JASC 5315
Service difficulty reports · 44,220
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 FDEA201210223703Floorbeam · corrodedCABIN FLOORBEAM AT BS 1640 FOUND WITH CORROSION AT UPPER TEE SURFACES. CORROSION FOUND 100 PERCENT THROUGH AND OUT OF LIMITS IAW SRM 53-00-51, FIG 101 ALLOWABLE DAMAGE 1, REV 107. FLOORBEAM REMOVED IAW SRM 51-40-02, REV 107. NEW FLOORBEAM FABRICATED IAW DWSDR EIAA20121022080Floorbeam · crackedFORWARD CARGO FLOORBEAM CHORD CRACKED BS 560 WL 120 LBL 6-24. REMOVED CHORD, FABBED NEW CHORD PER DRWG 65B02721 SHT 9 REV E PL65B38614 REV C. INSTALLED PER SRM 51-30-02.SDR EIAA20121022070Floorbeam · damagedM/D BS 1740 WL 200 LBL 59 FLOORBEAM UPPER CHORD SCREW HOLE ELONGATED. REPAIRED M/D FLOORBEAM UPPER CHORD AT BS 1740 WL 200 LBL 0-109 PER B747 SRM 51-40-040 FIG 1.SDR USAA2012110500003Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y465. REPLACED FLOORBEAM AT FR66, -Y465 IAW A319 SRM 51-42-11, FIG 9, PAR 5.SDR USAA2012110200015Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A319 SRM 51-42-11 FIG 3, 4, 8, 9, 10 & 20.SDR USAA2012110200014Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR67 TO FR68, -Y1292 IAW A319 SRM 51-42-11 FIG 3, 4, 8, 9, 10 & 20.SDR USAA2012110200013Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IAW A319 SRM 51-42-11 FIG 3, 4, 8, 9, 10 & 20.SDR USAA2012110200012Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Y1292. REPLACED FLOORBEAM AT FR66, Y1292 IAW A319 SRM 51-42-11 FIG 3, 4, 8, 9, 10 & 20.SDR USAA2012110100013Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y765 IAW A319 SRM 51-74-00 FIG 201.SDR USAA2012110100012Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IAW A319 SRM 53-41-14 FIG 101 & FIG 201.SDR ASAA2012102193208Floorbeam · corrodedFWD CARGO FLOORBEAM AFT BULKHEAD FS 500I. R & R FLOORBEAM IAW SRM 51-40-02.SDR UALA2012102206027Floorbeam · corrodedSTA 1681 FLOORBEAM UPPER CAP HAS CORROSION BETWEEN RBL 24 AND RBL 53. MAJOR REPAIR ACCOMPLISHED: REMOVED, FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM AT STA 1681 PER BAC DWG 146N511 1 AND 146N5091 AND SRM 51-40-02.SDR UALA2012102206026Floorbeam · corrodedSTA 1660 FLOORBEAM UPPER CAP HAS CORROSION AT LBL 1. MAJOR REPAIR ACCOMPLISHED: CUT OUT CORROSION DAMAGE. FABRICATED 2 REPAIR ANGLES, FILLER, STRAP AND INSTALLED PER SRM 53-00 -51 AND SRM 51-40-02.SDR UALA2012102206024Floorbeam · corrodedSTA 1640 FLOORBEAM UPPER CAP HAS CORROSION BETWEEN LBL 12 AND RBL 60. REF SCAL LP 9984854. MAJOR REPAIR ACCOMPLISHED: REPLACED CORRODED SECTION OF FLOORBEAM UPPER CHORD STA 1640 BETWEEN LBL 9.5 AND RIGHT SIDE OF FUSELAGE BODY.SDR UALA2012102206021Floorbeam · corrodedSTA 365 FLOORBEAM UPPER CAP HAS CORROSION BETWEEN BL 0 AND RBL 61. REF SCAL LP 9985010. MAJOR REPAIR ACCOMPLISHED: REPLACED UPPER FLOORBEAM T-CHORD STA 365.25 BETWEEN LBL 10.5 AND RT SIDE OF FUSELAGE BODY. REF ECRA 5310-055 98 AND 5310-05536.SDR C77A20121023010Floorbeam · corrodedRT FLOORBEAM, AT Y= 260.4, X= 23453.0 HAS CORROSION. R & R RT SEAT TRACK IAW SRM 51-41-01 AND 51-43-01 ON WO 562432-290 EO E175-53MR-094 REV 4, WO 640749.SDR C77A20121023008Floorbeam · corrodedFLOORBEAM, AT FR 17 HAS CORROSION X=5064.0 Y=-228.6. R & R EXISTING REPAIR IAW SRM 51-41-01 AND 51-43-01 ON WO 562432-282 IAW ETD 2012-170-014760-A AND EO E175-53MR-053.2 REV IR WO 643081.SDR DALA12011020938Floorbeam · corrodedCORROSION ON BS 712 TO 840 BETWEE STA X=-54 TO -60 AT CABIN FLOOR STRUCTURE. REPAIRED IAW ER/A 398191-14 MA, REV B.SDR DALA1251213735Floorbeam · corrodedFLOORBEAM TEE CAP LBL-12 STA 312 HAS CORROSION REF AMM 51-05-01. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED IAW ER A 507330-14, REV C, REF NRC 25871/2700/0008.SDR DALA1251840933Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 256 LT SIDE UNDER FLOOR PANEL 200B AND 200A SUPPORT BRACKET HAS CORROSION AT NUT PLATE HOLE. REPAIRED IAW SRM 51-10-3B.SDR DALA1251610933Floorbeam · corrodedAFT LAV FLOORBEAM AT STA 1322 HAS CORROSION AT X 21, 34, 42(LT) X -18, -19, -41 (RT) LOCATION BLENDED AT X21 AND X42 STA 1322 BEAM ARE REPAIR DOUBLERS/FILLERS FROM PRIVIOUS REPAIR. REPAIRED IAW ER/A 507360-14, REV ORIG.SDR DALA1251590933Floorbeam · corrodedAFT LAV FLOORBEAM AT STA 1338 HAS CORROSION AT X=5, 26, 32,36, 46" L/H. X=-18, -19, -24, -31, -34, -37, -39, -47 RIGHT. INSTALLED NEW CAP ANGLE AT STA 1338 LBL 10 TO LBL 56.5 IAW SRM 51-30-5 PG1 AND 51-30-2 PG1.SDR DALA1251580933Floorbeam · corrodedTWO NUT PLATE HOLES AT FLOORBEAM BS 1309 F17 F19 HAVE CORROSION. REPAIRED IAW ER/A 507361-14, REV ORIG.SDR DALA1251390933Floorbeam · corrodedCABIN FLOOR SUPPORT STA 1079 X=22 TO -22 HAS CORROSION AT PANEL MOUNT HOLES ON LOWER SIDE. REPLACED FLOOR SUPPORT IAW SRM 51-30-5.SDR SWAA2012111509506Floorbeam · crackedCRACK ON THE RBL 24.5 LONGITUDINAL FLOORBEAM WEB AT LEVEL BS 708 IN CENTER WING SECTION STRUCTURE. REPAIRED BEAM IAW EO AND EA.SDR SWAA2012111509505Floorbeam · crackedCRACK ON LONGITUDINAL FLOORBEAM UPPER CHORD DIRECTED DOWNWARD OF OVAL HOLE BS 663 AT LBL 24.5 CENTER WING SECTION STRUCTURE. REPAIRED BEAM IAW EO AND EA.SDR N6WA2012101903Floorbeam · crackedBS 280 FLOORBEAM HAS CRACK ON LT SIDE. R & R BS 280 FLOORBEAM IAW REO 670-53-11-047, REV E.SDR AALA20121019017Floorbeam · corrodedSTATION 986.5 FLOORBEAM CORRODED FROM LEFT BUTTLINE 48 TO RIGHT BUTTLINE 48. REPLACED T-CAP PER SRM 53-70-51-2R4.SDR FDEA201210183671Floorbeam · crackedMAIN DECK CABIN FLOORBEAM BS 410, X = 27 TO X = 30 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR QXEA2012101801308Floorbeam · corrodedCORROSION ON AFT FACE OF FLOORBEAM AT BS 258 ABOVE STR 31P. REMOVED CORROSION IAW SRM 51-21-00-00-02. VERIFIFED AFFECTED AREA TO BE CRACK FREE USING HFEC REF NDTM PT 1 51-00-06-910-801. MIN REMAINING THICKNESS NOTED .026" REF NTM 51-00-04-910-801 PT 1. FLOSDR FDEA201210173657Floorbeam · corrodedUPPER DECK FLOORBEAM AT STA 1680 UPPER FLANGE LOWER SURFACE NUT PLATE STRIPS AT RBL 38, 46, AND 50 ARE CORRODED AND MISSING NUT PLATES. BLENDED OUT CORROSION ON FLOORBEAM UPPER FLANGE LOWER SURFACE STA 1681 RBL 38, 46, AND 50 IAW SRM 51-10-02. ORIGINAL THICSDR K11A2012102925001Floorbeam · corrodedFLOORBEAM STA 360 FLANGE CORRODED AT FASTENER HOLE, 1X1 INCHES (NR 0169,0231).SDR SIMA20121016006Support · crackedDURING B INSPECTION FOUND THE RIGHT FLOORBEAM SUPPORT CRACKED ON THE RIGHT SIDE BETWEEN FRAMES 47-48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM SUPPORT ON THE RIGHT SIDE BETWEEN FRAMES 47-48 IAW EMB SRM 53-23-02. THE OPSDR SIMA20121016005Support · crackedDURING B INSPECTION FOUND THE RIGHT FLOORBEAM SUPPORT CRACKED ON THE LEFT SIDE BETWEEN FRAMES 47-48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM SUPPORT ON LEFT SIDE BETWEEN FRAMES 47-48 IAW EMB SRM 53-23-02. THE OPERATIOSDR UALA2012101705924Floorbeam · corrodedMAIN CABIN FLOOR FRAME BS 365 UPPER SURFACE OF T-CAP CORRODED RBL 0 TO RBL 64. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF 'T' CHORD, FABRICATED AND INSTALLED NEW 'T' CHORD, SPLICE ANGLES AND STRAPS.SDR DALA12010573132Floorbeam · corrodedFORWARD CABIN FLOORBEAM BETWEEN FR 20 TO FR 24 Y-189 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT .080 DAMAGE DIM. L=6.0 W=2.0 D=.060. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOORBEAM IAW SRM 51-42-11.SDR SIMA20121015021Floorbeam · corrodedLAVATORY BEAM HAS CORROSION AROUND NUT PLATE HOLE. ACCOMPLISHED EO EM-53MR-2032 LAVATORY RT FLOORBEAM CORROSION REPAIR.SDR CALA2012101700665Floorbeam · corrodedFLOORBEAM HAS CORROSION AT BS 294 RBL 40. REPAIR FLOORBEAM IAW EC/RA 5321-01813.SDR F3LA2012101500803Floorbeam · corrodedFR66, -Y1292 FLOORBEAM CORROSION. R & R FLOORBEAM REF SRM 51-42 -11 , PARAGRAPH 5.SDR AALA20121015006Floorbeam · corrodedFLOORBEAM CORROSION AT STATION 1660. REMOVED CORROSION AND INSTALLED T-CAP REPAIR PER AARD 51-00-05-1.SDR UALA2012101505840Floorbeam · corrodedAFT CABIN FLOOR WET AREA, BS 1661 FLOORBEAM UPPER TEE HAS AREAS OF CORROSION, CENTERLINE TO RBL56. REMOVED DAMAGED SECTION OF TEE AND FABRICATED A NEW TEE, SPLICE ANGLES AND STRAPS AND INSTALLED PER SRM 53-00-51, REPAIR 3. MAJOR REPAIR.SDR QXEA2012101401255Floorbeam · crackedRIGHT FLOORBEAM 683.450 IS CRACKED. REMOVED FLOOR T-FITTINGS IAW SRM 51-40-07-02-01. REMOVED WEB GUSSET ANGLE, FLOORBEAM AND MOUNT BRACKETS IAW SRM 51-42-05-02-01. MATCH DRILLED NEW FLOORBEAM IAW SRM 51-40-07-02-01. INSTALLED FLOOR BEAM REF SRM 51-42-05-02-SDR R61A201210130585Floorbeam · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND FLOORBEAM FRAME 84 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FRAME 84 FLOORBEAM IAW EMB 170 SRM 51-40-02, 51-41-02, 51-41-01, 51-43-02, 51-41-11, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CSDR QXEA2012101301253Floorbeam · corrodedFLOORBEAM 698 IS CORRODED ON THE LT SIDE OF BL0. REMOVED RIVETS FOM AND REMOVED CORROSION IAW SRM 51-42-05-02-01 AND 51-21-00-00-02 MIN REMAINING THICKNESS .061", CONFIRMED AFFECTED AREA TO BE CRACK FREE REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801, PTSDR QXEA2012101301239Floorbeam · corrodedFLOORBEAM 1.0 BOTTOM ATTACHED FLANGE IS CORRODED ABOVE STR 26S. BLENDED AND REMOVED CORROSION REF SRM 51-21-00-00-01. MIN REMAINING THICKNESS .046" REF NTM 51-00-04-910-801 PT 1. VERIFIED AFFECTED AREA TO BE CRACK FREE REF NDTM 51-00-06-910-801 PT 1. FOUND BLSDR IPXA12576060Floorbeam · corrodedINSPECTION TYPE:C-CK, FLOORBEAM STA 1200 RBL 1 - 25 HAS 3 AREAS OF CORROSION. REPAIRED FLOORBEAM IAW DWG LORL5300R (REV B) REPAIR 1C.SDR IPXA12575960Floorbeam · corrodedINSPECTION TYPE:C, MAIN CABIN BS 1100 BETWEEN RBL 1, AND RBL 25 HAS SEVERAL AREAS OF CORROSION. REPAIRED IAW EA 121086, AND EOB757-5310-48 48872-A.SDR IPXA12575786Floorbeam · corrodedINSPECTION TYPE: C, FLOORBEAM, BS 1200, RBL 1- 25 HAS 3 AREA OF CORROSION. REPAIRED FLOORBEAM IAW LOR DWG LORL5300R (REV B) REPAIR 1C.SDR R61A201210110583Fitting · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT FF FLOORBEAM FITTING CORRODED FRAME 15 TO 18. MAINTENANCE REMOVED AND REPLACED LEFT FF FLOORBEAM FITTING IAW EMB 190 SRM 51-41-01, 51-41-02, 51-43-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE ISDR R61A201210110582Splice · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT FF FLOORBEAM SPLICE CORRODED FRAME 15 TO 18. MAINTENANCE REMOVED AND REPLACED THE LEFT FF FLOORBEAM SPLICE IAW EMB 190 SRM 51-41-01, 51-41-02, 51-43-02, 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN
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