JASC 5311
Service difficulty reports · 61,549
Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311' 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 = '5311' 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 SWIA2020013148005Frame · corrodedCORROSION FWD SIDE FRAME FLANGE ON FRAME AT FS319.70 BETWEEN STGR24L - STGR25R, MARKED (C-CHECK) RO 1/28/2020 REPAIRED FRAME FS319.70 BETWEEN STGR24L TO STGR25R PER COMPLIED WITH ALL STEPS OF BOMBARDIER REO.SDR SWIA2020013147996Frame · corroded*FS 349 FRAME OPPER FLANGE HAS CORROSION AT STR 26R (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON FRAME AT FS349 UPPER FLANGE STGR26R CRJ200 SRM, REPAIRED FRAME REF REO. COMPLIED WITH ALL STEPS OF REO, SEE CONTINUATION CARDE FOR DETAILS.SDR SWAA2020012240669Frame · corrodedAFT CARGO PIT FRAME CORRODED EMITTING UNDER SIDE PLATE AT BS. 727B, BETWEEN LBL 14.5 TO LBL 21. / REPAIRED FRAME IAW EA.SDR DALA2019122327515Frame · crackedDURING INSPECTION, FOUND ONE CRACK COMMON TO FRAME AT STA 654+121, BETWEEN S-9R AND S-10R. ONE CRACK COMMON TO FRAME AT STA 654+121, BETWEEN S-9R AND S-10R ACCOMPLISHED REPAIR IAW PRI 583789-14 REV.0 AND PRI 583789-14 REV.1, COMPARED AND COMPLIED WITH ER/A 583SDR DALA2019122727566Fitting · crackedCRACK INDICATION ON INTERCOSTAL FITTING ON UPPER AND LOWER INBOARD HOLES AT LEVEL DOOR STOP 7 LT, FRAME 16 AT FWD GALLEY AREA (2EA), REPLACED INTERCOSTAL FITTING ON UPPER AND LOWER INBOARD HOLES AT LEVEL DOOR STOP 7 LT FRAME 16 AT FWD GALLEY AREA AS PER A320 SSDR SWIA2020021848606Former · corrodedUPON REMOVAL OF FORMER F/S 323.963 TOFOM FOUND QTY 2 ATTACHEMENT CLEATS EXFOLIATED (C-CHECK) RO 2/14/2020 REMOVED AND INSTALLED QTY 2 NEW CLEATS IAW CRJ 900 SRM, COMPLETED FORM M-337.SDR SWIA2019122647091Gusset · corrodedAFT WET AREA- FRAME 90 RT GUSSET PLATE CORRODED. REMOVED AND REPLACED THE GUSSET PLATE IAW SRM.SDR SWIA2019122647090Frame Splice · corrodedAFT WET AREA- FRAME 90 CENTER SPLICE CORRODED. REMOVED AND REPLACED CENTER SPLICE ON FR 90 IAW SRM.SDR SWIA2019122647089Frame Splice · corrodedAFT WET AREA- FRAME 89 SPLICE CORRODED. REMOVED AND REPLACED AFT WET AREA- FRAME 89 SPLICE IAW SRM.SDR FDEA2020011680138Frame · corrodedAFT CARGO COMPT - STA 1964 AT L46 SHOWS CORROSION ON FRAME. REPAIRED NOTED AREA OF CORROSION I.A.W. SRM 53-00-07-2R FIG 202 SHT 1.SDR DALA2019122097467Frame · crackedCRACK INDICATION ON FRAME 16 UPPER INBD HOLE OF DOOR STOP 7 RH SIDE, C RACK DIRECTION 6 OCLOCK. DEPTH IS 0.220 INCH. AT FWD GALLEY AREA (1 E A). REPLACED FITTING 7 (INTERCOSTAL) RH SIDE FRAME 16 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DRAWING #D5311230SDR DALA2019121807404Frame · crackedCRACK INDICATION ON FRAME 16 LOWER INBD HOLE OF DOOR STOP 7 LH SIDE, C RACK DIRECTION 3 OCLOCK. DEPTH IS 0.160 INCH AT FWD GALLEY AREA (1 E A). REPLACED FITTING 7 (INTERCOSTAL) LH SIDE ON FRAME 16 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DRAWING #D53112SDR SWIA2020020348205Frame · corroded*FRAME FOUND CORRODED AT FS605.00 FROM STGR21LH THROUGH STGR24RH. CIRCLED WITH GREASE PENCIL V (C-CHECK) RO:1/29/2020REMOVED CORROSION ON FRAME FS605.00 AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW FRAME FS605.0SDR SWIA2020020348190Frame · corroded* THE LH FRAME AT FS513.00 HAS CORROSION AT LOWER END BY THE LH FLOOR SILL. (C-CHECK) RO:1/29/2020REMOVED CORROSION FROM LH FRAME AT FS513.00 AT FLOOR SILL REFERENCE CRJ200 SRM NDT INSPECTED NO DEFECTS NOTED,EVALUATED AND FOUND TO BE WITHIN LIMITS RESDR DALA2019121807403Frame · crackedCRACK FRAME 36 THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35RH AND FR36RH. MODIFY IN ACCORDANCE WITH WORK CARD 5311-01171-04B PRIOR TO FURTHER FLIGHT. AA 5311-01171. SB A320-53-1263. AD-2018-06-04. IN FWD CARSDR SWIA202002248809Frame · corrodedFS605.00 FRAME BELOW FLOOR UNDER CARGO DOOR SILL IS CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED LOWER FRAME AT FS605 WITH NEW FRAME IAW CRJ 200 SRM AND SRM.SDR SWIA202002248808Frame · corrodedFS349.00 FORWARD OF AVIONICS DOOR CUT-OUT THREE GROUNDING POINTS N3598/N3597/N3596 AND FRAME IS CORRODED. (C-CHECK) RO 2/20/2020 GROUNDING POINTS N3598/N3597/N3596 IS ON FS 333.00 AND NOT ON FS349.00. FRAME FS333 HAD 100% MATERIAL LOSS AND FOUND TO BE OUSDR SWAA2019123039992Stub Frame · crackedSTUB FRAME INBOARD FLANGE CRACKED AT BS. 294, RBL 55 COMMON TO FASTENER HOLES. / REPAIRED STUB FRAME IAW SRM.SDR DALA2019122077455Frame Angle · corroded(LOG 1405338) DURING INSPECTION FOUND CORROSION ON FRAME CLIP STA 336 BTW STR 20LH TO 23LH. FRAME CLIP STATION 336 BTW STR 20LH TO 23LH WAS REPLACED PER B737-800 SRM 51-40-02 PAR. 4 AND DWG: 141A8240 REV. D.SDR DALA2019122077453Frame · corroded(LOG 1405314) DURING INSPECTION FOUND CORROSION ON FRAME STATION 336 BTW STR 20LH TO 23LH. FRAME STATION 336 BTW STR 20LH TO 23LH WAS REPLACED PER B737-800 SRM 51-40-02.SDR SWIA2019121746882Frame · cracked*FRAME ABOVE THE PAX DOOR AT FS333 BETWEEN STGR O AND STGR 1 L IS CRACKED AT TOOLING HOLE. (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED REPLACEMENT FRAME AT FS333.00 FROM STR0 TO STR1L REF: SRM. SEE CONTINUATION CARD FOR DETAILS.SDR DALA2019121707365Frame · crackedCRACK INDICATION ON FRAME 20 FASTENER HOLE 5 AT LEVEL OF DOOR STOP 7, RH SIDE. CRACK DIRECTION 9 OCLOCK, DEPTH IS 0.100 INCH, WORK CARD 5310 -3024-1593 AND SSI 531155. AT FWD GALLEY AREA D =0.100INCH. PERFORMED REPAIR INSTRUCTION SECTION I ASPER PRI 583468-14 SDR DALA2019121607314Frame · crackedAD/EM-EO TASK - HFEC INSPECTION FOUND 01EA CRACK APPROX 0.700" IN LENGTH ON STA 1809 RIGHT FORWARD OUTER CHORD BETWEEN STR 6R AND 7R, ABOUT 1" FROM STR 6R AS MARKED PER W/C : 5310-01380-0202 STEP 6.SDR SWIA2020021848593Frame · corrodedFRAME FS313.56 BETWEEN DD4 AND DD5 IS CORRODED. (C-CHECK) RO 2/14/2020 PAX DOOR FRAME FS313.56 BETWEEN DD4 AND DD5 OUT OF LIMITS. REPLACED FRAME REF CRJ900 SRM, AND BOMBARDIER DRAWING. PRESSURE CHECK NOT REQUIRED DUE TO PASSENGER DOOR REPLACED ON CAMP#204SDR SWIA2019020348041Frame · corrodedFRAME 589 HAS CORROSION SPOTS ON THE FWD AND AFT SIDE BETWEEN STGR 22R AND 20R IN THE CARGO BAY BELOW THE FLOOR (C-CHECK) RO 1/28/2020 TRIMED OUT OUTER FLANGE FRAME AND PERFORMED REPAIR IAW CRJ200 SRM T.063 7075-T6 TAG B33959 S1710-1 TAG B13723 MS20420AD5-SDR IPXA2019121650049Frame · damagedINSPECTION TYPE:CSTA 720 UPPER SEGMENT DAMAGEDFRAMED REPAIR STA 720 BETWEEN S-14L TO S-10L P/N 143N1015-56 ACCOMPLISHED PER SRM 53-00-07-2R-1 REPAIR HAS FOLLOW UP INSP ASSIGNED SEE SECTION 2 PG FOR ALL REQUIREMENTSSDR IPXA2019121650048Frame · damagedINSPECTION TYPE:CSTA 740 UPPER FRMAE SEGMENT DAMAGEDFRAME REPAIR AT STA 740 BETWEEN S-14L AND S-9L ACCOMPLISHED IAW 757-200PF SRM REV - 53-00-07-2R1 REPAIR HAS FOLLOW UP INSP REQUIRED NOTE SEE SECTION 2 ENGINEERING BLOCK FOR REQUIREMENTS.SDR IPXA2019121650046Frame · damagedINSPECTION TYPE:CSTA 700 UPPER FRAME SEQMENT DAMAGEDREPAIRED FRAME SEGMENT IAW SRM 53-00-07-2R-1SDR DALA2019121657345Frame · dented(LOG 1403015) DURING INSPECTION FOUND DENT ON FRAME AT STA 1040 AND S-23L. FRAME AT STATION 1040 AND S-23L SEC 48 WAS REPAIRED PER ETI-37-19-359 REV.3 AND ERA 583804-14.SDR DALA2019121657343Frame Angle · corroded(LOG 1402727) DURING INSPECTION FOUND CORROSION ON FRAME CLIP STATION 319 BTW STR 20LH AND 23LH. FRAME CLIP STATION 319 BTW STR 20LH AND 23LH WAS REPLACED PER B737-800 SRM 51-40-02.SDR SWIA2020012147936Frame · cracked*FRAME CRACKED ABOVE PAX DOOR AT FS333 BETWEEN STGR0 AND STGR1L (C-CHECK) RO:1/17/2020 / VERIFIED THE FRAME CRACK. REMOVED FRAME REF CRJ 200 SRM 51-42-06. INSTALLED NEW FRAME SECTOR AT FS333 BETWEEN STGR 0 AND STGR 1L REF DWG AND SRM.SDR REXA2019123011829Frame · corrodedCORROSION WAS FOUND ON THE FRAME AT BS 349, BETWEEN STRINGERS 26 - 27R IN THE MAIN AVIONIC COMPARTMENT. THE CORROSION WAS REMOVED IAW SRM 51-21-06-001-001-A01, AND THE REWORKED AREAS WERE MEASURED AT ORIGINAL THICKNESS 0.050", MAXIMUM DEPTH REMOVED WAS 0.0SDR REXA2019122631762Frame · corrodedCORROSION ON FRAME BS 349 BETWEEN STRINGERS 25L TO 25R IN THE MAIN AVIONICS COMPARTMENT. THE FRAME WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.SDR DALA2019121647347Frame · cracked(LOG 1401906) DURING INSPECTION FOUND CRACK ON FRAME STATION 400 ATTACHING SUPPORT BETWEEN STR 8L AND STR 9L ON LEFT SIDE. FRAME WAS REPAIRED PER ERA 583866-14.SDR DALA2019121547306Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE, DOOR STOP 1 HOLE 3 (LOW/ INB), CRACK AT 8 O CLOCK. ON UPPER FUSELAGE (1 EA). PERFORMED TIME LIMITED REPAIR ON FR 16 LH SIDE DOOR STOP #1 HOLE 3 (LOWER INBOARD) AS PER PRI 583533-14AD REV. 0,1 AND ERA 583533-14AD.SDR DALA2019121307273Frame · crackedHFEC INSPECTION FOUND 01EA CRACK APPROX 0.350" IN LENGTH ON STA 1809 RIGHT FORWARD OUTER CHORD BETWEEN STA 4R AND 5R , ABOUT 1" FROM STR 5R AS MARKED . PER W/C 5310-0138-0202 STEP 6. STA 1809 RIGHT FORWARD CHORD BETWEEN S-4R AND 7R CRACK AREA CUTED OUT AND ERMSDR DALA2019121537304Frame · crackedCRACK INDICATION ON FRAME FR16 RH SIDE, DOOR STOP 7 HOLE 3 (LOW/ INB). CRACK AT 10 O CLOCK ON UPPER FUSELAGE (1 EA). PERFORMED ROTOTEST INSPECTION ON FITTING AND FRAME OF DOOR STOP #7 RH SIDE AND FOUND CRACK INDICATION ONLY IN FITTING AS PER NTM 51-10-01. REPLSDR DALA2019121307292Frame · cracked(LOG 1400191) DURING INSPECTION FOUND CRACK ON FRAME STATION 480 ATTACHING SUPPORT BETWEEN STR 8L AND STR 9L. FRAME WAS REPAIRED PER ER/A 583575-14AD REV.A.SDR DALA2019121307291Frame · cracked(LOG 1400186) DURING INSPECTION FOUND CRACK ON FRAME STATION 400 ATTACHING SUPPORT BETWEEN STR 8R AND STR 9R ON RIGHT SIDE. FRAME WAS REPAIRED PER ER/A 583575-14AD REV.A.SDR DALA2019121307290Frame · cracked(LOG 1400181) DURING INSPECTION FOUND CRACK ON FRAME STATION 400 ATTACHING SUPPORT BETWEEN STR 8L AND STR 9L ON LEFT SIDE. FRAME WAS REPAIRED PER ERA 583575-14AD REV.A.SDR DALA2019121307289Frame · cracked(LOG 1400165) DURING INSPECTION FOUND CRACK ON FRAME STATION 400 ATTACHING SUPPORT BETWEEN STR 8L AND STR 9L ON LEFT SIDE. FRAME WAS REPAIRED PER ER/A 583575-14AD REV.A.SDR DALA2019121307288Frame · cracked(LOG 1400163) DURING INSPECTION FOUND CRACK ON FRAME STATION 500A ATTACHING SUPPORT BETWEEN STR 8L AND STR 9L. FRAME WAS REPAIRED PER ERA 583575-14AD REV.A.SDR DALA2019121327283Frame · cracked(LOG 1398743) DURING INSPECTION CRACK WAS FOUND ON FRAME STATION 500A BTW S-8R AND S-9R AT PAX CABIN. FRAME WAS REPAIRED PER ERA 583575-14AD REV.A.SDR IPXA2019121324925Frame · damagedINSPECTION TYPE:SEGSTA.680 LH MAIN LOWER FRAM SEGMENT HAS A CRACK DUE TO IMPACT DAMAGELOWER FRAME SEGMENT REPAIR AT STA.680 AT STR.16L HAS BEEN COMPLETED IAW UPS EO.NO. B757-5310-74567-A WITH NO DEVIATIONS. THIS REPAIR IS TIME LIMITED TO 42,800 TOTAL AIRCRAFT SDR DALA2019121207257Frame · cracked(LOG 1398756) DURING INSPECTION FOUND CRACK ON FRAME STA= 727B ATTACHING SUPPORT BETWEEN STR 8R AND STR 9R ON RIGHT SIDE. FRAME WAS REPAIRED PER ER/A 583575-14AD REV.A.SDR DALA2019121207256Frame · cracked(LOG 1398737) DURING INSPECTION CRACK WAS FOUND ON FRAME STATION 500A BTW S-8R AND S-9R AT PAX CABIN. CRACK WAS FOUND ON FRAME STA 500A BTW S-8R AND S-9R WAS REPAIRED PER ERA 583575-14.SDR DALA2019121207260Frame · cracked(LOG 1398749) DURING INSPECTION FOUND CRACK WAS FOUND ON FRAME STATION 480 BTW S-8R AND S-9R AT PAX CABIN. FRAME WAS REPAIRED PER ERA 583575-14AD REV.A.SDR SWAA2022040621420Fitting · corrodedPASSENGER CABIN STA 695; BETWEEN STR 16L AND 17L; FWD HALF OF STUB FRAME HAS CORROSION ALONG EDGE OF INNER FLANGE / ACCOMPLISHED BLEND REPAIRS ON FRAME FITTING ASSEMBLY BETWEEN STR 16L AND STR 17L. I.A.W. EA 192544 IR AND SWA EA. 1-753-36234 REV IR BLENDS ACCOSDR SWAA2022040621423Stub Frame · corrodedPASSENGER CABIN STA 695; BETWEEN STR 16R AND 17R; AFT HALF OF STUB FRAME HAS CORROSION ALONG EDGE OF INNER FLANGE / ACCOMPLISHED BLEND REPAIR ON RH LANDING GEAR AFT HALF OF STUB BEAM AT STA 695 BETWEEN STR 16R AND STR 17R IAW EA. 192550 IR AND SWA E.A 1-753-36SDR SWAA2022040621424Flange · corrodedPASSENGER CABIN BS 716; BETWEEN STR 15R TO 17R; STUB FRAME HAS CORROSION ALONG EDGE OF INNER FLANGE. REMOVED CORROSION ALONG EDGE OF INNER FLANGE. EVALUATED MATERIAL LOSS (FWD EDGE) TO BE .057; & (AFT EDGE) LOSS TO BE .057. MAX ALLOWABLE IS .100. SUBFRAME
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