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 AALA202411134054Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL AT STA 747, S26R. ACCOMPLISHED SPLICE REPAIR PER AARD 51-00-05-1 AND SRM 53-00-53-2R-5,.SDR DALA2024111210860Web · corroded(LOG 0655176) CORROSION ON WEB STA 987+3 LBL 37, WL 208. REMOVED AND REPLACED. FABRICATED WEB PER B737 SRM 51-40-02-0G, DWG# 147A5700 REV- AND ERA 618756-14TR REV ORIGINAL.SDR IPXA2024110908905Adapter · crackedFOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1109 BL 0.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 90. AND BOEING DWG NO. 457T4000 SH. 11 REV. BSDR CALA2024111102827Channel · crackedL/H O/W HATCH HAS CRACKS AT RIVETS AT L/H AND R/H LOAD TRANSMITT ING PROGILE. REMOVED & REPLACED L/H O/W HATCH L/H & R/H LOAD TRANSMITTING PRO FILE (FRAME SEGMENT) IAW A319 SRM 51-72-11-911-001. PN: D5227902 620551, PO: 1153067.1, PN: D5227902620451, PO: 115SDR DALA2024110810748Shield · corroded(LOG 0649194) CORROSION ON AFT CARGO COMPARTMENT DOOR FWD SHIELD BETWEEN STA-767 AND STA-787, RBL-22. REMOVED AND REPLACED SHIELD AT AFT CARGO COMPARTMENT DOOR FWD BTW STA 767- AND 787 RBL-22 IAW B737-900 SRM 51-10-02-0G AND DWG # 146A0081 REV A.SDR DALA2024110810731Web · corroded(LOG 0645996) CORROSION ON WEB STA 987+7 RBL 40, WL 208. REMOVED AND REPLACED FABRICATED WEB PER B737 SRM 51-40-02-0G, DWG# 147A5700 REV B AND ERA 618756-14.SDR DALA2024110810730Web · corroded(LOG 0645636) CORROSION ON WEB STA 987+3 LBL 37, WL 208. REMOVED AND REPLACED. FABRICATED WEB PER B737 SRM 51- 40-02-0G, DWG# 147A5700 REV- AND ERA 618756-14TR.SDR DALA2024110510662Sill Drain · corrodedAIRCRAFT 3739, ***CORROSION*** PASSENGER COMP. MOPSIL STA 947+4 RBL 51, WL 208. CORRECTIVE ACTION: EVALUATED DAMAGE ON MOPSILL STA 947 + 4 RBL 51 WL 208. FOUND TO BE WITHIN LIMITS, ORIGINAL MATERIAL THICKNESS IS .080" MATERIAL LOSS .003" REMAINING THICKNESS .0SDR DALA2024110510657Intercostal · gougedAIRCRAFT 3739, GOUGE DAMAGE ON INTERCOSTAL WEB LOCATED AT E/E BAY DOOR CUTOUT RBL 15.47 ABOVE E/E DOOR LATCH PIN FITTING STA 325.38+14.25" AND WL 158.12. CORRECTIVE ACTION: GOUGE DAMAGE ON INTERCOSTAL WEB AT E & E BAY DOOR CUTOUT STA. 325.38, RBL 15.47 MEASURESDR DALA2024110410632Web · corrodedAIRCRAFT 3734, INITIAL INSPECTION: CORROSION ON WEB UNDER SCUFF PLATE OF FWD CARGO ENTRY AT STA 466 APPROX. CORRECTIVE ACTION: CORROSION LEVEL 2. WEB UNDER SCUFF PLATE OF FWD CARGO ENTRY AT STA 466 APPROX WAS REPLACED PER B737-800 SRM 51-40-02-0G. PAR 5.B. (LPSDR AALA202411044903Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500F, S26R. REPLACED CLIP PER AARD 51-00-05-1.SDR AALA202411043010Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500G, S26R. REPLACED CLIP PERAARD 51-00-05-1.SDR HNAA2024121001179Gusset · corroded53-2126 LH GUSSET CORRODED BTW FR59-61. RAR GUSSET IAW SRM 51-40-02SDR IPXA2024112190358Floor Support · crackedFWD CARGO FR 38.2 CENTRE UNDER MAIN DECK, FOUND A CRACKED FLOOR SUPPORT BRACKET (P/N A2557066900000). MB-60-012. INSTALLED SUPPORT BRACKET IAW A300-600 SRM 51-40-21 MATERIAL USED P/N EN6115V3-10 B/N 0004211121 RIVET P/N NAS1097AD6-7 B/N 0004056192. REVIEWEDSDR AALA202411259892Web · brokenAIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT BROKEN CEILING WEB LOCATED BETWEEN STA 1706 AND STA 1727 RIGHT HAND SIDE. REPLACED WEB PER SRM-51-40-02 AND DWG 146W5806 SHEET 6.SDR HNAA2024112501126Gusset · corroded53-2124 CTR GUSSET CORRODED BTW FR59-61. RAR GUSSET IAW SRM 51-40-02SDR SWAA2024112155337Angle · corrodedDOT#17 A-043 AFT CARGO COMPARTMENT INTERCOSTAL CORRODED UNDER 'Z' ANGLE AT STA 747 TO 767 RBL 22 WL 156<[01] 01 - REMOVED AND REPLACED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[02] VERIFIED STEP 1<BR>AUDIT CWSDR REXA2024112101505Floor Support · corrodedINITIAL INSPECTION: CORROSION ON FLOOR SILL BTW FS280.00 AND 319.70 AT CABIN FLOOR STRUCTURE. FLOOR SILL BTW FS280.00 AND 319.70 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-45-201-001-A01 AND WAS REPLACED PER EA CRJ753-17650 REV A AND CRJ700S SRM 51-42-06SDR HNAA2024112001119Gusset · corroded53-2126 LH GUSSET CORRODED BTW FR59-61. RAR GUSSET IAW SRM 51-40-02SDR IPXA2024111587934Bracket · crackedAFT CARGO FR 54 L/H MIDDLE FLOOR SUPPORT BRACKET IS CRACKED. MB-60-009. INSTALLED MIDDLE SUPPORT BRACKET IN STR-Z100 AFT CARGO FR 54 L/H IAW A300-600 SRM 51-40-21, MATERIAL USED: RIVET SOLID UNIVERSAL HEAD P/N: MS20470AD6-8, BATCH: 0004201341.SDR IPXA2024111587760Floor Support · crackedFR 54, CENTRE FLOOR SUPPORT BRACKET IS CRACKED. MB-60-006. INSTALLED SUPPORT BRACKET ON FRAME 54 IAW A300-600 SRM 51-40-21 AND SRM 51-76- 00 MATERIAL USED RIVETS P/N MS2047OAD5-6 B/N 0004190014 AND SEALENT P/N 04-001-01-09.SDR IPXA2024111586721Bracket · crackedAFT CARGO FR 54, R/H O/B FLOOR SUPPORT BRACKT IS CRACKED. MB-60-008. INSTALLED FLOOR SUPPORT BRACKET IN STR-Z100 AFT CARGO FR 54 R/H O/B IAW A300-600 SRM 51-40-21, MATERIAL USED: RIVET SOLID UNIVERSAL HEAD P/N: MS20470AD6-8, BATCH: 0004201341.SDR R61A2024111800549Doubler · corrodedCFIII FR-84, RBL10 FOUND CORRODED FLOOR SUPPORT DOUBLER. CFIII FR-84, RBL10 CORRODED FLOOR SUPPORT DOUBLER REMOVED AND REPLACED IAW EMBRAER 175 SRM 51-43-04.SDR R61A2024111800548Support Angle · crackedCFIII FR-86, RBL25 FOUND ANGLE BRACKET CRACKED. ANGLE BRACKET AT CFIII FR-86, RBL25 REMOVED AND REPLACED /INSTALLED IAW SRM 51-41-01.SDR R61A2024111700544Angle · crackedCOCKPIT FLOOR SUPPORT STRUCTURE, ANGLE AT FRAME 12, BL0 FOUND CRACKED. ANGLE AT FRAME 12,BL0 HAS BEEN REPLACED ON COCKPIT FLOOR SUPPORT STRUCTURE IAW SRM 51-42-02.SDR R61A2024111700542Shear Web · corrodedCFIII, SHEAR WEB SPLICE BETWEEN FR87-FR88, RBL 42 FOUND CORRODED. CFIII, SHEAR WEB SPLICE BETWEEN FR87-FR88, RBL42 HAS BEEN REPLACED IAW SRM 51-42-02.SDR R61A2024111700540Shear Panel · corrodedCFIII, SHEAR PANEL BETWEEN FR87-FR88, RBL12-RBL46 FOUND CORRODED. CFIII SHEAR PANEL BETWEEN FR87-FR88, RBL12-RBL46 HAS BEEN REPLACED IAW SRM 51-42-01.SDR IPXA2024111387810Floor Support · crackedFR 54 R/H MIDDLE FLOOR SUPPORT BRACKET IS CRACKED. MB-60-007. INSTALLED FR-54 R/H MIDDLE FLOOR SUPPORT BRAKET IAW SRM 51-40-21 AND 51-76-00, RIVET P/N: MS20470AD5-6 B/N:0004190014 AND SEALANT P/N: 04-001-0109 B/N: 0004318416.SDR ASAA2024103153731Baffle · crackedFWD CARGO FOUND BAFFLE CRACKED AT LH 500 TO 500A. GROUNDED - YES. REMOVED AND REPLACED BAFFLE AT L/H 500 TO 500A IAW B737-900ER SRM 51-40-02-0G-0.SDR REXA2024111201468Web · corrodedCORROSION ON LH LOWER WEB AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND CORROSION ON LH LOWER WEB, AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01, WAS FABRICATED PER CRJ700 SRM 53-11-10-201-004-A01 AND WASSDR REXA2024111101444Web · corrodedCORROSION ON RH LOWER WEB AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND CORROSION ON RH LOWER WEB, AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND OUT OF LIMITS PER CRJ700 SRM 53-11-10-201-003-A01, WAS FABRICATED PER CRJ700 SRM 53-11-10-201-004-A01 AND WASSDR DALA2024110810750Floor Support · corroded(LOG 0649183) CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT STA- 763+3 FROM RBL-21 TO LBL-21. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT STA - 763 + 3 FROM RBL - 21 TO LBL 21 PER B737 SRM 51-40-02-0G.SDR SWAA2024110555406Tape · missingFWD CARGO COMPARTMENT AFT BULKHEAD UPPER CHORD WITH MISSING CARGO TAPE. 2024-597257<[01] INSTALLED ON FWD CARGO COMPARTMENT AFT BULKHEAD UPPER CHORD IAW AMM 25-52-09-400-801 STEP 3.D.(10).;[02] INSTALLED TAPE ON FWD CARGO COMPARTMENT AFT BULKHEAD UPPER CHORD ISDR DALA2024110510663Intercostal · gougedAIRCRAFT 3739, GOUGE DAMAGE ON INTERCOSTAL WEB LOCATED AT E/E BAY DOOR CUTOUT LBL 6.74 ABOVE E/E DOOR LATCH PIN FITTING STA 325.8+13.2" AND WL 158.1. CORRECTIVE ACTION: GOUGE DAMAGE ON E & E BAY DOOR CUTOUT INTERCOSTAL WEB MEASURES L = 3.00" X W = 0.90" X D = SDR AALA202411041986Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500H, LBL 26. REPLACED CLIP PER AARD 53-00-01-6.SDR AALA202411041648Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500G, LBL 26. REPLACED CLIP PER AARD 53-00-01-6.SDR DALA2024110110575Web · damagedSHIP 3160 ELONGATED HOLE ON WEB INTERNAL STRUCTURE LOCATED BETWEEN FR56 TO FR57 AND STR38L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED WEB INTERNAL STRUCTURE LOCATED BETWEEN FR56 TO FR57 AND STR38L IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11. (SDR DALA2024110110568Pan · crackedCRACK ON INNER PAN FWD/AFT UPPER CORNER AT FWD CARGO COMPRTMENT. SUMMARY OF NRC 00112: INNER PAN FWD/AFT UPPER CORNER AT FWD CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0638113)SDR DALA2024110110567Web · crackedCRACK ON WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00380: WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. FIGURE 217. -PERFORM DECAL INSPECTION CONDITION EVERY "C" CSDR SWAA2024121055034Support · crackedCRACKED FLOOR SUPPORT AT BS 323 RBL 35 WL 208<[01] REMOVED FLOOR SUPPORT AT BS 320 - BS 340 RBL 35 WL 208 PER SRM 51-40-02-0G-0 AND LOCATED AND DRILLED NEW FLOOR SUPPORT FOR BS 320 - BS 340 RBL 35 WL 208 PER DWG: 141A5400 ID: 0039 REV: - AND SRM 51-40-05-0G-0 SDR SWAA2024121055036Support · crackedCRACKED FLOOR SUPPORT AT BS 353 RBL 3 WL 208<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 53-00-04-1A-1 IS APPLICABLE TO THIS AIRCRAFT. PART FOUND TO BE OUT OF LIMITS PER SRM 53-00-04-1A-1. NO REPAIR REFERENCE FOR CRACK PART WILL BE REPLACED. REMOVED FLOOR SUPPOSDR SWAA2024121055039Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 353 RBL 15 WL 208<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 53-00-04-1A-1 IS APPLICABLE TO THIS AIRCRAFT. PART FOUND TO BE OUT OF LIMITS PER SRM 53-00-04-1A-1. NO REPAIR REFERENCE FOR CRACK PART WILL BE REPLACED. COMPLETE MEASUREMESDR SWAA2024121055021Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 393 RBL 3 WL 208 CRACKED FLOOR SUPPORT BETWEEN BS 380-400 BL 0 WL 208.<[01] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 393 RBL 3 WL 208 IAW SRM 53-00-04-1A-1; SRM 51-40-05; BOEING DWG# 143A5400 REV:-; SRM 51-40-02;[02] VERIFISDR SWAA2024121055041Support · crackedCRACKED FLOOR SUPPORT AT BS 393 RBL 8.283 WL 208 CRACKED FLOOR SUPPORT BETWEEN BS 380-400 RBL 8.283 WL 208<[01] STEP 3 RBL DOES NOT MATCH THE SIGNOFFS AND THERE IS NO OVERALL CORRECTIVE ACTION.;[02] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 393 RBL 13 SDR SWAA2024121055044Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 393 LBL 16 WL 208 CRACKED FLOOR SUPPORT BETWEEN BS 380-400 LBL13.24 WL 208.<[01] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 393 LBL 16 WL 208 IAW 51-40-05; BOEING DWG# 143A5400 REV:-; SRM 51-40-02; SRM 53-00-04-1A-1;[02] VERISDR SWAA2024121055046Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 391 LBL 52 WL 208<[01] REMOVED FLOOR SUPPORT AT BS 380 - BS 400 LBL 52 WL 208 PER SRM 51-40-02-0G-0 AND LOCATED AND DRILLED NEW FLOOR SUPPORT FOR BS 380 - BS 400 LBL 52 WL 208 PER DWG: 143A5400 ID: 0141 REV: - AND SRM 51-40-05-0G-0 SDR SWAA2024121055048Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 391 RBL 42 WL 208<[01] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 391 RBL 42 WL 208 IAW SRM 51-40-02; SRM 51-40-05; BOEING DWG#143A5400 REV:-;[02] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 391 RBL 42 WL 208 IAW SRM 51SDR HNAA2024120901174Support Bracket · cracked53-2084 CARGO ENTRY, FR67 LWR POST UPPER SUPPORT BRACKET CRACKED. RAR SUPPORT BRACKET IAW SRM 51-40-02SDR HNAA2024120901173Support Bracket · cracked53-2083 CARGO ENTRY, FR67 LWR POST SUPPORT BRACKET CRACKED. RAR SUPPORT BRACKET IAW SRM 51-40-02SDR HNAA2024120901171Support Bracket · cracked53-2081 CARGO ENTRY, FR66 LWR POST SUPPORT BRACKET CRACKED. RAR SUPPORT BRACKET IAW SRM 51-40-02
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