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.

SDR A6WA202101137542Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 461.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 RBL 42.BY BLENDING. BLENDED AREA MEASURED (P1) 1.00''L X 1.700''W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03/20Dec 29, 2020 · N437AW · Cndair CL6002B19SDR A6WA202101137541Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 461.00 +9 RBL 36 TO RBL 38. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 + 9 RBL 36 TO RBL 38 BY BLENDING. BLENDED AREA MEASURED (P1) 1.20''L X 0.796''W TOOL USED DIGITAL CALIPER SDec 29, 2020 · N437AW · Cndair CL6002B19SDR A6WA202001137524Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 424.00+4, LBL 38 TO LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 424.00+4, LBL 38 TO LBL 42. REWORKED DIMENSIONS P (1) 0.4 L X 2.7 W, P(2) 0.76 L X 0.5, W P(3) 0.4 L X 0.3Dec 29, 2020 · N437AW · Cndair CL6002B19SDR A6WA202001137528Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 473.15 +5, RBL 36 TO RBL 38, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 473.15 +5, RBL 36 TO RBL 38. REWORKED DIMENSIONS 1.45 L X 0.55 W, REF REO 601R-53-41-666 REV (C) DATED 20Dec 29, 2020 · N437AW · Cndair CL6002B19SDR A6WA202001137521Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 439.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE POSITIONS AT FS 439.00, LBL 42. REWORKED DIMENSIONS 2.2 L X 1.8 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMDec 29, 2020 · N437AW · Cndair CL6002B19SDR FDEA202012270261Beam · crackedMAIN DECK R3 DOOR UPPER NR 1 BEAM CRACKED AT AFT STOP PIN, MRKD. REMOVED AND REPLACE ADA0006-1 BEAM PER ADA3462.Dec 27, 2020 · N523FE · Doug MD11FSDR REXA2021012000019Angle · corrodedFS 280 FWD FLOOR SUPPORT ANGLE IS CORRODED AROUND ALL NUTPLATES BETWEEN LBL 9.0 AND RBL 9.0. REMOVED & REPLAED FS 280 J ANGLE, IAW SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01. REMOVED & REINSTALL SAME AVI BAY LIGHT BRACKET, IAW SRM 51-42-06-001-001-A0Dec 27, 2020 · N310PQ · Cndair CL6002D24SDR SWIA202056409Floorbeam · damagedFLOOR BEAM AT LBL 33, FS 559+112 HAS FLOOR BOLT CEASED IN NUTPLATE. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED 2 (EA) NUT PLATES AT LBL 33, FS 559+112 IAW CRJ 200 SRM 51-45-00 REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Dec 22, 2020 · N246PS · Cndair CL6002B19SDR SWIA202056393Angle · corrodedFS 280.00 FWD J ANGLE HAS CORROSION AROUND NUTPLATES. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED FS 280.00 FWD J ANGLE AS REQUIRED IAW CRJ 200 SRM 51-40-11.Dec 22, 2020 · N246PS · Cndair CL6002B19SDR SWIA202056386Floorbeam · crackedFS 280.00 BEAM SPLICE CRACKED AT APPROX. RBL11. (C-CHECK) RO 2/21/2021. REMOVED DAMAGED SPLICE AT FS 280.00 RBL 9 AND INSTALLED A NEW SPLICE ANGLE IAW REO 601R-53-11-171 REV D DATED 13-FEB-07.Dec 22, 2020 · N246PS · Cndair CL6002B19SDR SWIA202056054Floorbeam · corroded*AVIONICS BAY FLOOR PANEL SUPPORT ON THE AFT SIDE OF FS280.00 FRAME IS CORRODED AT MULTIPLE AREAS. (MARKED) (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED SUPPORT ANGLE AT FS 280 PER DWG # CC670-32050.Dec 21, 2020 · N708SK · Cndair CL6002C10SDR SWIA202055707Floorbeam · crackedFOUND EXISTING REPAIR ON FLOOR SUPPORT BEAM AT FS 280.0 HAS: RH SPLICE DOUBLER RACKED. LBL IB CLIP CRACKED. RBL OB CLIP CRACKED . UPPER AFT ANGLE CORRODED. (C-CHECK) RO 1/29/2021 REO 601R-53-11-926 REV B DATED 2006/05/10 ALREADY INCORPORATED TO THIS Dec 21, 2020 · N447SW · Cndair CL6002B19SDR IPXA2021020165185Floorbeam · corrodedINSPECTION TYPE:3CLOWER AFT CARGO FLOOR SUPPORT ANGLE IS CORRODED AT STA. 1841 AND BETWEEN X=7 TO X= 43.REPAIRED FLOOR SUPPORT ANGLE AT STA. 1841 AND BETWEEN X= 7 TO X= 43 IAW VT-SAA EA 011-5310-01-A8790 REV. I/R AND UPS EO MD11-5310-79176-A. (MAJOR)Dec 21, 2020 · N263UP · Doug MD11FSDR JR2R20201221638Floorbeam · corrodedFLOOR BEAM CORRODED TOP SIDE ALONG THE FWD EDGE BETWEEN RBL 36 THRU RBL 48.Dec 21, 2020 · N86312 · Emb ERJ170200LRSDR SWIA202056201Floorbeam · damagedFLOOR BEAM BLEND LOCATED AT FS561 LBL 27 REQUIRES REPAIR (100% MATERIAL LOSS) (C-CHECK) RO 2/9/2021 REMOVED FLOOR BEAM SECTION FROM FS559.00+90 TO FS569.00 LBL27 AND INSTALLED NEW SECTION REF CRJ200 SRM 53-00-43 AND REO 601R-53-51-547 REV-- DATED 2021-01-0Dec 20, 2020 · N876AS · Cndair CL6002B19SDR A6WA202012237475Floorbeam · corrodedFLOOR SUPPORT STRUCTURE AT FS 559, RBL 28 TO RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR SUPPORT STRUCTURE AT FS 559, RBL 28 TO RBL 42, REF CRJ 200 REV (38) SRM 51-21-06. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED ARDec 19, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237474Floorbeam · corrodedFLOOR SUPPORT STRUCTURE AT FS 559, LBL 28 TO LBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR SUPPORT STRUCTURE AT FS 559, LBL 28 TO LBL 42, REF CRJ 200 REV (38) SRM 51-21-06. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED ARDec 19, 2020 · N457AW · Cndair CL6002B19SDR IPXA2021012965050Floorbeam · crackedINSPECTION TYPE: 3C LOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA 6-70 AND X=58. REPAIRED CRACKED FLOOR BEAM AT STA 6-70 AND X=58, IAW VT-SAA EA 011-5340-01-A8788 REV I/R AND UPS EO MD11-5340-79162-A. (MAJOR)Dec 18, 2020 · N263UP · Doug MD11FSDR IPXA2021012965040Floorbeam · crackedINSPECTION TYPE: 3C LOWER FWD CARGO FLOOR BEAM IS CRACKED AT STA 6-70 AND X= -58.0. REPAIRED CRACKED FLOOR BEAM AT STA 6-70 AND X= -58.0, IAW VT-SAA EA 011-5340-01-A8788 REV I/R AND UPS EO MD11-5340-79162-A. (MAJOR)Dec 18, 2020 · N263UP · Doug MD11FSDR REXA2021011200870Angle · corrodedFS 280.00 FLOOR SUPPORT J ANGLE CORRODED BETWEEN LBL 11 AND RBL 11. REPLACED J-ANGLE, IAW CRJ 900 SRM 51-42-06-001-001-A01,51-42-21-001-001-A01, 51-40-11-001-001-A01, AND 51-25-16-001-001-A01.Dec 18, 2020 · N311PQ · Cndair CL6002D24SDR SWIA202056364Floorbeam · crackedFOUR EA FS 280.00 ATTACH CLIPS CRACKED AT RBL 9 AND LBL 9. (C-CHECK) RO 2/17/2021. REPLACED 4 EA ATTACHING CLIPS AT FS 280 FROM RBL 9 TO LBL 9 IAW CRJ 200 SRM51-40-11 AND 51-24-36.Dec 17, 2020 · N506CA · Cndair CL6002B19SDR SWIA202056324Doubler · crackedFS 280.00 BEAM REPAIR DOUBLER AT RBL 13 CRACKED. (C-CHECK) RO 2/17/2021. REPLACED THE DOUBLER ON FS 280 AT RBL13 IAW CRJ 200 SRM 51-40-11 AND 51-24-36.Dec 17, 2020 · N506CA · Cndair CL6002B19SDR SWAA2021011137346Floorbeam · corrodedPASSENGER COMPARTMENT FLOOR STRUCTURE STA 947.5 WL 208.1 LBL 25 FLOOR BEAM IS CORRODED. REMOVED CORROSION AND VERIFIED LIMITS ON FLOOR BEAM AT STA 947.5 LBL 25 WL 208 ORIGINAL T: .180 LOSS: .042 REMAINING T: .138 MAX LOSS ALLOWED .027. OUT OF LIMITS, IAW SRMDec 17, 2020 · N8606C · Boeing 7378H4SDR SWAA2021011137347Floorbeam · corrodedPASSENGER COMPARTMENT FLOOR STRUCTURE WL 208.1 STA 947.5 LBL 48 FLOOR BEAM IS CORRODED. REMOVED CORROSION AND VERIFIED LIMITS ON FLOOR STRUCTURE AT STA 947.5 LBL 48 (FLOOR BEAM) ORIGINAL T: .180 LOSS: .050 REMAINING T: .130 MAX LOSS ALLOWED .027. OUT OF LIMIDec 17, 2020 · N8606C · Boeing 7378H4SDR 2021F00004Floorbeam · corrodedINTERGRANULAR CORROSION FOUND ON UPPER FLOOR BEAM "T" CAP ANGLE AT FRAME 1F. THE SECTION OF EXTRUDED T-ANGLE WAS CUT, REMOVED AND REPLACED WITH A PIECE OF 2024T3511 OF SIMILAR SIZE AND LENGTH. IT WAS ETCHED, ALODINED AND PAINTED AS REQUIRED, AND INSTALLED USDec 17, 2020 · N1331C · Casa C212CCSDR SWAA2021010637348Floorbeam · corrodedPASSENGER COMPARTMENT FLOOR STRUCTURE WL 208.1 STA 947.5 LBL 53, FLOOR BEAM IS CORRODED. REMOVED CORROSION AND VERIFIED LIMITS ON FLOOR BEAM AT STA 947.5 LBL 53 WL 208 ORIGINAL T .180 LOSS: .060 REMAINING T: .120 MAX LOSS ALLOWED .027 'OUT OF LIMITS', IAW SRMDec 17, 2020 · N8606C · Boeing 7378H4SDR SWIA202056736Floorbeam · cracked*SUSPECT CRACK IN THE RADIUS OF THE COCKPIT FLOORBEAM AT RBL12 ON THE FWD SIDE OF THE FS280 BULKHEAD/CROSSBEAMS (FLAGGED) (C-CHECK) RO 3/8/2021 REPAIRED COCKPIT FLOORBEAM AT RBL 12 FWD OF FS 280 REF CRJ-700 SRM 53-11-43-201-003-A01 REV 38 DATED JUL 25/20Dec 16, 2020 · N738EV · Cndair CL6002C10SDR SWIA202055706Floorbeam · crackedFS 280 FLOOR BEAM AT RBL 9 I/B, ANGLE CRACKED AT TOP. (C-CHECK) RO 1/29/2021 CRACKED FS280 FLOOR BEAM ANGLE AT RLB9, I/B REMOVED AND INSTALLED WITH NEW FABRICATION. SEE CONTINUE CARD FOR WORK ACCOMPLISHED. REF. CRJ200 SRM 51-42-21 & REO 601R-53-11-926 REV-Dec 16, 2020 · N447SW · Cndair CL6002B19SDR SWAA2021011136951Floorbeam · corrodedCORROSION ON BS 259.5 LATERAL BEAM AFT FLANGE UPPER SURFACE WL 208.1 LBL 10 TO RBL 10. CORROSION WAS FOUND TO BE OUT OF LIMITS ON BS 259.5 LATERAL BEAM AFT FLANGE UPPER SURFACE WL 208 LBL 10 TO RBL 10. THE AREA WAS REPAIRED, PER EA 20-153-02588 REV IR & ATS Dec 15, 2020 · N729SW · Boeing 7377H4SDR SWIA202054892Floorbeam · corrodedCORROSION AFT WET AREA FLOOR BEAM CORRODED FRAME 89. C-CHECK RO 12/27/2020. REMOVED AND REPLACED AFT WET AREA RT FLOOR BEAM FRAME 86/89, REF SRM.Dec 15, 2020 · N154SY · Emb ERJ170200LRSDR SWIA202055771Floorbeam · corrodedLEFT FLOOR SILL ASSY LBL41 TO LBL45 LFS560 HAS CORROSION (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH TENSION STRAP IAW CRJ 200 SRM 51-42-06Dec 14, 2020 · N498CA · Cndair CL6002B19SDR DALA2020121504103Floorbeam · corrodedCORROSION FLOOR BEAM LONGITUDINAL AT LEVEL -YC AND AT FR 73 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM LONGITUDINAL AT LEVEL -YC AND FR 73 AT GALLEY AREA, AS PER A330 SRM AND DWG.Dec 14, 2020 · N801NW · Airbus A330323SDR DALA2020121504096Floorbeam · corrodedCORROSION ON FLOOR BEAM -Y450 APPROXIMATELY AT LEVEL OF FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y450 APPROXIMATELY AT LEVEL OF FR 68 AT AFT GALLEY AREA, AS PER A320 SRM 51-72-11.Dec 14, 2020 · N343NW · Airbus A320212SDR DALA2020121504095Floorbeam · corrodedCORROSION FLOOR BEAM -Y1292 AT LEVEL OF FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 AT LEVEL OF FR 20 AT FWD GALLEY AREA, AS PER A320 SRM 51-72-11.Dec 14, 2020 · N343NW · Airbus A320212SDR R61A2021010200002Floorbeam · crackedFWD CARGO COMPARTMENT, CRACK FOUND ON FLOOR SUPPORT AT FR 26 BETWEEN STR 28L-28R. REPLACED IAW SRM 51-41-01.Dec 13, 2020 · N639RW · Emb ERJ170100SESDR A6WA202012237484Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 436, LBL 42, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE (2 EA) POSITIONS AT FS 436, LBL 42, STR. 17, W/L 73.50. REWORKED DIMENSIONS (P1)=2.6 L X 0.5 W, (P2)=0.7 L X Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237492Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 513+4, LBL 35 TO LBL 43, W/L 73.59, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 513+4, LBL 35 TO LBL 43, W/L 73.59, STR 17. REWORKED DIMENSION=1.6 L X 1.2 W, REF REO 601R-Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237491Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 499+1, LBL 41 TO LBL 43, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 499+1, LBL 41 TO LBL 43, W/L 73.50, STR 17. REWORKED DIMENSION=5.5 L X 0.8 W, REF REO 601R-Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237493Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 409+128+10 TO FS 424+4, LBL 36 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (4 EA) POSITIONS AT FS 409+128+10 TO FS 424+4, LBL 36 TO LBL 43, STR 17, W/L 73.50. REWORDec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237490Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 484, LBL 42, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 484, LBL 42, W/L 73.50, STR 17. REWORKED DIMENSION=2.3 L X 1.5 W, REF REO 601R-53-41-666 REV (C). PERFDec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237473Floorbeam · corrodedPRESSURE FLOOR ANGLE AND SUPPORT AT FS 544 TO FS 559, RBL 43, STR 17, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (2 EA) POSITIONS AT FS 544 TO FS 559, RBL 43, STR. 17, W/L 73.50, STR 17. REWORKED DIMENDec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237485Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 529+13, RBL 40, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (3 EA) POSITIONS AT FS 529+13, RBL 40, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1)=1.2 L X 0.8 W, (P2)=1.6 L X 1.15Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237489Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 529+11, LBL 40 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE (2 EA) POSITIONS AT FS 529+11, LBL 40 TO LBL 43, STR 17, W/L 73.50 REWORKED DIMENSIONS (P1)=0.25 Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237487Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 544, LBL 41 TO LBL 43, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 544, LBL 41 TO LBL 43, W/L 73.50, STR 17. REWORKED DIMENSION=1.0 L X 1.0 W, REF REO 601R-53-4Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237486Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 513+6, RBL 40 TO RBL 43, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 513+6, RBL 40 TO RBL 43, W/L 73.50, STR 17. REWORKED DIMENSION=1.8 L X 1.8 W, REF REO 601R-Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237472Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 559, LBL 33 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (2 EA) POSITIONS AT FS 559, LBL 33 TO LBL 43, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1)=1.2 W X 1.6 L, (P2Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237480Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 409+128, RBL 36, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE AT FS 409+128, RBL 36, W/L 73.50, STR 17. REWORKED DIMENSION=1.2 W X 1.6 L, REF REO 601R-53-41-666 REV (C). PERFDec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237482Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 439, LBL 41 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE (2 EA) POSITIONS AT FS.439, LBL 41 TO LBL 43, STR. 17, W/L 73.50. REWORKED DIMENSIONS (P1) = 2.0 L Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237483Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 449.85, LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (3 EA) POSITIONS AT FS 449.85, LBL 43, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1)=1.1 L X 0.7 W, (P2)=0.9 L X 0.5 Dec 13, 2020 · N457AW · Cndair CL6002B19SDR A6WA202012237494Floorbeam · corrodedPRESSURE FLOOR PANEL AT FS 513+5, LBL 42, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE (3 EA) POSITIONS AT FS 513+5, LBL 42, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1) = 0.6 L X 0.92 W, (P2)=1.Dec 13, 2020 · N457AW · Cndair CL6002B19
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