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 IXXA2022021113Shear Tie · corrodedCORROSION ON SHEAR TIE IN FLC BILGE AREA @ STA 742 AFT SIDE OF FLOOR SUPPORT BETWEEN STR 30L - 31LSDR SWIA202163298None · corrodedSKIN CORRODE ON INTERIOR BETWEEN FS349 TO FS 364 AND BETWEEN STGR21R TO STGR22R. (MARKED WITH TAPE) (C CHECK RO 12/28/2021) REPAIRED CORRODED SKIN BETWEEN FS 349 TO FS 364 STR 21R TO 22R IAW MHIRJ REO 601R-53-21-3506 REV -- DATED 2021-11-09. TASK CARD 51-SDR MASA20211105546None · corrodedFUSELAGE LOWER SKIN PANEL BETWEEN FS581.00 - FS613.00 & STGR26L - STGR26R WAS FOUND TO HAVE CORROSION. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-991-806, ITEM 1 B, EA 83-2021-047.
DEFECT LOCATION: FUSELAGE/FS581.00-FS613.00 & STSDR MASA20211105542None · noneSURFACE DAMAGE WAS NOTED ON THE UPPER SURFACE OF THE RING DOUBLER. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-23-991-801 SHEET 4, EA 10-2021-043. DEFECT LOCATION: FS661.00·FS661.00+16.STGR23L STGR24LSDR JJBA20211013062None · noneRUDER II PANEL 327FR LH UPPER LANDING CRACKED. REMOVE AND REPLACED RUDDER II PANEL 327FR LH UPPER LANDINGSDR JJBA20211013044None · noneMAIN CABIN - INTERNAL - CENTER FLR SUPPORT BEAM - IB (LWR) FLANGE HAS CORROSION AT RH FR50. REMOVED AND REPLACED MAIN CABIN INTERNAL CENTER FLR SUPPORT BEAM AT RH FR50SDR JJBA20211013043None · noneFLOOR BEAM HAS CORROSION AT SCREW HOLES FOR FLOOR PANEL 261DF. REMOVED AND REPLACED GUSSET AT FR59-FR61SDR JJBA20211013032None · noneCORROSION IN CARGO COMPARTMENT DOOR CUTOUT AFT LOWER SILL HAS 3 SPOTS AT FR65-FR68. REMOVED AND REPLACED COMPARTMENT DOOR LOWER SILL.SDR JJBA20211013047None · noneMAIN CABIN - INTERNAL - LH OMEGA BEAM LOCATED BETWEEN FR 15 - FR 23 CRACKED AT AFT END OF LOWER IB FLANGE. REPAIRED MAIN CABIN - INTERNAL - LH IB OMEGA BEAM LOCATED BETWEEN FR15-FR23SDR MASA20211013483None · damagedSURFACE DAMAGE WAS NOTED ON THE UPPER SURFACE OF THE RING DOUBLER. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-23-991-801 SHEET 4, EA 10-2021-043. DEFECT LOCATION: FS 661.00-FS 661.00+16.00 & STGR 23L STGR -24LSDR MASA20220329138None · crackedCRACKED STRINGER #3 [ LINTEL AREA] BTW STA. FS= 280 AND STA FS= 295 AT CIRCUNFERENTIAL SKIN JOINT. (CPAX).
INSTALLATION OF REPAIR PER BOMBARDIER SERVICE BULLETIN 670BA-53-040 REV. C AND REO 670-53-21-493 REV D ---- DEFECT LOCATION: CIRCUNFERENTIAL SKIN JOINTSDR SWIA202163145None · corroded*FWD BAGGAGE BAY AFT MACHINED BRACKET AT APPROX. FS.581 BETWEEN STRG 26L-27 HAS CORROSION (C CHECK RO 12-19-21) INSTALLED NEW FWD BAGGAGE BAY AFT MACHINED BRACKET FS581.00 BETWEEN STGR 26L-27 REF. DWG SH670-33600 REV Y, CRJ 700 SRM 51-42-21-001-001-A01, SRSDR SWIA202163144None · corroded*FWD BAGGAGE BAY AFT MACHINED BRACKET AT APPROX. FS.581 BETWEEN STRG 22L-23L HAS CORROSION (C CHECK RO 12-19-21) REMOVED AND REPLACED CORRODED FWD BAGGAGE BAY AFT MACHINED BRACKET AT APPROX FS581 BETWEEN STGR 22L AND 23L WITH NEW UNIT REF CRJ700 SRM 51-42SDR SWIA202162970None · cracked* L/H WHEEL WELL HAS WS48.30 CAP ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN CRACKED. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED WITH NEW CAP ANGLE AT LH SIDE WS48.30 PN:600-10389-1 REF CRJ200 SRM 51-42-21 AND DWG:600-10212, REV -D. COMPLIED WITH 5SDR IXXA2021120705Stanchion · corrodedSTANCHION ON O/B L/H SIDE STA 287 AND FORWARD OF P-36 LOWER END HAS HEAVY CORROSIONSDR IXXA20211028Fairing · crackedDMI 26031, L/P 572823-5 FOUND ON WALK- FWD OF MLG DOOR, STA 599, CRACK 9 IN. LONG FILLER SHEET METAL. AWAITING EO REPAIR FROM ENGINEERING.
AMES N/R 139923-0100-0011,ATI REV 1 ITEM 13: PER CUSTOMER REQUEST: C/W ATI EO 53-767-7984, FVCI EO 21176.1 (REPAIR- LSDR MASA20211021506Longeron · noneCORROSION ON LONGERON STGR 25R FS333-FS364 IN MAIN AVIONICS BAY |R&R LONGERONSDR AALA202110139093Unknown · unknownAIRCRAFT WAS GROUNDED: AROUND 1 MIN. AFTER TO, THERE WAS A SUDDEN SHUDDER AND LOUD THUMP. NO UNUSUAL INDICATIONS OR ODORS. FLIGHT ATTENDANT REPORTED AN ORANGE FLASH VISIBLE IN CABIN. (OPEN)SDR IXXA2021112204HSplice · corrodedCORROSION ALC STA 1255 STR 30R END FITTING. AMES NR 136876-0100-0167SDR IXXA2021112203HSupport · crackedALC STA 1260 RH SIDE WALL LWR CORNER GUSSET CRACKED. AMES NR 136876-0100-0169SDR SWIA202162518None · corrodedGUSSETT LOCATED AT APPROXIMATELY WL71, FS280 CROSSBEAM, AND LBL11 IS CORRODED (C-CHECK RO 11/10/2021) REMOVED AND REPLACED WITH NEW GUSSETT AT APPROX. WL 71.00 FS280.00 LBL11.00. REF CRJ 700 SRM 51-42-06-001-001-A01, DRAWING # CC670-33052 REV -G COMPLIEDSDR SCNA20211028092None · noneCORROSION FOUND ON SHEAR WEB @STA. 986.5, RBL 44, WL 208. CORROSION FOUND TO BE OUT OF LIMITS @ STA. 986.5, RBL 44, WL 208 PER SRM HAS NO LIMITS. MACHINED REPLACEMENT SHEER WEB PER PO 839525-SCA. LOCATED AND DRILLED REPLACEMENT SHEAR WEB PER SRM 51-40-05-0G-0 SDR JJBA20211011042None · noneCORROSION ON ANGLE AT CARGO DOOR CUTOUT STA X22010.2 FWD FRAME LOWER BETWEEN STRG 16L AND STRG 17L COMMON TO FUSELAGE SKIN. REPAIRED CARGO DOOR CUTOUT STA X22010.2 FWD FRAME LOWER ANGLE SEGMENT SHEAR CLIP AT FRAME 65 BETWEEN S15L AND S18LSDR MK1Y20211011014None · noneSCRATCHES IN EXTERNALS FUSELAGE SKIN AMONG FASTENERS AREA, IN STA 1368, 0.4'' ABOVE S-31R. MAINTENANCE CLEANED DAMAGED AREA IN ACCORDANCE WITH BOEING 767-300 SRM 51-10-02, AND REMOVED AN EXISTING FASTENER IN ACCORDANCE WITH BOEING 767-300 SRM 51-40-02.
NDT INSDR MK1Y20211011013None · noneM0079:
SCRATCHES IN EXTERNALS FUSELAGE SKIN AMONG FASTENERS AREA, IN STA 1354, S-29R. MAINTENANCE CLEANED DAMAGED AREA IN ACCORDANCE WITH BOEING 767-300 SRM 51-10-02, AND REMOVED AN EXISTING FASTENER IN ACCORDANCE WITH BOEING 767-300 SRM 51-40-02.
NDT INSPECSDR MK1Y20211011012None · none: STA 1307 - STA 1373, STR-22L - STR-26L:
DURING TRIMMING OF STRINGER 25L FOR PRESSURE RELIEF VALVE INSTALLATION IN
DATUM AREA AS PER DWG 371-21-30-C1104 REQUIREMENTS, EXTERNAL FUSELAGE
SKIN WAS DAMAGED IN TWO LOCATIONS AS SHOWN IN RFTA 02780-0015.SDR MK1Y20211011011None · noneSATCOM ANTENNA, STA 977 TO STA 1043, STR 2L TO STR 2R: AS PER COSTUMER REQUEST, HIGH GAIN SATCOM ANTENNA WAS REMOVED FROM THE AIRCRAFT. THE ANTENNA WAS MOUNTED TO AN ADAPTER, WHICH LOCATED BETWEEN STA 999 TO STA 1043, AND BETWEEN STR 1L TO STR 1R. ON FUSELAGE SDR MK1Y20211011006None · nonePROBLEM DESCRIPTION: EXTERNAL FUSELAGE SKIN – STA 1417 – STA 1426, S-29L – S-34L:
DURING CONVERSION AT IAI, MAINTENANCE HAVE FOUND SCRATCHES AT BLENDED AREA IN EXTERNAL FUSELAGE SKIN, AMONG FASTENERS AREA. THE DAMAGED AREA IS LOCATED IN THE FOLLOWING LOCATIOSDR MK1Y20211011005None · noneDENT EXTERNAL FUSELAGE SKIN – STA 1233, COMMON TO S-27R: STA 1233, 0.14” ABOVE S-27R DENT A/Y RATIO EQUALS TO 24.6 (A=1.77, Y=0.072) GAGE: 0210” CLAD 2024-T3 (MACHINED TO 0.056”).SDR DALA2021101506362None · none(LOG 1979908) DURING INSPECTION FOUND DENT, FUSELAGE SKIN, LOCATED STA 727J+2.3" BY 2.8" BELOW S-2L. PERMANENT REPAIR ACCOMPLISHMENT COMPLETED PER ERA 594805-14 REV "ORIGINAL" , AND PRI 594805 REV"0".SDR MK1Y20211011004None · noneEXTERNAL FUSELAGE SKIN – STA 1216, COMMON TO S-31: DURING CONVERSION AT IAI, MAINTENANCE HAVE FOUND DENT IN EXTERNAL FUSELAGE SKIN, COMMON TO DOORS CUTOUTS, LAP SPLICE, BUTT SPLICE AND AMONG FASTENERS AREA. DENT A/Y RATIO EQUALS TO 26 (A=1.25, Y=0.048).SDR MK1Y20211011003None · noneEXTERNAL FUSELAGE SKIN – STA 1349.5, BETWEEN S-23R AND S-24R, AND STA 1363.5, S-26R: DURING CONVERSUON AT IAI, MAINTENANCE HAVE FOUND TWO (2) EXISTING BLEND OUT ZONES IN EXTERNAL FUSELAGE SKIN AMONG FASTENER AREAS.
M0383: STA 1349.5, BETWEEN S-23R AND S-24R. SDR 2A6R2021101162002Floor Skin · corrodedFUSELAGE - COCKPIT FLOOR - OUTER SKIN DELAMINATION AND CORROSION DAMAGE - DAMAGE TO THE COCKPIT FLOOR (PN: L533M1013107) IN THE FORM OF AN AREA OF DELAMINATION ON THE UPPER SKIN PANEL MEASURED TO BE APPROXIMATELY 3.0” X 1.25”, AS WELL AS AN AREA OF CORROSION SDR 2A6R2021101162001Frame · crackedFRAME 5 CRACK FOUND ON L/H FWD LOWER SIDE OF METRO BOX BEAM ASSY. CRACK LENGTH IS .75 INCHESSDR MK1Y20211011002None · noneEXTERNAL FUSELAGE SKIN – STA 1540, BETWEEN S-25R AND S-26R: MAINTENANCE HAVE FOUND SCRATCHES AT BLENDED AREA IN EXTERNAL FUSELAGE SKIN AMONG FASTENERS AREA. MAINTENANCE CLEANED DAMAGED AREA AND REMOVED AN EXISTING FASTENER WHICH INTERFERED BLEND OUT PROCEDURE.SDR MK1Y20211011001None · noneDENT WITH CREASE BEYOND SRM LIMITS IN EXTERNAL FUSELAGE SKIN AT STA 1373, 3.5” ABOVE S-29R. THE DAMAGE IS COMMON TO CUTOUT AND IS LOCATED IN FASTENERS AREA. DENT A/Y=25. MAINTENANCE ALSO FOUND AN NON-STANDARD SHEAR TIE INSTALLED IN THE INNER SKIN SIDE OF THE DSDR SWIA202163479None · dented*DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS1015.00 €“ 1047.00, STGR 20L €“ 19L (C-CHECK RO 1/7/2022) REPAIRED DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS1015.00 €“ 1047.00, STGR 20L €“ 19L REF REO 670-53-61-1993 REV-A, DATED 2021-12-28. COMPLIED WITH 5SDR CALA2021101101847Beam · corroded(A3NB-25-3-6221) FLOOR BEAM -Y765 BETWEEN FR 68/70 HAS CORROSION DOT 52-33 () REMOVED AND REPLACED FLOOR BEAM P/N D5347209200000 BETWEEN FR 68 /70 IAW SRM 51-42-11.SDR CALA2021101101846Intercostal · noneDURING ROTO PROBE INSPECTION OF THE LH DOOR STOP FITTING #7 AT F R16, CRACK INDICATION WAS NOTED IN LOWER I/B HOLE FWD LAST TWO L AYERS, REPAIR BEFORE NEXT FLIGHT. (AD2019-20-10)SDR JR2R20211010403Web · corrodedRH FLOOR WEB, FR87 - FR88 RBL12 - 40 CORRODED OUT OF LIMITSSDR JR2R20211010406Support · corrodedFLOOR SUPPORT RBL 28 FR87 CORRODED OUT OF LIMITSSDR JR2R20211010316Angle · corrodedLH WHEEL WELL STUB ANGLE CRACKED AT FR52SDR SWIA202162917None · cracked* CO-PILOT SIDE WINDSHIELD OB POST LOWER AFT MOUNTING BRACKET HAS A SUSPECTED CRACK (FLAGGED). (C-CHECK RO 11-27-21) REMOVED AND REPLACED LOWER AFT MOUNTING BRACKET ON CO-PILOT SIDE WINDSHIELD OB POST REF. CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-33SDR SWIA202162916None · cracked* PILOT SIDE WINDSHIELD OB POST LOWER AFT MOUNTING BRACKET HAS A SUSPECTED CRACK (FLAGGED). (C-CHECK RO 11-27-21) REMOVED AND REPLACED LOWER AFT MOUNTING BRACKET ON PILOT SIDE WINDSHIELD OB POST REF. CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-33055 RESDR SWIA202161624None · damagedFUSELAGE SKIN HAS DAMAGE FROM LOW PRESSURE COVER, APPROX. BETWEEN FS1015.00 - FS1040.00 AND BETWEEN STRINGERS 27R - 24R. (FILED CLOSED) PERFORMED REPAIR OF THE DISCREPANT AREA (FUSELAGE SKIN APPROX. BETWEEN FS1015.00 - FS1040.00 AND BETWEEN STRINGERS 27RSDR MASA20211011476None · noneTHE FLOOR BEAM BETWEEN FS661+16 & FS661+42 AT RBL 9.0 WAS FOUND TO HAVE CORROSION DAMAGE ON THE UPPER FLANGE, WHICH WAS THEN BLENDED. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-43 , FIGURE 53-31-43-991-801, ITEM 7, EA 83-2021-046.SDR R61A2021102700839None · corrodedFWD CARGO, SHEAR CLIP FOUND CORRODED AT FR 16 BETWEEN STR 28-27R. REMOVED AND REPLACED SHEAR CLIP IN FWD CARGO AT FR 16 BETWEEN STR 27-28R IAW EMBRAER 170-175 SRM 51-41-01 AND 51-41-02.SDR R61A2021102700835None · corrodedFWD CARGO SHEAR CLIP AT FR 17 BETWEEN STR 28-27R. FWD CARGO SHEAR CLIP AT FR 17 BETWEEN STR 28-27R REPLACED IAW SRM 51-41-02.SDR IPXA2021101274853None · noneINSPECTION TYPE:18FODAMAGE ON MAIN DECK FLOOR PANEL ASSY (P/N : 144U5803-28) BETWEEN STA 1235 AND STA 1265 , AND BETWEEN RBL 98.58 AND RBL 117.40 , PANEL NO. 242AGFABRICATE A NEW FLOOR PANEL I.A.W UPS EO B747-5320-42648-ASDR MASA20211011479None · damagedLH CORE COWL REINFORCING LATCH WAS FOUND TO HAVE WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-01-001-002-A01, EA 12-2021-251.
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