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 VNAA202407120041Floorbeam · corrodedHN00147598 DISCREPANCY: LBL 27 FLOOR BEAM IS CORRODED AT F.S. 1031. CORRECTIVE ACTION: REPAIRED/REPLACED CORRODED SECTIONS OF FLOOR BEAM AT LBL 27 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2254 REV -- DATED 2024-04-05.SDR VNAA202407120039Floorbeam · corrodedHN00147488 DISCREPANCY: FS 280 FWD FLOOR SUPPORT ANGLE IS CORRODED AT LBL 9. CORRECTIVE ACTION: REMOVED J-ANGLE @ FS 280 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE J-ANGLE PN/ CC670-34095-1SB - ASSY, ANGLE IAW CRJ70SDR VNAA202407120007Floorbeam · corrodedHN148582 DISCREPANCY: FS 280 FRAME AFT AVIONICS BAY FLOORBOARD SUPPORT ANGLE IS CORRODED BETWEEN LBL 26 AND RBL 26. CORRECTIVE ACTION: REMOVED UNSERVICEABLE FLOORBOARD SUPPORT ANGLE IAW CRJ700 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE ANGLESDR VNAA202407120006Floorbeam · crackedHN148550 DISCREPANCY: LBL9 FLIGHT COMPARTMENT FLOOR BEAM IS CRACKED ON THE FWD SIDE OF F.S. 280. CORRECTIVE ACTION: REPAIRED FLIGHT COMPARTMENT FLOOR BEAM IAW CRJ 700 SRM 53-11-43-201-003-A01SDR VNAA202407120001Floorbeam · corrodedHN148044 DISCREPANCY: RBL 27 FLOOR BEAM IS CORRODED FROM 1007 TO FS 1024. CORRECTIVE ACTION: REPAIRED RBL 27 FLOOR BEAM IAW CRJ-700 SRM 53-00-41-201-001-A01 AND MHIRJ REO 670-53-61-2254 REV-- DATED 2024-04-05.SDR SWAA2024072310835Floorbeam · corrodedDUE TO INTERFERENCE WITH BL 0 INTERCOSTAL ON FWD SIDE OF FLOOR BEAM; REPAIR AT BS 294.5 FLOOR BEAM AT BL 0 REQUIRES RE-MAKING REPAIR PARTS AND INSTALLING ON UPPER SIDE OF FLOOR BEAM.<[01] REPAIRED FLOOR BEAM BS 294.5; BL-0; PER SRM 53-10-51-2R-14 ALTERNATIVE 2SDR DALA2024071907279Floorbeam · corroded(LOG 0449041) CORROSION ON FLOOR BEAM WL-208, STA-947.5, RBL-50. FLOOR BEAM WL-208, STA 947.5, FROM RBL 38 TO 60 WAS REPAIRED IAW B737-800 SRM 53-70-51-2R-5.SDR DALA2024071007006Floorbeam · corroded(LOG 0438541) CORROSION OUT OF LIMITS ON FLOOR SUPPORTS BTW STA 727A LBL 13.84 AND RBL 12.5 AND STA 727I RBL 8.1 AND 3.0. FLOOR SUPPORT STA 727A LBL 13.84 AND RBL 12.5 WERE REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 3 REPAIR 3 AND FLOOR SUPPORT ON STA. 72SDR AALA202407316020Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 20 AND -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.SDR SWIA202409160814Floorbeam · crackedFS280.00 CROSSBEAM BL9R OUTBOARD ANGLE CRAKED IN ANGLE RADIUS (C-CHECK RO 9/15/2024) REMOVED AND INSTALLED NEW OUTBOARD ANGLE P/N CC670-34099-2SB AT RBL9.00 FS 280.00 REF CRJ900 SRM 51-42-21-01-001-A01 AND DWG CC670-34010 REV -K SKYWEST TASK CARD 51-90SDR SWIA202409160811Floorbeam · crackedFS280.00 CROSSBEAM BL9L OUTBOARD ANGLE CRAKED IN ANGLE RADIUS (C-CHECK RO 9/15/2024) REMOVED AND REPLACED NEW OTBD ANGLE AT LBL9 FS280 REF CRJ 900 SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV K. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE SDR CALA2024081202193Floorbeam · corrodedIT WAS FOUND CORROSION UPPER SURFACE PLATE FLOOR BEAM STRUCTURE STATION 303 LBL 20 TO 54. ( ORIGINATING DOCUMENT NR 2080547)SDR AALA202408122733Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER CHORD OF PASSENGER CABIN FLOOR BEAM AT STA 947, RBL 25. REPLACED UPPER CHORD (T-CAP) PER SRM 53-70-51-2R-5.SDR DALA2024071207064Floorbeam · corroded(LOG 0440101) CORROSION ON FLOOR BEAM WL-208, STA-947.5, RBL-4. REPAIRED DAMAGED AREA I.A.W B737 SRM 53-70-51-2R.SDR SWI2024F00806Floorbeam · corrodedCABIN FLOOR LEFT T CAP LBL27 BETWEEN APPROXIMATELY FS1010.00 AND FS1040.00 CORRODED AS MARKED (C-CHECK RO 9/15/2024) BLENDED CORROSION @ LBL 27 FS 1000-1040 AND FOUND OUT OF LIMITS, REPAIRED PER CRJ900 SRM 53-00-41-201-001-A03 AND COMPLIED WITH ALL STSDR SWIA20240916706Floorbeam · corrodedCABIN FLOOR LEFT T CAP LBL9 BETWEEN APPROXIMATELY FS1010.00 AND FS1065.00 CORRODED AS MARKED (C-CHECK RO 9/15/2024) FOUND TO BE OUT OF LIMITS, INSTALLED NEW LBL9 FLOOR BEAM REPAIR AT FS1005 TO FS1056 REF CRJ900 SRM 53-00-41-201-001-A03, CRJ900 SRM 51-42SDR SWAA2024082609807Floorbeam · corrodedCORROSION ON FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-420778<[01] FLOR BEAM UPPER SURFACE LOCATED BS 986.5 LBL43 AFT GALEY AREA MUST BE REPAIR DUE TO CORROSION EXCEED ALLOWABLE DAMAGE LIMITS IAW B737-700 SRM 53-70-51-1A-1 ALLOWABLE DSDR DALA2024070906950Floorbeam · corroded(LOG 0434122) CORROSION ON FLOOR SUPPORT BEAM AT WL-208, STA-328, RBL-13. REPAIRED FLOOR SUPPORT BEAM I.A.W B737-800 SRM 53-10-51-2R 8-. ALTERNATIVE 3.SDR VNAA202407050004Floorbeam · corrodedUPON REMOVAL OF CORROSION CAP PLATE FOUND CORROSION ON FS 280 L/H CROSS BEAM BETWEEN BL 0 AND LBLSDR VNAA202407050002Floorbeam · crackedL/H COCKPIT FLOOR BEAM IS CRACKED AT FS 280.SDR SWAA2024070509040Floorbeam · crackedCABIN FLOOR BOARD PANEL BREAK ASSEMBLY AT STA. 540 CRACKED AT INBOARD END L/H OF CENTER IN A/C DISTRIBUTION BAY.<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.;[02] IS: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51SDR SWAA2024070509041Floorbeam · crackedCABIN FLOOR BOARD PANEL BREAK ASSEMBLY AT STA. 540 CRACKED AT INBOARD END RIGHT OF CENTER IN A/C DISTRIBUTION BAY.<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.;[02] IS: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM SDR SWAA2024081309096Floorbeam · corrodedCORROSION ON TOP FLANGE OF BS 986.5 FLOOR BEAM RBL 45-RBL 28 AND LBL 44 WL 208<[01] COMPLETED STEP 1; UPDATED TABLE;[02] EDITED STATEMENT;[03] EVALUATED CORROSION ON TOP FLANGE OF BS 986.5 FLOOR BEAM RBL 45-RBL 28 AND LBL 44 WL 208. FOUND TO BE OUT OF LIMITS DSDR VNAA202408090013Floorbeam · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00. CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PESDR ASAA2024070351520Floorbeam · corrodedCABIN FLOORBEAM CORROSION FR-16 -Y254 GROUNDED - YES. REMOVED CORROSION IAW A320 SRM 51-74-00/001 REV. 149- 01 MAY 2024 ON RAIL P/N: D5313531220001 FR16, -Y254, Z1955 IN AN AREA MEASURING 1.1" X .5". ORIGINAL THICKNESS BEFORE RE-WORK .087, REMOVED .020, AMOUNTSDR CALA2024072202075Floorbeam · corrodedFWD PASSENGER COMPARTMENT, STA 344 FLOOR BEAM IS CORRODED IN MULTIPLE LOCATIONS FROM LBL 3 TO LBL 60 AND WAS REPAIRED ON BAM NON-ROUTINE 002006247. A SIGNIFICANT FINDING REPORT IS REQUIRED TO BE ISSUED. ENTERED INTO ESFR SYSTEM. REFERENCE BAM NR 2006247SDR DALA2024070506789Floorbeam · corroded(LOG 0427216) CORROSION ON FLOOR BEAM UPPER SURFACE AND FASTENERS HOLES STA 985.5 AND LBL.45 TO RBL.45 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR BEAM STA.986.5 WAS REPAIRED PER B737-800 SRM 53-70-51-2R REPAIR 4.SDR DALA2024070506788Floorbeam · corrodedFLOOR ANGLE: 1EA ( STA. 991 AND RBL.34 TO RBL.45) ( OUT OF LIMITS ) AT PASSENGER CABIN. FLOOR ANGLE STA. 991 AND RBL.34 TO RBL.45 AT PASSENGER CABIN WAS REPLACED PER DWG 147A5700 REV.C AND B737-800 SRM 51-40-02-0G.SDR DALA2024070506787Floorbeam · corroded(LOG 0427149) CORROSION ON FLOOR BEAM BELOW LAVATORY ATTACH FITTING BTW STA. 947.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR BEAM BELOW LAVATORY ATTACH FITTING BTW STA. 947.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER B737-800 SRSDR SWAA2024080908355Floorbeam · corrodedCORROSION FLOOR BEAM LOCATED BS 986.5 AND RBL 44 WL 208.1 AT AFT GALLEY AREA 2024-414886<[01] TOOL USED STEP 9: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600; S/N: 60007161486; DUE DATE: 28 JULY 24.;[02] STEPS 12 AND 13 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 5SDR DALA2024070406750Floor Support · corrodedELONGATED HOLE FLOOR SUPPORT +Y1292 AT LEVEL FR66 AT AFT GALLEY AREA. REPLACED FABRICATED FLOOR SUPPORT Y1292 POSITIVE, BRACKETS (3 E/A) AND SPLICES (4 E/A) LOC. BTW FR64 TO FR66 AT LEVEL STR23L AFTGALLEY AREA ASPER A320 SRM 51-42-11 AND DWG# 10N01474, REVISIOSDR SWIA202408260701Floorbeam · crackedCRACK FOUND ON R/H FLOOR SUPPORT ANGLE COMMON TO CENTER FLOORBEAM AT FS 280.0 RBL 12.0 (C-CHECK RO 8/24/2024) REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT RBL 12.0 FS 280.0 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV-G. COMPLIED WITH SKYWSDR SWAA2024080907945Floorbeam · corrodedCORROSION FLOOR BEAM LOCATED BS 947.5 AND LBL 24 WL 208.1 AT AFT GALLEY AREA 2024-414863<[01] TOOL USED ON STEP 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] PERFORMED REPAIR ON FLOOR BEAM LOCATED BS 947.5 AND LBL 24 WL 208.1 ASDR DALA2024070506766Floorbeam · corroded(LOG 0423548) CORROSION OUT LIMITS ON FLOOR " T" SUPPORT 1EA (BTW. STA.947.5 AND RBL.26.5 TO RBL.49) AT PASSENGER CABIN FLOOR STRUCTURE. PASSENGER CABIN FLOOR STRUCTURE WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024070506763Floorbeam · damaged(LOG 0421908) CABIN FLOOR STRUCTURE BEAM AT STA 360 WL 208 LBL 0 TO LBL 8 HAS DAMAGE ON FWD & AFT EDGES. WORK ACCOMPLISHED ON ER/A 619106-14 REV-ORIGINAL.SDR AALA202407036213Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR SUPPORT BRAEAK ASSEMBLY PANEL AT STATION 540, LBL 49. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-01.SDR CALA2024070101948Floorbeam · damaged(B737-06-3-0049) MAIN CABIN STA 947.5 APPROX LBL 4 TO RBL 14 FLOOR SUPPORT STRUCTURE HAS CORROSION IN SEVERAL AREAS. REMOVED DAMAGE AND INSTALLED NEW T-CHORD TRANSVERSE FLOOR BEAM STA 947.5 LBL 7.80" - RBL 58.60" PER BOEING SRM 53-70-51-2R-5 PAR 4. A-P.SDR AALA202407012470Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOORBOARD SUPPORT BREAK ASSEMBLY PANEL AT STA 540, RBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-01.SDR AALA202407016077Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOORBOARD SUPPORT BREAK ASSEMBLY PANEL AT STA 540, LBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-01.SDR SWIA20240629Floorbeam · corrodedCORROSION AND CRACK ON FLOOR SUPPORT BEAM IN THE CARGO BAY THAT RUNS LATERALLY FROM STGR 17L AND STGR 17R AT FS 589.00 AND LBL 38.40. (FILED CLOSED) THIS IS CURRENTLY A WORK IN PROGRESSSDR SWIA20240809629Floorbeam · corrodedCORROSION AND CRACK ON FLOOR SUPPORT BEAM IN THE CARGO BAY THAT RUNS LATERALLY FROM STGR 17L AND STGR 17R AT FS 589.00 AND LBL 38.40. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR SWAA2024072907360Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM BS947 RBL50 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 50 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.075IN MATERIAL; REMAINISDR SWAA2024072907356Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM BS947 RBL25 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 25 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINISDR SWAA2024072607354Angle · corrodedPASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. CUT AND REMOVED DAMAGED PART OF FLOORBEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4. NDT PART 6;51-00-00 PROCESDR SWAA2024072617793Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE.<[01] REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] CUT AND REMOVED DAMAGED PART OF FLOOR BEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.;[03] C/W INSPECTIOSDR SWAA2024072607355Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM BS947 LBL51 UNDER LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.100IN MATERIAL; REMAINING THICKNESSDR SWAA2024072607357Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM BS947 RBL28 HAS SURFACE CORROSION ON TOP SIDE .<[01] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINING 0.128IN; FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1..;[02] ENTIRE LENGTH OF FLOOR BEAM UPSDR AALA202407080886Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR SUPPORT BREAK ASSEMBLY AT STA 540 FROM BL 0 TO LBL 20. REPLACED BREAK ASSEMBLY PER AARD 51-00-05.SDR AALA202407178830Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER CHORD (T CAP) OF FLOOR BEAM AT STA 947, LBL 6. REPAIRED UPPER CHORD PER 53-70-51 REPAIR 5 ALTERNATIVE 2 AND EA 356105.SDR DALA2024070206710Floorbeam · cracked(LOG 0417664) MAIN CABIN, STA 540 -3 RBL 2, FLOATING FLOOR SUPPORT IS CRACKED IN THE I/B SIDE I14-002. REMOVED AND REPLACED MAIN CABIN, STA 540 -3 RBL 2, FLOATING FLOOR SUPPORT IAW B737 SRM 51-40-05 AND B737 SRM 51-40-02.
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