JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, 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 = '5310' 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 = '5310' 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 SWAA2024030650192Pressure Deck · crackedCRACK FOUND AT FASTENER HOLE AT FLIGHT DECK FLOOR WEB BS 250+9 RBL 9. CORRECTION ON ORIGINAL WRITE UP CRACK FOUND AT FASTENER HOLE AT FLIGHT DECK FLOOR WEB BS 253 RBL 4.2<[01] ??WORK ACCOMPLISHED PER EA 24-153-00402.';[02] VERIFIED STEP 1SDR SWAA2024022950351Beam · crackedCRACK FOUND AT R1 DOOR STRUCTURE LOWER BEAM #4 AT PERIMETER OF I/B FASTENER HOLE. REMOVED DAMAGE BEAM #4 AT R1-DOOR IN REF B737-700 SRM 51-40-02-0G-0 AND INSTALLED NEW BEAM #4 AT R1 DOOR IN REF B 737-700 SRM 51-40-02-0G-0 AND DWG 141A6535 REV: F AND DWG 141ASDR AALA202402151692Pressure Deck · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB AT BS 663.75, FROM LBL 24.92 TO LBL 31.83. REPAIRED WEB PER SRM 57-10-10-2R-3 ALTERNATIVE 3.SDR JJBA20240213038Crossbeam · crackedCF1, RH SERVICE DOOR OUTBD CROSSBEAM AT FR20 FOUND CRACKED. RH SERVICE DOOR OUTBD CROSSBEAM AT FR20 REPLACED BY NEW CROSSBEAMSDR DALA2024020901763Cap · crackedCRACK ON CAP STA 1022 AND LONG 1. SUMMARY OF NRC 00351: CAP STA 1022 AND LONG 1 WAS REPAIRED PER PRI 615124-14 REV 0 AND ERA 615124-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615124 ADDED FOR AC 9566. (LP #0192767)SDR DALA2024020801697Door Frame · crackedSHIP 3330 DAMAGE ON FWD CARGO DOOR FRAME, 8 INCHES UP FROM BOTTOM FWD CORNER. CORRECTIVE ACTION: PERFORMED REWORK IAW A330 SRM 53-21-11. OK TO CONTINUE. (5477020)SDR SWAA2024031250012Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB BTW RBL 39 TO RBL 50 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH:0.316 INCH APPROX. 2024-121306<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOSDR SWAA2024022949816Pressure Deck · crackedCRACK FOUND AT HORIZONTAL PRESSURE DECK WEB AT STA 675 RBL 42. CRACK LENGTH : 0.531'.<[01] ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN HORIZONTAL PRESSURE DECK WEB BETWEEN STA 663.75 AND STA 675 FROM RBL 38 TO RBL 60 REF B737-700 SRM 53-40-51-2R-2 TABLE 201 FISDR SWAA2024022649824Pressure Web · crackedINTERNAL HORIZONTAL PRESSURE DECK WEB STA 663 TO STA 675 - .3' CRACK NOTED AT LBL 30+7. MARKED LOCATION.<[01] VERIFIED STEP 12 IN PARTIAL.;[02] VERIFIED STEPS 3;4;5;12 COMPLETE.;[03] REMOVED DAMAGED SECTION OF THE PRESSURE DECK BS663-BS675 LBL30-LBL60 WL199 ANSDR REXA2024021900202Electrical Box · crackedFOUND EXTERIOR POWER PLUG BOX SURROUND TO BE CRACKED. REMOVED EXTERNAL POWER PROVISIONS BOX (CC670-33401-3) IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. INSTALLED NEW EXTERNAL POWER PROVISIONS BOX (CC670-33401-3) IAW CRJ 900 SRM 51-42-06-001-SDR DALA2024020901759Vertical Beam · crackedSHIP 3261 DISC: FWD AVIONICS BAY, AT FR-1, TOP OF VERTICLE POST AT R/H Y-330 HAS 1.5 IN CRACK. SEEN ON O/B SIDE. REF BY AIRBORNE/PEMCO NR .15017.111. C/A: C/W STEPS 1-3 OF PRI615368-14 REV 0 EA HOLE CRACKED AWATING ENGINEERING P108 1604328 Q951 516209 C/W ALL SDR DALA2024020801691Door Frame · crackedSHIP 3124 FR16RH AT DOOR STOP NO 7 LEVEL, DBL JGL AREA / FASTENER HOLE #6 CRACK. CORRECTIVE ACTION: REPAIRED PER ER/A 614228-14. (0191951).SDR DALA2024020801690Door Frame · crackedSHIP 3124 FR16RH AT DOOR STOP NO 7 LEVEL, DBL JGL AREA / FASTENER HOLE #6 CRACK. CORRECTIVE ACTION: REPAIR PER ER/A 614198-14. (0191626).SDR IPXA2024020837884Adapter · brokenO/B L/H CLS ADAPTER AT FR37 IS BROKEN REMOVED AND REPLACED CLS ADAPTER IAW A300-600 SRM 51-40-21. INSTALLED SIDEWALL PANEL 131PW AND CEILING PANELS 131UC AND 131WC IAW A300-600 SRM 51-40-21SDR IPXA2024020737884Adapter · brokenO/B L/H CLS ADAPTER AT FR37 IS BROKEN REMOVED SIDEWALL PANEL 131PW AND CEILING PANELS 131UC AND 131WC FOR ACCESS IAW A300-600 SRM 51-41-21SDR VNAA202402050031Buttstrap · corrodedCORROSION ON FUSELAGE CIRCUMFRENTIAL JOINT BTW FS280.00/ FS282.86 AND STGR 24LH/23RH. CORROSION ON FUSELAGE CIRCUMFRENTIAL JOINT BTW FS280.00/ FS282.86 AND STGR 24LH/23RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, BTW STGR 27 TO STGR 23R WAS EVALUATEDSDR EE4Y2023122819077Skin Panel · damagedFORWARD FUSELAGE, FR03, STRINGER 22RH+130MM, EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD 2023-190-030945 GUIDELINES AS STATED IN ENGINEERING ORDER NO: COO-EO-2023-18945-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SDR VNAA202402050016Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1334 REV.SDR CALA2024032700873Window Frame · crackedCRACK CONFIRMED AT LEFT EXTERNAL FLIGHT DECK #3 WINDOW FRAME FWD FASTENER HOLE #2, CRACK LENGTH FWD DIRECTION 0.156 INCHES AND AFT 0.156 INCHES OF FASTENER HOLE. REF. AAR N/R:9876305 ACCOMPLISHED REPAIR AND MODIFICATION AT L/H SIDE NO.3 WINDOW FRAME AS PER ESRSDR 2024FA0000250Beam · corrodedMAIN DECK AFT CABIN RIGHT SIDE Y1447.8 BETWEEN FR74-FR77 FOUND LONGITUDINAL BEAM CORRODED.SDR 2024F00086Beam · corrodedMAIN DECK AFT CABIN RGHT SIDE Y1447.8 BETWEEN FR74-FR77 FOUND LONGITUDINAL BEAM CORRODED.SDR SWAA2024030648820Pressure Deck · crackedCRACK FOUND AT HORIZONTAL PRESSURE DECK WEB AT STA 663 RBL 41. CRACK LENGTH 0.218'<[01] ACCOMPLISHED REPAIR AT HORIZONTAL PRESSURE DECK WEB AT STA 663 RBL 41 IN REF WITH 53-40-51-2R-2;[02] VERIFIED STEP 1SDR R61A2024022900091Crossbeam · corrodedRH CROSSBEAM AT FR17 HAS AREA OF CORROSION. PERFORMED PERMANENT REPAIR BY CUTOUT AND L-ANGLE INSTALLED INSTALLED ON RH CROSSBEAM AT FR-17, REF SRM 53-00-10/R03P.SDR AALA202402096005Door Frame · damagedAIRCRAFT IN BASE MAINTENANCE: FORWARD RIGHT HAND EMERGENCY EXIT FRAME HAS LOOSE NUTS ARROUND TRIM STRIP. SECURED FORWARD RIGHT HAND EMERGENCY EXIT TRIM STRIP NUTS. PER B737 NG AMM 52-22-51.SDR DALA2024020901756Fitting · crackedSHIP 1604 CABIN WING CENTER SECTION AREA FOUND FRAME END FITTING CRACKED AT STA927 LH. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER PRI 615135-14 REV 0 (0187696)SDR UIEA2024013100057Longeron · crackedFUS - 2EA CRACKS WERE FOUND ON RH BS 1480-1540 STR 32-33 LONGERON EXTENSION FITTING(<P>LONGERON EXTENSION FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO 4453A818 R19 PART 4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024020100059Ladder · crackedM/D CREW LADDER I/B SIDE #7 & 10 STEP FOUND CRACK(<P>#7 AND #10 STEP CRACK AREA REPAIRED AS PER RI-25-50-16667 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100064Closeout Panel · crackedM/D STA 1241 LBL 77-99 CLOSURE PNL FOUND CRACK.(<P>CLOSURE PNL REPLACED AS PER SRM 51-10-02, NEW PNL HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW PNL INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)SDR CALA2024020700348Pressure Deck · crackedSUPPORT TASK : AD 2001-18-09, EA 5300-01502 REV A OP 001 - 1EA CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB BETWEEN STA 1287 AND 1308, LBL 18.3 AND 25.7. TRANSFER REF.NON-ROUTINE HX NRC WO.2707022. HORIZONTAL PRESSURE DECK WEB BETWEEN STA 1287 AND 1308 LBL 18.3SDR KCSA202402051006Closeout Panel · crackedCANTED PRESSURE DECK COMPOSITE CLOSEOUT PANEL EVIDENCE OF CRACK AT STA 1240 LBL 91SDR VNAA202402050005Canister · crackedCRACK IN CANISTER WELDED #3 IN STA WS148 OF INTERNAL LH MAIN FUEL TANK. CORRECTIVE ACTION: WELDED #3 IN STA WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.-SDR VNAA202402050004Seat Track · corrodedCORROSION AT SIDE SEAT RAIL OF STGR 15RH BETWEEN FS 847.00 + 62.00 TO FS 862.00. CORRECTIVE ACTION: SIDE SEAT RAIL OF STGR 15RH BETWEEN FS 847.00 + 62.00 TO FS 862.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-49-41-101-001-A02 AND REPLACE PER CRJ900 AMM SDR R61A2024022900090Crossbeam · corrodedSEVERAL AREAS OF CORROSION ON FRAME 84 BETWEEN LH FLOOR SILL AND LH INBD SEAT TRACK. REMOVED AND REPLACED CROSSBEAM FRAME 84 BETWEEN LH FLOOR SILL AND LH FLOOR SILL AND LH INBD SEAT TRACK REFER SRM 51-40-08.SDR DALA2024020601609Crossbeam · crackedSHIP 3124 CRACKS FOUND IN HOLE #25 AND HOLE #26 OF FR 20 LHS CROSSBEAM SPLICING. CORRECTIVE ACTION: REPAIRED PER ER/A 614242-14. (0186903)SDR DALA2024020601576Doubler · crackedCRACK ON INTERNAL DOUBLER AFT EDGE BTW BEAM #1 AND #2 AT FWD CARGO DOOR. SUMMARY OF NRC 00104: INTERNAL DOUBLER (WEB) AFT EDGE BTW BEAM #1 AND #2 AT FWD CARGO DOOR WAS FABRICATED AND REPLACED PER BOEING DWG 9957664 REV "N", B717-200 SRM 51-41-01-0G, 51-41-02-0SDR CALA2024020500324Torque Box · corrodedAFT PIT TORSION BOX COVERSHEET CORRODED. REMOVED AND REPLACED AFT CARGO TORSION BOX COVER SHEET AND THRES HOLD SHEET IAW A319 SRM 51-72-11-911-001 AND SRM 51-72-11-911-00 2.SDR SWI202403190237Window Frame · crackedRIGHT WINDSHIELD SIDE POST SUPPORT STRUCTURE HAS A CRACK, BELOW THE POST. (MARKED & FLAGGED) (C-CHECK RO 3/19/2024) REPLACED SUPPORT BRACKET PER BOMBARDIER DRAWING 601R34032 (REV P) -AND- CRJ200SRM 51-40-06 & SRM 51-42-06.COMPLETED SKYWEST TASK CARD 51-90SDR SWI202403190236Window Frame · crackedLEFT WINDSHIELD SIDE POST SUPPORT STRUCTURE HAS A CRACK, BELOW THE POST. (MARKED & FLAGGED) (C-CHECK RO 3/19/2024) REMOVED CRACKED LEFT WINDSHIELD POST SUPPORT STRUCTURE AND INSTALLED NEW. REF. CRJ200 SRM 51-40-06, DWG NO. 601R34032 REV. P, & DWG NO. 601RSDR SWIA20240319203Cam · gougedPASSENGER DOOR FRAME FORWARD CAM GOUGED (C-CHECK RO 3/19/2024) REPLACED CAM FITTING & SHIM AT PAX DOOR FWD FS310 FRAME PER CRJ200 SRM 51-23-00 & SRM 51-42-21 & BOMBARDIER DWG 600-31900 REV K. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND SKYWEST FORM M-SDR SWAA2024022948456Access Panel · crackedCRACK ON MARKER BEACON ANTENNA ACCESS PANEL 192F BODY STATION 616 AT KEEL BEAM. REPLACED MARKER BEACON ANTENNA PANEL 192F AT LOWER FUSELAGE I.A.W B737-700 AMM 34-32-11-401-NG; PERFORMED TEST OF THE MARKER BEACON ANTENNA; TEST IS OK.SDR R61A2024022900089Beam · corrodedFWD CARGO DOOR CUTOUT LOWER BEAM FWD DOUBLER HAS CHAFF.REMOVED AND REPLACED FWD FINGER DOUBLER AT FWD CARGO DOOR CUTOUT LOWER BEAM REF E175
SRM 51-40-08.SDR R61A2024020300056Door Frame · corrodedWHILE IN HEAVY CHECK - L1 DOOR CUTOUT STRUCTURE HAS MULTIPLE AREAS OF CORROSION AS MARKED. REMOVED AND REPLACED L1 DOOR CUTOUT STRUCTURE. REF: SRM 51-40-08SDR CALA2024030500637Structure · corrodedUPPER FUSLAGE FR 66 AFT SURFACE HAS CORROSION. 2.5 IN INBD EDGE. 2.0 & 3.0IN FROM FLOOR SUPPORT STRUCTURE FOUND DURING COMPLIANCE OF N/R#78715.() 53-41-12-205-003 TABLE 1 INSP THRESHOLD FROM 1ST FLIGHT 2400FC, FOR THIS INSP, SRM 1.F (2) NOTES FOR TIME FOR FIRSSDR R61A2024022300082Crossbeam · corrodedFWD FUSELAGE FR 19 LBL 11 FOUND TO HAVE CORROSION ON CROSSBEAM. CROSSBEAM WAS REPAIRED IAW EMB 175 SRM AND ETD 2024-170-003553. MAJORSDR R61A2024022630082Crossbeam · corroded******MAJOR*****FWD FUSELAGE FR 19 LBL 11 FOUND TO HAVE CORROSION ON CROSSBEAM. CROSSBEAM WAS REPAIRED IAW EMB175 SRM AND ETD 2024-170-003553*******MAJOR*****SDR SWIA20240320201Structure · chafedLEFT MAIN LDG GEAR WHEEL WELL OB CORNER FS511.0 AND WS50.54 AREA EVAL CHAFFING (C-CHECK RO 3/19/2024) PERFORMED REPAIR ON DAMAGE AREA AT L/H MLG WHEEL WELL O/B CORNER ON LWR WING PLANK LBL 45.00 STR #3 IAW CRJ 200 REO 601R-57-21-3824, AND CRJ 200 SRM 57-21SDR ASAA2024020148089Door Frame · corrodedR2 DOOR FASTENERS, HEADS, AND LOWER AFT CORNER DOOR FRAME HAS EVIDENCE OF CORROSION. GROUNDED - YES. PROCURED, LOCATED, DRILLED, AND INSTALLED R2 DOOR AFT LOWER CORNER FITTING IAW A320 SRM 51-44-11/001 REV. 147SDR YENA2024020600241Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT (1 EA); REFAEROMAN NR 2023-741053 REMOVED AND REPLACED CONTINUITY FITTINGS IAW RESDR YENA2024020600238Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE A. CRACK DI RECTION AT 9 O CLOCK. D= 0.160 INCH; REF AEROMAN NR 2023-741039 WO 2023 362/1 PERFORMED REPAIR ON HOLE #A LOCATED ON FOR 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INSTRSDR YENA2024020600232Flange · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ONN FR68 LH SIDE HORIZONTAL FLANGE RADIUS AT STR 22LH, CRACK LENGTH .300 INSCH APPROX, AT AFT GALLEY AREA; REF AEM WO: 2023 362/1, NR 2023-741036. ACCOMPLISHED REPAIR ON RADIAL FLANGE STOP FITTING AT FR68,STR22L
Back to JASC 5310