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 DALA2024051505224Intercostal · crackedCRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00679: CRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1. (LP #0343135)SDR IXXA2024051501Panel · damagedP32 PANEL HAS DAMAGE AROUND WIRE PASS THRUSDR 2024FA0000926Bracket · crackedFLAP HANDLE FORWARD SUPPORT BRACKET FOUND CRACKED. NOTED AREA OF STRESS/CRACK A LACK OF RADIUS. REPLACED WITH FACTORY NEW BRACKET.SDR HNAA2024091200769Support Bracket · cracked784- TEMP REPAIR IAW EO1-53-21-0254 & ETD2021-145-030320 PERFORMED AT TAT:47747 & TAC: 44977 REQUIRES REPLACE OF PART (145-21873-007) AT FRAME 73 SUPPORT BRACKET AT STR 16R AT OR BEFORE 5000FC.SDR SWIA20240813514Angle · crackedRIGHT TORQUE BOX BL9R FS280.00 OUTBOARD ANGLE OUTBOARD SIDE OF THE TORQUE BOX AT FS280.00 IS CRACKED. (C-CHECK RO 8/11/2024) REMOVED DAMAGED OUTBD ANGLE AT FS280-00 RBL-9 OUT BOARD OF TORQUE BOX. REF CRJ-700 SRM 51-42-21-001-001-A01. INSTALLED 1 EA NEWSDR VNAA20240726008Angle · corrodedCORROSION ON ANGLE, LOWER SILL (4EAS) BTW FS 319.70 TO FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. ANGLE, LOWER SILL (4EAS) BTW FS 319.70 TO FS 349.00 WERE EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-00-00-101-001 -A01 AND WERE REPLACED PER CRJ900 SRM 51-42SDR VNAA20240726007Strap · corrodedINITIAL INSPECTION: CORROSION ON STRAP, INNER (2EAS) FS 319.70 AND FS 349.00 OF STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE. STRAP, INNER (2EAS) FS 319.70 AND FS 349.00 OF STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ900 SSDR VNAA20240724003Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. FLOOR SUPPORT RBL 12.00 BTW FS 220.00 TO FS 229.00 WAS REPAIRED PER REO 690-53-11-1797 REV. - -SDR VNAA20240724001Fitting · corrodedCORROSION ON SETTLEMENT FITTING (1EA) FS 310 ( LBL37) OF ENTRANCE COMPARTMENT AT FUSELAGE FLOOR STRUCTURE. SETTLEMENT FITTING AT FS310 LBL37 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR VNAA20240723009Plate · corrodedINITIAL INSPECTION: CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT. CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT.SDR VNAA20240723006Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RH FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.SDR VNAA20240723005Support · crackedAFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM). REFUEL DUCT MOUNTING SUPPORT WAS REPAIRED PER REO 690-28-25-022 REV.--SDR VNAA202407110012Fitting · corrodedCORROSION ON SETTLEMENT FITTING (3EAS) OF ENTRANCE COMPARTMENT AT FUSELAGE FLOOR STRUCTURE. CORROSION ON SETTLEMENT FITTING (3EAS) OF ENTRANCE COMPARTMENT AT FUSELAGE FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WERE REPSDR VNAA20240619023Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA20240619022Plate · corrodedCORROSION ON JOINT PLATE FS 519.64 OF FWD BAGGAGE BAY DOOR SURROUND STRUCTURE AT FWD CARGO COMPARTMENT. JOINT PLATE FS 519.64 OF FWD BAGGAGE BAY WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-23-001-001-A02, AND WAS REPLACED PER CRJ900 SRM 51-42-22-001-001-SDR VNAA20240619021Strap · corrodedCORROSION ON STRAP OF FLOOR STRUCTURE FS 581.00 BTW STGR 24RH TO STGR 27 AT FWD CARGO COMPARTMENT. STRAP OF FLOOR STRUCTURE FS 581.00 BTW STGR 24RH TO STGR 27 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01, WAS FABRICATED PER DWG: SH670-33320SDR VNAA20240619013Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EAS) BTW STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (2 EAS) BTW STA. FS= 349 TO FS= 364 NEAR STGR 27 WERE EVALUATED OUT OF
LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND WERE REPLACED PER CRJSDR VNAA20240619009Web · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB. UPPER WEB OF ADG COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01.SDR SWAA2024061485504Floor Support · corrodedFLOOR SUPPORT STRUCTURE AT BS 953 BL 24 LEFT HAS A SPOT OF CORROSION AT FASTENER LOCATION. AS MARKED.<[01] REMOVED CORROSION FROM AREA; ORIGINAL THICKNESS WAS .080'. REMOVED .014' OF MATERIAL. REMAINING THICKNESS IS .066'. FOUND TO BE OUT OF LIMITS IAW B737-80SDR JJBA20240610013Floor Support · corrodedRF1, UNDERFLOOR, RH OMEGA BEAM FOUND CORRODED BTW FR 59-60 AND 60-62 AROUND ANCHOR NUT. RH OMEGA BEAM BTW FR 60-62 BLENDED, FOUND WITHIN LIMITS. REPAIR DOUBLER PERFORMED ON CTR FUSELAGE IV, RH OMEGA BEAM UPPER SURFACE BTW FR 59-60SDR SWAA2024060685757Angle · crackedCRACK ANGLE - CLIP LOCATED BS500H STR26L FWD FACE FWD CARGO COMPARTMENT 2024-318189<[01] REPLACED ANGLE - CLIP LOCATED BS500H STR26L FWD FACE FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 175 REV -.;[02] CORRECTED STEP 1. REPLACEDSDR SWAA2024060685758Support Angle · corrodedCORROSION ON SUPPORT ANGLE LOCATED BS500I WL156 AND BTW STR26L TO STR26R AT FWD CARGO COMPARTMENT 2024-318190<[01] REPLACED SUPPORT ANGLE LOCATED BS500I WL156 AND BTW STR26L TO STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRAWING 143A9481 SHEESDR REXA2024052800406Floor Support · corrodedPREVIOUS FLOOR BEAM REPAIR AT L.B.L 27.00 HAS CORROSION ON THE CAP AT F.S. 1025.00 TO F.S. 1037.00. REPAIRED DAMAGE I.A.W. BOMBARDIER CRJ900 SRM 53-00-41-201-001-A03.SDR AALA202405246910Channel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE CHANNEL ASSEMBLY AT STA 500D, LBL 19. REPLACED CHANNEL ASSEMBLY PER AARD 51-00-05-1.SDR AALA202405221299Floor Support · looseAIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOOR BOARD SUPPORT FROM STA 520 TO STA 540 LOOSE AT AFT END. REPLACED FLOOR BOARD SUPPORT PER SRM 51-40-02-0G.SDR FDEA202405140668Support Angle · gougedDURING INSPECTION FOUND DAMAGE TO FWD. LOWER CARGO DOOR CEILING SUPPORT ANGLE COVER. MARKED WITH TAPE. REPAIRED DAMAGE TO FWD. LOWER CARGO DOOR SEAL REF. EA H-5320-T0379144. FOR REPAIR WORK...SEQ. 161. SEE JPF FOR OTHER WORK PERFORMED. (WRI 53200994)SDR DALA2024051605267Web · corroded(LOG 0344090) CORROSION AT AFT GALLEY FLOOR WEB HAS CORROSION AT STA 986+12 -1016+4" LBL36 WL208. REMOVED AND REPLACED AFT GALLEY FLOOR WEB AT STA 986+12" - 1016+ 4" LBL 36 WL 208 I.A.W B737 SRM 51-40-02-0G, DWG# 147A5700 REV-. AFT GALLEY FLOOR WEB FABRICATED SDR DALA2024051605266Web · corroded(LOG 0344082) AFT GALLEY FLOOR WEB AT STA 986+12"-1006+5" RBL36 WL208 HAS CORROSION. REMOVED AND REPLACED AFT GALLEY FLOOR WEB AT STA 986+12" - 1006+ 5" RBL 36 WL 208 I.A.W B737 SRM 51-40-02-0G, DWG# 147A5700 REV-. AFT GALLEY FLOOR WEB FABRICATED PER ER/A 6176SDR DALA2024051505228Floor Support · corrodedSHIP 3132 CORROSION FLOOR BEAM -Y765 LOCATED FR 17 TO FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 AND FASTENERS LOCATED BETWEEN FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM51-72- 11.SDR DALA2024051505227Floor Support · corrodedSHIP 3132 CORROSION FLOOR BEAM -Y765 LOCATED FR 17 TO FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 AND FASTENERS LOCATED BETWEEN FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM51-72-11. (0342254)SDR CALA2024051501480Support Beam · damagedWING CENTER SECTION LOWER SUPPORT BEAM LOWER CHORD AT RBL 40.875 DAMAGED ( SRM REPAIR 57-10-13-2R-3 LP CREATED FOR ESFR PURPOSE ONLY SEE ORIGINATING NR 1997479 FOR WORK PERFORMED ESFR CREATED. POSITIVE # 1036193SDR FDEA202405140664Frame · chafedMAIN DECK - CARGO BARRIER NET LEFT HAND SUPPORT YOKE AT STATION 535 LONGERON LONGERON 19 - LEFT EXISTING REPAIR OUTER ANGLE FOUND CHAFFED. MAIN DECK AT EXISTING REPAIR AT LEFT HAND FRAME STATION 535 LONGERON 19 LEFT CHAFED OUTER REPAIR ANGLE REMOVED AND RESDR IPXA2024062742586Web · crackedAGING ACFT INSP.- FRAME WEB BETWEEN FRAME 86L AND 87L IN AFT ACCESORY COMPT. ARE BENT AND CRACKED. DOT AA025. INSTALLED FRAME WEB BETWEEN FRAME 86 & 87 LH STGR 34 IAW SRM 51-40-21 P/N:CR3213-5-02, BTCH:0004070310. APPLIED CIC AT FRAME WEB BETWEEN FR 86 & 87 LHSDR VNAA20240619016Bracket · corrodedCORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON BRACKETS, MACHINED (7EAS) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM
53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-01; CRJ900 SRM 5SDR VNAA20240619015Plate · corrodedCORROSION ON PLATES (BL0) (2EAS) PLATE 1 BTW FS 517.00 STGR 27. PLATE 2 BTW FS565.00 STGR 27. AT FWD CARGO COMPARTMENT. STRINGER 27 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE FABRICATED PER (EO) SH670-3337, AND WERE REPLACED PESDR VNAA20240619014Mount · crackedAFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) WAS REPAIRED PER REO 690-28SDR SWAA2024061485219Floor Support · corrodedCORROSION FOUND ON INTERCOASTAL FLOOR BEAM BETWEEN BS 294-312; BL 0; WL 208 UPDATE-CORROSION FOUND ON INTERCOASTAL FLOOR BEAM BETWEEN 294-312 LBL 11 WL 208.<[01] REMOVED AND REPLACED NEW INTERCOSTAL FROM BS294-BS312; LBL11 PER SRM 51-40-02 AND PER DWG#141A5600SDR AALA202406143803Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR SWAA2024061385206Scuff Plate · crackedR-1 DOOR SCUFF PLATE CRAKED AT AFT CORNER<[01] WELD REPAIRED SCUFFPLATE FOR R1 DOOR PER SRM53-10-15-2R-2; WORK ACCOMPLISHED BY J.L. WELDING; W/O# 16612; PO# 414702.<BR>SCUFFPLATE WILL BE INSTALLED ON (TTG8Q003GBLY);[02] VERIFIED STEP 1SDR IPXA2024052144309Support Angle · crackedFAULT -A300 OPEN Z200 - RH FR 37 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21 P/N HL11VF6-3 BATCH# 0004186230 P/N 3D0006-3 BATCH# 0004273630 REVIEWED.SDR IPXA2024052144327Support Angle · crackedFAULT -A300 OPEN Z200 - RH FR 38.1 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED. INSTALLED STIFFENER AT FRAME 38.1 R/H TO 38.2 R/H IAW SRM 51-40-21 P/N HL11VF6-3 BATCH #0004186230 P/N HL116-6 BATCH# 4279917 P/N 3D0006-3 BATCH# 0004273630 REVIEWED.SDR AALA202406121049Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR SWAA2024060685370Angle · crackedCRACK ANGLE LOCATED BS867 AND LBL11 AFT CARGO COMPARTMENT 2024-318172<[01] REPLACED ANGLE LOCATED BS867 AND LBL11 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-05-0G-0; DWG 149A8102 SHEET 19 REV A. AND DWG 149A8104 SHEET 1 REV B.;[02] CORRECTED STEP 1. REPLACEDSDR IPXA2024052844359Support Angle · crackedRH FR 38.2 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED TREATED AND PRIMED NEW CUSP WEB IAW A300 SRM 51-21-10 PRIMER PN: 10P4-2NF BATCH: 8473297014 ALODINE1132 BATCH: 1445846. APPLIED TOPCOAT IAW A300 SRM 51-75-10-201 P/N ECL-G-101SDR AALA202405200396Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR BOARD SUPPORT BREAK ASSEMBLY PANEL AT STA 538, LBL 1. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR AALA202405204154Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR BOARD SUPPORT BREAK ASSEMBLY PANEL AT STA 538, RBL 1. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR VNAA2024051700002Floor Support · corrodedRH GALLEY FLOOR SILL FS280-FS310HAS CORROSION AROUND GALLEY FLOOR BOLT HOLE. REMOVED CORRODED FLOOR SIDE SILL. LOCATED AND DRILLED RH GALLEY FLOOR SILL (P/N: SH670-32172-11) IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE RH GALLEY FLOOR SILL (SDR A6WA202405138748Support Bracket · crackedCRACK FOUND ON POWER RECEPTACLE SUPPORT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET SUPPORT MEMBER P/N 600-33-83-33 ON POWER RECEPTACLE IAW SRM 51-42-06 REV. 39. ALL WORK PERFORMED UNDER WORK ORDER 004309, CARD 20031, TT: 47,227:03 TC: 4SDR DALA2024051405209Stiffener · crackedSHIP 1818 MFEC FOUND 01 EA CRACK AT NOSE WHEEL WELL RH VERTICAL STIFFENER AT STATION 287 BETWEEN WL159 AND WL 185 ABOUT 1 INCH LONG AS MARKED. CORRECTIVE ACTION: THE CRACK LENGTH:1", CARRIED OUT THE RH VERTICAL STIFFENER REPAIR AT NOSE W/W STA287 BETWEEN WL159SDR DALA2024051405175Support Angle · crackedCRACKS (2 EA) ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 5L AND 6L ALSO 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA. SUMMARY OF NRC 00400: CRACK ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA WAS REPA
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