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 SWAA2026021863961Access Panel · damagedELONGATE HOLES ON ACCESS PANEL 193AR BODY FAIRING, LOWER FUSELAGE. REPAIRED THE ACCESS PANEL 193AR IAW SRM 51-70-05-2R-9, REPAIR 9.SDR SWAA2026021863962Access Panel · damagedELONGATE HOLES ON ACCESS PANEL 193AL ON THE BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AL BODY FAIRING IAW SRM 51-70-05-2R-9, REPAIR 9.SDR IPXA2026021193646Angle · corrodedSTR- BROKEN NUT PLATE ON RH AFT WING TO BODY JUST ABOVE RAM AIR TURBINE MARKED JK200-25 ATA 53-40. INSTALLED 01 EA TEE CHORD LOWER BEAM P/N 149N7630-38 BATCH 0004458867 (STA 1180-STA 1240) AND (1EA) INTERCOSTAL PREVIOUSLY REMOVED FOR ACCESS AT STA 1240 THRU 1SDR SWAA2026012862894Skin · damagedPANEL 191CL OUTER SKIN IS CREASED. REPAIRED IAW SRM 53-30-70-2R-1.SDR SWAA2026011962115Access Panel · delaminatedRIGHT AIRCRAFT SKIN PANEL, FORWARD OF RAM AIR FLAP DELAMINATING. DELAMINATION AT ACCESS PANEL 191FR, RT FWD WING TO BODY FAIRING PANEL, MID FAIRING ABOVE RT RAM AIR INLET. APPLIED ALUMINUM FOIL TAPE TO SEAL THE DAMAGED AREA PER EA EA 26-153-00171.SDR SWAA2026021861447Access Panel · crackedCRACKED ACCESS PANEL 191D, LOWER FUSELAGE. REPAIRED THE ACCESS PANEL PANEL 191D IAW SRM 51-70-05-2R-2, REPAIR 2.SDR DALA2026011500361Access Panel · corrodedTAIL CONE ACCESS PANEL NUMBER 317AL INTERNAL ANGLES WITH CORROSION. REPLACED TAIL CONE ACCESS PANEL 317AL INTERNAL ANGLES (2EA) IAW SRM 51-72-11-911-001 PARAG 2C REV 155, AND AIPC 53-58-04-05B SHEET 1 & 2 DETAIL H & J, REV 133.01, AND AIRBUS REFERENCE DWG D92SDR IPXA2026013069167Tee Angle · corrodedWING TO BODY FAIRING STRUCTURE LOWER T-CHORD EXFOLIATED AND WITH MULTIPLE SPOTS OF HEAVY CORROSION FROM BS 1180 TO 1240 AT RBL 57.50. DOT 21-40. EVALUATED TEE FITTING BETWEEN STA 1180-1240 AT RBL 57.5 AND FOUND TO BE EXFLOIATED WITH 100% MATERIAL LOSS AND ISSDR IPXA2026012869037Tee Fitting · corrodedWING TO BODY FAIRING STRUCTURE UPPER TEE FITTING EXFOLIATED AND WITH MULTIPLE SPOTS OF HEAVY CORROSION FROM BS 1180 TO BS 1240, RBL 57.50. REMOVED AFT WTB PANEL 198LR TO FOM IAW AMM 53-66-01-004-001. INSTALLED THE TEE FITTING IAW SRM 51-40-02.SDR IPXA2026012868936Channel · corrodedWING TO BODY FAIRING SUPPORT STRUCTURE WITH EXFOLIATED CORROSION AT BS 1219 RBL 6. INSTALLED NEW CHANNEL, 2EA SUPPORT PLATES, 1EA ANGLE, IN WING TO BODY, BS 1219 RBL 6, IAW B757 SRM 51-40-02-0G-0.SDR IPXA2026012869140Tee Fitting · corrodedWING TO BODY FAIRING STRUCTURE, VERTICAL T-FITTING EXFOLIATED AT LWR END AT BS 1200 RBL 57.50. INSTALLED T-FITTING IAW SRM 51-40-02.SDR SWAA2026012760380Access Panel · delaminatedACCESS PANEL 191CL HAS SMALL AREA OF DELAMINATION ON OUTSIDE OF PANEL APROX 22" FROM FWD END AND 15" FROM UPPER END. REMOVED THE AREA OF DELAMINATION IAW SRM 51-70-05-0G-0. ACCOMPLISHED A REPAIR TO AREA IAW SRM 51-70-05-2R-1.SDR IPXA2026012833721Tee Fitting · corrodedLEFT WING TO BODY FAIRING STRUCTURE WITH TEE FITTINGBEAM EXFOLIATED BTWN STA 1200 AND 1220 AT BL 57.50. INSTALLED NEW T-FITTING P/N: UP-149N7630-37 BETWEEN STA 1180-1240 LBL 57.50 I.A.W B757-200 SRM 51-40-02-OG.SDR SWAA2026020962499Support · crackedCRACK ANGLE BODY FAIRING SUPPORT STRUCTURE BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE. REPLACED ANGLE BODY FAIRING SUPPORT STRUCTURE IAW SRM 51-10-02-0G-0, STEP 9, SRM 51-40-02-0G-0, AND DWG 116A3010, SHEET 23, REV D.SDR IPXA2026012314754Tee Fitting · corrodedRT WING TO BODY FAIRING PANEL 196CR AREA, BTWN STA 1180 AND STA 1200, T-FITTING EXFOLIATED. INSTALLED NEW T-FITTING 1 EA RT WING TO BODY FAIRING PANEL 196CR BTW STA 1180 AND 1200 IAW B757-200 SRM 51-40-02. INSTALLED FRAME SECTION FROM STA 1140 -1200 I.A.W. B7SDR IPXA2026012734754Tee Fitting · corrodedRIGHT WING TO BODY FAIRING PANEL 196CR AREA, BTWN STA 1180 AND STA 1200, T-CHORD EXFOLIATED. DOT 90-018 REVIEWEDSDR SWAA2026020959203Access Panel · delaminatedDELAMINATED ACCESS PANEL 193CL BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193CL BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-05-2R-6. REPAIR 6.SDR SWAA2026020358926Access Panel · elongatedELONGATED HOLES ON THE ACCESS PANEL 192E OF BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.SDR DXTA2026010806466Sealant · defectiveNOTICED A WEIRD HUMMING AND NOTICABLE VIBRATION DESCENDING THROUGH FL300 AND CONTINUING OFF AND ON THROUGH 3000 FT. NOTICED IT WAS STRONGEST NEAR THE MIDDLE OF CABIN BELOW MIDDLE SEATS ON LT SIDE OF AIRPLANE. WAS STRONGER AT HIGHER AIRSPEEDS INSPECTED THE LASDR SWAA2026020357620Angle · crackedCRACKED ANGLE ON BODY FAIRING SUPPORT STRUCTURE BS 500D, STRINGER 19L, LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 116A3010, SHEET 23, REV D.SDR SWAA2026020357480Access Panel · delaminatedACCESS PANEL 194AL LOWER CORNER IS DELAMINATED. REPAIRED IAW SRM 51-70-05-2R-6-A00737, REPAIR 6.SDR YENA2026010600015Skin · corrodedDURING HEAVY MAINTENANCE: TAIL CONE SKIN BETWEEN FR83-84 & ABOVE S15L CORRODED, PERMANENT REPAIR; REFERENCES: /1/ A321 SRM TASK 53-51-11-50-A ITEM 5 /2/ A321 SRM TASK 53-51-11-283-006 /3/ SRM TASK 53-51-11-300-002. /5/ AIRBUS DOSSIER 81714282 /6/ ECA 331 /SDR SWAA2026020358541Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 194CL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.SDR SWAA2026020358542Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 194CR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.SDR SWAA2026020358543Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 195AL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCES PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.SDR SWAA2026020358544Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 195AR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.SDR SWAA2026020358545Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 194HL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.SDR SWAA2026020358548Access Panel · damagedELONGATED HOLES OF ACCESS PANEL 194DL WING TO BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.SDR SWAA2026020358546Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 195BL OF THE BODY FAIRING FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.SDR SWAA2026020358547Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 195BR, BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.SDR SWAA2026012756879Access Panel · crackedACCESS PANEL 191CL HAS 1 FASTENER HOLE CRACKED & THE COUNTER SINK IS DAMAGED. REMOVED THE DAMAGE IAW SRM 51-70-05-2R-0. INSPECTED REMOVED DAMAGE TO AREA IAW SRM 51-70-05-2R-0. ACCOMPLISHED A REPAIR TO FASTENER HOLE IAW SRM 51-70-05-2R-8.SDR SWAA2026012257072Floor Panel · debondedFLOOR PANEL 193B DEBONDED ON INNER SURFACE. REPAIRED THE FLOOR PANEL IAW SRM 51-70-05-2R-2-A00733, REPAIR 2.SDR SWAA2026020356928Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-9, REPAIR 9.SDR SWAA2026020356929Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193CR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.SDR SWAA2026012856040Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193AL ON BODY FAIRING. REPAIRED ACCESS PANEL 193AL IAW SRM 51-70-05-2R-8, REPAIR 8.SDR SWAA2026011255864Tee Fitting · crackedPANEL 195AL FWD SUPPORT TEE FITTING CRACKED AT LOWER END BS 520. REMOVED PANEL 195AL FOR ACCESS IAW AMM 53-51-21-000-802. REMOVED AND REPLACED WING TO-BODY FIRING SUPPORT FRAME BS 520 IAW SRM 51-40-02 AND DWG 116A3010 REV: B. CLOSED PANEL 195AL IAW AMM 53-51SDR DALA2025122509406Seal · damagedDIVERTED TO MSP DUE TO A REPORTED LOUD SQUEAL BETWEEN ROWS 11-22. SPEED TAPE APPLIED ON LEFT WTB FAIRING SEAL FOUND DEGRADED. SAME REAPPLIED. OK FOR SERVICE. LATER, REMOVE AND REPLACE THE DISCREPANT UPPER RUBBER BLADE SEAL WITH A NEW OR SERVICEABLE PART IAW ASDR REXA2026030900179Support · crackedCRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17. CRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17. WAS REPAIRED PER EA NO:CRJ953-21165 REV IRSDR SWAA2026011554811Support Frame · crackedLEFT FWD WING-TO-BODY FAIRING SUPPORT STRUCTURE FRAME AT BS 500A CRACKED. REMOVED AND REPLACED THE LT FWD WING-TO-BODY FAIRING SUPPORT STRUCTURE FRAME AT BS 500A IAW SRM 51-40-02 AND DWG 116A3118, REV A.SDR DALA2025122909459Release Mech · out of adjustFOUND TAIL CONE RELEASE MECHANISM CAM CLOCKED WRONG. TAILCONE RELEASE MECHANISM CAM REF B717 AMM 53-52-03 (1362721)SDR VNAA20260511021Angle · corrodedAFT FUSELAGE FAIRING SUPPORT WEB IS CORRODED ON THE FWD FACE AT FS 939. INSTALLED NEW SERVICEABLE CENTER ANGLE PN: SH670-39189-1 ON AFT FUSELAGE FAIRING SUPPORT WEB AFT FACE AT FS 939 IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-15-001-001-A01.SDR SWAA2026011453062Panel · debondedDEBOND ON OUTER SKIN OF PANEL 193AR. REPAIRED IAW SRM 51-70-05-2R-1-A00732, REPAIR 1.SDR DALA2025121509140Tee Angle · corrodedCORROSION ON WING TO BODY FAIRING TEE ANGLE AT BS 900, LBL 10. FWD OF PANEL 193HL. (REF. PREVIOUS REPAIR LOG PG 1416404 & ERA 583732-14) REMOVED DAMAGE ON WING TO BODY TEE ANGLE AT BS 900, LBL 10 FWD OF PNL 193HL ADDED REPAIR CHORD AND SPLICE IAW DELTA ERA #63SDR DALA2025121209082Radome · delaminatedDURING WALK AROUND, FOUND DELAMINATION TO RADOME. R & R RADOME IAW A319 AMM 53-15. (7892405).SDR SWAA2025121551818Radome · crackedNOSE RADOME HAS THREE CRACKS AT 9:00 POSITION, (LOOKING FWD). ALL ARE 1.5' IN LENGTH, STARTING AT AFT EDGE EXTENDING FWD. R & R NOSE RADIOMETER IAW AMM 53-52-00. R & R NOSE RADOME IAW 53-52-00..SDR SWAA2025121551820Guide · crackedRADOME ANGLE GUIDE FLANGES CRACKED AT 9:00 POSITION (LOOKING FWD). CW EA 25-153-03384.SDR SWAA2026011544112Panel · delaminatedPANEL 194CL HAS DELAMINATION DAMAGE ON OUTER SURFACE.SDR SWAA2026011447694Access Panel · delaminatedPANEL 194CL HAS DELAMINATION DAMAGE ON OUTER SURFACE. PANEL 194CL WITH DELAMINATION DAMAGE ON OUTER SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2, & SRM 53-60-70-2R-1.SDR SWAA2025121244268Fairing · dentedLEFT AFT WING TO BODY FAIRING 194FL, DENTED AND DELAMINATED. DENT MEASURES 4.5 X 3.5 X .100.SDR SWAA2025121250721Fairing · delaminatedLEFT AFT WING TO BODY FAIRING 194FL DENTED AND DELAMINATED. 4 INCHES FROM AFT EDGE AND 20 FROM LOWER EDGE. DENT MEASURES 4.5 X 3.5 X .100. R & R LT AFT WING TO BODY FAIRING PANEL 194FL IAW AMM 53-51-21. APPLIED TOP COAT FINISH TO LT AFT BODY TO WING PANEL
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