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 DALA1501990967Angle · crackedTAILCONE UPPER RT L ANGLE INTERCOSTAL IS CRACKED. REMOVED UPPER L ANGLE, DRILLED NEW , PRIMED AND INSTALLED IAW SRM 51-30.SDR DALA13006799240Spring · corrodedTAIL-CONE JETTISON RELEASE MECHANISM PIN SPRINGS ARE CORRODED. R & R TAIL CONE JETTISON RELEASE MECHANISM PIN SPRINGS IAW AMM.SDR DALA13005730967Cable · frayedMX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR ABXA20120202393Structure · corrodedCORROSION FOUND ON THE INBOARD AND OUTBOARD FACE OF RIGHT PICKLE FORK LEG. REMOVED CORROSION FROM INBOARD AND OUTBOARD FACE OF RIGHT PICKLE FORK LEG PICKLE FORK LEGS IAW B767 SRM 53-50-08, PERFORMED ULTRASONIC THICKNESS INSPECTION OF BLENDED AREAS IAW B767 NDSDR SWAA2013021212604Rub Strip · corrodedWING TO BODY FAIRING RUB STRIP HAS CORROSION UNDER FILLET PANEL 160SL 26-013. REMOVED CORRODED RUB STRIP UNDER FILLET FAIRING 150SL IAW B717 MM 53-53-01. TREATED AND PRIMED NEW RUB STRIP IAW B717 SRM 51-10-04. INSTALLED SERVICEABLE RUB STRIP UNDERSDR DALA13006590977Structure · damagedDURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE CATWALK OVER THE VENTRAL STAIRWAY WAS DAMAGED AND JAMMING. THE MOVEABLE CEILING (CATWALK) WAS REPAIRED, ADJUSTED, AND RIGGED. IT NO LONGER BINDS DURING OPERATION AND MEETS PUBLISHED SPECIFICATIONS.SDR CA130201008Fairing · damaged(CAN) DAMAGE WAS CAUSED BY THE OIL TUBE BONDING LEAD ATTACHMENT BOLT WHICH WAS POSITIONED IN A MANNER THAT RESULTED IN CONTACT WITH THE FAIRING RESULTING IN A SMALL HOLE BEING CHAFED IN THE FAIRING. MFG ENGINEERING IS INVESTIGATING.SDR DALA13006249018Receptacle · wornDURING SERVICE CHECK, TAILCONE LT UPPER RECEPTACLE WORN. R & R LT UPPER RECEPTACLE IAW AMM.SDR DALA13006239018Cable · frayedDURING SERVICE CHECK, KEVLAR CABLE INT TAILCONE FRAYED AT CAM ATTACH POINT. R & R KEVLAR CABLE IAW AMM. KEVLAR CABLE TO TAILCONE RELEASE MECHANISM CAM WILL BE ACCOMPLISHED ON AMDS 5350-01077-0101.SDR DALA13006229018Receptacle · wornTAILCONE LT UPPER RECEPTICLE WORN LT UPPER SPADE. R & R LEFT UPPER RECEPTICLE IAW AMM.SDR ABXA20120122396Structure · corrodedLEFT SIDE FRAME FITTING (PICKLE FORK) HOLES NR 10 & 11 HAS CORROSION IN THEM. REAMED HOLES TO 1/64 OVERSIZE 1.015 IAW B767 SRM 51-40-05, ACFT WAS GROUNDED.SDR SWAA2013012811980Plate · crackedCRACK ON PLATE LOCATED WING TO BODY FAIRING RIGHT AFT. REPLACED PLATE LOCATED WING TO BODY FAIRING RIGHT AFT IAW SRM B737-300 51-10-02 ITEM 8.SDR SWAA2013012111688Rub Strip · crackedWING TO BODY PANEL CHAFE STRIP CRACKED AND PEELING AT LEFT UPPER WING STA 715. REMOVED AND REPLACED STRIP IAW SRM AND BOEING.SDR SWAA2013012111683Rub Strip · crackedWING TO BODY PANEL CHAFE STRIP CRACKED & PEEL AT RIGHT UPPER WING STA 674 TO 699. REMOVED AND REPLACED STRIP IAW MM AND BOEING.SDR DALA13002410927Release Mech · stuckMX DISCOVERED THAT THE TAILCONE RELEASE SYS CAM WAS STUCK, CAM AND BLOCKS FOR THE RELEASE CABLE WERE WORN AND OUT OF RIG BEYOND ALLOWABLE LIMITS. THE MATING FLANGE WAS CRACKED AT MULTIPLE ALIGNMENT PIN POSITIONS. THE CABLE CAMS AND BLOCKS WERE REPLACED ANDSDR DALA13000680962Spring · inoperativeBOTH THE UPPER RT AND THE UPPER LT TAILCONE RELEASE LATCH SPRINGS ARE NOT FUNCTIONING, ARE WEAK, AND HAVE GOUGED INTO THE TAILCONE FLANGE. BOTH UPPER RT AND LT LATCH ASSEMBLIES WERE REPLACED IAW AMM 53-53-00. THE TAILCONE FUNCTIONAL CHECK WILL BE ACCOMPLISHESDR SWAA2013012511847Rub Strip · crackedLEFT WING TO BODY FAIRING RUB STRIP CRACKED AT STA 560- LONGERON 18L. REPAIRED RUB STRIP IAW SRM.SDR USAA2013011000002Skin · crackedTAIL CONE REPAIR - SKIN CRACK ON TAIL CONE BETWEEN FR84 TO FR85 & BETWEEN R19L TO S19R. REPLACED TAIL CONE IAW A320 AMM 53-58-11-400-007-A.SDR SWAA2013011711510Rub Strip · crackedLEFT WING TO BODY FAIRING AT STA 617 STG 18L RUB STRIP CRACKED. REMOVED AND REPLACED LEFT WING-TO-BODY FAIRING AT STA 617 STR 18L RUBSTRIP P/N 5971042-3, PO 2229024 IAW B717 SRM 51-20-05.SDR IPXA3576620Skin · dentedTAILCONE OUTER SKIN DENTED, DAMAGE 2 INCHES IN DIA, DEPTH .016 AT FS 1954 3.4, LBL. REPAIRED IAW EO B757-5330-47030-B.SDR SWAA2013011111360Seal · crackedLEFT FWD STRUT FAIRING ACCESS PANELS 431AZ AND 431AR HAVE CRACKED SEALS. REMOVED AND REPLACED SEAL AT LT FWD STRUT FAIRING ACCESS PANELS 431AL AND 431AR IAW B737 AMM 51-40-02.SDR SWAA2013011111359Seal · crackedRIGHT FWD STRUT FAIRING ACCESS PANELS 441AR HAVE CRACKED SEALS. REMOVED AND REPLACED SEAL AT RIGHT FWD STRUT FAIRING ACCES PANELS 441AL AND 441AR IAW B737 SRM 51-40-02.SDR SWAA2013012812008Rub Strip · corrodedWING TO BODY ATTACH AREA RUB STRIPS CORRODED 2 EACH - LT AND RT SIDES APPROX STA 851. REMOVED & REPLACED LT & RT WING TO BODY RUB STRIPS AT APPROX STR 851 IAW B717 SRM 51-20-05.SDR SWAA2013012812003Rub Strip · corrodedWING TO BODY ATTACH AREA RUB STRIPS CORRODED 2 EACH - LT AND RT SIDES APPROX STA 851. REMOVED & REPLACED LT & RT WING TO BODY RUBSTRIPS AT APPROX STR 851 IAW B717 SRM 51-20-05.SDR SWAA2013012111652Strip · crackedCRACKED CHAFE STRIP WING TO BODY FILLET STA 898 BETWEEN L21R - L22R. REMOVED AND REPLACED CHAFE STRIP ON WING TO BODY FILLET AT STA 898 WITH NEW SERVICEABLE PART IAW B717 SRM 53-53-01.SDR DALA12016939017Pin · wornDURING TAIL CONE DROP, MX FOUND INTERNAL TEE PIN WORN. REPLACED T-PIN IAW AMM.SDR VNAA2012121700011Radome · damagedCREW REPORTED LIGHTNING STRIKE TO LEFT FRONT SIDE OF AIRCRAFT DURING APPROACH WITH AIRCRAFT IN A CLEAN CONFIGURATION. CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED RADOME ASSEMBLY DUE TO BURN MARKS OSDR DALA12016060955Cam · wornTAILCONE RELEASE CAM LUG - WORN, KEVLAR CABLE RELEASE CAM MAX MATERIAL LOSS IS .025", BLENDED WEAR MARKS, HFEC INSPECTED WORN AREA IAW NTM 06-01-01.001. NO DEFECT NOTED QC1971 INSTALLED TAILCONE RELEASE CAM IAW AMM 53-53-02. AWAITING FINAL ER/A. 255074. COMSDR UALA2012121007147Panel · shearedDURING FLAP RETRACTION PANEL SEPARATED FROM AIRCRAFT AT LEFT FUSELAGE WING TO BODY FAIRING BY LEFT INBD T/E FLAP. REMOVED TORQUE TUBE FOR SHEARED DOOR PER MM 27-51-07. CONT OF AMIS ITEM 3642044. INSTALLED REPLACEMENT FAIRING DOOR AND TORQUE TUBE ASSY AS REQSDR IPXA2576351Skin · dentedTAILCONE DAMAGED HAS THREE DENTS. REPAIRED IAW EO B757-5330-47031-B.SDR ABXA20121130351Structure · corrodedTAIL CONE RIGHT LOWER OUTER CHORD LOWER TENSION BOLT HOLE HAS CORROSION. REMOVED AND REPLACED CHORD SECTION IAW B767-200 SRM 51-40-02 & BOEING DWG 624T0020. ACFT WAS GROUNDED.SDR UALA2012112806828Fairing · vibrationVIBRATION AND AUDIBLE RUMBLE FELT AND HEARD THRU OUT THE FLIGHT DECK. DUE TO "SCORE" ON VIB REPORTING SHEET, APPLY SPEED TAPE TO BELLY FAIRING SEALS IDENTIFIED IN MT53-004. CREATE CF WITH "AK" AS REPAIR LIMIT AND "D" IN METERS. PERFORMED MT53-005 AND BELLY SDR SWAA2012121210529Access Panel · delaminatedDELAMINATION ON ACCESS PANEL 3802R TAIL CONE ACCESS. REPAIRED ACCESS PANEL 3802R, TAIL CONE ACCESS IAW B737-300 SRM 51-70-07-0G-0.SDR SWAA2012121010379Fairing · crackedCRACK ON HOLES 4(EA) LOCATED ON UPPER AFT WING TO BODY FAIRING PANEL 3678R (BETWEEN 57" FWD LOWER EDGE). REPAIRED 3678R IAW B737-300 SRM 51-70-16-0G-0 REP 9.SDR SWAA2012121010378Fairing · crackedCRACK ON HOLES (4EA) LOCATED ON UPPER AFT WING TO BODY FAIRING PANEL 3578L BETWEEN 57" FROM UPPER FWD EDGE. REPAIRED WING TO BODY FAIRING PANEL 3578L IAW B737-300 SRM 51-70-16-0G-0 REP 9.SDR C77A20121124028Baffle · crackedAPU TAIL CONE BAFFLE NR 6, HAS A 0.550" CRACK AT 3 O'CLOCK POSITION AT THRU FLANGE, 6 RIVET ROWS AFT OF FRAME 100, X=31229.19 Y=146.94 TO 159.64. PERFORMED WELDING OF CRACK IAW NE SPEC 40-056. VISUALLY INSPECTED AND NDT PERFORMED VERIFYING NO MORE CRACKINGSDR SWAA2012113010060Drain Mast · delaminatedDRAIN MAST ON WING TO BODY FAIRING BS 727B +10 LBL 65 TRAILING EDGE DELAMINATED. REMOVED AND REPLACED MAST IAW AMM.SDR ASOA2012121102635Attach Angle · crackedLT UPPER WING UNDER WING TO FUSELAGE FAIRING 161DL FAIRING ATTACHMENT ANGLE AT FS 449.85 IS CRACKED. R & R LT UPPER WING UNDER WING TO FUSELAGE FAIRING 161DL FAIRING ATTACHMENT ANGLE AT FS 449.85 IAW SRM 51-42-06.SDR ASOA2012121102634Attach Angle · crackedRT UPPER WING UNDER WING TO FUSELAGE FAIRING 162DL FAIRING ATTACHMENT ANGLE AT FS 449.85 IS CRACKED. R & R RT UPPER WING UNDER WING TO FUSELAGE FAIRING 162DL FAIRING ATTACHMENT ANGLE AT FS 449.85 IAW SRM 51-42-06.SDR DALA12013429226Slider · out of rigTAILCONE UPPER SLIDER BLOCKS NOT RIGGED IN CORRECT POSITION. IMPROPER INSTALLATION LT AND RT UPPER SLIDING BLOCKS. ADJUSTED CLAMPS IAW AMM AND OPS CHECKED GOOD.SDR DALA12013409217Cable · frayedDURING TAILCONE FUNCTIONAL CHECK, FOUND TAILCONE JETTISON BOTTLE ACTIVATION CABLE FRAYED. R & R WORN CABLE WITH NEW CABLE. OK FOR SERVICE.SDR UALA2012111606625Seal · misinstalledTROUBLESHOOT VIBRATION WHEN FLAPS FULL EXTEND. FOUND WING TO FUSELAGE PANEL 193AT SEAL INSTALLED BACKWARDS AND NOT CONTACTING WING SURFACE PER MM. ALSO SEAL RETAINER INSTALLED INCORRECTLY. REPOSITIONED SEAL AND INSTALLED RETAINER CORRECTLY FOUND PANEL 194ATSDR DALA12012280938Release Cable · frayedMX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.SDR SWAA2012111909570Fairing · damagedWING TO BODY FAIRING FWD UPPER 191 FL CRACKED. REPAIRED DAMAGED AREA PER SRM 51-70-05 REPAIR 10.SDR DALA12012100938Bearing · wornDURING INSPECTION OF THE TAILCONE RELEASE SYSTEM, MX FOUND THE RELEASE CAM BEARING WORN BEYOND LIMITS, ALLOWING EXCESSIVE FREE PLAY. THE CAM BEARING WAS REPLACED. FOLLOW UP FUNCTIONAL CHECKED GOOD.SDR UALA2012102906186Seal · faultyLOUD SQUEAL BETWEEN ROWS 1+2 REPEAT WRITEUP AT FL360 8.0 PSID. SAMC TEXT: CREW REPORTED STARTED TO HEAR NOISE AFTER TAKEOFF, CLOSER TO SEAT 2F, DOES NOT APPEAR TO BE RELATED TO AREA ASSOCIATED WITH 1R. PRESSURIZED ACFT TO 4 PSI PER JRH, NO DEFECTS NOTED. INSDR UIEA2012102800498Radome · damagedON POST FLIGHT, FOUND BIRD STRIKE ON RADOME. R & R NOSE RADOME IAW 53-12-01, CHP 5 INSPECTION 05-51-18.SDR SWAA2012111509461Strip · crackedNUMEROUS LOCATIONS OF CRACKED RUB STRIPS LEFT FWD FILLET STA 560 TO STA 653 BETWEEN L18L-L27L. 88-52. REMOVED AND REPLACED LEFT WING TO BODY FAIRING RUB STRIP IAW B717 SRM 53-20-70.SDR UALA2012102206040Radome · damagedLOUD THUMP ON UNDERSIDE OF COCKPIT DURING DESCENT. SUSPECT POSSIBLE BIRD STRIKE. FOUND 5" CIRCULAR DAMAGE AREA LOWER LEFT OF RADOME. PER AMM OUT OF LIMITS, DISBOND OF SKIN TO HONEYCOMB.SDR DALA12010770984Release Cable · out of limitsPERFORMED TAILCONE RELEASE SYS FUNCTIONAL CHECK AND FOUND THAT THE AFT DOOR EMERGENCY HANDLE RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS. THIS DISCREPANCY IS THAT THE DOOR COULD BE OPENED WITH LESS THAN THE REQUIRED 8 POUNDS OF PULL FORCE. THE TAILCONE RELEASE S
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