JASC 5320
Service difficulty reports · 216,095
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 ASAA2025051058854Support Angle · corrodedAFT CARGO L/H TRANSITION F.S. 727D+10 -847 CORRODED. GROUNDED - YES. REMOVED AND RELACED LH TRANSITION SUPPORT ZEE LH ON AFT CARGO AT FS 727D+10- FS847 IAW B737-700, SRM 51-40-02, REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW BOEIGN 737-700 SRM 53-00-53-1A-2SDR ASAA2025051058404Shield · corrodedAFT CARGO R/H FWD SHEILD HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ON AFT CARGO R/H FWD SHIELD AND WAS FOUND OUT OF LIMITS IAW B737-700 SRM 53-60-15-1A-1, REMVOED AND REPLACED SHIELD IAW B737-700 SRM 51-40-02-0G-0W =1" O= .050 R= .043 L= 1" D= .007.SDR IPXA2025060310145Angle · crackedCRACK-ANGLE, AFT CARGO COMPARTMENT FORWARD WALL R/H SUPPORT BELOW FLOOR AREA, STA 1087, S-35R.REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.92.INSTALLED NEW CLIP I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO. 140T0130 SHEET 10 REV: GSDR SWAA2025060269521Scuff Plate · crackedR1 DOOR SCUFF PLATE CRACKED FWD AREA<[01] REMOVED SCUFFPLATE IAW B737-700 SRM 51-40-02. CLEANED BARE SURFACES AT CRACKED AREA OF SCUFF PLATE PER B737-700 SRM 53-10-15-2R-2 REPAIR 2. WELDED CRACKED AREA OF SCUFF PLATE USING TITANIUM ERTI-5 6AL4V FILLER MATERIALSDR REXA2025052900620Support · crackedCRACK ON FWD SUPPORTS (2EAS) OF INBOARD BRAKE ACCUMULATOR WAS FOUND FWD SUPPORT OF INBOARD BRAKE ACCUMULATOR WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01SDR ASAA2025051058058Web · corrodedIN FWD PIT, CARGO DOOR LOWER THRESHOLD SUBPANEL HAS SEVERAL AREAS OF CORROSION, MARKED IN RED. GROUNDED - YES. REMOVED CORROSION ON FWD CARGO DOOR LOWER SILL WEB. ORIGINAL THICKNESS IS .045", MATERIAL REMOVED IS .002", REMAINING THICKNESS IS .043", FOUND TO BESDR ASAA2025051058057Floor Support · corrodedIN FWD CARGO PIT, FIXED SUB-FLOOR SUPPORT HAS CORROSION IN AND AROUND BOLT HOLE, AT STA 500H LBL 24. MARKED IN RED. GROUNDED - YES. REMOVED CORROSION, ORIGNAL THICKNESS .040, MATERIAL REMOVED 0.001, REMAINING MATERIAL .039 FOUND TO BE WITHIN LIMITS IAW B737-90SDR CALA2025051604724Shear Plate · corrodedMAIN CABIN AFT WET AREA FR69-70 LH SHEAR PLATE HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED LH FR 69-70 SHEAR PLATE IAW A320 SRM 51-42- 11/001.SDR IPXA2025051510145Angle · crackedCRACK-ANGLE, AFT CARGO COMPARTMENT FORWARD WALL R/H SUPPORT BELOW FLOOR AREA, STA 1087, S-35R. (REPLACE) 1. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.92 2. INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO. 140T0130 SHEET 10 REV: G 3. JOB COMSDR DALA2025051403744Support · corrodedPRODUCTION REQUEST: RH SIDE WTBF SUPPORT AT FR48 HAS CORROSION. REMOVED CORROSION ON FR48 R/H WTBF SUPPORT FRAME IAW A220 ASRP J51-21-06. REMOVED AND REPLACE SUPPORT FRAME IAW A220 ASRP J51- 42-20. (LP# 0959651)SDR DALA2025051203671Angle · corrodedCORROSION ON CHORD ANGLE FROM STA 360 TO STA 291 BTW RBL 57 AT (FLOOR STRUCTURE) W1. CHORD ANGLE BTW STA 360 TO STA 251, RBL 57 AT (FLOOR STRUCTURE) W1 WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR 4. AND 51-40-02-0G PAR 7.D.SDR DALA2025051203669Angle · corroded(LOG 0958988) CORROSION SUPPORT ZEE LOCATED BTW STA 727 TO STA 767 AND STR 25R AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW STA 727 TO STA 767 AND STR 25R AFT CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02-0G, DWG 146A7502.SDR SWI2025F01231Intercostal · corrodedCORROSION NOTED ON PAX DOOR MID DD3 INTERCOSTAL AND UPPER FLANGE (MARKED) (C-CHECK RO 09/07/2025) INSTALLED NEW PAX DOOR INTERCOSTAL DD3 FS320.00 - FS338.00 . REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV NSDR 9WGA2025081854625Angle · crackedDURING HEAVY MAINTENANCE ANGLE BELOW FWD RH PATIO FLOOR HAS A CRACK. FABRICATED AND INSTALLED ANGLE STIFFENER AT PATIO FLOOR BELOW RH FWD IAW MD-11 SRM 51-31-10 AND DRAWING AKC7546. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AALA202507251007Fitting · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT S32R. REPLACED RIGHT HAND LATERAL FITTING FOR END PER EA 364841.SDR AALA202507228325Fitting · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT S32L. REPLACED LEFT HAND LATERAL FITTING PER EA 364841.SDR SWI2025F00891Floor Support · corrodedLH PRESSURE FLOOR SILL PANEL HAS SEVERAL SPOTS OF CORROSION FS409+128 €“ 559 (C-CHECK RO 07/11/2025)REMOVED CORROSION ON LH SIDE PRESSURE FLOOR SILL NUMBERED #1 BETWEEN FS424- FS439 AT FASTENER HOLE REF CRJ-200 SRM 51-21-06. REPAIRED IAW REO 601R-53-41-666 SDR SWI2025F00890Floor Support · corrodedRH PRESSURE FLOOR SILL PANEL IS CORRODED AT APPROX FS449 AND APPROX FS517 (C-CHECK RO 07/11/2025)BLENDED OUT CORROSION AND RESTORED FINISH ON RH PRESSURE FLOOR PANEL AT MARKED LOCATIONS. FOUND WITHIN LIMITS. REF. REO 601R-53-41-666 REV-C ISSUED 2012-11-06.COMSDR HNAA2025061600451Bracket · crackedF045768 LH LATERAL BRACKET IS CRACKED IN COCKPIT. REMOVED CRACKED LH LATERAL BRACKET IN COCKPIT AND INSTALLED L/H LATERAL BRACKET IN COCKPIT IAW EMB 145 SRM 51-40-02.SDR SWAA2025061169183Support Angle · corrodedCORROSION ON SUPPORT ANGLE LOCATED BS 947.5 BTW STR 26L TO STR 26R WL 156.1 AT AFT CARGO COMPARTMENT 2025-309348<[01] REPLACED SUPPORT ANGLE LOCATED BS 947.5 BTW STR 26L TO STR 26R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 51-40-02-0G-0 AND DWG# 149A8117 SDR SWAA2025061169193Support · corrodedCORROSION ON SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 RBL 22 WL 156.1 AT CARGO COMPARTMENT 2025-309359<[01] TOOL USED ON STEP 3: ULTRASONIC THICKNESS GAUGE P/N 45MG; S/N 130066701 DUE DATE JUL-12-2025;[02] REPLACED SUPPORT ZEE; REPAIR SPLICE 1(EA) AND FASTENESDR SWAA2025061069195Support · corrodedCORROSION ON SUPPORT ZEE LOCATED BTW BS 727C TO BS 727E RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-309360<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 AND RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT BECAUSE THE CORROSION EXCEEDS THE LIMITS IAW B7SDR SWAA2025061069194Support · corrodedCORROSION ON SUPPORT ZEE LOCATED BTW BS 727A TO BS 727C RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-309362<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 AND RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT BECAUSE THE CORROSION EXCEEDS THE LIMITS IAW B7SDR HNAA2025061000416Floor Support · cracked53-2150 LH OMEGA BEAM IB FLANGE CRACKED AT FR35. REPAIRED IAW ETD2025-145-921567 AND EO1-53-25-0188SDR HNAA2025061000415Floor Support · cracked53-2149 LH OMEGA BEAM IB FLANGE CRACKED AT FR31. REPAIRED IAW ETD2025-145-921567SDR SWAA2025060969317Angle · crackedCRACK ON ANGLE - CLIP LOCATED BS500B AND LBL21 FWD CARGO COMPARTMENT 2025-310010<[01] REPLACED CLIP LOCATED BS 500B AND LBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 143A7505 SHEET 118 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACSDR SWAA2025060969320Angle · crackedCRACK ON ANGLE - CLIP LOCATED BS500C AND LBL21 FWD POSITION FWD CARGO COMPARTMENT 2025-310011<[01] REPLACED CLIP LOCATED BS 500C AND LBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 143A7505 SHEET 117 AND REV -. SEE INDIVIDUAL SIGN OFF BELOWSDR SWAA2025060969179Angle · crackedCRACK ANGLE LOCATED BS 695 LBL1 AT CENTER WING BOX 2025-309996<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 29 JAN 26; TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE 28 JAN 26.;[02] REPLACED ANGLE AND FASTESDR SWAA2025060969383Angle · crackedCRACK BILGE AREA ANGLE ON BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2025-298069<[01] REPLACED ANGLE BILGE AREA BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A7902 SHET 126 REV A. SEE INDIVIDUAL SIGNOFF BESDR HNAA2025060600394Floor Support · cracked53-2151 LH OMEGA BEAM IB FLANGE CRACKED AT FR24. REPAIRED IAW ETD2025-145-921486 AND EO1-53-25-0186SDR HNAA2025060600393Floor Support · cracked53-2144 LH OMEGA BEAM CRACKED ON IB FLANGE AT FR26. REPAIRED IAW ETD2025-145-921486 AND EO1-53-25-0186SDR SWAA2025060269360Support Bracket · crackedCRACKED ON CHORD BS695; RBL2; BELOW UPPER DECK<[01] REPAIRED PER EA 25-153-01245-WIP1;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR HNAA2025052800368Support · cracked53-2140 RH SILL CORRODED BTW FR23-29. RAR SILL IAW SRM 51-40-02SDR AALA202505238934Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 948, LBL 48. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR EVCA202250515001Stiffener · crackedSTATION 145 CLIP IS CRACKED IN MULTIPLE RIVET HOLES ON THE LH SIDE.SDR DALA2025051203665Baffle · damaged(LOG 0957880) SECONDARY FINDING EXISTING HOLES IN BAFFLE WEB LOCATED BETWEEN BS500F TO BS500G AT LEVEL STR 26L NOT MEET REQUIREMENTS OF SUPPORT ZEE REPAIR ASPER SRM B737-800 53-00-53-2R REPAIR 6 BAFFLE MUST BE REPLACED. REPLACED BAFFLE WEB LOCATED BETWEEN BS50SDR IXXA2025050900001Intercostal · corrodedFOUND CORROSION IN THE HOLES WHERE THE STUDS WERE REMOVED AND ALSO DEEP PITTING IN THE INTERCOSTAL, LOCATED IN THE RWW, STA.1120 TO STA.1140, 26 INCHES ABOVE THE BOTTOM OF THE KEEL BEAM.RRSDR VNAA202505090007Angle · damagedFS 280 CROSSBEAM AND AFT J-ANGLE ARE CORRODED ALONG THE UPPER EDGE. CORRECTIVE ACTION: CORROSION FOUND ON MULTIPLE CROSS SECTIONS. REPLACE J-ANGLE WITH NEW. LOCATED AND DRILLED NEW "J" ANGLE CC670-34095-1 IAW CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED NEW J-ASDR VNAA202505090003Angle · corrodedUPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: FABRICATED, LOCATED AND DRILLED NEW RH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6 .040" IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-24-36-001-001-A01. MATERIAL ID REF. CRJ SDR VNAA202505090002Angle · corrodedUPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: FABRICATED, LOCATED AND DRILLED NEW RH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6 .040" IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-24-36-001-001-A01. MATERIAL ID REF. CRJ SDR VNAA202505090001Web · corrodedUPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: LOCATED AND DRILLED NEW R/H CROSSBEAM PN# CC670-34094-2 IAW CRJ 700 SRM 51-40-11-001-001-A01. R/H LOWER WEB, R/H BUTTSTRAP & R/H CROSSBEAM INSTALLED PER SERVICE BULLETIN 67SDR REXA2025050900574Floor Support · corrodedFLOOR SUPPORT AT PAX DOOR FS310-FS333 HAS CORROSION. REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR MID CAP ANGLE PN# SH670-31825-9S IAW CRJ 51-41-02-001-001-A01 AND 51-41-04-001-001-A01.SDR VNAA202509030007Floor Support · corrodedLBL 27 FLOOR BEAM BETWEEN FS 1015 AND F.S 1047 HAS CORROSION ON UPPER SURFACE. CORRECTIVE ACTION: COMPLIED WITH REPAIR OF LBL 27 FLOOR BEAM CORROSION REPAIR BETWEEN FS 1015 AND F.S 1047 IAW CRJ-900 SRM 53-00-41-201-001-A03.SDR VNAA202509030002Stiffener · bentAT FS 280,00 LBL 9.0 WL 97.80 STIFFENER CC670-34138-1 IS BENT AT COCKPIT DOOR ENTRANCE. CORRECTIVE ACTION: . REMOVED AND REPLACED STIFFENER ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.SDR AALA202605236527Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND DOOR STOP 7. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.SDR SWI2025F01232Floor Support · corrodedCORROSION NOTED AT R/H PRESSURE FLOOR SILL ANGLE AT APPROX. FS712.00 - FS769.00 (MARKED) (C-CHECK RO 09/07/2025)REMOVED CORROSION FROM RH PRESSURE FLOOR SILL ANGLE. REPAIRED PER REO 690-53-41-536 REV -- DATE 2025-05-19 . SEE CONTINUATION CARD FOR DETAILS. COMSDR SWIA2025090900508Floor Support · corrodedCORROSION NOTED AT L/H PRESSURE FLOOR SILL ANGLE AT APPROX. FS712.00 - FS769.00 (MARKED) (C-CHECK RO 09/07/2025)REMOVED CORROSION FROM LH PRESSURE FLOOR SILL ANGLE. REPAIRED PER REO 690-53-41-536 REV -- DATE 2025-05-19 . SEE CONTINUATION CARD FOR DETAILS. COSDR AALA202508015847Fitting · wornAIRCRAFT IN BASE MAINTENANCE: WEAR ON UPPER FITTING LOCATED AT LEVEL FR20 WHEEL WELL STRUCTURE IN LATERAL AVIONIC COMP LH L= 0.576 IN. MAINTENANCE REPLACED FITTING LOCATED FR20 LH AT LEVEL OF Y520 WHEEL WELL STRUCTURE IN LATERAL AVIONIC COMPARTMENT LH IAW A319SDR SWI2025F00893Floor Support · corrodedLBL9 FLOOR BEAM IS CORRODED FS616 €“ 589 (C-CHECK RO 07/11/2025)REPAIRED DAMAGE ON LBL9 FLOOR BEAM FROM FS616-589 REF REO 601R-53-61-8337 REV -- DATED 2025-06-15. COMPLIED WITH ALL STEPS OF REO 601R-53-61-8337 REV -- DATED 2025-06-15. COMPLIED WITH TASK CARDSDR JJBA20250711023Floor Support · corrodedRH OB FLOORSILL IS CORRODED FROM FRAME 36 TO 41. REMOVED CORROSION RH OB FLOORSILL FROM FRAME 36 TO 41. REMOVED AND REPLACED PART.
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