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 IPXA2021083173380Unknown · noiseINSPECTION TYPE:N/ALOUD LOW FREQUENCY NOISE(SUSPECT AIR LEAK)COMINE FROM AREA BELOW FLT DECK.NOISE STARTED AT 12100FT AND THEN GRADUALLY WENT AWAY BETWEEN 20000FT & 27000FT.PRESSURIZETION WORKED NORMALLY.DETAIL CKED MAIN E/E COMPT INSIDE AREA,MAIN E/E COMPT DOSDR SWIA202162641None · corrodedL/H WS 53.60 BATT RIB, INBOARD ANGLE IS CORRODED COMMON TO CANNON PLUGS J411 AND J413 ATTCAHING HARDWARE. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH WS 53.60 BATT RIB ANGLES IAW CRJ 200 SRM 51-42-21 AND 51-42-06.SDR SWIA202162038None · crackedCRACK FOUND AT ANGLE ASSY WL 72.10 BETWEEM FS280 AND FS265 (C-CHECK RO 10/29/2021) REMOVED AND REPLACED ANGLE ASSY P/N CC670-33199-4 REF DWG NO. CC670-33052 REV -G, CRJ700 SRM51-42-06-001-001-A01 REV 38 JUL 25/2020. SEE CONTINUE CARD FOR DETAILS. COMPLISDR SWIA202162298None · corrodedG1 - FWD OTBD MOUNT IS CORRODED (C-CHECK RO 11/04/2021) REPLACED 1 EA G1 FWD OTBD MOUNT WITH NEW. REF CRJ-900 SRM 51-41-02-001-001-A01SDR SWIA202162297None · corrodedG1 - INBD (AT FLIGHT COMPARTMENT DOOR BRACKET) MOUNT IS CORRODED (C-CHECK RO 11/04/2021) REPLACED 1 EA G1 FWD INBD MOUNT WITH NEW. REF CRJ-900 SRM 51-41-02-001-001-A01SDR SWIA202162296None · corrodedG1 - AFT INBD MOUNT IS CORRODED (C-CHECK RO 11/04/2021) REPLACED 1 EA G1 AFT INBD MOUNT WITH NEW. REF CRJ-900 SRM 51-41-02-001-001-A01SDR SWIA202162573None · dentedDURING NDT AND VISUAL INSPECTIONS OF THE FS 621.00 REAR PRESSURE BULKHEAD FOUND THERE TO BE SEVERAL CHAFES, DENTS, AND FAILED NDT INDICATIONS ON THE FWD FACE OF THE BULKHEAD.SEE CONTINUATION CARD FOR TYPE/LOCATION OF DAMAGE. (C-CHECK- RO 11/11/21) REMOVED SDR SWIA202162483None · dented* DENT ON EXTERIOR SKIN UNDER AFT CARGO DOOR PROTECTOR PLATE AT APROX. FS.1000.00 STR.18L (MARKED). (C-CHECK RO 11/10/2021) FOUND DENT OUT OF LIMITS DRESSED BACK DENTED SKIN AND INTERNAL DOUBLER TO INITIAL CONTOUR IAW REO 670-53-61-1971 REV -- DATED 2021-SDR SCNA20210927082None · noneCORROSION FLOOR TO SIDEWALL SUPPORT (ZEE CHANNEL) BS 500G +11 TO 500I RBL 25. CORROSION ON SIDEPLATE STA. 500G-500I RBL 25 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE IAW SRM 53-00-53-1A-2 DETAIL "D" REV 73. REMOVED AND REPLACED SIDEPLATE WITH SDR SWIA202162447None · damagedPAX DOOR OUTER SKIN IS DAMAGED AT AREA FWD AND AFT OF PIANO HINGE (C-CHECK RO 11/5/2021) REPAIRED PAX DOOR OUTER SKIN DAMAGE REF REO 670-52-11-1250 REV -- DATED 2021-09-15SDR SWIA202161305None · corrodedFS319.70, STGR 18L TO 21L HAS CORROSION PRESENT (C-CHECK RO 9/27/2021) FRAME SECTOR P/N SH670-31891-3S BETWEEN STGR 18L AND 21L AT F.S.319.70 INSTALLED PER CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DRAWING #SH670-SDR EE4Y2023031017362Pressure Plate · crackedWHILE PERFORMING INSPECTION AND REPAIR PER ALLEGIANT E.O. E5331-0007 R3 RELATED TO AD2018-06-04, PRESSURE PLATE FASTENER HOLES WERE FOUND CRACKED BETWEEN FR35-FR36 UNDER LONGITUDINAL BEAM. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER E.O. E5331-00SDR A6WA202110017892Skin · dentedDENT WITH CREASE ON AFT FUSELAGE SKIN AT FS634.00 AND S25L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN AT FS634.00 AND S25L. DENT DIMENSION L = 0.500Ï¿½ X W = 0.400Ï¿½ X D = 0.018Ï¿½. CUTOUT DIMENSIONS L= 1.600Ï¿½ SDR IPXA2021093074429Floor Panel · damagedINSPECTION TYPE:SEGPNL 241XCF DAMAGEDFABBED PER SREP B757-5320-9692-KSDR SWIA202161129None · crackedFLOOR BEAM RBL 12.0 AT FS 232.0 IS CRACKED AT BOTTOM SIDE. (C-CHECK RO 9/21/2021) PERFORMED PERMANENT REPAIR TO RBL12.00 FLOOR BEAM IN REF REO 670-53-11-1727, REV --, DATED 2021-09-07. ALL STEPS COMPLETED AT THIS TIME. ST 51-900-1002-SKY COMPLETE. SEE CSDR SWIA202162466None · chafed*AFT WASTE WATER SYSTEM, CANNON PLUG DOUBLER HAS CHAFFING (MARKED) (C-CHECK RO 11/10/2021) REPLACED AFT LAV WASTE WATER SYSTEM, CANNON PLUG DOUBLER / SACRIFICIAL PLATE WITH NEW PN: SH670-37567-1 PO: T62435, REF DWG # SH670-37560, REV -E. PERFORMED PRESSURSDR SWIA202162465None · corroded*LH EXTERIOR FUSELAGE AFT WATER SYSTEM FILL/DRAIN VALVE HANDLE BRACKET (LOWER SIDE) HAS CORROSION PRESENT (MARKED) (C-CHECK RO 11/10/2021) REPLACED THE AFT WATER SYSTEM FILL/DRAIN VALVE HANDLE BRACKET DOUBLER REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG#.SDR SWIA202162359None · corrodedGALLEY SERVICE DOOR SURROUND: 'KICK ANGLE" ON THE PROTECTOR, WEB FLOOR FWD-MID IS CORROSION FS 327 (C-CHECK RO 11-05-2021) REPLACED ANGLES PN: SH670-31982-1 AND SH670-32040-3 WITH NEW FROM STOCK REF CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01SDR SWIA202164024None · dentedTHERE'S DENT ON LOWER SKIN AT FS 589 BETWEEN STGR 26, 25 AND STGER 24 (C CHECK RO 1/20/22) REPAIRED FUSELAGE SKIN BETWEEN FS574.00 - FS621.00 STR24R- 24L. IAW REO601R-53-61-7719 REV-- DATED 2021-10-16 AND CRJ200 SRM 53-00-31. AIRCRAFT NOT TO BE OPERATED BSDR SWIA202162408None · corroded*AREAS OF CORROSION ON LH OVERWING EMER EXIT SURROUND LOWER INNER STRAP. AREAS MARKED. (C-CHECK RO 11/5/2021) REPAIRED LEFTHAND OVERWING EMERGENCY EXIT SURROUND LOWER INNER STRAP IAW REO 670-53-41-545 REV -- DATE 2021-09-15 STEPS.1-5 ( SEE CONTINUATION SDR 2022FA0000581None · noneA CRACK LIKE INDICATION WAS FOUND ON LEFT MAIN SWIVEL PIN. THE IDICATION WAS 1/2" LONG IN THE AREA OF INTEREST. CRACK WAS FOUND WITH FLUORESCENT MAGNETIC PARTICLE TESTING. INSPECTION WAS DONE PER ASTM E1444 AS REQUESTED BY CLIENT. AD 97-01-01 R1 PIPERSDR SWIA202161855None · gougedGOUGES IN FUSELAGE EXTERNAL SKIN; FS913.00- FS927.00, STRINGER 27. (C-CHECK RO 10/22/2021) BLENDED GOUGES AT STGR 27 BETWEEN FS913 TO FS927 REF REO 670-53-00-290 REV - F DATED 2019/04/26 LEAK CHECK GOOD.SDR SWIA202162568Seal · corrodedL/H EMERGENCY EXIT DOOR FWD AND AFT LOWER INTERNAL CORNERS OF DOOR STRUCTURE IS CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED L/H EMERGENCY EXIT FORWARD AND AFT LOWER INTERNAL BRACKETS I.A.W. BOMBARDIER CRJ 200 SRM 51-42-11 AND 51-42-21. COMPLETED TSDR SWIA202162389None · corroded*EVIDENCE OF CORROSION EXIST ON SIDE SEAT RAIL STRUCTURE @ STRGR 15R BETWEEN FS785.00 & FS813.00 (C-CHECK RO 11/5/2021) REMOVED CORROSION FROM ANGLE BENEATH RH SIDE SEAT RAIL AND RETAINER AT FS785-813 REF CRJ700 SRM 51-21-06-001-001-A01. EVALUATED AND FSDR SWIA202161721None · corroded* AFT WING TO BODY FAIRING 195BB HAS MULTIPLE CORRODED DOME NUTS A/C SIDE (MARKED) (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED NEW AFT WING TO BODY FAIRING NUTPLATES REF CRJ-200-SRM 51-42-06 AND INSTALLED ALTERNATE FASTENERS FOR THE GROUND AIR CONDITISDR SWIA202161718None · bent* LH TRU BAY DOOR AFT SEAL LANDING IS BENT/DEFORMED (C-CHECK RO 10/8/2021) REMOVED AND REPLACED THE LH TRU BAY DOOR AFT SEAL LANDING WITH 1EA. NEW PART REF. CRJ200 SRM 51-42-06 & DWG 600-34011 REV -K. COMPLIED WITH 51-900-1003-SKY.SDR SWIA202161128None · crackedUPON REMOVAL OF RIVETS ON FWD RH UPPER SKIN BETWEEN FS 169 AND FS 172 FOUND FASTENER HOLE CRACKED (C-CHECK RO 9/21/2021) REMOVED AND REPLACED FWD RH UPPER SKIN P/N CC670-33107-2 PO# T000062212/1 IN REF DWG CC670-33040, REV G, CRJ700 SRM 51-42-06-001-00SDR SWIA202162345None · corroded*FRAME, FS517: NOTED CORROSION BETWEEN STGR 19L AND STGR 18L (MARKED). (C-CHECK RO 11/5/2021) INSTALLED NEW FRAME STUB AT FS517.00 BETWEEN STGR 19L-18L IAW CRJ 700 SRM 51-42-06-001-001-A01,DWG SH670-33100 REV K- AND 51-42-21-001-001-A01. PRESSURE CHECK SDR SWIA202162332None · corroded* CORROSION FOUND JUST AFT OF FS 1031.00 ON FUSELAGE SKIN JUST LEFT OF STR 27 LOOKING FWD.(MARKED) (C-CHECK RO 11/5/2021) BLENDED CORROSION ON INTERIOR AND EXTERIOR FUSELAGE SKIN AT FS1031.00 JUST AFT OF STGR27 IAW REF DRAWING MM670-35007 REV. V, CRJ 70SDR EVCA08192021Bulkhead · crackedWHILE DOING THE 300 HOUR PERIODIC INSPECTIONS WE NOTICED WORKING RIVETS AT STA. 145. WE OPENED ON THE BULKHEAD PANELS AND USED A BORESCOPE AND FOUND A CRACK ON THE RH 145 BULKHEAD FLANGE ATTACHED TO THE ROOF.SDR SWIA202161300None · corrodedMAIN AVIONICS BAY STGR 21L BACK-UP SILL CORRODED BETWEEN FS310.00- FS333.00 (C-CHECK RO 9/27/2021) BLENDED CORROSION ON F.S 310.00 TO 333.3 STGR 21 L BACK UP SILL, 100% MATERIAL LOSS. REMOVED AND INSTALLED NEW BACK-UP SILL ON STRG 21L BETWEEN F.S.310.0SDR R61A2021090300689Shear Panel · corrodedINTERNAL FUSELAGE, AFT GALLEY FLOOR SUPPORT STRUCTURE, R/H SHEAR PANEL AT FR 87-88 BETWEEN R/H SEAT TRACK AND STR 17AR FOUND CORRODED. REMOVED AND REPLACED IAW ERJ-175 SRM 51-42-01.SDR R61A2022091000550None · corrodedCORROSION SHEAR CLIP FRAME 88, STRINGER 25R-26R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 BETWEEN STGR 25R-26R REFER SRM 51-40-08. RESTORED SURFACE PROTECTION TO FASTENERS PER SRM 51-23-06.SDR SWIA202162323None · gouged* FUSELAGE SKIN GOUGED AFT SIDE OF PAX DOOR SURROUND AT AFT LOWER PIN FITTING (MARKED) (C-CHECK RO 11/5/2021) REPAIRED FUSELAGE SKIN AFT SIDE OF PAX DOOR SURROUND AT AFT LOWER PIN FITTING IAW REO 670-53-21-2135 REV -- DATE 2021-09-15 STEPS.1-3 (SEE CONTSDR SWIA202162321None · chafed* LH EMERGENCY EXIT DOOR SURROUND FORWARD UPPER CORNER CHAFFING (MARKED) (C-CHECK RO 11/5/2021) BLENDED CHAFF ON LH EMERGENCY EXIT DOOR SURROUND FORWARD UPPER CORNER IAW REF CRJ700 SRM 51-12-00-001-001-A01. WITHIN LIMITS COMPLIED WITH REO 670-53-41-558 SDR SWIA202162320None · chafed* RH EMERGENCY EXIT DOOR SURROUND FORWARD UPPER CORNER CHAFFING (MARKED) (C-CHECK RO 11/5/2021) BLENDED CHAFFING ON RH EMERGENCY EXIT DOOR SURROUND FORWARD UPPER CORNER AND RESTORED FINISH PER REO 670-53-41-544 REV -- DATE: 2021-09-11. COMPLIED WITH TASSDR SWIA202161354None · corrodedAFT WING TO BODY LH FRAME AT FS939 PN: SH670-39264-1 IS CORRODED AT BL0 (C-CHECK RO 9/27/2021) AFT WING TO BODY LH FRAME AT FS939 IAW CRJ700 SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS OF CRJ700 SRM 53-82-55-101-002-A01, INSTALLED NEW LH FRAME WSDR SWIA202161353None · corrodedAFT WING TO BODY RH SUPPORT ANGLE AT FS939 PN: SH670-39265-6 IS CORRODED (C-CHECK RO 9/27/2021) REMOVED AND REPLACED R/H SUPPORT ANGLE PN SH670-39265-6 PO# 10291-0009 PER CRJ 700 SRM 51-42-06-001-001-A01SDR SWIA202161352None · corrodedAFT WING TO BODY LH SUPPORT ANGLE AT FS939 PN: SH670-39265-5 IS CORRODED (C-CHECK RO 9/27/2021) REMOVED AND REPLACED L/H SUPPORT ANGLE PN SH670-39265-5 PO# 10291-0009/116 PER CRJ 700 SRM 51-42-06-001-001-A01SDR SWIA202161210None · corrodedCORROSION FOUND ON STRINGER 24R BETWEEN FS349.00 AND FS364.00. (C-CHECK RO 9-21-21) REMOVED AND REPLACED CORRODED STRINGER AT 24R BETWEEN FS349.00 AND FS364.00 WITH NEW FABRICATED STRINGER AND SPLICES USING NEW FASTENERS. REF CRJ700 SRM'S 53-00-03-201-001SDR SWIA202161209None · corrodedCORROSION FOUND ON R/H LONGERON BETWEEN FS333.00 AND FS349.00. (C-CHECK RO 9-21-21) REMOVED AND INSTALLED NEW R/H LONGERON BETWEEN FS333.00 AND FS349.00. REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-32050 REV J, COMPLSDR SWIA202161127None · corrodedRH FLOOR SILL FS280 TO FS319, ATTACH ANGLE STN 319.7, PART# SH670-31503-1 IS CORRODED. (C-CHECK RO 9/21/2021) CORROSION IS 100% THROUGH ATTACH ANGLE STN 319.7 ON RH FLOOR SILL FS280 TO FS319 AND IS OUT OF LIMITS REF CRJ700 SRM 53-00-00-101-001-A01. REMOSDR SWIA202161126None · corrodedRH FLOOR SILL FS280 TO FS319, SPLICE ANGLE STGR 17R, PART# SH670-31580-1 IS CORRODED. (C-CHECK RO 9/21/2021) CORROSION IS 100% THROUGH SPLICE ANGLE STGR 17R ON RH FLOOR SILL FS280 TO FS319 AND IS OUT OF LIMITS REF CRJ700 SRM 53-00-00-101-001-A01. REMOVESDR SWIA202162600None · corrodedF.S. 280 ANGLE IS CORRODED BETWEEN LBL9 AND RBL9. (C-CHECK- RO 11/11/21) REMOVED CORROSION ON FS 280 ANGLE BETWEEN LBL9 AND RBL 9 IAW CRJ 200 SRM 51-21-06.SDR A6WA202110217919Seat Track · corrodedCORROSION AT MULTIPLE LOCATIONS ON RH SIDEWALL SEAT TRACKS AT FS424, FS439, FS461, FS478, FS484, FS499, FS513, FS559+24 AND FS559+56. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED R/H SIDEWALL SEAT RAILS AT MULTIPLE CORROSION AT FS424, FS439, FS461, FS478, SDR A6WA202110217917Seat Track · corrodedCORROSION AT MULTIPLE LOCATIONS ON L/H SIDEWALL SEAT TRACKS AT FS424, FS439, FS461, FS473.15, FS484, FS499, FS513, FS529, FS544, FS559+8 AND FS559+64. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED L/H SIDEWALL SEAT RAILS AT MULTIPLE CORROSION AT FS 424, FS43SDR MASA20210915423Stringer · corrodedCORROSION ON STGR 26R BTW FS280-319 AT MAIN AVIONICS COMPARTMENT. STRINGER 26RH BTW FS=280 TO FS=333 WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01SDR SWIA202162590Bracket · crackedRH AND LH UPPER OBLEAK ANGLES ON FS.621.00 BULKHEAD AT STR. 14L AND 14R ARE CRACKED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH AND LH UPPER OBLEAK ANGLES ON FS.621.00 BULKHEAD AT STR. 14L AND 14R IAW CRJ 200 SRM 51-42-21-00SDR SWIA202162560None · dentedEXTERNAL FUSELAGE SKIN HAS SEVERAL DENTS/PRTRUDING DENTS FROM FS 574 TO FS 621, BETWEEN STR 27 AND STR 21L. (C-CHECK- RO 11/11/21) REPAIRED DAMAGE AT FS 574- FS 621 STR 27- STR 21L IAW REO 601R-53-61-7711 REV -- DATED 2021-10-08, REO 601R-53-61-7712 REV L SDR SWIA202161208None · corrodedCORROSION FOUND ON STRINGER 26R BETWEEN FS333.00 AND FS 349.00. (C-CHECK RO 9-21-21) REMOVED AND REPLACED STRINGER AT STGR 26R BETWEEN FS333-364 REF CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG SH670-31350 REV A. LEAK TEST GOOD. COMPLIED WITH SKY
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