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 SWI2023F00392Unknown · corrodedFRAME AT FS597 STGR19L HAS CORROSION (C-CHECK RO 10/4/2023) FRAME AT FS 597 BETWEEN STGR 19L - 18L REMOVED AND REPLACE WITH NEW FABRICATED FRAME P/N SH670-33178-1 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 DWG SH670-33750 REV: SDR AALA202308143815Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN REAR SPAR LEFT HAND FRAME ASSEMBLY (PICKLE FORK) LOCATED AT BS 663, S17L. REPLACED FRAME ASSEMBLY PER EA 346632.SDR AALA202308144000Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN REAR SPAR RIGHT HAND FRAME ASSEMBLY (PICKLE FORK) LOCATED AT BS 663, S17R. REPLACED FRAME ASSEMBLY PER EA 346632.SDR CALA2023080702433Frame · crackedRH FR16 UPPER DOUBLE JOGGE AREA HOLE 7, A AND C HAVE CRACK INDICATIONS IN FRAME LAYER. "REPAIR BEFORE NEXT FLIGHT" GEN BY V89244 4 ON HAECO LCQ NR 9294380/34380 TO ACMP INITIAL INSP OF RH FR16 UPPER DBL JOGGLE HOLES 7,8,A,&B 36,316 TOTAL FC. REPEAT INSP AT INTSDR AALA202308256803Stub Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD GALLEY DOOR STUB FRAME LOCATED AT BS 296, S8R. REPLACED STUB FRAME PER SRM 51-40-02, AARD 51-00-05-1 AND DWG 141A8370.DSDR DALA2023080706381Unknown · unknown(LOG 2899390) RIGHT FUSELAGE F.S. 727D FRAME IS CRACKED AT AC RAIL BRACKET I/B FASTENER BETWEEN STR 8 AND 9. REPAIRED R/H FRAME STA. 727D IAW DELTA TASK CARD 2526-01236-02B.SDR DALA2023080406343Unknown · unknownSHIP 3165 CRACK INDICATION ON FRAME 68 LH SIDE DOOR STOP FITTING 5 LOWER INBOARD HOLE (4) CRAC DIRECTION 5 O CLOCK AT AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC ON FRAME 68 LH SIDE DOOR STOP FITTING 5 LOWER INBOARD HOLE (4) AT AFT GALLESDR CALA2023080402418Frame · corrodedELECTRICAL AND ELECTRONICS COMPARTMENT FRAME STA312+7 STRINGER 21L TO LONGERON22L HAS EVIDENCE OF CORROSION (REF AAR NR 9204606)SDR DALA2023080406295Unknown · unknownCORROSION ON FRAME STA 1037 BETWEEN LONGERON 24 TO LONGERON 21 LH AT AFT CARGO COMPARTMENT IS OUT LIMITS WITH 0.040 IN PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL PAR. 4. C. FIGURE 103. SUMMARY OF NRC 00660: CORROSION LEVEL 2. FRAME STA 1037 BTW LONGSDR SWAA2023090185169Frame · crackedCRACK ON FRAME LOCATED BS 727D BTW STR 8L TO STR 9L AT PASSENGER CABIN 2023-470152<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 210138103; DUE DATE: 02-MAY-24.;[02] FRAME LOCATED BS 727D BTW STR 8L TO STR 9L AT PASSENGER CABIN NOT REPAIRED DUE TO CRACKSDR DALA2023080306278Unknown · unknownCORROSION ON WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 00179: CORROSION LEVEL 2. WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR WERE REPAIRED PER B717-200 SRM 51-70-10SDR AALA202310168570Window Frame · unknownAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND WINDSHIELD FRAME AT THE CENTER POST LOWER ATTACHMENT INTERNAL AREA AT FR 2 AND Y0 REQUIRES MIRROR REPAIR PROCEDURE ACCOMPLISHED AS PART OF THE MAJOR REPAIR ACCOMPLISHED TO THE WINDSHIELD FRAMING ON EA 346973.SDR WX0A202308040001Unknown · unknownPERFORMED NDT EDDY CURRENT INSPECTION I/A/W AIRBUS 320 NTM TASK 51-10-08-250-803-A01. @ L/H FWD FUSELAGE @ FRAME 14 BETWEEN STRINGERS 12-13 FOUND CRACK AFT OF RIVET 9MM LENGTH/INSTALLED EXTERNAL DOUBLER AND FILLER IAW TD/81261153/005/2023#A. SEE NR1178600, NR1SDR REXA2022080200581Frame · corrodedFRAME 364 IS CORRODED BETWEEN STRINGERS 25L TO 25R. COMPLIED WITH FRAME 364 REPAIR IAW CRJ 900 SRM 53-21-23-201-008-A01 REPAIRSDR SWAA2023090184424Stub Frame · crackedCRACK ON STUD FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2023-470093 CORRECTIVE DESCRIPTION FAULT CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DASDR SWAA2023090184421Frame · crackedCRACK ON FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2023-470090<[01] REPAIRED FRAME BS 312 AT LEVEL STR 6L AT PASSENGER CABIN IAW EA# M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPAIRED FRAME BS 312 AT LEVEL STR 6L AT PASSENGER CABIN IAW ESDR DALA2023080206247Unknown · unknownCORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 908 BTW L29-L AND L29 -R. SUMMARY OF NRC 00561: CORROSION LEVEL 2. REPAIR SPLICE AT FRAME STA 908 BTW LONGERON 27R TO LONGERON 28L WERE FABRICATED AND REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIRSDR DALA2023080106207Unknown · unknownCORROSION ON ANGLE OF FRAME BTW LON 27R TO LON 28L STA 908 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00161: CORROSION LEVEL 2. ANGLE OF FRAME BTW LONG 26L TO LONG 26R STA 908 AT AFT CARGO COMPARTMENT WAS FABRICATED AND REPLACED PER DWG 9975524 REV P AND B717-20SDR DALA2023080106205Unknown · unknownCRACK WAS FOUND ON LH OVERWING FRAME STA Y=696, GREATER THAN 0.125IN IN REF TASK CARD 5310-01436-01B JOB #078-0002 STEP 10. SUMMARY OF NRC 00181: LH OVERWING FRAME STA Y=696 WAS REPLACED PER B717-200 TASK CARD 5310-01436-03A JOB 107-0001. ASSOCIATED AA 5310-01SDR DALA2023080106204Unknown · unknownCORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R. SUMMARY OF NRC 00560: CORROSION LEVEL 2. FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R WERE FABRICATED AND REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 PAR 5, 51- 41-02-0G,SDR REXA2022073100573Frame · corrodedFRAME 333 HAS CORROSION FROM STRINGER 25L TO 24R REPAIRED IAW CRJ 900 SRM 53-00-06-201-004-A01SDR REXA2022073100571Frame · corrodedFRAME 319 HAS CORROSION FROM STRINGER 24R TO 25L FABRICATED, LOCATED, AND DRILLED REPAIR PARTS IAW CRJ 900 SRM 53-00-06-201-004-A01 STEPS C(3-6) AND INSTALLED REPAIR PARTS PER CRJ900 SRM 53-00-06-201-004-A01SDR SWI2023F00383Unknown · corrodedFS280 BEAM BETWEEN RBL9 AND LBL9 ANGLE HAS CORROSION (MARKED). (C-CHECK RO 9/26/2023) REPAIRED CORROSION ON FS280 BEAM BETWEEN RBL9 AND LBL9 ANGLE REF. REO 601R-53-11-3884 REV - A, DATED 2023-08-18 & GREO 601R-53-11-136 REV - A, DATED 2007/11/01. BOMBARDISDR SWIA20230822728Unknown · crackedLINTEL STGR3 BTWN FS280 AND FS295 IS CRACKED (C-CHECK RO 8/20/2023) PERFORMED REPAIR ON LINTEL STGR3 BETWEEN FS280 AND FS295. REF. REO 670-53-21-493 REV. D, DATED 2015/07/10 AND SB 670BA-53-040 REV. C, DATED 09/20/2012. COMPLIED WITH SKYCARD 51-900-1002SDR DALA2023080106226Unknown · unknownSHIP 0676 FUSELAGE / FRAME / RHS BS 1640 / STR 14R / LOWER OUTBD HOLE & LOWER INBD HOLE / CRACKED. CORRECTIVE ACTION: REF ERA 591624-14. (2889387)SDR DALA2023080106200Unknown · unknownCRACK ON FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN. SUMMARY OF NRC 00289: FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN WAS REPAIRED PER B717 SRM-53-20-07-2R-4 (PERMANENT REPAIR). (LP #2890030)SDR SWI2023F00255Unknown · crackedLH FS235 FRAME UPPER GUSSET IS CRACKED (C-CHECK RO 8/20/2023) REMOVED AND REPLACED LH FS235 FRAME UPPER GUSSET IS CRACKED CRJ 900 SRM 51-42-06-001-001-A01 REVISION 38 JUL 25/2020B DWG CC670-34040 REV -C COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWIA20230822727Unknown · crackedLH FS235 UPPER FRAME IS CRACKED (C-CHECK RO 8/20/2023) VREMOVED AND REPLACED LH FS235 FRAME UPPER SECTOR WITH NEW P/N CC670-34133-9 REF CRJ 900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND DWGCC670-34040 REV -CPERFORMED LEAK TEST OF THE LH FS2SDR DALA2023072706098Unknown · unknownCORROSION ON FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00645: CORROSION LEVEL 2. FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #2886682)SDR DALA2023073106168Unknown · unknown(LOG 2885892) FORWARD CARGO COMPARTMENT RH SIDE BS 500C FRAME HAS A DENT BETWEEN STRINGERS 24R AND STRINGER 25R. REMOVED DENT DAMAGE AND ACCOMPLISHED REPAIR ON FORWARD CARGO COMPARTMENT RH SIDE BS 500C FRAME BETWEEN STRINGER 24R AND STRINGER 25R IAW B737 SRM 5SDR DALA2023073106165Unknown · unknown(LOG 2885873) DURING HCK DENT LOCATED ON FORWARD CARGO COMPARTMENT RH SIDE BS 500C FRAME BETWEEN STRINGERS 24R AND 25R. REMOVED DENT DAMAGE AND ACCOMPLISHED REPAIR ON FORWARD CARGO COMPARTMENT RH SIDE BS 500C FRAME BETWEEN STRINGER 24R AND STRINGER 25R IAW B73SDR DALA2023073106172Unknown · unknown(LOG 2885867) AFT CARGO COMPARTMENT STA 727L FRAME DENTED AT APPROX RBL 21 WL 155. REMOVED DAMAGE AND REPAIRED IAW B737 SRM 53-60-07-2R-2 ALT 2 AND ER/A 610423-14 REV ORIGINAL.SDR SWAA2023082482249Frame · crackedCRACK ON FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2023-461340<[01] TRIMMING OUT FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW EA M-22-153-01244;[02] CERTIFIED WORK PERFORMEDSDR DALA2023073106158Unknown · unknown(LOG 2884100) DURING HCK DENT LOCATED ON FORWARD CARGO COMPARTMENT LH SIDE BS 500D FRAME BETWEEN STRINGERS 25L AND 26L. FRAME BETWEEN STRINGERS 25L AND STRINGER 26L IAW B737 SRM 53-30-07-2R REPAIR 1.SDR DALA2023073106157Unknown · unknown(LOG 2884121) FORWARD CARGO COMPARTMENT LH SIDE BS 500D FRAME HAS A DENT BETWEEN STRINGERS 25L AND STRINGER 26L. REMOVED DENT DAMAGE AND ACCOMPLISHED REPAIR ON FORWARD CARGO COMPARTMENT LH SIDE BS 500D FRAME BETWEEN STRINGERS 25L AND STRINGER 26L IAW B737 SRM SDR DALA2023072606042Unknown · unknownSHIP 3209 DURING ACCOMPLISHMENT OF ALI 531153 IN FEB 2018 CRACKS FOUND IN FR16 LH IN HOLES #6 & #C. DURING CCK IN JAN 2023 ISB 53-1373 ACCOMPLISHED AND ADDITIONAL CRACKS FOUND IN HOLES #8, #A, #E. ALSO, HOLES #3, #4, #5, #7, #B, #C, #D & #F WERE FOUND WITH HOLSDR 2A6R2023072567601Frame · crackedCRACK DAMAGE WAS DISCOVERED ON THE 7° BULKHEAD FLANGE (PN: 350A21-4694) AT APPROXIMATELY RBL 34”. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC130-53-2023-2148, ISSUE A DATED 17SDR SWI2023F00426Unknown · unknownAFT FUSELAGE - TOP L/H SIDE - @ 67.5% REAR SPAR DATUM - FWD BRACKET CONNECTING FUSELAGE TO VERTICAL PYLON @ 67.5% DISPLAYING EVIDENCE OF CRACKING (C-CHECK RO 10/4/2023) REPAIRED LH FWD DRAG ANGLE AT AFT FUSELAGE LH 67.5% REAR SPAR VERTICAL STABILIZER RESDR CALA2023072602326Frame · puncturedREF. BAM NR1483836, PUNCTURE ON FRAME STRUCTURE STA. 259.5, S-12L AFT AND O/B OF P18 PANEL. SEE ATTACHED IMAGES. AREAS MARKED.SDR DALA2023072505989Unknown · unknownSHIP 3262 HOLE #6 AT DOOR FRAME CRACKED. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD REV A. (2882936)SDR DALA2023072505988Unknown · unknownSHIP 3262 HOLE #5 CRACKED ON FRAME. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD REV. A. (2882931)SDR DALA2023072505987Unknown · unknownSHIP 3262 HOLE #4 AT FRAME CRACKED. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD REV A. (2882930)SDR DALA2023072505986Unknown · unknownSHIP 3262 HOLE #3 ON FRAME CRACKED. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD REV A. (2882928)SDR DALA2023072505984Unknown · unknownLOWER FRAME SECTION STA 132 WAS DAMAGED DURING LANDING. MAINTENANCE REMOVED LOWER FRAME SECTION PER B717 SRM 51-40-02. LOCATED AND DRILLED NEW SPLICES PER B717 DWG 9911512. INSTALLED NEW SPLICES AND REPLACEMENT 132 FRAME SECTION PER B717 SRM 51-40-02 AND DWG #SDR DALA2023072606096Unknown · unknownSHIP 3158 DAMAGE FOUND TO RH MLG DOOR FWD HINGE FITTING. CORRECTIVE ACTION: REPAIRED PER 610627-14AD. (2880772)SDR DALA2023072505990Unknown · unknownSHIP 3262 FR 16LH HOLES #5 AND #6 DISCREPANCIES FOUND. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD. (2881575)SDR SWIA20231006722Unknown · crackedREAR FUSELAGE - TOP R/H SIDE @ 67.5% DATUM - BRACKET CONNECTING FUSELAGE TO VERTICAL PYLON DISPLAYS EVIDENCE OF A POSSIBLE CRACK (C-CHECK RO 10/4/2023) REPAIRED RH FWD DRAG ANGLE AT AFT FUSELAGE RH 67.5% REAR SPAR VERTICAL STABILIZER REF-CRJ-700 SRM 55SDR SWI2023F00342Unknown · crackedFS280 LBL9 INBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 9/13/2023) REMOVED AND REPLACED WITH NEW CLIP AT FS 280 LBL 9 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND REO 601R-53-11-171 REV-D DATE 13-FEB-07. COMPLIED WITH SKYCARD 51-900-1003-SKY.SDR SWI2023F00338Unknown · cracked*CRACK NOTED ON FRAME 333 BETWEEN STRG1L-2L (MARKED), MX#26924717 (C-CHECK RO 9/13/2023) INSTALLED REPAIR DOUBLER BY COMPLYING WITH REO 601R-53-21-3644 REV -A, DATED 2023-08-15. COMPLIED WITH SKY WEST TC 51-900-1003-SKY.SDR SWI2023F00333Unknown · corrodedFRAME SPLICE STGR17AT FS319.70 HAS CORROSION (MARKED). (C-CHECK RO 9/13/2023) REMOVED AND INSTALLED NEW FWD FUSELAGE LWR FRAME BRACKET P/N: 601R38335-1 REF CRJ200 SRM 51-42-21 AND DWG 601R38303, REV AR. COMPLIED WITH 51-900-1003-SKY
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