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 CALA2025040803641Angle · damaged(SUPPORT TASK) LEFT SIDE FUSELAGE BETWEEN STA 879 TO STA 984 UPP ER WING WBL95.00 HAS 01 SUPPORT WING TO BODY FAIRING PANEL 191DL WITH HOLE MISSDRILL.-(DOT 6-73).-() REFERENCE NR#125288. REMOVED AND REPLACED SUPPORT ANGLE ON L/H WING TO FAIRING BODY S TATION SDR WRXR202504070102Bracket · corrodedFOUND CORROSION ON BRACKET AND LAMINATED SHIMS SUPPORT FUSELAGE TO FAIRING PANEL 193AR RH BL 22.50 (2EA BRACKETS), REMOVED CORROSION IAW REO 690-53-82-221 REV -- DATED 2025-03-20 WITH LIMITATIONS "ACCEPTABLE FOR 8000 FLIGHT HOURS FROM THE TIME OF INCORPORATIONSDR WRXR202504070101Bracket · corrodedFOUND CORROSION ON BRACKET AND LAMINATED SHIMS SUPPORT FUSELAGE TO FAIRING PANEL 193AL (2EA BRACKETS). CORROSION REMOVED IAW REO 690-53-82-224 REV -- DATED 2025-03-31.SDR DALA2025050603513Pin · misinstalledINSPECTION FOUND THAT THE RELEASE CAM PIN WAS INSTALLED INCORRECTLY AND THAT AN ADJUSTMENT WAS NEEDED ON THE TAIL CONE DEPLOYMENT SYSTEM. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OSDR SWAA2025051956159Angle · crackedCRACK ANGLE LOCATED BS 500D BODY FAIRING BETWEEN S-18L TO S-20L AT LOWER FUSELAGE 2025-242251<[01] REPLACED NEW ANGLE LOCATED BS 500D BODY FAIRING BETWEEN S-18L TO S-20L AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DWG 116A3110 SHEET 5 REV B; DWG 116A3SDR IPXA2025040323286Tee Angle · corrodedFAULT, STR, ZONE 100,T-CHORD AT FS 1220 RBL 15 UNDER WING TO BODY PANEL 198 MR HAS CORROSION DOT#21-10. REMOVED FRAME AT 1220 RBL 15 UNDER WTB PANEL 198MR IAW B757 SRM 51-40-02. RECIEVED NEW T-CHORD FROM MACHINE SHOP ON TRAVLER # T25/1809365.LOCATED AND DRILLESDR DALA2025040202483Fairing · chafedSHIP 3360 BELLY FAIRING 197GB AND FUSELAGE ATTACH SURFACE FOUND CHAFING. CORRECTIVE ACTION: COMPLIED WITH ERA 624942-14 REV ORIGINAL. (0890739)SDR VNAA202504020012Channel · crackedCRACKED CHANNEL AND STRAP JOINT BTWN AFT FAIRING ACCESS PANEL 195DL1196DR. EVALUATED,VISUAL INSPECTION AFTER CLEANED ON STRAP AND CHANEL WAS PERFORMED PER CRJ 900 SRM 51-11-00-001-001-A01 AND CRJ 900 NDT MANUAL 51-20-009-210 CORROSION ON STRAP WAS FOUND, NO CSDR SWAA2025043020501Access Panel · delaminatedDELAMINATED ACCESS PANEL 193B BODY FAIRING AT LOWER FUSELAGE 2025-238170<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-41435; DUE DATE: 11/APR/25.;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 FSDR SWAA2025043055804Access Panel · delaminatedDELAMINATED ACCESS PANEL 193B BODY FAIRING AT LOWER FUSELAGE 2025-238170<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-41435; DUE DATE: 11/APR/25.;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 FSDR SWAA2025043020344Access Panel · crackedCRACK AROUND HOLES ACCESS PANEL 561CB TRAILING EDGE AT LT WING 2025-238153<[01] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:190984811; DUE DATE:24-FEB-26;[02] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH800; S/N: 08193228; DUE DATE: SDR SWAA2025040820054Hinge Fitting · crackedNOSE RADOME LH HINGE FITTING CRACKED<[01] REMOVED FITTING LH CRACKED AT NOSE RADOME AND INSTALLED NEW FITTING P/N 141A8882-9; LOT 1600355-1 IAW SRM 51-40-02.SDR DALA2025032802305Skin · chafedSHIP 3360 BELLY FARING 198GB AND FUSELAGE ATTACH SURFACE FOUND CHAFING. CORRECTIVE ACTION: REPAIRED PER ERA 624941-14 REV ORIGINAL. (0881918)SDR DALA2025033102372Panel · damaged(LOG 0880597) AD."AA 5352-01035" ON REF STEP #11 ELONGATED HOLES ON AFT EDGE ALL POSITIONS, PANEL 193D. PANEL 193D WERE REPAIRED PER B737-800 SRM 51-70-05-2R PROCEDURE 8 REPAIR 8 WITH REFERENCE TO B737-800 SRM 53-40-70-2R PROCEDURE 1 REPAIR 1.SDR IPXA2025041380768Angle · corroded-WING/BODY STRUCTURE ON PANEL 192DR NUTPLACE BRACKET WITH CORROSION DOT 07-036. INSTALLED (BRACKET) AND NUT PLATES AT WING/BODY STRUCTURE ON PANEL 192DR IAW B757-200 SRM 51-40-02. REVIEWEDSDR IPXA2025041180978Bracket · corrodedRH WING/BODY STRUCTURE IN PANEL 196AR NUTPLACE HAVE CORROSION DOT 07-038. REMOVED BRACKET ON WING BODY 196AR IAW B757-200 SRM 51-40-02-0G-0 BRACKET P/N 149N7550-50.LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-05-0G-0.TRETATED AND PRIMED NEW BRACKET IAW SRM 51SDR WRXR20250325001Strap · corrodedSTRAP THAT JOINS PANEL 194AB TO 195AB PANEL HAS MULTIPLE SPOTS OF CORROSION AT RH BL22.50 TO LH BL 22.50.00. FS 761.85. FABRICATED, LOCATED AND DRILLED STRAP IAW CRJ 900 SRM 51-24-21-001-001-A01. INSTALLED NUT PLATES 20EA. IAW CRJ 900 SRM 51-45-00-001-001-A01.SDR R61A2025041400194Strap · corrodedCENTER FUSE 3 EXTERNAL, WING TO FUSE FAIRING STRAP CORRODED BTWN FR 73-76 STR 19L-29L. MX REPLACED STRAP PN 170-92409-003 IAW SRM 51-41-02, 51-43-04.SDR R61A2025041400193Strap · corrodedCENTER FUSE 3 EXTERNAL, WING TO FUSE FAIRING STRAP CORRODED BTWN FR 73-76 STR 19R-29R. MX REPLACED STRAP PN 170-92406-003 IAW SRM 51-41-02, 51-43-04.SDR DALA2025033002339Radome · damagedSHIP 3258 DISC: BIRD STRIKE RADOME, BIRD REMNANTS FOUND ON RIGHT ENGINE COWL AND ON BLADES. ALL ENGINE INDICATIONS NORMAL ON APPROACH. C/A: C/W BIRD STRIKE INSPECTION PER A320 AMM 05-51-14-200-803-A. FOUND NOSE RADOME DAMAGED BEYOND LIMITS. DA788048. R&R RADOMSDR DALA2025032402161Subframe · crackedSHIP 3351 CRACK IN BELLY FAIRING LATERAL FRAME AT FR53.2. CORRECTIVE ACTION: COMPLIED WITH ERA 608483-14 REV A. (0874126)SDR SWAA2025050154273Access Panel · delaminatedDELAMINATED ACCESS PANEL 193CL AT LOWER FUSELAGE 2025-224103<[01] TOOL USED: CALIPER PN: 8647A42 SN: B22440130 DUE DATE: 20-SEP-25.;[02] TOOL USED: SCALE PN: 91847 SN: AE-409315 DUE DATE: 29-JUN-25.;[03] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH80SDR DALA2025040802695Release Mech · out of adjustTHE TAILCONE RELEASE MECHANISM CAM WAS FOUND TO BE INCORRECTLY ADJUSTED: PIN ALIGMENT IS MORE THAN 38.5. 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 00166: TAILCONE RELEASE MECSDR 2025F00074Tail Cone · corrodedMECHANICALLY REMOVED 4 AREAS OF CORROSION LOCATED ON TAILCONE SERVICE DOOR FRAME ASSEMBLY WITH ADDITIONAL 4 AREAS OF CORROSION AFTER FRAME ASSEMBLY WAS REMOVED IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS EXCEEDING .SDR JJBA20250401049Support · crackedLH WING TO BODY FAIRING, UPPER STRIP SUPPORT CRACKED BTW FRAME 48-49. LH WING TO BODY FAIRING UPPER STRIP SUPPORT BTW FR 48-49 CUT OUT AND REPAIR PARTS FABRICATED AND INSTALLED.SDR JJBA20250401046Angle · crackedCF3 RH TOP WING TO BODY FAIRING ANGLE FOUND CRACKED AT FR47. AT CF3 RH TOP WING TO BODY FAIRING AT FR47, ANGLE REPLACED.SDR SWAA2025032407691Radome · crackedFOUND CRACK ON CENTER OF NOSE RADOME<[01] FOUND TO BE DAMAGE LIMITED TO EROSION BOOT. REPAIRED PER EA M-21-153-01060-REPREF;[02] FOUND TO BE DAMAGE LIMITED TO EROSION BOOT. REPAIRED PER EA M-21-153-01060-REPREFSDR VNAA20250320080Support Angle · corrodedHN00200808 DISCREPANCY: FS909 LBL16 TO RBL16 WING TO BODY SUPPORT STRUCTURE FAYING SURFACE STRAP BOTTOM SURFACE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED NEW MIDSTRAP PN SH670-39338-1 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-45-00-001-001-A01SDR VNAA20250320072Splice Plate · corrodedHN00200904 DISCREPANCY: FWD WING TO BODY, PLATE, SPLICE JOINT LOCATED AT FS. 629 HAS MULTIPLE AREAS OF CORROSION FROM LBL28 TO RBL28. CORRECTIVE ACTION: .REMOVED CORRODED SPLICE JOINT. LOCATED AND INSTALLED A NEW SPLICE JOINT IAW CRJ 700 SRM 51-42-06-001-001-ASDR YENA2025032000285Tail Cone · damagedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / SB-53-1500 TAIL CONE / LH/RH FIREWALL / BTWN FR81-83 / DEVIATION - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-0008-25 (COVER + PART 1) REV 0 /2/ AIRBUS RDAF 81545334/003/2025#A /3/ AIRBUS TD/81545334/007/20SDR FDEA202503170432Tee Fitting · crackedLEFT EXTERIOR FUSELAGE, WING TO BODY FAIRING FRAME AT STATION 698, FRAME TO PANEL 191BL ATTACH LOWER INTERCOSTAL "T" FITTING, FITTING IS CRACKED ALONG "T" LOWER RADIUS AS MARKED. LEFT LEADING EDGE BODY TO WING FAIRING ATTACHMENT AREA, CRACKED FITTING 149T7SDR SWAA2025042805959Access Panel · delaminatedDELAMINATED ACCESS PANEL 194BL BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 194BL BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10.SDR SWAA2025031805737Panel · delaminatedFOUND DELAMINATION ON WING TO BODY FAIRING PANEL 192BR REF TO TTG8Q00YYM37. <[01] R & R WING TO BODY FAIRING PANEL 192BR PER SRM 51-40-02 REF ( TTG8Q00YYM37 ).SDR IPXA2025031442035Radome · damagedBIRD STRIKE ON RIGHT SIDE OF RADOME AT 3:00 POSITION REMOVED AND REPLACED NOSE RADOME WITH REF TO MM 53-52-01-201.SDR WRXR20250314003Fairing · corrodedON 193AB PANEL, AT BL0.00, WL68.00, FS732.00, FOUND MULTIPLE SPOTS OF CORROSION ON LH AND RH STRAPS (P/NS CC670-39052-3 AND CC670-39052-4). REMOVED AND REPLACED LH AND RH STRAPS (P/NS CC670-39052-3 AND CC670-39052-4) IAW CRJ. 900 SRM 51-42-13-001-001-A01.SDR WRXR20250314002Fairing · corrodedON 193AB PANEL, AT BL0.00, WL68.00, FS732.00, FOUND MULTIPLE SPOTS OF CORROSION ON LH AND RH STRAPS (P/NS CC670-39052-3 AND CC670-39052-4). REMOVED AND REPLACED LH AND RH STRAPS (P/NS CC670-39052-3 AND CC670-39052-4) IAW CRJ. 900 SRM 51-42-13-001-001-A01.SDR SWAA2025040715555Access Panel · crackedCRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-203626<[01] TOOL USED CALIPER PN: 8647A43; SN: B22440130; DUE DATE: 20/SEP/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 22-FEB-26.;[03] TOOL USED; SCALE PN: SCA-301; SN: AE-412135; DUE DATESDR SWAA2025040704618Access Panel · crackedCRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-203626<[01] TOOL USED CALIPER PN: 8647A43; SN: B22440130; DUE DATE: 20/SEP/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 22-FEB-26.;[03] TOOL USED; SCALE PN: SCA-301; SN: AE-412135; DUE DATESDR HALA20250314011Radome · damagedPOSSIBLE BIRD STRIKE DESCENDING BETWEEN 6-5000 FEET. REMOVED & REPLACED RADOME PER AMM 53-15-11. OK FOR SERVICE.SDR DALA2025031602004Access Panel · erodedSHIP 3141 EROSION ACCESS PANEL 191BB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 542077-14TR. (0851374)SDR VNAA202503070010Support · crackedAFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25SDR JJBA20250324034Angle · crackedCF3 RH TOP WING TO BODY FAIRING ANGLE FOUND CRACKED AT FR51. AT CF3 RH TOP WING TO BODY FAIRING ANGLE AT FRAME 51 CRACKED PART PLUS REPAIR PARTS FABRICATED. ALL REPAIR PARTS INSTALLED.SDR IPXA2025031364002Bracket · corrodedFAULT: WTB PANEL BRACKET AT 196AR HAS HEAVY CORROSION. DOT 95334-5. INSTALLED 1 NEW BRACKET IAW B757-200-SRM 51-40-02-OG FASTENERS INSTALLED QTY 5 BACB30NX6K4X BTCH 000434215. REVIEWED.SDR DALA2025031001827Radome · damaged(LOG 6892042) DAMAGE ON FRONT LEFT OF AIRPLANE NOSE. REPAIRED DAMAGED AREA IAW ERA 624396-14 REV O. VERIFIED ER/A AND PRI REVS 1-5 MATCH.SDR JJBA20250401048Support · crackedLH LOWER WING TO FUSE LATERAL FAIRING SUPPORT FOUND CRACKED AFT ON WW. LH LOWER WING TO FUSE LATERAL FAIRING SUPPORT AFT ON WW REMOVED AND REPLACED.SDR SWAA2025030400996Fairing · delaminatedLH WING TO BODY PANEL 191FL LEADING EDGE DELAMINATION<[01] RAISED NEW FAULT L/H WING TO BODY PANEL 191FL HAS EVIDENCE OF LEADING EDGE DELAMINATION [TTG8Q00Z03EP] AS DIRECTED BY 25-153-00420-TLD (N8615E- SWA - REPAIR - FUSELAGE SECTION 44 EDGE EROSION AND DELAMSDR SWAA2025030400997Fairing · delaminatedR/H WING TO BODY PANEL 192BR HAS EVIDENCE OF DELAMINATION<[01] REMOVED RH WING TO BODY PANEL 192BR TO FOM PER AMM 53-51-21;[02] REMOVED DAMAGE; AND LAYED UP REPAIR PER SRM 53-40-70-2R-1 AND SRM 51-70-05; BEGAN CURE.;[03] UNBAGGED REPAIR; TAP TESTED GOOD; APPLISDR SWAA2025030400998Panel · delaminatedLH WING TO BODY PANEL 192BL LEADING EDGE DELAMINATION<[01] REMOVED LH WING TO BODY PANEL 192BL TO FOM PER AMM 53-51-21;[02] REMOVED DAMAGE; LAYED UP REPAIR PLIES; AND STARTED CURE PER SRM 53-40-70-2R-1 AND SRM 51-70-05.;[03] REMOVED DAMAGE AND APPLIED A PERMANSDR SWAA2025030400999Panel · delaminatedR/H WING TO BODY PANEL 191FR HAS EVIDENCE OF DELAMINATION DELAMINATING AT LE<[01] REMOVED RH WING TO BODY PANEL 191FR TO FOM PER AMM 53-51-21;[02] REMOVED DAMAGE; AND LAYED UP REPAIR PER SRM 53-30-70-2R-1 AND SRM 51-70-05; BEGAN CURE.;[03] REMOVED DAMAGE AND ASDR DXTA2025030402548Seal · unsecureFUSELAGE PLATES / SKINS / PANELS: REPEAT WRITE UP, 3RD TIME. INTERMITTENT, LOUD, NOTICEABLE HUMMING SOUND AND VIBRATION COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. VIBRATION MOSTLY NOTICEABLE NEAR RIGHT MIDDLE PASSENGER SEAT, AND NOISE IS LOUDER IN THE CABIN T
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