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 DALA2019120637123Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 9 INCH OB FROM +Y1292, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), REPAIR PER ER/A 00-582610SDR DALA2019120637121Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 5.2 INCH OB FROM -Y1292, CRACK DIRECTION IS 6 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), PERFORMED SECTION 1 AS REPAIR AS PER ERA 582610-14AD REV. ORIGINAL AND PRI 58210-14 REV. 0 TO 9 SECSDR DALA2019120637120Frame · crackedCRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 8.750 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK. (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PRE SSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PERSDR DALA2019120637119Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 3.2 INCH OB FROM +Y1292, CRACK DIRECTION ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV. ORIGINAL AND PRI 582610-14 REV. 0 TO 9SDR DALA2019120637118Frame · crackedCRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL AREA AND 15.250 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, REPSDR DALA2019120637117Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 5.2 INCH OB FROM +Y1292, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV. ORIGINAL AND PRI 582610-14 REV 0 TO 9 SECSDR DALA2019120637116Frame · crackedCRACK INDICATION ON FRAME 36 ON PRESSURE PANEL AREA AND 17.625 INCHES APPROX. INBOARD POSITION FROM Y +1292.0 ( CRACK DIRECTIONS 7 & 1 OCLOC K, 2 EA IN THE SAME HOLE) IN FWD CARGO COMPARTMENT (1 EA) (A CRACK TH AT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND ASDR SWAA2019121839804Frame · corrodedFRAME CORRODED AT BS. 867, BETWEEN LBL 22 TO LBL 33. / REPAIRED FRAME PER SRM, ER, AND EA.SDR R61A2019121431370Frame · corroded***AIRCRAFT IN HEAVY CHECK***AFT CARGO COMPT., FR 82 LOWER FLANGE CORRODED BTW STR 28-29R. REPLACED LOWER FLANGE IAW SRM 51-41-01 AND 51-41-02***AIRCRAFT REMAINS IN HEAVY CHECK***SDR VNAA2019112999902Frame · corrodedCORRECTED ID NUMBER. FWD PAX DOOR FWD FRAME AT FS 311.75 IS CORRODED ON BOTH SIDES. REMOVED FWD FRAME PAX DOOR @ 311.75 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW PAX DOOR FWD FORMER IAW CRJ 700 SRM 51-42-06-21-001-001-A01 REV 37 AUG 15,2019. LOCATED SDR CALA2019120302118Frame · dentedB757-53-3-0492 DENT ON FWD CARGO FRAME UPPER FLANGE AT STA 580 B ETWEEN STR 23L AND 24L, RG1. REF ST-ENG N/R 0077707 CHECKED LIMITS TO DENT ON FRAME AT STA 580 BETWEEN S-23L AND S-2 4L; L-1.0", W=1.10" D=.025". OUT OF LIMITS IAW B757-300 ARM 53-0 0-07 AD1, FIGSDR CALA2019120302119Frame · dented(B757-53-3-0492) DENT ON FWD CARGO FRAME UPPER FLANGE AT STA 520 BETWEEN STR 24L - 25L. REF ST-SAA NR 0077708. CHECKED LIMITS TO DENT ON FRAME UPPER FLANGE AT STA 520 BETWEEN S24L AND S-25L; L=1.4", W=.80", D=.020". OUT OF LIMITS IAW B757- 300 SRM 53-00-07 AD1SDR SWAA2020010340153Frame · crackedFRAME CRACKED AT BS. 360 BETWEEN STR. 7R TO STR. 10R. / REPAIRED FRAME IAW EA.SDR SWAA2019123140089Frame · crackedFRAME CRACKED AT BS. 440, BETWEEN STR. 8R TO STR. 9R. / REPAIRED FRAME IAW EA.SDR SWIA2019122747343Frame · crackedBS 235 FRAME HAD A CRACK INDICATION NOTED IN THE I/B RADIUS AT STINGGER 13L. 0.130" LONG. FAILED NDT. REMOVED, LOCATED, DRILLED , AND INSTALLED NEW FRAME IAW SRM.SDR SWIA2019122647123Frame · corrodedTHE FRAME AT BS 589 FROM STRINGERS 20L TO 17L HAD CORROSION AT MULTIPLE AREAS. REMOVED CORROSION IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS IAW SRM. RESTORED FINISH IAW SRM. . PRESSURE CHECKED GOOD.SDR SWIA2019122647122Frame · corrodedTHE FRAME AT BS 589 FROM STRINGERS 24R TO 20L HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND REPLACED THE FRAME IAW SRM. PRESSURE CHECKED GOOD,SDR SWIA2019122647121Frame · corrodedTHE FRAME AT BS 589 FROM STRINGERS 17R TO 19R HAD CORROSION. REMOVED CORROSION IAW SRM. MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM. RESTORED FINISH AND CIC.SDR SWIA2019122647120Frame · corrodedTHE FRAME AT BS 605 FROM STRINGERS 20L TO 17L HAD CORROSION. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. LEAK CHECKED GOOD.SDR SWIA2019122647119Frame · corrodedTHE FRAME AT BS 605 FROM STRINGERS 25R TO 20L HAD CORROSION AT MULTIPLE LOCATIONS. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. . LEAK CHECKED GOOD.SDR SWIA2019122647116Frame · corrodedTHE FRAME AT FS 574.00 FROM STRINGER 24L TO 25R HAS CORROSION. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. OPS CHECKED GOOD.SDR SWIA2019122647115Frame · corroded* THE FRAME AT FS 574.00 FROM STRINGER 17L TO 18L HAS CORROSION. (C-CHECK) RO 12/23/2019 REMOVED CORROSION FROM FS 574.00 FRAME BETWEEN STRINGER 17L AND18L AND RESTORED FINISH. REF CRJ200 SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. SEE CONTINUE CARD SDR SWAA2019122339862Frame · crackedFRAME CRACKED AT BS. 867, BETWEEN STR. 8R TO STR. 9R. REPAIRED FRAME IAW SRM.SDR SIMA201912126006Frame · corrodedFRAME AT FS295.00 BETWEEN STRINGERS 26 LEFT TO 26 RIGHT IS CORRODED.-C/A-REPAIRED FRAME AT FS295.00 IAW CRJ SRM CH. 53-00-06-201-006.SDR DALA2019120276978Frame · crackedCRACKED FRAME BS 1580, STRINGERS 8R AND 9R. REPAIRED THE FRAME IAW SRM 53-00-07, REPAIR 8, PAR 4, DETAIL II.SDR DALA2019112505470Frame · crackedSHIP 3264 WHILE INSPECTING PER JIC 5311-2036 (ALI 53-11-53) A CRACK INDICATION FOUN IN HOLE #6 OF FR16 RHS PER NTM 53-11-53-250-801. CORRECTIVE ACTION: FRAME 16 R/H WAS REPLACED AND IS DOCUMENTED ON DELTA WORKCARD 17/220 AND ER/A 583103-14AD REV A. (1375408)SDR N6WA20191127504Floorbeam · damagedLH SIDE FS280.00 BEAM DAMAGED.COMPLEATED INSTALL OF RH SIDE FS280.00 BEAM IAW E.O.
C700-53MR-011-OSDR REXA2019112651707Frame · corroded"INITIAL INSPECTION : CORROSION ON FRAME FS295 BTW STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09)
"SUMMARY: ON NRC. 00189, CORROSION LEVEL 2. FRAME FS295 BTW STGR 25LH O 25RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA NO. CRJ953-098SDR SWIA2019112646796Frame · crackedF.S. 220.00, LH UPPER FRAME SECTOR IS CRACKED. (C-CHECK) RO: 11/24/2019 REMOVED AND INSTALLED NEW LH COCKPIT FRAME SECTOR P/N CC670-34146-5 AT FS220.0 IAW SRM. COMPLIED WITH SKY CARD AND SWA M-337. LEAK CHECK GOODSDR CALA2019112862076Frame · dentedB757-06-3-0230 DENT ON FWD CARGO LH FRAME UPPER FLANGE AT STA 68 0 BETWEEN STR 24L-25L. RG35. REF ST ENGINEERING. N/R 0080866 CHECKED LIMITS TO DENT ON FWD CARGO LH FRAME UPPER FLANGE AT STA 680 BETWEEN 24L AND 25L; L=1.36", W=1.0", D=.038". OUT OF LIMI TS ISDR CALA2019112862075Frame · dentedB757-06-3-0230 DENT ON FWD CARGO LH FRAME UPPER FLANGE AT STA 70 0 BETWEEN STR 22L-23L. REF ST ENGINEERING N/R 0080867 CHECKED LIMITS TO DENT ON FWD CARGO LH FRAME UPPER FLANGE AT STA 700 BETWEEN S-22L-23L; L=1.49", W=1.0", D=.040".OUT OF LIMITS I AW B757-200 SDR REXA2019112631706Frame · corroded"INITIAL INSPECTION : CORROSION ON FRAME FS310 BTW STGR 24LH TO 25RH AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09)
"SUMMARY OF NRC 00188: |CORROSION LEVEL 2| FRAME FS 310 BTW STGR 24LH TO 25RH WAS REPAIRED PER REO 690-53-21-1169 REVSDR SWAA2022032461336Frame · crackedSUPPLEMENTAL INFORMATION: FOUND CRACK AT FRAME STRUCTURE STA 312 AT L1 DOOR UPPER SILL BETWEEN STRINGER 5L AND STRINGER 6L . / PERFORMED HFEC AT L1 DOOR UPPER SILL BETWEEN STR 5L AND STR 6L VERIFIED CRACK. TRIMMED OUT FRAME AND REMOVED DAMAGE. PERFORMED HFEC OSDR DSCR201911293161Flange · crackedRH SIDE FRAME 5 STATION 4735 AFT 90 DEGREE FLANGE P/N L533M1105218 IS CRACKED AT Z2200 LOCATION.SDR REXA2019112521710Frame · corroded"AWR, MPEDV [IN REF NRC 00189]: FRAME FS295 BTW STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. ( E/E ).
""SUMMARY : REPAIR PARTS WERE FABRICATED PER EA CRJ953-09882 REV. IR
"SDR REXA2019112621705Frame · corroded"INITIAL INSPECTION : CORROSION ON FRAME FS364 FWD ATTACHED FLANGE BTWSTGR 26RH TO 27 AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09)
"COMPLETE: SUMMARY: ON NRC: 00166, CORROSION LEVEL 2. FRAME FS364 BTW STGR 26RH TO 27 AT MAIN AVIONICS COMPARTMENT WAS RSDR REXA2019112621704Frame · corroded"INITIAL INSPECTION : CORROSION ON FRAME FS333 BTW STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT ( E/E ) (TCI 100-09)
"
"SUMMARY: ON NRC. 00165, CORROSION LEVEL 2. FRAME FS333 BTW STGR 25LHTO 25RH AT MAIN AVIONICS COMPARTMENTWAS REPAIRED PER EA NO. CRJ9SDR SWIA2019122747152Frame · corrodedFRAME AT FS549.00 AT STGR 18LH HAS CORROSION. (C-CHECK) RO 12/24/2019 REPAIRED CORROSION ON FRAME FS549.00 AT STGR18LH, REF BOMBARDIER DWG. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRITY. LEAK CHECK PERFORMED AND LEAK CHECK GOOD. SEE CONTINUATION CARD FOR FSDR CALA2019112542053Frame · crackedREFERENCE AAR DLH N/R 9031163 & 9031164, ROTO PROBE INSPECTION S HOWS CRACK INDICATION AT DOUBLE JOGGLE, RH SIDE, FRAME 16 AT DOO R STOP #7, HOLES 4 AND B ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5311-02316 ON HOL ES 4 AND B AT RH FRAME 16 DOOR STOP #7 DSDR SWIA2020010947561Frame · crackedSUSPECT CRACK FOUND ON LOWER FRAME FLANGE AT FS605.00 AND O/B OF STGR 24L. (MARKED) (C-CHECK) RO 01/07/2020 REMOVED AND REPLACED FRAME AT FS605.00 P/N 601R36026-27R. PER BOMBARDIER DWG 601R36026 REV AF AND REF CRJ200 SRM. NO LEAKS NOTED. COMPLIED WITH SKYWESSDR SWIA2019122747333Frame · crackedLH FS 220.00 UPPER FRAME SECTOR HAS A VISUAL CRACK BTWEEN STR 13L & STR 14L. REMOVED, LOCATED AND DRILLED UP TO SIZE, INSTALLED L/H 220 FRAME IAW SRM.SDR SWIA2019122747224Frame · corrodedFRAME BS 349 WAS CORRODED, STRINGERS 26L & 26R. REMOVED AND REPLACED THE FRAME IAW DWG, AND SRM.SDR SWIA2019122747223Frame · corrodedFRAME AT BS 333 WAS CORRODED ON THE FORWARD & AFT WEB AND LOWER FLANGE STRINGER 25R TO 26L. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, AND DWGS 601R31111 REV E, 601R31022 REV B, AND 601R32004 REV N.SDR SWAA2019122639907Frame · crackedFRAME WEB CRACKED AT BS. 360, BETWEEN STR. 6R TO STR. 9R. REPAIRED WEB PER EO AND EA.SDR SWAA2019122639906Frame · crackedFRAME WEB CRACKED AT BS. 360, BETWEEN STR. 7L TO STR. 9L. / REPAIRED WEB PER EO AND EA.SDR U2RA2019122000001Frame · corrodedCORROSION BEYOND LIMITS, COMMON TO THE FUSELAGE BODY STATION 263 NOSE WHEEL WELL BULKHEAD OUTBOARD CHORD VERTICAL FLANGE, BETWEEN LEFT BUTT LINE 10.6 TO LEFT BUTT LINE 18.8 - ACCOMPLISHED MAJOR REPAIR TO BLEND DAMAGE IN ACCORDANCE WITH BOEING SERVICE REQUEST ISDR SWAA2019121639642Frame · crackedMAIN CABIN TOP OF L1 DOOR CUTOUT FRAME EDGE CRACKED AT BS. 312, STR. 5L. / REPAIRED FRAME PER EA.SDR DALA2019121607315Frame · 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. C/W 53-80-01. STA 1809 RIGHT FORWARD CHORD BETWEEN S-4R AND 7R CRACK AREA CUTED OUT AND ERMOVED AS PER B767-4SDR CALA2019112542046Frame · damagedDURING L/H FR35 INSPECTION PER EA 5330-05216 FOUND NUMEROUS HOLES HAD DEFECTS REPAIRED IN ACCORDANCE WITH ECRA 5331-02514 PLACED ON DIP TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5331-02514 ON OR BEFORE 18 MAY 2020. PLANNING TO CONTACT ENGINEERING AFTSDR SWIA2020010947586Frame · corrodedAVIONICS BAY FS310.00 FWD AND AFT SIDE FRAME CORRODED BETWEEN STGR25L - STGR25R, MARKED (C-CHECK) RO 01/07/2020 BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW LOWER FRAME SECTOR FS310.00 REF CRJ-200 SRM AND BOMBARDIER. COMPLIED WITH TASK CARD.
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