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 ASAA2021030334439Floorbeam · corrodedFLOORBEAM AT STATION 986 @R2 DOOR AREA CORRODED AT MOUNT FITTING. GROUNDED - YES. REMOVED DAMAGE PER B737-800 SRM 53-70-15 ORIG THICKNESS .040, MAT LOSS .015NEW THICKNESS .025, AREA OUT OF LIMITS PER B737-800 SRM 53-70-15. REMOVED WEB PER B737-800 SRM 51-40-02SDR ASAA2021030334438Floorbeam · corrodedMAIN CABIN AFT @ L2 DOOR. FLOORBEAM CORRODED AT STATION 986. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 53-70-51. ORIG MAT IS .150, REMAINING MAT IS .103. MAT LOSS OF .047 IS BEYOND ALLOWABLE LIMITS. REMOVED UPPER T-CAP CHORD AND INSTALLED NEW T-CAP CHSDR A6WA202103087687Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR PANEL SILL NUTPLATE AT FS461.00+6, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL SILL NUTPLATE AT FS461.00+6, LBL 42. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED SDR A6WA202103087686Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS461.00+1, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE AT FS 461.00+1, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. PERFORMED UT THICKNESS CHECK AND FOUND TO BE SDR A6WA202103087685Floorbeam · corrodedCORROSION COMMON TO FLOOR PANEL SILL AT FS 449.85+3, LBL 43. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL SILL AT FS449.85+3, LBL 43. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED BLEND AREA, FOUND TO BE SDR A6WA202103087698Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS544.00, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS544.00, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS EVALUATED BLEND AND FOUND WITHIN LIMITS REF REO601R-53SDR A6WA202103087690Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR PANEL SILL AT FS484.00+4, LBL 43 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL SILL AT FS484.00+4, LBL 43. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED BLEND AREA, REMAINSDR A6WA202103087691Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS484.00+12, LBL 44 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE AT FS 484.00+12, LBL 44, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. PERFORMED UT THICKNESS CHECK AND FOUND TO BSDR A6WA202103087705Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS449.85+.5 LBL43. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE AT FS449.85+.5, LBL43. PERFORMED HFEC WITH NO INDICATION. PERFORMED UT THICKNESS CHECK, FOUND TO BE WITH IN LIMITS RESDR A6WA202103087688Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS473.15+4.5, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE AT FS 473.15+4.5, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS. PERFORMED UT THICKNESS CHECK AND FOUND TOSDR A6WA202103087684Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS439.00+8, LBL44 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS439.00+8 LBL 44. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. EVALUATED BLEND AREA AND FOUND TO BSDR A6WA202103087696Floorbeam · corrodedCORROSION COMMON TO PRESSURE FLOOR SILL AT FS 513.00, LBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR ANGLE FS 513.00, LBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL WITHSDR DALA2021030801296Floorbeam · crackedREF NRC 131. CRACK FOUND EXTENDING THROUGH MULTIPLE ATTACH FASTENERS ON FLOOR BEAM STA 737. LOCATED RT SIDE OF A/C JUST I/B OF THE OVERWING EXIT FUSELAGE FRAMES. MARKED. NRC 131. MAINTENANCE REPLACED FLOOR BEAM PER DWG #5940863 & INSTALL FLOOR PANELS PER B717 SDR REXA2021030500080Floorbeam · corrodedMAJOR CORROSION DAMAGE ON FLOOR BEEM POST AT FS280 AND RBL 11.16
AIRCRAFT WAS PREPARED AND INSPECTED IAW EA CRJ953-11244 FOR FERRY FLIGHT INTENDED FOR PERMANENT REPAIR.SDR IPXA2021032867392Floorbeam · crackedINSPECTION TYPE:3CLOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70, X= 57.5 AND Z= -98.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70, X= 57.5 AND Z= -98 IAW SRM 53-40-51 REPAIR 1 FIG. 201. (MAJOR)SDR IPXA2021032867391Floorbeam · crackedINSPECTION TYPE:3CFWD. LOWER CARGO FLOOR BEAM IS CRACKED AT STA. 6-70, X= -57.5 AND Z= -98.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70, X= -57.5 AND Z= -98 IAW SRM 53-40-51 REPAIR 1 FIG. 202. (MAJOR)SDR DALA2021030901349Floorbeam · corrodedDURING INITIAL CORROSION LEVEL 2 FOUND PASSENGER CABIN FLOOR STRUCTURE CORROSION AT STA1480 LBL41 TO LBL53. REPAIRED PER ERA 529123-14. (LP 1749097)SDR SWIA202157333Floorbeam · dentedAFT BAGGAGE FLOOR CROSSBEAM AT FS1031 IS DENTED (C-CHECK RO 4/3/2021) REMOVED UNSERVICEABLE ATTACHING SUPPORT ANGLE AND INSTALLED NEW ATTACHING SUPPORT ANGLE ON CROSSBEAM AT FS1031.00 REF CRJ 700 SRM 51-42-06-001-001-A01 DWG MM670-35360 REV A. COMPLIED WISDR IPXA2021032767341Floorbeam · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR SUPPORT AT STA 1481 AND RBL 101 HAS CORROSION.REMOVED AND REPLACED CORRODED MAIN CABIN FLOOR SUPPORT AT STA 1481 AND RBL 101 IAW SRM 51-33-01. (MINOR)SDR IPXA2021032767340Floorbeam · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR SUPPORT AT STA 5-73 AND RBL 82 HAS CORROSION UNDER FLOOR PANEL 272JF.REMOVED AND REPLACED CORRODED MAIN CABIN FLOOR SUPPORT AT STA 5-73 AND RBL 82 IAW SRM 51-35-01. (MINOR)SDR IPXA2021032767338Floorbeam · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR SUPPORT AT STA 1361 AND BETWEEN RBL 47.5 & RBL 75.5 HAS CORROSION.REMOVED AND REPLACED CORRODED MAIN CABIN FLOOR SUPPORT AT STA 1361 AND BETWEEN RBL 47.5 & RBL 75.5 IAW SRM 51-33-01. (MINOR)SDR IPXA2021032767337Floorbeam · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR SUPPORT AT STA 1481 AND RBL 50 HAS CORROSION UNDER FLOOR PANEL 272HF.REMOVED AND REPLACED CORRODED MAIN CABIN FLOOR SUPPORT AT STA 1481 AND RBL 50 IAW SRM 51-35-01. (MINOR)SDR IPXA2021032767336Floorbeam · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR SUPPORT AT STA 1401 AND RBL 15 HAS CORROSION UNDER FLOOR PANEL 273QF.REMOVED AND REPLACED CORRODED MAIN CABIN FLOOR SUPPORT AT STA 1401 AND RBL 15 IAW SRM 51-35-01. (MINOR)SDR IPXA2021032767335Floorbeam · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR SUPPORT HAS CORROSION AT STA 1239 AND RBL 50 UNDER FLOOR PANEL 262EF.REMOVED AND REPLACED CORRODED MAIN CABIN FLOOR SUPPORT AT STA 1239 AND RBL 50 IAW SRM 51-33-01. (MINOR)SDR REXA2021032200163Floorbeam · corrodedFS 280.00 FWD J ANGLE HAS MULTIPLE SPOTS OF CORROSION. "REMOVED AND REPLACED FS280 FWD J ANGLE IAW CRJ 200 SRM 51-42-21 & 51-42-06.
"SDR SWIA202157652Floorbeam · crackedCRACK FOUND AT COCKPIT FLOOR BEAM LBL12 FS280.00 (C-CHECK RO 4/21/2021) REMOVED CRACKED SECTION AND INSTALLED NEW REPAIR SECTION OF COCKPIT FLOOR BEAM LBL12.00 FS280.00 - FS265.00 REF CRJ700 SRM 53-11-43-201-003-A01. SEE CONTINUE CARD FOR DETAILS. COMPSDR ASAA2021022834351Floorbeam · corrodedFLOOR BEAM 986.5 UPPER SECTION HAS CORROSION SPOTS AT THE UPPER & LOWER SIDE BETWEEN RBL 28 THRU RBL 45 IN AFT CABIN BELOW THE FLOOR GROUNDED - YES. REPAIRED FLOOR BEAM IAW 737-700 SRM 53-70-51-2R-4 W=1 O=.150 R=.070 L=2 D=.080SDR ASAA2021022834350Floorbeam · corrodedFLOOR BEAM 947.5 HAS CORROSION AROUND FITTING AT RBL 51, IN THE AFT CABIN BELOW THE FLOOR GROUNDED - YES. REPAIRED FLOOR BEAM IAW 737-700 SRM 53-70-51-2R-5 W=1 O=.180 R=.140 L=2 D=.040SDR DALA2021030301210Floorbeam · corrodedDURING INITIAL INSPECTION MAINTENANCE FOUND SEVERAL POINTS OF CORROSION LEVEL 2 ON BEAM STA 1640 BTW LBL 55 TO RBL55 AND REPAIRED PER SRM 53-00-51. (LP 1742132)SDR SWIA202157649Floorbeam · corrodedR/H AND L/H FLOOR BEAM AT FS280.00 FOUND CORRODED. (C-CHECK RO 4/21/2021) REMOVED AND REPLACE NEW RH AND LH NEW COSSBEAM P/N CC670-34094-1S AND P/N CC670-34094-2S AT FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700SDR DALA2021030101152Floorbeam · corrodedDURING INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON CABIN FLOOR BEAM AROUND STA 303, LBL 48. THE CORROSION REMOVED AND CUT THE DAMAGE SECTION CHORD. (LP 1741579)SDR SWIA202157641Floorbeam · corroded*CORROSION AT FLOOR PANEL SUPPORT ANGLE COMMON TO FS280.00 CROSSBEAM (C-CHECK RO 4/21/2021) REMOVED AND REPLACED WITH NEW FLOOR SUPPORT ANGLE P/N CC670-34095-1SB AT FS 280.00REF CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-06-001-001-A01 DRAWINGSDR SWIA202157702Floorbeam · corroded*CORROSION NOTED ON A-BAY FLOORBOARD SUPPORT BRACKET AFT OF FS280 BULKHEAD (C-CHECK RO 4/21/2021) REPLACED WITH NEW A-BAY FLOOR BOARD SUPPORT ANGLE @ FS280.00. P/N CC670-34256-3 REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, CSDR AALA202103199027Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND 0.5 INCH CRACK IN BREAK ASSEMBLY AT STA 540 AND LBL 0 TO LBL 20. REMOVED AND REPLACED BREAK ASSEMBLY IAW SRM 51-10-02.SDR DALA2021030901351Floorbeam · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 PASSENGER CABIN FLOOR STRUCTURE CORROSION AT STA 325 RBL22-RBL55.SDR FDEA202102250451Floorbeam · corrodedFLOOR SUPPORT AT STA 1881 RBL 10-20 IS CORRODED MAIN DECK REMOVED AND REPLACED MAIN DECK FLOOR SUPPORT AT STA 1881 RBL 10-20. REF. SRM 51- 35-01, VOL IISDR SWAA2021031751061Floorbeam · corrodedAFT CABIN WET AREA STA 947 FLOOR BEAM LBL 51 CORROSION FOUND ON UNDERSIDE OF TOP FLANGE. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 5370511A1 ORIGINAL T = .180 LOSS .044 REMAINING T = .136 T CAP REPAIR WAS ACCOMPLISHED ON NRC Y249437 PN 147A550429SDR SWAA2021031751812Floorbeam · crackedPASSENGER CABIN FLOOR PANEL SUPPORT IS CRACKED AT B.S. 540; L.B.L. 24.5 - L.B.L. 45; W.L. 208.1. / REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL SUPPORT AT BS540 LBL.24.5 TO LBL 45 WL. 208.1 I.A.W SRM 51-40-02-OG-0 AND 51-40-05-OG-0 DRAWING #143A0060; PART SDR SWAA2021031751813Floorbeam · crackedPASSENGER CABIN FLOOR PANEL SUPPORT IS CRACKED AT B.S. 540; R.B.L. 24.5 - R.B.L. 45; W.L. 208.1. / REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL SUPPORT AT BS 540 RBL 24.5 TO RBL 45 WL 208.1 I.A.W SRM 51-40-02-OG-0 AND 51-40-05-OG-0 DRAWING #143A0600; PASSESDR SWAA2021031751805Floorbeam · corroded***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 727D+5; L.B.L. 24 - R.B.L. 24; W.L. 154. / RECIEVED NEW/SERVICABLE AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 727D+5; L.B.L.29-R.B.L.24; W.L.159 TO BE INSTALLED ON JPANEL-141-CLOSE. 57609U 09MAR21SDR SWAA2021031751804Floorbeam · corroded***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 887; L.B.L. 10 - R.B.L. 21; W.L. 154. / REMOVED AND REPLACED PANEL SUPPORT AT B.S.887 LBL10 RBL21 WL154 IAW SOPM 20-50-01 56334U 09MAR21 LEAD 67 09MAR21 INSP 86 09MAR21SDR R61A2021031200247Floorbeam · corrodedWHILE AC WAS IN HVY CK CORROSION FOUND ON CENTER FUSELAGE 3 FLOOR STRUCTURE LH LONGITUDINAL BEAM AT FR87. REPLACED BEAM PN 170-65669-003 IAW SRM 51-41-01, 51-42-01. SEE AARNRC# 4500861-1000-0040 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.SDR R61A2021031200246Floorbeam · corrodedWHILE AC WAS IN FOR HVY CK CORROSION FOUND ON CENTER FUSELAGE 3 FLOOR STRUCTURE RH LONGITUDINAL BEAM AT FR87 REPLACED BEAM PN 170-65669-004 IAW SRM 51-41-01, 51-42-01, 51-43-01. AC REMAINS IN YQG FOR COMPLETION. SEE AAR NRC# 4500861-1000-0039 FOR WORK PERFORSDR R61A2021031000228Floorbeam · corrodedWHILE AC WAS IN FOR HVY CK FOUND CORROSION ON FWD FUSELAGE FLOOR STRUCTURE CROSS BEAM UPPER FLANGE AT FR14 RH SIDE. AAR MX REPLACED PN 1307903722 FWD FUSELAGE FLOOR STRUCTURE CROSS BEAM UPPER FLANGE AT FR14 RH SIDE IAW SRM 53-00-10SDR MASA20210302062Floorbeam · crackedCRACK ON FLOOR BEAM [ UPPER FLANGE] IN STA. FS= 280 AT PAX CABIN FWD WET AREA|NEW BEAM IN STA FS-280 AT PAX CABIN FWD WET AREA WAS INSTALLED PER CRJ900 SRM-51-42-06-001-001-A01SDR REXA2021022300123Floorbeam · corrodedFLOORBOARD SUPPORT ANGLE IS CORRODED AT F.S. 280, STGR 27. - REMOVED AND REPLACED SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01. WVAC EMP STAMP# 711 MTCSDR LR7A2021022302782Chine · corrodedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND THE LT CHINE CAP FS517 TIED OWN WELL CORRODED, WL146, LBL50.5-61.6. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR 0080. PSE 53-40-10, AD 2012-06-09.SDR SWIA202156995Floorbeam · damaged*280.00 LEFT FLOOR POST HAS A DRILL START AT THE TOP END FORWARD SIDE. (MARKED) (C-CHECK) RO 3/24/2021 REMOVED AND INSTALLED NEW LH FLOOR POST AT FS 280 LBL 9 REF CRJ 200 SRM 51-42-06 AND DRAWING# 600-34017 REV AA, AND MHIRJ REO 601R-53-11-3674 REV --, DSDR SWIA202156994Floorbeam · cracked*FLOOR MEMBER, FS280.00, FWD FLOOR ANGLE IS CRACKED OUTBOARD ENDS, LBL9 €“ RBL9. (MARKED) (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED FS280.00, FWD FLOOR ANGLE LBL9 €“ RBL9 REF. CRJ 200 SRM 51-42-06 AND DWG 600-34017 REV. AD. COMPLIED WITH TASK CARD 51SDR SWIA202156993Floorbeam · cracked*FLOOR MEMBER, FS280.00, IS CRACKED OUTBOARD ENDS, LBL9 €“ RBL9. (MARKED) (C-CHECK) RO 3/24/2021 REPAIRED FS280 BULKHEAD ASSY REF. REO 601R-53-11-926 REV. -B DATED 2006-05-10 ALL STEPS COMPLIED WITH, AND REO 601R-53-11-3666 REV. -- DATED 2021-03-12 ALL
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