JASC 5521
Service difficulty reports · 520
Reports filed under 5521 · Elevator, Spar/Rib, 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 = '5521' 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 = '5521' 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 UPS203493Rib · crackedWHILE IN C-CHECK, MAINTENANCE FOUND RT NR 4 BALANCE BAY I/B RIB CRACKED. REPLACED RIB IAW SRM 51-30-2, 51-30-5.SDR UPS203445Rib · crackedWHILE IN C-CHECK, MAINTENANCE FOUND RT ELEVATOR SUPPORT RIB AT STA 99.79 IS CRACKED. REPLACED RIB IAW SRM 51-30-2.SDR DL72S952250Spar · oversized holesOVERSIZED HOLES WERE FOUND IN THE REAR SPAR AND SKIN. THE SPAR WAS REPAIRED PER SRM 55-20-1 AND THE SKIN WAS REPAIRED PER SRM 55-20-3, FOR THE RIGHT ELEVATOR AT HMV.SDR 95ZZZX3250Channel · crackedFOUND BOTTOM FORWARD CHANNEL CRACKED ON LEFT ELEVATOR INBOARD FORWARD RIB. SUBMITTER RECOMMENDS REINFORCING CHANNEL PLATES ON ELEVATOR RIBS.SDR DL767952598Rib · delaminatedDURING SHOP INSPECTION, NR 1 RIB FROM I/B EDGE FOUND TO BE CRACKED AT FWD EDGE, NR 2 RIB FROM I/B EDGE FOUND TO BE CRACKED AT FWD EDGE, AND NR 8 RIB FROM I/B EDGE WAS DELAMINATED AT FWD EDGE. REPAIRED RIBS AS PER SRM 55-20-02, FOR RT ELEVATOR.SDR 9505349948Spar Cap · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 1.25 INCH CRACK IN THE LEFT ELEVATOR SPAR CAP STA 156 AND A .75 INCH CRACK IN THE RIGHT ELEVATOR SPAR CAP STA 74. OVERHAULED BOTH PER CMM 27-27-30.SDR 9504481152Rib · damagedDURING PERIODIC CHECK, FOUND THE RIGHT DETACHABLE ELEVATOR RIB DAMAGED AT FS XE =67.226, 49.5 INCHES FROM TRAILING EDGE. REPAIRED PER SRM 55-20-00.SDR 95ZZZX2123Rib · crackedINSPECTION ON LEFT ELEVATOR INBOARD WHERE TORQUE TUBE ATTACHES TO END RIB, FOUND RIB AND BRACKET CRACKED. REPLACED PARTS WITH NEW.SDR 95ZZZX2121Rib · crackedFOUND RIB AND BRACKET CRACKED ON LEFT ELEVATOR INBOARD WHERE TORQUE TUBE ATTACHED TO END RIB. CAUSE UNKNOWN. REPLACED PARTS WITH NEW. SPAR END ALSO CRACKED FROM WORKING OF TORQUE TUBE. REPAIRED BY DOUBLER IAW AC 43.13.SDR 95ZZZX1909Rib · crackedEND RIB WHERE PN 1532009-203 ATTACHES, BADLY CORRODED AND CRACKED. ELEVATOR ACTUATING ARM HAS STEEL BRACKET, WAS BADLY RUSTED AND RIVETS SHEARED.SDR 95ZZZX1722Rib · corrodedLEFT ELEVATOR TIP RIB WAS FOUND PERFORATED BY CORROSION UNDER MASS BALANCE WEIGHTS C2TE-113 AND DASH 115. ONLY ONE FASTENER WAS RETAINING THE WEIGHTS. THE LEAD WEIGHTS ARE ON BOTH SIDES OF THE ALUMINUM RIB AND ARE RETAINED BY STEEL SCREWS. THE CONDITIONS ARSDR 95ZZZW562Rib · crackedDURING A SCHEDULED INSPECTION IN CKB, MAINTENANCE FOUND THE RIGHT ELEVATOR STATIC WICK FAIRING CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE INBOARD SKIN PANEL, P/N 8550057-014 AND RIBS P/N'S 85520100-102 AND 855200028-102 IAW DEHAVILLAND SRM 51-40-00. (WSDR 95ZZZW561Rib · crackedDURING A SCHEDULED INSPECTION IN CKB, MAINTENANCE FOUND THE RIGHT ELEVATOR STATIC WICK FAIRING CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE INBOARD SKIN PANEL, P/N 8550057-014 AND RIBS P/N'S 85520100-102 AND 855200028-102 IAW DEHAVILLAND SRM 51-40-00. (WSDR DL72S950763Rear Spar · crackedDURING INSPECTION, THE RT ELEVATOR REAR SPAR WAS FOUND TO HAVE A CRACK EMANATING .25 INCH FROM INBD SIDE OF THE SHEAR PLATE AT THE SECOND FROM OUTBD TAB HINGE FITTING-TO-REAR SPAR ATTACHMENT. IN ACCORDANCE WITH B727 S/B 55-0087, THE CRACK WAS STOP DRILLED ANDSDR DL72E950758Spar · crackedDURING INSPECTION, THE RIGHT ELEVATOR REAR SPAR WAS FOUND TO HAVE A CRACK EMANATING .1250 INCH FROM THE INBD SIDE OF THE SHEAR PLATE AT THE SECOND FROM THE OUTBD TAB HINGE FITTING TO REAR SPAR ATTACHMENT. THE CRACK WAS STOP DRILLED IN ACCORDANCE WITH B727 S/BSDR 95ZZZX1102Bracket · crackedWHEN INSPECTING ACCORDING TO CESSNA SB SE 84-17, FOUND 2 CRACKS AT LT BRACKET ATTACHMENT SCREW.SDR DLL17950728Spar · crackedDURING LETTER CHECK, FOUND RIGHT ELEVATOR, SPAR WEB CRACKED AT LIGHTENING HOLE JUST INBOARED OF THE OUTBOARD ATTACH FITTING. REPAIRED PER SRM 55-21-00.SDR 95ZZZX600Spar · crackedUPON REPLACEMENT OF OUTBOARD HINGE ATTACHMENT OF RT ELEVATOR, CRACKS WERE FOUND IN SPAR. INSPECTION OF LT ELEVATOR REVEALED SAME CRACKS ONLY WORSE. CRACKS ARE FOUND BY BOLT HOLES FOR OUTBOARD HINGE ATTACHMENTS. CRACKS CAN BE SEEN THROUGH HOLES IN OUTBOARD RSDR 95ZZZX599Spar · crackedUPON REPLACEMENT OF OUTBOARD HINGE ATTACHMENT OF RT ELEVATOR, CRACKS WERE FOUND IN SPAR. INSPECTION OF LT ELEVATOR REVEALED SAME CRACKS ONLY WORSE. CRACKS ARE FOUND BY BOLT HOLES FOR OUTBOARD HINGE ATTACHMENTS. CRACKS CAN BE SEEN THROUGH HOLES IN OUTBOARD RSDR DL72S950033Angle · crackedDURING LETTER CHECK, THE LEFT ELEVATOR INTERNAL SUPPORT ANGLE INSIDE ACCESS PANEL 9307 WAS FOUND CRACKED. REPAIRED PER SRM 55-21-4 FIG 1.
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