JASC 5310
Service difficulty reports · 38,548
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 SWIA2020021848515Crossbeam · corroded*THE FS280.00 CROSSBEAM HAS MULTIPLE LOCTAIONS OF CORROSION. (C-CHECK) RO 2/14/2020 RH FS280 CROSSBEAM IS MISSING 100% MATERIAL IN MULTIPLE AREA AT RBL4. NO CORROSION NOTED LEFT OF BL 0 ON THE LH FS280 CROSSBEAM. REMOVED AND REPLACED THE RH 280 CROSSBEAM SDR SWIA2020021848514Crossbeam · corroded* THE FS280.00 CROSSBEAM CLIP AT LBL 9.00 HAS CORRSION. (C-CHECK) RO 2/14/2020 REMOVED CORRODED REPAIR PARTS AND REPLACED WITH NEW REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLETED FORM M-337.SDR SWAA2019121739743Crease Beam · corrodedCABIN FLOOR CREASE BEAM INBOARD CHORD CORRODED BETWEEN BS. 889 TO BS. 1006, STR. 17R. / R&R CREASE BEAM IAW SRM & DWG.SDR AALA2019121329051Expansion Joint · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN FLOOR EXPANSION JOINT AT BS 540 AND RBL 10. REPLACED EXPANSION JOINT PER AARD 51-00-05-1.SDR AALA2019121329050Expansion Joint · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN FLOOR EXPANSION JOINT AT BS 540 AND LBL 10. REPLACED EXPANSION JOINT PER AARD 51-00-05-1.SDR UIEA2019120906036Longeron · corrodedLEFT SIDE OVERWING LONGERON CORRODED.(<P>REMOVED CORROSION ON LEFT SIDE OVERWING LONGERON IAW B767-200 SRM 51-10-02 AND REPAIRED IAW AMES NO. #47389REA05. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #9, PGS 1 & 2.</P>)SDR UIEA2019120906037Door Frame · corroded ALC DOOR CUTOUT, FWD EDGE FRAME STRAP UPPER SURFACE IS CORRODED AT STA 1270, S32R.(<P>REPAIRED FRAME IAW B767-200 SRM 51-40-02 AND AMES 47389REA06. SEE PARTIAL WORK ACCOMPLISHED AND PWS 46.</P>)SDR FDEA201912043170Beam · corrodedTRANSVERSE BEAM B/S 900 - 1040, LBL 46 IS CORRODED BEYOND PERMITTED LIMITS IAW SRM 53-00-51-1A ALLOWABLE DAMAGE 1, DETAIL III. INSTALLED NEW TRANSVERSE BEAM IAW SRM 51-40-02 AND BOEING DRAWING #111N5201SDR FDEA201912033164Beam · corrodedTRANSVERSE BEAM B/S 900-1040 LBL 25 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A ALLOWABLE DAMAGE DETAIL III. REPLACED TRANSVERSE BEAM B/S 900-1040 LBL 25 IAW SRM 51-40-10 AND BOEING DRAWING# 111N5202SDR SWAA2022040532641Web · corrodedAFT CARGO COMPARTMENT BETWEEN STA 787+7' AND 847 UNDER CENTER LOWER DOOR TRESHOLD PLATE ;TRESHOLD WEB IS CORRODED IN SEVERAL AREAS BETWEEN RBL 20 AND RBL 28 WL 155.3 AS MARKED / REMOVED CORROSION AFT CARGO COMPARTMENT THRESHOLD WEB STA 787+7 TO 847 IAW SRM 51-SDR R61A2019121731386Beam · corroded***AIRCRAFT IS IN HEAVY CHECK***LONGITUDINAL BEAM UPPER FLANGE REPAIR CORRODED AT FR 19 AND LBL 11. REPLACED REPAIR IAW SRM 53-10-10 REP. 01 ***AIRCRAFT REMAINS IN HEAVY CHECK***SDR R61A2019121731383Crossbeam · corroded***AIRCRAFT IS IN HEAVY CHECK*** CROSSBEAM UPPE5R FLANGE FOUND CORRODED AT FR14, RBL24.REPAIRED CROSSBEAM UPPER FLANGE IAW SRM 53-10-10 ***AIRCRAFT REMAINS IN HEAVY CHECK***SDR R61A2019121631379Beam · corroded***AIRCRAFT IS IN HEAVY CHECK***AFT PAX DOOR THRESHOLD BEAM CORRODED BTW FR 85-87. REPLACED BEAM IAW SRM 51-43-03.***AIRCRAFT REMAINS IN HEAVY CHECK***SDR SWAA2019120939444Crease Beam · corrodedAFT CABIN R-2 CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 947+12 TO BS. 986+3, RBL 51. / R&R CREASE BEAM IAW SRM AND DWG.SDR DALA2019120547084Beam · corroded(LOG 1385795) DURING INSPECTION FOUND CORROSION ON PREVIOUS REPAIR OF LH BEAM BTW STA= 986.5 W2 AREA. FILLER WAS REPLACED PER. B737-800 SRM 51-40-02 PAR 4 AND , ER/A 464736-14MA REV. A.SDR DALA2019120547083Beam · corroded(LOG 1385764) DURING INSPECTION FOUND CORROSION ON PREVIOUS REPAIR OF RH BEAM BTW STA= 986.5 W2 AREA. FILLER WAS REPLACED PER B737-800 SRM 51-40-02 PAR 4 AND ER/A 464736-14MA REV. A.SDR DALA2019120547069Plate · missing(AIRCRAFT 5651, L/P 5373087) DURING SERVICE CHECK FOUND: DOOR L1 AFT FRAME DOOR STRESS PLATE MISSING. 4TH UP FROM BOTTOM. CORRECTIVE ACTION: REPLACED PLATE AS REQUIRED PER B757AMM 52-11-00-968-001.SDR FDEA2019120433164Beam · corrodedTRANSVERSE BEAM B/S 900-1040 LBL 25 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A ALLOWABLE DAMAGE DETAIL III. REPLACED TRANSVERSE BEAM B/S 900-1040 LBL 25 IAW SRM 51-40-10 AND BOEING DRAWING# 111N5202SDR R61A2019121721385Beam · corroded***AIRCRAFT IS IN HEAVY CHECK*** LONGITUDINAL BEAM BTW FR 86-89 AND RBL 10 CORRODED. REPLACED BEAM IAW SRM 51-43-03. ***AIRCRAFT REMAINS IN HEAVY CHECK***SDR DALA2019120637122Pressure Panel · crackedCRACK INDICATION ON PLATE PRESSURE PANEL OPEN HOLE FR36RH Y-773, CRACK DIRECTION 12 OCLOCK LOOKING AFT. THE CRACK EXCEEDS THE AUTHORIZED REPAIR AREA AT THE PRESSURE PANEL BETWEEN FR35RH AND FR36RH. PERFORMED SECTION 1AS REPAIR AS PER ERA 582610-14AD REV. ORIGISDR AALA2019120439009Bracket · brokenAIRCRAFT WAS GROUNDED: PILOT REPORTS RIGHT THROTTLE STICKS AT MID POSITION. NEED TO FORCE IT PAST MID POSITION TO SET THRUST. MAINTENANCE FOUND RIGHT ENGINE THROTTLE CONTROL BOX HAS BROKEN SHIELD, BLENDED EDGE OF BRACKET, REINSTALLED RIVETS AND VERIFIED THROTTSDR FDEA2019120423161Beam · corrodedTRANVERSE BEAM B/S 900-1040 RBL 25 CORRODED REPLACED TRANSVERSE BEAM B/S 900-1040 IAW SRM 51-40-02 AND BOEING DRAWING#111N5202SDR SIMA2019121930002Frame · corrodedFRAME AT FS319.00 CORRODED BETWEEN STRINGER 26 LT AND 27 LT.-C/A-REPAIRED FS319.00 BETWEEN STR 26LT AND 27LT IAW ERS-CR-53MR-3980.LSDR CALA2019120302121Torsion Box · corrodedAFT CARGO TORSION BOX UPPER SURFACE HAS LIGHT SURFACE CORROSION MULTIPLE AREAS, A3NB-33-3-6010, PER LCQ NR 9290450, REMOVED AND REPALCED AFT CARGO TORSION BOX WRB R/H SIDE FR52-56 IAW A320 SRM 51-42-11-801 PARAGRAPH 6 2E,2F.SDR SWAA2019123140091Beam · corrodedFLOOR STRUCTURE BEAM CORRODED AT BS. 986.5, STR. 17L. / REPAIRED FLOOR STRUCTURE BEAM IAW EA.SDR SWAA2019121639632Support Frame · corrodedAFT CARGO COMPARTMENT BULKHEAD PANEL SUPPORT FRAME HAD SURFACE CORRODED AT BS. 947, BETWEEN LBL 9 TO RBL 18. / R&R SUPPORT IAW SOM & DWG.SDR VNAA201911299990Door Frame · crackedPAX DOOR FS 347.25 FRAME IS CRACKED BELOW THE SUPPORT WHEEL AND FASTENERS ARE PULLING THROUGH SKIN. J.ROY 10/10/19(JW) M/A: 1. REMOVED FRAME PAX DOOR @ FS 347.25 IAW CRJ 700 SRM 51-42-00-001-001-A01. J.DROZDIK,B.KELLEY 10/17/19 C/A: 1. INSTALLED NEW PAX DOOR ASDR VNAA201911299990BDoor Frame · corrodedFWD PAX DOOR FWD FRAME AT FS 311.75 IS CORRODED ON BOTH SIDES. J.ROY 10/10/19(JW) M/A: 1. REMOVED FWD FRAME PAX DOOR @ 311.75 IAW CRJ 700 SRM 51-42-06-001-001-A01. J.DROZDIK,B.KELLEY 10/17/19 C/A: 1. INSTALLED NEW PAX DOOR FWD FORMER IAW CRJ 700 SRM 51-42-06-2SDR SWAA2022032599438Intercostal · elongatedELONGATED HOLE WEB - INTERCOSTAL LOCATED BETWEEN BS 440 AND BS 460 AT LEVEL S-26L AT FWD CARGO COMPARTMENT / REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS 440 AND BS 460 AT LEVEL S-26L FWD C.C IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 143A7505 REV.4SDR R61A2019120781355Beam · corroded***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** AT FR 87 & RBL 11, CORROSION FOUND ON LONGITUDINAL BEAM. REPLACED LONGITUDINAL BEAM IAW SRM 51-41-01 & 51-43-03. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR AALA2019120439056Expansion Joint · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN EXPANSION JOINT AT BS 540 AND LBL 7. REPLACED EXPANSION JOINT PER AARD 51-00-05-1.SDR SWAA2022032525944Intercostal · corrodedAFT CARGO COMPARTMENT STA 747-767 RBL 22 WL 158; INTERCOSTAL IS CORRODED ON UPPER FLANGE AT NUTPLATES. / REMOVED AND EVALUATED CORROSION ON INTERCOSTAL STA 747-767 RBL 22. ORIGINAL THICKNESS .030' LOSS OF .010' WITH .020' REMAINING BLENDS FOUND TO BE OUT OF LISDR SWAA2022032525943Intercostal · corrodedAFT CARGO COMPARTMENT STA 727A-727B LBL22 WL 158; INTERCOSTAL IS CORRODED ON UPPER FLANGE AT FASTENER HOLES. / REMOVED AND EVALUATED CORROSION. ORIGINAL MATERIAL THICKNESS .030' LOSS OF .020' WITH .010' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-SDR SWAA2022032599424Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BTW BS380 AND BS400 AT BL0 AT PASSENGER CABIN (1 EA) / REPLACED ANGLE FLOOR STRUCTURE LOCATED. BETWEEN BS380 AND BS400 BL0 AT_PASSENGER CABIN (1E/A) IAW B737-700 SRM 51-40-02 AND DWG 143A5400SDR SWAA2022032547893Support · corroded***CORROSION*** FWD CARGO PIT LOWER AFT BULKHEAD SUPPORT HAS CORROSION BS 520 LBL 25 TO RBL 25 WL 156 / AFTER EVALUATION OF CORROSION DAMAGE ON THE FWD CARGO AFT LOWER BULKHEAD SUPPORT STA 520 LBL 25 - RBL 25 WL 156 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1SDR SWAA2022032547892Support · corroded***CORROSION*** FWD CARGO PIT R/H AFT BULKHEAD SUPPORT HAS CORROSION BS 520 RBL 25 WL 156 / AFTER EVALUATION OF THE CORROSION DAMAGE ON THE FWD CARGO R/H AFT BULKHEAD SUPPORT FOUND TO BE OUT OF ALLOWABLE LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM. REMOVED ANSDR SWAA2022032547891Channel · corroded***CORROSION*** FWD CARGO PIT L/H Z CHANNEL HAS CORROSION BS 500 TO BS 520 LBL 25 WL 156 / CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED FWD CARGO L/H 'Z' CHANNEL FROM STA 490 TO 520 LBL 25 WL 156 SPLICE LOCATED AT STA SDR SWAA2022032547890Channel · corroded***CORROSION*** FWD CARGO PIT R/H Z CHANNEL HAS CORROSION BS 500A TO BS 520 RBL 25 WL 156 / CORROSION FWD CARGO R/H Z CHANNEL AT 400DA TO 520; RLB 25; WL 156; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED FWD CARGO R/H Z CHANNEL STA 500SDR SWAA2022032547883Channel · corroded***CORROSION*** AFT CARGO PIT Z CHANNEL R/H SIDE FROM BS 867 TO BS 887 RBL 25 WL 156 HAS CORROSION / REMOVED AND REPLACED AFT CARGO PIT Z CHANNEL R/H SIDE FROM BS 867 TO BS 887 RBL 25 WL 156 IAW SRM 51-40-02-0G-0 DWG# 146A7502 + DWG# 146A7500 57903U 02DEC19SDR SWAA2022032547882Channel · corroded***CORROSION*** AFT CARGO PIT Z CHANNEL L/H SIDE FROM BS 807 TO BS 727F LBL 25 WL 156 HAS CORROSION / AFTER EVALUATION OF CORROSION DAMAGE ON THE AFT CARGO L/H 'Z' CHANNEL STA 727F TO 847 LBL 25 WL 156 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED DSDR SWAA2022032547881Channel · corroded***CORROSION*** AFT CARGO PIT Z CHANNEL R/H SIDE FROM BS 767 TO 727F RBL 25 WL 156 HAS CORROSION / CORROSION AFT CARGO PN-'Z' CHANNEL R/H SIDE FROM BS 767 TO 727 E+12 RBL 25. WL 156 OUT OF LIMITS REMOVED AND REPLACED 'Z' CHANNEL I-A-W SRM 57-40-02-0G-0 AND BOESDR SWAA2019121139543Crease Beam · corrodedCREASE BEAM WEB CORRODED BETWEEN BS. 718 TO BS. 728, RBL 63.5. / R&R WEB PER SRM & DWG.SDR SWAA2019121139542Crease Beam · corrodedCREASE BEAM WEB CORRODED AT BS. 712, RBL 66.5. / R&R WEB PER SRM AND DWG.SDR DALA2019112806952Door Frame · crackedRH OVERWING EXIT FRAME HAS A CONDITION 3 CRACK AT STA 674 FRAME TAB UPPER RADIUS REF 5310-01436-01D STEP 7. NRC 138-0004:5310-01436-01D/001 00087: REPLACED FRAME REF AMDS 5310-01436-03B. (LP #1377797)SDR AALA201911289010Beam · corrodedAIRCRAFT IN BASE VISIT: DOOR SILL/FLOOR SUPPORT NUTPLATE HOLE HAVE CORROSION AT FR68, Z-500, Y1292. INSTALLED REPAIR ANGLE AND FILLER REPAIR IAW SRM 53-41-14-283-002.SDR ABXR2019112700321Failsafe · corrodedFAILSAFE STRAP ON FRAME AT ALC DOOR CUTOUT WAS CORRODEDSDR SWAA2022032525936Support Angle · corrodedFORWARD CARGO PIT STA 500D BULKHEAD STRUCTURE RIGHT CURVED LOWER CHORD RBL 25 WL 157 HAS CORROSION AROUND LOWER FASTENER HOLE / REPLACED FORWARD CARGO STA 500D RH COVERED BLKHD SUPPORT PN 143A9485-34 I/A/W SRM 51-40-02-0G-0 & DWG 143A7902 SHEET 209.SDR SWAA2022032499423Intercostal · elongatedELONGATED HOLE FLOOR STRUCTURE INTERCOSTAL LOC.BS540 RBL24.5 TO RBL45. 5 AT PASSENGER CABIN (3 EA) / REPLACED FLOOR STRUCTURE INTERCOSTAL LOC BS540 RBL 24.5 TO RBL 45.5 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DRAWING 143A0060 SHEET 51 REV-SDR SWAA2022032599420Intercostal · elongatedELONGATED HOLE FLOOR STRUCTURE ON INTERCOSTAL LOC.BS540 LBL24.5 TO LB L45.5 AT PASSENGER CABIN (3 EA) / REPLACED FLOOR STRUCTURE INTERCOSTAL(PANEL BREAK) LOC BS540 LBL 24.5 TO LBL 45.5 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DRAWING 143A0060SDR C77A2019121360002Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE UPPER FLANGE OF THE FR84 CROSSBEAM IN THE CABIN FLOOR STRUCTURE OF THE CENTER FUSELAGE III. REFER ETD2019-170-15
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