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 SWAA2024061886559Floorbeam · corrodedCORROSION ** AFT CABIN WET AREA FLOOR SUPPORT BEAM FASTENER HOLE FWD EDGE RBL 45 STA 986.5 MKD DOT<[01] REMOVED CORROSION ON FLOOR BEAM AT STA 986.5 RBL 45 AT FASTENER HOLE AS PER B 737 SRM 51-10-02-0G-0. EVALUATE DAMAGE: ORIGINAL MATERIAL 150'; MATERIAL LOST SDR SWAA2024061386561Floorbeam · crackedMAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL 1 MKD DOT<[01] SUMMARY <BR>REMOVED MAIN CABIN FLOOR PANEL 231UF FOR ACCESS PER B737-700 SRM 51-40-02-0G-0.<BR>REMOVED FLOOR SUPPORT BREAK AT STA 540 LBL 1 AS PER B-737 SRM 51-40-02-0G-0LOCATESDR IPXA2024060200520Floorbeam · corroded*SDR FILED OPEN* FAULT - CORROSION - FOUND M/D FLOOR BEAM CLIP CORROSION AT STA - 2100, LBL 16 (REPLACE) PAPER CHECK OK.SDR SWIA2024F00615Floorbeam · crackedLH COCKPIT FLOOR BEAM AT LBL12 IS CRACKED AT FS280 (C-CHECK RO 8/4/2024) REPAIRED LH COCKPIT FLOOR BEAM AT LBL12 REF CRJ700 SRM 53-11-43-201-003-A01 REV 38 JUL 25/2020. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWIA2024F00613Floorbeam · crackedRH COCKPIT FLOOR BEAM AT RBL12 IS CRACKED AT FS280 (C-CHECK RO 8/4/2024) REPAIRED RH COCKPIT FLOOR BEAM AT RBL12 REF CRJ700 SRM 53-11-43-201-003-A01 REV 38 JUL 25/2020. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWAA2024061485918Floorbeam · corrodedFLOOR STRUCTURE FLOOR BEAM AT MOUNT FITTING BS 947 RBL 50 HAS A SMALL AREA OF CORROSION AT MOUNT FITTING BASE<[01] REMOVED CORROSION ORIG. .180; MATERIAL LOSS .015; REMAINING .165 FOUND TO BE OUT OF LIMITS DUE TO LOCATION AT HARD POINT RBL 51 REF B737-NG SRM 5SDR R61A2024060500247Floorbeam · chafedWHILE IN HEAVY CHECK - INTERNAL FLOOR STRUCTURE CENTER CROSSBEAM AT FR 78 HAS 2EA SPOTS OF CHAFFING DAMAGE ON BOTTOM EDGE AS SEEN THROUGH AFT CARGO. COMPLIED WITH ETD2024-170-013947 BY FABRICATING AND INSTALLED AN ''L'' ANGLE REPAIR DOUBLER TO CROSSBEAM FRAMESDR YENA2024051500732Floorbeam · corrodedDURING HEAVY MAINTENANCE: CORROSION ON CROSS BEAM FR17-700 AT CABIN FLOOR STRUCTURE. (W1); REPAIRED PER EMB-190 SRM 51-10-03, SRM 51-12-01, ETI-19024-115 REV 3 AND ETD2024-190-011591.'SDR VNAA202407110020Floorbeam · crackedAFTER REMOVAL, CRACK ON FWD FLOOR SUPPORT ANGLE AT 280 FLOOR STRUCTURE. FLOOR SUPPORT ANGLE AT FS280 FLOOR STRUCTURE CRJ900 SRM 53-11-43-001-001-A01 ITEM 137SDR VNAA20240619005Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR BEAM RBL 12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1758 REV. --SDR VNAA20240619004Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1758 REV. --SDR SWAA2024061485499Floorbeam · corrodedFWD WET AREA FLOOR BEAM AT STA 328 AND RBL 45.50 HAS SIGNS OF CORROSION.<[01] REPAIRED IAW SRM 53-10-51-2R-7-B00540 (REPAIR 7 - SECTION 41 - DAMAGE ON THE UPPER CHORD OF THE FLOOR BEAM AT STA 328 - PERMANENT);[02] VERIFIED REPAIR ACCOMPLISHED IAW SRM 53-10-51-SDR AALA202405225910Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR BOARD SUPPORT BREAK ASSEMBLY PANEL AT STA 540. REPLACED BREAK ASSEMBLY PANEL PER SRM 51-40-02-0G.SDR AAL2024F00002Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR BOARD SUPPORT BREAK ASSEMBLY PANEL AT STA 540. REPLACED BREAK ASSEMBLY PANEL PER SRM 51-40-02-0G.SDR DALA2024051605262Floorbeam · corroded(LOG 0342534) CORROSION ON FLOOR BEAM STA 986 RBL 44 WL 208. ACCOMPLISHED REPAIR ON FLOOR BEAM STA 986 RBL 44 WL 208 PER B737-900 SRM. 53-70-51-2R-6.SDR DALA2024051505229Floorbeam · corrodedSHIP 3140 CORROSION FLOOR BEAM -Y464.8 AT LEVEL FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM -Y464.8 AT LEVEL FR68 AT AFT GALLEY AREA AS PER SRM A319 51-42-11-801. (0342357)SDR VNAA2024051700003Floorbeam · corrodedFLOOR CROSSBEAM AT F.S. 310.00 BETWEEN RBL. 9.00 AND R.B.L. 24.00 HAS CORROSION AROUND FASTENER HOLE. REPAIRED DAMAGE I.A.W. MHIRJ REO 690-53-21-1755 REV.A., DATED 2024-04-23SDR IPXA2024070830033Floorbeam · crackedFAULT STR FUSELAGE RH SIDE BETWEEN (Y= -450 TO Y= -953) FR 50 CROOSBEAM CROKED DOT 108-120. INSTALLED NEW CROSSBEAN IAW SRM 51-40-21 AND APPLIED CIC IAW EO NO:M-5100-2780-L. REVIEWEDSDR IPXA2024070830019Floorbeam · crackedFAULT STR FUSELAGE RH SIDE BETWEEN (Y= -450 TO Y= -953 FR 51 CROOSBEAM BROKEN DOT 108-119. VERIFIED CROSSBEAM REPLACEMENT AND INSTALLATION PER IAW A300-600 SRM 51-40-21. REVIEWEDSDR SWAA2024060684943Floorbeam · corrodedCORROSION FLOORBEAM LOCATED BS 947; RBL 50; WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOOR STRUCTURE BEAM LOCATED BS 947; RBL 50; WL 208.1 AT AFT GALLEY AREA THE REPAIR WAS ACCOMPLISHED IAW SRM 53-70-51-2R-5 WITH MINOR DEVIATIONS DOCUMENTED IN EA 24-153-01398. SDR SWAA2024060684947Floorbeam · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BS 947; LBL50; WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOOR STRUCTURE BEAM LOCATED BS 947; LBL38 TO LBL 60; WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM-53-70-51-2R-5 REPAIR 5; THIS IS REPAIR CATEGORY A .SDR FDEA202405120652Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FR67 CROSSBEAM BETWEEN Y1456 AND Y1959 FOUND A CRACK. REPAIRED THE CRACKED CROSSBEAM AT MAIN DECK CARGO COMPARTMENT FR67 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.14 FIGURE.211. THIS IS CATEGORY A REPAIR. MAJOSDR FDEA202405120651Floorbeam · crackedMAIN DECK CARGO COMPARTMENT CROSSBEAM FR30 BETWEEN Y1456 AND Y1959 FOUND A CRACK REPAIRED THE MAIN DECK CARGO COMPARTMENT CRACKED CROSSBEAM FR30 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.15 FIGURE 212 AND EA 6-5310-T0379137 P1. TITLE: FUSDR REXA2024102500981Floorbeam · crackedRH COCKPIT REPAIRED FLOORBEAM IS CRACKED ON OB REPAIR PART ON AFT ATTACHING FLANGE AT FWD SIDE OF FS 280. REPAIRED RIGHT COCKPIT FLOOR BEAM IAW IAW MHIRJ REO 690-53-11-1286 REV -A DATE 2021-12-09SDR REXA2024073000576Floorbeam · corrodedLH FS 280 CROSSBEAM IS HEAVILY CORRODED ON EDGE OF TOP FLANGE IN MULTIPLE LOCATIONS AND REQUIRES REPLACEMENT. REMOVED F.S. 280 L/H CROSS BEAM IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01. INSTALLED NEW SERVICEABLSDR REXA2024073000575Floorbeam · corrodedF.S. 280 R/H CROSS BEAM IS HEAVILY CORRODED IN RADIUS. REMOVED F.S. 280 R/H CROSS BEAM IAW CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01. INSTALLED NEW SERVICEABLE RH FS 280 CROSSBEAM PN: CC670-34094JP-2S IAW CRJ 900 SDR CALA2024051301463Floorbeam · corrodedAFT PASSENGER COMPARTMENT WET AREA FLOOR BEAM. HAS POSSIBLE CORR OSION STA 986.5 LBL 12. (REF. AAR NR 100010373) REPAIRED FLOOR BEAM STA 986.5 LB 12 ALL WORK DONE IAW SRM 51-10-02, 53-70-51-1A-1,53-70-51-26-6, AMM 20-60-07-913-801 , SOPM 20-10-03, SRM 51-21-01SDR CALA2024052701591Floorbeam · corrodedAFT CABIN STA 986.5 BETWEEN RBL 17 AND 45 WL 208.1 FLOOR BEAM HAS CORROSION.(REF AAR NR 9884765) REPAIRED AFT CABIN STA 986.5 BETWEEN RBL 17 AND 45 T CHORD BAL 1505-1014747050-T6511. ANGLE BAC WL 208.1 FLOOR BEAM IN REF SRM 53-70-37-2R-4 149028117075T6 PO #203SDR YENA2024051500744Floorbeam · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / FORWARD FUSELAGE / CROSS BEAM AT FR17 Y=700 / EXISTING DOUBLER / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2024051500742Floorbeam · corrodedDURING HEAVY MAINTENANCE: CORROSION ON CROSS BEAM FR17-700 AT CABIN FLOOR STRUCTURE. (W1); (RESOLVED ON W/O: 1308135 TASKCARD: NR-00015 ) REPAIRED PER EMB-190 SRM 51-10-03, SRM 51-12-01, ETI-19024-115 REV 3 AND ETD2024-190-011591.SDR YENA2024051500740Floorbeam · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON CROSS BEAM LOCATED BTW FR84 AND Y=800LH TO Y=1080LH OF CABIN PAX FLOOR STRUCTURE AT CENTER FUSELAGE III (W2); (RESOLVED ON W/O: 1308135 TASKCARD: NR-00009 ) REF TOMEX WO N265JB/2552/E1SDR YENA2024051500735Floorbeam · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON CROSS BEAM LOCATED BTW FR84 AND Y=800LH TO Y=1080LH OF CABIN PAX FLOOR STRUCTURE AT CENTER FUSELAGE III (W2); REF TOMEX WO N265JB/2552/E190/BRIDGE CHECK NR 00085 CORROSION ON CROSS BEAM SDR SWIA2024F00572Floorbeam · corrodedFLOOR SUPPORT ON THE AFT SIDE OF THE FS280.00 FRAME HAS CORROSION. (C-CHECK RO 7/9/2024) INSTALLED NEW FLOOR SUPPORT PER CRJ 900 SRM 51-42-21-001-001-A01, CRJ 900 SRM 51-42-06-001-001-A01, AND CRJ 900 SRM 51-23-00-001-001-A01. CRJ 900 SRM 51-42-13-001SDR SWAA2024061484289Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 LBL43 WL208. MARKED<[01] ACCOMPLISHED REPAIR PER SRM 53-70-51-2R-6 REPAIR 6;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024061484282Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL43 WL208. MARKED<[01] REMOVED AND REPLACED REPAIR PARTS PER SRM 51-40-02 AS SHOW IN SWA EA# 1-753-33013 REV IR;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.;[03] VERIFIED ALL STEPS AND CORRSDR AALA202406103672Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER CHORD (T-CAP) OF FLOORBEAM AT STA 986, LBL 48. REPAIRED CHORD PER SRM 53-70-51-2R.SDR SWAA2024060684064Floorbeam · damagedELONGATED HOLE IN FWD FLANGE OF BS 887 FLOOR BEAM; RBL 4; WL 208. DAMAGE WAS FOUND TO A FLOOR PANEL ATTACH HOLE IN THE FWD FLANGE OF THE BS 887 FLOOR BEAM (146A5518-7#C) AT RBL 4. THE DAMAGE WAS REMOVED BY OVERSIZING THE HOLE. THERE ARE NO ALLOWABLE DAMAGE LISDR SWAA2024060683900Floorbeam · corrodedCORROSION AROUND FITTING ON FLOOR BEAM BS 947; RBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947 RBL 50 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.180' REMAINING THICKNESS IS 0.100' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51SDR SWAA2024060683901Floorbeam · corrodedCORROSION AROUND FITTING ON FLOOR BEAM BS 947; LBL 25 (MARKED)<[01] REMOVED DAMAGE ON BS 947 LBL 25 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.180' REMAINING THICKNESS IS 0.105' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51SDR SWAA2024060683904Floorbeam · corrodedCORROSION AROUND FITTING ON FLOOR BEAM BS 947; LBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947 LBL 50 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.180' REMAINING THICKNESS IS 0.100' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51SDR SWAA2024060484156Floorbeam · cracked(CUSTOMER REQUEST) PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-293943<[01] REPLACED NEW SUPPORT BREAK INSTALLED NEW SUPPORT BREAK LOCATED ON PASSENGER CABIN; FLOOR STRUCTURE AT STA 540; BL 0 TO RBL 24.75 IAW B737-700 SSDR ASAA2024050949961Floorbeam · corrodedAFT WET AREA STA 986 FLOOR BEAM HAS AREAS OF CORROSION RBL 5 TO RBL 60. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REPAIRED STA 986 FLOOR BEAM IAW B737-800 SRM 53-70-51-2R-4W 1 O .150 R .090 L 1 D .060.SDR ASAA2024050949926Floorbeam · corrodedAFT WET AREA STA 947 FLOOR BEAM HAS SPOTS OF CORROSION RBL 5 TO LBL 5. GROUNDED - YES. REMOVED CORROSION FROM 947 FLOOR BEAM FROM RBL 5 TO LBL 25 DETERMINED TO BE OUT OF LIMITS IAW BOEING 737-800 SRM 53-70-51-1A-1 REPAIRS MADE IAW BOEING 737-800 SRM 53-70-51-2SDR ASAA2024050949925Floorbeam · corrodedAFT WET AREA FLOOR SUPPORT STA 950 LBL 25 TO LBL 45 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1, REMOVED AND REPLACED FLOOR SUPPORT IAW B737-800 SRM 51-40-02W= 1.0" O= .080 R= .068 L= 2.0" D= .012.SDR ASAA2024050949924Floorbeam · corrodedAFT WET AREA STA 986 FLOOR BEAM HAS AREAS OF CORROSION LBL18 TO LBL 60. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REPAIRED DAMAGE IAW B737-800 SRM 53-70-51-2R-6W= 2 O= .150 R= .028 L= 1.5 D= .122.SDR DALA2024051405179Floorbeam · corroded(LOG 0336505) 986.5 FLOOR BEAM HAS CORROSION FROM LBL43-RBL45 WL208. C/W ER/A 617771-14 REV ORIGINAL.SDR FDEA202405090631Floorbeam · gougedMAIN CABIN FLOOR BEAM FWD WEB AND BTM SURFACE OF UPPER T-CHORD AT STA 580 RBL35 HAVE GOUGE. THIS IS MAJOR REPAIR. ACOMPLISHED EA T F-5310-T0378982 P1 FUSELAGE- MAINFRAME-FLOOR BEAM WEB, STA 580 RBL 35, GOUGE REPAIR.SDR JR2R20240509054Floorbeam · corrodedFLOOR BEAM AT FR87 LBL10 CORRODED. REPAIRED.SDR 2A6D20240509003Floorbeam · corrodedDAMAGE IS ON THE LH CABIN FLOOR EDGE FITTING (P/N: 350A214753.20) IN THE FORM OF CORROSION AND CRACKS. THE LH FITTING PLATE IS EXCESSIVELY CORRODED AND THE CRACK DAMAGES AT TWO FASTENER HOLES TO EOP WHICH RESULTS IN REPLACEMENT OF LH FITTING.SDR SWAA2024052983791Floorbeam · crackedAAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. 2024-286867<[01] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO RBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9<BR>S
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