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 99ZZZM531Frame · crackedLEFT WINGROOT FORWARD FAIRING SUPPORT FRAME CRACKED IN FLANGE AT FRAME 26. C/W SRM 51-71, REPAIR TO CRACKED CORNER FLANGE USING .040 2024-T3 AN 8 AD RIVETS. (M)Apr 20, 1998 · N608AW · Bag BAE146200ASDR 9806889993Release Mech · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. RIGGED TAIL CONE DEPLOYMENT SYSTEM, FUNCTIONAL CHECK OK.Apr 17, 1998 · N8986E · Doug DC931SDR CALA9800670Latches · out of adjustTHE FORCE REQUIRED TO RELEASE TAILCONE USING THE AFT ENTRANCE DOOR AND INTERIOR RELEASE HANDLES DURING DROP TEST, WAS EXCESSIVE. THE TAILCONE LATCHES WERE ADJUSTED AND LUBRICATED IAW MM 53-53-00.Apr 15, 1998 · N72830 · Doug DC982SDR 9806079974Tail Cone · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY THE TAIL CONE. ALSO, FOUND THE BAYONET CABLES RUSTY AND THE LATCHES WOULD NOT RETURN TO THE CLOSED POSITION. REPLACED THE CABLES, LUBRICATED THE LATCHES, AND RIGGED THE DEPLApr 4, 1998 · N9338 · Doug DC931SDR RRXA98172Fillet · corrosionDURING A MAINTENANCE VISIT, FOUND FILLET PANEL CORRODED RIGHT WING. FILLET PANEL DAMAGED BEYOND SRM REPAIR, FABRICATED AND INSTALLED NEW FILLET PANEL IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04463.Apr 2, 1998 · N865F · Doug DC863FSDR CALA9800609Cables · out of adjustTHE TAILCONE PULL FORCE FROM THE OUTSIDE, INSIDE, AND AFT ENTRY DOOR HANDLES WAS EXCESSIVE. THE TAILCONE CABLES WERE RIGGED IAW MM 53-53-00.Apr 2, 1998 · N71828 · Doug DC982SDR RRXA98185Fillet · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT WING FILLET PANEL, NR 162. REMOVED FILLET PANEL FOR REPLACEMENT, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FILLET PANEL IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04608.Apr 1, 1998 · N865F · Doug DC863FSDR CA980424010Skin · delaminated(CAN) RADOME DELAMINATED DUE TO LIGHTNING STRIKE. REPLACED.Apr 1, 1998 · Boeing 767209SDR 9805329924Spring · misinstalledDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ALSO, FOUND THAT TAIL CONE RELEASE HANDLE CABLE WAS NOT INSTALLED IN SWITCH PLUNGER. MAINTENANCE FOUND THE LATCH SPRINGS IMPROPERLY INSTALLED. REPLACED LATCH SPRMar 31, 1998 · N926RC · Doug DC932SDR CALA9800601Cables · out of adjustTAIL CONE PULL FROM INTERIOR RELEASE HANDLE WAS LOW AT SIX POUNDS. AN ADJUSTMENT/TEST WAS PERFORMED IAW WORK CARD 08-5350-1-0008 AND PULL TEST WAS WITHIN SPECIFICATIONS AT 20 POUNDS.Mar 30, 1998 · N16804 · Doug DC982SDR VTZA98140Radome · damagedFLT 6718 - ATL-IAD - DURING CRUISE, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH AIRCRAFT WAS DAMAGED BY HAIL AND A/C HAD A ENGINE SHUTDOWN DUE TO FLAMEOUT. ENGINE WAS RESTARTED WITH NO PROBLEMS INDICATING. AIRCRAFT LANDED AT IAD AND WENT TOMar 20, 1998 · N624BR · Cndair CL6002B19SDR CALA9800541Radome · erodedINSPECTION FOUND THE RADOME EXTERIOR SKIN HAD SOME SPOTS OF EROSION AND A SMALL HOLE. THE RADOME WAS REMOVED AND REPLACED IAW MM 53-15-0.Mar 19, 1998 · N73751 · Boeing 727227SDR CALA9800489Mount · crackedINSPECTION FOUND TAILCONE UPPER SECTION RT WORK PLATFORM FORWARD MOUNT RIVETS LOOSE AND CRACKED. THE MOUNT WAS REMOVED AND A NEW MOUNT WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-52-01, FIGURE 2.Mar 18, 1998 · N14063 · Doug DC1030SDR 9804619178Latch · wornDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY THE TAILCONE AFTER HANDLE WAS REMOVED FROM CLIPS. ALSO, FOUND THE UPPER LEFT LATCH SPADE WORN AND SEVERAL GUIDE PIN RECEPTACLES WORN. REPLACED LATCH SPADE AND GUIDE PIN RECEPMar 18, 1998 · N3310L · Doug DC914SDR 99ZZZM490Attach Links · corrodedRIGHT WING TO FUSELAGE AFT ATTACH LINKS HAVE SURFACE CORROSION ON ENDS (PAINT MISSING). CLEANED, PRIMED AND PAINTED ENDS. (M)Mar 17, 1998 · N609AW · Bag BAE146200ASDR TWAA9803702Radome · puncturedMSY - FLT 8689 - CREW REPORTED LOUD BANG FROM NOSE OF AIRCRAFT, MADE UNSCHEDULED LANDING AT MSY. FOUND BIRD STRIKE TO RADOME AT 9 O'CLOCK POSITION. REPLACED RADOME AND REPAIRED METAL DAMAGE AT THE JOINT BETWEEN RADOME AND FUSELAGE. CHECK-C 2-11-98 STL. (M)Mar 15, 1998 · N923L · Doug DC932SDR P5CA9800512Fairing · crackedFUSELAGE LT BODY FAIRING STA 1460-1520 JUST AFT LT BODY WHEEL WELL CRACKED AT 2 PLACES. REMOVED AND REPAIRED PANEL PER SRM 51-40-15.Mar 10, 1998 · N850FT · Boeing 747122SDR P5CA9800465Fairing · delaminatedLT FUSELAGE LWR FAIRING FWD OF W/GEAR W/W DELAMINATED. REPAIRED PER SRM 51-40-09.Mar 7, 1998 · N854FT · Boeing 747122SDR DHL9872692DTail Cone · delaminatedAT D CHECK, VERT STAB TAIL CONE HAS DELAMINATION AFT OF LT ACCESSS. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 4315.Mar 6, 1998 · N726DH · Boeing 727228SDR 9803719905Release Mech · out of adjustDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE. RIGGED RELEASE SYSTEM. FUNCTIONAL CHECK OK.Mar 5, 1998 · N955N · Doug DC931SDR SWIA971105Fairing · departedBOTTOM CENTER PANEL OF FUSELAGE (MID WING), FWD OF LEFT AIR CONDITIONING PACK, DEPARTED THE AIRCRAFT. (FERRIED FROM PIH TO SLC). INSTALLED NEW WING CENTER FAIRING PANEL, IAW MM 57-11-01. ALL CHECKS GOOD.Mar 4, 1998 · N204SW · Emb EMB120ERSDR DHL9872644DFairing · crackedAT D CHECK, RT FUSELAGE BODY FAIRING 3621 IS CRACKED AT FASTENER HOLE AND L/E. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 3451.Mar 3, 1998 · N726DH · Boeing 727228SDR DHL9872621DFillet · delaminatedAT D CHECK, LEFT WING PANEL 3505 INNER SKIN BOTTOM AREA IS DELAMINATED. INSTALLED REPAIR PER SRM 51-40-8, 4 BY 6. N/R 1444.Mar 3, 1998 · N726DH · Boeing 727228SDR DHL9872620DFillet · damagedAT D CHECK, LEFT WING FILLET PANEL 3505 HAS NUMEROUS ELONGATED HOLES. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, 4 BY 4. N/R 1447.Mar 3, 1998 · N726DH · Boeing 727228SDR C2XA98BT017Radome · lightning strikeEWR - EN ROUTE SYR AIRCRAFT STUCK BY LIGHTNING DIVERTED TO SWF. AIRCRAFT HAD LIGHTNING INSPECTION AND FERRIED TO EWR, PERFORMED FURTHER CHECKS AND MAINTENANCE FERRIED AIRCRAFT TO BTV FOR FINAL REPAIRS. MAJOR REPAIR PERFORMED ON FORWARD PRESSURE BULKHEAD AT UMar 3, 1998 · N14833 · Aerosp ATR42320SDR CALA9800367Clips · out of adjustTHE TAILCONE INTERIOR RELEASE HANDLE PULLED FROM CLIPS AT FORTY POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND FUNCTIONAL CHECK WAS GOOD IAW MM 53-53-00.Mar 2, 1998 · N17812 · Doug DC982SDR CALA9800366Clips · out of adjustTHE EXTERIOR TAILCONE RELEASE HANDLE PULLED FROM CLIPS AT FIVE POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND FUNCTIONAL CHECK WAS GOOD IAW MM 53-53-00.Mar 2, 1998 · N17812 · Doug DC982SDR REXA98061Radome · contaminatedWEATHER RADAR PAINT DOTS, INOPERATIVE. CLEANED WATER OUT OF RADOME. OPS CHECK GOOD. (X)Feb 26, 1998 · N112PX · Saab SF340ASDR CALA9800305Fitting · gougedINSPECTION FOUND TAIL CONE RT LATCH HOOK FITTING WITH SUNK RIVETS AND A GOUGE JUST FORWARD OF INNER ACCESS DOOR ASSEMBLY AREA. THE DAMAGED AREA WAS REMOVED IAW SRM 51-31-01. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-52-01 AND 51-31-01.Feb 23, 1998 · N17087 · Doug DC1030SDR 98ZZZX1068Fairing · damagedGROUND EQUIPMENT DAMAGED FIBERGLASS FAIRING FORWARD OF AFT CARGO DOOR OPENING. DAMAGE IS 2.5 INCHES BY 1.5 INCHES BY 0.5 INCH DEEP. TERMPORARY REPAIR CARRIED OUT BY GEMINI.Feb 23, 1998 · N604GC · Doug DC1030FSDR P5CA9800264Fairing · delaminationFUSELAGE BODY FAIRING EXTERIOR MID AREA FOUND DELAMINATION FAIRING 192KR. BODY FAIRING FIBERGLASS REPAIRED PER SRM 51-40-14.Feb 18, 1998 · N3203Y · Boeing 747128SDR P5CA9800333Fairing · delaminatedFUSELAGE BODY FAIRING 193G AND 194G EXTERIOR LAYER FOUND CRACKED AND DELAMINATED. AREA REPAIRED PER SRM 51-24-11.Feb 17, 1998 · N3203Y · Boeing 747128SDR P5CA9800350Fairing Support · corrodedLEVEL 1 CORROSION ON AIR CONDITIONING ACCESS PANEL SUPPORT AT BS 1175 TO 1235, LBL 60. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.Feb 14, 1998 · N3203Y · Boeing 747128SDR CALA9800215Cables · out of adjustTHE TAILCONE EXTERIOR RELEASE HANDLE PULLED AT 15 POUNDS. THE TAILCONE WAS RIGGED IAW WORK CARD 08-5350-1-0008.Feb 11, 1998 · N14890 · Doug DC982SDR 9802409863Release Mech · out of adjustDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT THE INTERIOR TAILCONE RELEASE HANDLE FAILED PULL TEST. ADJUSTED INTERNAL TAILCONE RELEASE SYSTEM. FUNCTIONAL CHECK OK.Feb 9, 1998 · N772NC · Doug DC951SDR 9802349983Cable · wornDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXTERNAL RELEASE HANDLE HANGS UP ON HINGED SPRING DOOR DURING PULL TEST OF THE EMERGENCY RELEASE. ALSO, FOUND THE INTERIOR TAILCONE RELEASE CABLE WORN AT THE HANDLE. RESHAPED HINGED SPRING DOOR AND REPLACED CABLE.Feb 9, 1998 · N983US · Doug DC932SDR WTAA980026Radome · birdstrikeSBA - BIRDSTRIKE ON NOSE DURING APPROACH REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)Feb 6, 1998 · N271YV · Emb EMB120RTSDR P5CA9800222Fairing · corrosionFUSELAGE LOWER BODY FAIRING PANEL HAS CORROSION. REMOVED CORROSION, APPLIED FILLER, APPLIED CONDUCTIVE COATING, PRIMED AND PAINTED PER SRM 51-10-01, 51-40-08, 51-24-17.Feb 6, 1998 · N852FT · Boeing 747122SDR CALA9800186Clips · brokenINSPECTION FOUND AFT FUSELAGE TAIL CONE EXTERIOR RELEASE HANDLE CLIPS BENT AND BROKEN. NEW CLIPS WERE INSTALLED AND TESTED IAW MM 53-53-00.Feb 5, 1998 · N14890 · Doug DC982SDR DHL9880699CFairing · chippedAT C-CHECK, UNDER WING FAIRING HAS EDGE PANEL CHIPPED OFF. REMOVED AND REPLACED DAMAGED PANEL PER SRM 51-1-15.Feb 2, 1998 · N806DH · Doug DC873FSDR P5CA9800395Fairing · delaminatedFUSELAGE BODY FAIRING 1920 FOUND PUNCTURE HOLE AND DELAMINATION. BODY FAIRING FIBERGLASS REPAIRED PER SRM 51-40-15.Jan 29, 1998 · N3203Y · Boeing 747128SDR CALA9800134Cables · out of adjustTHE PULL FROM EXTERIOR TAILCONE RELEASE HANDLE WAS LOW. THE TAILCONE CABLES WERE ADJUSTED.Jan 28, 1998 · N14839 · Doug DC982SDR 9801779975Clips · out of adjustDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE EXTERIOR RELEASE HANDLE FROM CLIPS AND INADEQUATE FORCE WAS REQUIRED TO REMOVE INTERIOR RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS. FUNCTIONAL CHECK OK.Jan 28, 1998 · N9339 · Doug DC931SDR LR7A9815Fairing · crackedDURING C-CHECK/BRIDGING INSPECTION, CENTER WING LEADING EDGE TO INBOARD ENGINE NACELLE FAIRING ASSY WEB HAS 2 CRACKS AT CW STA 174. TRIMMED OUT CRACKS, INSTALLED FILLER AND DOUBLER.Jan 27, 1998 · N903SJ · Lkheed 382GSDR 9801549301Tail Cone · fell offDURING LANDING ROLLOUT, TAIL CONE FELL OFF THE AIRCRAFT AND DEPLOYED SLIDE. MAINTENANCE REPLACED AND RIGGED THE SLIDE AND TAIL CONE, FUNCTIONAL CHECK OK.Jan 24, 1998 · N301RC · Doug DC982SDR 9801439301Tail Cone · deployedDURING LANDING ROLLOUT, THE AIRCRAFT EXPERIENCED AN INADVERTANT TAIL CONE DEPLOYMENT. MAINTENANCE REPLACED TAIL CONE ASSEMBLY AND SLIDE.Jan 24, 1998 · N301RC · Doug DC982SDR 9801679908Clips · wornDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE DEPLOYMENT HANDLE FROM CLIPS. REPLACED SPRING CLIPS, FUNCTIONAL CHECK OK.Jan 23, 1998 · N958N · Doug DC931SDR CALA9800098Cable · damagedINSPECTION FOUND TAILCONE RELEASE CABLE KINKED AT TOP LEFT PULLEY. THE CABLE WAS REMOVED AND REPLACED AND RIGGED IAW MM 53-53-00.Jan 21, 1998 · N936AS · Doug DC982SDR DLM88980148Radome · collapsedA/C EXPERIENCED LOUD POP AND THEN LOUD RUSH OF AIR NEAR COCKPIT EXTERIOR. PRESSURIZATION OK. RTB ATL WHERE TWR NOTIFIED THE CREW THE RADOME HAD COLLAPSED. REMOVED AND REPLACED RADOME. INSPECTED BOTH ENGS FOR FOD AND AIRFRAME FOR DAMAGE, NONE NOTED. TESJan 19, 1998 · N918DE · Doug MD88SDR 9801979935Clips · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR RELEASE HANDLE FROM THE CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK.Jan 17, 1998 · N1332U · Doug DC931
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