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 UIEA2011100300535Skin · dentedTAIL CONE LT UPPER HALF EXT SKIN HAS A DENT MARK AT STA 2707 APPROX BWL 359.7. SKIN PATCH REPAIRED IAW R5-53-81-37225 REV A.SDR CHQA201100355Attach Angle · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE FAIRING ATTACHMENT ANGLE. REPAIRED THE WING TO FUSELAGE ATTACHMENT ANGLE NUMBER 2 AFT SECTION IN ACCORDANCE WITH ETD 2011-145-104225.SDR DALA1151656309Rib · crackedCRACK WAS FOUND ON RIB OF RADOME SUPPORT AT STA 134, LBL 6, L=1.5" DFRD PER B747-400 SRM 51-40-02 P1 REPLACED THE RIB WITH NEW PART.SDR P5CA2011082000460Radome · damagedBIRD STRIKE TO NOSE AREA DURING CLIMBOUT. (BIRD STRIKE CONDITIONAL INSPECTION COMPLIED WITH AS PER AMM 05-51-14-202-001 RADOME TIME LIMITED REPAIR CARRIED OUT AS PER EO 4453A617 PART 1 WITH A FAA 8110-3 FORM ISSUED ON 20 AUGUST 2011. PER EO 4453A617 ASDR VNAA2011082500012Radome · damagedAT MDT, CREW REPORTED POSSIBLE LIGHTNING STRIKE TO NOSE OF AIRCRAFT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RADOME AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.SDR ASMF201108004Radome · damagedCAPTAIN REPORTED THAT DURING TAKEOFF, ACFT FLEW INTO A HAIL RAIN. A HAIL STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18-212-801 DETECTING LT AND RT RETRACTABLE LANDING LIGHTS WITH CRACKS, NOSE RADOME WITH DAMAGES OUT OF LIMITS; VHF COMMUNICATION SDR UALA2011081104225Radome · damagedRADOME NOSE SKIN PITTED DOWN TO HONEYCOMBED. REPLACED NOSE RADOME PER MM.SDR UIEA2011081000452Fairing · crackedDURING WALK-AROUND INSP, MX REPORTED LT INBD WING TO FUSELAGE PANEL 293AL - WBL 128.46 CRACK/DAMAGE (REF FIG 1). PERFORMED A TIME LIMITED REPAIR.SDR DALA1146289016Tube · wornDURING HMV A WORN FUSELAGE TUBE OF T/E TAIL CONE CONTROL CABLES RELEASE SYSTEM WAS FOUND AT STA Y=1510 CANT 5 AND 7 O'CLOCK POSITION. FUSELAGE TUBE WAS REPLACED IAW MM 20-30-01-201.SDR UALA2011080304013Fairing · missingDURING RAMP CHECK FOUND PANEL MISSING ON AFT TOP OF RIGHT LANDING GEAR BODY DOOR AREA. ACCOMPLISH REPAIRS PER EVA 81169. RT WING MLG SIDE STRUT SWIVEL FAIRING ASSEMBLY TEMPORARY FAIRING INSTALLED AS PER EVA-8 1169. VERIFICATION REQUIRED BEFORE EACH FLIGHT SDR UIEA2011080200415Fairing · crackedDURING WALK-AROUND INSPECTION, MX REPORTED RT BS 1067 - WING TO BODY FAIRING 192CR CRACKED, LOCATED APPROX 8 -10 INCHES AFT OF RT CTR FUEL TANK DRAIN. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE RESDR FDEA201107272992Strut · corrodedFUSELAGE TAIL SECTION FR 86, 2EA CROSS STRUTS CORRODED AT STR15 LT AND RT.SDR UALA2011072503797Radome · damagedRADOM DIVIDER STRIPS MISSING IN SPOT R AND SURFACE IS CHIPPED TO EXPOSE COMPOSITE MATERIAL 14 SPOTS. REPLACED AND ADJUSTED RADOME IAW MM.SDR UALA2011071903666Radome · damagedON WALKAROUND NOTICED SEVERAL SMALL HOLES IN RADOME EVIDENCE OF LIGHTNING STRIKE. TAPED OVER HOLES IN RADOME. OPENED RADOME AND VERIFIED THAT HOLES DIDN'T PENETRATE THROUGH TO INNER SURFACE. CLOSED RADOME. PERFORMED LIGHTNING STRIKE INSP OF ENTIRE AC. NO SDR JR2R2011071200277Channel · crackedAFT WING TO BODY FAIRINGS CTR ATTACH STRAP AFT STIFFENER IS CRACKED.SDR AALA20110613DFW03Radome · damagedDFW - CREW REPORTED MULTI BIRD STRIKES TO RADOME, WINGS AND POSSIBLE ENGINE INGESTION. NO VIBRATIONS OR ENGINE INDICATIONS. EMERGENCY DECLARED FLIGHT RETURNED DFE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SEVRICE. REPLACED RADOME. SYSTEM GROUND CHECKSDR JR2R2011060100228Skin · debondedPERM REPAIR FOR A LARGE AREA DISBONDED ON TAIL CONE.SDR UIEA2011052200266Fairing · damagedDURING LOADING OPERATIONS; A CARGO DOLLY STRUCK ACFT CAUSING DAMAGE TO WING TO BODY FAIRINGS FROM BS800 TO BS1000. UPON INSPECTION OF THE DAMAGED AREAS FOUND 3 WING/BODY FAIRINGS WITH PUNCTURES AND SCRATCHES. THE DRAIN MAST WAS ALSO DAMAGED DURING THIS INCIDSDR UALA2011051802446Skin · damagedRT WHEEL WELL AFT SIDE OF WHEEL WELL FUSELAGE FAIRING DAMAGED. FAIRING SKIN CRACKED AROUND ATTACHMENT BASE OF FAIRING SUPPORT ROD FITTING. REMOVED PANEL 148FB AND BEGAN REPAIR REF SRM.SDR CA110520004Access Panel · departedTHE OPERATOR REPORTED TO MFG THAT DURING A PREFLIGHT WALKAROUND, THE FLIGHT CREW FOUND A SECTION OF THE AFT BELLY FAIRING MISSING. PHOTOGRAPHIC EVIDENCE PROVIDED BY THE OPERATOR SHOWED 2 BELLY FAIRING ACCESS PANELS 185CL (PN GS297-0137-7) & 186CR (PN GS297-01SDR IPXA1566689Stiffener · corrodedINSPECTION TYPE:C, RT LOWER WING TO BODY FAIRING SUPPORT CHORD AT BS 1193 RBL-64 WL 138 IS CORRODED. R & R CHORD IAW SRM 51-40-02-0G, SRM 51-20-01-0G AMM 51-21-04-7, 51-21-00-7.SDR DALA1131780917Cable · brokenBROKEN STRANDS ON TAIL CONE RELEASE SYSTEM CONTROL CABLE STA 1510 CANT 08 O'CLOCK POSITION. REPLACED CABLE PER MM 53-53-00-501.SDR UALA2011050602222Radome · damagedUPON ARRIVAL CHKD FOUND BIRD STRIKE EVIDENCE ON RADOME. CHK'D AREA NO CRACK AND NO PUNCTURE, BUT SKIN HAS DELAMINATIONS AT LEFT-TOP POSITION, THE SPONGY DAMAGE SIZE IS 19" X 19". REPLACED A RADOME PER MM. REPLACED WITH JAL PARTS PN 284T0052-39 SN 000169.SDR DALA1138880915Pulley · corrodedDURING MAINTENANCE VISIT, MECHANIC FOUND RUSTED AND DAMAGED HARDWARE AND PULLEYS ON TAIL CONE RELEASE SYSTEM. MAINTENANCE REMOVED AND REPLACED DAMAGED AND RUSTY PULLEYS AND HARDWARE.SDR UALA2011042702060Radome · crackedRADOME OPENED FOR INSPECTION AFTER BIRD STRIKE. FOUND RADOME CRACKED & DELAMINATED AT UPPER LEFT EDGE (LOOKING AFT) BY BIRD STRIKE, LATCHED 2-EA MIDDLE LOCKS FOR TAXI TO HANGAR. REPLACED RADOME.SDR DALA1131550917Tube · wornWORN FUSE TUBE OF TAIL CONE RELEASE CABLE AT 5 O'CLOCK POS STA 1510 CANT. REPLACED CABLE.SDR UALA2011042501990Radome · damagedCREW REPORTED A BIRD STRIKE ON TAKEOFF. 140KTS AT ROTATION JUST BELOW RADOME. ACCOMPLISHED INSP REF AMM, DAMAGE FOUND TO RADOME ONLY. REPLACED RADOME.SDR VNAA2011042800019Radome · damagedAT CLT, CREW REPORTED LIGHTNING STRIKE. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED RADOME, LOWER VHF ANTENNA, RIGHT LANDING LIGHT, FCC NR 1 (FLIGHT CONTROL COMPUTER), LOWER TAIL NAV LIGHT LENS AND RING, AFT DRAIN MAST, RIGHT STROBE POWER SUPPLY ASDR UALA2011042501999Radome · damagedRADOME BIRD STRIKE. MEASURE DELAMINATED AREA 11X15 INCHES DELAMINATED. OUT OF MM LIMITS, REPLACED RADOME. ACCOMPLISHED VISUAL INSP OF AIRCRAFT AND NO DEFECTS NOTED. RADOME SECURED CLOSED.SDR UALA2011041801860Radome · damagedFUSELAGE INCURRED LIGHTNING STRIKES. REPLACED RADOME.SDR UALA2011041501813Radome · damagedBIRD STRIKE ON CLIMBOUT. LARGE BIRD HIT RADOME, RADAR INOPERATIVE. ACCOMPLISHED BIRD STRIKE INSPECTION PER MM. SEE SMC WRITE-UPS FOR DAMAGED AREAS AFFECTED (RADOME AND LT MLG WRITE-UP). DURING INSP FOUND L-WING LE PANEL HAS SEVERAL CRACKS WILL NEED TWO 250SDR DALA1131520917Tube · wornWORN FUSE TUBE OF TAIL CONE RELEASE CABLE BTWN 6 AND 7 O'CLOCK. REPLACED TUBE.SDR DALA1125619213Tail Cone · damagedTAIL CONE T/E LWR END CAP LIGHTNING DAMAGE.SDR HALA2011041200153Paint · damagedON OVERNIGHT FOUND LIGHTNING STRIKE ON LOWER NOSE RADOME. UPON INSP OF METALIC STRUCTURE FOUND NO STRUCTURAL DAMAGE CLEANED & PAINTED BURN MARK. C/W HAL M251-767 & AMM 05-51-19-212-001. NO FURTHER EVIDENCE OF LIGHTNING STRIKE DAMAGE.SDR ZZDA2011382Release Mech · out of adjustTAIL CONE RELEASE MECHANISM, OUT OF ADJUSTMENT. ACCOMPLISHED RELEASE MECHANISM ADJUSTMENT PER B717 AMM 53-52-03-820-801.SDR HYIA14834VIBFairing · misinstalledON APPROACH, THE ACFT STARTED TO EXPERIENCE ABNORMAL VIBRATIONS. WHEN VIBRATION STARTED THE AUTO PILOT WAS DISENGAGED AND THE ACFT WAS FLOWN MANUALLY. AS THE ACFT DESCENDED AND SLOWED DOWN, THE VIBRATION ALSO DECREASED. WHEN VIBRATION STARTED, THE F/A REPORTESDR DALA1131510917Fastener · corrodedRUSTED HARDWARE ON TAIL CONE RELEASE SYSTEM CONTROL CABLE HARDWARE STA 1510 CANT. REPLACED HARDWARE.SDR DALA1124745523Fairing · damagedDAMAGE TO LEFT BODY FAIRING PANEL 191AL IAW ER/A 491594-14 MADE TEMP REPAIR. REFERENCE LOG PAGE 0332195. ER/A 491594 SECTION I ISSUED FOR WING TO BODY FAIRING DAMAGE, PANEL 191AL AT BS 800. ASSOCIATED ER/A CHANGED FROM 13-491594 TO 14-491594 FOR AC 5523 APPSDR FDEA201104061352Skin · dentedDENT FR93-94 LT SIDE. TAILCONE AREA 9 O'CLOCK LOCATION ALF. EA 6-5330-149398 RAISED TO COVER DAMAGE SITE, AND FOUND TO BE WITHIN LIMITS.SDR V0XR20110404025Attach Angle · crackedLEFT LOWER FWD FAIRING ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED LT LOWER FWD FAIRING ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 5068SDR IPXA11566223Support · chafedINSPECTION TYPE:C1, AFT RT WING TO BODY FAIRING 196AR, AFT ATTACH SUPPORT, OUTER SURFACE OF CHORD CHAFED, AT THE LWR CORNER OF THE PANEL AREA (MARKED) REMOVED, FABRICATED AND REPLACED FAIRING 196AR AFT ATTACH SUPPORT IAW SRM 53-40-70, SRM 53-40-70-OI. SRM SDR IPXA11566209Support · chafedINSPECTION TYPE:C1, AFT LT WING TO BODY FAIRING 195AL, AFT ATTACH SUPPORT, OUTER SURFACE OF CHORD CHAFED, AT THE LWR AFT CORNER OF THE PANEL AREA. MARKED REMOVED, FABRICATED AND REPLACED FAIRING 195AL AFT ATTACH SUPPORT IAW SRM 53-40-71-1, SRM 53-40-71-0ISDR VNAA2011040500001Radome · damagedCREW REPORTED LIGHTNING STRIKE ON RT SIDE OF THE NOSE AREA. MAINTENANCE INSPECTED AND REPAIRED DAMAGE. THE RADOME WAS ALSO REMOVED AND REPLACED. ALL WORK WAS ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR V0XR20110401007Strip · cracked(V0XR) LT WING-BODY FAIRING STRIP NR 4 BACK HAS CRACK. REMOVED AND REPLACED LT WING-BODY FAIRING STRIP NR 4 IAW EMB145 SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 2061SDR V0XR20110331008Strip · crackedRT UPPER WING-BODY FAIRING STRIP, NR 4 BACK IS CRACKED. REMOVED AND REPLACED RT UPPER WING-BODY FAIRING FAIRING STRIP IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 2057SDR V0XR20110331007Strip · crackedRT UPPER WING-BODY FAIRING STRIP, NR 2 BACK IS CRACKED. REMOVED AND REPLACED RT UPPER WING-BODY STRIP NR 2 IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 2056SDR CNMA20110008Radome · dentedBIRD STRIKE - AFTER BIRD STRIKE INSP FOUND RADOM DAMAGE INDENTED APPROX 2 FT ROUND SLIGHT LT OF CTR. R & R NOSE RADOME IAW AMM 53-12. LATCHED AND OK FOR SERVICE, RADOME WAS NOT PERFORATED AND RADAR ANTENNA AREA WAS INTACT.SDR DXTA2011031004502Drain · obstructedON CLIMB OUT, PASSING FL 220, RUDDER EFFECTIVENESS LOST. RUDDER FELT FROZEN. FREEZING LEVEL FL160. ON DESCENT REGAINED RUDDER EFFECTIVENESS AT FL140, JUST BELOW FREEZING LEVEL. RUDDER WAS NORMAL FOR APPROACH AND LANDING. REMOVED ACCESS PANEL AND FOUND ICE.SDR ZZDA2011265Skin · dentedFORWARD OF TAIL CONE FUSELAGE SKIN, DENTED. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER B717 SRM 53-00-01 REP 6 AND EA 17-53-02869IR.SDR ZZDA2011254Pin · out of alignmentTAIL CONE DEPLOYMENT SYSTEM RELEASE MECHANISM CAM PIN NOT ALIGNED. ROTATED TAIL CONE RELEASE MECHANISM CAM PIN FULLY CLOCKWISE TO CORRECT POSITION WAS REQUIRED IAW BOEING 717 MM 53-52 NO ADJUSTMENTS MADE TO SYSTEM OR SETTINGS. OK FOR CONTINUED SERVICE.
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