JASC 5315
Service difficulty reports · 44,218
Reports filed under 5315 · Fuselage Main, Floor Beam, 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 = '5315' 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 = '5315' 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 SWAA2020081001135Floorbeam · corrodedFLIGHT DECK FLOOR LATERAL BEAM AT BS 270 HAD CORROSION BETWEEN LBL 3.5 AND LBL 6.5 UPPER FORWARD FLANGE. WL 207.54. ACCOMPLISHED REPAIR AT FLIGHT DECK LATERAL BEAM STA 270 BETWEEN LBL 3.5' AND LBL 6.5' UPPER FORWARD FLANGE IAW EA # 20-153-01200, REV IR.SDR ASAA2020080372962Floorbeam · corrodedSTA 986 FLOOR BEAM HAS CORR AT NUTPLATE HOLE RBL 48. GROUNDED - YES. REMOVED CORR, FOUND TO BE OUT OF LIMITS IAW B737 800 SRM 53 70 51 1A 1 CUT OUT DAMAGED SECTION OF FLOOR BEAM AND ACCOMPLISHED PERMANENT REPAIR IAW B737 800 SRM 53 70 51 2R 4 REP 4 W 2 O .150 SDR ASAA2020072472925Floorbeam · corrodedSTA 986 FLOOR BEAM HAS CORR AT NUTPLATE HOLE LBL 48. GROUNDED - YES. BLENDED OUT CORR ON FLOOR BEAM AT STA 986, LBL 48. AREA FOUND TO BE OUT OF LIMITS IAW B737 800 SRM 53 70 51 1A 1 FIG 104.C. FABBED REPAIR PART IAW B737 800 SRM 53 70 51 2R 6 AND INSTALLED IAWSDR FDEA202007171569Nut Plate · corrodedMAIN CABIN, FWD R/H WET AREA, FLOOR BAEM CORRODED AT NUT PLATES STA 325 RBL 35-58 REMOVED CORROSION ORIGINAL THICKNESS .120 REMOVED .011 NEW THICKNESS .109 WICH IS FOUND TO BE WITHIN LIMITS WICH IS FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-10-08-1A AND BOESDR FDEA202007161533Floorbeam · corrodedFLOOR BEAM LOWER NUT PLATE STRIP IS CORRODED BS 1681.8 LBL 4. REMOVED AND REPLACED FLOOR BEAM LOWER NUTPLATE STRIP AT BS 1681.8 LBL 4, IAW FEDEX B757 SRM 51-40-02 AND DWG 146N5693 REV C.SDR SWAA2020081702378Floorbeam · crackedCRACKED FLOORBEAM AT BS 540, BL 0 - LBL 24.5, WL 208.1. REMOVED AND INSTALLED NEW FLOORBEAM IAW SRM 51-40-02-0G-0.SDR SWAA2020081702679Floorbeam · corrodedCORROSION ON AFT BULKHEAD LOWER SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL23 TO RBL23 WL157. CORROSION FOUND ON FCB AFT BULKHEAD LOWER SUPPORT ANGLE BS-500D LBL-23 TO RBL-23 WL-157 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS REPAIRED BY REPLACEMENT SDR SWAA2020081702691Floorbeam · corrodedCORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 RBL20 WL181. MARKED / REMOVED AND REPLACED AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 RBL20 TO LBL10 WL181 IAW SRM 51-40-02 REF DWG 149A8117.SDR IPXA202008058655Floorbeam · crackedINSPECTION TYPE: C3, FWD CARGO BAY STA 6-70 FLOORBEAM UNDER RT SIDE RAIL HAD A CRACK. REPAIRED THE FLOORBEAM IAW SRM 53-40-51, REPAIR 1, FIG 202, REV 67. MAJOR REPAIR.SDR FDEA2020072361533Floorbeam · corrodedFLOOR BEAM LOWER NUT PLATE STRIP IS CORRODED BS 1681.8 LBL 4 REMOVED AND REPLACED FLOOR BEAM LWR NUTPLATE STRIP AT BS 1681.8 LBL 4 IAW FEDEX B757 SRM 51-40-02 AND DWG 146N5693 REV CSDR FDEA2020072361532Floorbeam · corrodedFLOOR BEAM LOWER NUT PLATE STRIP IS CORRODED BS 1681.8, LBL39 REMOVED AND REPLACED FLOOR BEAM LWR NUTPLATE STRIP AT BS 1681.8 LBL 39 IAW SRM 51-40-02 AND DWG 146N5693 REV CSDR AALA2020072219017Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE, CRACK IN FLOOR BREAK, INSTALLED NEW BREAK IAW SRM 51-40-02.SDR FDEA202007161542Floorbeam · corrodedMAIN CABIN, FWD RIGHT WET AREA , PRIOR TEE CAP REPAIR HAS CORROSION AT SEAT TRACK AREAS, BS 365 BL 0 TO RBL 64. REMOVED CORROSION, ORIGINAL THICKNESS (.125") REMOVED (.005") REMAINING (.120") CROSSECTIONAL AREA IS LESS THAN 5% WITH A1=.250" AND A2= .0025SDR FDEA2020071761535Floorbeam · corrodedFLOORBEAM UPPER SURFACE WAS CORRODED AT SEVERAL AREAS, BS 1681.8, LBL 4 - LBL 47. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53-60-51-1A, TREATED BARE METAL IAW SRM 51-20-01.SDR FDEA2020071761534Floorbeam · corrodedFLOORBEAM UPPER SURFACE WAS CORRODED, BS 1681.8, RBL 11. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53- 60-51-1A, TREATED BARE METAL IAW SRM 51-20-01.SDR FDEA2020071761533Nut Plate · corrodedFLOORBEAM LOWER NUT PLATE STRIP WAS CORRODED AT BS 1681.8, LBL 4. REMOVED AND REPLACED THE FLOORBEAM LWR NUTPLATE STRIP IAW SRM 51-40-02, AND DWG 146N5693, REV C.SDR FDEA2020071761532Nut Plate · corrodedFLOORBEAM LOWER NUT PLATE STRIP WAS CORRODED, BS 1681.8, LBL 39. REMOVED AND REPLACED THE FLOORBEAM LWR NUTPLATE STRIP IAW SRM 51-40-02, AND DWG 146N5693, REV C.SDR FDEA2020072351517Floorbeam · corrodedMAIN DECK STA 1015 BETWEEN LBL24.75-LBL45.5 FLOOR SUPPORT CORRODED REMOVED CORR ON FLOOR SUPPORT STRAP ONLY IAW B757 SRM 51-10-02. ORIG MAT .012 REM .005 LOSS .007 FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101. REMOVE, FABRICATED AND INSTALLED NEW SDR AALA2020072219016Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE, CRACK IN END OF BREAK, REPLACED BREAK WITH NEW IAW SRM 51-10-02.SDR FDEA2020071751517Strap · corrodedMAIN DECK BS 1015 BETWEEN LBL 24.75 - LBL 45.5 FLOORBEAM CORRODED. REMOVED THE CORROSION ON THE STRAP ONLY IAW SRM 51-10-02. ORIG MAT .012 REM .005 LOSS .007, FOUND OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101. REMOVED, FABRICATED AND INSTALLED A NEW STRASDR KCSA202007151119Floorbeam · corrodedFLOORBEAM UPPER CHORD HAS CORROSION AT STA 2240 APPROXIMATELY AT RBL 72 ON MAIN DECK.SDR KCSA202007151118Floorbeam · corrodedFLOORBEAM UPPER CORD CORRODED AT STA 2240 - BL 65 NEXT TO L5 DOOR.SDR SWIA2020090252178Floorbeam · crackedFS 484 ANGLE CLIP ON OB SIDE OF RBL 27 FLOOR BEAM IS CRACKED. C-CHECK RO 8/29/2020. R & R ANGLE CLIP ON OB SIDE OF RBL 27 IAW CRJ-200 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA202008252017Floorbeam · corroded* A BAY - FS 280 - FLOORBOARD BRKT ON 280 FACING AFT CORRODED @ MULTIPLE LOCATIONS AS MARKED (C-CHCECK 8/23/2020) / REPLACED A BAY - FS 280 - FLOORBOARD BRKT ON 280 FACING AFT REF CRJ700SRM.SDR FDEA2020080541507Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64 , BETWEEN -Y953 AND -Y1456 REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR CROSSBEAM AT FR64 , BETWEEN -Y953 AND -Y1456. PER A300-600F SRM51-10-15 FIG211.THIS REPAIR WAS CATEGORY CATEGOSDR FDEA2020080514506Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACKED, AT FRAME 64, BETWEEN -Y1456 AND -Y1959. REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR CROSSBEAM IAW SRM 53-10-15 FIG211. THIS REPAIR WAS CATEGORY A REPAIR, MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA2020080314507Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOORBEAM CRACKED, AT FRAME 64 , BETWEEN -Y953 AND -Y1456. THE FLOORBEAM WAS REPAIRED IAW SRM 51-40-21, & SRM 53-10-15, FIG 211. CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA2020080314506Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOORBEAM CRACKED, AT FRAME 64, BETWEEN -Y1456 AND -Y1959SDR SWAA2020073099920Floorbeam · corrodedAFT GALLEY FLOORBEAM STA 947.5 LBL 6 AND LBL 14 HAS CORROSION ON INSIDE AND AROUND AFT SCREW HOLES. REMOVED CORROSION AND REPAIRED IAW EA 20-153-01120 PART 1 AND 2K, AND SRM 53-70-51-2R-8.SDR AALA202007279023Floorbeam · wornAIRCRAFT IN BASE MAINTENANCE: WEAR TO FLOOR BEAM AT STA 445 AND RBL 6, MEASURING L=1.0 IN, W=2.0 IN, D=0.008 IN. ACCOMPLISHED PERMANENT REINFORCING SPLICE REPAIR IAW SRM 53-00-53-2R-2.SDR COEA2020082804807Floorbeam · corrodedWO 216488 NR 100010 HEAVY CHECK COE, MINOR REPAIR. FLOORBEAM 39 TOP SURFACE HAS LEVEL 2 CORROSION BETWEEN AFT CARGO DOOR THRESHOLD AND SERVICE DOOR THRESHOLD. CORRECTIVE ACTION: REPLACED WITH OEM PART.SDR COEA2020082803807Floorbeam · corrodedWO 216488 NR 100009 HEAVY CHECK COE, MINOR REPAIR. FLOORBEAM 38 TOP FLANGE HAS LEVEL 2 CORROSION BETWEEN AFT CARGO DOOR THRESHOLD AND SERVICE DOOR THRESHOLD. CORRECTIVE ACTION: REPLACED WITH OEM PART.SDR SWIA202008252012Floorbeam · crackedLEFT FS274 CRACKED LEFT OF LBL9.00. REPAIRED CRACKED LEFT FLOORBEAM LBL9.00 AT FS280.00 TO FS265.00 REF CRJ700 SRM.COMPLIED WITH STRUCTURAL MAJOR REPAIR AND FORM M-337 ATTACHED.SDR VNAA202007139994Angle · corrodedFS 280 J-ANGLE LOCATED AT FLIGHT DECK ENTRANCE IS CORRODED AT 2 PLACES ON UPPER SURFACE. REMOVED FS 280 J-ANGLE AND INSTALLED NEW SERVICEABLE FS 280 J-ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.SDR SWAA2021072200922Floorbeam · corroded***CORROSION*** ON FLOOR SUPPORT SPLICE AT ACB BS727D+6 LBL18 TO RBL18 WL156. / RECEIVED NEW/SERVICABLE FLOOR SUPPORT SPLICE AT ACB BS 727D+6 LBL18 TO RBL18 TO BC INSTALLED ON JPANEL-141-CLOSE; 57609U 21JUL20SDR SWIA2020081151747Angle · corrodedBS 280 J ANGLE WAS CORRODED ALONG ENTIRE LENGTH, REMOVED AND REPLACED THE FWD J CHANNEL IAW SRMSDR SWIA2020081151737Angle · crackedF.S.280.00 FLOORBEAM CLIPS ON THE INBOARD SIDE OF LBL 9.00 AND RBL 9.00 ARE CRACKED. REMOVED AND REPLACED LBL9 AND RBL9 IB CLIPS IAW SRM.SDR SWIA2020072951536Floorbeam · crackedFS280 LOWER BULKHEAD STIFFENER AT RBL 26 FOUND CRACKED (C-CHECK) RO 7/25/2020 REPLACED RBL26 LOWER BULKHEAD STIFFENER AT FS280.00 REF CRJ-700 SRM AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASKCARD.SDR AALA202007279025Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO LOWER FLOOR ATTACH ANGLE FOR FWD CARGO AFT BULKHEAD CENTER ACCESS PANEL AT STA 500I AND STR 26L-26R, MEASURING L=1.0 IN, W=1.0 IN, D=0.05 IN. REPLACED ATTACH ANGLE WITH NEW IAW SRM 51-40-02 AND AARD 51-00-05-1.SDR SWIA202082051866Angle · crackedCOCKPIT FLOOR SUPPORT GUSSET IS CRACKED ON FWD SIDE ON THE FS 280.00 CROSS-BEAM AT RBL 9. REMOVED AND REPLACED COCKPIT FLOOR SUPPORT GUSSET ON FWD SIDE OF FS280.00 CROSS-BEAM AT RBL 9 IAW SRM AND DWG.SDR AALA2020072439001Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR BEAM AROUND FLOOR PANEL HOLE AT FR68 AND WL Y765, MEASURING L=0.5 IN, W=0.075 IN, D=0.027 IN. FLOOR BEAM REPLACED IAW SRM 51-42-11 AND AIRBUS DRAWING D53472001.SDR FDEA202007091480Floorbeam · crackedMAIN DECK FLOOR BEAM CRACKED, BS 580 BELOW SEAT TRACK LBL 44.5. TRIMMED UPPER FLANGE OF THE FLOORBEAM SPLICE, FABRICATD A REPAIR ANGLE , RADIUS STRAP, AND INSTALLED IAW EA TF-5310-T0355035 P1.SDR FDEA2020071091480Floorbeam · crackedMAIN DECK FLOORBEAM CRACKED BS 580 BELOW SEAT TRACK LBL 44.5.SDR SWAA2021072298527Floorbeam · crackedCABIN FLOOR STRUCTURE; STA 540; LBL 1; PNL BRAKE STRUCTURE IS CRACKED. / REMOVED CRACKED PANEL BRAKE STA 540BL0 TO LBL 24.5 AND INSTALLED NEW PANEL BRAKE ALL IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV B. APPLIED CIC IAW AMM 51-21-91-620-802.SDR SWAA2020080600155Floorbeam · crackedCRACKED FLOORBEAM, BS 540, BL 0 - LBL 24.5, WL 208.1. REMOVED THE CABIN FLOORBEAM IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW FLOORBEAM ANGLE IAW SRM 51-40-05-0G-0, AND DWG 143A5240, REV-B. AND INSTALLED THE NEW FLOORBEAM IAW SRM 51-40-02-0G-0, AND DSDR SWIA2020081251770Floorbeam · corrodedLH FLOOR BEAM LBL9 CORRODED FS693.00 (MARKED) (C-CHECK) RO 8/10/2020 REPAIRED LH LBL9 FLOOR BEAM AT F.S. 693.00, REF MHIRJ REO COMPLIED WITH SKYWEST TASK CARD STRUCTURAL MAJOR REPAIRSDR SWIA2020081251769Floorbeam · corroded* RH FLOORBEAM AT FS693.00 IS CORRODED. FLAGGED. REPAIRED LBL 9 FLOORBEAM AT BS 693, REF REO.SDR SWAA2020081098605Floorbeam · crackedCRACKED FLOOR PANEL SUPPORT AT B.S. 540; B.L. 0 - L.B.L. 24.5; W.L. 208.1. / REPLACED CRACKED FLOOR SUPPORT AT BS540 BL0-LBL24.5 WL208.1 PER SRM 51-40-02-0G-0 AND AIPC 53-31-00-05. 57449U 8JUL20SDR SWIA2020082051885Floorbeam · cracked*FS280 CROSS-MEMBER, RBL9 OUTBD ANGLE POSSIBLE CRACKED. FLAGGED (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED FS280 CROSS-MEMBER, RBL9 OUTB ANGLE (P.N. CC670-34099-2) REF. CRJ700 SRM AND DWG.SDR SWIA202082051853Floorbeam · crackedUNDER THE COCKPIT WHERE FLOORBEAM RBL 9 AND BS 280 ARE ATTACHED. THE RT COCKPIT FLOORBEAM POSSIBLY BE CRACKED ON THE OUTBD SIDE. NDT CONFIRMED THE CRACK. PERFORMED A FLOORBEAM REPAIR IAW SRM.
Back to JASC 5315