JASC 5350
Service difficulty reports · 6,118
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 AALA202506031978Radome · delaminatedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: WEATHER RADAR ECHOES DOES NOT REFLECT ACCURATE WEATHER DEPICTION IN WINDSCREEN. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT DFW. PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST AND BITE TEST, PER AMM 34-43SDR R61A2025060200261Strap · corrodedDURING HEAVY CHECK CF III WING TO FUSELAGE FAIRING STRAP FOUND TO BE CORRODED BETWEEN FR73-76 STR 23R-29R. REMOVED AND REPLACED FUSELAGE FAIRING STRAP IAW EMB 170/175 SRM 51-43-04SDR R61A2025060200260Strap · corrodedDURING HEAVY CHECK CF III WING TO FUSELAGE FAIRING STRAP FOUND TO BE CORRODED BETWEEN FR 73-76 STR 23L-29L.REMOVED AND REPLACED FUSELAGE FAIRING STRAP IAW EMB 170/175 SRM 51-43-04SDR DALA2025060204206Support Frame · corrodedAIRCRAFT 8110, CORROSION ON WING TO BODY FAIRING SUPPORT FRAME AT FR 48, BETWEEN BL0 TO RBL 13. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ERA 626621-14 REV ORG. (LP 0998166)SDR IPXA2025060944382Angle · crackedCRACKED ANGLE, L/H LOWER WING TO BODY AREA, STA 785. (AGING A/C INSPECTION).REMOVED DAMAGE ANGLE I.A. W SRM 51-40-02-0G REV. 92. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.92, BOEING DWG NO.140T0705 SHEET 2 REV.- AND BOEING DWG NO.149T7340 SHEET 1 REV.DSDR IPXA2025060622941Splice · corrodedFAULT - CORROSION - SPLICE TEE , LOWER WING - TO - BODY FAIRING PANEL #149AL INTERNAL FORWARD SURFACE.REMOVED DAMAGE SPLICE TEE I.A.W SRM 51-40-02-0G REV.92.INSTALL NEW SPLICE TEE I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO. 145T8629 SHEET 2 REV: ASDR DALA2025053004147Support Fitting · damagedSHIP 3123 ELONGATED HOLE (1EA) ON RADOME SUPPORT FITTING I/B LH SIDE ON SKIN PAN EL OF WINDSHIELD FRAME. CORRECTIVE ACTION: APPLIED CORRECTLY ALODINE ON PREVIOUS STEP. REPLACED SUPPORT FITTING I/B LH SIDE ON SKIN PANEL OF WINDSHIELD FRAME AS PER A319 SRM 51-42SDR DALA2025060604326Support Fitting · wornSHIP 9577 WEAR ON SUPPORT FITTING AND BUSHING ALSO RUSTED HARDWERE OF SPRING RELEASE MECHANISM AT TAILCONE. REPAIRED PER B717-200 SRM 51-41-01-0G (0988292)SDR SWAA2025061674209Access Panel · crackedCRACK ACCESS PANEL 194GR BODY FAIRING AT LOWER FUSELAGE 2025-340197<[01] REJECT STEP 10. BECAUSE THE REPAIR PLIES INSTALLED DO NOT MEET THE OVERLAP REQUIREMENTS IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2>CURED THE REPAIR PLIES AND PERFORMED POST REPAIR INSPECTIONSDR R61A2025061100292Support · corrodedCORRODED RIB-X=11653.0 WTB FAIRING SUPPORT ON CF2 MLG BAY. MX REPLACED SUPPORT PN 170-02456-003 IAW SRM 51-41-00, 51-42-02.SDR IPXA2025052917198Bracket · corrodedR/H WING TO BODY PANEL 194CR LOWER NUTPLATE BRACKET HAS CORROSION. 33-032. INSTALLED PARTS R/H WING TO BODY IAW B757-200 SRM 51-70-12-0G-0. VERIFIED INSTALLED PARTS ON R/H WING TO BODY PANEL 194CR STRUCTURE.SDR SWAA2025051971750Fairing · delaminatedLH WING TO BODY FAIRING PANEL 192CL HAS EDGE DELAMINATION LH WING TO BODY FAIRING PANEL 192CL HAS EDGE DELAMINATION AT FWD OB CORNER 2IN.X 2IN.<[01] REPAIRED PANEL PER SRM 51-70-08.SDR SWAA2025051971730Radome · delaminatedRADOME HAS MULTIPLE DELAMINATION SPOTS OUT OF LIMITS. DELAMINATIONS PAST THE ANTI-STATIC COATING AND ARE NOT MINIMUM 10 INCHES FROM OTHER DAMAGED AREA<[01] R&R NOSE RADOME AMM 53-52-00SDR IPXA2025052803409Support · corrodedWING TO BODY FAIRING SUPPORT STRUCTURE PANEL AR STA1040 HAS CORROSION. INSTALLED NEW SUPPORT STRUCTURE PANEL 195AR STA1040. IAW.51-40-02.SDR DALA2025051503774Longeron · crackedDURING WTB FAIRING INSP TASK CARD 5352-01038-01B-AD RELATED. STEP 4. LONGERON P/N C02383111-002 @ RBL40 OB SIDE ABOUT 2 FEET FROM FWD EDGE CRACK APPROX 3" LONG. LOCKED OUT RAD ALT 1, 2 AND 3 PER A220 AMP 34-44. REMOVED RAD ALT ANTENNA 3 PER A220 AMP 34-44. REMSDR SWAA2025061671408Panel · delaminatedWING TO BODY PANEL 191FL DELAMINATED<SDR SWAA2025061671409Panel · delaminatedWING TO BODY PANEL 191FR HAS DELAMINATION<[01] WORK ACCOMPLISHED ON CARD TTG8Q010BAFH;[02] C/W;[03] CERTIFICATION OF WORK STATED ABOVE CAN'T BE SIGNED OFF BY INSPECTOR. MAINTENANCE IS CERTIFYING WORK STATED ABOVE.SDR SWAA2025061671410Panel · delaminatedWING TO BODY PANEL 192AL HAS DELAMINATION<SDR SWAA2025062369214Panel · delaminatedLH WTB PANEL 193AL IS DELAMINATED LH WTB PANEL 193AL IS DELAMINATED (REPAIRABLE).SDR SWAA2025061669211Panel · delaminatedRH WTB PANEL 191AR IS DELAMINATED RH WTB PANEL 191AR IS DELAMINATED AND REPAIRABLE PER SRM 53-30-70-2R-1<[01] ALL WORK ACCOMPLISHED ON CARD # TTG8Q010JUZS;[02] COMPLETESDR SWAA2025061669212Panel · delaminatedLH WTB PANEL 191FL IS DELAMINATED LH WTB PANEL 191FL IS DELAMINATED (REPAIRABLE)<[01] C/W;[02] COMPLIED WITH INSPECTION;[03] COMPLIED WITH INSPECTIONSDR SWAA2025061669213Panel · delaminatedRH WTB PANEL 191FR IS DELAMINATED<SDR DALA2025051203678Cable · wornTAILCONE EMERGENCY RELEASE HANDLE CABLE ASSEMBLY WAS FOUND WORN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00623: RELEASE HANDLE CABLE ASSEMBLY WAS REPLACED PER B717 AMM 20-0SDR 2025FA0000345Longeron Fitting · crackedDURING THE ACCOMPLISHMENT OF ADSI IB744530165, THE LONGERON FITTING WAS FOUND CRACKED AS OUTLINED IN THE ADSISDR 2025FA0000344Longeron Fitting · crackedDURING THE ACCOMPLISHMENT OF ADSI IB744530165, THE LONGERON FITTING WAS FOUND CRACKED AS OUTLINED IN THE ADSISDR HNAA2025060900406Support · cracked53-2028 RH UPPER SUPPORT WING TO BODY FAIRING CRACKED BTW FR41-42. REPAIRED IAW SRM 53-23-12RE ITEM 3 FIG 202SDR HNAA2025060900405Support Angle · cracked53-2030 RH WING TO BODY FAIRING, LWR ANGLE SUPPORT#4 FRO FWD IS CRACKED. REPAIRED IAW SRM 57-20-01RE ITEM 3 FIG 203,204SDR HNAA2025051500352Support Angle · cracked53-2033 LH WING TO BODY FAIRING, LWR ANGLE SUPPORT #2 FROM FWD IS CRACKED. RAR SUPPORT IN IAW SRM 51-40-02SDR 2025FA0000343Longeron Fitting · crackedDURING AN INSPECTION OF THE EXTENSION FITTING OF THE WING TO BODY FARING, A CRACK WAS FOUND AS OUTLINED IN ADSI IB744530165-LH.SDR HNAA2025051400350Support Angle · cracked53-2029 WING TO BODY FAIRING, RH LWR ANGLE SUPPORT #2 FROM FWD IS CRACKED. RAR SUPPORT IAW SRM 51-20-02SDR HALA20250505025Radome · damagedFOUND BIRD STRIKE ON RADOME DAMGE BEYOND LIMITS. REMOVED AND REPLACED RADOME IAW AMM 53-15-11. OPS CHECK GOOD . OK TO CONTINUESDR SWAA2025060266423Support Frame · crackedWING TO BODY PANEL SUPPORT HAS CRACK AT BS 500D STR 19R<[01] REMOVE AND REPLACED WING TO BODY PANEL SUPPORT FRAME IAW SRM 51-10-02-0G-0 AND DWG# 116A3118 ID: 0004 REV: ASDR REXA2025060900639Support Strap · corrodedCORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB. CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-0SDR WRXR20250428001Strap · corrodedON STRAP P/N BA690-00001N3403 FOUND MULTIPLES SPOT CORROSION ON BOTH SIDES, AT FS881.00 TO 927.00, BL00 LWR FAIRING PANEL 195DL. REMOVED CORROSION IAW CRJ 900 SRM 51-21-06-001-001-A01. REMOVED MORE CORROSION ON BOTTOM SIDE IAW CRJ 900 SRM 51-21-06-001-001-A01.SDR 2025F00103Fairing · corrodedLH AND RH FWD FUSELAGE CHIN FAIRINGS HAVE CORROSION EXTENDING FROM THEM. MECHANICALLY BLENDED 6 AREAS OF CORROSION ON LH AND RH CHIN FAIRING FUSELAGE SKIN. IAW CESSNA 680 SRM 51-70-02 AND SRM 51-10-01. FOUND BLENDED AREAS TO BE BEYOND LIMITS PER CESSNA 680 SRMSDR JR2R20250423379Fairing · bentLH WING ROOT FAIRING BENT I/B OF LENS AND PAINT MISSING SHOWING BARE METAL.SDR R61A2025042100199Spacer · corrodedDURING HEAVY CHECK WING TO FUSELAGE FAIRING PANEL 192C, CORROSION FOUND AT DOUBLER. REMOVED AND REPLACED DOUBLER AT PANEL 192CR IAW SRM 51-41-02SDR SWAA2025051957543Fairing · crackedWTB FAIRING PNL 194BL CRACKED<[01] WTB FAIRING PNL 194BL CRACK WAS REPAIRED IAW SRM 51-70-05-2R-10.;[02] VERIFIED CORRECTIVE ACTION #1SDR DALA2025042103076Cable · out of trackGOT A TAILCONE UNLOCK MSG DURING TAXI IN TO GATE. WHILE VERIFYING M PROCEDURES FOR MEL 53-52-018, FOUND LOCKING CABLE LEADS LOOSE, MEL STATES LEADS SHOULD BE TIGHT/NO EVIDENCE OF SLACK. FOUND CABLE OUT OF T FITTING. THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCYSDR SWAA2025042825939Panel · pulledPANEL 193D FASTENERS ARE PULLED THROUGH THE PANEL. REMOVED AND REPLACED PANEL 193D FASTENERS AND PANEL. I.A.W. SRM 51-40-02.SDR WRXR20250418002Angle · corrodedCORROSION FOUND ON SUBSTRUCTURE AT FS 847.00 - FS 847.00+32.00 LBL 36.00 ALONG TOP ANGLES. REMOVED CORROSION ON SUBSTRUCTURE AT FS 847.00 - FS 847.00+32.00 LBL 36.00 ALONG TOP ANGLE PN SH670-39345-7 (INB) IAW CRJ900 SRM 51-21-06-001-001-A01. MATERIAL LOSS FOR SDR WRXR20250418001Angle · corrodedCORROSION FOUND ON SUBSTRUCTURE AT FS 847.00 - FS 847.00+32.00 LH BL 36.00 ALONG BOTTOM STRAP. REMOVED CORROSION ON SUBSTRUCTURE AT FS 847.00 - FS 847.00+32.00 LH BL 36.00 ALONG BOTTOM STRAP IAW CRJ900 SRM 51-21-06-001-001-A01. FABRICATED STRAP SH670-39347-7 FSDR WRXR20250417003Angle · corrodedCORROSION FOUND ON SUBSTRUCTURE AT FS 847.00 LH BL22.50 - RH BL22.50 TOP SIDE. REMOVED CORROSION AT ANGLE SH670-39332-10 (RH) LOCATED ON SUBSTRUCTURE AT FS 847.00+32.00 - RH BL22.50 TOP SIDE. ALL WORK COMPLIED WITH IAW EA 53-2025-0471 REV --.SDR SWAA2025051956536Panel · debondedPANEL 191CL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 191CL WITH OUTER SKIN DISBONDED NEAR CENTER OF PANEL WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR UIEA2025041400471Bracket · corrodedCORROSION - BRACKET LOWER FUSELAGE WING-TO-BODY SUPPORT BRACKET STA 920 BL 0.(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 103. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 14240130 SHEET 1 REV A. 3. JOB COMPLETED AND CONDITION CHECK NSDR DALA2025041402912Bracket · wornRH SIDE SECTION 48 FUSELAGE SKIN AND BRACKET UNDER SEAL PANEL 314CRX AT STA 1730 FOUND WORN. THE WORN SKIN REMOVED AND MEASURED: THE ORIGINAL THICKNESS IS T=0.080". THE DEPTH OF CLEAN UP X=0.056" >20%T. FOUND OUT OF LIMIT PER B767-300 SRM 53-80-70-1A-1 FIG 101SDR DALA2025041502958Fairing · damagedSHIP 3252 DISC: PANEL 197GB WING TO BODY FAIRING HAS SEVERAL FASTENER HOLES DAMAGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 016-0001:10-0553-8-6853/001 00007 ACCOMPLISHED HOLE REPAIR PER A320 SRM 51-77-12. (LP: 0SDR CALA2025041103713Angle · corroded(SUPPORT TASK) LEFT SIDE FUSELAGE BETWEEN STA 879 TO STA 984 AT WBL95.00 UPPER WING HAS FAIRING PANEL SUPPORT STRUCTURE 191DL WI TH LIGHT CORROSION. SDR REPORTING REMOVED AND REPLACED SUPPORT ANGLES BETWEEN STATION 900 TO STATI ON 960 IAW B757-300 SRM 51-40-02SDR CALA2025041103698Fairing · damaged(SDR) - LH WING-TO-BODY FAIRING 197BL HAS A FEW AFT SUPPORT CLIP FASTENER HOLES ELONGATED (OVER DRILLED) FROM RIVET REMOVALS WIT H 1EA RIVET NOT PUNCHED OUT ENTIRELY RESULTING IN A BENT ANGLE A ND POTENTIAL CRACK. REF: 124978 SDR REPORTING ONLY REMOVED AND REPSDR CALA2025041103691Angle · damaged(SDR) - LEFT WING SIDE OF BODY SPLICE INTERNAL LOWER METALIC ANG LE LOCATED BELOW OVERWING EMERGENCY EXIT HAS 02 PIECES OF SCREW STUCKED INTO NUT PLATE (02 EA). DOT 75-067 HA-75. REF: 124735 SDR REPORTING PURPOSE ONLY ANGLE LOCATED BELOW OVERWING EMRGENCY EXIT
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