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 MASA20220329150None · corrodedWEAR ON SEVERAL PLACES ON LEFT FLOOR SEAT RAIL FS364-FS485 BL 27.0 AT PAX CABIN
LEFT FLOOR SEAT RAIL FS364-FS485 BL 27.0 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49SDR MASA20220329147None · corrodedCORROSION ON FLOOR BEAM 9LBL IN STA. FS= 985 TO FS= 1088 AT AFT BAGGAGE BAY |CORRECTIVE ACTION: SECTION FLOOR BEAM 9LBL IN STA. FS= 985 TO FS= 1088 AT AFT BAGGAGE BAY WAS REPLACED PER CRJ-900 SRM 53-00-41-201-001-A03.SDR MASA20220329137None · corrodedCORROSION ON LEFT SIDE SEAT RAIL FS661+14-FS672 AT PAX CABIN | LEFT SIDE SEAT RAIL FS661+14-FS672 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49.SDR MASA20220329136None · corrodedCORROSION ON LEFT SIDE SEAT RAIL FS549-FS573 AT PAX CABIN | LEFT SIDE SEAT RAIL FS549-FS573 WAS REPLACED PER CRJ-900 AMM 53-00-49SDR MASA20220329135None · wornWEAR ON LEFT SIDE SEAT RAIL FS483-FS517 AT PAX CABIN | LEFT SIDE SEAT RAIL FS483-FS573 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49SDR MASA20220329134None · corrodedCORROSION ON RIGHT SIDE SEAT RAIL FS661+14-FS672 AT PAX CABIN.
RIGHT SIDE SEAT RAIL FS661+14-FS672 AT PAX CABIN WAS REPLACED PER CRJ-900 AMM 53-00-49.SDR MASA20220329133None · corrodedCORROSION ON RIGHT SIDE SEAT RAIL FS483-FS573 AT PAX CABIN | SEAT RAIL RIGHT SIDE FS483 - FS573 AT PAX CABIN WAS REPLACED PER AMM 53-00-49SDR MASA20220329132None · corrodedCORROSION ON LEFT FLOOR SEAT RAIL FS661+32-FS693 BL 9.0 AT PAX CABIN | LEFT FLOOR SEAT RAIL FS661+32-FS677 BL 9.0 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49SDR MASA20220329131None · wornWEAR ON SEVERAL PLACES ON LEFT SIDE SEAT RAIL FS379-FS483 AT PAX CABIN.
LEFT SIDE SEAT RAIL FS379-FS483 WAS INSTALLED PER CRJ-900 AMM 53-00-49.SDR MASA20220329129None · corrodedCORROSION ON LEFT SIDE SEAT RAIL FS905-FS969 AT PAX CABIN.
LEFT SIDE SEAT RAIL FS905-FS969 AT PAX CABIN WAS REPLACED PER.CRJ-900 SRM 53-00-49.SDR MASA20220329128None · corrodedCORROSION ON LEFT SIDE SEAT RAIL FS847+14-FS905 AT PAX CABIN. | LEFT SIDE SEAT RAIL FS847+14-FS905 WAS REPLACED PER CRJ/900 AMM 53-00-49.SDR MASA20220329127None · corrodedCORROSION ON LEFT SIDE SEAT RAIL FS785.15-FS847+14 AT PAX CABIN
LEFT SIDE SEAT RAIL FS785.15 TO FS847+14 PAX CABIN WAS REPLACED PER CRJ-900 AMM 53-00-49SDR MASA20220329126None · corrodedCORROSION ON RIGHT SIDE SEAT RAIL FS847+14-FS868 AT PAX CABIN
NEW RIGHT SIDE SEAT RAIL FS847+14-FS868 AT PAX CABIN WAS REPLACED PER.CRJ-900 SRM 53-00-49SDR MASA20220329125None · corrodedCORROSION ON RIGHT SIDE SEAT RAIL FS744.15-FS761.85 AT PAX CABIN.
RIGHT SIDE SEAT RAIL FS744.15-FS761.85 AT PAX CABIN WAS REPLACED PER CRJ-900 AMM 53-00-49SDR MASA20220329124None · corrodedCORROSION ON RIGHT SIDE SEAT RAIL FS672-FS720.85 AT PAX CABIN| RIGHT SIDE SEAT RAIL FS672-FS722 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49SDR MASA20220329123Angle · corrodedCORROSION ON MID CAP ANGLE OF L 1 SURROUND STRUCTURE WAS FOUND. CORRECTIVE ACTION: MID CAP ANGLE OF L 1 SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01SDR HNAA2021111500554None · noneE885848 - PILOTS BULKHEAD UPPER PIN OUTBD HOLE IS OBLONG. (ON THE REINFORCING STRUCTURE DOUBLER).... REMOVED UNSERVICEABLE PREVIOUS REPAIR AND INSTALLED SERVICEABLE REPAIR FOR PILOTS BULKHEAD UPPER PIN OUTBOARD ( ON THE REINFORCING STRUCTURE) IAW EO1-53-21-030SDR HNAA2021110900546Not Reported · not reportedE885868 - AFT FLOOR SUPPORT CORRODED JUST INSIDE THE PAX DOOR ... RAR AFT FLOOR SUPPORT JUST INSIDE THE PAX DOOR IAW EMB145 SRM 51-40-02.SDR HNAA2021110900545Not Reported · not reportedE885867 - FORWARD FLOOR SUPPORT CORRODED JUST INSIDE THE PAX DOOR ... RAR FORWARD FLOOR SUPPORT JUST INSIDE PAX DOOR IAW EMB145 SRM 51-40-02SDR HNAA2021110900544Not Reported · not reportedE885864 - RCENTER ISLE CROSSBEAM CORRODED AND CHAFED AT FRAME 20 ... REMOVED CORRODED AND CHAFED CENTER ISLE CROSSBEAM AT FR 20 AND INSTALLED SERVICEABLE CROSSBEAM IAW EMB 145 SRM 51-40-02.SDR HNAA2021110900543Not Reported · not reportedE885825 - R/H FLOOR SILLS #2 ARE CORRODED ... RAR R/H FLOOR SILLS #2 IAW EMB 145 SRM 51-40-02.SDR HNAA2021110900542Not Reported · not reportedE885824 - L/H FLOOR SILLS #4 ARE CORRODED ... RAR L/H FLOOR SILL #4 IAW EMB 145 SRM 51-40-02.SDR HNAA2021110900541Not Reported · not reportedE885821 - L/H FLOOR SILLS #2 ARE CORRODED ... RAR L/H FLOOR SILL #2 IAW EMB 145 SRM 51-40-02SDR HNAA2021110900540Not Reported · not reportedE885809 - R/H LOWER SEAT TRACK SUPPORTS #5 ARE CORRODED ... REMOVED AND INSTALLED SERVICEABLE R/H LOWER SEAT TRACK SUPPORT IAW EMB 145 SRM 51-40-02.SDR HNAA2021110900539Not Reported · not reportedE885807 - R/H LOWER SEAT TRACK SUPPORTS #3 ARE CORRODED ... RAR R/H LOWER SEAT TRACK SUPPORT #3 IAW EMB 145 SRM 51-20-03, AND 51-40-- 02. RESTORED TO ORIGINAL FINISH IAW EMB 145 CPM 51-21-06, AND PIEDMONT BULLETIN #51-02.SDR HNAA2021110900538Not Reported · not reportedE885802 - L/H LOWER SEAT TRACK SUPPORTS #4 ARE CORRODED ... RAR LH LOWER SEAT TRACK SUPPORT #4IAW EMB 145 SRM 51-20-03,51-40-02.RESTORED TO ORIGINAL FINNISH IAW EMB 145 CPM 51-21-06,PIEDMONT BULLETIN #51-02.SDR HNAA2021110900537Not Reported · not reportedE885801 - L/H LOWER SEAT TRACK SUPPORTS #3 ARE CORRODED ... RAR L/H LOWER SEAT TRACK SUPPORT #3 IAW EMB 145 SRM 51-20-03,51-40-02,- RESTORED TO ORIGINAL FINISH IAW EMB 145 CPM 51-21-06,PIEDMONT BULLETIN #51-02.SDR HNAA2021110900536None · noneE885795 - L/H LOWER SEAT TRACK # 1 ARE CORRODED ... BLENDED L/H LOWER SEAT TRACK # 1 DAMAGED AND CORRODED AREAS AND FOUND AREAS TO BE OUT OF ALLOWABLE LIMITS IAW EMB-145 SRM 53-- 00-11 EASI 8639. REMOVED AND REPLACED LH LOWER SEAT TRACK #1 IAW EMB 145 AMM 53-0SDR HNAA2021110900535None · noneE885794 - L/H UPPER SEAT TRACK # 5 ARE CORRODED ... BLENDED L/H UPPER SEAT TRACK #5 AND FOUND REMAINING THICKNESS TO BE BEYOND LIMITS IAW EMB145 SRM 53-00-11, ITEM 2. REMOVED AND REPLACED LH UPPER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06,SDR HNAA2021110900534None · noneE885791 - L/H UPPER SEAT TRACK # 1 ARE CORRODED ... REMOVED AND REPLACED L/H UPPER SEAT TRACK # 1 IAW EMB 145 AMM 53-01-06SDR HNAA2021110900533None · noneE885790 - R/H UPPER SEAT TRACK #4 ARE CORRODED ... BEGAN BLENDING AND FOUND R/H UPPER SEAT TRACK # 4 TO BE BEYOND LIMITS IAW EMB145 SRM 53-00-11, ITEM 2. (REQUIRES PART REPLACEMENT). REMOVED AND REPLACED RH UPPER SEAT TRACK #4 IAW EMB 145 AMM 53-01-06SDR R61A2021110200846Track · corrodedWHILE AC WAS ION FOR HVY CK FOUND CENTER FUSELAGE 1 CABIN FLOOR STRUCTURE FR23 TO FR 34 LBL 11 SEAT TRACK CORRODED FROM FR 29 TO FR 34. MX REPLACED SEAT TRACK PN 170-67358-009 IAW SRM 51-41-02, 51-43-02, 51-43-01. SEE AAR NRC# 4500976-1000-0113. AC REMAINS INSDR SCNA20211028094None · noneCABIN FLOOR STRUCTURE, SHEAR WEB STA. 1016 TO PRESSURE BULKHEAD RBL6 CORRODED. PERFORMED BLEND REPAIR IAW ATS ER 21-02631 REV IRSDR A6WA202110157934Skin · dentedMULTIPLE DENTS AND GOUGES ON AFT FUSELAGE SKIN BTW FS589.00 Ï¿½ FS605.00 AND STR24R Ï¿½ STR26R. DRESSED 4 DENTS AND BLENDED 22 GOUGES ON AFT FUSELAGE SKIN BTW FS589.00 Ï¿½ FS605.00 AND STR24R Ï¿½ STR26R. SKIN PN 601R35005. POST DRESS DENT DIMENSIONS P1 - L=SDR CALA2021101801898None · corrodedCORROSION ON STRINGER AT AFT FUSELAGE OUTFLOW VALVE CUT-OUT AREA , FR65 STRINGER 31R. REMOVED AND INSTALLED OUTFLOW VALVE IAW AMM 21-31-51 OPS TEST GO OD IAW AMM 21-31-00-710. BLENDED AREA ON S31R FR65 IAW SRM 51-74 -00 L=4.110" W=0.940" ORIGINAL THICKNESS 0.1SDR SWIA202162948None · corrodedTHE GALLEY #1 HAS A CORRODED DOUBLER BEHIND THE FWD EDGE/INBD FLOOR FITTING. (C-CHECK RO 11-27-21) REPLACED THE GALLEY #1'S DOUBLER BEHIND THE FWD EDGE/INBD FLOOR FITTING (P/N=9331071-1 AND 8EA SCREWS P/N=NAS517-3-1) WITH A SERVICABLE FITTING REFERENCING SDR EE4Y2021112614435Stringer · corrodedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT CENTER FUSELAGE III, BETWEEN FR85 AND FR86 THE STRINGER 23L WITH CORROSION ON HORIZONTAL FLANGE ONLY, THE DAMAGE
WAS REPAIRED INSTALLING REPAIR DOUBLER AS PER E.O. # COO-EO-2021-14157 R00 - WOA1K276 ÍTEM 1-86, SDR IXXA2021112201HBracket · corrodedVERTICAL STANCHION BASE IS CORRODED AT STA 1087 LBL 26. AMES NR 136876-0100-0258SDR HNAA2021110900528None · noneE885189 LAV. R/H FLOOR GUSSET IS CORRODED ... REMOVED AND REPLACED LAV. R/H FLOOR GUSSET IAW EMB 145 SRM 51-40-02SDR SCNA20211028095None · noneCABIN FLOOR STRUCTURE, STIFFENER STA. 990 RBL42 CORRODED. REMOVED AND REPLACED SUPPORT STIFFENER STA 990 RBL 32-44 IAW B737 SRM 51-40-02-0G-0 AND DWG 14A5700.SDR JJBA20211014049None · noneMAIN CABIN - INTERNAL - FASTENERS HAVE CORROSION ON SHEAR TIE - AT FWD SIDE OF LH FR 51 BETWEEN STGR 18 AND STGR 19. REMOVED AND REPLACED SHEAR CLIP AT FRAME 51 LH BETWEEN STRINGER 18 AND STRINGER 19.SDR A6WA202110147933Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS605.00 Ï¿½ FS621.00 AND S21L TO S23L. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 4.200Ï¿½ X W = 0.800Ï¿½ X D = 0.008Ï¿½. PERFORMED HFEC WSDR A6WA202110147931Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS672.00 Ï¿½ FS682.00 AND S22-L TO S23L. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS672.00 Ï¿½ FS682.00 AND S22-L TO S23L. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 0.150Ï¿½ X W = 0.100Ï¿½ X D = 0.004Ï¿½. PERFORMED HFECSDR A6WA202110147932Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 0.600Ï¿½ X W = 0.250Ï¿½ X D = 0.006Ï¿½. PERFORMED HFEC WSDR 2A6D2021101409003None · chafedRING FRAME CHAFING DAMAGE AT APPROXIMATELY STA 4918, WL 1759, AND BL 320L MEASURING 0.92” LONG X 0.08” WIDE AND IS 0.008” AT ITS DEEPESTSDR CALA2021101401882Panel · missingPDA 3 GENERATED PDA CATEGORY 3 LOG REF TO LOG PAGE 7230526 PANEL 192 FB MISSING FASTENERS-IAW GMM 02-30-95. CATEGORY 3: THE TECHNICIAN DOCUMENTS AND REPORTS THIS OCCURRENCE THROUGH THE AIRCRAFT LOGBOOK. THE CORRECTIVE ACTION DOCUMENTED IN THE AIRCRAFT LOGBOOK SDR CALA2021101401881None · 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) REPLACED L/H DOOR STOP #7 FITTING INTERCOSTAL BY C/W EC/RA 5311- 02649, REPLACEMESDR CALA2021101401862None · noneBIRD STRIKE. INSPECTION REQUIRED PER AMM. ACCOMPLISHED BIRD STRIKE INSPECTION IAW AMM TASK 5-51-18-210-801. BIRD STRIKE IS LIMITED TO RADOME AREA. CLEANED AREA AND INSPECTED FOR DAMAGE, NO DAMAGE NOTED AMM TASK REQUIRES RADOME INTERNAL INSPECTION STEP 2. A. (2SDR MASA20220329139None · crackedCRACK ON FLOOR BE AM 12 RBL IN STA. FS= 280 CPIL | CORRECTIVE ACTION : FLOOR BEAM SECTION 12 RBL BTW. FS STA= 265 AND FS STA= 280 CPIL WAS REPLACED PER CRJ/900 SRM 51-40-11-001-001-A01 AND CRJ-900 SRM 51-42-20-001-001- A01SDR MASA20220329120None · crackedCRACK IN UPPER WEB OF INTERNAL ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMP. CRACK IN UPPER WEB OF INTERNAL ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMP WAS REPAIR PER CRJ-900 SRM 53-11-43-201-001-A01
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