALVE ACCESS PNL #482EL 1EA HOLE FOUND ELONGATION(<P>#4 PYLON V/V ACCESS PNL #482EL FASTENER HOLE REPAIR</P>)SDR P5CA2022012600021None · none#4 ENG R/H CORE COWL EXHAUST LWR EDGE FOUND SEVERAL RIVET HOLES CRACKED.(<P>#4 ENG R/H CORE COWL PRECOOLER EXTERNAL DOUBLER REPAIR.</P>)SDR IXXA2022012902Door · wornIDG DOOR HINGES AND LATCHES WORN
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