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 SWAA2022072723755Frame · crackedBS 312 FRAME CRACKED AT I/B RADIUS STR 5L-6L (ABOVE FED CUTOUT) / [01] JOB COMPLETED ON CUSTOMER CARD#M-22-153-01244 (1992) OR TTG8Q00D947C.<BR><BR>SELECTED 'EA-GENERAL' REPAIR REFERENCE PER EA#M-22-153-01244 STEP 10;[02] VERIFIED REPAIRED PER EA M-22-153-0124SDR SWAA2022072723759Stub Frame · crackedCRACK ON FUSE INNER SKIN AT FWD EDGE OF FSD CUTOUT; BS 294.5+4' STR 10R / [01] HFEC INSPECTED INNER SKIN PER 737NDT PART 6 51-00-00 PROCEDURE 23. MARKED ENDS OF CRACK IN RED INK. CRACK STARTS AT EDGE OF SKIN AT FWD SERVICE DOOR CUTOUT AND RUNS FWD AND IS 2 INCSDR AALA202207057527Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND S22R AT DOOR STOP #1 LOWER INBOARD BOLT HOLE. REPAIRED FRAME PER SRM 53-41-12-300-011.SDR DALA2022070104609None · noneSHIP 664 DENTS ON FRAME BTW STA 1480 AND S- 27L TO S- 26L AT AFT CARGO COMP. CORRECTIVE ACTION: SUMMARY OF NRC 00239: DENTS ON FRAME BTW STA 1480 AND S- 27L TO S-26L AT AFT CARGO COMP. WERE REPAIRED PER B757-200 SRM. (2297862)SDR DALA2022070104608None · noneSHIP 664 DENTS ON FRAME BTW STA 1480 AND S- 27L TO S- 26L AT AFT CARGO COMP. CORRECTIVE ACTION:SUMMARY OF NRC 00239: DENTS ON FRAME BTW STA 1480 AND S- 27L TO S-26L AT AFT CARGO COMP. WERE REPAIRED PER B757-200 SRM. (2297857)SDR CALA2022062901601Intercostal · crackedL/H Y+1292 FR 11-8" HAS CRACKED WEB. GENERATED AT HAECO LCQ PER NR 9294798 (30798) BY V061673. {SUPPORT TASK} REPAIRED CRACKED WEB AT L/H Y+1292 FR 11-8 IAW A320 SRM 53-11-14 -300-005. PERFORMED BY V929087 INSP BY V919150.SDR SWIA202266126None · corrodedCORROSION ON AFT WET AREA FR84 CROSSBEAM IN 4 LOCATIONS AS MARKED. (C-CHECK RO 7/13/2022) PERFORMED PERMANENT REPAIR TO FR84 FLOOR CROSSBEAM REF ETD2022-170-021925. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED. REPAIR PARTS WEIGHED 0.395 LBS, NO WESDR DALA2022070704745None · noneSHIP 177 CRACK FOUND ON THE FRAME END FITTING AT STA852. RBL90. WHICH IS ATTACHED TO THE WING CENTER SECTION UPR SURFACE. CORRECITVE ACTION: THE FRAME END FITTING FABRICATED FROM 7050-T7451 PLATE AND REPLACED AS PER PRI 600102-14 (2304167)SDR DALA2022062804505Structure · corrodedSHIP 178 BULK CARGO COMPARTMENT T CHORD CORROSION AT STA 1562 AND S-39L TO S-39R. CORRECTIVE ACTION: CORRODED LOWER CHORD REPAIRED AND ACCOMPLISHED AS PER PRI599984-14. (2294459)SDR DALA2022062804512Frame · dentedSHIP 686 AD, AA. IN REF AMDS 5311-01227-01A: EXISTING REPAIR WAS FOUND DENTED IN THE INSPECTION AREA STA 1460 S-26L. CORRECTIVE ACTION: SUMMARY OF NRC 00156: FRAME ON STA 1460 S-25L TO S-27L WAS REPAIRED PER. ER/A 599756-14AD REV. ORIGINAL SECTION I: PERMANENTSDR LR7A2022062403184Ring · corrodedDURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS370 RH RING SEGMENT CORRODED AT WL144, RBL64. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-21. NR# 1000753556.SDR LR7A2022062403160Frame · corrodedDURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH FS517 FRAME CORRODED AT LBL63, WL144. / REPAIRED IAW LAC MEA 382-53-22-036. NR# 1000695358.SDR LR7A2022062403146Ring · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5315, FOUND THE FS817.0E/FS737 RING SEGMENT CRACKED AND CORRODED AT RBL61-65, WL143-153 / REPAIRED IAW LAC MEA 382-53-22-064. NR# 1000690375.SDR LR7A2022062403144Window Sill · crackedDURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH WINDSHIELD FRAME (SILL) WITH NDI CRACK INDICATIONS AT FS132 & FS135.5, RBL38, WL251. / REPAIRED IAW LAC MEA 382-53-22-018. NR# 1000690244.SDR LR7A2022062403119Ring · corrodedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5317, FOUND THE FS245 RH FRAME (RING SEGMENT) CORRODED AT WL146, RBL61-67 / REPAIRED IAW LAC MEA 382-53-22-051. NR# 1000684783.SDR SWIA2022081666279Frame · corrodedMAIN AVIONICS BAY FRAME FS333.00 CORRODED AROUND GROUND STUDS APPROX TO STR 19L (C-CHECK RO 8/14/2022) REMOVED AND REPLACED FS333.00 FRAME SECTION FROM STR 18L TO STR 21L REF. DRWG SH670-31810 REV. Y, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51SDR HNAA2022071800241None · noneE922303 - FRAME 67 IS CRACKED AT CARGO DOOR SILL .... REMOVED AND REPLACED FRAME 67 (LOWER FRAME SECTION) AT CARGO DOOR SILL IAW EMB145 SRM 51-40-02.SDR SWIA202265984None · corrodedFWD WET AREA - RH CROSSBEAM 14 CORRODED AS MARKED / REPAIRED R/H CROSSBEAM FR 14. REF EMB 53-00-10/REPAIR03P. SEE CONTINUATION FOR WORK PERFORMED. REPAIR MATERIAL WEIGHS 782 GRAMS. WEAIGH SCALE ASSET# S44-61127 DUE 03-28-23SDR DALA2022062704479Frame · noneSHIP 686 DTE, ERA 599756-14 REV -, MONITOR INSPECTION LOG REPAIR AT FRAME STA 1460 BETWEEN S-25L & S-27L REQUIRES ADDITIONAL ENGINEERING APPROVAL, AN EXISTING REPAIR WAS FOUND AFFECTING THE STA 1460 BOTTOM FRAME, BETWEEN S-25L & S-27L. REF ERA 599756-14 REV ORSDR 2A6D20220623001Support Beam · elongatedDAMAGE WAS DISCOVERED ON THE L/H BEAM UNDER THE ENGINE DECK (P/N: 355A21-2110.25) IN THE FORM OF AN ELONGATED HOLE IN THE LOWER FLANGE NEAR THE AFT END OF THE PARTSDR SWIA202266372None · corrodedCOCKPIT FLOOR STRUCTURE CENTER CROSS BEAM AT FRAME 11 CORRODED AS MARKED / (C-CHECK RO 8/29/2022) BLENDED COCKPIT FLOOR STRUCTURE CROSS BEAM AT FR 11 2EA LOCATIONS. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-10/AD02. ASSET#:TC2-8911 CAL DUE:11-9-22SDR SWAA2022072821729Stub Frame · crackedR-1 DOOR FWD FRAME UPPER STUB FRAME HAS A CRACK / [01] PLACED EWIS PROTECTION AROUND R-1 DOOR AREA PER B737-700 AMM 20-60-07-913-801.;[02] VARIFIED STEP 1;[03] APPLIED PAINT STRIPING TO OUTER FUSELAGE SKIN AT R-1 DOOR FWD FRAME PER B737-700 AMM 51-21-11-150-80SDR DALA2022062704488Frame · cracked(LOG 2288381) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 867 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 867 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062304388Frame · cold solder jtSHIP 3230 NEED TO COLDWORK HOLE 8 AND HOLE 9 IN ACCORDANCE WITH WORK CARD 5311-01171-03A. CORRECTIVE ACTION: COMPLIED WITH COLD WORKING. OK FOR SERVICE. (2289588)SDR AALA202210048827Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK RIGHT HAND WINDOW FRAME 4 VERTICAL STIFFENER. REPLACED WINDOW FRAME PER EA 337210.SDR SWIA202266371None · corrodedCORROSION CENTER FUSELAGE III FRAME 80 JUST OUTBOARD OF STRINGER 28R CORRODED. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED CENTER FUSELAGE III FRAME 80 R/H LOWER SECTION REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. FRAME 80 REPLACED WITH SDR DALA2022062404454Frame · cracked(LOG 2288188) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 500D BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 500D BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062404453Frame · cracked(LOG 2288177) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 827 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 727 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062404452Frame · cracked(LOG 2288161) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 727B BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 727B BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062404451Frame · cracked(LOG 2288152) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 500C BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062404450Frame · cracked(LOG 2288043) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 500A BTW S-8 AND S-9. AD. CRACKS ON LH FUSELAGE FRAME STA 500 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062404449Frame · cracked(LOG 2288030) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 480 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 480 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062404448Frame · cracked(LOG 2288018) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 440 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 440 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062404447Frame · cracked(LOG 2288000) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 400 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 400 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062404446Frame · cracked(LOG 2287988) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 380 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 380 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.SDR DALA2022062204357Frame · crackedSHIP 3121 - CRACK INDICATION ON FRAME FR16 LH, DOOR STOP 7, HOLE 3 (LOWER INB) ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR LOC FRAME 16 LH, DOOR STOP 7, HOLE 3 AS PER ER/ A 599711-14AD REV. ORIGINAL(2287502)SDR DALA2022062204356Frame · crackedSHIP 3121 - CRACK INDICATION ON FRAME FR 16 LH, DOOR STOP 7, HOLE 1 (UPPER INB) ON UPPER FUSELAGE . CORRECTIVE ACTION: PERFORMED REPAIR LOC FRAME 16 LH, DOOR STOP 7, HOLE 1 AS PER ER/ A 599711-14AD REV. ORIGINAL(2287509)SDR DALA2022062104315Frame · corrodedSHIP 178 EO TASK HFEC INSPECTION FOUND 01 EA CRACK AT LH-BS859.5 FRAME INNER CHORD TRANSITION RADIUS, CORRECTIVE ACTION: LH CABIN AT STA 859.5 FRAME. 01 EA CRACKED INNER CHORD TRANSITION RADIUS REPAIRED AND ACCOMPLISHED AS PER W/C:5311- 01195-09A. (2286961)SDR SWIA202266088None · corrodedFUSELAGE FRAME FS265 REINFORCEMENT ANGLE CORRODED BETWEEN STGR 26L AND 26R. (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED THE NEW STIFFENER ANGLE TO FRAME FS.265 LOWER SECTION REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG #CC670-34020 REV.-A. COMPLIED SDR DALA2022062304384Frame · cracked(LOG 2286321) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 440 BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 440 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-04B.SDR DALA2022062304382Frame · cracked(LOG 2286284) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 480 BTW S-8 AND S-9 (INBD & OUTBD FASTENER HOLES OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 480 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-04B.SDR DALA2022062304381Frame · cracked(LOG 2286216) DURING INSPECTION FOUND CRACK ON RH FUSELAGE FRAME STA 500F BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 500F BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.SDR DALA2022062304380Frame · cracked(LOG 2286207) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 400 BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 400 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.SDR DALA2022062304379Frame · cracked(LOG 2286195) DURING INSPECTION FOUND CRACK ON RH FUSELAGE FRAME STA 827 BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 827 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.SDR DALA2022062304378Frame · cracked(LOG 2286174) DURING INSPECTION FOUND CRACK ON RH FUSELAGE FRAME STA 727B BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET). CRACKS ON RH FUSELAGE FRAME STA 727B BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.SDR DALA2022062304377Frame · cracked(LOG 2286166) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 (INBD & OUTBD FASTENER HOLES OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.SDR DALA2022062304376Frame · cracked(LOG 2286136) DURING INSPECTION FOUND CRACK ON RH FUSELAGE FRAME STA 500H BTW S-8 AND S-9 (INBD FASTENER HOLE OF SUPPORT BRACKET). CRACKS ON RH FUSELAGE FRAME STA 500H BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.SDR DALA2022062304375Frame · cracked(LOG 2286104) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 500A BTW S-8 AND S-9 (INBD & OUTBD FASTENER HOLES OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 500A BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.SDR SWAA2022072920512Frame · crackedFWD CABIN WET AREA L/H FUSELAGE ATTACHED FRAME CRACKED @ LOWER FLAGE CUTOUT ABOVE L-1 DOOR CUTOUT SILL STA 312 MKD DOT / [01] REMOVED FASTENERS AS REQUIRED TO ACCESS REPAIR UPPER CHORD AT STA 312 BETWEEN STG 5L AND 6L IN REFERENCE B-737 SRM 51-40-02.;[02] VERISDR R61A2022070700420Panel · corrodedWHILE AC WAS IN FOR HVY CK FOUND CENTER FUSE 3 CORROSION FOUND ON WASTE ACCESS DOOR SKIN, HINGE, BRACKET. REPLACED WASTE DOOR PANEL PN 170-86668-403 IAW AMM 20-10-01. AC REMAINS IN HVY CK FOR COMPLETION.
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