JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 A6WA202102047585Pressure Deck · corrodedPRESSURE FLOOR PANEL AT FS. 542.00, RBL 42, HAS CORROSION ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 542.00, RBL 42, BLENDED AREA MEASURES 1.54Ï¿½ L X 1.26Ï¿½ W REF BOMBARDIER REO 601R-53-41-666, REV (C), ISSUE DASDR A6WA202102047580Pressure Deck · corrodedPRESSURE FLOOR PANEL AT FS. 529.00 + 7, LBL 42, HAS CORROSION AROUND NUT-PLATE ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 529.00 + 7, LBL 42, AT NUT-PLATE HOLE, BLENDED AREA MEASURES 1.46Ï¿½ L X 0.740Ï¿½ W REF BOMBSDR A6WA202102047584Pressure Deck · corrodedPRESSURE FLOOR PANEL AT FS. 536.00, RBL 42, HAS CORROSION ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 536.00, RBL 42, BLENDED AREA MEASURES 1.53Ï¿½ L X 0.96Ï¿½ W REF BOMBARDIER REO 601R-53-41-666, REV (C), ISSUE DASDR A6WA202102047581Pressure Deck · corrodedPRESSURE FLOOR PANEL AT FS. 529.00 + 2, LBL 42, HAS CORROSION AROUND NUT-PLATE ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 529.00 + 2, LBL 42, AT NUT-PLATE HOLE, BLENDED AREA MEASURES 0.88Ï¿½ L X 0.81Ï¿½ W REF BOMBASDR A6WA202102047598Pressure Deck · corrodedPRESSURE FLOOR PANEL AT FS. 513.00 + 6, LBL 42, HAS CORROSION AROUND NUT PLATE HOLE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 513.00 + 6, LBL 42, BLENDED AREA MEASURES 0.88Ï¿½ L X 0.34Ï¿½ W, REF BOMBARDIER REO: SDR A6WA202102047583Pressure Deck · corrodedPRESSURE FLOOR PANEL AT FS. 531.00, RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 531.00, RBL 42, BLENDED AREA MEASURES 1.540Ï¿½ L X 1.00Ï¿½ W REF BOMBARDIER REO 601R-53-41-666, REV (C), ISSUE DATE: 1SDR SWAA2021022345692Pressure Deck · damagedFLIGHT DECK FLOOR DAMAGED / ACCOMPLISHED PERMANENT REPAIR AT FLIGHT DECK FLOOR IAW EA # 1-A53-33179 REV 1.SDR SWIA202156948Door Frame · corrodedPAX DOOR FRAME FS 327 HAS COROSION (C-CHECK) RO 3/11/2021 REMOVED AND REPLACED PAX DOOR FRAME AT FS 327 REF DWG 601R31702 REV. N. & CRJ700 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-100SDR SWAA2021021748211Pressure Deck · dentedSTA 260 COCKPIT FLOOR PREVIOUS REPAIR DENTED. REMOVED AND REPLACED REPAIR PARTS AT PREVIOUS REPAIR LOCATED AT STA 260 COCKPIT FLOOR IN REFERENCE EA NO 1-A53-33179 REV 1 AND SRM 51-40-02-0G-0 AND 51-40-05-0G-0.SDR AALA202102099013Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION ON CREASE ANGLE AT STA 992 AND RBL 37 TO 42.5. REMOVED AND REPLACED CREASE ANGLE REF AARD 51-00-05.SDR A6WA202102057609Skin Panel · dentedOUTWARD DENT AT FUSELAGE EXTERIOR SKIN AT FS. 654.50 + 22, STGR 23R + 3. AIRCRAFT REMOVED FROM SERVICE. MEASURED DENT AT FS. 654.50 + 22, STGR 23R + 3, DENT MEASURES 0.750” L X 0.600” W X 0.010” D REF AIR WISCONSIN SUPPLEMENT NO. 14-239. CALIPER SN: 0036003SDR SWAA2021020245321Landing · crackedGROUND POWER DOOR LOWER FLANGE CRACKED / TRIMMED OUT DAMAGE ON GROUND POWER DOOR LOWER FLANGE PER SRM 53-10-15-2R-4. HFEC REQUIRED. C/W HFEC OF DAMAGE CUTOUT PER NDT PART 6 51-00-00 PROD 23. NO DEFECTS NOTED. (D127). COMPLETED REPAIR PER SRM 53-10-15-2R-4SDR MK1Y01292021007Skin · damagedDURING MAINTENENCE INSPECTION FOUND EXISTING UNDOCUMENTED REPAIR ON FUSELAGE SKIN.SDR MK1Y01292021005Skin · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION DAMAGE ON THE AFT UPPER SKIN OF CENTER WING THAT EXCEEDS UNDER THE TENSION FITTING.SDR SWIA202157328Support Beam · gougedCARGO DOOR SUPPORT BEAM IS GOUGED JUST FORWARD OF 621 BULKHEAD FROM CARGO DOOR ASSIST CABLE. (C-CHECK RO 4/2/2021) REMOVED AND REPLACED CARGO DOOR BEAM IAW CRJ 200 SRM 51-42-06 AND 51-42-21SDR EVCA2021021001Stiffener · crackedDURING ROUTINE INSPECTION FOUND VERTICAL TUNNEL RIGHT REAR STIFFENER CRACKED.SDR A6WA202102047586Pressure Deck · corrodedPRESSURE FLOOR PANEL AT FS. 559.00, LBL 42, HAS CORROSION ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 559.00, LBL 42, BLENDED AREA MEASURES 2.17Ï¿½ L X .73Ï¿½ W REF BOMBARDIER REO 601R-53-41-666, REV (C), ISSUE DATSDR JJBA20210128042Skin · dentedCF II RT FUSELAGE DENTED BETWEEN FR 26-27 STR 11-12. CENTER FUSELAGE II DENT BETWEEN FR 26-27, STR 10R-12R REPAIRED.SDR SWAA2021030445580Web · corroded***CORROSION*** AFT CARGO BAY ON VERTICAL WEB BS 787 TO BS 807 STR 27R WL 150 / CORROSION EVALUATION ON ACB VERTICAL WEB BS787-807; STR27R. WAS FOUND TO BE OUT OF LIMITS; DUE TO PROXIMITY TO A HOLE PER SRM 53-60-15. REMOVED AND INSTALLED NEW ACB VERTICAL WEB BSDR SWAA2021030445579Web · corrodedCORROSION AFT CARGO BAY ON VERTICAL WEB BS 767 TO BS 787 STR 27R WL 150 DAMAGE EVALUATION ON ACB VERTICAL WEB BS767-787; STR27R; WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO A HOLE PER SRM 53-60-15. REMOVED AND INSTALLED NEW ACB VERTICAL WEB BS767-787;STSDR UIEA2021012600128Receptacle · damagedNR 1 EXTERNAL POWER RECEPTACLE DAMAGED. REPAIRED PER EO 4453B956/PART 1. FABRICATED AND INSTALLED INTERNAL REPAIR WASHERS. PERMANENT, CATEGORY B/REPAIR AWAITING DTE.SDR SWIA202157584Box Beam · corrodedCORRISION INSIDE OF BOX FRAME ABOVE FWD CARGO DOOR, BETWEEN STR 18 AND 19, F/S 533.00 AND 549.00 (C-CHECK RO 4/20/2021) REPAIRED FWD CARGO DOOR LINTEL DAMAGE AT L/H FS533 TO FS549 BETWEEN STR18L TO STR19L IAW MHIRJ REO # SH670-53-31-604.SDR SWAA2021022450248Pressure Deck · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR DENT AT BS 255; RBL 4 - LBL 14; WL 207; PER SWA EA 1-A53-33179 REV 1SDR A6WA202102087626Landing · corrodedAVIONICS DOOR CUT OUT LAND HAS FRETTING DAMAGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED FRETTING DAMAGE AT AVIONICS DOOR CUT OUT REF CRJ-200 SRM 51-21-06 REV 38. PERFORMED UT THICKNESS MEASUREMENT ON AVIONICS DOOR CUT OUT INTERIOR SURFACE BLENDED AREA REF CRJSDR VNAA202101309993Door Frame · corrodedAFT CARGO DOOR SILL AFT INNER CHORD CORRODED.SDR VNAA202101309992Door Frame · corrodedAFT CARGO DOOR LOWER SILL CORRODED.SDR SWAA2021021848201Mount · deterioratedDETERIORATED ENTRY FWD DOOR CUT OUT MOUNT AT FWD GALLEY AREA (2 EA). REPLACED SHOCK MOUNT LOC ENTRY FWD DOOR CUT OUT AT FWD GALLEY AREA (2EA) DUE TO DETERIORATED NOT FOUND ALLOWABLE DAMAGE PART NUMBER USED BAC514K1 PO 202019825900101 IAW B737-700 SRM 51-40-02SDR ASAA2021012534007Panel · corrodedFORWARD CARGO TRANSITION PANEL AT RBL 25 CORRODED BETWEEN STA 500B=10 TO STA 500L. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2 REPAIRED TRANSITION PANEL IAW B737-900ER SRM 53-00-53-2R-5W=1.2 O=.040 R=.020 L=2.SDR CALA2021012700094Profile · crackedOFF-AIRCRAFT PART: LT AFT EMERGENCY EXIT HATCH FWD LOAD TRANSMITTING PROFILE CRACKED, PER HAECO LCQ NON ROUTINE 9292230. REMOVED CRACKED SEGMENT INSTALLED NEW SEGMENT, IAW A320 SRM 51-42 -11-801.SDR CALA2021012700093Profile · crackedLT AFT EMERGENCY EXIT HATCH AFT LOAD TRANSMITTING PROFILE CRACKED OFF. AIRCRAFT PART: (A3NB-52-4-6031) PER HAECO LCQ NON ROUTINE 9292231. REMOVED CRACKED SEGMENT INSTALLED NEW SEGMENT, IAW A320 SRM 51-42 -11-801.SDR SIMA20210125002Structure · crackedTHE COCKPIT RT DIAGONAL CEILING MEMBER IS CRACKED JUST FORWARD OF THE SPEAKER, AS MARKED. C/A: R & R COCKPIT RT DIAGONAL CEILING MEMBER, IAW EMB 145 SRM 51-40-02. REPLACEMENT PN: 123-07751-006.SDR JR2R20210125393Crossbeam · corrodedCROSS BEAM 17 CORRODED FROM LBL 9 RO RBL 9.SDR SWIA202156683Door Frame · corrodedPAX DOOR FRAME F/S 313.56 BETWEEN FWD DD4 AND DD5 INTERCOSTAL HAS CORROSION (C-CHECK) RO 3/4/2021 REPLACED PAX DOOR FRAME AND CLEAT @ FS313.56, BETWEEN FWD DD4 AND DD5 INTERCOSTALS PER CRJ-900 SRM 51-42-06-001-001-A01 & DRAWING 601R31702 REV N. SEE CONTSDR AALA202103059024Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND L= 0.925 INCH CRACK ON SHEAR PLATE AT FR 69 PLUS 4 INCHES AND STR 23R. REPLACED SHEAR PLATE IAW A321 SRM 51-42-11-801, 51-72-11-911-001 AND DRAWING #D53474180.SDR SWIA202156677Door Frame · corrodedPAX DOOR FRAME F/S 327.763 HAS EXFOLIATED CORROSION (C-CHECK) RO 3/4/2021 INSTALLED NEW PAX DOOR FRAME F/S 327.763 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N / SEE CONTINUATION CARD FOR DESDR DALA2021012500461Structure · corrodedTHE AFT CARGO BIN SHOWS EVIDENCE OF SURFACE CORROSION AT J FRAME AT STA 1022, BETWEEN STR 29L-29R. LOCATED JUST FORWARD OF LAV TANK VENT MOTOR, MARKED. COMPLETED REPAIR AT J FRAME AT STATION 1022 BETWEEN STR 29L-29R, REF B717 SRM 53-20-07-2R. ALL WORK COMPLSDR AALA202103229013Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND L=0.121 INCH CRACK ON LEFT FITTING AT FR1 AND Y0. PERFORMED REPAIR, REPLACING LEFT CONTINUITY FITTING LOCATED ON FRAME 1 TO FRAME 2 AND LEVEL OF Y0 IAW EA # 311074.SDR AALA202103229012Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND L= 0.280 INCH CRACK ON CENTER WINDSHIELD FRAME AT FR2 AND Y0. PERFORMED ON WINDOW CENTER POST LEFT FROM LOWER INBOARD RADIUS LOWER ATTACHMENT INTERNAL AREA SIDE IN COCKPIT IAW EA 311073.SDR SWIA202156766Crossbeam · corrodedCROSSBEAM CAP AT FS 280 L/H SIDE HAS HEAVY CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED LH CROSSBEAM CAP AT F.S. 280 IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY AND FORM M-337. .WEIGHT NOT AFFECTED.SDR SWAA2021021548010Isolator · damagedISOLATORS DAMAGED STA. 578 3 EA. LEFT SIDE / R&R'D 3 EA. ISOLATORS AT STA. 578 PER SRM 51-10-02.SDR ASAA2021012234017Frame · crackedUPPER FUSELAGE FRAME IS CRACKED AT STA 727D & STR 8RT FLAGGED. GROUNDED - YES. REPAIRED LT FRAME STA 727D IAW ALASKA TC AD20090102-700-25-1R STEP 51.SDR SIMA20210122005Door Frame · deformedFRAME 67 HAS 1 OBLONG HOLE BENEATH THE CARGO DOOR SILL. C/A REPAIRED FRAME 67 BENEATH THE CARGO DOOR SILL IAW SRM 53-00-04.SDR SIMA20210122004Door Frame · deformedFRAME 66 HAS 2 OBLONG HOLES BENEATH THE CARGO DOOR SILL. C/A-REPAIRED FRAME 66 BENEATH THE CARGO DOOR SILL IAW SRM 53-00-04.SDR ASAA2021012233963Transition Panel · corrodedAFT PIT FLOOR TRANSITION PANEL LT SIDE BETWEEN STA 727I & J- STA 797 HAVE CORROSION AROUND FASTENER HOLES. GROUNDED-YES. REMOVED CORROSION ORG THICKNESS .040, PER B737-900ER SRM 53-60-53-01-2. REMOVED .008 MATERIAL OUT OF LIMITS, PER B737-900ER SRM 53-00-53SDR ASAA2021012233961Transition Panel · corrodedAFT PIT FLOOR TRANSITION PANEL RT SIDE BETWEEN STA 727I&J- STA 767 HAVE CORROSION AROUND FASTENER HOLES. GROUNDED-YES. REMOVED CORROSION ORG THICKNESS .040, PER B737-900ER SRM 53-60-53-01-2. REMOVED .005 MATERIAL OUT OF LIMITS, PER B737-900ER 53-00-53-1A-2.SDR ASAA2021012233960Transition Panel · corrodedAFT PIT FLOOR TRANSITION PANEL RT SIDE BETWEEN STA 727E&F- STA 727I & J HAVE CORROSION AROUND FASTENER HOLES. GROUNDED-YES. REMOVED, FABRICATED AND INSTALLED AFT PIT TRANSITION PANEL ON RT BETWEEN FS 727E AND F TO FS 727I AND J. REMOVED CORROSION ORIG THICKSDR SWAA2021012643957Vapor Barrier · crackedRT 663 VAPOR BARRIER HAS A CRACK AT APPROXIMATELY RBL 49 AND 9 IN FROM STRINGER. COMPLETED TIME LIMITED REPAIR EA 1-A57-13410 REV 01 REPETITIVE INSPECTION ACTION. REMOVE ALUMINUM FOIL SPEED TAPE AND INSPECT CRACKS FOR ADDITIONAL GROWTH. IF NO ADDITIONAL GROSDR DALA2021012500468Door Frame · crackedFUSELAGE FRAME 16 NOSE FWD LT DOOR STOP 1 & DOOR STOP 7 CRACKED HOLES. CORRECTIVE ACTION: ACCOMPLISHED ER/A 589094-14 SECTION II INSPECTION. CONT ON MON.SDR SWIA202156669Door Frame · corrodedPAX DOOR FRAME AT FS338.963 HAS CORROSION (MARKED ON FRAME) (C-CHECK) RO 3/4/2021 REPLACED PAX DOOR FRAME AND CLIP AT FS338.963 PER CRJ-900 SRM 51-42-06-001-001-A01,CRJ-900 SRM 51-42-21-001-001-A01 & DRAWING 601R31702 REV N. SEE CONTINUATION CARD FOR DETSDR ASAA2021012134025Frame · crackedUPPER FUSELAGE FRAME IS CRACKED AT STA 500C & STR 8 R/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1R.
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