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 SWIA2023071809Unknown · dentedDENT BETWEEN LEFT FUSELAGE STATION FR 10 AND FR 11, STGL 14L AND 15L. NEXT TO SKYWEST LOGO. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF DENT DAMAGE ON FWD FUSELAGE SKIN AT FR10 AND FR11, STGR14L AND STGR15L, IN ACCORDANCE WITH ERJ175 SRM 53-10-01/REPAIR 1SDR DALA2023071205663Unknown · unknownCORROSION ON FRAME STA Y=1021 LONGERON 30+1.5 IN RH/LH. SUMMARY OF NRC 00513: CORROSION LEVEL 2. FRAME STA Y=1021 LONGERON 30 WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. (LP #2857160)SDR SWIA2023071009Unknown · dentedDENT BETWEEN LEFT FUSELAGE STATION FR 10 AND FR 11, STGL 14L AND 15L. NEXT TO SKYWEST LOGO. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR SWIA2023090800708Unknown · crackedLEFT SIDE FS235.00 UPPER FRAME SECTOR IS CRACKED. (MARKED) SRM 53-11-15 (C-CHECK RO 9/6/2023) REPLACED LH SIDE FS235.00 UPPER FRAME SECTOR/ANGLE P/N: 601R34032-21, NEW CLIP P/N: 601R34032-31 AND NEW ATTACHMENT ANGLE P/N:601R34032-19. REF CRJ200 SRM 51-4SDR SWAA2023080476423Frame · crackedCRACK ON FRAME LOCATED BS 312AT LEVEL STR 5LAT FWD GALLEY AREA 2023-431241<[01] PERFORMED REPAIR ON BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L IAW EA M-22-153-01244 <BR>SEE TASK CARD: TTG8Q00M3J6Z;[02] PERFORMED REPAIR ON BS 312 FRAMSDR DALA2023071305691Unknown · unknownSHIP 3123 A CRACK INDICATIONW AS FOUND IN LH CONTINUITY FITTING. CORRECTIVE ACTION: REPAIRED PER ER/A 608962-14. (2854527)SDR DALA2023070705488Unknown · unknownCRACK ON FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00291: FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE SDR SWI2023F00207Unknown · corrodedSTGR26R AREA OF CORROSION BETWEEN FS295-310 (C-CHECK RO 8/16/2023) REPLACED WITH NEW STGR26R REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOODSDR SWI2023F00206Unknown · corrodedCORROSION ON FRAME AT FS319 STGR20L -21L (C-CHECK RO 8/16/2023) REPLACED FRAME SECTION AT FS 319 STR 19L -21L REF CRJ 700 SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670-31810 REV AE. LEAK CHECK GOOD. COMPLIED WITH TASK CARSDR SWI2023F00205Unknown · corrodedFRAME AT FS295 HAS CORROSION AT STGR20L (C-CHECK RO 8/16/2023) REMOVED CORROSION ON FRAME AT FS295.00 STGR 20L AND FOUND OUT OF LIMITS PER CRJ700SRM 53-21-06-101-002-A01. REMOVED AND REPLACED FRAME SECTION AT FS295.00 FROM STGR 18L TO STGR 20L WITH STOCSDR SWI2023F00204Unknown · crackedFS280 CROSSBEAM HAS A CRACKED STIFFNER/ANGLE FWD SIDE AT APPROX RBL33 (C-CHECK RO 8/16/2023) REPLACED STIFFENER/ANGLE PN CC670-34106-1 ON FS280 CROSSBEAM APPROX. RBL33. REF CRJ700 SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01 AND CRJ700 DWG CC670-3401SDR SWI2023F00203Unknown · corrodedSTGR19L HAS AREAS OF CORROSION FS295-FS310 (MARKED) (C-CHECK RO 8/16/2023) INSTALLED NEW STRINGER AT 19L, FS280 - FS310 REF DRAWING SH670-31550 REV F CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEASDR SWI2023F00000208Unknown · corrodedFUSELAGE STGR 27 HAS CORROSION AT BOTTOM FLANGE BETWEEN RIVETS AFT OF FS 295 FRAME. MARKED. (C-CHECK RO 8/16/2023) INSTALLED NEW REPLACEMENT STRINGER P/N SH670-31642-1 AT INSIDE STRUCTURE OF FUSELAGE SKIN PANEL STGR27 BETWEEN FS.280.00 & FS.295.00 REF. SDR SWI2023F00200Unknown · corrodedOMNIDIRECTIONAL TCAS ANTENNA DOUBLER HAS HEAVY CORROSION ON INSIDE SURFACE AROUND CONNECTOR HOLE. MARKED (C-CHECK RO 8/16/2023) INSTALLED NEW MAIN AVIONICS BAY TCAS ANTENNA DOUBLER REF. CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-ASDR SWI2023F00208Unknown · corrodedFUSELAGE STGR 27 HAS CORROSION AT BOTTOM FLANGE BETWEEN RIVETS AFT OF FS 295 FRAME. MARKED. (C-CHECK RO 8/16/2023) INSTALLED NEW REPLACEMENT STRINGER P/N SH670-31642-1 AT INSIDE STRUCTURE OF FUSELAGE SKIN PANEL STGR27 BETWEEN FS.280.00 & FS.295.00 REF. SDR SWIA2023072700006Unknown · damagedRH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625% WAS MIS-DRILLED. FABRICATE A NEW RH DRAG ANGLE (C-CHECK RO 7/23/2023) REMOVED & INSTALLED NEWLY FABRICATED RH FUSELAGE DRAG ANGLE REPAIR SECTION NEAR DATUM 61.5625% REF CRJ 200 SRM 51-42-21 ,CRJ 200 SRM 51-42-SDR DALA2023071005521Frame · corroded(LOG 2852208) CORROSION ON FRAME AT STA 947.5 NEAR STR 27 AND 28 RBL 8.1-LBL 8.1 AT AFT CARGO COMPARTMENT. REMOVED AND REPLACED. FRAME AT AFT CARGO STA 947.5 RBL 28 - LBL 28 WL 176 PER B737-900 SRM 51-40-02-0G PAR. 4. B AND DWG# 147A1047 REV.- R.SDR DALA2024070206702Frame · unknownSHIP 6703 DTE, ERA 563827-14AD REVISION B, FUSELAGE / FRAME / FS620 / STR 3L - 4L / GROUND STUD FASTENER INTERFERENCE. CORRECTIVE ACTION: REF ERA 563827-14. (2850925)SDR SWI2023F00310Unknown · corrodedAFT FORMER @ APPROX. FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED AFT FORMER @ FS347 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 DWG 601R31702 REV-N. NO DEFECTS NOTED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (STRUCTURAL MAJSDR SWI2023F00307Unknown · corrodedFWD FORMER @ APPROX. FS311 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW FWD PASSENGER DOOR FORMER REF CRJ-200-SRM 51-42-06 , CRJ-200-SRM 51-42-21, AND DRAWING 601R31702 REV N . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SESDR SWI2023F00235Unknown · corrodedCORROSION NOTED ON BATH TUB FITTING AT APPROX FS286 AND RBL18 (MARKED) (C-CHECK RO 8/16/2023) REMOVED AND REPLACED FITTING P/N SH670-32149-3 AT FS286 AND RBL18 REF DRAWING SH670-32120 REV -D AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TSDR SWIA20230721005Unknown · crackedAFT WET AREA FLOOR FRAME AT FR86 HAS 2 EA. CRACKED / BROKEN PANEL SUPPORTS ON LH AND RH SIDE AS MARKED. (C-CHECK RO 7/21/2023) REMOVED AND REPLACED AFT WET AREA FLOOR FRAME AT FR86 2 EA. PANEL SUPPORTS ON LH AND RH REF: EMB SRM 51-40-08, RESTORED SURFACSDR DALA2023070605470Unknown · unknownSHIP 3123 CRACK WAS FOUND IN FR20 LHS AT DBL JOGGLE AREA IN HOLE #C. CORRECTIVE ACTION: PER 565846-14 REV A, REPETITIVE INSPECTION. (2850605)SDR FDEA202307051147Frame · crackedFUSELAGE FRAME FR73A FOUND 1EA CRACKED AT S24L - S25L REPAIRED THE CRACK ON THE FUSELAGE FRAME FR73A S24L - S25L PER FEDEX EA: #: 6-5310- T0375001, TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH&RH DOOR FRASDR FDEA202307051146Frame · crackedFUSELAGE FRAME FR73A FOUND 1EA CRACKED AT S24R - S25R REPAIRED THE CRACK ON THE FUSELAGE FRAME FR73A S24R - S25R PER FEDEX EA:#:6-5310- T0375001, TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH &RH DOOR FRSDR SWAA2023081474759Frame · crackedCRACK ON FRAME LOCATED BS 747 BTW STR 8R TO 9R AT PASSENGER CABIN 2023-413296<[01] PERFORMED REPAIR ON FRAME LOCATED BS 747 BTW STR 8R TO 9R AT PASSENGER CABIN IAW EA 1-A53-12114 SEE INDIVIDUAL SIGN OFFS BELOW.;[02] PERFORMED REPAIR ON FRAME LOCATED BS 747 BTWSDR SWAA2023080777740Frame · crackedCUSTOMER REQUEST CRACK ON CUT OUT OF EXTERNAL GROUND SERVICE DOOR 114AR LOWER FUSELAGE 2023-431020<[01] ET TOOL USED PN NORTEC 600D; SN 210138203; DUE DATE 09-JUN-24;[02] REPAIRED CUT OUT OF EXTERNAL GROUND SERVICE DOOR 114AR LOWER FUSELAGE IAW B737-700 SRM 53SDR DALA2023071005514Unknown · unknown(LOG 2849189) DURING ROUTINE MAINTENANCE, DENT AND BEND DAMAGE WAS FOUND ON THE BS 500K FRAME (PN 143A1200-204) AND DOUBLER (143A1203 192), BETWEEN S-22R AND S-25R. DAMAGE REPAIRED PER ERA 609626-14.SDR AALA202307057255Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT MAIN FRAME FORWARD SIDE LOCATED AT BS 927 FROM S20R TO S22R. REPAIRED FRAME PER EA EA345591.SDR DALA2023070305309Unknown · unknownCORROSION ON WEB SEVERAL POINTS AT AREA DOOR AFT COMPARTMENT (ENTRY AREA) (C2). SUMMARY OF NRC 00175: CORROSION LEVEL 2. WEB AREA DOOR AFT COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #2846580)SDR SWI2023F00297Unknown · crackedRH VERTICAL STABILIZER TO FUSELAGE, AFT DRAG ANGLE APPEARS CRACKED (C-CHECK RO 8/31/2023) CUT AWAY DAMAGED PORTION OF AFT RH DRAG ANGLE AND REMOVED ALL BURRS AND SHARP EDGES REF CRJ700 SRM 55-31-00-201-001-A01. INSTALLED NEW FABRICATED FILLER REPAIR ANSDR SWI2023F00296Unknown · crackedLH VERTICAL STABILIZER TO FUSELAGE, FWD DRAG ANGLE APPEARS CRACKED (C-CHECK RO 8/31/2023) REPAIRED CRACKED LH VERTICAL STABILIZER TO FUSELAGE FORWARD DRAG ANGLE PER REO 670-55-31-164 REV-- , DATED 2023-07-10, SEE CONTINUE CARD FOR DETAILS OF WORK PERFOSDR SWIA20230702Unknown · crackedLH VERTICAL STABILIZER TO FUSELAGE, AFT DRAG ANGLE APPEARS CRACKED (C-CHECK RO 8/31/2023) REPAIRED CRACK ON THE LH VERTICAL STABILIZER TO FUSELAGE, AFT DRAG ANGLE REF CRJ-700 SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURASDR SWAA2023080474163Stub Frame · crackedCRACK ON STUB FRAME LOCATED BS 294.5 BTW STR 9R TO STR 11R CUTOUT AT FWD SERVICE DOOR 2023-422409<[01] REPLACED STUB FRAME LOC. BS 294.5 BTW STR 9R TO STR 11R CUTOUT AT FWD SERVICE DOOR IAW SRM B737-700 51-10-02. SRM 51-40-02; DRAWING: 141A8370 REV. D. SEE INDSDR IPXA2023072486756Frame · damagedFAULT: AFT CARGO PIT - STA 1560 RH SIDE FRAME HAS AN EXISTING REPAIR INBOARD OF STR 26R - NEED ALTERNATIVE METHOD OF INSPECTION PER UPS EO-73926-JIC002 REVIEWEDSDR DALA2023070305302Unknown · unknownCRACK ON FRAME STA 1037 BTW LONGERON 17 LH AT CABIN. SUMMARY OF NRC 00239: FRAME STA 1037 BTW LONGERON 17 LH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4. (LP #2844142)SDR DALA2023111709501Unknown · unknownSHIP 6703 FUSELAGE / FRAME / FS620 / STR 2L & 3R / OVERSIZE HOLES. CORRECTIVE ACTION: REF ERA 609749-14AD. (2843063)SDR SWAA2023081473876Stub Frame · crackedCRACK STUB FRAME LOCATED BS294.5 AT LEVEL STR17R AT PASSENGER CABIN 2023-413225<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 220272512; DUE DATE: 17-DEC-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220273012;DUE DATE:17-DESDR DALA2023070305298Unknown · unknownCORROSION ON FITTING STA 893.5 BELOW FLOOR LEVEL CUSP WEB AREA WAS FOUND. SUMMARY OF NRC 00503: CORROSION LEVEL 2. FITTING SPLICE ON STA 893.5 RH WAS REPLACED PER DWG 9910151 REV CH AND B717 SRM 51-41-05-0G. (LP #2842912)SDR DALA2023063005263Unknown · unknownSEVERAL CRACKS ON CUSP WEB LH SIDE LOWER SIDE STA Y=586 BTW X=+60 AT PAX CAB. SUMMARY OF NRC 00520: CUSP WEB LH STA 579 TO STA 598 WAS FABRICATED PER B717-200 SRM 53-00-55-2R-4 AND DWG: 9910151 REV CH AND REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G.SDR DALA2024112711264Frame · corrodedCORROSION ON FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00311: CORROSION LEVEL 2. FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 TASDR SWIA2023090529Unknown · dentedSHEAR CLIP DENTED ON FRAME 3 BETWEEN STGR 18 AND 19 (FILED CLOSED)REMOVED AND REPLACED SHEAR CLIP LOCATED ON FR.3 BETWEEN STGR 18 AND 19 (REF. P/N 170-03772-001) WITH A SERVICEABLE UNIT IN REFERENCE TO SRM 51-41-00 AND ETD 2023-170-016085 REV./ DATED 06-30-202SDR SWIA20230727629Unknown · damagedFOUND DOUBLE HOLE ON THE LH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625% (C-CHECK RO 7/23/2023) REPLACED AND PERFORMED REPAIR TO LH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625%. PERFORMED AND COMPLIED WITH ALL STEPS OF REO 601R-55-31-445 REV -- DATED 2023-07-04. SDR DALA2023063005256Unknown · unknownSHIP 3123 DURING M2 AND WHILE INSPECITON PER JIC 5310-4040, (4) ELONGATED HOLES FOUND COMMON TO CROSSBEAM AT FR68, SECTION CONNECTION AT FR68 AND LONGITUDINAL BEAM. CORRECTIVE ACTION: REPAIRED PER ER/A 609536-14. (2841496)SDR DALA2023063005255Unknown · unknownSHIP 3123 WHILE ACCOMPLISHING NTM 53-11-55 A CRACK INDICACTION WAS FOUND IN FR20 RHS IN UPPER AREA AT LEVEL OF DOOR STOP #7. CRACK IN HOLE "A". CORRECTIVE ACTION: PER SECTION IV OF 565847-14, REV A, ACCOMPLISH SECTION IV REPETITIVE INSPECTION WITHIN EVERY 5,40SDR SWIA2023072000628Unknown · crackedDIAPHRAGM AT FS724 RHS IS CRACKED. (C-CHECK RO 7/20/2023) INSTALLED NEW DIAPHRAGM P/N: SH670-36115-2 AT FS724 RHS. REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG SH690-36110 REV P C/W TASK CARD 51-900-1002SDR DALA2023062905213Unknown · unknownCORROSION ON CUSP WEB BTW STA Y=218/220 AND BTW STA X=-44/-54 AT PAX CABIN (W1). SUMMARY OF NRC 00377: CORROSION LEVEL 2. CUSP WEB BTW STA Y=218/220 WAS REPLACED B717-200 SRM 51-41-02 PAR 4 AND 51 -41-05-0G. (LP #2839683)SDR DALA2023062905211Unknown · unknownAFTER CORROSION REMOVAL ON CUSP WEB (LIGHTNING HOLE) STA 539, STA 648, STA 890 TO 907, AND STA 929 TO 935 AREAS WERE FOUD OUT OF LIMITS PER B717 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4 A. SUMMARY OF NRC 00480: CORROSION LEVEL 2. (LIGHTNING HOLE) SSDR DALA2023062805190Unknown · unknownCORROSION ON CUSP ANGLE FROM STA Y=168 TO STA Y=218 AND -X=54 TO -X=60 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00452: CUSP ANGLE FROM STA Y=168 TO STA Y=218 AND -X=54 TO -X=60 WAS REPAIRED PER PRI 608991-14 REV 2 AND ER/A 608991-14 REV ORIGINAL SECTSDR DALA2023062805189Unknown · unknownEXFOLIATION CORROSION ON DIAPHRAGM STA Y=178 TO Y=198 X=-45 X=-52 AT PAX CABIN W1. SUMMARY OF NRC 00303: CORROSION LEVEL 2. DIAPHRAGM STA Y=178 TO Y=198 X=-45 TO X=-52 WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2838515)
Back to JASC 5311