JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 IXXA2022101101Floor Mat · crackedFLC LEFT AFT BALL MAT HAS CRACKED AND RAISED SKINSDR CALA2022093002564Skin · noneDURING PERFORMED AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR DOUBLER LOCATED LOWER FUSELAGE SKING AT FR31 TO FR32 BTW 38L TO STRG 39L. SEE AEROMAN NON ROUTINE 2022-308900 01-E FIGURE 005 VIEW B (SHEET 02) DOUBLER REPAIR MATERIAL: DAMAGE IAW NTM 51-90-00, TSDR CALA2022092802528Doubler · noneDURING PERFORMED AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR DOUBLER LOCATED LOWER FUSELAGE SKING AT FR31 TO FR32 BTW 38L TO STRG 39L. SEE AEROMAN NON ROUTINE 2022-308900 01-E FIGURE 005 VIEW B (SHEET 02) DOUBLER REPAIR MATERIAL: DAMAGE IAW NTM 51-90-00, TSDR CALA2022092802537Skin · crackedNO RECORD PROVIDED FOR AGING AIRCRAFT INSPECTION AND RECORD REVIEW TO ACCOUNT FOR INSTALLATION AND RE-INSPECTION STATUS OF EXISTING DOUBLER ON EXTERIOR FUSELAGE FRAME 32, STRINGER 38-39L, SEE AEROMAN NON ROUTINE 2022-308927. WITH INSPECTION THRESHOLD 65,000FC SDR CALA2022092802535Skin · noneNO RECORD PROVIDED FOR AGING AIRCRAFT INSPECTION AND RECORD REVIEW TO ACCOUNT FOR INSTALLATION AND RE-INSPECTION STATUS OF EXISTING DOUBLER ON EXTERIOR FUSELAGE FRAME 69-70 STRINGER 29-30R. SEE AEROMAN NON ROUTINE 2022-308928 LAGE SKIN AT FR69/FR70 BETWEEN 5-3SDR SWIA202266690None · gougedGOUGE ON EXTERNAL FUSELAGE SKIN BETWEEN FS 349.00 - 364.00, STGR 22R - 23R (C-CHECK RO 10/29/2022) / COMPLIED WITH ALL STEPS OF REO 690-53-21-1551 REV -- DATED 2022-10-11 DISPOSITION FOR BLENDED CHAFE DAMAGE TO FUSELAGE LOWER SKIN BETWEEN FS349.00 AND SDR SWIA202266689None · gougedGOUGES ON EXTERNAL FUSELAGE SKIN FS 379.00 - 394.00, STGR 22R - 23R (C-CHECK RO 10/29/2022) / REPAIRED GOUGES ON EXTERNAL FUSELAGE SKIN AT FS 379.00 - 394.00, STGR 22R - 23R REF REO 690-53-21-1551 REV -- DATED 2022-10-11 COMPLIED WITH ALL STEPS, SEE COSDR CALA2022092602523None · noneDUE TO C1 ADP FAILURE , PLEASE ACCOMPLISH A VISUAL INSPECTION OF THE EXTERIOR OF AIRCRAFT FOR ANY SIGN OF DAMAGE MAY CAUSED BY ADP FAILURE...TOMC MO PERFORMED BSI OF LWR TURBINE GEARBOX ASSY(TGA) PER STEP 15A OF C/W STEPS 1 THRU 12 , 16 & 17 OF AVO10049 REV ASDR CALA2022092602522None · noneECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - REPLACED DAMAGED UNION O-RING TO DUAL VALVE. SERVICED YELLOW ACCUMULATOR TO PROPER LEVEL. COMPLIED WITH ALL LEAK CHECKS AND SYSTEM CHECKS FOR NORMAL OPERATION OF HYDRAULICS.SDR CALA2022092602520None · damagedPERMANENT REPAIR "PE REPAIR AREA AND NOT FOUND CRACK INDICATION. GENER RFORMED DVI ON INTERNAL AND EXTERNAL REPAIR AREA AND STRUCTURE PERFORMED HFEC INSPECTION ON INTERNAL AND EXTERNAL SKIN AT ATE A 2ND DIP THAT REFERENCE THE LOG PAGE NUMBER OF DTA DIP FOR ANDSDR YENA2022092700971None · noneDURING HEAVY MAINTENANCE: AFTER MID-SEAL REST REMOVAL, FOUND CORROSION IN LWR BEAM-BAG DOOR FR, AL. LOCATED BETWEEN FR 77/80 AFT CARGO DOOR CUTOUT; REF. TOMX WO N339JB/2012 NR-00321 -: CORROSION IN LWR BEAM-BAG DOOR AT AFT CARGO DOOR CUTOUT WAS REMOVED AND EVASDR YENA2022092700970None · noneDURING HEAVY MAINTENANCE: CRACK: NLG WHEELWELL FR15 AT HORIZONTAL RH UPPER WEB INTERNAL SIDE OF FUSELAGE L= 1.400"; REF TOMX WO: N339JB/2012/E190/B5 CHECK NR 00292: FR15 AT HORIZONTAL RH UPPER WEB WAS REPAIRED PER JETBLUE E/C E22-729-01, TOMX ETI-190-22-644 RESDR YENA2022092700969None · noneDURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP, LOCATED BTW FR 90 AND STGR 29L / 29R AT AFT CARGO COMPARTMENT INTERNAL STRUCTURE; REF TOMX WO 2012 N/R 00226 SHEAR CLIP, LOCATED BTW FR 90 AND STGR 29L / 29R AT AFT CARGO COMPARTMENT INTERNAL STRUCTURE WAS REPSDR YENA2022092700968None · noneDURING HEAVY MAINTENANCE: FROM TECHOPS MX WO2012, NRC00208. (CPCP FINDING): CORROSIÓN ON BEAM FLOOR STRUCTURE UNDER FWD GALLEY, BTW FR 12 AND FR 14; APPROX. Y+ 290 MM; REF TECHOPSMX WORK ORDER # 2012 N/R# 00208, TECHOPSMX TECH #201532129, TECHOPSMX RII INSPECTSDR CALA2022092602494Skin · corrodedCORROSION SKIN BTW FR 69 TO FR 70 AND BTW STR 1L TO STR 2L ON UP PER FUSELAGE. SEE AEROMAN NON ROUTINE 2022-308664. AIRED AREA OF FUSELAGE SKIN AT FR69/70 BETWEEN S-2 LH AND S-2RH ABOVE FOR PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION CTION DONE ON CUT OSDR VNAA2022092499981Stringer · crackedSTRINGER 3L LINTEL IS CRACKED FROM THE FWD EDGE OF THE STRINGER THRU .2" AFT OF THE 3RD AFT FASTENER HOLE. FAILED NDT INSPECTION. PERFORMED REPAIR OF STRINGER 3L LINTEL IAW REO 670-53-21-493 REV D.SDR IXXA2022092400001Skin · crackedFUSELAGE SKIN CRACKED, BS 1723-1725 S20-21R.SDR 2022FA0000546None · crackedUPON REMOVING THE L/H AND R/H OVER-WING ACCESS PANELS FOR AN ZONAL INSPECTION, FOUND THE L/H AND R/H SIDE DRAG ANGLES ARE CRACKED AND THE R/H SIDE SUPPORT STRAP IS CRACKED AT TWO PLACES - BOTH ON THE SUPPORT STRAP. PROVIDED ENGINEERING DOCUMENTATION TO SUPPORTSDR YENA2022092700973None · noneDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 35 & STR 30L / PRESSURE BULKHEAD / CRACK AT FASTENER HOLE – TIME-LIMITED REPAIR. (CONSIDERED A MAJOR REPAIR)SDR CALA2022092302482None · noneRII INSPECTION REQUIRED REFERENCE CARD 27-0520-8-0018 LH WING LEADING EDGE PANELS FOIL MESH INSPECTION REQUIRES INSPECTION BY BACK PER GMM - 03-20-20. ITEMS CLEARED IAW WORK CARD 27-0520-8-0021 . ITEMS HAVE BEEN REPAIRED AND ARE IN COMPLIANCE WITH SRM51-70-14SDR CALA2022092302475None · noneRII INSPECTION REQUIRED RII INSPECTION REQUIRED REF LP 9585915 AND LP 9579613 PANEL 511NB WAS INSTALLED AFTER REPAIR WITHOUT INSPECTION. REPAIR WAS A MAJOR REPAIR AND REQUIRES INSPECTION RII. CLEARED TO INSTALL REPAIR IAW SRM 51-70-14-2R-3 STEP 6 REMOVED CONDUSDR CALA2022092302456Skin · noneREF. CATEGORY B REPAIR PERFORMED ON FUSELAGE SKIN STA. 835 AT S-23L ON LT. SIDE REAR 12" FORWARD OF TOILET SERVICE PANEL REQUIRES INSPECTION AT INITIAL THRESHOLD OF 50,000 TOTAL FLIGHT CYCLES AND REPEAT INTERVALS OF 4,000 FLIGHT CYCLES AS LISTED IN TABLE 203. SDR CALA2022092302454None · corrodedAFT CABIN, FR65/FR70, Y1292, SEAT TRACK CORRODED. REMOVED CORROSION ON SEAT TRACK Y1292 BETWEEN FR64 TO FR66 IAW S RM 53-00-14-283-002 WAS FOUND WITHIN DAMAGE LIMITS. REMOVED AND INSTALLED SEAT TRACK BETWEEN FR66 TO FR68 IAW SRM 51-42-11/001 WORK ACCOMPLISHED SDR CALA2022092302453None · corrodedFWD CABIN, FR20/FR24, Y-765, SEAT TRACK CORRODED. REMOVED CORROSION ON FWD CABIN BETWEEN FR20 TO FR24 Y-765 SEAT T RACK IAW SRM 53-11-15-283-011. FOUND WITHOUT DAMAGE LIMITS. REMO VED AND INSTALLED SEAT TRACK Y-765 IAW SRM 51-42-11/001 WORK ACC OMPLISHED AT SSDR CALA2022092302452None · corrodedFWD CABIN, FR16/FR24, Y-1292, SEAT TRACK CORRODED. REMOVED CORROSION AT SEAT TRACK -Y1292 FR12 TO FR24, FOUND OUT O F LIMITS IAW SRM 53-11-15-283-011 AND REMOVED AND REPLACED SEAT TRACK -Y1292 FR12 TO FR24 IAW SRM 51-42-11/001 WORK ACCOMPLISHED AT ST ENGINEERISDR IXXA2022092302Web · corrodedFLC WEB CORRODEDSDR SWIA202266691None · chafedFWD CARGO DOOR INNER SKIN AND AFT FRAME CHAFED ON AFT END OF DOOR (MARKED). (C-CHECK RO 10/29/2022) FWD CARGO DOOR INNER SKIN AND AFT FRAME CHAFE ON AFT END OF DOOR FOUND TO BE OUT OF LIMITS REF CRJ 900 SRM 52-35-01-101-001-A01 RECEIVED AND COMPLIED WITSDR SWIA202266684None · chafedCENTER CARGO DOOR INNER SKIN AND AFT FRAME CHAFED ON AFT END OF DOOR (MARKED). (C-CHECK RO 10/29/2022) CENTER CARGO DOOR INNER SKIN AND AFT FRAME CHAFE ON AFT END OF DOOR FOUND TO BE OUT OF LIMITS REF CRJ 900 SRM 52-35-01-101-001-A01 RECEIVED AND COMPLISDR SWIA202266683None · chafedCENTER CARGO DOOR INNER SKIN AND FORWARD FRAME CHAFED ON FORWARD END OF DOOR (MARKED). (C-CHECK RO 10/29/2022) CENTER CARGO DOOR INNER SKIN AND FWD FRAME CHAFE ON FWD END OF DOOR FOUND TO BE OUT OF LIMITS REF CRJ 900 SRM 52-35-01-101-001-A01 RECEIVED ANSDR SWIA202266682None · chafedFWD CARGO DOOR INNER SKIN AND FORWARD FRAME CHAFED ON FORWARD END OF DOOR (MARKED). (C-CHECK RO 10/29/2022) FWD CARGO DOOR INNER SKIN AND FWD FRAME CHAFE ON FWD END OF DOOR FOUND TO BE OUT OF LIMITS REF CRJ 900 SRM 52-35-01-101-001-A01 RECEIVED AND COMPSDR CALA2022092302463Skin · noneRAMP REPORTED SCRATCH ON LEFT SIDE REAR FUSELAGE 12" FWD OF TOILET SERVICE PANEL. APROX 1/16" DEPTH. AND PERMANENT REPAIR PER PART 3 WITHIN 250 FLIGHT CYCLES (NO LATER THAN 1829 TFC) INTERIM REPAIR COMPLIED WITH IAW ECRA 5330-06968. ACCOMPLISH INSPECTION OF RESDR SWIA202266784None · crackedCENTER WINDSHIELD POST - LOWER LEFT MOUNT BRACKET IS CRACKED. (MARKED) (C-CHECK RO 11/8/2022) REMOVED AND INSTALLED NEW CENTER WINDSHIELD POST LOWER LEFT MOUNT BRACKET REF CRJ200 SRM51-42-21 AND DWG NO. 601R33007 REV -U COMPLIED WITH 51-900-1003-SKYSDR R61A2022101800639Doubler · corrodedDURING HEAVY MAINTENANCE FOUND CORROSION BETWEEN FR 97 - FR 98 AND STGR 28R -STGR 28L UNDER A/C DATA PLATE. CORROSION FOUND UNDER A/C DATA PLATE BETWEEN FR 97-98 AND BETWEEN STGR 28L-28R WAS REPAIRED IAW ETD2022-170-030122.SDR SWIA202266771None · corrodedPAX DOOR ENTRY BOTH FWD AND AFT CUPS ON FUSELAGE FLOOR SUPPORT HAVE CORROSION. L/H SIDE (C-CHECK RO 11/8/2022) REMOVED AND REPLACED CAPS P/N 601R31527-217 AND CLEATS P/N 601R31527-137. REF CRJ200 SRM 51-42-06 AND DWG 601R31527 REV AM COMPLIED WITH 51-90SDR SWIA202266770None · corrodedL/H SIDE AT AFT LOWER CORNER OF PAX DOOR ENTRY JUST AFT, AT STRAP AT FS 349.0 THERE IS EXFOLIATION. (C-CHECK RO 11/8/2022) CORROSION ON JOINT BRACKET AT F.S. 349.0 FOUND OUT OF LIMITS OF CRJ 200 SRM, REMOVED AND REPLACED JOINT BRACKET AT FS349.00 P/N: 6SDR GTIA2022092336673None · noneFA REPORTS FUMES SMELL OF DIRTY SOCKS LATE DESEND / APPROACH IN TO MIA-PERFORMED TROUBLESHOOTING PER TSM 05-50-00-810-831--A, R&R RECIR FILTER CARTRIIDGES IAW AMM 21-21-41. PERFORMED ECS DECONTAMINATION LEVEL C IAW AMM 21-00-00. NO FUMES OR SMELL NOTED AT THISSDR CALA2022092102433Floor Support · corrodedFWD CABIN, FR16, Y765/Y254, AREA WITH CORROSION AND SCRATCHES.SDR CALA2022092102432Seat Track · corrodedAFT CABIN, FR65/FR70, Y1292, SEAT TRACK CORRODED.SDR CALA2022092102431Seat Track · corrodedFWD CABIN, FR16/FR24, Y-1292, SEAT TRACK CORRODED.SDR CALA2022092102435Seat Track · corrodedFWD CABIN, FR20/FR24, Y-765, SEAT TRACK CORRODED.SDR SROM091801Support · corrodedCORROSION DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS. CORROSION ON FORWARD WARDROBE SUPPORT STRUCTURE. 11.4" AFT OF STA. -18.250 AND 2.85" FORWARD OF STA. 1.0.SDR SROM0918202202None · corrodedCORROSION DAMAGE BEYOND MANUFACTURER’S PUBLISHED LIMITS. CORROSION DAMAGE ON FUSELAGE FRAME UPPER WEB AND CAP. PN: 85329152-103(LH) AND 85329256-101(RH).SDR CALA2022091902418Skin · noneBIRD STRIKE UNDER CAPT NOSE FOUND SMALL DENT JUST FWD OF FWD E&E DOOR LOCATED A LITTLE FWD STA 188, MEASURED 2"W 1.5L & .046D, PER SRM 53-00-01-1A-1 WITHIN LIMITS D < .125 & W/Y RATIO > 30 ACCOMP ACFT BIRD STRIKE INSP PER MM 05-51-18 LOCATED ON FUSELAGE CENTESDR CALA2022091902410Seat Track · corrodedSEAT TRACK SUPPORT SECTION RBL 24 STA 720 TO 779 HAS CORROSION (I/B). THIS L/P CREATED FOR ESFR PURPOSES ONLY. SEE N/R 964612 FOR WORK PERFORMED. SEE N/R 980278 FOR ESFR ORIGINATION. CREATED ESFR #1029739. SUBMITTED SIGNED COPY TO PLANNING FOR INCLUSION INTO ASDR SWIA202266644None · crackedCRACKED ANGLE BRACKET ON FS280.00 FLOOR BEAM AT LBL12. (C-CHECK RO 10/24/2022) REMOVED AND INSTALLED NEW BRACKET P/N CC670-34099-1. REF: DWG CC670-34010, REV: J, CRJ700 SRM 51-42-21-001-001-A01. COMPLIED WITH THE SKYWEST TASK CARD 51-900-1002-SKYSDR R61A2022101800635Seat Track · corrodedCORROSIO ON PREVIOUSLY BLENDED AREA OF L/H I/B SEAT TRACK AT FR52 FOUND OUT OF LIMITS. R&R IAW SRM 51-43-02, 51-43-03 & 51-41-01.SDR R61A2022100600621Crossbeam · corrodedSEVERAL AREAS OF CORROSION AS MARKED ON FR 14 CROSSBEAM OUTBOARD OF RH SEAT TRACK. PERFORMED PERMANENT SPLICE REPAIR ON CROSSBEAM FR 14 O/B OF RH SEAT TRACK. REF EMB SRM 53-00-10/ REPAIR 03P.SDR YENA2022091900927None · noneFLT#943, RNO-LAX. ' AFT CABIN DIRTY SOCK SMELL ON DESCENT BELOW 10K UNTIL GATE. PACK 2 TURNED OFF AT GATE; COMPLIED WITH INFORMATION NOTICE 2017-T015 J SECTION A. ISOLATED FAULT TO TYPE 10, (A), 1, C PER TSM 05-50-00-810-085-B. THE AIRCRAFT IS OK FOR SERVICE. SDR YENA2022091600923None · noneFLT#745, JKF-PSE. 'ROTTEN EGG/ DIRTY SOCK SMELL VERY STRONG AT LANDING (PACKS); REF MDDR 485574, THIS ACTION CLEAR MDDR 485569 (AS PER W/O 1205088 PERFORMED APU COMP CLEANING & APU CLEANING PROCEDURE. THIS ACTION CLEAR MDDR 485574. MX-4 UPDATED PLACARD REMOVEDSDR CALA2022091902406Door Sill · corrodedR2 DOOR SILL AFT CORNER HAVE CORROSION AROUND GIRD BAR PLATE PER HAECO LCQ NR 9290380/30380 GENERATED BY V061682 (SUPPORT TASK) REMOVED & REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11. PERFORMED BY V052030 INSP BY V061771.
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