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 JR2R202304125155Shear Panel · corrodedFLOOR WEB ON TOP OF FR87 CORRODED BETWEEN RBL12 THRU RBL40SDR CALA2023041201099Panel · missingPANEL MISSING JUST AFT OF R MLG SEE PICS ATTACHED. INSTALLED PANEL P/N 149A7654-8. CHECKS SECURE.OK TO CONT PARTS USED: 29-5351-3-0028,QTY :1SDR SWIA20230530410Unknown · unknownLEFT OVERWING EMER EXIT DOOR CUT- OUT HAS CHAFFING ON AFT UPPER DOOR FITTING ON UPPER SILL (C-CHECK RO 5/23/2023) REMOVED AND REPLACED THE LH AFT UPPER FITTING (LH EMER. DOOR CUT OUT) WITH NEW REF. CRJ 200 AMM 20-21-00-910-801 AND DWG #601R31108 REV. J.SDR R61A2023042600251Service Panel · corrodedTOILET WASTE SERVICE PANEL HEAVILY CORRODED. REPLACED TOILET WASTE SERVICE PANEL WITH NEW IAW AMM 20-10-01 AND SRM 51-40-02SDR FDEA202304100619Panel · dentedDENTS ON FLOOR PANEL 222BFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4.B FIG 201 SHEET 2. REV 85 DEC 15/2022SDR FDEA202304100617Panel · dentedDENTS ON FLOOR PANEL 222AFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4.B FIG 201 SHEET 2 REV 85 DEC 15/2022SDR FDEA202304100616Panel · dentedDENTS ON FLOOR PANEL 221DFF AT SECTION 41 OF MDC MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4.B FIG 201 SHEET 2 REV 85 DEC 15/2022SDR FDEA202304100613Panel · dentedDENTS ON FLOOR PANEL 222CFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR SWIA2023041100001Unknown · crackedCRACK IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE ROD THROUGH HOLE. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 WILL BE REQUIRED. (FILED OPEN)SDR EE4Y2023041017582Fitting · crackedPLEASE NOTE THAT DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: 531135-01-2-001 MPD, IT WAS FOUND RH WINDSHIELD SIDE POST UPPER AND FITTING P/N: D5311086520303 ATTACHMENT AT FRAME 4 (1 HOLE WITH CRACK INDICATION) CORRECTIVE ACTION: DAMAGE REPORT SDR EE4Y2023041017581Frame · unknownDURING THE EO E5311-0051, 53-0004-19 ALLEGIANT EO´S ACCOMPLISHMENT RELATED TO AD 2022-08-08 PARAGRAPH (G) AND SB 53-1379 REV. 00, SB 53-1380 REV. 01, SB 53-1381 REV. 01 WERE FOUND HOLES AT FR16 (HOLE #4) UPPER FWD CORNER LH SIDE WITH DIAMETER THAT IS MORE THANSDR EE4Y2023100317580Fitting · crackedDURING THE ALLEGIANT TASK 53-210-003_P1-OP-UP-NDT/00 WORK CARD INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE RH CONTINUITY FITTING WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST THE KITS P/N FOR REPLACEMENT. AIRBUS PROVIDED THE INFORMATION WSDR IXXA2023011001Skin · gougedGOUGE ON DOUBLER AT FWD LOWER CORNER BY AFT CARGO DOORSDR SWIA202305300409Unknown · crackedNLG WHEEL WELL - FS 193 @ RBL 6 AND TOP OF WELL - BRACKET CRACKED (C-CHECK RO 5/23/2023) LG WHEEL WELL - FS 202 @ RBL 6 AND TOP OF WELL BRACKET PART# 604-33101-188 IS CRACKED AND IS OUT OF LIMITS REF CRJ200 SRM 53-00-00. REMOVED CRACKED BRACKET REF CRJ2SDR SWIA2023053000409Unknown · corrodedL/H PRESSURE FLOOR SILL PANEL CORROSION FROM FS 409.0+128 TO FS 559.0 ( MARKED WITH READ GREASE PENCIL ) (C-CHECK RO 5/23/2023) REPAIRED LH PRESSURE FLOOR SILL FROM FS 409.00+128 TO FS 559.00 REF REO 601R-53-41-666 REV C DATED 2012-11-06 DISPOSITION 1.2SDR SWIA20230526409Unknown · corrodedCORROSION ON L/H SEAT RAIL BETWEEN FS 409.0+128 AND FS 559.00 (C-CHECK RO 5/23/2023) REMOVED AND REPLACED LH SEAT RAIL BETWEEN FS409.0+128 AND FS559.00 REF. CRJ-200 AMM, 53-01-11-000-802 AND CRJ-200 AMM, 53-01-11-400-802.SDR HNAA2023042800143Unknown · unknownE968665 FRAME 68 IS CRACKED JUST BELOW CARGO DOOR HOLD OPEN CUP. REPAIRD IAW EMBREAR ETD2023-145-009411 AND PIEDMONT EO 1-*53-23-0106.SDR HNAA2023042800142Unknown · unknownE968646 PILOT SIDE BULHEAD OUTB GUIDE PIN HOLE ELONGATED. REPAIRED IAW EMB148 SRM 53-21-02 ITEM 4 FIGURE 204 AND PIEDMONT EO1-53-23-0105SDR EE4Y2023030917568Stringer · corrodedDURING ACCOMPLISHMENT CORROSION TASK 532180-01-2, IT WAS FOUND LOWER FUSELAGE, FWD CARGO COMPARTMENT, AT FR 29 +355MM, STGR 41R, STRINGER WITH CORROSION.DUE THIS FACT. IT WAS REPAIRED STRINGER SECTION AT STGR 41 R/H, FROM FR 29 TO FR 30 +460 MM, IAW A320-SRM-5SDR HNAA2023042800141Unknown · unknownE968631 LEVEL 2 CORROSION ON CENTER #3 OMEGA BEAM GUSSET. REMOVED AND REPLACED IAW EMB145 SRM 51-40-02SDR HNAA2023042800140Unknown · unknownE968627 LEVEL 2 CORROSION ON CENTER #5 OMEGA BEAM GUSSET. REPAIRED IAW EMB145 SRM 51-10-03, 53-23-10, AND 51-40-02.SDR HNAA2023042800139Unknown · unknownE968626 LEVEL 2 CORROSION ON CENTER #4 OMEGA BEAM GUSSET. REPAIRED IAW EMB145 SRM 51-40-02SDR HNAA2023042800138Unknown · unknownE968625 COROSSION ON LH #5 OMEGA BEAM GUSSET. REPAIRED IAW EMB145 SRM 51-10-03, 53-23-10, AND 51-40-02.SDR HNAA2023042800137Unknown · unknownE968624 LEVEL 2 CORROSION ON LH #6 OMEGA BEAM GUSSET. REPAIRED IAW EMB145 SRM 51-10-03, 53-23-10, AND 51-40-02SDR HNAA202304280136Unknown · unknownE968620 LEVEL 2 CORROSION IN LAV AREA ON CENTER FLOOR GUSSET. REPAIRED IAW EMB145 SRM 51-40-02.SDR HNAA2023042800135Unknown · unknownE968619 LEVEL 2 CORROSION IN LAV AREA ON RH FLOOR GUSSET REPAIRED IAW EMB145 SRM 51-40-02SDR HNAA2023042800134Unknown · unknownE968586 SSI LEVEL 2 CORROSION ON CARGO DOOR FLOOR SILL REPAIRED IAW EMB145 SRM51-10-03, 51-40-02,51-40-03,51-40-06 AND 51-40-09SDR DALA2023041102835Unknown · unknownSHIP 665 CORROSION ON RH SIDE PLATE OF LWR SILL AREA FROM STA. 1380 TO 1440 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00347. RH SIDE PLATE OF LWR SILL AREA FROM STA. 1380 TO 1440 AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (271039SDR CALA2023041001076Web · crackedAFT WET AREA WEB STA 986.5 - STA 1016 AND RBL 33 - RBL 45 FOUND CRACKED. (REF AAR NR 975230) REMOVED AND REPLACED AFT WET AREA WEB AT STA 986.5 TO STA 1016 AND RBL 33- RBL 45 AS PER SRM 51-40-02-0G-0 AND DRAWING # 147A5700. ACCOMPLISHED BY V928494.SDR SWIA20230530407Unknown · cracked* INTERCOSTAL FROM FS621 TO FS625, STR13L, IS CRACKED. (C-CHECK RO 5/23/2023) REMOVED AND REPLACED INTERCOSTAL FROM FS621 TO FS625, STR13L REF. DRWG 601-35012 REV. D AND CRJ 200 SRM 51-42-21. COMPLIED WITH 53-900-1003-SKY AND SKYWEST FORM M-337SDR NACA202304070001Unknown · unknown1.5 INCH CRACK FOUND IN FUSELAGE SKIN @ STR 23L EIGHT INCHES FORWARD OF BS 727E. INSTALLED REPAIR IN LOCATION GIVEN IAW BOEING SRM 53-00-01 REPAIR 31. SEE PROJECT WORKSHEET FOR DETAILS.SDR A6WA202304078541Frame · corrodedFRAME AT FS 310 HAS CORROSION STRG26L-26R. AC REMOVED FROM SERVICE. INSTALLED NEW LOWER FRAME SECTOR TO THE LOWER SKIN @ FS310 REF CRJ-200 SRM 51-42-06 AND DWG 601R32002 REV.AC.SDR CALA2023041001069Web · crackedWHILE PERFORMING UAL EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491), CRACK WAS FOUND AT FR 68 RHS STGR 22 LOWER WEB HORIZONTAL FLANGE RADIUS. CRACK LENGTH APPROX .439". RCRAFT N408UA (4108) REACHES 50,000 TOTAL AIRCRAFT FLIGHT CYCLES R PART 2 OF THE LATESDR CALA2023041001075Skin · corrodedCORROSION FOUND IN THE SKIN OF GROUND CONDITIONED AIR CONNECTION DUCT. REQUIRE EVALUATION (REF. AAR NR 99967000). ACCUMULATION OF 48,000 TOTAL AIRCRAFT FLIGHT CYCLES, PLANNING TO ELAGE SKIN AND KEEL BEAM DOUBLER REPAIR BETWEEN STA 500H AND STA PART 2 OF THE LASDR CALA2023041001074Frame · crackedCOMPLETE REQUIRED SFR FOR WINDOW REPAIR ON L/H WINDOW FRAME DUE TO CRACK LOCATED AT THE TOP UNDER MOD (REF: AAR NR 99959435) EA 5310-04554 REV B OP 007 REPAIR ACCOMPLISHED FOR CONFIG B REVIEWED AND APPROVEDSDR SWIA202305190006Unknown · corroded*CORROSION NOTED AT MULTIPLE SPOTS ON 605 FRAME BETWEEN STRG24R-18L (MARKED) (C-CHECK RO 5/15/2023) REPAIRED CORROSION AT MULTIPLE SPOTS ON 605 FRAME BETWEEN STRG24R-18L REF REO 601R-53-61-8010 REV -- DATED 2023-05-02, COMPLIED WITH ALL STEPS.COMPLIED WSDR IPXA2023051132657Cap · corrodedCORROSION - UPPER CAP, MAIN DECK CARGO COMPARTMENT FLOOR AREA, STA 2374, RBL 15 (REPLACE) ALL PAPERWORK C/WSDR SWIA2023042600008Unknown · corrodedRH INBD SEAT TRACK CORRODED AS MARKED BETWEEN FR73, 74, 76, 77, 78, 79, 80, 81, 82, AND 83. (C-CHECK RO 4/25/2023) REMOVED AND REPLACED RH INBOARD SEAT TRACK BETWEEN FR 73 -83, REF EMB 175 SRM 51-40-08. PART REPLACED WITH NEW OEM PART. THIS ACTION DOES SDR SWIA202304260007Unknown · gougedRH FLOOR SEAT TRACK SEGMENT LOCATED BETWEEN FR 60 AND FR74, GOUGED AND HAS CORROSION IN SEVERAL AREAS. (C-CHECK RO 4/25/2023) REMOVED AND REPLACED RH FLOOR SEAT TRACK SEGMENT LOCATED BETWEEN FR 60 AND FR74, REF EMB 175 SRM 51-40-08. PART REPLACED WITH NSDR SWIA2023042600006Unknown · gougedRH FLOOR SEAT TRACK SEGMENT LOCATED BETWEEN FR 34 AND FR60, GOUGED AND HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 4/25/2023) REMOVED AND REPLACED RH FLOOR SEAT TRACK LOCATED BETWEEN FR34 AND FR60. REF. E175 SRM 51-40-08. SEE CONTINUATION CARDS FOR ALLSDR IPXA2023042192949Angle · crackedINSPECTION TYPE:C3R/H FUSELAGE BODY FAIRING AREA STA 1341 UPPER SIDE ANGLE SUPPORT LWR SIDE IS CRACKED.REMOVED, FABRICATED AND REPLACED ANGLE AT THE R/H FUSELAGE BODY FARING AREA AT STA 1341 IAW SRM 51-31-01.SDR CALA2023041001067Unknown · corrodedFWD PASSENGER COMP WET AREA R/H CORROSION ON INNER CHORD STA 277+14 TO 328+4 REF AAR N/R 974893 REMVOED AND REPLACED THE INNER CHORD STA 251 TO STA 360 AT FWD PASSENGER CABIN COMP WET AREA R/H PER B737 SRM 51-40-02-0G-0 AND DWG 141A8310 WORK ACCOMPLISHED BY V8SDR CALA2023041001062Floorbeam · corrodedAFT WET AREA FLOOR BEAM STA 986,LBL 24 TO LBL 55 HAS SEVERAL SPOTS OF CORROSION.(REF AAR NR 975082) REMOVED CORROSION ON FLOOR BEAM STA 986.5 LBL TO ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM LBL 55 AS PER SRM 51-10-02-0G-0 ORIGINAL MAT. 53-70-51-2R-4. ALTERNATSDR A6WA202304068536Intercostal · corrodedCORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS 338.00 TO FS 349.00 ******AIRCRAFT REMOVED FROM SERVICE******** REPLACED PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS 338.00 TO FS 349.00 REF DWG 601R31702 REV-NSDR FDEA202304060575Angle · corrodedAREA OF AFT CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE AND NUTSTRIP ARE CORRODED BETWEEN STA 1701 AND 1720 APPROX RBL 13 REMOVED AND REPLACED ANGLE (FLOOR SUPPORT) AND NUTPLATE STRIP IAW BAC DWG 146N5300 REC C 140N2524 REV A, B757 SRM 51-40-02SDR FDEA202304060573Angle · corrodedAREA OF THE BULK CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE AND NUTSTRIP ARE CORRODED BETWEEN STA 1701 AND 1720 APPROX LBL5 REMOVED AND REPLACED ANGLE ( FLOOR SUPPORT) WITH NUTPLATE STRIP IAW BAC DWG 146N5300 REV C 140N2524 REV A B757 SRM SDR FDEA202304060572Angle · corrodedAREA AFT OF THE BULK CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE & NUT STRIP ARE CORRODED BETWEEN STA 1701 & 1720 APPROX RBL 5 REMOVED AND REPLACED FLOOR SUPPORT AND NUTPLATE STRIP IAW B757 SRM 51-40-02-0G AND BAC DWG 146N5300 REV C AND 140N2524 SDR CALA2023040601055Web · crackedWHILE PERFORMING UAL EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491), CRACK WAS FOUND AT FR 68 RHS STGR 22 LOWER WEB HORIZONTAL FLANGE RADIUS. CRACK LENGTH APPROX .439". RCRAFT N408UA (4108) REACHES 50,000 TOTAL AIRCRAFT FLIGHT CYCLES R PART 2 OF THE LATESDR SWIA202305300405Unknown · chafedCHAFFING DISCOVERED ON INSIDE SURFACE OF DECOMPRESSION PANEL CUT OUT (C-CHECK RO 5/23/2023) COMPLIED WITH REO REPAIR 601R-52-11-2977 REV. - DATED 2023-05-04 SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.C/W 51-900-1003-SKYSDR IPXA2023042893027Longeron · corrodedINSPECTION TYPE:3C*MAJOR REPAIR* CENTER CARGO BILGE AREA LONGERON 49L HAS CORROSION BETWEEN STA Y=1681 - Y=1710.REPAIRED CORRODED LONGERON 49L AT THE CENTER CARGO BILGE AREA BETWEEN STA Y=1681 - Y=1710 IAW VTSAA EA 011-5310-01-A9908 I/R, UPS EO MD11-5310-86649
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