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 SWAA2025081494258Sidewall Support · corrodedCORROSION ON ACB RH FLOOR TO SIDEWALL SUPPORT, RBL 21, BS 727A TO 767. REMOVED AND REPLACED ACB RH FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 146A7500.SDR SWAA2025081494259Sidewall Support · corrodedCORROSION ON ACB LH FLOOR TO SIDEWALL SUPPORT, LBL 21, BS 727A TO 847. REMOVED AND REPLACED ACB LT FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 146A7500.SDR SWAA2025081494268Sidewall Support · corrodedMULTIPLE SPOTS WITH CORROSION ON FCB SIDEWALL TO FLOOR SUPPORT NUTPLATE HOLES AT BS 460+2 TO 500B+2, LBL 22, WL156. REMOVED AND REPLACED FCB AT FLOOR SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 143A7500, REV-.SDR SWAA2025081494806Shield · corrodedCORROSION ON FCB AFT SHIELD FROM BS492 TO 500+7, RBL 22, WL156. REMOVED AND REPLACED FCB AFT SHIELD IAW SRM 51-40-02, AND DWG 143A0080, REV-.SDR SWAA2025081494262Angle · crackedCRACK ON ANGLE ACB STA-867 LBL-13'' FLOOR AREA. REMOVED AND REPLACED ANGLE ACB STA 867 LBL 13<BR>IAW SRM 51-40-02-0G-0; IAW SRM 51-40-05 AND DWG#149A8102 REV:-.SDR SWAA2025081494263Support Fitting · crackedCRACK ON ACB WATER TANK SUPPORT FITTING STA-947 LBL-10''. REMOVED AND REPLACED SUPPORT FITTING STA-947 LBL-10 IAW SRM 51-40-02 AND DWG 149A8103 ID:0007 REV: A.SDR SWAA2025081494260Web · corrodedCORROSION ON SUB THRESHOLD WEB ACB BS 787 TO 847 RBL-33. REMOVED AND REPLACED ACB SUBTHRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340 ID:0012 REV: C.SDR SWAA2025081494266Web · corrodedMULTIPLE SPOTS WITH CORROSION ON FCB DOOR CUTOUT SURROUND THRESHOLD BS440+14; BS460;460+9 RBL30;WL156. REMOVED AND REPLACED SUBTHRESHOLD WEB AT FCB; BETWEEN BS 440 TO BS 492 RBL 30 WL 156 IAW SRM 51-40-02 AND DWG 143A8330 REV -.SDR IPXA2025080766917Support Angle · corrodedEVIDENCE CORROSION PANEL 192 DR UPPER SUPPORT R/H SIDE. CLEANED AREA AT PANEL 192 DR UPPER SUPPORT R/H SIDE IAW SOPM 20-30-03.TREATED AND PRIMED AREA IAW SRM 51-20-01.APPLIED TOP COAT AT AREA IAW AMM 51-21-15-370-801.SDR ASAA2025072259891Angle · corrodedAFT CARGO R/H TRANSITION CORRODED BETWEEN STA 727D TO STA 847. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REPAIRED TRANSITION IAW BOEING 737-800 SRM 53-00-53-2R-6W 1" O .040 R .000 L 2" D .040.SDR ASAA2025072259863Transition Panel · corrodedFORWARD CARGO COMPARTEMENT R/H SIDE TRANSITION PANEL HAS NUMEROUS AREAS OF CORROSION BETWEEN STA 500C & 500I. GROUNDED - YES. REMOVED CORR. FROM FWD CARGO COMP. RT TRANSITION PANEL AT BS 500C TO 500I ORIG. THICKNESS .040 IAW SRM 53-30-53. MAT. LOSSED .008, RSDR ASAA2025072259805Transition Panel · corrodedAFT CARGO L/H TRANSITION CORRODED BETWEEN STA 727D TO STA 887. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REPAIRED TRANSITION IAW BOEING 737-800 SRM 53-00-53-2R-6W 2" O .040 R .000 L 1" D .040.SDR JJBA20250728098Angle · crackedAT FR 59 LH ANGLE BTW FR 59 AND OMEGA BEAM FOUND CRACKED. AT FR59 LH ANGLE BTW FR 59 AND OMEGA BEAM REMOVED. AT FR59 LH ANGLE BTW FR 59 AND OMEGA BEAM REPLACEDSDR DALA2025072405563Transition Panel · corroded(LOG 1099307) FWD CARGO RH TRANSITION PANEL BS 500C+10 - 500I. CORRODED MULTIPLE AREAS. REMOVED AND REPLACED FWD CARGO TRANSITION PANEL R/H SIDE BS 500C +10''-500I IAW B 737 SRM 51-40-02.SDR DALA2025072305545Web · corrodedSHIP 3155, CORROSION SHEAR PLATE STR 23 L LOCATED BETWEEN FR 69 TO FR 70 AT AFT GALLEY AREA. REPLACED WEB (SHEAR PLATE) AND FASTENERS LOC ON FR 69 TO FR 0 AT LEVEL STR 23L AFT GALLEY AREA IAW SRM 51-42-11 SRM 51-72-11.SDR DALA2025072305544Floor Support · corrodedSHIP 3155, CORROSION FLOOR SUPPORT +Y765 AT FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT Y765 LOC FR 66 TO FR 70 AT AFT GALLEY AREA AS PER SRM 51-72-11 AND SRM 51-42-11.SDR DALA2025072305543Floor Support · corrodedSHIP 3155, CORROSION FLOOR SUPPORT -Y464.8 AND FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPROT -Y464.8 LOC. BTW FR 68 TO FR 70 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11.SDR JJBA20251024083Floor Support · corrodedRH FLOOR SILL BETWEEN FR 22 AND 23 CORRODED AROUND FWD NUTPLATE. REMOVED AND REPLACED RH FLOORSILL BETWEEN FR 22 AND 23.SDR VNAA20251015014Support · corrodedCORROSION ON SILL BETWEEN FS1000 / FS1088 AND STGR17R. CORROSION ON SILL BETWEEN FS1000 / FS1031 AND FS1051 / FS1088 STGR17R WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-45-201-001-A01. AND SILL BETWEEN SDR IPXA2025081434048Floor Support · crackedMAJOR REPAIR, MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 74 AND 75, Y2127.5 HAS A CRACK ON Z CHANNEL. VERIFIED ACCOMPLISHMENT OF PERMANENT REPAIR IAW EA 300-5318-27-A4081, REV. -.SDR AALA202509107240Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL AT LEVEL STR23L BTW FR66 AND FR68 AT AFT GALLEY AREA MEASURES OF CORROSION ARE L=0.939 IN, W=0.589 IN,D=0.040 IN. MAINTENANCE REPLACED LOWER SILL LH SIDE BTW FR66 TO FR68 AND STR 23L AFT GALLEY AREA IAW A319SDR AALA202509101294Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR SUPPORT +Y1292 BTW FR65 AND FR66 AT AFT GALLEY AREA L=0.887 INCH, W=0.380 INCH, D=0.020 INCH. MAINTENANCE REPLACE FLOOR SUPPORT Y1292 LOC. BTW FR64 AND FR66 AT AFT GALLEY IAW SRM 51-42-11-801, SRM 51-72-11-911-001SDR SIMA20250721005Intercostal · corrodedSSI 53-23-003 STIFFENER SUPPORT IS CORRODED BETWEEN FR86-87 AND STR27R-28R. (LEVEL 2 CORROSION) REMOVED AND REPLACED STIFFENER SUPPORT BTW FR 86-87 AND STGR 27R-28R IAW ERJ 170 SRM 51-40-08.SDR SWAA2025082193713Intercostal · elongatedELONGATED HOLE ON WEB INTERCOSTAL LOCATED BTW BS 747 TO BS 767 AT LEVEL OF STR 25R AND WL 156.4. REPLACED WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, DWG 146A7500, SHEET 88, REV A, DWG 146A7502, SHEET 26, REV-.SDR IPXA2025081544048Floor Support · crackedMAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 74 AND 75, Y2127.5 HAS A CRACK ON Z CHANNEL VERIFIED STEP # 16 OF EA # 300-5318-27-A4081 OF PRELIMINARY 2 WERE RIISDR IPXA2025080234385Strap · corrodedAPU INLET DOOR FWD STRAP AT STA 1787.45 FROM STR 3R TO STR 6R HAS EXFOLIATION. INSTALLED NEW FWD STRAP IAW SRM 51-40-02-0G-0.SDR ASAA2025072160015Angle · corrodedAPU COMPARTMENT STRUCTURE L/H ANGLE 148A8615 BETWEEN STA 1088 AND STA 1104 HAS CORROSION. GROUNDED - YES. REMOVED CORROISON, FOUND TO BE OUT OF LIMITS, REMVOED AND REPLACED L/H ANGLE IAW B737-800 SRM 51-40-02-0G-0W= 1.25 O= .063 R= .043 L= 4" D= .020.SDR IPXA2025080234761Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1826 AT STR 3R HAS CORROSION. INSTALLED NEW UPPER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.SDR IPXA2025080234656Angle · corrodedAPU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1826 AT STR 6R HAS EXFOLIATION CORROSION. INSTALLED 1EA LOWER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.SDR JJBA20250811029Floor Support · crackedCF3 LH OMEGA AT FR 36 FLANGE IB CRACKED. CF3 LH OMEGA BEAM FR 36 CUTOUT PERFORMED. CF2 LH OMEGA BEAM FR 36 DOUBLER AND FILLER FABRICATED. CF3 LH OMEGA BEAM FR 36 DOUBLER REPAIR INSTALLEDSDR JJBA20250808022Floor Support · crackedLH OMEGA BEAM FR27 FLANGE IB CRACKED. REPAIR DOUBLER ON CFII LH OMEGA BEAM ON INBD VERTICAL FLANGE AT FR 27SDR IPXA2025080337337Tee Angle · corrodedEVIDENCE OF CORROSION ON T-CHORD UPPER R/H SECTION STA 1200. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.063''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.5, W:1.4, DEPTH: 0.018'', REMAINING MAT.: 0.045'', %DAMAGE:28.6%. REMOVED UPPER RSDR IPXA2025080700384Stiffener · corrodedEVIDENCE OF CORROSION ON CHANNEL UPPER L/H STA 1120. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.050''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.1, W:1.2, DEPTH: 0.007'', REMAINING MAT.: 0.043'', %DAMAGE:14%. REMOVED STIFFENER STA 1220SDR IPXA2025080237575Tee Angle · corrodedEVIDENCE OF CORROSION ON T-CHORD NEAR TO RAM AIR R/H STA 1220 RBL50. .REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.071''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.2, W:1.1, DEPTH: 0.020'', REMAINING MAT.: 0.051'', %DAMAGE:28.1%. LOCATEDSDR IPXA2025080737989Tee Angle · corrodedEVIDENCE OF CORROSION ON T-CHORD L/H STA 1180 TO 1240 LBL50.DOT 5846-12. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.080''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:1.9, W:1.4, DEPTH: 0.006'', REMAINING MAT.: 0.074'', %DAMAGE:7.5%. TREATSDR IPXA2025080738248Tee Angle · corrodedEVIDENCE OF CORROSION ON T-CHORD NEAR TO RAM AIR LT STA 1220 LBL50. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.071''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.1, W:1.4, DEPTH: 0.031'', REMAINING MAT.: 0.040'' PERCENT, DAMAGE:43.7 PERCESDR IPXA2025080239097Support Angle · corrodedAPU INLET DOOR UPPER CORNER ANGLE AT STA 1787.45 S3R HAS CORROSION. REMOVED UPPER CORNER ANGLE WITH CORROSION IAW B757-200 SRM 51-40-02-0G.REMOVED AND REPLACED ONE S3R CORNER SUPPORT ANGLE (P/N: 148N3141-6) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRSDR IPXA2025080239271Angle · corrodedAPU INLET DOOR LOWER CORNER ANGLE AT BS 1787.45 STR 6R HAS CORROSION.REMOVED LOWER CORNER ANGLE WITH CORROSION IAW B757-200 SRM 51-40-02-0G.REMOVED AND REPLACED 1 EACH S-6R CORNER SUPPORT ANGLE (P/N: 148N3141-5) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PSDR REXA2025080600787Channel · corrodedSECUNDARY NRC IN REFERENCE WITH NRC 00160: AFTER SUPPORT DIAPHRAGM REMOVAL, CORROSION AND ELONGATED HOLES WAS FOUND ON ATTACHMENT AREA. SUPPORT OF DIAPHRAGM WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-2SDR AALA202507285527Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD FROM BS 767 TO BS 787 AT RBL 25. REPLACED SHIELD PER AARD 51-00-05-1.SDR DALA2025072505606Floor Support · corroded(LOG 1097320) CORROSION AROUND FASTENER HOLES IN FWD CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT INTERCOSTAL, BS.500F-BS.500G STR.26R. REMOVED AND REPLACED INTERCOSTAL IN FWD CARGO COMPT BS .500F BS500G STR 26R IAW B 737 SRM 53-30-53-2R1 AND IAW B 737 SRM 51-40-SDR JJBA20250723089Partition · corrodedRIGHT FR 61 FRAME PARTITION FOUND CORRODED AT FLOOR LEVEL. RT FR 61 FRAME PARTITION BLENDED, FOUND OUT OF LIMIT. RT FR 61 FRAME PARTITION REMOVED AND REPLACED.SDR 2025FA0000509Frame · crackedA CRACK WAS FOUND ON THE LUG FOR DOOR STRUT ARM ON THE 7411351-8 SURROUND FRAME. ACCOMPLISHED FR-680A-139-15365 REV - DATED: 25-JUN-2025 - FIELD REPAIR - CRACK, FUSELAGE, AFT DOOR SURROUND FRAME, DOOR STRUT DRIVE ARM ATTACH.SDR JJBA20250721072Floor Support · corrodedLH OB FLOORSILL FROM FRAME 53 TO 65 IS CORRODED. REMOVED CORROSION LH OB FLOORSILL FROM FRAME 53 TO 59. TREATED AND PRIMED LH OB FLOORSILL FROM FRAME 53 TO 59. LH OB FLOOR SILL BETWEEN FRAME 59 AND 61 CORRODED BEYOND LIMITS. REMOVED FLOOR SILL, LOCATED, DRILLESDR SWIA2025120900720Floor Support · corrodedLBL 9 FLOOR SUPPORT IS CORRODED BETWEEN BS 863 AND 879 ON THE UPPER INBD FLANGE. REMOVED CORROSION BY BLENDING IAW REO 670-53-51-353, REV -. COMPLETED TASK CARD 51-900-1002- SKY.SDR SWIA2025110300720Floor Support · crackedLBL12.00 FLOORBEAM COCKPIT HAS CRACK. BETWEEN FS270 AND FS280. TRANS #30519326 (C-CHECK RO 11/01/2025)REPARED LBL12.00 FLOORBEAM COCKPIT REF CRJ900 SRM 53-11-43-201-003-A01. SEE CONTNINUE CARD FOR MORE DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FOSDR IPXA2025081425004Profile · crackedMAJOR REPAIR, MAIN DECK FLOOR STRUCTURE AT FRAME 79, -Y1580.5 HAS A CRACK THROUGH FASTENER HOLE COMPLIED WITH EO-94650-REQ1 AND VT-MAE EA 300-5318-27-A4086, REV. -.SDR IPXA2025090625333Support · brokenFR 75, BTW Y1221.2 AND Y1580.5, CLS ADAPTER WITH CORROSION. INSTALLED ADAPTER CLS AT THE MDC, FR 75 BTW Y1221.2 AND Y1580.5. I.A.W AIRBUS SRM 51-40-21-001.SDR IPXA2025082800037Profile · crackedMAJOR REPAIR, MDC, BTW FR 78 AND FR 79, Y2127.5, Z PROFILE WITH CRACK COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94651-REQ1 AND VT-MAE EA 300-5318-27-A4088, REV. -.SDR SWAA2025082793413Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 IAW SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 143A5400 SHEET 142 REV - AND DWG 143A5400 SHEET 138 REV -.
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