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.

SDR FDEA201010013857Fitting · chafedINSIDE NR 2 PRECOOLER COMPARTMENT, RIGHT SIDE FRAME SUPPORTS CHAFED. BLENDED FRAME SUPPORTS PER SRM 54-20-00 AND E.A. 8-5450-142268. CLASSIFIED AS A MAJOR REPAIR.Oct 1, 2010 · N359FE · Doug MD1010FSDR IPXA10563193Support Angle · chafedINSPECTION TYPE:C4, NR2 ENG FAN CASE DIAPHRAGM AFT SUPPORT ANGLE IS CHAFED FROM CONTACT WITH TR COWL AT 5 O'CLOCK POSITION. R & R SUPPORT ANGLE IAW RREM 72-34-11-300-001.Sep 30, 2010 · N453UP · Boeing 75724APFSDR IPXA10563192Support Angle · chafedINSPECTION TYPE:C4, NR 2 ENG AFT FAN CASE DIAPHRAM FWD SUPPORT ANGLE IS CHAFED FROM CONTACT WITH FAN COWL AT 4-5 O'CLOCK POSITION. R & R SUPPORT ANGLE IAW RREM 72-34-11-300-001.Sep 30, 2010 · N453UP · Boeing 75724APFSDR ZZDA2010461Structure · crackedLEFT PYLON APRON LOWER NR 4 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 4 HINGE CUTOUT AREA DOUBLER REPAIR PER TRA 17-54-TR00129.Sep 27, 2010 · N956AT · Boeing 717200SDR ABXR201009250045Fitting · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD. UPPER SPLICE FITTING CORRODED. R & R NR2 PYLON FWD UPPER SPLICE FITTING IAW AMM.Sep 25, 2010 · N934AX · Doug DC933FSDR ABXR201009250044Fitting · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD LOWER SPLICE FITTING CORRODED. R & R SPLICE FITTING IAW SRM.Sep 25, 2010 · N934AX · Doug DC933FSDR FDEA201009243705Stiffener · crackedNR 1 ENGINE NOSE COWL EXTERIOR AFT BACKSIDE BULKHEAD I/B AT 5 O'CLOCK POSITION VERTICAL ANGLE STIFFENER SUPPORT IS CRACKED AT TOP END REMOVED VERTICAL STIFFENER NR 1 ENG NOSE COWL AFT AT 5 O'CLOCK BULKHEAD IAW SRM REV 103 51-30-2 FABRICATED NEW STIFFENER FROMSep 24, 2010 · N204FE · Boeing 7272S2FSDR DALA1024431503Angle · crackedFOUND CLOSEOUT ANGLE CRACKED WHILE CONDUCTING INSP IAW 1T204. CONDUCTED HFEC INSP OF BOLT HOLES IAW EA 01-074944-12ADME04. NO FURTHER DAMAGE NOTED. REPLACED CLOSEOUT ANGLE IAW DWG 311T2150.Sep 21, 2010 · N153DL · Boeing 7673P6SDR DALA1024420184Angle · crackedFOUND CLOSEOUT ANGLE ON NR 2 PYLON CRACKED WHILE CONDUCTING INSP IAW 1T204. CONDUCTED HFEC INSP OF BOLTS IAW EA 01-074944-12ADME04 AND ERA 485953-14AD. NO FURTHER DAMAGE NOTED. REPLACED CLOSEOUT ANGLE IAW DWG 311T3150.Sep 21, 2010 · N184DN · Boeing 767332SDR KCSA101127Stiffener · crackedNR 4 PYLON O/B UPPER STIFFENER CRACKED AT APPROX NAC STA 130.Sep 20, 2010 · N700CK · Boeing 747246BSDR IXXA10SMN083SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND NR 4 PYLON TEE DOUBLER HORIZ FLANGE CRACKED IN UPPER INTERNAL PART AT STA YN 335.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED SPACER.Sep 15, 2010 · N606AL · Doug DC873FSDR C2XA10SH300Support Fitting · crackedSHV - DURING C-CHECK ANGLE SUPPORT CLIP CRACKED IN PYLON AT FRAME 73 STRINGER 8R. MAINTENANCE REMOVED AND INSTALLED NEW FABRICATED ANGLE SUPPORT CLIP IN PYLON AT FRAME 72-74 STRINGER 8R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSep 15, 2010 · N14974 · Emb EMB145LRSDR C2XA10SH299Support Fitting · crackedSHV - DURING C-CHECK ANGLE SUPPORT CLIP CRACKED IN PYLON FRAME 73 STRINGER 8L. MAINTENANCE REMOVED AND FABRICATED NEW ANGLE SUPPORT CLIP IN PYLON AT FRAME 72-73 STRINGER 8L. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 15, 2010 · N14974 · Emb EMB145LRSDR ZZDA2010421Structure · crackedRIGHT PYLON APRON LOWER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.Sep 14, 2010 · N955AT · Boeing 717200SDR ZZDA2010419Structure · crackedRIGHT PYLON APRON LOWER 2ND HINGE CUTOUT, CRACKED. ACCOMPLISHED HINGE CUTOUT DOUBLER REPAIR PER B717 SRM 54-50-02 FIG 203 REP 1.Sep 14, 2010 · N955AT · Boeing 717200SDR ZZDA2010418Structure · crackedLEFT PYLON APRON UPPER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.Sep 14, 2010 · N955AT · Boeing 717200SDR FDEA201009133364Support · wornNR 1 PYLON, TOP SUPPORT FAIRING, PN 313N5004-29, METAL IS WORN. WORN SUPPORT AT NR 1 PYLON FAIRING. R & R IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 13, 2010 · N935FD · Boeing 7572T7SDR FDEA201009133361Angle · crackedNR 2 PYLON AFT FAIRING FWD BULKHEAD HAS CRACK AND CHAFF MARK OTBD SIDE. CRACKED ANGLE ON NR2 PYLON AFT FAIRING R & R IAW SRM 51-40-02, REV 100.Sep 13, 2010 · N935FD · Boeing 7572T7SDR FDEA201009123351Support · corrodedNR 2 PYLON PANEL SUPPORT STRIP HAS FRETTING CORROSION. CORRODED NR2 PYLON PANEL SUPPORT R & R IAW DWG 313N5004, SHT 1, REV D. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 12, 2010 · N935FD · Boeing 7572T7SDR IPXA10562797Fairing · delaminatedINSPECTION TYPE:C3, PYLON PANEL 441AT AFT EDGE IS DELAMINATED. REPAIRED DELAMINATED EDGE ON PYLON PANEL IAW SRM 54-51-70-1A-1.Sep 5, 2010 · N425UP · Boeing 75724APFSDR IPXA10562397Support Angle · crackedINSPECTION TYPE:C3, NR 1 PYLON AFT FAIRING SUPPORT ANGLE OTBD END IS CRACKED IN RADIUS AT NAC STA 204. REPLACED IAW SRM 51-40-02, SRM 54-52-01-4, SRM 51-40-05.Sep 2, 2010 · N425UP · Boeing 75724APFSDR IPXA10562395Support Angle · crackedINSPECTION TYPE:C3, NR1 PYLON AFT FAIRING FWD INBD SUPPORT ANGLE IS CRACKED AT NAC STA 206 FWD END OF PNL 435AR CUTOUT. REPLACED IAW SRM 51-40-02.Sep 2, 2010 · N425UP · Boeing 75724APFSDR DALA1021005811Support Angle · crackedLT PYLON VERTICAL SUPPORT ANGLE ABOVE SKATE ANGLE CRACKED. R & R CRACKED ANGLE IAW SRM 51-10-02.Sep 1, 2010 · N591NW · Boeing 757351SDR DALA1020995811Angle · crackedPYLON TO FAIRING FIRESEAL ANGLE CRACKED JUST AFT OF AFT ENG MOUNT. VERIFIED WITH EDDY CURRENT (CRACKS BY 3 FASTENERS FROM OTBD END) REPLACED CRACKED ANGLE IAW SRM 51-10-02.Sep 1, 2010 · N591NW · Boeing 757351SDR DALA1021065811Angle · crackedPYLON TO FAIRING FIRESEAL ANGLE CRACKED JUST AFT OF AFT ENG MOUNT. VERIFIED WITH EDDY CURRENT (CRACKS BY 3 FASTENERS FROM OTBD END) REPLACED CRACKED ANGLE IAW SRM 51-10-02.Sep 1, 2010 · N591NW · Boeing 757351SDR IXXA10KILN086SAngle · crackedDURING ROUTINE C-INSP FOUND ANGLE CRACKED ON NR 2 ENGINE PYLON. REMOVED CRACKED ANGLE. WELDED CRACKED ANGLE. REINSTALLED ANGLE IAW AMES PSM CHAP 7 SECTION 03, REV 3 6-14-10, AND SRM 51-40-02.Aug 31, 2010 · N762CX · Boeing 767232SDR ASOA201001195Fairing · crackedLT LOWER STANG FAIRING, 434BB, INBD SIDE IS CRACKED. RECEIVED LT LOWER STANG FAIRING 434BB. REF MASTER PANEL BOOK PAGE 30 OF 49 FOR INSTALLATION.Aug 28, 2010 · N846AS · Cndair CL6002B19SDR FDEA201008263142Web · crackedREF EO F5450-7-5006 PT2 : STRUT 2 TO DIAGONAL BRACE FITTING INSP WORK INSTRUCTION E STEP 2 FAILED NDT. CRACK 0.020" AT 1.00 POS ON LOWER WEB AT HOLE FIG 3, CIRCLE 1. CRACK REPAIR CARRIED OUT IAW EA F-5450-139376 (PYLON STRUCTURE AD 2008-05-10 -NR2 PYLON LOWER Aug 26, 2010 · N935FD · Boeing 7572T7SDR USAA2010082791842Fuse Pin · corrodedCLT - Q2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON NR 2 ENGINE OUTBOARD MIDSPAR FUSE PIN. REPLACED NR 2 ENGINE OUTBOARD MIDSPAR FUSE PIN IAW B737 AMM 54-10-01.Aug 25, 2010 · N533AU · Boeing 7373B7SDR USAA2010082791841Fuse Pin · corrodedCLT - Q2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON NR 1 ENGINE OUTBOARD MIDSPAR FUSE PIN. REPLACED NR 1 ENGINE OUTBOARD MIDSPAR FUSE PIN IAW B737 AMM 54-10-01.Aug 25, 2010 · N533AU · Boeing 7373B7SDR USAA2010082791840Fuse Pin · corrodedCLT - Q2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON NR 2 ENGINE INBOARD MIDSPAR FUSE PIN. REPLACED NR 2 ENGINE INBOARD MIDSPAR FUSE PIN IAW B737 AMM 54-10-01.Aug 25, 2010 · N533AU · Boeing 7373B7SDR USAA2010082791839Fuse Pin · corrodedCLT - Q2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON NR 1 ENGINE INBOARD MIDSPAR FUSE PIN. REPLACED NR 1 ENGINE INBOARD MIDSPAR FUSE PIN IAW B737 AMM 54-10-01.Aug 25, 2010 · N533AU · Boeing 7373B7SDR EIAA2010051Doubler · crackedNR 3 PYLON INBOARD SIDE NAC STA 252 APPROX 22 INCHES ABOVE SKIRT REPAIR DOUBLER HAS CRACK. REMOVED DAMAGE, NDT AREA FABBED REPAIR AND INSTALLED PER ECRA 470-54-309-2.Aug 20, 2010 · N470EV · Boeing 747273CSDR FDEA201008112935Web · crackedNR 3 PYLON INSIDE COMPARTMENT 487 DL, WEB CRACKED UNDER THE FUEL LINES. REMOVED WEB 487 DL IAW SRM 51-35-01, VOL II. REMOVED DAMAGED AREA AND FABRICATED DOUBLER AND FILLER IAW SRM 54-00-01, FIG 2-B, SHEET 2, VOL I. ALODINED AND PRIMED IAW 51-21-01, VOL II. Aug 11, 2010 · N304FE · Doug MD1030FSDR FDEA201008112926Support · crackedNR 2 PYLON LT UPPER PANEL SUPPORT BRACKET FOUND CRACK AT PP STN 174. CRACKED BRACKET ON NR 2 PYLON LT UPPER PANEL SUPPORT REMOVED AND REPLACED IAW SRM 51-40-02 REV. 100. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Aug 11, 2010 · N935FD · Boeing 7572T7SDR FDEA201008112924Nut Clip · corrodedNR 1 PYLON AFT FAIRING FWD NUTPLATE CLIP HAS CORROSION. LOCATED ABOVE PANEL 434AL FWD SIDE. CORRODED NR 1 PYLON AFT FAIRING NUTPLATE CLIP DOUBLER PLATE R & R IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 11, 2010 · N935FD · Boeing 757200SDR FDEA201008102909Rib · chafedNR1 PYLON AFT FAIRING RIB 19 WEB IS CHAFED. R & R RIB 19 ASSY IN THE NR1 PYLON AFT FAIRING IN REF TO SRM 51-40-21, PARA 6 AND PARA 13.Aug 10, 2010 · N417FE · Airbus A310222SDR A6WA201040593Bracket · crackedLT NOSE INLET MOUNTING FLANGE WIRE HARNESS BRACKET IS CRACKED AT 8 O`CLOCK POSITION. REPLACE BRACKET IAW SRM. REO`S REMOVAL OF INLET TO ACCOMPLISH REPLACEMENT.Aug 9, 2010 · N446AW · Cndair CL6002B19SDR A6WA201040742Channel · chafedLT PYLON PANEL 412BT DIVIDER CHANNELS ARE CHAFED. R & R DIVIDER CHANELS ON PANEL 412BT.Aug 8, 2010 · N445AW · Cndair CL6002B19SDR A6WA201040741Channel · chafedPANEL 422DB DIVIDERS CHAFED. R & R DIVIDERS ON PANEL 422DB.Aug 8, 2010 · N445AW · Cndair CL6002B19SDR SWIA201024677Structure · crackedLEFT NACELLE OUTBOARD REINFORCEMENT FOR EXHAUST COWL CRACKED. (SVC CHECK) REPLACED PER SRM.Aug 6, 2010 · N270YV · Emb EMB120ERSDR FDEA201008062854Angle · corrodedNR 2 PYLON AFT STRUCTURE, FWD / RT INBD VERTICAL ANGLE IS FRETTED. BLENDED OUT DAMAGED AREA IAW SRM 51-73-10, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-00, FIG 10, PG 111 (MORE THAN 25 PERCENT). REMOVED RIB. INSTALLED NEW RIB PN A5451521950100 IAW SRM 54-54-1Aug 6, 2010 · N417FE · Airbus A310222SDR IPXA10561534Spacer · corrodedINSPECTION TYPE:C2, NR 1 ENGINE PYLON INBD SKATE ANGLE, BACKING ANGLE, FWD SPACER AT NAC STA 205 IS CORRODED. REPLACED SPACER IAW SRM 51-40-02-0G, SRM 51-10-02-0G STEP 8, SRM 51-40-05-0G, SRM 51-40-08-0G.Aug 3, 2010 · N430UP · Boeing 75724APFSDR IPXA10561538Splice · chafedINSPECTION TYPE:C2, CHAFING ON NR2 PYLON STRUCTURE AT UPPER OTBD CORNER OF AFT MATING SURFACE FOR NR 2 PYLON FAIRING NR441AT. REMOVED FABRICATED AND REPLACED IAW SRM 51-40-02, 51-40-08.Jul 29, 2010 · N430UP · Boeing 75724APFSDR FDEA201007292723Bracket · crackedNR 2 PYLON OTBD RIB 8 BRACKET IS CRACKED AND FASTENER ATTACH HOLES ARE OVERSIZED RIB 8 - RIB 8 R & R BRACKET IAW SRM 51-40-20, PARA 6 & 7.Jul 29, 2010 · N417FE · Airbus A310222SDR FDEA201007282694Web · crackedNR 2 PYLON, INTERNAL STRUCTURE WEB IS CRACKED FWD LT SIDE OF THE PRECOOLER STRUCTURE BOX. REMOVED & REINSTALLED SUPPORT BRACKET IN REF TO SRM 51-40-21, PARA 5. STOP DRILLED CRACK AND INSTALLED REPAIR BOUBLER IN REF TO SRM 54-50-00, FIG 203.Jul 28, 2010 · N417FE · Airbus A310222SDR IPXA10561595Angle · chafedINSPECTION TYPE:C2, NAC STRUT NR 1 STRUCTURE OF PANEL NR 434BL FWD UPPER ATTACH AREA IS CHAFED. REPLACED SPLICE ANGLE IAW SRM 51-40-02 AND SRM 51-10-02-0G, BAC DRW 313N3004.Jul 26, 2010 · N430UP · Boeing 75724APFSDR UIEA2010072600123Stiffener · crackedDURING D-CHECK IN TPE, THE NR 3 STRUT WAS FOUND TO HAVE A CRACK IN A STIFFENER TEE ANGLE NEAR NAC STA 298 AND NAC WL 140. FIG 1 FOR DAMAGE LOCATION. (THE DAMAGE WAS CUT OUT WITH AN ANGLE AND FILLERS BEING INSTALLED AS SHOWN IN FIG 2 AND IAW SRM 54-51-02 REPAIRJul 26, 2010 · N498MC · Boeing 74747UFSDR UIEA2010082600122Stiffener · crackedDURING D-CHECK, THE NR2 STRUT WAS FOUND TO HAVE A CRACK IN A STIFFENER TEE ANGLE ON THE INBD SIDE NEAR NAC STA 377 AND NAC WL 155. SEE FIG 1 FOR DAMAGE LOCATION AND REPAIR DETAILS. (THE DAMAGE WAS CUT OUT WITH AN ANGLE AND FILLERS BEING INSTALLED AS SHOWN IN FJul 26, 2010 · N498MC · Boeing 74747UFSDR IPXA10561565Bracket · crackedINSPECTION TYPE:C2, NAC-STRUT NR 1 STA 203-85 INBD SIDE VERTICAL CHANNEL HAS ATTACH LOWER ANGLE BRACKET CRACKED. R & R INBD SIDE VERTICAL CHANNEL IAW SRM 51-10-02, SRM 5 51-40-02.Jul 24, 2010 · N430UP · Boeing 75724APF
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