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 SWAA2025121050826Access Panel · crackedCRACKED ACCESS PANEL 193AL, BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-2, REPAIR 2.SDR REXA2026051200558Angle · crackedCRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17'' WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17' WAS REPAIRED PER EA CRJ953-20683 REV. IRSDR REXA2025121201034Support · crackedCRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17'' WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17'' WAS REPAIRED PER EA CRJ953-20784 REV IR.SDR DALA2025110308009Fairing · damagedRIGHT BELLY FAIRING #192KB HAS COMPOSITE DAMAGE. COMPLIED WITH ER/A 597056-14. (1281022).SDR SWAA2025110729234Panel · delaminatedPANEL 191FL LOWER AFT EDGE HAS EDGE DELAMINATION. REPAIRED PER [AMM 51-21-99-300-802.SDR CALA2025102910714Radome · delaminatedPILOT REPORTED BIRDSTRIKE DURING TAKE OFF. COMPLIED WITH BIRD STRIKE INSPECTION IAW AMM 05-51-14. FOUND EVIDENCE OF BIRD ON BELLY PANEL 191BB AND RT WING ROOT. NO DAMAGE NOTED AND DEBRIES CLEANED. RADOME DAMAGED DURING BIRD STRIKE INSPECTION, FOUND A 15X15INSDR SWAA2025120428478Access Panel · damagedELONGATED HOLES OF ACCESS PANEL 195BL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195BL IAW SRM 51-70-05-2R-10, REPAIR 10.SDR SWAA2025120428479Access Panel · elongatedELOGANTED HOLES OF ACCESS PANEL 195AR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195AR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10, REPAIR 10.SDR DALA2025102707834Radome · delaminatedRADOME HAS 2 BIRD STRIKES. TAP TEST SHOWS DELAMINATION. R & R RADOME PER THE AMM 53-15. (6683119)SDR DALA2025102707823Radome · delaminatedPOSSIBLE BIRD STRIKE FO SIDE RADOME. DURING BIRD STRIKE INSPECTION FOUND DELAMINATION OF RADOME OUT OF LIMITS PER A320 AMM 53-15. REMAINING BIRD STRIKE INSP WILL NEED TO BE C/W. R/R RADOME PER A320 AMM 53-15. C/W BIRD STRIKE INSPECTION PER A320 AMM 05-51. FOUSDR SWAA2025120127302Former · crackedWING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN S19 & 20L. REMOVED AND REPLACED THE WING TO BODY FAIRING SUPPORT IAW SRM 51-40-02, AND DWG 116A3010, REV-.SDR DALA2025102307767Skin · gougedSHIP 3314 FOUND GOUGE ON FUSELAGE SKIN WITH BELLY FAIRINGS 198HB AND 198GB TOUCH AREA.. COMPLIED WITH ER/A 629866-14. (1266681).SDR SWAA2025120126766Panel · delaminatedPANEL 194CL DELAMINATED ON OUTER SURFACE. PANEL 194CL REPAIRED IAW SRM 51-70-05-2R-2.SDR DALA2025102207715Cable · twistedSHIP 9520 DURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. CORRECTIVE ACTION: PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT WAS INSTALLED CORRECTLY PER B717-200 AMM 53-52-01-830-802 ONLSDR DALA2025102207714Cable · twistedDURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT WAS INSTALLED CORRECTLY PER AMM 53-52-01-830-802 ONLY STEP E. (1) (S). (1262180)SDR N6WA2025102201Strap · corrodedAFT WING TO FUSELAGE FAIRING CENTER STRAP HAS CORROSION. REMOVED AND REPLACED AFT WING TO FUSELAGE FAIRING CENTER STRAP IAW CRJ AMM 53-82-83SDR SWAA2025110627997Panel · erodedPANEL 193CL L/E WAS WIND ERODED. REPAIRED IAW SRM 51-70-05-2R-6.SDR DALA2025102207711Release Mech · out of positionIN REFERENCE AMDS 5352-4002 DURING INSTALL TAILCONE SLIDE WAS FOUND TAILCONE RELEASE MECHANIS CAM OUT POSITION. TAILCONE RELEASE MECHANISM CAM WAS ADJUSTED PER AMM 53-52-03 (1257600)SDR DALA2025101707586Radome · damagedRADOME DAMAGED DUE TO BIRD STRIKE. REMOVED RADOME PER A319 AMM 53-15. (7744877).SDR VNAA20251015069Fairing · damagedFOUND ENLONGATED HOLE UNDER LH SIDE WING TO FUSELAGE FAIRING AT FS FS893. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-53-51-335 REV --.SDR CALA2025100909856Angle · corrodedWING TO BODY FAIRING 193AL, ANGLE GOING FORWARD FROM AFT APPROX 36 INCHES FROM CENTER HAS CORROSION UNDER NUTPLATES. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DRAWING 149N7125SH3, REV.SDR SWAA2025110721822Panel · delaminatedPANEL 194CL HAS AREAS OF DELAMINATION ON OUTER SURFACE. PANEL 194CL WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2025102721479Tail Cone · delaminatedDELAMINATED TAIL CONE ON EXTERNAL SKIN. REPAIRED TAIL CONE ON EXTERNAL SKIN IAW SRM 51-70-04-2R-1 REPAIR 1.SDR CALA2025100609664Structure · gougedAFTER HIGH PRESSURE DOOR WAS REMOVED FOR OTHER MAINTENANCE, FOUND GOUGES ON THE WING TO BODY FAIRING CHORD AT BS540. TRANSCRIBED FROM HAECO GSO NRC 9280981 UPDATED. REPAIRED CHORD AT BS 540 RH SIDE IAW B737-800 SRM 53-30-71-2R-2 REPAIR 2 PROCEDURE II PO# 1085SDR DALA2025100207183Access Panel · deterioratedDETERIORATED ALUMINUM MESH ON ACCESS PANEL 191BB BELLY FAIRING. COMPLIED WITH ER/A 542077-14TR. (1229102).SDR SWIA20260105930Fairing · damaged1EA ELONGATED HOLE NOTED UNDER FUSELAGE FAIRING 191BB, BETWEEN STR18L-STR19L AT FS409+96. REPAIRED 1EA ELONGATED HOLE UNDER FUSELAGE FAIRING 191BB, BETWEEN STR18L-STR19L AT FS409+96, REF. REO REO 601R-53-31-1356 REV -.SDR SWAA2025103019744Angle · crackedCRACK ON ANGLE WING TO BODY FARING STRUCTURE BS 500D AT LEVEL STR19L AT LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 116A3010, SHEET 39, REV-.SDR N6WA2025100302Strap · corrodedCORROSION ON STRAP RH AND LH FS879 ON PANEL 195AB. PREFORMED REPAIR ON ANGLE AND STRAP AT FS879 ON PANEL 195AB IAW CRJ SRM 51-42-06SDR N6WA2025100301Strap · corrodedCORROSION ON STRAP SUPPORT STRUCTURE, AFT WING TO FUSELAGE FAIRING FS879-FS909 RBL17.63. PERFORMED REPAIR ON ANGLE AND STRAP AT FS879-FS909 RBL17.63 IAW CRJ SRM 51-42-06SDR CALA2025100109506Tee Angle · crackedRIGHT WING TO BODY FAIRING, UNDER PANEL 196BR, ABOVE SLIDE DOOR COMPARTMENT, AFT BRACKET HAS A CRACK. REMOVED AND REPLACED AFT T ANGLE BS 1180. FABRI CATED ON TRAVELER T25/1834639, TREATED, PRIME, AND TOPCOAT AND REINSTALL PANEL 196CR. IAW SRM 51-40-02, SRMSDR N6WA2025100107Angle · corrodedCORROSION ON ANGLE, MID SUPPORT STRUCTURES AFT WING TO FUSELAGE FAIRING AT FS939. REMOVE AND REPLACED ANGLE SUPPORT STRUCTURE AT AFT WING TO FUSELAGE FAIRING AT FS939 IAW CRJ SRM 51-42-06SDR SWAA2025110519250Access Panel · crackedCRACK ANTENNA ACCESS PANEL 192F WING TO BODY FAIRING AT FUSELAGE EXTERIOR. REMOVED AND REPLACED MARKER BEACON ANTENNA ON ACCESS PANEL 192F WING TO BODY FAIRING AT FUSELAGE EXTERIOR IAW AMM 34-32-11-400-802 TESTED OK.SDR IPXA2025101389818Bracket · gougedLH WING, UPPER SURFACE, WTB, THROUGH FAIRING 577DT, CLOSE TO FALSE REAR SPAR, BRACKET SUPPORT HAS GOUGE. REMOVED BRACKET SUPPORT AT LH WING, UPPER SURFACE, WTB IAW A300-600 SRM 51-40-21. ++INSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21.SDR IPXA2025100979085Skin · delaminatedTAIL CONE STA1963-1992 BOTTOM SKIN INTERNAL BELOW THE APU EXHAUST MANIFOLD CORRODED/DELAMINATED. REMOVED SKIN BELOW APU EXHAUST MANIFOLD IAW SRM 51-40-02. INSTALLED NEW BOND ASSY (SKIN PANEL) IAW SRM 51-40-02-0G-0 AND DWG 148N3770. INSTALLED APU EXHAUST DUCSDR DALA2025092907060Release Cable · tornINITIAL INSPECTION: TORN CABLE OF RELEASE MECHANISM OF TAIL CONE AT AFT ACCESORIES COMPARTMENT. CORRECTIVE ACTION: CABLE ASSY RELEASE HANLDE P/N: 3913359-545 OF RELEASE MECHANISM OF TAIL CONE WAS REPLACED PER B717-200 AMM 20-00-02 AND ADJUSTED WAS PERFORMED PESDR CALA2025092909384Support Angle · crackedFOUND CRACK RT FWD BODY FAIRING SUPPORT ANGLE INBD END OF FRONT SPAR FIXED LEADING EDGE. REMOVED AND REPLACED ZEE ANGLE RH BETWEEN STA. 727J AND 767 RBL 21 PER SRM 51-40-02-0G-0 AND DWG 146A7500.SDR AALA202509231235Fairing · inflt separationAIRCRAFT WAS GROUNDED: WTB PANEL197AL MISSING ABOVE LEFT WING ON ARRIVAL AT FRA. MAINTENANCE INSTALLED NEW PANEL 197AL AND ACCOMPLISHED TIME LIMITED REPAIR IAW EA368352A.SDR DALA2025091906887Access Panel · crackedDELAMINATED ACCESS PANEL 191BB BELLY FAIRING AT LOWER FUSELAGE. COMPLIED WITH ER/A 542077-14TR. (1205793).SDR SWAA2025092415148Skin · debondedPANEL 195CR OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. PANEL 195CR REPAIRED PER SRM 51-70-05-2R-2.SDR CALA2025091809039Radome · no discrepancyREJECTED T/O FOR BIRDSTRIKE TO THE NOSE AT AROUND 115 KNOTS PERFORMED BIRDSTRIKE INSPECTION REF AMM 05-51-18-210-801. FOUND SMALL BLOOD SPOT ON UPPER RIGHT SIDE OF NOSE RADOME. CLEANED BIRDSTRIKE AND INSPECTED AREA WITH NO DEFECTS NOTED,SDR SWAA2025102114261Access Panel · delaminatedDELAMINATED ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-04-2R-2 REPAIR 2.SDR N6WA2025091202Splice · crackedAFT BELLY FAIRING SPLICE JOINT BETWEEN 195DL/196DR IS CRACKED. REMOVED AND REPLACED AFT BELLY FAIRING SPLICE JOINT BETWEEN 195DL/196DR IAW CRJ SRM 51-42-13SDR N6WA2025091201Splice · corrodedAFT FAIRING SPLICE FWD JOINT HAS CORROSION. REMOVED AND REPLACED AFT FAIRING SPLICE FWD JOINT IAW CRJ SRM 51-42-13SDR SWAA2025091612536Seal · crackedNOSE RADOME BOOT HAS CRACKING<[01] REMOVED AND REPLACED RADOME PROTECTIVE BOOT IAW AMM 53-52-00;[02] VERIFIED THE FOLLOWING:<BR>REMOVED AND REPLACED RADOME PROTECTIVE BOOT IAW AMM 53-52-00SDR REXA2025101400935Angle · corrodedCORROSION AT UNION ANGLE BTW AT AFT BODY FAIRING FRAME FS 881.00 CORROSION ON UNION ANGLE BTW AT AFT BODY FAIRING FRAME FS 881.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-82-55-101-002-A02 AND WAS FABRICSDR SWAA2025092912193Panel · delaminatedPANEL 194CR HAS AREA OF DELAMINATION ON OUTER SURFACE. PANEL 194CR WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2025092611931Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B IAW SRM 51-70-05-2R-8 REPAIR 8.SDR SWAA2025100212739Fairing · temp repairPREVIOUS TEMP REPAIR NOTED ON FAIRING 193CR. TEMP REPAIR REMOVED AND REPLACED WITH A PERMANENT REPAIR IAW SRM 51-70-05-2R-2.SDR DALA2025090106460Radome · damagedBIRD STRIKE. RT SIDE OF NOSE. REMOVED AND REPLACED RADOME IAW AMM 53-11-51. (7866658).SDR SWAA2025082607869Boot · crackedNOSE RADOME BOOT CRACKED. REMOVED AND REAPPLIED NOSE RADOME BOOT PER AMM 53-52-00-400-802. REMOVED AND REPLACED PER AMM 53-52-00-400-802-NG.
Back to JASC 5350