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 USAAF97025Radome · damagedMDT - FL 1861 - AFTER TAKEOFF FROM PHL, CREW NOTED BIRD STRIKE ON LEFT SIDE OF NOSE. NO ADVERSE EFFECTS WERE NOTED ON COCKPIT GAUGES. FLIGHT CONTINUED. AT APPROXIMATELY 17,500 FEET, CREW NOTED THAT THE LEFT SIDE OF THE RADOME BEGAN TO COLLAPSE AND THE AIRSPMar 5, 1997 · N859US · Fokker F28MK0100SDR 9704849865Shear Pins · wornDURING LINE CHECK, FOUND THAT TAILCONE HUNG UP DURING FUNCTIONAL CHECK DUE TO STICKY SEAL. ALSO FOUND 12 SHEAR PINS WORN AND 3 BEARING PLATES WITH GROOVES IN THEM. CLEANED SEAL, REPLACED SHEAR PINS AND BEARING PLATES, FUNCTIONAL CHECK OK.Mar 4, 1997 · N774NC · Doug DC951SDR 9704819860Release Mech · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE. ALSO FOUND THAT TAILCONE DID NOT RELEASE WHEN LATCHES ROTATED. RIGGED TAILCONE RELEASE SYSTEM.Mar 4, 1997 · N769NC · Doug DC951SDR 9704809948Cables · frayedDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE EXTERIOR HANDLE FROM CLIPS AND TO RELEASE THE TAILCONE. ALSO FOUND CABLES FRAYED IN FOUR LOCATIONS. REPLACED CABLES, ADJUSTED CLIPS AND RIGGED RELEASE SYSTEM.Mar 4, 1997 · N8929E · Doug DC931SDR 9704979870Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERIOR TAILCONE RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS. FUNCTIONAL CHECK OK.Mar 3, 1997 · N779NC · Doug DC951SDR 9704879870Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERIOR TAIL CONE RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK.Mar 3, 1997 · N779NC · Doug DC951SDR 9704639948Release Mech · out of adjustDURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, TAILCONE DROP CHECK AND PULL TEST OF EXTERIOR HANDLE BOTH EXCEEDED MAXIMUM FORCE LIMITS. TAILCONE WAS RIGGED AND EXTERIOR HANDLE CLIPS WERE ADJUSTED.Mar 2, 1997 · N8929E · Doug DC931SDR CALA9700542Fillet · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING FILLET PANEL. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-51-0.Feb 27, 1997 · N17543 · Doug DC932SDR 9704259903Cables · damagedDURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DEPLOY THE TAILCONE. ALSO, FOUND COATING ON INTERIOR RELEASE HANDLE CABLE CRACKED. REPLACED CABLE, RIGGED CABLES AND LATCHES, FUNCTIONAL TEST OK.Feb 27, 1997 · N953N · Doug DC931SDR 9704059907Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL EXTERIOR RELEASE HANDLE FROM CLIPS. ADJUSTED CLIP PRESSURE.Feb 25, 1997 · N957N · Doug DC931SDR CALA9700496Rib · corrodedINSPECTION FOUND CORROSION ON RIB OF LOWER WING TO FUSELAGE FAIRING AT STA 1360. THE RIB WAS REMOVED AND A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 53-00-01.Feb 23, 1997 · N68046 · Doug DC1010SDR CALA9700329Fairing Support · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING TO BODY FAIRING SUPPORT AT STA 540, STRINGER 22. A .25 INCH CRACK WAS FOUND IN LT WING TO BODY FAIRING SUPPORT AT STA 540, STRINGER 22. THE SUPPORTS WERE REPAIRED IAW ECRA 5350-01227.Feb 20, 1997 · N17329 · Boeing 7373T0SDR CALA9700303Cables · out of adjustTHE TAILCONE RELEASE USING EXTERIOR HANDLE WAS LOW AT 20 POUNDS. THE TAILCONE RELEASE SYSTEM CABLES WERE ADJUSTED IAW MM 53-53-00.Feb 19, 1997 · N72822 · Doug DC982SDR CALA9700480Fairing · corrodedINSPECTION FOUND RT SIDE AFT NR 2 ENGINE FAIRING SKIN CORRODED WITH PULLED FASTENERS. THE SKIN WAS REMOVED AND REPLACED IAW SRM 54-32-01A AND 51-31-01.Feb 17, 1997 · N68041 · Doug DC1010SDR 9703399944Alignment Pins · wornDURING LINE CHECK, TAILCONE FAILED DROP CHECK, IT WAS HANGING UP ON TOP LEFT BAYONET. ALSO, FOUND ALIGNMENT PINS WORN. REPLACED WORN PINS AND RIGGED TAILCONE RELEASE SYSTEM, FUNCTIONAL CHECK OK.Feb 17, 1997 · N1309T · Doug DC931SDR 9703189917Clips · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL RELEASE HANDLE FROM CLIPS. ADJUSTED CLIP PRESSURE.Feb 11, 1997 · N967N · Doug DC932SDR 973009307Cable · frayedDURING LINE CHECK, TAILCONE FAILED TO DROP USING INTERIOR HANDLE. REPLACED CABLE AND RIGGED, DEPLOYMENT CHECK OK.Feb 9, 1997 · N309RC · Doug DC982SDR 9703209754Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL INTERIOR HANDLE FROM CLIPS. ALSO, FOUND THAT LOWER LEFT LATCH SPRING POPS OUT OF BAYONET HOLE. REPLACED SPRING AND ADJUSTED CLIP PRESSURE.Feb 8, 1997 · N754NW · Doug DC941SDR 9703219915Cable · damagedDURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DEPLOY TAILCON. ALSO, FOUND CABLE RUN NR 301C KNICKED. REPLACED CABLE, CABLE CONDUIT AND RIGGED TAILCONE RELEASE SYSTEM.Feb 6, 1997 · N965N · Doug DC931SDR P5CA9700262Fairing · corrodedLWR BODY FAIRINGS, CORROSION BY RAD ALT ANTENNAS AND CIRCULAR ACCESS COVERS. REPAIRED PER BOEING SRM 51-40-11.Feb 5, 1997 · N853FT · Boeing 747122SDR P5CA9700236Fairing · damageRT BODY FAIRING, 194DR HAS HOLE. REPAIRED PER BOEING SRM 51-40-09.Feb 5, 1997 · N858FT · Boeing 747123SDR P5CA9700226Fairing · puncturedHOLE IN WING TO FUSELAGE FAIRING, LEFT SIDE. REPAIRED PER BOEING SRM 51-40-09.Feb 5, 1997 · N858FT · Boeing 747123SDR 9703199152Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE TAILCONE RELEASE HANDLE FROM CLIPS. ALSO, FOUND SIX BEARING PLATES WORN. REPLACED BEARING PLATES AND ADJUSTED CLIPS.Feb 4, 1997 · N8911E · Doug DC914SDR DHL9780442CFillet Bracket · crackedAT C-CHECK, UPPER LEFT WING TO FUSELAGE FILLET PANEL BRACKET HAS CRACKED 24 INCHES FROM L/E. STOP DRILLED CRACK AND REPLACED BRACKET PER SRM 53-2-0.Feb 1, 1997 · N804DH · Doug DC873FSDR 9703229861Guide Pins · wornDURING LINE CHECK, FOUND THAT IT TOOK EXCESSIVE FORCE TO DEPLOY TAILCONE. ALSO, FOUND FOUR GUIDE PINS WORN. REPLACED GUIDE PINS AND ADJUSTED INTERIOR HANDLE RELEASE PRESSURE.Jan 31, 1997 · N770NC · Doug DC951SDR DHL9780451CFairing · crackedAT C-CHECK, TAIL SKID ENERGY ABSORBER LOWER FAIRING HAS SMALL CRACK T/E END. ROUTED OUT SMALL CRACK PER SRM 51-1-0.Jan 27, 1997 · N804DH · Doug DC873FSDR DHL9780429CFillet Strap · crackedAT C-CHECK, RT WING LWR SURFACE TO BODY STA 680 FILLET SUPPORT METAL STRAP DAMAGED. REMOVED AND INSTALLED FABRICATED STRAP PER SRM 51-1-0.Jan 26, 1997 · N804DH · Doug DC873FSDR MWEA97093Release Mech · lack of lubeDURING C-CHECK, TAIL CONE DID NOT DROP OFF PROPERLY DURING TEST. MAINT RIGGED TAILCONE CABLES AND LUBED LATCHES IAW DOUGLAS MM 53-50-3.Jan 25, 1997 · N302ME · Doug DC932SDR P5CA9700199Fairing · delaminatedPANEL NR 194FR WING TO BODY FAIRING DELAMINATED. REPAIRED PER BOEING SRM 51-40-09 AND 51-24-11.Jan 22, 1997 · N858FT · Boeing 747123SDR P5CA9700197Fairing · puncturedHOLE IN PANEL NR 292BR RIGHT FORWARD WING TO BODY FAIRING. REPAIRED PER BOEING SRM 51-40-09.Jan 22, 1997 · N858FT · Boeing 747123SDR P5CA9700194Fairing · delaminatedRT FWD WING TO BODY FAIRING PANEL 292AR DELAMINATED AT PREVIOUS REPAIR. REMOVED OLD REPAIR, SANDED AND CLEANED, APPLIED FIBERGLASS FILLERS AND OVERLAYS, PAINTED PER SRM 51-40-09 AND 51-24-01.Jan 22, 1997 · N858FT · Boeing 747123SDR P5CA9700191Fairing · puncturedHOLE IN PANEL NR 292CR RIGHT FORWARD WING TO BODY FAIRING. REPAIRED PER BOEING SRM 51-40-09 AND PAINTED PER BOEING SRM 51-40-11.Jan 22, 1997 · N858FT · Boeing 747123SDR GTIA9700110Tailcone · delaminatedFIBERGLASS REPAIR ON LEFT INSIDE OF TAILCONE IS DELAMINATION. REPAIRED DELAMINATION PER SRM 51-90-0. (M)Jan 15, 1997 · N928ML · Doug DC931SDR UPS97822202Angle · crackedINSPECTION TYPE:D, LT FWD UPPER WING FILLET PANEL ATTACH ANGLE IS CRACKED IN TWO, BS 640. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21.Jan 12, 1997 · N748UP · Doug DC871FSDR 9700509956Handle · out of adjustDURING PERIODIC CHECK, INTERIOR HANDLE EXCEEDED MAXIMUM FORCE LIMITS ON PULL TEST AND TAILCONE DID NOT DROP. MAINTENANCE RIGGED HANDLE AND TAILCONE.Jan 10, 1997 · N923RW · Doug DC931SDR CALA9700271Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN L-ANGLE WING BODY FAIRING SUPPORT AT LT WING ROOT, STA 1360. THE ANGLE WAS REPLACED IAW SRM 51-30-101 AND 53-53-01, FIGURE 3A.Jan 9, 1997 · N49082 · Doug DC1030SDR 9700479606Latches · out of adjustUPON ARRIVAL AT AIRCRAFT, TAILCONE ANNUNCIATOR LIGHT WAS ILLUMINATED. HANDLE HAD BEEN INADVERTANTLY PULLED. TAILCONE DID NOT DEPLOY BUT ALL LATCHES WERE RELEASED. MAINTENANCE ADJUSTED LATCHES.Jan 4, 1997 · N606NW · Doug DC932SDR 9627919981Release Mech · malfunctionedDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. ADJUSTED TAILCONE RELEASE MECHANISM, FUNCTIONAL TEST OK.Dec 19, 1996 · N994Z · Doug DC931SDR 9627929873Pin Plates · wornDURING LINE CHECK, FOUND INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ALSO, FOUND EIGHT TAILCONE GUIDE PINS WORN, UPPER LEFT LATCH WORN AND TWO ALIGNMENT PIN PLATES WORN. REPLACED CLIPS, GUIDE PINS, LATCH AND PIN PLATES.Dec 17, 1996 · N782NC · Doug DC951SDR 9627909869Latch Mechanism · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. RIGGED TAILCONE LATCHING MECHANISM.Dec 16, 1996 · N778NC · Doug DC951SDR 9626299945Tailcone · out of adjustDURING PERIODIC CHECK, TAILCONE RELEASE FORCE EXCEEDED MAXIMUM LIMITS ON FUNCTION DROP CHECK. ADJUSTED PER CITEXT 09-5350-1-0021, SECOND TEST WAS WITHIN LIMITS.Dec 10, 1996 · N8925E · Doug DC931SDR CALA9601907Former · crackedINSPECTION FOUND A 1 INCH AND 3 INCH CRACK IN FUSELAGE WING TO BODY FAIRING SUPPORT FORMER AT STA 540R. A DOUBLER WAS INSTALLED IAW ECRA 5350-01227.Dec 9, 1996 · N12327 · Boeing 7373T0SDR 9625789991Clips · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE HANDLE FROM CLIPS. MAINTENANCE ADJUSTED CLIPS. OPERATIONAL CHECK NORMAL.Dec 3, 1996 · N8957E · Doug DC931SDR CALA9601711Cables · out of adjustTHE TAILCONE RELEASE HANDLE PULL WAS HIGH AT BOTH THE INTERIOR AND EXTERIOR HANDLES AND THE TAILCONE FAILED TO DROP FROM AIRCRAFT. THE TAILCONE RELEASE SYSTEM CABLES WERE ADJUSTED IAW MM 53-53-00, PAGE 501.Nov 14, 1996 · N10801 · Doug DC982SDR CALA9601710Clips · out of adjustTHE TAILCONE INTERIOR AND EXTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LESS THAN 25 POUNDS AND LESS THAN 10 POUNDS, RESPECTIVELY. THE HANDLE RETAINER CLIPS WERE ADJUSTED IAW MM 53-53-00.Nov 14, 1996 · N10801 · Doug DC982SDR DHL96712005Radome · poppedDURING TAKEOFF ROLL IMMEDIATELY PRIOR TO ROTATION, CREW HEARD A POP, F/O FELT AND IMPACT UNDER HIS FEET. BURNED RUBBER SMELL IN COCKPIT LASTED 5 MINUTES AND GEAR RETRACTION WAS NORMAL. NO GEAR WARNING OR OTHER ABNORMAL INDICATIONS WERE NOTED. PERFORMED ABNONov 13, 1996 · N712DH · Boeing 72729SDR P5CA9600919Radome · delaminatedDELAMINATED AREAS ON RADOME. REPAIRED PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11.Nov 4, 1996 · N850FT · Boeing 747122SDR 9623259979Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS. ADJUSTED CLIPS.Nov 3, 1996 · N9343 · Doug DC931SDR RAAA96B2041Fairing Door · missingON DESCENT, AT 25,000 FT LOUD BANG SOUNDED IN CARGO COMPARTMENT AREA. CHECKED AREA, APPEARED NORMAL. AFTER LANDING AT AKN FOUND BODY FAIRING SECTION 46 ACCESS DOOR NR 3401 AT BS 740 MISSING. REPLACED ACCESS DOOR NR 3401 AT AKN AND RETURNED TO ANC. REPLACEDOct 31, 1996 · N832RV · Boeing 72722CSDR 9623269987Latch Arm · wornDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ALSO, FOUND A WORN UPPER LEFT LATCH ARM AND AN INCORRECT LOWER RIGHT LATCH HOUSING. ADJUSTED THE CLIPS AND REPLACED THE LATCH ARM AND LATCH HOUSINOct 31, 1996 · N987US · Doug DC932
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