JASC 5550
Service difficulty reports · 66
Reports filed under 5550 · Empennage Flight Control Surfaces, Attach Fittings, 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 = '5550' 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 = '5550' 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 C2XA00IA379Pin · corrodedREFERENCE OPEN SDR C2XA00IA337 DURING C-CHECK INSPECTION, LT HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED PIN, AND A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA337Pin · corrodedDURING C-CHECK INSPECTION, THE LT HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. THIS SDR IS BEING FILED OPEN AWAITING FINAL CORRECTIVE ACTION.SDR USAA001356Clevis · corrodedCLT - FOUND CLEVIS LUG CORRODED .5 INCH BY .5 INCH, RIGHT HORIZ STAB FORWARD UPPER CLEVIS ON BOX BEAM. CORROSION LEVEL 1. MACHINED SPOT FACES BOTH FORWARD AND AFT CLEVIS LUGS PER SRM 55-10-10. (M)SDR USAA001355Clevis · corrodedCLT - FOUND CLEVIS LUG CORRODED .5 INCH BY .5 INCH, FORWARD AND AFT CLEVIS LUGS LEFT HORIZ STAB. MACHINE SPOT FACES BOTH FORWARD AND AFT CLEVIS LUGS PER SRM 55-10-10. CORROSION LEVEL 1. (M)SDR USAA001354Clevis · corrodedCLT - FOUND FORWARD UPPER LUG CLEVIS CORRODED .5 INCH BY .75 INCH, RIGHT HORIZ STAB. INSTALLED NEW BUSHING PER SRM 55-10-10 AND SRM 20-10-03. (M)SDR QXEA0002198Bracket · crackedPDX- FUSELAGE BOTTOM PANEL 98F SUPPORTING BRACKET IS CRACKED AT STATION 16495. REPAIRED IAW FOKKER SRM 55-53-04, PAGE 9 AND SRM 51-31-01.SDR C2XA00IA216Fitting · corrodedDURING CONTINENTAL EXPRESS C-CHECK, THE NR 1 RUDDER BOTTOM ATTACH FITTING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ATTACH FITTING IAW EMB145 MM 55-31-01-400-801A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 20000720SH006Fitting · crackedFOUND CRACK RUNNING FROM .25 INCH MOUNTING HOLE TO EDGE OF PART. POSSIBLE CAUSE WAS OVERTORQUE OF FITTING TO ELEVATOR BELLCRANK ATTACH BOLT. FITTING TIES ELEVATOR TORQUE TUBE TO BELLCRANK ASSEMBLY. (X)SDR DL73K001231Fitting · corrodedDURING HMV CORROSION WAS FOUND ON THE AFT FACES OF THE LEFT AND RIGHT VERTICAL STABILIZER PRIMARY REAR SPAR TERMINAL FITTING. THE AREA WAS BLENDED AND TREATED PER ERA 334527-14AT HMV.SDR SWAA000995Attach Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB LT FWD, AFT AND RT AFT PRIMARY BODY ATTACH LUGS CORRODED. REPAIRED LUGS PER ER 00-5162.SDR 20000720SH013Fitting · crackedUPON INSPECTION, NOTICED A CRACK BEHIND UPPER LEFT BOLT HOLE EXTENDING TO RIVET HOLE. (X)SDR RRXA000012Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, BRACKET FOR H.F. ANTENNA CANNON PLUG CRACKED & CORRODED VERT STAB TIP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & SDR C2XA99IA637Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101SDR C2XA99IA636Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101,SDR DLM88971327Elev Hinge Ftg · corrosionTHE XE = 157-.9 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT HORZ STABILIZER WAS FOUND TO CONTAIN CORROSION. THE CORROSION WAS DISCOVERED IN THE BORE OF THE INBOARD LUG OF THE BRACKET UPON BUSHING REMOVAL. THE CORROSION WAS REMOVED BY OVERSIZING THE DIASDR AU961163Fitting · loose(AUS) RUDDER LOWER ATTACHMENT FITTING NOT SECURED BY RIVETS ON TOP AND BOTTOM SIDES - SUSPECT MANUFACTURING ERROR
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