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 SWIA202052784Rod · chafedCHAFE LOWER ROD ASSEMBLY AS MARKED ON CO-PILOTS DV WINDOW. C-CHECK RO 9/24/2020. BLENDED CHAFFED AREA ON LOWER ROD ASSEMBLY, IAW EMB-175 AMM. ROD DIAMETER BEFORE BLEND WAS: 18.05MM. ROD DIAMETER AFTER BLEND: 17.82MM. AMM MIN ALLOWABLE DIAMETER 17.69MM.SDR SWIA202052783Rod · chafedCHAFE LOWER ROD ASSEMBLY AS MARKED ON PILOTS DV WINDOW. C-CHECK RO 9/24/2020. BLENDED CHAFED AREA ON LOWER ROD ASSEMBLY, IAW EMB-175 AMM. ROD DIAMETER BEFORE BLENDING WAS 18.03MM AND ROD DIAMETER AFTER BLENDING: 17:86MM. AMM MINIMUM ALLOWED DIAMETER 17.69MSDR SWAA2021042715331Pressure Deck · dentedFLIGHT DECK FLOOR REQUIRES REPAIR UNDER SECOND OBSERVER SEAT @ FS259 / REMOVED 2ND OBSERVER SEAT AT FLIGHT DECK AREA AS PER B737-700 AMM 25-11-02-000-802; ACCOMPLISHED FLIGHT DECK FLOOR WEB DENT REPAIR AT BS 260 AS PER EA NO 1-A53-33179 REV 1; RE-INSTALLED 2NDSDR SWIA202053598Fitting · chafedPASSENGER DOOR SURROUND AT AFT UPPER PIN FITTING HAS CHAFE DAMAGE. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT UPPER PIN STOP FITTING, REF CRJ 200 AMM (TESTS GOOD).SDR R61A2020093000669Crossbeam · corrodedCORROSION FOUND ON CENTER FUSELAGE FLOOR STRUCTURE CROSSBEAM UPPER FLANGE AT FR 16 RT SIDE. REPAIRED IAW SRM 53-00-10.SDR SWAA2020092815418Beam · crackedCRACK INDICATION FOUND AS A RESULT OF HFEC INSPECTION OF THE 141A6536-14 BEAM [LOWER] AT THE FWD FILLET REGION. REMOVED BEAM NR 4 FROM R1 DOOR, PER B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW BEAM P/N 141A65036U20, PER B737-700 SRM 51-40-05-0G-0 DRAWSDR FDEA202009102310Panel · crackedAFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-SDR FDEA202009102309Panel · crackedAFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2SDR FDEA202009102308Panel · crackedAFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-100.SDR FDEA202009102307Panel · crackedAFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-100.SDR SWIA202052772Crossbeam · brokenFRAME 86 CROSSBEAM LT AND RT PANEL SUPPORTS BROKEN OFF. C-CHECK RO 9/24/2020. REMOVED AND REPLACED FR 86 CROSSBEAM LT AND RT PANEL SUPPORTS, PER SRM. SEE CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA202052769Crossbeam · corrodedCORROSION FWD WET AREA FR 17 CROSSBEAM AS MARKED IN BETWEEN LT AND RT FLOOR TRACKS. C-CHECK RO 9/24/2020. PERFORMED CUTOUT OF CORROSION ON FRAME 17 CROSSBEAM. FABRICATED AND INSTALLED FILLER AND DOUBLER, REF EMB SRM. ADDED WEIGHT DOES NOT CHANGE WEIGHT AND SDR SWAA2020091415295Angle · crackedCENTER TANK UPPER WING SKIN ANGLE AT BS 663 AND LBL 45-48 APPROXIMATE. VISUAL CRACK INDICATION NOTED.SDR DALA2020091103031Crease Beam · crackedDURING INSPECTION FOUND CRACK ON CREASE BEAM TRUSS AT STA 418 AND 65 LBL PASSENGER CABIN. REPAIRED PER ERA 587698-14.SDR SWIA2020091052435Windshield · crackedFO WINDSHIELD HAS SEVERAL CRACKS DUE TO FLYING DEBRIS. FILED CLOSED. REMOVED AND REPLACED FO WINDSHIELD, IAW TASK CARD AND AMM. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME. TORQUE WRENCH INFO S/N A7U149009 DUE 07/2021, S/N 0312800028 DUE 06/2021.SDR SWIA202053526Window Post · crackedLEFT SIDE WINDSHIELD POST LOWER OUTBOARD CLIP CRACKED. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED NEW LT SIDE WINDSHIELD POST LOWER CLIP, REF CRJ-200-SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053525Window Post · crackedRIGHT SIDE WINDSHIELD POST LOWER OUTBOARD CLIP CRACKED. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED NEW RT SIDE WINDSHIELD POST LOWER CLIP, REF CRJ-200-SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202053470Support · crackedRIGHT WINDSHIELD SIDE POST SUPPORT P/N 601R34032-22 IS CRACKED IN THE RADIUS ABOVE THE STRINGER. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SUPPORT, IAW CRJ 200 SRM. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, WAS A PART FOR SDR SWAA2020100519631Floor Skin · dentedFLIGHT DECK FLOOR IS DENTED AT BS 255, RBL 4-LBL 14; WL 207.54. FLIGHT DECK FLOOR AT BS 255 RBL 4-LBL 14 WL 207.54 REPAIRED, IAW EA 1-A53-33179 REV 1.SDR A6WA202009189287Pressure Deck · corrodedLT PRESS FLOOR SILL PANEL HAS CORROSION AROUND FASTENER HOLE AT FS 452.35 & BL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT FLOOR SILL PANEL AT FS 452.35 & BL 43 WITH A REWORK AREA THAT MEASURES L=1.88 X W=1.134 X D=.003" ORIGINAL THICKNESS .080" SDR IPXA2020091196039Crossbeam · crackedINSPECTION TYPE: A 300 MAIN CABIN FLOOR STRUCTURE SUPPORT IS CRACKED AT F 31 AND -Y450. REMOVED & REPLACED IAW SRM 51-40-21.SDR SWAA2020100519509Floor Skin · corrodedFLIGHT DECK, SURFACE CORROSION ON UPPER SURFACE OF STRUCTURE THAT SUPPORTS FLOOR PANEL 211 AF, MARKED. REPAIRED PER EA 1-A53-13812.SDR SWAA2020100519511Floor Skin · dentedFLIGHT DECK, DENTS IN THE FLIGHT DECK FLOOR. LOCATED FWD OF PANEL 211AF STA 250 TO STA 257 LBB 11 TO RBL 11 APPROX, MARKED. REPAIRED PER EA 1-A53-33179.SDR DALA2020090982986Panel · corrodedCORROSION LEVEL: 2 DURING INITIAL INSPECTION FOUND SEVERAL POINTS OF CORROSION ON AFT SERVICE WASTE PANEL AND ENCLOSURE AT AFT CARGO COMPARTMENT (C2) AND REPLACED PER SRM.SDR DALA2022111007262Stop Fitting · crackedSHIP 3221 ERA 585867-14AD REVISED TO REV 'A'. SECTION I ISSUED FOR CRACK FINDINGS AT HOLES 5, 6, A, B, E, AND F AT FR16 DOOR-STOP. CORRECTIVE ACTION: COMPLIED WITH REVISION. (1609685)SDR DALA2022111007261Stop Fitting · crackedSHIP 3221 ERA 585867-14AD REVISED TO REV 'A'. SECTION I ISSUED FOR CRACK FINDINGS AT HOLES 5, 6, A, B, E, AND F AT FR16 DOOR-STOP. CORRECTIVE ACTION: COMPLIED WITH ERA 585867-14. (1609684)SDR SWIA202053400Fitting · corrodedPAX DOOR SURROUND: AFT CLOSING FITTING HAS CORROSION, MARKED. C-CHECK RO 10/16/2020. PAX DOOR SURROUND AFT CLOSING FITTING REPLACED, REF: CRJ700 SRM.SDR SWIA202053399Fitting · corrodedPAX DOOR SURROUND: FWD CLOSING FITTING HAS CORROSION, MARKED. C-CHECK RO 10/16/2020. PAX DOOR SURROUND FWD CLOSING FITTING REPLACED, REF: CRJ700 SRM.SDR SWIA202053307Windshield · crackedTHE RT WINDSHIELD SIDE POSTS LOWER AFT FITTING IS CRACKED, MARKED WITH ORANGE FLAG TAPE. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RT WINDSHIELD SIDE POST LOWER AFT FITTING, REF CRJ200 SRM DWG.SDR SWIA202053306Windshield · crackedTHE LT WINDSHIELD SIDE POSTS LOWER AFT FITTING IS CRACKED, MARKED WITH ORANGE FLAG TAPE. C-CHECK RO 10/13/2020. REMOVED AND REPLACED LT WINDSHIELD SIDE POST LOWER AFT FITTING, REF CRJ200 SRM DWG.SDR SWIA202053235Fitting · gougedCOPILOTS WINDSHIELD SIDE POST LOWER FORWARD FITTING IS GOUGED AT FORWARD END FROM CONTACT WITH WINDSHIELD STRAP SCREW. C-CHECK RO 10/13/2020. REMOVED AND REPLACED COPILOTS WINDSHIELD SIDE POST LOWER FORWARD FITTING, IAW CRJ-200 SRM AND DRAWING 601R33007. SKSDR SWAA2020092814877Support Plate · crackedCRACK FLOOR STRUCTURE SUPPORT PLATE LOCATED BS 540 BETWEN LBL 24.82 AND RBL 24.82 AT PASSENGER CABIN (2 EA). REPLACED FLOOR STRUCTURE SUPPORT PLATE LOCATED BS 540 BETWEEN LBL 24.82 AND RBL 24.82 AT PASSENGER CABIN 2 EA, IAW B737-700 SRM 51-40-02 AND DRAWING 1SDR AALA202009089016Stop Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN DOOR STOP FITTING #7 OF LH FR66 AT STR 10L, MEASURING L=0.02 IN. REPLACED STOP FITTING WITH MODIFIED PART IAW SRM 53-41-12-300-0011 AND EA308342.SDR 6PMR202009050010Pressure Web · corrodedAIRBORNE/PEMCO NON-ROUTINE 2867N675 DISCREPANCY: (EO 20366-7) REPAIR RT KEEL BEAM WEB (SECTION 44), STATION 1125.00 AND WL 183.00 (LOCATION 14) MIRROR EO. CORRECTIVE ACTION: REPAIRED RT KEEL BEAM WEB SECTION 44 STATION 1125 AND WL 183 IAW EO# 20366-7 REV IR.SDR ABXA20200803190Door Frame · damagedDURING MAINTENANCE VISIT AT HAECO GSO, PRODUCTION PERSONNEL REPORTED DAMAGE ON THE MAIN CARGO DOOR OPENING FORWARD FRAME STA 492 BETWEEN S-7L AND S-8L. DAMAGES ARE MINOR, HOWEVER, IAI B767 SRM SUPPLEMENT NOTES TO CONTACT IAI FOR ALLOWABLE DAMAGE LIMITS. THE SDR ABXA20200803191Door Frame · damagedDURING MAINTENANCE VISIT AT HAECO GSO, PRODUCTION PERSONNEL REPORTED DAMAGE ON THE MAIN CARGO DOOR OPENING AFT FRAME STA 632 BETWEEN S-6L AND S-8L. DAMAGES ARE MINOR, HOWEVER, IAI B767 SRM SUPPLEMENT NOTES TO CONTACT IAI FOR ALLOWABLE DAMAGE LIMITS. THE DAMASDR SWIA202053606Post · corrodedFS 280.00 RT DOOR POST BOTTOM ISLE SIDE, CORROSION AROUND FASTENER, MARKED. C-CHECK RO 10/22/2020. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PART ON RT BOTTOM DOOR POST AT FS 280.00, REF CRJ700 SRM. COMPLIED WITH SKYWEST TASK CARD STRUCTURAL MAJOR REPAIR (RSDR SWAA2020092417809Floor Skin · dentedFLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4-LBL 14 WL 207.54. DENT ON FLIGHT DECK FLOOR AT BS 255 RBL 4 TO LBL 14. REPAIRED IAW EA NO: 1-A53-33179 REV 1. 55981U 22SEP20.SDR 2A6D2020090302701Frame · chafedWEAR DAMAGE WAS NOTED ON THE LT X-FRAME P/N 350A21-4450.20 ON THE INSIDE AFT SURFACE OF THE LOWER LEG.SDR VNAA2020090299911Frame · corrodedFS 1047 FRAME IS CORRODED BETWEEN STRINGER 27 AND STRINGER 26L. REPAIRED FRAME SEGMENT.SDR VNAA202009029993ALintel · crackedSTRINGER 3L, PASSENGER DOOR LINTEL IS CRACKED AT FS 283. REPAIRED PER REO 670-53-21-1793 REV-P2.SDR VNAA202009029991Crossbeam · corrodedLT FS 280 CROSSBEAM IS CORRODED. INSTALLED NEW SERVICEABLE LT FS280 FLOORBEAM IAW SB670BA-53-041 REV H DATED JUNE 14/2019.SDR SWAA2020092914528Floor Skin · dentedCOCKPIT FLOOR DENTED AT STA 255.6. REPAIRED DENTED COCKPIT FLOOR AT STA 255.6, AS PER SWA EA NR: 1-A53-33179.SDR UIEA2020090431937Structure · crackedFX RT CENTER WING LOWER CHORD FOUND CRACK AT STA 1241 RBL 105. FX RT CENTER WING LOWER CHORD REPLACED AS PER SRM 51-10-02 AT STA 1180 TO 1241 RBL 105.SDR MK1Y20200831004Failsafe · corrodedCORROSION DAMAGE FOUND ON FAIL SAFE CHORD.SDR SWIA2020091452487Beam · corrodedFWD PAX DOOR LOWER BEAM, AFT ESCAPE FITTING FWD SIDE OF MOUNT POCKET HAS CORROSION ON EDGE OF POCKET, MARKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED FWD PAX DOOR LOWER BEAM WITH A NEW PART FROM FACTORY. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF ESDR AALA2020091439018Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED PRESSURE DECK PANEL INBOARD FASTENER HOLE AT FR 36L AND +Y1292. REPAIRED PRESSURE DECK PANEL, PER EO 5316Y209.SDR AALA202009119010Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLOOR PRESSURE DECK PLATE PANEL INBOARD FASTENER HOLE AT FR 36 AND -Y1292. REPAIRED FLOOR PRESSURE DECK PLATE PANEL PER EO 5316Y209.SDR MASA2020090530559Skin · puncturedPUNCTURE IN FUSELAGE AFT OF PAX DOOR FS 21-22 STR 13L-14L, REPAIRED IAW SRM.SDR SWAA2021070712837Panel · bentEXTERNAL POWER RECEPLACLE PANEL BENT. WILL NOT CLOSE MOD / C/W DVI OF GRD POWER RECEPTACLE DOOR PER E.A. NO 20-153-01597 REPLACED LATCHES AND SECURED GRD POWER RECEPTACLE DOOR. PERMANENT REPAIR LIMIT ACTION REQUIRED: ACCOMPLISH A PERMANENT REPAIR (REF 737-700
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