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 DALA2024022502575Frame · crackedSHIP 3267 DISC: CRACK INDICATION ON FRAME 68 LH SIDE IN FRAME WEB AFT FACE HORIZONTAL FLANGE AT LEVEN OF STGR 22, CRACK LENGTH IS 0.688 INCH. REQUESTING REP AIR DISPOSITION. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED, AND REPAIR MUST BE ACCOMPLISHED PRIOSDR DALA2024022202462Frame · crackedCRACK ON FRAME STA Y1037 OVER LONG 17 LH AT CPAX. SUMMARY OF NRC 00408: FRAME STA Y1037 OVER LONG 17 LH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. PERFORM AN GVI ON FRAME STA Y=1037 OVER LONG 17 LH AT CPAX EVERY "C" CHECK PER B717 SRM 53-20SDR I5EA2024031400008Frame · damagedFWD CARGO COMPARTMENT STA 500C BETWEEN STR 20L TO STR 21L FRAME HAS DOUBLE HOLE. INSTALLED ANGLES ( 2 EA ) REPAIR ON FWD CARGO COMPARTMENT STR 20L TO 21L FRAME IAW B737-400 SRM 51-30-02, 51-30-01, AND 51-40-02.SDR JJBA20240304024Frame · crackedCF4, CRACK FOUND ON LH FRAME 59 AT FLOOR STRUCTURE BTW STR 15L-16L. FRAME REPAIREDSDR DALA2024022302552Frame · crackedSHIP 5657 FOUND 1EA CRACK IN THE FUSELAGE FRAME (INBOARD UPPER FASTENER HOLE) AT LEFT BS 1640, S-14. CORRECTIVE ACTION: REPAIRED FRAME @STA. 1640, STR 14L PER ER/A 615799-14AD REV ORIGINAL. (0211744)SDR DALA2024022302549Frame · bentSHIP 698 BENT FRAME STA 1320 BTW S-27R AND S-26R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00573: FRAME STA 1320 BTW S-27R AND S-26R AT AFT CARGO COMPARTMENT.WAS REPAIRED PER B757-200 SRM 53-00-07-2R PROCEDURE 5, REPAIR 5. (0212443)SDR AALA202402215284Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT CARGO COMPARTMENT FORWARD BULKHEAD FRAME INNER CHORD WEB ASSEMBLY AT STA 727, STR 18A LEFT. REPAIRED WEB AT LEFT HAND STA 727 STR 18A PER EA 350812 AND SRM 51-40-02-OG.SDR AALA202402272860Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FASTENER HOLE 6 AND FASTENER HOLE C IN THE DOUBLE JOGGLE AREA FOR DOOR STOP 7 AT FR 16 AND S10R. REPLACED FRAME PER EA 349690.SDR DALA2024022002326Frame · crackedCRACKED FRAME ON STA Y=715 BTW S-27L AND S-28L AT CANTED KEEL BEAM AREA. (FUS) SUMMARY OF NRC 0549: CRACKED FRAME ON STA Y=715 BTW S-27L AND S-28L AT CANTED KEEL BEAM AREA WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. PERFORM AN EXTERNAL GVISDR DALA2024022002325Frame · crackedA.D. CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00265: CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH WAS REPAIRED PER AMDSDR 2024FA0000181Frame · crackedWHILE PERFORMING INSPECTIONS AS PER ADSI IB744530107, QTY: 02 OFF FASTENER HOLES ON STA 840 LH FRAME ASSY WERE FOUND CRACKED.SDR DALA2024022102426Frame · cracked(LOG 0207515) RIGHT FUSELAGE FRAME STA 907 IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 907 AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-03B.SDR DALA2024022102425Frame · cracked(LOG 0207510) LH FUSELAGE FRAME STA 907 IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L - 9L. REPAIRED LH FUSELAGE FRAME STA 907 AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-03A.SDR DALA2024022102424Frame · cracked(LOG 0207506) RIGHT FUSELAGE FRAME STA 727D IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 727D AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-04B.SDR DALA2024022102423Frame · cracked(LOG 0207502) RIGHT FUSELAGE FRAME STA 867 IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 867 AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02B.SDR DALA2024022102422Frame · cracked(LOG 0207499) RIGHT FUSELAGE FRAME STA 727B IS CRACKED AT THE I/B FASTENER OF AC RAIL ATTACH BRACKET STR 8. REPAIRED RH FUSELAGE FRAME STA 727B AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02B.SDR DALA2024022102421Frame · cracked(LOG 0207496) LH FUSELAGE FRAME STA 727B IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L - 9L. REPAIRED LH FUSELAGE FRAME STA 727B AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02A.SDR DALA2024022102420Frame · cracked(LOG 0207488) LH FUSELAGE FRAME STA 500D IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L - 9L. REPAIRED LH FUSELAGE FRAME STA 500D AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02A.SDR DALA2024022102419Frame · cracked(LOG 0207478) RIGHT FUSELAGE FRAME STA 500C IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED FUSELAGE FRAME STA 500C AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-04B.SDR DALA2024022102418Frame · cracked(LOG 0207465) RIGHT FUSELAGE FRAME STA 500A IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 500A AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02B.SDR DALA2024022102417Frame · cracked(LOG 0207454) FUSELAGE FRAME STA 500C IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L - 9L. REPAIRED LH FUSELAGE FRAME STA 500C AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02A.SDR DALA2024022102416Frame · cracked(LOG 0207421) LH FUSELAGE FRAME STA 500A IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L & 9L. REPAIRED LH FUSELAGE FRAME STA 500A AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-1236-04A.SDR DALA2024022102415Frame · cracked(LOG 0207403) RIGHT FUSELAGE FRAME STA 440 IS CRACKED AT THE I/B, O/B FASTENER AND IN THE RADIUS AT THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED FUSELAGE FRAME STA 440 AT THE AC RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-04B.SDR DALA2024022102414Frame · cracked(LOG 0207386) RIGHT FUSELAGE FRAME STA 480 IS CRACKED AT I/B & O/B FASTENERS OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 480 AT AC BIN RAIL BRACKET IAW DELTA TASK CARD 2526-01236-02B.SDR DALA2024022102413Frame · cracked(LOG 0207369) FUSELAGE FRAME STA 440 IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STR 8L & 9L. REPAIRED LH FUSELAGE FRAME STA 440 AT AC BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02A.SDR DALA2024022102412Frame · cracked(LOG 0207353) FUSELAGE FRAME STA 400 IS CRACKED AT I/B HOLE FOR BIN ATTACH BRACKET BETWEEN STA 8L & 9L. REPAIRED LH FUSELAGE FRAME STA 400 AT AC BIN RAIL BRACKET IAW DELTA TASK CARD 2526-01236-02A.SDR DALA2024022102411Frame · cracked(LOG 0207337) RH FUSELAGE FRAME STA 400 IS CRACKED AT THE I/B FASTENER OF THE AC BIN RAIL BRACKET AT STR 8R. REPAIRED RH FUSELAGE FRAME STA 400 AT BIN RAIL ATTACH BRACKET IAW DELTA TASK CARD 2526-01236-02B.SDR DALA2024022102410Frame · cracked(LOG 0207323) FUSELAGE FRAME AT STA 380 IS CRACKED AT I/B AND O/B HOLES FOR BIN RAIL ATTACH BRACKET BETWEEN STA 8L & 9L. REPAIRED LH FUSELAGE FRAME STA 380 AT BIN RAIL BRACKET IAW DELTA TASK CARD 2526-01236-04A.SDR DALA2024022102409Frame · cracked(LOG 0207293) RIGHT FUSELAGE FRAME STA 380 IS CRACKED AT THE I/B FASTENER OF THE AC RAIL ATTACH BRACKET AT STR 8. REPAIRED RH FUSELAGE FRAME STA 380 AT AC RAIL BRACKET IAW DELTA TASK CARD 2526-01236-02B.SDR DALA2024022002361Frame · crackedAIRCRAFT 0175, FOUND CABIN LH FRAME END FITTING ABOVE CENTER FUEL TANK AT STA 927 CRACKED. CORRECTIVE ACTION: REMOVED THE CRACKED FRAME END FITTING AT STA 927.5 LBL 97.42 AND FABRICATED A NEW FITTING AND TREATED PAINTED AS PER PRI 615753-14 REV 0.THE PRI 61575SDR DALA2024022102362Frame · crackedSHIP 3267 DISC: CRACK INDICATION ON FRAME 68 LH SIDE, HOLE 4 (I/B LOWER HOLE) DOOR STOP 1. D1-D2= 0.109 INCH. DIAMETER HOLE: 0.250 INCH. AA 5311-01216. AD RELATED. ACTION REQUIRED PRIOR TO FURTHER FLIGHT. IN PASSENGER CABIN (1 EA) (CRACK AT 11 O CLOCK) C/A: PESDR IPXA2024032607705Frame · corrodedTHE MIDDLE FASTENER HOLE FOR L/H SIDE FRAME 40 UPPER JUNCTION HAS CORROSION / DAMAGE INDICATIONS INSIDE THE HOLE. AREA MARKED IN RED. ACCOMPLISH TIME LIMITED REPAIR PER EO-89836-REQ1 AND EA 300-5710-27-A3522 REV.SDR DALA2024022002316Frame · crackedSHIP 175 FOUND CABIN RH FRAME END FITTING ABOVE CENTER FUEL TANK AT STA 927 CRACK. CORRECTIVE ACTION: THE CRACKED RH FRAME END FITTING (CRACK LENGTH IS 1.7") AT STA 927 REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 (0203921)SDR ABXA2024021900629Frame · crackedDATUM AIRCRAFT IS IN CPZ FOR C24 MAINTENANCE CHECK. CPZ WAS TASKED WITH ACCOMPLISHING INSPECTIONS OF THE STA 1809.5 DATUM AIRCRAFT IS IN CPZ FOR C24 MAINTENANCE CHECK. CPZ WAS TASKED WITH ACCOMPLISHING INSPECTIONS OF THE STA 1809.5 BULKHEAD OUTER CHORD (LH) ASSDR AALA202404126727Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME LOWER INBOARD FASTENER HOLE FOR DOOR STOP FITTING #1 AT FR 68 AND S22L. REPAIRED FRAME PER EA 352259.SDR AALA202404126333Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME LOWER INBOARD FASTENER HOLE FOR DOOR STOP FITTING #1 AT FR 68 AND S22R. REPAIRED FRAME PER EA 352275.SDR DALA2024021602282Frame · crackedSHIP 1605 CABIN RH FRAME END FITTING CRACK AT FUEL TANK UPPER SURFACE AT STA 852. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER PRI:615402-14.SDR DALA2024021502246Frame · crackedSHIP 3124 CRACK INDICATION FOUND ON FR16 RH SIDE DOUBLE JOGGLE AREA LOCATED IN HOLE 6. CORRECTIVE ACTION: REPAIRED PER ER/A 614228-14AD. (0201028)SDR EE4Y2024021419450Frame · out of toleranceDURING ACCOMPLISHMENT OF ALLEGIANT ENGINEERING ORDER E5311-0019 FR 16 LH DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP # 7 HOLES # 1 THRU #6,#8,#B,#D AND AT LEVEL OF DOR STOP#1 HOLES #9 THRU #19 WERE FOUND GREATER THAN THE STARTING HOLE DIAMETER FOR COLDWORK PROCESSDR EE4Y2024021419449Frame · out of toleranceDURING ACCOMPLISHMENT OF ALLEGIANT ENGINEERING ORDER E5311-0018 FR 16 RH DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP # 7 HOLES # 1,#2,#4 THRU #8, #A THRU D AND AT LEVEL OF DOR STOP #1 HOLES #9,#10,#12 THRU #19 WERE FOUND GREATER THAN THE STARTING HOLE DIAMETER SDR EE4Y2024021419448Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 534123-01-2-001 FR 66 RH SIDE INNER CAP JOINTTO GUSSET PLATE AT STGR 10R FOUND FIRST HOLE (FROM UP TO DOWN) WITH CRACK. THE REPAIR WASPERFORMED FOLLOWING THE REPAIR INSTRUCTIONS AS PER A319 SRM 53-41-12-300-018.THE RSDR EE4Y2024021419444Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT ENGINEERING ORDER E5311-0019 , FR 16 AT DOUBLE JOGGLE AREA LH SIDE HOLE # 13 HAS BEEN FOUND WITH CRACK INDICATION.AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR SOLUTION UNDER DOSSIER 81014204SDR EE4Y2024021419443Frame · crackedDURING ALLEGIANT TASK 53-120-003 ACCOMPLISHMENT FR 16 LH CROSSBEAM SPLICING UPPER ROW OF FASTENER HOLE IDENTIFIED AS H2 WITH CRACK WAS FOUND.AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81345090. THE RESDR SWAA2024031352107Frame · crackedCRACK FRAME ON BS 312 BETWEEN STR 5L TO STR 6L FWD GALLEY AND LAV 2024-123220<[01] PERFORMED REPAIR ON FRAME IAW EA M-22-153-0124.;[02] CORRECTED STEP 1.<BR>PERFORMED REPAIR ON FRAME IAW EA M-22-153-0144. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[03] CORRECTED STEP 2.SDR ASAA2024021348097Frame Splice · corrodedAFT CARGO COMPATMENT, RIGHT FRAME SPLICE CORRODED AT STA 727I (AREA MARKED IN RED). GROUNDED - YES. EVAL'S CORRODED AFT PIT R/H FRAME SPLICE AT STA 727I. CORROSION IS LOCATED ON THE INNER CHORD. DAMAGE IS NOT PERMITED ON THIS LOCATION IAW B77-900ER SRM 53-00-0SDR DALA2024021402188Frame · crackedSHIP 187 REPAIR WAS REQUIRED DUE TO A CRACK IN FRAME STA 720 AND COMPLETED PER ERA 615867-14. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. CORRECSDR SWI2024F00116Skin · scratchedDEEP SCRATCHES ON THE LEFT SIDE OF FUSELAGE ABOUT 8€™ FROM THE MAIN CABIN DOOR. (FLIGHT 3270 FILED OPEN)DAMAGE HAS BEEN EVALUATED AND DETERMINED TO BE OUT OF LIMITS. SEE EAML 1296863 FOR DAMAGE.SDR DALA2024021402135Frame · crackedSHIP 3128 CRACK INDICATION ON FRAME 16 RH SIDE IN INTERCOSTAL FITTING OPEN FASTENER HOLE H1. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING LOC. BTW FR15 TO FR16 RH AT LEVEL DOOR STOP 7 AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0200566)SDR EE4Y2024021319442Frame · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK 53-260 -003 DOOR STOP FITTING # 1 I/B LOWER HOLE AT FR68 WEB LH SIDE HAS BEEN FOUND CRACKED.AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS AND APPROVAL DOCUMENTATION. THE REPAIR SDR SWAA2024031351007Frame · crackedCRACK FRAME ON BS 312 BETWEEN S-5L TO S-6L FWD GALLEY AND LAV 2024-121484<[01] REPAIRED FRAME ON BS 312 BETWEEN S-5L TO S-6L FWD GALLEY AND LAV IAW M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPAIRED FRAME ON BS 312 BETWEEN S-5L TO S-6L FWD GALLEY AND
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