JASC 5310
Service difficulty reports · 38,548
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 R61A201712160942Finger Doubler · corrodedWHILE IN HVY MX CHECK REMOVED AND REPLACED FWD CARGO DOOR BEAM FWD FINGER DOUBLER REF.
EMB-175-SRM 53-21-11/AD03, 51-41-02, 51-43-04, 51-23-04- FWD CARGO DOOR BEAM FWD FINGER DOUBLER CORRODED
AND GOUGED AS MARKED.SDR SWIA201744186Structure · corrodedCOMPARTMENT DOOR SURROUNDING STRUCTURE CORRODED. REMOVED CORROSION IAW REO AND SRM.SDR SIMA20171215014Floor Support · corrodedLEFT OMEGA BEAM SIDEWALL CORRODED BETWEEN FRAMES 44 - 45. ACCOMPLISHED A REPAIR ON THE OMEGA BEAM IAW SRM 53-00-10.SDR CALA2017121504461Seal · corrodedAFT WET AREA L2 DOOR SILL MID SECTION SHAPE SEAL HAS CORROSION. L2 DOOR SILL MID SECTION FITTING FOUND TO HAVE 100% MATERIAL LOSS. REMOVED OLD DOOR SILL MID SECTION FITTING. REPLACED WITH NEW DOOR SILL MID SECTION FITTING PN 5348004820203 IAW A319 SRM 51-7 2-SDR GLBA2017121500697Door Frame · crackedMAJOR REPAIR - MAINTENANCE NOTED THAT THE FUSELAGE DOOR FRAME WAS CRACKED AT STRINGER 11L AND FS 171.0. CRACK IS APPROXIMATELY 1.1 INCHES IN LENGTH. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **SDR V0XD20171214002Crossbeam · crackedF.S. 280.00 CROSS BEAM LEFT HAND SIDE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED F.S. 280.00 CROSSBEAM(PN:CC670-34094-1) IAW CRJ 900 SRM 51-25-16, 51-40-11, 51-42-21, 51-42-13, 51-21-11, 51-42-06, 551-40-11, AND CRJ 900 AMM 20-70-00.SDR AALA201801269003Window Frame · crackedCRACKED RIGHT WINDSHIELD FRAME AT FRAME 4, -Y1292. REPLACED THE RIGHT WINDSHIELD FRAME IAW EA 276624.SDR AALA201801199027Fitting · crackedCRACK INDICATION ON L1 DOOR CUTOUT INTERCOSTAL FITTING AT FR 16 AND THE INBOARD LOWER HOLE AT DOOR STOP FITTING 1. REPAIRED PER EA 276159.SDR 2017FA0000639Canopy · openPILOT STATED THAT HE CLOSED CANOPY BEFORE TAKEOFF. AFTER TAKEOFF, THE CANOPY OPENED AND THE PILOT TRIED TO MANUALLY PULL THE CANOPY CLOSED AND COULD NOT. HE LANDED AT THE DEPARTURE END OF THE RUNWAY AND LANDED HARD. THE AIRCRAFT CAUGHT FIRE AND WAS DESTROYESDR KC8A20171213007Door Frame · crackedCRACKS FOUND IN CARGO DOOR LOWER FORWARD AND AFT FORMERS AT FRAME 11. THE FOLLOWING DAMAGED FORMERS REPLACED WITH NEW:
P/N 17219-5105-1 FORMER 1-EA.
P/N 17219-5105-2 FORMER 1-EA.
ALL WORK DONE IN ACCORDANCE WITH AVCON INDUSTRIES INC. CARGO DOOR MAINTENASDR SIMA20171212008Support · crackedRIGHT OMEGA BEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47 - 48. REMOVED AND REPLACED THE SUPPORT IAW SRM 53-23-02.SDR SIMA20171212009Crossmember · corrodedCENTER AISLE CROSSMEMBER CORRODED BETWEEN FRAMES 33-34. REMOVED AND REPLACED THE CROSSMEMBER IAW SRM 51-40-02, SRM 51-20-01, AND ETN-EM-53-241.SDR SIMA20171212010Crossmember · corrodedCENTER AISLE CROSSMEMBER CORRODED BETWEEN FRAMES 24-25. REMOVED AND REPLACED THE CENTER AISLE CROSSMEMBER IAW SRM 51-40-02, SRM 51-20-01, AND ETN-EM-53-241.SDR DALA2017121308555Pan · crackedINITIAL INSPECTION: CRAKED LH AFT UPPER RING PAN STA Y=1212 AND 1250 AT PAX CABIN. DAMAGE AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122. HFEC INSPECTION WAS ACCOMPLISHED ON LH AFT UPPER RING PAN STA Y=1212 AND 1250 AT PAX CABIN, CRACK OF 0.1875" WAS CONFIRSDR DALA2017121308554Pan · crackedINITIAL INSPECTION : CRACKED LH RING PAN STA Y= 1041 AND 1079 AT LOWER FWD CORNER PAXCABIN. DAMAGE AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122. HFEC INSPECTION WAS ACCOMPLISHED ON LH RING PAN STA Y= 1041 AND Y=1079 AT LOWER FWD CORNER, NO CRACKS WERE FOSDR DALA2017121308553Pan · crackedINITIAL INSPECTION : CRACKED LH RING PAN STA Y= 927 AND 946 AT UPPER FWD CORNER PAX CABIN. DAMAGE AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122. HFEC INSPECTION WAS ACCOMPLISHED ON LH RING PAN STA. Y= 927 AND Y=946 AT UPPER FWD CORNER, NO CRACKS WERE FOUNDSDR C77A20171212001Fitting · corrodedCORROSION HAS BEEN FOUND ON THE AFT CARGO DOORWAY – FWD FITTING P/N 170-85492-403, CENTER FITTING P/N 170-85251-401,
AND/OR AFT FITTING P/N 170-85493-403 ON SEVERAL COMPASS AIRCRAFT DURING BASIC CHECK. SINCE EMBRAER CLASSIFIES THESE FITTINGS
AS PSES, COMPASSSDR DALA2017121208525Pan · crackedINITIAL INSPECTION : CRACKED RH RING PAN STA Y= 1231 AND 1250 AFT UPPER CORNER PAX CABIN. DAMAGE AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122 (ET)(HFEC) WAS ACCOMPLISHED ON RH RING PAN STA Y =1231 AND 1250 AFT UPPER CORNER PAX CABIN AND NO CRACK INDICATIOSDR DALA2017121208524Pan · crackedINITIAL INSPECTION : CRACKED RH RING PAN STA Y= 807, 886, 927 AND 946 AT UPPER FWD CORNER PAX CABIN. SUMMARY OF NRC 00301: DAMAGE AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122 (ET)(HFEC) WAS ACCOMPLISHED ON RH RING PAN STA Y=807, 886, 927 AND 946 AT UPPER SDR DALA2017121208523Pan · crackedINITIAL INSPECTION : CRACKED RH RING PAN STA Y= 905 AND 1231 LOWER AFT CORNER PAX CABIN. AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122. HFEC INSPECTION WAS ACCOMPLISHED ON 1231 LOWER AFT CORNER AND TWO CRACKS WERE FOUND OF 0.200" AND 0.120". HFEC INSPECTIOSDR DALA2017121208522Pan · crackedINITIAL INSPECTION : CRACKED RH RING PAN STA Y= 984 AND 1041 AT LOWER FWD CORNER PAX CABIN. DAMAGE AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122. (ET)(HFEC) WAS ACCOMPLISHED ON RH RING PAN STA Y=984 AND 1041 AT LOWER FWD CORNER PAX CABIN AND NO CRACK INDICSDR YENA201712110996Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN R2 DOOR SILL Y-1732 23R FR 68; REPAIRED MAIN CABIN R2 DOOR SILL AT Y-1732 STR 23R FR 68 IAW A320-41-14-300-001.SDR SWIA201744152Door Frame · corrodedPAX DOOR FWD FRAME HAS CORROSION. INSTALLED A NEW DOOR FRAME IAW SRM.SDR SWIA201744151Door Frame · corrodedPAX DOOR AFT FRAME HAS CORROSION. INSTALLED THE DOOR FRAME IAW SRM.SDR SIMA20171209004Door Frame · crackedBAGGAGE DOOR FORWARD FRAME BOX FOR LIFT/LOERING MECHANISM HAS CRACK AT FORWARD LOWER END.-C/A-COMPLETED REPAIR IAW SRM 53-23-02.SDR JJBA20171208009Receptacle · damagedDAMAGE TO EXTERNAL POWER RECEPTACLE AND SURROUNDING STRUCTURE. REMOVED EXTERNAL POWER RECEPTACLE IAW EMB 145 AMM 24-40-01. REMOVED EXTERNAL POWER RECEPTACLE HOUSING IAW EMB 145 SRM 51-40-02. PERFORMED PERMANENT REPAIR IAW CONNUTAIR TECHNICAL ORDER E145-5311-20SDR SWIA2017122644104Structure · chafedSTRUCTURE CHAFED RBL 36.20 APPROXIMATELY 30 INCHES? UP FROM THE FLOORBOARD, BLENDED THE AREA. REPAIRED IAW REO.SDR JR2R20171207294Frame Angle · crackedSTA 1437 RH FRAME CLIP CRACKED. REMOVED AND REPLACED CLIP IAW MD80 SRM 51-30-5 AND 51-30-8 PARA 11 FIG 4.SDR AALA201712149005Beam · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION OF L4 DOOR SILL BEAM BETWEEN FR 66 TO FR 68, STA 38529 TO STA 39511 AT LEFT STRINGER 23. REPLACED DOOR SILL BEAM BETWEEN FR 66 TO FR 68, STA 38529 TO STA 39511 AT LEFT STRINGER 23 PER SRM 51-42-11.SDR DALA2017120408414Not Reported · corrodedC/W PRI 563889-14 REV ORIGINAL. CORROSION FUSELAGE STATION 480 AND LONGERON L-30. C/W PRI 563889-14 REV 1. C/W 563889-14 REV 0. (LP0323707)SDR FDEA201712023467Roller Tray · corrodedFWD CARGO BAY, BS 959 - 1099 ROLLER TRAY CORRODED AT THE LOCKS AND ROLLER AREAS. REMOVED AND REPLACED THE ROLLER TRAY IAW SRM 51-31-01. FOUND TO BE BEYOND LIMITS IAW SRM 51-21-02, VOL 2, PAGE 6, PARA (I). FABRICATED IAW DWG ADJ7036, INSTALLED IAW ADJ6230SDR R61A201712010898Beam · corrodedCORROSION FOUND AT 2 AREAS ON BEAM AT FRAME 12. REMOVED AND REPLACED THE BEAM IAW SRM 51-41-02, 51-43-03, AND 51-43-04.SDR SWAA2022020761229Angle · corrodedFWD CARGO R/H SIDEWALL TRANSITION ANGLE HAS CORROSION BETWEEN STA.500-500B / WP:E105601-WONG; JOHN - 12/02/2017 10:07 COMPLETE: REMOVE AND REPLACED FWD CARGO R/H SIDEWALL TRANSITION ANGLE BETWEEN STA.500-500B IAW SRM 53-00-53-2R-5 AND SEE BELOW FOR INDIVIDUAL SDR SWAA2022020761230Angle · corrodedFWD CARGO L/H SIDEWALL TRANSITION ANGLE HAS CORROSION BETWEEN STA.500-500C. / REMOVED AND REPLACED DAMAGED SECTION OF TRANSITION ANGLE PER SRM 51-40-02 AND SRM 53-00-53-2R-5.SDR SWAA2022020790061Angle · corrodedAFT CARGO BAY STA 887 TO STA947 RBL22; CORROSION ON UPPER SURFACE OF STRUCTURE. / REMOVED CORRSION AT Z-ANGLE STA 867-947 RBL 22' 'OUT OF LIMITS' ORIGINAL MATERIAL .040; REMAINING .033' LOSS .007 REMOVED 17% MAX ALLOWABLE 10% AND REMOVED; INSTALLED NEW Z-ANGLESDR DALA2019012940511Structure · damagedWHILE IN FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING REV. C (REFERENCE AMDS WORKCARD) AT FS 680 AT STR 3R, MTC REPORTED SIX (6) EXISTING OVERSIZED FASTENER HOLES. REF ERA 563820-14 REV A.SDR SWIA2017122644100Structure · dentedDENT LOCATED BETWEEN BS 672.2 AND 682. REPAIRED IAW REO.SDR SWAA2022020734724Channel · corrodedSUPPLEMENTAL INFORMATION: ***CORROSION*** FWD CARGO COMPARTMENT LH SIDE PLATE STA 500B+15 TO 500F+2.5 / CORROSION ON L/H SIDE FWD CARGO ZEE CHANNEL (SIDE PLATE) AT NUMEROUS LOCATIONS. MEASURE'S .020' AT THE DEEPEST POINT. FOUND TO BE OUT OF LIMITS IAW SRM 53-0SDR SWAA2022020734725Channel · corroded***CORROSION*** FWD CARGO COMPARTMENT LH SIDE PLATE STA 500G+20.5 TO 500H+12 / CORROSION ON ZEE CHANNEL (SIDE PLATE) AT NUMEROUS LOCATIONS FWD CARGO L/H SIDE FROM STA 500B+15-500D MAXIMUM DEPTH MEASURES .020'. FOUND TO BE OUT OF LIIMITS. REMOVED CORRODED ZEE CSDR SWAA2022020734726Angle · corroded***CORROSION*** NUMEROUS AREAS ON FWD CARGO COMPARTMENT UPPER SURFACE OF AFT BULKHEAD SUPPORT ANGLE STA 500 I / CORROSION ON LWR AFT BULKHEAD SUPPORT AT THE FWD CARGO STA 500I FOUND TO BE OUT LIMITS. REMOVED CORRODED BULKHEAD SUPPORT LOCATED; DRILLED; DEBURREDSDR SWAA2022020734727Channel · corroded***CORROSION*** AFT CARGO LH SIDE PLATE STA 727C TO STA 801 / MULTIPLE AREA'S OF CORROSION ON L/H ZEE CHANNEL AFT CARGO FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED ZEE CHANNEL. LOCATED; DRILLED; AND DEBURRED SIDE PLATE AND SPLICES FROM BAC 1496-377 LOT# 5049572SDR SWAA2022020734728Channel · corroded***CORROSION*** AFT CARGO RH SIDE PLATE STA 727D TO STA 767 / MULTIPLE AREA'S OF CORROSION ON R/H ZEE CHANNEL STA 727-767 AFT CARGO FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED ZEE CHANNEL. FABRICATED; DRILLED; AND DEBURRED NEW ZEE CHANNEL USING BAC 1496-377 707SDR SWAA2022020461218Angle · corrodedAFT. CARGO COMPARTMENT CORROSION ON L/H TRANSITION ANGLE AROUND FLOOR PANEL FASTENER HOLE AT STA. 747+9. / L/H TRANSITION ANGLE REMOVED AND REPLACED FROM STA. 747+8 TO 807+11; ALL WORK ACCOMPLISHED ON G509781SDR SWAA2022020461219Angle · corrodedAFT. CARGO COMPARTMENT CORROSION ON L/H TRANSITION ANGLE AROUND FLOOR PANEL FASTENER HOLES IN BETWEEN STA. 767+3 AND STA. 807+10.5 / REMOVED AND REPLACED L/H TRANSITION ANGLE SECTION STA. 755-817 PER SRM 53-00-53-2R-5. SEE WIP'S AND TASK'S FOR INDIVIDUAL SIGN SDR SWAA2022020489983Angle · crackedFWD CARGO COMPARTMENT STA 500C LBL 25; INTERCOSTAL SUPPORT ANGLE IS CRACKED. / REMOVED FWD CARGO STA 500C LBL 25 INTERCOSTAL SUPPORT ANGLE THAT WAS CRACKED IAW SRM 51-40-02-0G-0. LOCATED; MATCH DRILLED AND INSTALLED NEW INTERCOSTAL SUPPORT ANGLE P/N 143A7502-1SDR SWAA2022020489984Angle · crackedFWD CARGO COMPARTMENT STA 500B LBL 25; INTERCOSTAL SUPPORT ANGLE IS CRACKED. / REMOVED FWD CARGO STA 500B LBL 25 INTERCOSTAL SUPPORT ANGLE DUE TO PART BEING CRACKED IAW SRM 51-40-02-0G-0. LOCATED; MATCH DRILLED AND INSTALLED NEW INTERCOSTAL SUPPORT ANGLE P/N 1SDR SWAA2022020489985Angle · crackedFWD CARGO COMPRTMENT STA 500B RBL 25; INTERCOSTAL SUPPORT ANGLE IS CRACKED. / FWD CARGO STA 500B RBL 25 SUPPOSRT ANGLE CRACKED. DRILLED AND REMOVED CRACKED ANGLE SUPPORT IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE CLIP SUPPORT IAW SRM 51-40-05-0G-0 ALSDR AALA201801049003Window Frame · crackedCRACKED LATERAL RIGHT WINDOW FRAME BETWEEN FRAMES 4 TO 8 AT -Y1292. MODIFIED THE RIGHT WINDOW FRAME IAW EA 275851.SDR AALA201801039031Window Frame · crackedCRACK INDICATION ON WINDOW LATERAL FRAME LEFT SIDE UPPER CUT OUT BETWEEN FRAMES 4 - 8, Y1292. REPLACED THE WINDOW FRAME IAW EA 275851.SDR R61A201711280958Beam · corroded*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION IN THE FORWARD WET AREA AROUND THE GALLEY MOUNT HOLE AT FR13-FR14, RBL10. MAINTENANCE REMOVED CORROSION AND REPAIRED DAMAGED IN THE FORWARD WET AREA AROUND THE GALLEY MOUNT HO
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