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 MASA20201223139Floorbeam · corrodedCORROSION ON FLOOR BEAM, UPPER/AFT FLANGE IN STA F2-280 AND LBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) FLOOR BEAM UPPER/AFT FLANGE IN STA F2-280 AND LBL AT PAX CABIN FWD WET AREA WAS REPLACED, PER CRJ900 SRM-51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 PNov 28, 2020 · N916FJ · Cndair CL6002D24SDR MASA20201215092Floorbeam · corrodedCORROSION ON FLOOR SUPPORT IN STA FS 260 BETWEEN STRG 26LT TO 26RT. CORRECTIVE ACTION: FLOOR SUPPORT IN STA FS 260 BETWEEN STRG 26LT TO 26RT WAS REPLACED, PER CRJ-900-SRM 51-42-20-001-001 AO1 PAR 6A.Nov 28, 2020 · N916FJ · Cndair CL6002D24SDR FDEA202011282985Floorbeam · corrodedCENTER CARGO COMPARTMENT STATION 1841 LEFT HAND X=6 FLOOR PANEL SUPPORT FOUND CORRODED. CENTER CARGO COMPARTMENT STATION 1841 LEFT HAND X=6 FLOOR PANEL SUPPORT. CORROSION REMOVED AND FOUND EXCEED LIMIT, AS PER SRM 53-00-00-2R FIGURE 206. REPAIR GENERAL. RENov 28, 2020 · N607FE · Doug MD11FSDR FDEA202011282984Floorbeam · corrodedAFT CARGO COMPARTMENT STATION 1902.15 X=18 TO -18 FLOOR PANEL SUPPORT FOUND CORRODED. AFT CARGO COMPARTMENT STATION 1902.15 X=18 TO -18 FLOOR PANEL SUPPORT. CORROSION REMOVED FOUND EXCEED LIMIT AS SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL. REPAIRED AS PER ENov 28, 2020 · N607FE · Doug MD11FSDR SCNA20201201364Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER CAP SURFACE AT STA 328 RBL 54 WL 208. REMOVED DAMAGED SECTION OF FLOOR BEAM UPPER FLANGE FROM BS 328 RBL 1.10" TO RBL 65 WL 208, PER SRM 53-10-51-28-7 PARA 4, FABRICATED-1 T-CHORD PER SRM 53-10-51-2R-7 AND INSTALLED, PER ER 20-03Nov 28, 2020 · N817SY · Boeing 7378K2SDR SWAA2021040832598Attach Angle · crackedBS 500H; LBL 24; WL 153; STR 26L; L/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON FWD SIDE OF FRAME 500H; MARKED IN BLACK / REMOVED AND REPLACED L/H FLOOR BEAM & ANGLE INTERCOSTAL ATTACH CLIP P/N 143A7502-159 TAG #A74757 STA 500H LBL 24 STRINGER 26Nov 25, 2020 · N8607M · Boeing 7378H4SDR SWAA2021040862363Attach Fitting · crackedBS 500H; LBL 24; WL 153; STR 26L; L/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON FWD SIDE OF FRAME 500H; MARKED IN BLACK / REMOVED AND REPLACED L/H FLOOR BEAM & ANGLE INTERCOSTAL ATTACH CLIP P/N 143A7502-159 TAG #A74757 STA 500H LBL 24 STRINGER 26Nov 25, 2020 · N8607M · Boeing 7378H4SDR SWAA2021040832596Attach Fitting · crackedBS 500G; RBL 24; WL 153; STR 26R; R/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON AFT SIDE OF FRAME 500G; MARKED IN BLACK / REMOVED AND REPLACED R/H FLOOR BEAM Z ANGLE INTERCOSTAL ATTACH CLIP AFT SIDE OF FRAME STA 500G RBL 24 STRINGER 26R P/N 143A7Nov 25, 2020 · N8607M · Boeing 7378H4SDR SWAA2021040832597Attach Fitting · crackedBS 500G RBL 24; WL 153; STR 26R; R/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON FWD SIDE OF FRAME 500G; MARKED IN BLACK / REMOVED AND REPLACED R/H FLOOR BEAM Z ANGLE INTERCOSTAL ATTACH CLIP FWD SIDE OF FRAME STA 500G RBL 24 STRINGER 26R P/N 143A75Nov 25, 2020 · N8607M · Boeing 7378H4SDR SWAA2021040832595Attach Fitting · crackedBS 500H; RBL 24; WL 153; STR 26R; R/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON FWD SIDE OF FRAME 500H; MARKED IN BLACK / REMOVED AND REPLACED R/H FLOOR BEAM Z ANGLE INTER COSTAL ATTACH CLIP FWD SIDE OF FRAME STA 500H RBL 24 STRINGER 26R P/N 143ANov 25, 2020 · N8607M · Boeing 7378H4SDR SWIA202054823Floorbeam · corrodedCORROSION ON FLOOR BEAM TOP SURFACE AT FS 1031.00, RBL 9. C-CHECK RO 12/26/2020. CORROSION IS BEYOND ALLOWABLE DAMAGE LIMITS. PERFORMED SPLICE REPAIR OF RBL 9 FLOORBEAM FROM FS 1015-1047, REF CRJ 900 SRM AND REO. COMPLETED FORM M-337. SEE CONTINUATION CARNov 25, 2020 · N802SK · Cndair CL6002D24SDR FDEA202011252971Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 24. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.Nov 25, 2020 · N780FD · Boeing 757222SDR FDEA202011252970Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 39.5. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.Nov 25, 2020 · N780FD · Boeing 757222SDR FDEA202011252969Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 32. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.Nov 25, 2020 · N780FD · Boeing 757222SDR FDEA202011252968Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681-RBL 18. REPLACED NUTPLATE AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV"F", AND B757 SRM 51-40-02.Nov 25, 2020 · N780FD · Boeing 757222SDR FDEA202011252967Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 12. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.Nov 25, 2020 · N780FD · Boeing 757222SDR FDEA202011252966Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE AT PRESSURE DECK THRU AFT PIT BULKHEAD PANEL BS 1681-RBL 36. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 "F", AND B757 SRM 51-40-02.Nov 25, 2020 · N780FD · Boeing 757222SDR JR2R20201125510Floorbeam · corrodedLT SIDE OF FLOOR BEAM RBL 9 CORRODED AT FR 90.Nov 25, 2020 · N89317 · Emb ERJ170200LRSDR JR2R20201125503Floorbeam · corrodedFLOOR BEAM RBL 9 AT FR 87 CORRODED.Nov 25, 2020 · N89317 · Emb ERJ170200LRSDR SWIA202055469Strap · corrodedFLOOR STRAP CORRODED RBL 29-RBL 43 FS 559.00, MARKED. C-CHECK RO 1/16/2021. REMOVED CORROSION ON 3 EA AREAS STRAP FLOOR RBL 29-RBL 43, FS 559.00, REF CRJ200 SRM 51-21-06 ORIGINAL MATERIAL THICKNESS IS .050", LOWEST REMAINING THICKNESS IS .043", MATERIAL RENov 24, 2020 · N868AS · Cndair CL6002B19SDR SWIA202055425Strap · corrodedFLOOR STRAP CORRODED, LBL 29-LBL 43 FS 559.00, MARKED. C-CHECK RO 1/16/2021. BLENDED CORROSION FROM FLOOR STRAP LOCATED AT FS 559.00 BETWEEN LBL 29 AND LBL 43, REF CRJ 200, SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. INSTALLED 1 EA NEW FLOOR STRNov 24, 2020 · N868AS · Cndair CL6002B19SDR SWIA202055419Floorbeam · corrodedFLOOR SUPPORT ANGLE ON THE AFT SIDE OF FS 280.00 BEAM BETWEEN LBL 9 & RBL 9 IS CORRODED AT MULTIPLE AREAS, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FS 280 LBL 9 RBL 9 AFT ANGLE, REF CRJ 200 SRM 51-42-06-00, CRJ200 SRM 51-42-21-00, AND PREVIOUSLY INNov 24, 2020 · N868AS · Cndair CL6002B19SDR SWIA202055418Floorbeam · corrodedFLOOR SUPPORT ANGLE ON THE FORWARD SIDE OF FS 280.00 BEAM BETWEEN LBL 9 & RBL 9 IS CORRODED AT MULTIPLE AREAS, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FS 280 LBL 9 RBL 9 FWD ANGLE, REF CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 600-3401Nov 24, 2020 · N868AS · Cndair CL6002B19SDR FDEA202011242962Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 24. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F" AND B757SRM 51-40-02.Nov 24, 2020 · N780FD · Boeing 757222SDR FDEA202011242961Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 4. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N 5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.Nov 24, 2020 · N780FD · Boeing 757222SDR FDEA202011242960Floorbeam · corrodedMAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1681, LBL 24-BL 47. REMOVED SURFACE CORROSION AS REQUIRED, IAW B757 SRM 53-60-51-1A. ORIGINAL MATERIAL THICKNESS .071. MATERIAL LOSS .006. REMAINING MATERIAL THICKNESS .065 FOUND TO BE WINov 24, 2020 · N780FD · Boeing 757222SDR FDEA202011242959Floorbeam · corrodedMAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1681, BL 4-RBL 54. REMOVED SURFACE CORROSION AS REQUIRED, IAW B757 SRM 53-60-51-1A. ORIGINAL MATERIAL THICKNESS .071, MATERIAL LOSS .004 REMAINING MATERIAL THICKNESS .067 FOUND TO BE WITHIN Nov 24, 2020 · N780FD · Boeing 757222SDR SWIA202055410Floorbeam · corrodedTHE LBL 9.0 FLOOR-SUPPORT BEAM'S CAP HAS CORROSION ALONG ITS ENTIRE LENGTH, FROM APPROXIMATELY FS 409+128 TO APPROXIMATELY FS 559, THE CORROSION IS ON BOTH THE INBOARD AND OUTBOARD FLANGES, AND EXTENDS UNDER THE FLOOR BEAM SEAT RAILS (MARKED WITH RED GREASE PENov 23, 2020 · N868AS · Cndair CL6002B19SDR SCNA20201201389Floorbeam · corrodedSTA 947.5, RBL 50 WL 208 FLOOR BEAM UPPER CAP HAS CORROSION. CORROSION ON STA 947.5 FLOOR BEAM UPPER CHORD RBL 50, WL 208 FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-51-1A-1 FIG 104 DETAIL C. REMOVED DAMAGE AND REPAIRED, IAW SRM 53-70-51-2R-5.Nov 23, 2020 · N817SY · Boeing 7378K2SDR R61A2020112300810Floorbeam · gougedWHILE IN HEAVY CHECK, MAJOR REPAIR. KNIFE MARK (GOUGE) FR 17 CROSSBEAM. REPAIRED PER ETD2020-170-032112.Nov 23, 2020 · N117HQ · Emb ERJ170200LRSDR R61A2020112300809Floorbeam · corrodedWHILE IN HEAVY CHECK, MAJOR REPAIR. FR 84 CROSSBEAM INBOARD OF RT FLOOR BEAM CORROSION. REPAIRED PER ETD2020-170-031987.Nov 23, 2020 · N117HQ · Emb ERJ170200LRSDR REXA202012070825Floorbeam · corrodedFWD "J" ANGLE CORRODED AT FS 280 BETWEEN RBL 11 AND LBL 11 AND CLIPS ATTACHED TO "J" ANGLE CORRODED. REMOVED AND REPLACED J ANGLE AND REPLACED/REPAIRED CORRODED CLIPS, IAW SRM 57-42-06-001-001-A01, 51-42-21-001-001-A01, 51-21-06-001-001-A01.Nov 22, 2020 · N304PQ · Cndair CL6002D24SDR R61A2020120700849Floorbeam · corrodedAFT CARGO COMPARTMENT, CORROSION FOUND ON RT FLOOR SUPPORT AT FR 76 BETWEEN STR 29L-29R. REPLACED IAW SRM 51-41-01.Nov 22, 2020 · N212JQ · Emb ERJ170200LRSDR REXA2020120700810Floorbeam · corrodedFS 280 CROSSBEAM J ANGLE CORRODED. FS 280 CROSSBEAM "J" ANGLE OUT OF LIMITS. REMOVED AND REPLACED "J" ANGLE, IAW 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. P/N CC670-340-951SB.Nov 22, 2020 · N309PQ · Cndair CL6002D24SDR SWIA202055595Floorbeam · corrodedCABIN FS 549 FLOOR CROSSBEAM BETWEEN LBL 9 AND RBL 9 CORRODED, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON FS 549 FLOOR CROSSBEAM BETWEEN LBL 9 AND RBL 9, REF CRJ 700 SRM 51-21-06-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-53-31-579 REV- DATENov 21, 2020 · N758EV · Cndair CL6002C10SDR SWIA202055557Floorbeam · corrodedCABIN, FS 549 FLOOR CROSS BEAM BETWEEN RBL 9 AND RBL 27 CORRODED, AS MARKED. C-CHECK RO 1/17/2021. COMPLIED WITH ALL STEPS OF REO 670-53-31-579 REV - DATED 2020-12-03 FOR CORROSION ON FLOOR CROSS BEAM AT FS 549 BETWEEN RBL 9 AND RBL 27.Nov 21, 2020 · N758EV · Cndair CL6002C10SDR REXA2020120700811Floorbeam · corrodedFS 280 BEAM CORRODED BETWEEN RBL 9 AND LBL 9. INSTALLED A NEW SERVICEABLE LT CROSS BEAM P/N CC670-34094-1S, IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01. INSTALLED DRIP TRAY LEFT SRM CRJ 900 51-42-13-001-001-A01.Nov 21, 2020 · N309PQ · Cndair CL6002D24SDR SWIA202055541Floorbeam · corrodedCOCKPIT AFT FLOOR SUPPORT ANGLE ON FWD SIDE OF 280 BEAM LBL 9-RBL 9 IS CORRODED. C-CHECK RO 1/17/2021. BLENDED CORROSION ON THE COCKPIT AFT FLOOR SUPPORT "OUT OF LIMITS", REF CRJ700 SRM 53-00-00-101-001-A01, SRM 51-21-06-001-001-A01 ORIGINAL: .063; REMAININGNov 20, 2020 · N758EV · Cndair CL6002C10SDR REXA2020120700830Floorbeam · corrodedFS 280 LT FLOOR SUPPORT CROSSBEAM IS CORRODED. REMOVED & REPLACED LT FLOOR SUPPORT P/N CC670-34094-1S, IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01, 51-42-22-001-001-A01.Nov 20, 2020 · N304PQ · Cndair CL6002D24SDR A6WA202011207425Floorbeam · corrodedCAP STRIP CORRODED ON CROSS BEAM 62, FS 589 BETWEEN LBL 9 AND LBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAP STRIP ON CROSS BEAM 62 FS 589 BETWEEN LBL 9 AND LBL 27, IAW CRJ200 SRM 51-42-06.Nov 20, 2020 · N414ZW · Cndair CL6002B19SDR R61A2020120700850Floorbeam · corrodedCROSSBEAM AT FR 14 RT FOUND WITH CORROSION. REPAIRED IAW SRM 53-00-10 FIG 203.Nov 19, 2020 · N212JQ · Emb ERJ170200LRSDR AALA202011249012Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. FOUND AREA OF CORROSION ON FLOOR SUPPORT BEAM AROUND LAVATORY MOUNT POINT AT FR 66 AND Y-1292, MEASURING 1 INCH X 1 INCH X 0.030 INCH. REPLACED FLOOR BEAM SUPPRT, REF SRM 51-72-11.Nov 19, 2020 · N193UW · Airbus A321211SDR AALA202011249011Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. FOUND AREA OF CORROSION ON FLOOR SUPPORT BEAM AT LAVATORY MOUNT POINT AT FR 66, MEASURING 0.750 INCH X 0.750 INCH X 0.025 INCH. REMOVED AND REPLACED FLOOR BEAM, REF SRM 51-72-11.Nov 19, 2020 · N193UW · Airbus A321211SDR AALA202011239012Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. FOUND CORROSION AT FLIGHT ATTENDANT SEAT MOUNT FLOOR BEAM Y-465 AND FR 66 PLUS 6 INCHES. REPLACED FLOOR BEAM, REF SRM 61-42-11.Nov 19, 2020 · N193UW · Airbus A321211SDR SWIA202055331Angle · corrodedFS 280 FWD J ANGLE CORRODED BETWEEN LBL 9 AND RBL 9. C-CHECK RO 1/6/2021. REMOVED AND REPLACED J ANGLE, IAW CJR 700 SRM 51-42-06-001-001 (A01)/51-42-06-001-001 (A010). SEE CONTINUE CARD FOR MAINTENANCE PERFORMED.Nov 18, 2020 · N755SK · Cndair CL6002C10SDR SWIA202054916Floorbeam · crackedCOCKPIT FLOOR SUPPORT, FLOOR BEAM AT LEFT BUTT LINE 12 HAS THE APPEARANCE OF A CRACK IN THE RADIUS OF ITS AFT VERTICAL FLANGE (APPROXIMATELY AT FS 280 ON THE FWD SIDE OF THE BULKHEAD BETWEEN WL 72.50 AND THE BOTTON OF THE BEAM. C-CHECK RO 12/28/2020. CUT OUTNov 18, 2020 · N787SK · Cndair CL6002C10SDR DALA2020111903779Floorbeam · corrodedDURING INSPECTION FOUND CORROSION LEVEL 2 ON STRINGERS STA 650 RBL 2.90, RBL 7.55, LBL 7.55, LBL 10.45, LBL 16.10 AND STA 700 RBL 2.90 AT FWD CARGO COMPARTMENT. STRINGERS REPAIRED PER SRM.Nov 18, 2020 · N590NW · Boeing 757351SDR EE4Y2020111811945Floorbeam · corrodedUPPER FUSELAGE BODY STATION 986, FLOOR BEAM UPPER CHORD WITH CORROSION AT SEVERAL PLACES. NOTE: THE FLOOR BEAM UPPER CHORD WAS REPAIRED, AS PER PEMCO ENGINEERING AUTHORIZATION NUMBER PD37-53-3198 INSTRUCTION (REF: JOB: A1J184 NRI: 2-32).Nov 18, 2020 · N288AU · Boeing 737490SDR SWAA2021080331018Floorbeam · crackedCRACKED BREAK PANEL STA 540; BL0-LBL 25; WL 207. / REMOVED AND REPLACED BREAK PANEL ASSY AT STA 540; BL0 - LBL25; WL 207; PER SRM 51-40-02-0G-0.Nov 17, 2020 · N730SW · Boeing 7377H4SDR SWAA2021080331019Floorbeam · crackedCRACKED BREAK PANEL STA 540; BL0-RBL 25; WL 207. / REMOVED AND REPLACED BREAK PANEL ASSY AT STA 540; BL0 - RBL 25; WL 207; PER SRM 51-40-02-0G-0; PARAGRAPH 7.Nov 17, 2020 · N730SW · Boeing 7377H4
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