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.
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
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 REXA2016090201697Fairing · chafedRIGHT STUB FAIRING HAS CHAFE DAMAGE. REPAIRED IAW REO 601R-53-82-003.SDR IPXA2016092708698Fairing · damagedINSPECTION TYPE:3CL/H HORZ. STAB. WING TO BODY FAIRING ATTACH HOLE AT STA. Y=2007 AND LONG. 29TR IS ELONGATED.REPAIRED BODY ATTACH FAIRING SKIN HOLE AT SAID LOCATION IAW VT-SAA EA 011-5330-01-A6435 REV. I/R AND UPS EO MD11-5330-61929-A. (MAJOR)SDR DALA2016083106307Release Mech · wornWORN TAILCONE RELEASE CAM AT AFT ACCESSORY COMPARTMENT. WORN ON TAILCONE RELEASE MECHANISM CAM BASE WAS MEASURED AND WAS FOUND OUT OF LIMITS, MAX PERMISSIBLE 0.025" X 0.280" MAX MEASURED 0.062" X 0.- 328 IAW CMM 53-50-07. THEREFORE CAM WAS REPLACED IAW AMM 5SDR IPXA2016092108518Frame · crackedINSPECTION TYPE: 3C, FWD TAIL CONE FRAME IS CRACKED AT UPPER TAIL CONE LATCH. REPAIRED THE FRAME IAW DWG AKC7539 AND SRM 53-80-07 REPAIR 4.SDR DALA2016102607675Support · corrodedCORROSION ON FILLET FAIRING SUPPORT, STA 807. FABRICATED AND INSTALLED REPAIR PARTS IAW ERA 549283-14, REV O.SDR REXA2016082501601Panel · crackedAFT WING TO FUSELAGE PANEL 195DL ANGLE PN CC690-39251-1IS CRACKED. REMOVED AND REPLACED THE ANGLE, AND AFT JOINT STRAP IAW SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, DRAWING CC690-39171 AND REO 690-53-82-052.SDR SWAA2016091255687Angle · crackedWING TO BODY FAIRING STRUCTURE ANGLE CRACKED AT BS 500D, STR 19L, AT LOWER FUSELAGE. R & R ANGLE IAW SRM AND DWG.SDR DALA2016081906150Cable · frayedTAILCONE NITROGEN CYLINDER CABLE FRAYED. REMOVED AND REPLACED CABLE.SDR DALA2016081606048Lanyard · frayedLANYARD FOR TAILCONE IS FRAYED. REPLACED THE LANYARD ASSY IAW AMM 53-53-02.SDR IPXA2016081206965Fairing · damagedINSPECTION TYPE: 12Y, LEFT WING TO BODY PANEL 577FT HAS EDGE DAMAGE IN TWO PLACES. REPAIRED THE DAMAGE IAW EO A300-5350-61565-A.SDR IPXA2016090207765Doubler · chafedINSPECTION TYPE:3C, EXTENDED TAILCONE LT SIDE INTERNAL DOUBLER CHAFE DAMAGE REPAIR AT STA 2165.6 Z=60.0. REPAIRED CHAFE DAMAGE IAW EA 011-5320-01-A6385, REV IR AND EO MD11-5350-61475-A, MINOR.SDR IPXA2016082807528Tail Cone · damagedINSPECTION TYPE: 3C, FWD TAILCONE RT SIDE SKIN CREASED BS 2224 - 2229 BELOW DOOR HINGE SKIN CREASE. REPAIRED IAW EA 011-5320-01-A6397 REV. IR AND EO MD11-5350-61631-A.SDR QXEA2016072900469Panel · damagedWING TO FUSELAGE PANEL 262HT DAMAGED. REMOVED AND REPLACED IAW SRM 51-42-05 REPAIR-01, AND DWG 85700005 REV-A.SDR IPXA2016080306630Structure · dentedINSPECTION TYPE: 1C, AFT EXTENDED TAILCONE IS DENTED AND CRACKED. REPAIRED IAW EA 011-5350-01-A6370 REV I/R AND EO MD11-5350-61344-A.SDR IPXA2016080206621Structure · dentedINSPECTION TYPE: 1C, EXTENDED AFT TAILCONE AFT END IS DENTED AND GOUGED AT AFT STATIC WICK. REPAIRED DAMAGED AFT EXTENDED TAILCONE IAW EA 011-5320-01-A6373 REV. I/R AND EO MD11-5320-61368-A.SDR DALA2016071205222Latch · out of adjustTAILCONE SEPARATION NOTICED ON PREFLIGHT WALK AROUND. ADJUSTED TAILCONE LOCKPIN LATCH IAW AMM 53-53-00. ALL CHECK NORMAL.SDR DALA2016070705157Release Mech · out of toleranceDURING TAILCONE RELEASE SYSTEM FUNCTIONAL CHECK, OPENING FORCE REQUIRE TO OPEN AFT VENTRAL DOOR IS 30 LBS. PULL TEST OUT OF LIMITS. RIGGED TAILCONE IAW AMDS 5350-01077-0101. ADJUSTED TEE PIN CLIPS, LATCHES, AND LUBED IAW AMDS 5350-01077-0101. PERFORMED TASDR DALA2016070605119Doubler · wornWEAR ON PREVIOUS REPAIR DOUBLER OF TAIL CONE SLIDE PLATFORM AT AFT ACCESSORY COMPARTMENT. DOUBLER WAS REPLACED IAW ER/A 41283-14AM.SDR SWAA2016072254144Fairing · crackedWING TO BODY FAIRING NR 195CL CRACKED IN THE LOWER AFT CORNER IN THE RADIUS. REPAIRED FAIRING IAW SRM.SDR REXA2016063001223Support Strap · corrodedMLG FAIRING 193AB, LT AND RT SUPPORT STRAPS ARE CORRODED. CONTINUATION CARD 81514111, OP 192. REPLACED SUPPORT STRAPS ON MLG FAIRING 193AB IAW SRM 51-42-13-001-001-A01, 51-42-15-001-001-A01, 51-40-11-001-001-A01, 51-25-01-001-001-A01, AMM 51-23-00-390-820-A01SDR SWAA2016062953345Web · crackedLT WHEEL WELL AFT OUTBOARD WING TO BODY FILLET FAIRING UPPER AND LOWER CHORD WEB CRACKED. R&R WEB IAW DWG AND SRM.SDR SWAA2016061652957Support Frame · crackedLEFT WING TO BODY PANEL 191L FORWARD SUPPORT FRAME CRACKED. R & R FRAME IAW SRM.SDR DALA2016062004884Cable · missingTAILCONE NITROGEN CYLINDER PULL CABLE MISSING. REPLACED CABLE IAW MM. AIRCRAFT OK FOR SERVICE.SDR V0XD20160615125Strap · corrodedAFT FUSELAGE FAIRING STRAP MISSING SEVERAL RIVETS. UPON EVALUATION FOUND LIGHT CORROSION ON STRAP AND
C-CHANNELS. STRAP CORRODED OUT OF LIMITS. FABRICATED NEW STRAP IAW DWG CC670-39171-3, REV NC. DATED 4/98. REPLACED RIVETS IAW SRM 51-42-06.SDR SWAA2016062753254Channel · crackedLEFT WING TO BODY FAIRING AT LOWER FUSELAGE CHANNEL CRACKED AT BS 706. R & R CHANNEL IAW SRM.SDR QXEA2016062100389Channel · damagedFOUND DAMAGE ON EXTERNAL PANEL 262HT FUSELAGE LANDING, MARKED. REMOVED REAR SPAR WING TO FUSELAGE FAIRING LANDING STRIP STA X 426.974, PN: 85713402-105, REF SRM 51-42-05, REPAIR-01, PARA 4E, 1-3. INSTALLED REPLACEMENT REAR SPAR WING TO FUSE FAIRING LANDING SSDR UIEA2016061000419Skin · delaminatedFX BODY FAIRING NR 1R3CL EXT SURFACE MID AREA FOUND APPROXIMATELY 22" X 16" DELAMINATED, SEVERAL DENT MARKS. BODY FAIRING NR 1R3CL EXT SURFACE REPAIRED IAW NR R1-53-67-11428, REV A.SDR DALA2016060604360Cable · damagedTAILCONE KEVLAR CABLE DAMAGED. REPLACED KEVLAR CABLE REF. AMDS CARD 5350-01077-0101.SDR DALA2016060604361Latch · wornUPPER LEFT TAIL CONE ATTACH LATCH LOCK IS WORN. R & R AND ADJUSTED LATCH IAW AMM 53-53-00.SDR ASOA2016060315036Skin · dentedDENT IN TAILCONE LEFT SKIN AT THE 6:00 POSITION. VERIFIED ALL STEPS OF PERMANENT REPAIR WERE COMPLIED WITH ON STS EA32-2014-308. AND COMPLIED WITH ECTC EA32-2014-308.SDR DALA2016060704411Buckle · brokenTAILCONE STRAP BUCKLE BROKEN. REINSTALLED BLIND THREADED SELF LOCKING INSERT.SDR NI6R201606010033Radome · damagedAIRCRAFT WAS STRUCK BY LIGHTNING IN CLIMB AFTER TAKEOFF. FM RADIO INOP AFTER STRIKE. ACFT DIVERTED TO COMPANY MAINTENANCE BASE AND WAS INSPECTED FOR DAMAGE. ENTRY POINT OF STRIKE WAS ON NOSE RADOME, EXIT POINT WAS ON TAIL CONE SPEED BRAKE DOORS. ALL DAMAGE SDR DALA2016060104269Tail Cone · out of rigVAULT DOOR FORCE REQUIRED TO DROP TAIL CONE EXCEEDED 20 LBS TENSION. ADJUSTED TAIL CONE RIG IAW AMM 53-53-00 AND AMDS 5350-01077-0101.SDR WX0A2016052373158Panel · crackedFAIRING PANEL 197NL, THE PANEL IS CRACKED & HAS THE OUTER SKIN PENETRATED, BETWEEN FS 1240 - 1300 AT STRINGER 28R. THE DAMAGED AREA MEASURES 12 INCHES LONG BY 3 INCHES WIDE. REPAIRED BODY FAIRING 197N IAW SRM 53-00-70 REPAIR 1 & ERO 536-006 REV ORIG.SDR UIEA2016051600285Support Bracket · corrodedCORROSION, SUPPORT BRACKET, FWD LOWER FUSELAGE, WING TO BODY FAIRING SUPPORT STRUCTURE, STATION 984, LBL 3. REPLACED DAMAGE PART WITH NEW PART IAW SRM 51-40-02-0G-0 REV 96. JOB COMPLETED & CONDITION CHECKED NORMAL.SDR DALA2016051603936Handle · no testTAILCONE FUNCTIONAL IAW AMDS 5350-01077-0101, STEP 11D. FAILED INTERIOR HANDLE PULL TEST 37LBS. SEE NR FOR ADDITIONAL INFORMATION 036-0001:5350-01077-0101/007 00009 REINSTALLED AND TESTED TAIL CONE IAW AMM 53- 53-00, WITHIN LIMITS, 27LBS.SDR DALA2016051603935Release Mech · failedTAILCONE RELEASE MECHANISM CAM FAILED TORQUE CHECK OF AMDS 5350-01077-0101, STEP NR 12. SEE NR FOR ADDITIONAL INFORMATION 036-0001:5350-01077-0101/005 00007. REPLACED IAW AMM 53-53-02, AJUSTED AND TORQUED.SDR DALA2016051603959Pin · misinstalledTHE TAILCONE FAILED TO DEPLOY DURING ROUTINE DROP TEST. MAINTENANCE DISCOVERED THAT THE RELEASE LATCH T-PIN NR 12 FOR THE TAILCONE WAS NOT PROPERLY ENGAGED. THE T-PIN WAS REENGAGED AS DESIGNED AND IN COMPLIANCE WITH AMDS 5352-2001 THE SYSTEM WAS RIGGED TO SPESDR DALA2016051603958Cable · damagedMAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE KEVLAR CABLE WAS DAMAGED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR DALA2016051203900Block · damagedTAIL INTERIOR, TAIL CONE RELEASE LOCK CABLE BLOCK IS NOT .5" AWAY FROM TUBING, CONDUIT, AS REQUIRED IAW STEP 7. OPS CHECKED GOOD IAW AMDS 5350-01077-0101.SDR SWIA201642201Support · corrodedTHE AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE AT FS 939.00 HAS CORROSION, ON THE UPPER AND LOWER SIDE, OF THE ANGLE THAT JOINS THE LT ANGLE AND RT ANGLE. INSTALLED NEW SERVICABLE ANGLE, PN SH670-39189-1 IAW SRM.SDR DALA2016051703968Door · lack of lubeDURING TAILCONE RELEASE FUCTIONAL CHECK FOUND ARMING HANDLE HARD TO ROTATE. LUBED DOOR IAW AMM 12-21. CONFIRMED RIGGING AND RELEASE FORCE IAW AMM 52-12. OPS CHECK GOOD.SDR SWAA2016062253139Access Door · delaminatedLEFT FAIRING ACCESS DOOR 3302 DELAMINATED ON EXTERIOR SURFACE. REPAIRED DOOR IAW SRM.SDR DALA2016050603718Spring · missingDURING THE TAILCONE RELEASE SYSTEM FUNCTIONAL CHECK, MAINTENANCE FOUND THAT THE TAIL CONE FAILED TO DROP BECAUSE A SINGLE SPRING WAS MISSING FROM A RELEASE CABLE SYSTEM PIN. THE SPRING WAS INSTALLED AND THE SYSTEM WAS SUCCESSFULLY FUNCTIONALLY CHECKED IAW AMMSDR DALA2016050203510Frame · crackedCANTED FRAME BS 1510 CRACKED AT TAILCONE ALIGNMENT PIN AT 2 O'CLOCK. REPAIRED IAW PRI 546574-14, REV 1 AND COMPLIED WITH ER/A 546574-14, REV ORIGINAL.SDR IPXA2016051603390Skin · corrodedINSPECTION TYPE:2C, TAILCONE SKIN FOUND CORRODED AT BS CANT 2163.6 TO CANT 2244.0 AND Z=10. REPAIRED CORRODED TAILCONE SKIN AT SAID LOCATION IAW EA 011-5330-01-A6249, REV I/R AND EO MD11-5330-60778-A.SDR IPXA2016051603447Skin · chafedINSPECTION TYPE:2C, FORWARD TAIL CONE RT FWD INNER SKIN IS CHAFED AT FUSELAGE MATING SURFACE. REPAIRED TAIL CONE RT FORWARD INNER SKIN AT FUSELAGE IAW EA 011-5330-01-A6233 REV I/R AND EO MD11-5330-60694-A.SDR IPXA2016051403340Door · tornINSPECTION TYPE:2C, EXTERIOR SKIN TORN ON FORWARD EXTENDED TAILCONE LT UPPER DOOR 317BT. REPAIRED NOTED DOOR SKIN DAMAGE IAW EA 011-5240-01-A6238, REV IR AND EO MD11-5240-60715-A.SDR IPXA2016051403339Tail Cone · gougedINSPECTION TYPE: 2C, REPAIR DOUBLER GOUGED ON FWD TAILCONE LATERAL BEAM, LT SIDE. REPAIRED TAILCONE BEAM IAW EA 011-5310-01-A6245, REV IR AND EO MD11-5320-60738-A.SDR DALA2016042503297Spring · brokenMAINTENANCE FOUND THE TAILCONE DEPLOYMENT MECHANISM SPRING BROKEN. THE SPRING WAS REPLACED IAW DWG 5910828.
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