JASC 5311
Service difficulty reports · 61,540
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 SWIA202264067None · dentedEVALUATE AND REPAIR IF NECESSARY DENT ON ADM N291SY7481 (C-CHECK RO 1/22/2022) PERFORMED SKIN DOUBLER REPAIR AT FRAME 97, STRINGER 28R. REF ERJ 175 SRM 53-30-01/REPAIR 12. SEE CONTINUTAION CARD FOR WORK PERFORMEDSDR SWIA202264879None · crackedLEFT WINDSHIELD LOWER OB SIDEPOST FITTING IS CRACKED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LEFT WINDSHIELD LOWER O/B SIDEPOST FITTING IAW CRJ200 SRM 51-40-11 AND 51-42-21.SDR DALA2022011000157None · none(LOG 2077536) DURING INSPECTION FOUND CORROSION ON WEB WAS FOUND DURING REMOVAL OF SCUFF PLATE OF AFTER CARGO COMPARTMENT BTW STA 807 TO STA 840. CORROSION ON DOOR SILL WEB OF AFTER CARGO COMPARTMENT BTW STA 807 TO STA 840 WAS REPAIRED PER ETI-37-21-554 REV. 1SDR CALA2022010700060Frame · corrodedFWD CARGO FR33 STR40L-STR41L HAS CORRODED CLEAT REMOVED AND REPLACED CLEAT AT FR33 STR40L-STR41L IAW ARM 51-75-1 2-911-001 ADD EMP:V052030SDR CALA2022010700056Frame · crackedL/H FR35 STR 30 HOLES #2 HAS CRACK INDACTIONS AT THE 5:00, 6:00, AND 11:00 POSITIONS CONTACT ENGINEERING FOR REPAIR INSTRUCTION BEFORE NEXT FLIGHT. FOR A REFERENCE FOR #2 HOLE. FINIAL HOLE SIZE .250". ACCOMPLISH OF THE REVISION OF ECRA 5331-02825 ON OR BEFORE SDR DALA2022010600103None · noneSHIP 3261 AFT MAIN CABIN PAX DOOR SILL SHAPE SILL FRAME 66-68 STR 23LH HAS CORROSION. CORRECTIVE ACTION: R/R PER A320 SRM 51-42-11. (2076797)SDR YENA2022031400192Window Post · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.250 INCH APPROX IN COCKPIT (1EA); REMOVED AND REPLACED CONTINUITY FITTING RH (1E/A) AND FASTENERS LOC. BTW FR1 TO FR2 WISDR YENA2022031400185Tie Clip · corrodedDURING HEAVY MAINTENANCE, CORROSION INTERNAL STRUCTURE TIE CLIP LOCATED AT FR 32 AND BTW STR 41R AND 42R IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED TIE CLIP IAW A32O SRM 51-72-11-911-001 AND DWG D53232982SDR AALA202201077233None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME CLIP AT FR 28 BETWEEN S43R AND S44. REPLACED CLIP PER SRM 41-42-11.SDR CALA2022010700037Frame · crackedLH SIDE FRAME 68 AT STR 22 INNER CAP AND WEB FLANGE IS CRACKED. CRACK LOCATED ABOVE THE LOWER MOUNT HOLES OF THE #1 DOOR STOP, A FT SIDE, IN AND ABOVE RADIUS. CRACK APPROX 2.25" WITH ENDS MARKE D IN BLACK. L2 DOOR DRAME 68 DOOR STOP FITTING #1 LOWER I/B HOLE ISDR CALA2022010700036Frame · crackedL/H FR35 STR30L HOLE #2 HAS CRACK AT THE 5:00, 6:00, AND 11:00 P OSITIONS. HOLE #3 HAS CRACK INDICATIONS AT 2:00, 3:00, AND 4:00. #1 HAS CRACK INDICATIONS AT 5:30 AND 6:30 POSITIONS. PER HAECO LCQ NR 9294149/22149, 9294150/22150, 9294148/22148. GENERATED BY V0SDR DALA2022010600099None · noneSHIP 3255 NEED TO REPLACE FR43 R/H FRAME FOOT COUPLING. MAJOR REPAIR. CORRECTIVE ACTION: REPLACED IN ACCORDANCE WITH AIRBUS REPAIR DRAWING R533-70232 AND AA TASK CARD 5311-01239-02B. (2076200)SDR DALA2022011000177None · noneSHIP 6813 CORROSION ON UPPER CUTOUT BTW STA 1640 AND 1680 AT 4RH PASSENGER DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00030. AREA WAS REPAIRED PER ETI-57-21-620 REV 1 AND ER/A 596413-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (2075288)SDR DALA2022010700145None · noneSHIP 670 DURING VIASAT MOD IN VQQ, MTC REPORTED INTERFERENCE BETWEEN DUCT SPUDS/HOSE ASSEMBLIES AND VIASAT INTERCOSTALS BETWEEN STA1240-STA 1260; AND STA 1260-STA 1280 (BOTH LH & RH SIDE). CORRECTIVE ACTION: REF ERA 596391-14. (2074940)SDR V0XD20220113001Splice Angle · corrodedCORROSION ON SPLICE ANGLE ON RIB STA. FS939 BETWEEN SRT 26R -26L- CORROSION OUT OF LIMITS REMOVED AND REPLACED PART IAW CRJ SRM 51-40-11, 51-42-06SDR DALA2022010700138None · noneSHIP 670 ECS BAY STA 900 RBL 6 FRAME CORRODED. DOT 39-073. CORRECTIVE ACTION: CLEANED AND EVALUATED AREA, FOUND TO BE OUT OF LIMIT IAW B757 SRM 53-30-71. REMOVED, LOCATED, DRILLED AND INSTALLED NEW CHORD AT ECS BAY STA.900 RBL80 TO LBL 80 IAW BOEING DWG# 1 REVSDR AALA202201042640Frame · noneAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LATERAL WINDOW RIGHT HAND UPPER FRAME BETWEEN FR 4 AND FR 8 REQUIRES REPLACEMENT PER EO 5319Y017-004 AND EA 332235 REQUIREMENTS. REPLACED FRAME PER EO 5319Y017-004 AND EA 332235.SDR MASA20220103006None · noneTHE FUSELAGE FRAME WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-21-06 AND 51-12-00 AND 51-21-16, SRM 51-21-11. DEFECT LOCATION: FS 1088.20 BETWEEN STGR. 26R-26LSDR SWIA202264517None · corrodedCORROSION FOUND ON FRAME SECTOR AT FS379.00 BETWEEN STGR 22R AND STGR 23R. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW FRAME SECTOR AT FS379.00 BETWEEN STGR 25R AND STGR 20R. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32050 REV J. COMPLIED WITSDR DALA2022010300017None · noneSHIP 3248 CRACK INDICATION ON FRAME 68 LH DOOR STOP FITTING HOLE 1. CORRECTIVE ACTION: REPAIRED PER ER/A 596000-14AD REV. ORIGINAL. (2072462)SDR VNAA202201029991Frame · corrodedFRAME AT FS310 IS CORRODED FROM STR 24L TO 26RSDR SWIA202164633None · corrodedUPPER SURFACE OF LONGITUDINAL FLOORBEAM AT FS1016 - FS1047 LBL27 HAS CORROSION. (C CHECK RO 02/22/2022) REPAIRED FLOORBEAM AT APPROXIMATELY FS1016-FS1047 LBL 27 REF. CRJ-700 SRM 53-00-41-201-001-A01. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY. SEE CONSDR DALA2022010300012None · noneSHIP 3248 CRACK INDICATION FOUND IN OPEN HOLE (H2) ON CROSSBEAM SPLICING AREA AT FRAME 16 LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 595688-14AD REV ORIGINAL. (2070932)SDR DALA2022010300011None · noneSHIP 3248 CRACK INDICATION FOUND ON HOLE #8 LOC. REAR EMERGENCY EXIT DOOR CUTOUT EXTERNAL FUSELAGE LH STR20 BTW FR40 AND FR41. CORRECTIVE ACTION: COMPLIED WITH PRI 595702-14AD. (2070925)SDR CALA2022010300005Frame · crackedL/H FR68 DOOR STOP #1 LOWER I/B HOLE HAS A CRACK INDICATION SUPP ORT TASK: AD 2018-03-12. PER HAECO LCQ N/R 9294109/ 32109 GENERA TED BY V061632. "B", REAMED TO .506" INSTALLED FREEZE PLUG REAMED TO .281"BOLT S CTION THRESHOLD FROM THE TIME OF ADL/REPAIR EMBODSDR SWIA202164513None · corrodedFRAME AT FS319.70 LH BETWEEN STGR18L AND 21L CORRODED. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW REPLACEMENT FRAME AT FS319.70 BETWEEN STGR18L AND 21L USING ALL NEW FASTENERS. REF BOMBARDIER DWG# SH670-31810 REV AE AND CRJ700 SRM 51-42-21-001-001-ASDR DALA2022010308202None · noneSHIP 3248 CRACK INDICATION ON FRAME 16 LH DOUBLE JOGGLE AREA HOLE C IN COCKPIT. CORRECTIVE ACTION: REPAIRED PER ER/A #595611-14AD REV.ORIGINAL. (2070176)SDR DALA2022010308200None · noneSHIP 3248 CRACK FOUND IN OPEN FASTENER HOLE #13 FRAME 20 RH SIDE DOOR STOP #1 LOWER CORNER. CORRECTIVE ACTION: REPAIRED PER ER/A #595607-14AD REV. ORIGINAL. (2069788)SDR CALA2021123002483Frame · crackedR1 DOOR FRAME 16 DOUBLE JOGGLE HOLE #6 IS CRACKED IN THE FRAME L AYER AR 11:00 POSITION. PER HAECO LCQ NR 9292446/20446 GENERATED BY V061680 CRA 5311-02722 AND HAECO REO-L23506 WITH NO DEVIATIONS. DIP READ GLE AREA PER PART 2 OF THE LATEST REVISION OF ECRA 531SDR SWAA2022021157100Stub Frame · crackedCRACK STUB FRAME LOCATED BS 294.5 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN ; 2021-576211 / [01] REPLACED STUB FRAME LOCATED BS 294.5 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A8370 REV D; [02] CORRECTED SSDR SWAA2022020857223Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 10; W.L. 164. ; / CUT OUT DAMAGED AREA AT BS 663 UPPER ATTACH ANGLE RBL 15 WL 164 PER SRM 57-10-10-2R-5 REPAIR 5 REQUEST NDI OPEN HOLE INSPECTION AT REPAIR AREA; [05] HFEC ROTARY INSPECTSDR DALA2021123008177None · noneDTA MONITOR INSPECTION LOG REFERENCE ER/A 596000-14 SECTION IV REQUIRES DTA APPROVAL WITHIN 60000 CYCLES AFTER SECTION I. CONTACT ENABLING TECHNOLOGIES DOUG JURY, 404-714-2928. DISCONTINUE REVENUE SERVICE WITHIN 60000 CYCLES AFTER SECT I PENDING A DAMAGE TOLERSDR DALA2021123008176None · noneDTA MONITOR INSPECTION LOG REFERENCE ER/A 596000-14 SECTION III REQUIRES DTA APPROVAL WITHIN 37900 CYCLES AFTER SECTION I REPAIR CONTACT ENABLING TECHNOLOGIES DOUG JURY, 404-714-2928. DISCONTINUE REVENUE SERVICE WITHIN 37900 CYCLES AFTER SECT I PENDING A DAMAGSDR DALA2021123008175None · noneREAR FUSELAGE / FRAME - FR 68LH - DOOR STOP FITTING #1 - HOLE 4 - CRACK. ACCOMPLISH ER/A 596000-14 SECTION II INSPECTION WITHIN EVERY 19700 CYCLES AFTER ACCOMPLISHMENT OF THE SECTION I REPAIR. ASSOCIATED ER/A 00-596000 ADDED FOR AC 3248. (LP# 2068997)SDR DALA2021123008174None · noneCRACK FOUND ON WINDSHIELD FRAME RH SIDE, CRACK LENGTH: 0.200 INCH, CRA CK AT 11 O CLOCK . AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING R EPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. SIDE AS PER ER/A 595453-14AD REV. ORIGINAL ANDSDR CALA2021122902475Frame · crackedR/H FR68 DOOR STOP #1 LOWER I/B HOLE HAS A CRACK INDICATION- SUP PORT TASK: AD 2018-03-12. PER HAECO LCQ NR 9294110/32110 GENERAT ED BY V061632.SDR DALA2021122908147None · noneCRACK FOUND ON CONTINUITY FITTING LH SIDE , CRACK LENGTH: 0.190 INCH APPROX, VERTICAL DIRECTION. AD 2020-17-03/ WORKCARD 5311-01226- 01 REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. PERFORMED REPAIR INSTRUCTION ON CONTINUISDR DALA2021122908146None · noneCRACK FOUND ON CONTINUITY FITTING RH SIDE, CRACK LENGTH: 0.190 INCH, V ERTICAL CRACK. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. PERFORMED REPAIR INSTRUCTIONS FOR CONTINUITY FITTINSDR JR2R20211229771Frame · crackedLH WHEEL WELL FRAME 52 CRACKEDSDR SWIA202163826None · corrodedCORROSION FOUND ON FR.87 AFT WET AREA CROSS BEAM DURING REPLACEMENT OF THE ATTACHING R/H I/B BEAM AS MARKED. (C-CHECK RO 1/15/2022) REPAIRED FR.87 AFT WET AREA CROSS BEAM BY WAY OF CUTTING OUT DAMAGE AND INSTALLING A FILLER AND DOUBLER PER ETD2021-170-0SDR DALA2021122908139None · noneCRACK INDICATION FOUND IN OPEN FASTENER HOLE (1EA) LOCATED AT UPPER AT TACHMENT FRAME 4 SIDE POST AREA RH SIDE, CRACK DIRECTION: 07 O CLOCK ( D1-D2=0.075 INCH). PERFORMED PERMANENT REPAIR ON UPPER ATTACHMENT FRAME 4 SIDE POST AREA RH SIDE AS PER ER/A 543313-14SDR DALA2021122908138None · noneCRACK INDICATION FOUND IN OPEN FASTENER HOLE (1EA) LOCATED AT UPPER AT TACHMENT FRAME 4 SIDE POST AREA LH SIDE, CRACK DIRECTION: 01 O CLOCK APPROX (D1-D2=0.0665 INCH). PERFORMED PERMANENT REPAIR ON UPPER ATTACHMENT FRAME 4 SIDE POST AREA LH SIDE AS PER ER/A 54SDR DALA2021122908133None · noneOUT LIMIT FRAME 68 DOOR STOP FITTING 1L DIAMETER HOLE ?1= 0.252INCH,?2= 0.254INCH,?3=0.251INCH ,?4=0.258INCH AA 5311 -01216 AD RELATED ACTIONS R EQUIRED PRIOR TO FURTHER FLIGHT AT AFT GALLEY AREA (4 EA). PERFORMED PERMANENT REPAIR FRAME 68 DOOR STOP FITTING 1LSDR DALA2021122908132None · noneOUT LIMIT FRAME 68 DOOR STOP FITTING 1 RH HOLE DIAMETER ?1= 0.257IN, ?2 =0.258IN, ?3=0.256IN, ?4=0.256IN AA 5311-01216 AD RELATED. ACTIONS REQ UIRED PRIOR TO FURTHER FLIGHT AT AFT GALLEY AREA (4 EA). ERFORMED PERMANENT REPAIR FRAME 68 DOOR STOP FITTING 1 RH ATSDR N6WA2021122904Former · corrodedPAX DOOR FORWARD FORMER AT FS311.75 IS CORRODED BEYOND REPAIRABLE LIMITS, REQUIRES REPLACEMENT. R&R PAX DOOR FORWARD FORMER AT FS311.75 IAW SRM 51-42-00 & EO C550/700-52MR-OO4-O.SDR N6WA2021122903Stringer · corrodedCORROSION AROUND RIVETS AT FS 280 TO FS 295, STR 25R. R&R STR 25R FROM FS280 TO FS302 IAW CRJ 700 SRM 53-00-03SDR SWIA202163824None · corrodedAFT WET AREA R/H INBOARD BEAM HAS CORROSION BETWEEN FR. 87-88 AS MARKED. (C-CHECK RO 1/15/2022) REMOVED AND REPLACED AFT WET AREA RH INBD BEAM BETWEEN FR, 87-88 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 AND CPM 51-25-00. SEE CONTINUSDR DALA2021122808123None · noneSHIP 185 FUSELAGE FRAME AND FAIL SAFE CHORD, STA 1540, S-38L-39R. 595941-14AD SECTION I ACCOMPLISHED, FOLLOW ON ACTION REQUIRED. CORRECTIVE ACTION: ER/A 595941-14AD SECTION I REPAIR IS LIMITED TO 50000 TOTAL FLIGHT CYCLES. (2066349)SDR DALA2021122808096None · noneSHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR THE LH FRAME 68 INSPECTING FOR CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUE ON MON. (2066495)SDR DALA2021122808095None · noneSHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR LH & RH FRAME 68. CORRECTIVE ACTION: COMPLIED WITH ERA. (2066491)
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