JASC 5320
Service difficulty reports · 216,159
Reports filed under 5320 · Fuselage Miscellaneous 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 = '5320' 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 = '5320' 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 SWAA2024112150126Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] LINE ITEM 2 ON PART REQUIREMENTS FOR P/N 146A7502-27 WAS BAD FROM STOCK AND NOT ISSUED TO N7741C FOR USE; THAT PART WAS RETURNED SDR SWAA2024112150127Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED FWD SHIELD BETWEEN BS767 TO BS787 RBL 22 WL 156 ACB PER SRM 51-40-02 AND BOEING DWG 146A0081.;[02] ADDED REV LEVEL TO DWG; SSDR SWAA2024112150128Support · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SUPPORT AS PER SRM 51-40-02-0G-0; DWG 146A7500 REV: ASDR SWAA2024112150177Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES ON UNDERSIDE STA.767-794. MRKD<[01] BLENDED CORROSION AND FOUND TO BE OUT OF LIMIT IN REFERENCE TO SRM 53-00-53.;[02] REMOVED AFT CARGO R/H TRANSITION ANGLE STA.767-794 PER SRM 51-40-02.;[03] DRILLED NESDR SWAA2024112150157Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA.727F+16. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] COMPLETSDR SWAA2024112150170Angle · corrodedFWD CARGO L/H TRANSITION ANGLE HAS CORROSION AT NUMERUS NUT PLATE HOLES BS 500A - 500H (SEE ATTACHED PICS)<[01] BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] REMOVED FWD CARGO L/H TRANSITION ANGLE BETWEEN STA 500-500I PER SRM 5SDR SWAA2024112150160Floor Panel · corrodedFWD CARGO; AFT BULKHEAD TO FLOOR CORD HAS CORROSION BS 500I LBL 16<[01] BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-30-08-1A-1.;[02] REMOVED FWD CARGO; AFT BULKHEAD TO FLOOR CORD PER SRM 51-40-02.;[03] DRILLED NEW FWD CARGO; AFT BULKHEAD TO FSDR SWAA2024112150171Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727I +3+8+10.5+14.5+18.5. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00SDR SWAA2024112150172Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727J +6+10=14.5. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNRSDR SWAA2024112150162Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.747-767. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNRSDR SWAA2024112150173Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.767-787. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] COMPLESDR SWAA2024112150174Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.787-807. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON CARD TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] CSDR SWAA2024112150163Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA.727E+20.MRKD<[01] REMOVED R/H TRANSITION ANGLE STA 727-767. IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW TRANSITION ANGLE STA 727-767 IAW SRM 51-40-02.;[03] VERIFIED WORK PERFORMED ON CORRECTIVE ACSDR SWAA2024112150164Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727F+20.MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVTSDR SWAA2024112150175Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727H +6+9+13+16. MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVTSDR SWAA2024112150176Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727I +8+10.5+14.5+16+18.5. MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVTSDR SWAA2024112150165Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727J +2+2.5+6.5+10.5+12+14.5+18.5. MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVTSDR SWAA2024112150166Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.747-767. MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVTSDR SWAA2024112050349Panel · crackedSTA 540 BREAK PANEL CRACKED AT LBL 1; WL 208<[01] REMOVED AND REPLACED BREAK PANEL LOCATE AT PAX CABIN CENTER BS.540 BL.0 - LBL.24.75 WL 208 IAW B-737-700 SRM 51-10-02 & SRM 51-40-02 DWG#143A0060 REV: A.;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1;2; MEASDR SWAA2024112050350Panel · crackedSTA 540 BREAK PANEL CRACKED AT RBL 1; WL 208<[01] REMOVED AND REPLACED BREAK PANEL LOCATE AT PAX CABIN CENTER BS.540 BL.0 - RBL.24.75 WL 208 IAW B-737-700 SRM 51-10-02 & SRM 51-40-02 DWG#143A0060 REV: A.;[02] COMPLETED ALL STEPS.;[03] VERIFIED ALL STEPS; CORRESDR REXA2024111101446Door Sill · corrodedAFT BAGGAGE-BAY DOOR LOWER DOOR SILL HEAVILY CORRODED IN MULTIPLE AREAS BLENDED AND FOUND THE AFT CARGO DOOR SILL TO BE OUT OF LIMITS IAW CRJ-700 SRM 51-12-00-001-001-A01, 53-61-23-101-001-A01. LOCATED AND DRILLED NEW SERVICEABLE LOWER SILL P/N MM670-35655-003SDR SWAA2024110550016Stiffener · crackedVERTICAL STIFFENER IS CRACKED BS 663 LBL 26 WL 145<[01] CRACKED STIFFENER FOUND AT BS 663 LBL 26 WL 145; REMOVED AND INSTALLED NEW VERTICAL STIFFENER AT BS 663 LBL 26 WL 145 PER SRM 51-40-02-0G-0 AND DWG 111A1000 REV: A. FASTENERS COMMON TO VAPOR BARRIER WEB WSDR ASAA2024101853400Shear Web · corrodedCABIN FLOOR SHEAR WEB AFT OF R2 DOOR OPENING IS CORRODED. GROUNDED - YES. LOCATED AND DRILLED NEW SHEAR WEB ON AFT CABIN FLOOR OF R2 DOOR P/N 147A5712U35 TAG AS9388 IAW B737-700 SRM 51-40-05-0G-0 AAR MIG5 NON-ROUTINE 1022693-2000-0164 OK397800 ACCOMPLISHMENT FSDR AALA202410248836Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN BRACKET LOCATED IN INTERNAL TAIL COMPARTMENT STRUCTURE AT STA 2293.5. REPLACED BRACKET PER SRM 51-40-02-0G.SDR DALA2024102210287Channel · corroded(LOG 0620451) CORROSION ALONG AFT CARGO COMPARTMENT L/H ZEE CHANNEL FROM STA-727A TO STA-807. REMOVED AND REPLACED AFT CARGO L/H ZEE CHANNEL STA . 727 + 4 -847 IAW B737-900 SRM 51-40-02-0G, B737-900 SRM 53-00-53-2R PROCEDURE 5 AND BOEING DWG# 146A7500.SDR DALA2024102110230Floor Support · corroded(LOG 0616005) PASSENGER COMPARTMENT FLOOR STRUCTURE, STA. 915, LBL 28, WL 208 FLOOR SUPPORT/INTERCOSTAL, OUTER FLANGE UPPER SURFACE CORRODED. C/W ERA 621339-14 REV ORG.SDR DALA2024102110225Pressure Plate · corrodedSHIP 5650 CORROSION AROUND FASTENER HOLES IN AFT CABIN FLOOR STRUCTURE PRESSURE PLATE FWD END BS.1681 APROX BL.0 TO LBL.50. DOT 129-093. CORRECTIVE ACITON: COMPLIED WITH ERA 621334-14 REV ORIGINAL ATMAIN CABIN STA 1681 BL 0 TO LBL 50. (0615782)SDR FDEA202410181540Floor Support · no discrepancyEXISTING REPAIR ON MAIN DECK FLOOR SUPPORT AT Y730 BETWEEN FR11 AND FR13A REQUIRES EVALUATION FOR CONFORMITY ENTRY IN ERROR DUPLICATE WITH SDR#: 24-1506SDR VNAA202411240010Web · crackedCRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193. CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193 WAS REPAIRED PER CRJ/900 SRM 53-11-43-201-001-A01SDR 2A6R2024101771708Tee Fitting · corrodedDURING 1000 HOUR INSPECTION, FOUND CORROSION ON T CAP PN L533M1028203 AT THE CABIN FLOOR RAIL ATTACHMENT. FABRICATED REPLACEMENT PART IAW EC 135 MTC AND AIR METHODS ENGINEERING AUTHORIZATION 23-5300-EA-4882 REV. - DATED 09-05-2024.SDR SWAA2024111250202Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 727I-727J AROUND FASTENER HOLES.<[01] WORKED CORROSION PER SRM 53-00-53-1A-2.<BR>REMOVED .002 FROM ORIGINAL THK .40<BR>REWORK WITHIN LIMITS;[02] REWORKED AREA OUT OF LIMITS SDR SWAA2024111250193Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 727H-727I AROUND FASTENER HOLES.<[01] WORKED CORROSION PER SRM 53-00-53-1A-2.<BR>REMOVED .002 FROM ORIGINAL THK .40<BR>REWORK WITHIN LIMITS;[02] REWORKED AREA OUT OF LIMITS SDR SWAA2024111250203Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 727J-747 AROUND FASTENER HOLES.<[01] WORKED CORROSION PER SRM 53-00-53-1A-2.<BR>REMOVED .002 FROM ORIGINAL THK .40<BR>REWORK WITHIN LIMITS;[02] REWORKED AREA OUT OF LIMITS PSDR SWAA2024111250204Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 747-767 AROUND FASTENER HOLES.<[01] WORKED CORROSION PER SRM 53-00-53-1A-2.<BR>REMOVED .002 FROM ORIGINAL THK .40<BR>REWORK WITHIN LIMITS;[02] REWORKED AREA OUT OF LIMITS PESDR SWAA2024111250205Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 767-787 AROUND FASTENER HOLES. UPPER AND LOWER SURFACES.<[01] WORKED CORROSION PER SRM 53-00-53-1A-2.<BR>REMOVED .002 FROM ORIGINAL THK .40<BR>REWORK WITHIN LIMITS;[02] REWOSDR SWAA2024110649940Floor Support · crackedCABIN FLOOR INTERCOSTAL CRACKED AT STA 540 LBL 1.<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02;[02] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02;[03] JAMES LYNCH (TECHNICIAN); 17-OCT-2024 22:33 UTC<BR>REMOVED AND REPLACED INTERCOSTAL PER SRM 51-SDR SWAA2024110649941Floor Support · crackedCABIN FLOOR INTERCOSTAL CRACKED AT STA 540 RBL 1. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02SDR REXA2024110501421Angle · corroded"PASSENGER DOOR LOWER SILL ANGLE IS HEAVILY CORRODED BETWEEN F.S.310 TO F.S.349 PAX DOOR LOWER SILL ANGLE (KICK PLATE) HAS CORROSION ENTIRE THE CROSS-SECTIONAL ON BOTH SIDE OF THE ANGLE, 100% CORRODED IN SOME SPOT. FOUND TO BE ""OUT OF LIMITS"" IAW CRJ-900 SSDR REXA2024102500961Angle · corrodedFS280 J-ANGLE BETWEEN LBL12 AND RBL12 IS CORRODED. LOCATED AND DRILLED NEW J-ANGLE P/N CC670-34065-1SB, AT FS280 BETWEEN LBL12 TO RBL12, IAW CRJ-900 SRM 51-40-11-001-001-A01.REMOVED AND REPLACED J-ANGLE P/N CC670-34065-1SB, AT FS280 BETWEEN LBL 12 TO RBL 12 SDR CALA2024102202702Web · crackedFLIGHT DECK FLOOR STRUCTURE WEB CRACKED FR 8-11 LBL20. FLIGHT DECK FLOOR STRUCTURE WEB REMOVED AND REPLACED PER A320 SR M 51-72-11-911-002.SDR DALA2024101810191Pan · crackedCRACK PAN INTERNAL SIDE FWD EDGE ON BEAM #4 AND #5 (2 EA) AT AFT CARGO DOOR. SUMMARY OF NRC 00129: INNER PAN ON FWD EDGE BETWEEN BEAM #4 AND #5 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620739-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 62073SDR AALA202410185971Plate · out of adjustAIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR GETS STUCK IN THE CLOSED POSITION. ADJUSTED FLOOR PLATE, OPERATION CHECKS NORMAL.SDR YENA2024101701367Floor Support · corrodedDURING HEAVY MAINTENANCE: PASS CABIN AFT ZONE AT BEAM Y765 AND FR 67-68 (4 POINTS) WITH CORROSION; REF. MEX WO. 1318489, 1327754, 1328846 S/N: 00416 - FLOOR BEAM REPLACED ON PASS. CABIN AFT ZONE Y765 FR 67-68 IAW A320 SRM 51-42-11 REV. 150 01-AUG-2024.SDR YENA2024101701366Door Sill · corrodedDURING HEAVY MAINTENANCE: PASS CABIN, AFT ZONE AT LH SIDE SILL BEAM AT FR 68 - 6 IN WITH CORROSION; REF. MEX. WO. 1318489, 1327754, 1328846 S.N: 00420 - SILL BEAM AT AFT PAX DOOR L2 WAS REPLACED I.A.W SRM 51-72-11-911-001, REV-150, 01 -AUG-2024.SDR YENA2024101701362Floor Support · corrodedDURING HEAVY MAINTENANCE: PASSENGER CABIN, AFT ZONE AT BEAM Y765 AND FRAMES 66-67 POINTS WITH CORROSION; REF. MEX. WO 1318489,1327754,1328846 N/R S/N: 00415 - : FLOOR BEAM WAS INSTALLED ON PASSENGER CABIN AFT ZONE Y765 FR 66-67 I.A.W A320 SRM 51-42-11 REV.150 SDR YENA2024101701350Floor Support · corrodedDURING HEAVY MAINTENANCE: FLOOR SUPPORT PANEL WITH CORROSION, AT FR 16, BTW Y+254 AND Y+765; REF MEXICANA WO # 1318489,1327754,1328846 NR # 00367: FLOOR SUPPORT PANEL AT FR 16 BETWEEN Y+254 AND Y+ 765 WAS REPLACED I.A.W. A320 SRM 51-42-11 PARAGRAPH 2F REV 150 SDR IXXA20241017006Guide Track · crackedALC L/H GUIDE RAIL CRACKED AND DAMAGED IN ALC STA 1265 LBL 44SDR IXXA20241017005Intercostal · corrodedFLC CORROSION FOUND ON UNDERSIDE OF STRUCTURE @ STA 610 RBL 42SDR IXXA20241017002Strap · corrodedFLC FLOOR CORROSION FOUND DOOR THRESHOLD UNDERSIDE OF LONGITUDINAL STRAP @ STA 604 RBL 44.SDR IXXA20241017001Stiffener · corrodedFLC CORROSION FOUND ON UNDERSIDE OF STIFFENER AT THE CARGO DOOR THRESHOLD @ STA 562 RBL 44.
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