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 DALA13012390966Release Mech · damagedMX DISCOVERED THAT THE TAILCONE RELEASE CABLE, CABLE SLIDING BLOCKS, CAM RELEASE MECHANISM, TEE PIN BUSHINGS, LATCH HOUSING, AND LATCH SPRINGS WERE FRAYED, WORN, OR DAMAGED BEYOND ALLOWABLE LIMITS. THE ITEMS WERE ALL REPLACED AND THE SYS WAS RIGGED TO SPECIFIMar 14, 2013 · N966DL · Doug MD88SDR DALA13012869013Bracket · crackedDURING CHECK, TAILCONE UPPER LT BAYONET BRACKET WAS FOUND CRACKED. REMOVED, FABRICATED, HEAT TREATED, PRIMED AND INSTALLED BRACKET IAW DWG 9911957.Mar 11, 2013 · N913DE · Doug MD88SDR DALA13011189210Conduit · dentedDURING SERVICE CHECK, TAILCONE RELEASE CABLE CONDUIT FOUND DENTED, LOCATED AFT FRAME UNDER SLIDE PACK. R & R CABLE CONDUIT IAW MM. OPERATIONS AND CLEARANCE CHECK IAW AMDS 5352-7116.Mar 9, 2013 · N910DN · Doug MD9030SDR DALA13011179013Bracket · wornDURING SERVICE CHECK, TAILCONE BUNGEE SPRING BRACKET IS WORN. R & R IAW MM.Mar 8, 2013 · N913DE · Doug MD88SDR V0XR20130310J0175Fairing · looseLOOSE FASTENERS AT FRAME BETWEEN 59/60 BETWEEN STR 21L AND 21R. INSTALLED DOUBLERS IAW EC5320-01761 AND INSTALLED RT AND LT FAIRINGS IAW SRM 51-40-02.Mar 7, 2013 · N16987 · Emb EMB145LRSDR DALA13011393273Skin · dentedDURING INSPECTION, FOUND TAILCONE EXTERNAL SKIN DENTED AT FR80 RT SIDE APPROX 8" FROM TOP CENTER LINE. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-11, FIG 108, DIA 104. L=.850 W=.850 IAW SRM 53-51-11, FIG 203. FABRICATED REPAIR DOUBLER IAW SRM 53-51-11, FIG 203Mar 6, 2013 · N373NW · Airbus A320212SDR DALA13011169210Latch · lack of lubeDURING CHECK, VENTRAL STAIR DOOR TAILCONE RELEASE FAILED. CLEANED AND LUBRICATED TAILCONE LATCHES AND CABLES. PERFORMED TAILCONE FUNCTIONAL CHECK IAW MM. OPS CHECK OF THE AFT ENTRY DOOR WITHIN LIMITS.Mar 5, 2013 · N910DN · Doug MD9030SDR QXEA2013030500540Fairing · chafedUPPER WING TO FUSELAGE FAIRING PANEL 262AT IS CHAFED ON MATING SURFACE. REMOVED DAMAGE IAW SRM 51-14-00-02-03, REV 12. CONFIRMED AFFECTED AREA CRACK FREE NTM 51-00-06-910-801 PT REV 7. DAMAGE IS IN LIMITS IAW SRM 53-75-06-02-01, REV 12.Mar 5, 2013 · N434MK · Bombdr DHC8402SDR QXEA2013030500526Fairing · chafedUPPER WING TO FUSELAGE FAIRING PANEL 262FT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE IAW SRM 51-14-00-02-03, REV 12. MECHANICALLY MEASURED MIN REMAINING THICKNESS IS 0.098" IN LIMITS IAW SRM 53Mar 5, 2013 · N434MK · Bombdr DHC8402SDR QXEA2013030500525Fairing · chafedUPPER WING TO FUSELAGE FAIRING PANEL 262HT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE IAW SRM 51-14-00-02-03, REV 12. MECHANICALLY MEASURED, MIN REMAINING THICKNESS IS 0.088" IN LIMITS IAW SRM 5Mar 5, 2013 · N434MK · Bombdr DHC8402SDR QXEA2013030300527Fairing · crackedRT UNDERWING FAIRING IS CRACKED AT FUSELAGE STA X428.500. REMOVED WING TO FUSELAGE FAIRING PANEL 262JT TO FOM IAW REV 40 20-50-53-000-802. REMOVED CRACKED UNDERWING FAIRING STRUCTURE IAW SRM REV 12 51-42-05-02-01. REMOVED 2(EA) FAIRING SUPPORT ANGLES TO FOMMar 3, 2013 · N434MK · Bombdr DHC8402SDR DALA13009730954Receptacle · wornDURING SCHEDULED MX, THE UPPER TOP RT TAILCONE LATCH RECEPTACLE WAS FOUND TO BE WORN. THE TOP RT LATCH RECEPTACLE WAS R & R IAW AMM 53-53. THE REQUIRED RII INSPECTION WAS PERFORMED.Mar 1, 2013 · N954DL · Doug MD88SDR DALA13009720954Cover · damagedDURING SCHEDULED MX, THE SLIDE COVER ON THE AFT TAILCONE SLIDE WAS FOUND TO BE IN POOR CONDITION WITH SOME MISSING HOOK AND LOOP STRAP, AND LOOSE STENCIL. THE SLIDE COVER WAS R & R IAW AMM 25-62-01 AND THE RII INSPECTION WAS ACCOMPLISHED.Mar 1, 2013 · N954DL · Doug MD88SDR DALA13009710954Latch · wornDURING SCHEDULED MX, THE LOWER RT TAILCONE RELEASE LATCH WAS FOUND TO BE WORN. THE LOWER RT LATCH WAS REPLACED IAW AMM 53-53 AND THE RII INSPECTION WAS PERFORMED.Mar 1, 2013 · N954DL · Doug MD88SDR DALA13009700954Spring · brokenDURING SCHEDULED MX, THE LOWER LT TAILCONE LATCH SPRING WAS FOUND TO BE WORN, THE WORN SPRING WAS REPLACED IAW AMM 53-53 AND THE RII INSPECTION WAS COMPLETED.Mar 1, 2013 · N954DL · Doug MD88SDR DALA13009690954Bushing · wornDURING SCHEDULED MX OF THE TAILCONE RELEASE MECHANISM, THE LT TAIL CONE TEE PIN & BUSHINGS WERE FOUND TO BE WORN BEYOND LIMITS. THE TEE PIN AND BUSHINGS WERE REPLACED IAW AMM 53-53 AND THE RII INSPECTION WAS COMPLETED.Mar 1, 2013 · N954DL · Doug MD88SDR DALA13009590954Bracket · wornDURING SCHEDULED CHECK, FOUND AFT TAILCONE RELEASE CABLE SPRING BRACKETS WORN. REPLACED WORN BRACKETS IAW SRM 51-30.Mar 1, 2013 · N954DL · Doug MD88SDR DALA13009580954Release Cable · wornDURING INSPECTION, FOUND TAILCONE RELEASE CABLE TO BE WORN. REPLACED KEVLAR CABLE IAW AMM 53-53.Mar 1, 2013 · N954DL · Doug MD88SDR UALA2013030101226Seal · deterioratedPAX AND F/A REPORT A VIBRATION AT FLOOR LEVEL, AT ROW 20DEF. NO ABNORMAL COCKPIT INDICATIONS. FOUND LOWER BELLY FAIRING SEALS ON PANELS 197GB AND 198GB DEGRADED FROM SKYDROL. TAPED SEALS PER MT53-004. REPLACED SEALS ON PANEL 197GB AND 198GB REF MT 53-017.Feb 28, 2013 · N437UA · Airbus A320232SDR DALA13009750954Receptacle · wornDURING SCHEDULED MX INSPECTION, THE TAILCONE ALIGNMENT PIN RECEPTACLES WERE FOUND TO BE WORN. THE WORN RECEPTACLES WERE REPLACED IAW AMM 53-53. THE REQUIRED RII INSPECTION WAS PERFORMED.Feb 28, 2013 · N954DL · Doug MD88SDR DALA13009740954Block · wornDURING SCHEDULED MX, AT THE UPPER LT TAILCONE LATCH, THE RELEASE CABLE BLOCK WAS FOUND TO BE WORN. THE CABLE BLOCK AT THE UPPER LT LATCH WAS REPLACED IAW AMM 53-53. THE REQUIRED RII INSPECTION WAS PERFORMED.Feb 28, 2013 · N954DL · Doug MD88SDR Q2SA20130224201Fairing · damagedON POSTFLIGHT WALKAROUND FOUND DAMAGE ON BODY FAIRING 191 B. REMOVED AND REPLACED PANEL 191 B WING TO BODY FAIRING IAW B-747 AMM 53-51-01. REPLACEMENT PANEL INSPECTED IAW B-747 SRM 51-10-06, NO DEFECTS NOTED.Feb 24, 2013 · N400SA · Boeing 747412SDR DALA13012179009Receptacle · wornDURING CHECK, MX FOUND TAILCONE LATCH RECEPTACLES WORN. R & R RT & LT RECEPTICLES IAW AMM 53-53-00.Feb 23, 2013 · N909DE · Doug MD88SDR DALA13012149009Bracket · wornDURING SERVICE CHECK, KEVLAR SPRING BRACKET WORN ON RT SIDE OF TAILCONE. R & R BOTH BRACKETS IAW SRM 51-30-02.Feb 23, 2013 · N909DE · Doug MD88SDR DALA13012139009Cable · wornDURING CHECK, KEVLAR CABLE ON TAILCONE FOUND WORN. R & R KEVLAR CABLE IAW MM 53-53-00.Feb 23, 2013 · N909DE · Doug MD88SDR DALA13012129009Cable · out of limitsDURING CHECK, CABLE BLOCK FOUND OUT OF LIMITS ON TAILCONE. R & R CLAMPS AND ADJUSTED CLEARANCE BETWEEN BLOCK AND CONDUIT IAW MM 53-53-00.Feb 23, 2013 · N909DE · Doug MD88SDR DALA13009509009Block · wornDURING CHECK, SLIDING BLOCK WORN. UPPER LT SIDE TAILCONE. R & R SLIDING BLOCK IAW AMM. RIG COMPLIED WITH.Feb 22, 2013 · N909DE · Doug MD88SDR DALA13009189009Receptacle · wornPIN RECEPTACLES WORN ON AFT FLANGE OF TAILCONE. R & R WORN PIN RECEPTACLES ON TAILCONE IAW SRM 51-30-02.Feb 22, 2013 · N909DE · Doug MD88SDR QXEA2013022100524Fairing · chafedUPPER WING TO FUSELAGE FAIRING PANEL 261LT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE SRM 53-75-06-02-01 REV 12. CONFIRMED CRACK FREE IN AFFECTED AREA REF NTM 51-00-06-910-801, PT 1, REV 7. MECHAFeb 21, 2013 · N434MK · Bombdr DHC8402SDR QXEA2013022100523Fairing · chafedUPPER WING TO FUSELAGE FAIRING PANEL 261FT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE IAW SRM 53-75-06-02-01, REV 12. CONFIRMED CRACK FREE REF NTM 51-00-06-910-801 PT 1, REV 7. MECHANICALLY MEAFeb 21, 2013 · N434MK · Bombdr DHC8402SDR QXEA2013022100522Fairing · chafedUPPER WING TO FUSELAGE FAIRING PANEL 261HT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE IAW SRM 53-75-06-02-01 REV 12. MECHANICALLY MEASURED, MIN REMAINING THICKNESS IS 0.099". DAMAGE IS IN LIMITFeb 21, 2013 · N434MK · Bombdr DHC8402SDR QXEA2013022100521Fairing · chafedUPPER WING TO FUSELAGE FAIRING PANEL 261CT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE IAW SRM 53-75-06-02-01, REV 12. MECHANICALLY MEASURED, MIN REMAINING THICKNESS IS 0.092" IN LIMITS IAW SRM 5Feb 21, 2013 · N434MK · Bombdr DHC8402SDR AALA20130221013Guide · gougedFRAME STATION 200 STRINGER 30 LOWER RADOME GUIDE GOUGED ON LOWER SIDE OF GUIDE ON PRESSURE BULKHEAD. REMOVED AND REPLACED GUIDE PER SRM 51-40-02 AND BAC DRAWING 141N7838 REV K.Feb 21, 2013 · N628AA · Boeing 757223SDR SWAA2013030613385Nut Plate · corrodedLEFT WING TO BODY FAIRING - HAS NUMEROUS CORRODED NUT PLATES BETWEEN STA 588-674, BETWEEN LONG 20L - 2R. REMOVED & REPLACED NUT PLATE IAW SRM.Feb 19, 2013 · N959AT · Boeing 717200SDR SWAA2013030613384Nut Plate · corrodedLEFT WING TO BODY FAIRING - HAS NUMEROUS CORRODED NUT PLATES BETWEEN STA 851-927, BETWEEN LONG 19L-19R. REMOVED & REPLACED NUT PLATES IAW SRM.Feb 19, 2013 · N959AT · Boeing 717200SDR SWAA2013030613383Nut Plate · corrodedRIGHT WING TO BODY FAIRING - HAS NUMEROUS CORRODED NUT PLATES BETWEEN STA 588-674, BETWEEN LONG 20L - 2R. REMOVED & REPLACED NUT PLATE IAW SRM.Feb 19, 2013 · N959AT · Boeing 717200SDR SWAA2013030613382Nut Plate · corrodedRIGHT WING TO BODY FAIRING - HAS NUMEROUS CORRODED NUT PLATES BETWEEN STA 851-927, BETWEEN LONG 19L-19R. REMOVED & REPLACED NUT PLATES IAW SRM.Feb 19, 2013 · N959AT · Boeing 717200SDR DALA13008489014Conduit · out of rigDURING TAILCONE FUNCTIONAL CHECK, LOWER CONDUITS FOR PULL CABLES IAW STEP 4D5, FOUND OUT OF RIG. REPOSITIONED CONDUIT IAW AMM.Feb 19, 2013 · N914DE · Doug MD88SDR DALA13008479014Bushing · wornDURING TAILCONE FUNCTIONAL TEST, FOUND TEE PIN BUSHINGS WORN. REPLACED TEE PIN BUSHINGS IAW AMM.Feb 18, 2013 · N914DE · Doug MD88SDR DALA13008469014Cable · frayedFOUND TAILCONE KEVLAR CABLE FRAYED. R & R KEVLAR INTERIOR CABLE IAW AMM. OPS CHECKS GOOD.Feb 18, 2013 · N914DE · Doug MD88SDR FDEA201302170357Skin · dentedDENT ON TAILCONE JUST AFT OF RIB 92 AND 93 BETWEEN STR 2L AND 3L APPROX. 1" X 1". REPAIRED DENT ON TAILCONE AFT OF FR 92 (RIB) BETWEEN STR 2 AND 3L IAW EA 6-5310-T0300131 REF WRI 53103597.Feb 17, 2013 · N410FE · Airbus A310203SDR DALA13007959015Cam · failedTAILCONE RELEASE MECHANISM CAM FAILED. R & R CAM ASSY IAW AMM.Feb 14, 2013 · N915DE · Doug MD88SDR UALA2013021300864Seal · damagedAIRFRAME VIBRATION WITH FLAPS FULL NOT EXISTENT AT FLAPS THREE. FREE MOVEMENT AT TRAILING EDGE OF FLAPS, SPHERICAL BEARING. FOUND RIGHT WING TO FUSELAGE FAIRING SEAL SEVERLY DAMAGED. REPLACED SEAL PER AMM. DIAGNOSED PER TSM 27-54-00. NO OTHER DEFECTS WERE FOFeb 13, 2013 · N474UA · Airbus A320232SDR R61A201302130155Fairing · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT 195 UPPER FAIRING SKIRT CRACKED. MAINTENANCE REPAIRED THE RIGHT 195 UPPER FAIRING SKIRT IAW EMB ETD2013-170-002709. THE AIRCRAFT WAS RELEASED FROM HEAVY CHECK 2-15-13.Feb 13, 2013 · N805MD · Emb ERJ170100SUSDR DALA13007550934Latch · wornUPPER LT AND RT TAILCONE RETENTION LATCHES WORN. REPLACED UPPER LT TAILCONE LATCH ASSY WITH PN 3913351 IAW AMM 53-53. BLENDED WORN PARTS W/IN LIMITS IAW DWG 4920459-3. INSTALLED LATCH RIGGING ACCOMPLISHED ON CARD 53-50-01077-0101. INSTALLATION IAW IPC 53-50-Feb 12, 2013 · N934DL · Doug MD88SDR UALA2013021100802Paint · missingRADOME HAS PAINT MISSING FROM NOSE. REMOVED AND REPLACED RADOME.Feb 10, 2013 · N673UA · Boeing 767322SDR DALA13006749232Release Mech · out of toleranceDURING TAILCONE FUNCTIONAL CHECK STEP 4 OF AMDS CARD 5352-7116, MX FOUND TAILCONE RELEASE OUT OF LIMITS. RELEASED TO HIGH. ADJUSTED CLIPS ON TEE PIN AND PULL HANDLE INTERIOR. LUBED TAILCONE. PULLED WITHIN LIMITS IAW AMDS CARD. OPS CHECKED GOOD.Feb 8, 2013 · N932DN · Doug MD9030SDR ABXA20120207395Structure · corrodedLEFT SIDE FRAME (PICKLE FORK) SEVERAL AREAS OF CORROSION, ON FORWARD MATING SURFACE COMMON TO REAR SPAR PAD AREA. REPAIRED AREAS OP CORROSION AS SPECIFIED IAW WITH AMES DOCUMENT 47033REA06. SPOT FACES 2.9" 5 EA 125R, DEPTH .020, 2EA 2.5" .125R, DEPTH .020 ARFeb 7, 2013 · N783AX · Boeing 767281SDR ERAA20130022Web · crackedCRACK FOUND ON LEFT WEB OF WING TO FUSELAGE FAIRING AT STA.X370.8. REPAIRED IAW BOMBARDIER REPAIR DRAWING RD8-53-12831 ISS. 2Feb 6, 2013 · N883EA · Dhav DHC8106SDR SWAA2013021212585Tail Cone · delaminatedTAIL CONE IS DELAMINATED ON TOP UPPER LEFT SIDE. REPAIRED TAIL CONE PER SRM.Feb 5, 2013 · N401WN · Boeing 7377H4
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