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.

SDR SWIA2020021848590Frame · gouged*RH FRAME (FS761.85) ABOVE SILL HAS A GOUGE. FLAGGED (C-CHECK) RO 2/14/2020 BLENDED OUT THE GOUGE DAMAGE ON RIGHT HAND FRAME FS 761.85 ABOVE SILL. NO DAMAGE ALLOWED ON THE FREE FLANGE OF THE FRAME. REPAIRED FRAME. REF REO. WEIGHT CHANGES ARE NEGLIGABLE, Dec 11, 2019 · N689CA · Cndair CL6002D24SDR SWIA2019020348038Frame · crackedFRAME 333 IS CRACKED AT TOOLING HOLE JUST I/B OF STGR 2L IN THE CABIN (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FRAME SECTION IAW CRJ-200 SRM.Dec 11, 2019 · N900EV · Cndair CL6002B19SDR DALA2019121207255Frame · cracked(LOG 1398246) DURING INSPECTION FOUND CRACK ON LH FRAME STATION 400 BTW STRINGER LH 8 AND STRINGER LH 9 AT PAX CAB. CRACK ON LH FRAME STA 400 WAS REPAIRED PER ERA 583519-14AD REV A.Dec 11, 2019 · N3766 · Boeing 737832SDR DALA2019121207254Frame · cracked(LOG 1397942) DURING INSPECTION FOUND CRACK ON RH FRAME STATION 380 BTW STRINGER RH 8 AND STRINGER RH 9 AT PAX CAB. CRACK ON RH FRAME STATION 380 WAS REPAIRED PER ERA 583519-14AD REV A.Dec 11, 2019 · N3766 · Boeing 737832SDR DALA2019121107221Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE DOOR STOP 7, HOLE 1 (UP/INB ). CRACK AT 4 O CLOCK. ON UPPER FUSELAGE (1 EA). PERFORMED ROTOTEST INSPECTION ON HOLE (UP/INB) OF THE DOOR STOP #7 AS PER NTM 51-10-01 CRACK INDICATION ON INTERCOSTAL LAYER ONLY. THE INTERCOSTALDec 11, 2019 · N346NB · Airbus A319114SDR DALA2019121107220Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE, DOOR STOP 7 HOLE 3 (LOW/ INB), CRACK AT 4 O CLOCK. ON UPPER FUSELAGE (1 EA). PERFORM ROTOTEST INSPECTION ON THE LOWER I/B HOLES TO VERIFY THE AFFECTED LAYER AS PER NTM 51-10-01. THE CRACKS ON THE INTERCOSTAL LAYER ONLY. REDec 11, 2019 · N346NB · Airbus A319114SDR SWAA2022040607476Frame · crackedCRACK IN RADIUS OF THE B.S. 312 FRAME JUST ABOVE FOR WARD ENTRY DOOR CUTOUT. / REPAIRED CRACK IN RADIUS OF THE FRAME OF BS 312; S-5L PER ER 19-06199 REV IR & SWA EA 1-753-36217 REV IR.Dec 10, 2019 · N7828A · Boeing 7377CTSDR SWIA2019123147478Frame · corrodedFRAME 605 IS CORRODED ON BOTH SIDES OF FRAME BETWEEN STR26R AND STR26L (C-CHECK) RO 12/27/2019 REPAIRED FRAME AT FS 605 IAW BOMBARDIER REO.Dec 10, 2019 · N8932C · Cndair CL6002B19SDR SWIA2019123147474Frame · corrodedFRAME 574IS CORRODED ON BOTH SIDES BETWEEN STR26L AND STR25R (C-CHECK) RO 12/27/2019 PERFORMED A MAJOR REPAIR TO FRAME 574 BETWEEN STR26L AND STR25R IAW REO. COMPLETED SKYWEST TASK CARD. FORM M-377 IS ATTACHED.Dec 10, 2019 · N8932C · Cndair CL6002B19SDR SWIA2020013147472Frame · corrodedFRAME 589 IS CORRODED ON BOTH SIDES BETWEEN STR25R AND STR25L (C-CHECK) RO 12/27/2019 REPAIRED FRAME AT FS 589 COMMON TO STRINGERS 25R AND 25 L IAW BOMBARDIER REO.Dec 10, 2019 · N8932C · Cndair CL6002B19SDR SWIA2019020348037Frame · crackedFS605.0 IS CRACKED AT STGRL9 (C-CHECK) RO 1/28/2020 REPAIRED FRAME 605 AT STGR 9L REF REODec 9, 2019 · N900EV · Cndair CL6002B19SDR SWAA2020011440444Frame · crackedFRAME CRACKED AT BS 520, BETWEEN STR 11L TO STR 12L. REPAIRED FRAME IAW SRM.Dec 9, 2019 · N7838A · Boeing 73773VSDR SWIA2020010247541Frame · corrodedFS 605.0 FRAMAE CORRODED BETWEEN STR 21L AND STR 22L (C-CHECK) RO 12/31/2019 BLENDED CORROSION ON FRAME. FOUND CORROSION OUT OF LIMITATIONS IAW CRJ200 SRM. REMOVED FRAME BETWEEN LEFT AND RIGHT FACTORY SPLICES. MATCH DRILLED REPLACEMENTAND INSTALLED WET IAW CDec 9, 2019 · N8968E · Cndair CL6002B19SDR SWAA2019121639645Frame · crackedL/H BODY FAIRING ATTACH FRAME CRACKED AT BS. 520, STR. 20L. / R&R FRAME PER SRM AND DWG.Dec 9, 2019 · N917WN · Boeing 7377H4SDR SWIA2020020348077Frame · corrodedFRAME 319.70 HAS CORROSION SPOTS ON THE FWD SIDE BETWEEN STGR 25L THRU 26R IN THE FWD E&E BAY (C-CHECK) RO 1/28/2020 REMOVED CORROSION IAW CRJ200 SRM. OUT OF LIMITS IAW CRJ200 SRM. WORK TO BE ACCOMPLISHED ON W/O 1018024 1000/0166 SN 7507330.Dec 8, 2019 · N900EV · Cndair CL6002B19SDR SWAA2022041267869Structure · crackedLH AFT AC BAY UPPER CHORD AT STA 663 LBL 10 EVIDENCE OF A CRACK AT FASTENER HOLE (MARKED) / REPAIRED STA 663 UPPER VAPOR BARRIER CHORD AT LBL 10 IAW SRM 57-10-10-2R-5 ACCOMPLISHED LEAK CHECK OF CENTER FUEL TANK FASTENERS IAW AMM 28-11-00-400-801 LEAK CHECK GOODec 7, 2019 · N944WN · Boeing 7377H4SDR SIMA2019121907001Frame · corrodedFRAME AT FS310.00 CORRODED BETWEEN STR 25 LT TO STR 25 RT-C/A-REAPIRED FS310.00 BEWTEEN STR 25LT AND 25RT IAW ERS-CR-53MR-3982.Dec 7, 2019 · N538EG · Cndair CL6002C10SDR DALA2019120987168Frame · cracked(LOG 1391480) DURING INSPECTION FOUND CRACKED FRAME ON STATION 440 BTW S-8R - S-9R AT PASSENGER CABIN. FRAME ON STATION 440 BTW S-8R - S-9R AT PASSENGER CABIN WAS REPAIRED PER ER/A 583347-14AD.Dec 7, 2019 · N3771K · Boeing 737832SDR DALA2019120987167Frame · cracked(LOG 1391469) DURING INSPECTION FOUND CRACKED FRAME ON STATION 400 BTW S-8R - S-9R AT PASSENGER CABIN. FRAME ON STATION 400 BTW S-8R - S-9R AT PASSENGER CABIN WAS REPAIRED PER ER/A 583347-14AD.Dec 7, 2019 · N3771K · Boeing 737832SDR SWAA2022040733384Intercostal · crackedPASSENGER CABIN FWD WET AREA BETWEEN STA 312 AND 328 LBL 44.50 INTERCOSTAL IS CRACKED AS MARKED / REPLACED NEW INTERCOSTAL FROM STA 312 TO 328; LBL 44.5 I.A.W. SRM 51-40-02-0G & BOEING DWG # 141A5400 TY:DWG ID:0026 REV:-Dec 6, 2019 · N8306H · Boeing 7378H4SDR SWAA2022040733388Intercostal · crackedPASSENGER CABIN FWD WET AREA BETWEEN STA 277 AND 294.5 RBL 01 FLOOR STRUCTURE INTERCOSTAL IS CRACKED AS MARKED / REMOVED CRACKED INTERCOASTAL AT MAIN CABIN BETWEEN STA 277 AND 294.5 RBL 1 I.A.W SRM 51-40-02-0G-0. DRILLED NEW INTERCOSTAL I.A.W SRM 51-40-05-0G-0Dec 6, 2019 · N8306H · Boeing 7378H4SDR QMLA2019120619094Frame · chafedCHAFFING DAMAGE TO EXTERNAL L/H X FRAME BULKHEAD FROM THE BAGGAGE COMPARTMENT TRIM PANELS AS WELL AS CHAFFING DAMAGE TO THE INTERNAL X FRAME FROM THE T/R CONTROL CABLE. ** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION. **Dec 6, 2019 · N267AM · Snias AS350B3SDR C77A20200229037Frame · corrodedEMBRAER HAS RECEIVED REPORTS ABOUT CORROSION ON THE WING-TO-FUSELAGE FAIRING ATTACHMENT (STRAP AND RIB) AT FRAME 45. INVESTIGATION HAS REVEALED THAT WATER ACCUMULATION IN THE WING-TO-FUSELAGE FAIRING REGION IS CAUSING THE CORROSION. THIS ISSUE IS USUALLY FOUDec 5, 2019 · N621CZ · Emb ERJ170200LRSDR SWIA2020021848577Frame · corroded* FS 517.00 FRAME CORRODED NEAR STGR 19R (C-CHECK) RO 2/14/2020 NO DAMAGE ALLOWED TO FS517 NEAR STR 19R, PERFORMED FRAME SPLICE REPAIR TO FS517 FROM STR 16R-20R REF CRJ 900 SRM LEAK CK GOOD. SEE CONTINUATION CARD FOR DETAILS. COMPLETED M-337Dec 5, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848576Frame · corroded* FS 501.00 FRAME CORRODED NEAR STGR 20R. (C-CHECK) RO 2/14/2020 CORROSION AT FS501 NEAR STR 20R IS IN A NO DAMAGE ALLOWED AREA. PERFORMED FRAME SPLICE REPAIR TO FS501.00 FROM STR AND BOMBARDIER DWG. LEAK CK GOOD. SEE CONTINUATION CARD FOR DETAIS. COMPLETDec 5, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848559Frame · corroded* FS 549.00 FRAME HAS CORROSION NEAR STGR 19R. (C-CHECK) RO 2/14/2020 FOUND CORROSION TO BE OUT OF LIMITS ON FS549.00 FRAME NEAR STGR 19R. REMOVED AND INSTALLED NEW FS549.00 FRAME SECTIONS FROM STR 16R TO STR 21R WITH A SPLICE AT STR 16R REF DWG, CRJ900 SDec 5, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848558Frame · corroded* FS 645.00 FRAME HAS CORROSION NEAR STGR 19R. (C-CHECK) RO 2/14/2020 FOUND CORROSION ON FS645.00 FRAME AT STR 19R TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW SECTION OF FRAME AT FS645.00 BETWEEN STR 16R TO STR 21R REF DWG, CRJ900 SRM AND REO. PRESSUREDec 5, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848556Frame · corroded* FS 661.00 + 16 FRAME HAS CORROSION NEAR STGR 19R. (C-CHECK) RO 2/14/2020 INSTALLED REPLACEMENT FRAME SECTION, FRAME SPLICE AND NEW STR 16R CLEAT AT FS661.00+16.00 FROM STR 16 TO STR 20 REF CRJ 900 SRM, REO AND BOMBARDIER DRWG. COMPLETED FORM M-337. ALL Dec 5, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848555Frame · corroded* FS 661.00 + 32 FRAME HAS CORROSION NEAR STGR 19R. (C-CHECK) RO 2/14/2020 INSTALLED REPLACEMENT FRAME SECTION, FRAME SPLICE AND NEW STR 16R CLEAT AT FS661.00+32.00 FROM STR 16 TO STR 20 REF CRJ 900 SRM, REO AND BOMBARDIER DRWG. ALL CHECKS GOOD.Dec 5, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848546Frame · crackedOUT OF SCOPE: FS333.00 FRAME CRACKED BETWEEN STR1R AND STR2R. (C-CHECK) RO 2/14/2020 REPLACED FS333.00 FRAME BETWEEN STR1R AND STR9R REF CRJ900 SRM, AND BOMBARDIER DRAWING. COMPLETED FORM FORM M-337. LEAKS AND OPS CHECK GOOD. SEE CONTIUATION CARD FOR DETADec 5, 2019 · N689CA · Cndair CL6002D24SDR CALA2019120762149Frame · damagedAFT CARGO DOOR AFT CUTOUT LATERAL FRAME AT FR 59 STR38R, STR 39R & STR 40R TOTAL 3 LOCATIONS. AFT CARGO DOOR AFT CUTOUT LATERAL FRAME AT FR 59 STR38R, 39R, 40 R REPAIRED AS PER ECRA 5311-02327 PART INTERIM REPAIR.FOR CORROS ION DAMAGE AND REQUIRES RE-INSPECTIODec 5, 2019 · N878UA · Airbus A319132SDR SWIA2020021848622Frame · corroded* THE FRAME AT FS295.00 AND STRG 19R HAS CORROSION. (C-CHECK) RO 2/14/2020 REMOVED CORROSION FROM DISCREPANT AREA OF FRAME AT FS295 AND STR19R REF. CRJ900 SRM, FOUND TO BE OUT OF LIMITS REF. CRJ900 SRM, REPAIRED FRAME REF. BOMBARDIER REO. ALL STEPS 1 THRODec 4, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848533Frame · corroded*CORROSION FOUND ON FRAME IN BELLY AT FS 597 BETWEEN STGR 24L AND STGR 24R. (C-CHECK) RO 2/14/2020 BLENDED CORROSION ON FRAME IN BELLY AT FS 597 BETWEEN STGR 24L AND STGR 24R REF CRJ-900 SRM. ORIGINAL MATERIAL THICKESS WAS 0.63", MATERIAL REMAINING IS 0.5Dec 4, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848532Frame · corroded*CORROSION FOUND ON FRAME IN BELLY AT FS 581 BETWEEN STGR 24L AND STGR 26R. (C-CHECK) RO 2/14/2020 REMOVED/BLENDED CORROSION FROM FRAME FLANGE AND VERTICLE WEB ON FRAME AT .F.S.581 BETWEEN STR 24L AND 26R.REF: CRJ-900 S.R.M. ORIGINAL THICKNESS: 0.063" REMADec 4, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848530Frame · corroded*CORROSION FOUND ON FRAME IN BELLY AT FS 469 BETWEEN STGR 26L AND STGR 27. (C-CHECK) RO 2/14/2020 BLENDED CORROSION ON FRAME IN BELLY AT FS 469 BETWEEN STGR 26L AND STGR 27 REF CRJ-900 SRM. ORIGINAL THICKNESS 0.050" REMAINIG THICKNESS IS 0.048" MAX MATERIDec 4, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848525Frame · corroded* FS 942.00 FRAME CORRODED BETWEEN STGR 22L AND 23R. (C-CHECK) RO 2/14/2020 REMOVED AND INSTALLED NEW FS 942.00 STGR 22L AND 23R. FRAME SECTOR QTY 3. INSTALLED QTY 2 NEW FRAME SPLICES, INSTALLED QTY 2 NEW CLIPS IAW CRJ 900 SRM AND BOMBARDIER REO AND BOMBARDec 4, 2019 · N689CA · Cndair CL6002D24SDR SWIA2020021848524Frame · corroded* FS 927.00 FRAME CORRODED BETWEEN STGR 22L AND 24R. (C-CHECK) RO 2/14/2020 PERFORMED SPLICE REPAIR TO LOWER FRAME SECTOR FOR FS927 REF CRJ 900 SRM. SEE CONTINUATION CARD FOR DETAILS. COMPLETED FORM M-337.Dec 4, 2019 · N689CA · Cndair CL6002D24SDR CALA2019120762144Frame · gouged(B757-53-3-0577) MAIN CABIN STA 1280 RH FRAME HAS MULTIPLE GOUGE S FROM STR 9R - STR 15R. REF ST-SAA NR 0077827. BLENDED AND CHECK LIMITS TO 5EA GOUGES ON FRAME AT STA 1280 FROM S-9R TO S-15R, 2 AREAS IN LIMITS AND 3 AREAS OUT OF LIMITS IAW ''S OF FRAME IAW ECDec 4, 2019 · N75851 · Boeing 757324SDR DALA2019120507091Frame · cracked(LOG 1387382) DURING INSPECTION FOUND CRACK ON FRAME STA 727B BTW STR 8/9LH AT PAX CABIN. FRAME STA 727B BTW STR 8/9LH AT PAX CABIN WAS REPAIRED PER ER/A 583347-14 AD.Dec 4, 2019 · N3771K · Boeing 737832SDR DALA2019120507090Frame · cracked(LOG 1387364) DURING INSPECTION FOUND CRACK ON FRAME STATION 480 BTW STR 8/9LH AT PAX CABIN. FRAME STATION 480 BTW STR 8/9LH AT PAX CABIN WAS REPAIRED PER ER/A 583347-14 AD.Dec 4, 2019 · N3771K · Boeing 737832SDR DALA2019120507089Frame · cracked(LOG 1387338) DURING INSPECTION FOUND CRACK ON FRAME STATION 380 BTW STR 8/9LH AT PAX CABIN. FRAME STATION 380 BTW STR 8/9LH AT PAX CABIN WAS REPAIRED PER ER/A 583347-14 AD.Dec 4, 2019 · N3771K · Boeing 737832SDR DALA2019120507088Frame · cracked(LOG 1387331) DURING INSPECTION FOUND CRACK ON FRAME STATION 440 BTW STR 8/9LH AT PAX CABIN. FRAME STATION 440 BTW STR 8/9LH AT PAX CABIN WAS REPAIRED PER ER/A 583347-14 AD.Dec 4, 2019 · N3771K · Boeing 737832SDR DALA2019120507087Frame · cracked(LOG 1387324) DURING INSPECTION FOUND CRACK ON FRAME STA 500C BTW STR 8/9LH AT PAX CABIN. FRAME STATION 500C BTW STR 8/9LH AT PAX CABIN WAS REPAIRED PER ER/A 583347-14 AD.Dec 4, 2019 · N3771K · Boeing 737832SDR DALA2019120507086Frame · cracked(LOG 1387322) DURING INSPECTION FOUND CRACK ON FRAME STA 400 BTW STR 8/9LH AT PAX CABIN. FRAME STA 400 BTW STR 8/9LH AT PAX CABIN WAS REPAIRED PER ERA 583347-14 AD.Dec 4, 2019 · N3771K · Boeing 737832SDR SWAA2019121639621Frame · crackedFRAME CRACKED AT BS. 787, STR. 8R. / REPAIRED FRAME IAW EA.Dec 3, 2019 · N7866A · Boeing 7377Q8SDR SWIA2020021848511Frame · corroded*EXTERNAL FORWARD FUSELAGE - FS661.00+62.00 (ENCLOSED BY WING-TO-FUSELAGE FAIRINGS) FRAME END CAP HAS MULTABLE AREA'S OF CORROSION. FLAGGED (C-CHECK) RO 2/14/2020 REPLACED THE SPLICE PLATE JOINT (END CAP) WITH A SERVICABLE SPLICE PLATE JOINT REFERENCING BDec 2, 2019 · N689CA · Cndair CL6002D24SDR SWIA2019122747217Frame · corrodedEVIDENCE OF CORROSION ON AFT SIDE OF RT BS 379 FRAME STRINGER 20R. BLENDED OUT THE CORROSION AND PERFORMED A REPAIRED IAW REO. LEAK CHECKED GOOD.Dec 2, 2019 · N745SK · Cndair CL6002C10SDR DALA2019120637126Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 9 INCH OB FROM -Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV.ORIGINAL AND PRI 582610-14 REV.0 TO 9Dec 2, 2019 · N331NW · Airbus A320211SDR DALA2019120637125Frame · crackedCRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 12.500 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK . (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PR ESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PDec 2, 2019 · N331NW · Airbus A320211SDR DALA2019120637124Frame · crackedCRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 11.325 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK . (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PR ESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PDec 2, 2019 · N331NW · Airbus A320211
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