JASC 5350

Service difficulty reports · 6,124

Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350'
  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.

SDR DL72W951202Fillet Pnl · damagedAT HMV, FILLET PNL 3441 FOUND WITH TIME LIMITED REPAIR. CUT OUT DAMAGE MFG SPLICE REPLACEMENT SECTION AND DOUBLER AS PER SRM 53-30-3 FIG 2, PER 53-50-1 FIG 1. INSTALLED REPAIR PER SRM 53-30-3 FIG 2,PER 53-50-1 FIG 1.Mar 5, 1995 · N2813W · Boeing 727247SDR DL757951298Radome · delaminatedINTERIOR AFT EDGE OF RADOME DELAMINATED AT 12 O'CLOCK POSTION. DAMAGE OCCURED WHILE INSTALLING RADOME IN HANGAR. REPAIRED AS PER SRM 53-10-72. REMOVED HINGES AND HINGE BRACKET, REPAIRED FIBERGLASS, INSTALLED BRACKET AND HINGES, AND PAINTED AS PER PS 900-9-1Mar 2, 1995 · N610DL · Boeing 757232SDR 9503549852Release Mech · wornDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. ALSO, FOUND A WORN CABLE SLIDER BLOCK AND LATCH LOCK ARM. REPLACED THE BLOCK AND ARM AND RERIGGED THE TAILCONE. CHECKED OK.Mar 2, 1995 · N761NC · Doug DC951SDR DL757951627Radome · delaminatedRADOME WAS ROUTED TO SHOP FOR REWORK, DUE TO DAMAGE FROM DELAMINATION AND MOISTURE ENTRAPMENT. REWORKED RADOME PER SRM 53-10-72.Mar 1, 1995 · N610DL · Boeing 757232SDR 95ZZZX1254Latch · not latchedTOP 2 LATCHES WERE NOT LATCHED PERFECTLY ALLOWING PRESSURE SEAL TO BLOW OUT AT THE TOP BETWEEN THE LATCHES. SUBMITTER SUGGESTION IS TO LATCH THE 2 TOP LATCHES FIRST TO INSURE THEIR INTEGRITY.Mar 1, 1995 · N428DA · Lkheed 1329SDR 9503089923Clips · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ADJUSTED THE CLIPS. CHECKED OK.Feb 26, 1995 · N927RC · Doug DC932SDR 9502599981Clips · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ADJUSTED THE INTERIOR AND EXTERIOR CLIPS.Feb 13, 1995 · N994Z · Doug DC931SDR 9502609951Cable · frayedDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ALSO, FOUND THE TAILCONE CABLE FRAYED BETWEEN THE RIGHT SIDE LATCHES AT THE LOWER PULLEY. REPLACED THE CABLE AND RERIGGED THE TAILCONE.Feb 12, 1995 · N9347 · Doug DC932SDR 9502059756Latches · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE LATCHES. CHECKED OK.Feb 9, 1995 · N756NW · Doug DC941SDR 9501989863Lock Arm · wornDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ALSO, FOUND THE UPPER LEFT LOCK ARM WORN. ADJUSTED HANDLE AND REPLACED/RE-RIGGED THE LOCK ARM. CHECKED OK.Feb 4, 1995 · N772NC · Doug DC951SDR DL757950929Radome · delaminatedINITIAL SHOP INSPECTION, MAINTENANCE FOUND 2 LARGE AREAS OF DELAMINATION AT THE 7 O'CLOCK POSITION. ALL REPAIRS WERE ACCOMPLISHED AS PER SRM 53-10-72. INTERIOR SKIN AND ALL HONEYCOMB CORE WERE REPLACED DURING REPAIR PROCEDURES. UPON REPAIR BEING COMPLETED Feb 3, 1995 · N606DL · Boeing 757232SDR DL757950684Radome · delaminatedNOSE OF RADOME WAS DELAMINATED AND EXCEEDED MOISTURE LIMITS. REMOVED AND REPLACED INNER SKIN AS PER B-757 SRM 53-10-72. DAMAGE WAS REPAIRED DURING SHOP VISIT.Feb 2, 1995 · N675DL · Boeing 757232SDR USAA950091Fairing · looseCLT - FLT 2442 - ON CLIMB, AIRFRAME VIBRATION AT HGH POWER SETTNGS. NO VIBRATION AT IDLE POWER DESCENT OR LOW POWER SETTING. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE RUN AT ALL POWER SETTINGS. VIBRATION INDICAJan 31, 1995 · N441US · Boeing 7374B7SDR CAL950124Cables · out of adjustHOU - THE EXTERIOR TAILCONE RELEASE HANDLE REQUIRED LESS THAN 25 POUNDS PULL TO RELEASE THE TAILCONE. THE TAILCONE RELEASE CABLES WERE RIGGED IAW MM 53-53-00, SO THAT HANDLE PULL WAS WITHIN SPECIFICATION. (Z)Jan 28, 1995 · N16895 · Doug DC982SDR DL72S950438Fairing · crackedDURING INSPECTION, FOUND FUSELAGE TO WING BODY FAIRING RIGHT SIDE WITH A 7 INCH CRACK FS 720E PLUS 12 INCHES. REPAIRED PER SRM 53-30-3.Jan 26, 1995 · N401DA · Boeing 727232SDR 9501049154Clips · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS. RERIGGED TAILCONE. CHECKED OK.Jan 17, 1995 · N8913E · Doug DC914SDR 9501009959Clips · out of adjustDURING LINE CHECK EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS. REMOVED PRIMER FROM THE BALL END OF THE CABLE AND ADJUSTED THE CLIPS. CHECKED OK.Jan 16, 1995 · N919RW · Doug DC931SDR 9500999856Latch Lever · wornDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. ALSO, FOUND THAT THE CLEVIS PIN HOLE WAS WORN IN THE UPPER LEFT LATCH LEVER. REPLACED THE LATCH LEVER AND RERIGGED THE RELEASE MECHANJan 13, 1995 · N765NC · Doug DC951SDR CAL950048Clip · brokenHOU - THE FORCE REQUIRED TO PULL HANDLE FROM CLIPS WAS TOO LOW DURING TAIL CONE DROP TEST. REMOVED AND REPLACED BROKEN CLIP. (W)Jan 11, 1995 · N18835 · Doug DC982SDR CAL950047Cables · out of adjustHOU - THE TAILCONE RELEASE PULL TEST FAILED AT ALL THREE POSITIONS. THE TAILCONE RELEASE CABLES WERE RIGGED PER MM 53-53-00, PARAGRAPH 3A, PAGE 502, CONFIGURATION 1. (Z)Jan 11, 1995 · N18835 · Doug DC982SDR 9500739305Release Mech · lack of lubeDURING LINE CHECK, FOUND THAT THE TAILCONE FAILED TO RELEASE AND DROP. CHECKED RIGGING AND LUBRICATED THE RELEASE MECHANISM. CHECKED OK.Jan 11, 1995 · N307RC · Doug DC982SDR 9503623232Angle · crackedDURING 'C' CHECK, FOUND THE LEFT FUSELAGE BELLY FAIRING CONNECTING ANGLE FOR PANEL 193B CRACKED. THE CRACK, EMINATES FROM THE FORWARD MOST EDGE TO THE 3RD FASTENER HOLE APPROXIMATELY 6 INCHES AFT OF THE FORWARD EDGE. THE ANGLE IS ATTACHED TO THE LEFT OVERWINJan 10, 1995 · N332NW · Airbus A320211SDR CAL950027Latches · lack of lubeHOU - THE TAIL CONE INTERIOR RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE LATCHES WERE LUBRICATED AND THE INTERIOR RELEASE HANDLE PULL FORCE CHECKED GOOD PER MM 53-50-00. (X)Jan 8, 1995 · N16894 · Doug DC982SDR 9500649908Release Mech · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED RELEASE MECHANISM.Jan 7, 1995 · N958N · Doug DC931
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