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 SWAA2016042651351Dome Nut · damagedRIGHT SIDE FUSELAGE AFT WING TO BODY PANEL 3678R, DOME NUT DAMAGED AT BS 747-4, BETWEEN STRINGER 19R - 20R. R & R DOME NUT IAW SRM.SDR DALA2016042503266Cam · dislodgedDURING A CHECK OF TAILCONE RELEASE MECHANISM, MAINTENANCE FOUND THE CAM ASSY FOR THE TAILCONE LATCH WAS DISLODGED. MAINTENANCE REINSTALLED THE CAM ASSY. THE TAILCONE WAS RIG CHECKED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII COMPLETED FOLLOWING MAINTSDR DALA2016040802711Cam · looseTAILCONE JETTISON CAM ASSY LOOSE. RIGGED JETTISON CAM IAW AMM 53-50.SDR DALA2016040602716Cable · brokenTAILCONE JETTISON BOTTLE CABLE BROKEN. INSTALLED NEW CABLE ASSEMBLY.SDR FDEA201603311134Radome · defectiveEXCESSIVE STATIC ON BOTH RADIOS WHILE IN CLOUDS. FOUND DEFECTIVE RADOME WITH STATIC TESTER IN TWO LOCATIONS, TOP LIGHTNING ARRESTER STRIP, 12 O'CLOCK POSITION, & BOTTOM LIGHTNING ARRESTER STRIP, 6 O'CLOCK POSITION. REST OF AREAS ON ACFT CHECKED WERE OKAY, TSDR P5CA2016033000073Radome · crackedRADOME FOUND WITH 18 INCH CRACK, OUT OF LIMITS. RADOME REPLACED IAW AMM 53-12-01.SDR SWAA2016040550622Support Angle · crackedWING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CRACKED AT BS 540, BETWEEN STRINGER 22R - 23R AT LOWER FUSELAGE. R & R ANGLE IAW SRM & DWG.SDR DALA2016032802379Pin · gougedTHE TAILCONE RELEASE OPS CHECK FAILED. MSP MAINTENANCE FOUND A T-PIN GOUGED AND REPLACED IT.SDR DALA2016032802378Pin · gougedON SHIP 945, MSP MAINTENANCE FOUND THE UPPER LT TAIL CONE RELEASE LOCK PIN GOUGED. THE LOCK PIN WAS REPLACED BY MSP MAINTENANCE.SDR DXTA2016032306211Tail Cone · corrodedCORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE TAIL CONE. ALL CORROSION WAS REMOVED BY BLENDING. THE REMAINING THICKNESSES WERE MAPPED AT EACH SITE USING ULTRASOUND. ACCOMPLISHED REPAIR DEFINITION S-750-0055 25RD, MAJOR REPAIR, REPAIR OF BAGGAGE DOOR & TAISDR DXTA2016032306210Skin · corrodedCORROSION WAS FOUND AT FOUR LOCATIONS ON THE TAIL CONE UPPER SKIN, AROUND THE PERIPHERY OF THE DORSAL FAIRING. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESSES WERE MAPPED AT EACH SITE USING ULTRASOUND. ACCOMPLISHED REPAIR DEFINITION SDR SWAA2016040450573Support · crackedWING TO BODY FAIRING SUPPORT STRUCTURE CHORD CRACKED AT BS 500D, BETWEEN STRINGER 18R - 19R. REPAIRED CHORD IAW SRM.SDR DALA2016032102289Cable · missingTAILCONE JETTISON BOTTLE CABLE MISSING ON VALVE HEAD. R & R BOTTLE IAW MM.SDR SWAA2016032850226Fairing · delaminatedFUSELAGE FAIRING 193B OUTER SURFACE DELAMINATED. REPAIRED FAIRING IAW EA.SDR 2016F00086Radome · misrepairedDURING THE PRELIMINARY INSPECTION, PREVIOUS REPAIRS WERE IDENTIFIED AS NOT COMPLIANT WITH THE CMM 53-15-11. THE FOLLOWING ANOMALIES HAVE BEEN IDENTIFIED: PREVIOUS REPAIR ON ALMOST ALL THE SANDWICH AREA IS AWAY FROM 20 TO 60 MM OF THE MONOLITHIC AREA WITHOUT OSDR DALA2016031502271Tail Cone · dentedDURING CHECK, FOUND DENT IN TAILCONE. REMOVED EXSISTING REPAIR AND INSTALLED NEW REPAIR IAW SRM 53-00-01, REPAIR 14.SDR V0XD201603014059Channel · crackedANGLE CRACKED ON AFT FUSELAGE FAIRING STRAP C CHANNEL. R & R AFT FUSELAGE FAIRING STRAP ANGLE C CHANNEL. PERFORMED MODSUM IS670538200021 REV C DATED 06 08 05 & SRM 51-21-11, 51-25-16, 51-25-06, 51-24-36, 51-40-11, 51-42-13 & 51-41-02.SDR 2016F00082Radome · misrepairedSEVERAL PREVIOUS REPAIRS IDENTIFIED DURING PRELIMINARY INSPECTION ARE NOT IAW CURRENT CMM 53-15-11, REV 31 MAY 2011: A PREVIOUS REPAIR N-1 WAS PERFORMED ON ALL SURFACE OF THE SHELL. THE HONEYCOMB WAS REPLACED IN AN AREA THAT IS 400MM AWAY FROM THE MONOLITHIC SDR REXA2016031300427Fairing · chafedAFTER REMOVAL OF ATTACH BRACKET FROM RT STUB FAIRING ON NR 4429263, FOUND RT STUB FAIRING TO CHAFED AT BRACKET ATTACH POINT. RECEIVED NEW RT STUB FAIRING PART 601R31199-92. INSTALLED ON 4428521, WO 1012596 000 0074.SDR SIMA20160311002Panel Support · crackedRT WING FUSELAGE LATERAL FAIRING, UPPER SUPPORT CRACKED AT FS 16783.5, 6.25" LENGTH. INSTALLED NEW OVERWING LATERAL UPPER PANEL SUPPORT IAW SRM 51-40-02.SDR CWQR20160311012Stringer · crackedDURING A SCHEDULED INSPECTION WE FOUND STRINGER 15L, CRACKED IN THE TAIL CONE SECTION OF THE ACFT. THE CRACK WAS AT THE AFT EDGE OF THE STRINGER WHERE THE BULB PORTION OF THE EXTRUDED STRINGER STOPS & THE STRINGER IS TAPER CUT BEFORE TERMINATING. A REPORT HASDR REXA2016030900407Angle · crackedAFT BELLY FAIRING PANEL 195DL, SPLICE ANGLE IS CRACKED. REMOVED CRACKED ANGLE, RECEIVED NEW ANGLE PN CC690-39251-1. PERFORMED EO R53573 REVISION 1, REVISION DATE 29 JAN 16.SDR DALA2016030801755Lanyard · tornMAINTENANCE FOUND YELLOW KEVLAR CORD TORN DURING THE TAILCONE KEVLAR CABLE INSPECTION. THE CABLE WAS REPLACED.SDR SWAA2016032950376Angle · crackedWING TO BODY FAIRING ANGLE CRACKED AT BS 540, RBL 41. R & R ANGLE IAW SRM & DWG.SDR V0XD20160229044Channel · crackedAFT FUSELAGE TO WING FAIRING, PANEL 195DL, CTR JOINT SUPPORT ANGLE IS CRACKED. R & R CHANNEL ON JOINT STRAP IAW SRM 51-42-06, 51-40-11.SDR DALA2016022801519Lanyard · misroutedMAINTENANCE FOUND THE TAILCONE RELEASE LANYARD ROUTED INCORRECTLY. THE TAILCONE RELEASE LANYARD WAS PROPERLY ROUTED. A FUNCTIONAL CHECK OF THE RELEASE SYSTEM WAS CONDUCTED AND CHECKED.SDR REXA2016022400306Fairing · gougedRIGHT STUB FAIRING HAS GOUGE MEASURING .015" DEEP. RECEIVED NEW SERVICEABLE STUB FAIRING ASSEMBLY PN 601R31199-92. INSTALLED SEAL ONTO STUB FAIRING IAW SRM 51-42-15. REF MWC JOB 8788610 OP 507 FOR INSTALL OF STUB FAIRING.SDR SWAA2016030249589Fairing · corrodedLOWER WING TO BODY FAIRING STRUCTURE CORRODED, BETWEEN BS 652 - 674, LBL 27. R & R FAIRING STRUCTURE IAW DWG.SDR SWAA2016030249590Fairing · corrodedLOWER WING TO BODY FAIRING STRUCTURE CORRODED, BETWEEN BS 652 - 674, RBL 27. R & R STRUCTURE IAW DWG.SDR REXA2016021900272Channel · cracked196 DR FUSELAGE FAIRING ATTACHING CHANNEL, PN CC 690-39251-1, IS CRACKED. R & R CRACKED CHANNEL, CC670-39251-1, IAW SRM 51-42-13-001-001-A01 & EO R53573.SDR DALA2016022201275Attach Bracket · crackedRT WING FIXED L/E WING ROOT INBD SIDE WING TO BODY FAIRING MOUNT STRUCTURE ATTACH BRACKET CRACKED. REPLACED RT WING ROOT FIXED L/E WING TO BODY FAIRING MOUNT ATTACH BRACKET IAW SRM 51-42-02, PG 1-11 AND DWG 5919110 SH5.SDR DALA2016022101278Lock Pin · wornTAILCONE RELEASE LOCK PIN AND RECEPTICAL WORN, LEFT UPPER. REPLACED THE LT UPPER TAILCONE LOCKPINE AND RECEPTICAL IAW MM. OPS CHECK OK.SDR DALA2016021701173Latch · wornTAILCONE LATCH SPADE WORN AT 8 O'CLOCK POSITION. REPLACED SPADE IAW MM.SDR DALA2016021701172Latch · wornTAILCONE LATCH SPADE WORN AT 1O'CLOCK POSITION. REPLACED SPADE IAW MM.SDR DALA2016021701171Latch · wornTAILCONE LATCH SPADE WORN AT 4 O'CLOCK POSITION. REPLACED SPADE IAW MM 535-52-01.SDR REXA2016021200281Support Angle · crackedRIGHT SIDE ACCESS FAIRING SUPPORT ANGLES AT FS 461.5, 469.63 & 476.67 ON TOP OF WING ARE CRACKED, 3 EACH. R & R RT SIDE ACCESS FAIRING SUPPORT ANGLES IAW SRM 51-42-06, 51-42-21 & 51-40-11.SDR DALA2016021201024Latch · misinstalledTAILCONE DOOR COVER LATCH, LEFT SIDE, DOES NOT OPERATE NORMALLY. IT APPEARS TO BE MOUNTED BACKWARDS. MAINTENANCE REINSTALLED QTR TURN LATCH FOR THE COVER OF THE AFT CABIN DOOR EMERGENCY OPERATING HANDLE, REF AMM 52-52.SDR SWAA2016030749701Skin · delaminatedTAIL CONE EXTERNAL SKIN DELAMINATED AT TAIL CONE. REPAIRED SKIN IAW SRM.SDR DALA2016021100980Handle · misinstalledMAINTENANCE FOUND THE TAILCONE EXTERNAL RELEASE HANDLE IMPROPERLY INSTALLED. CABLE WAS REINSTALLED PROPERLY IAW AMM 53-53-00-501.SDR DALA2016021000961Cable · wornMAINTENANCE FOUND A TAILCONE CABLE WORN AT THE LOOP END. THE CABLE WAS REPLACED IAW AMM 53-53.SDR DALA2016021000960Cable · obstructedMAINTENANCE FOUND THE TAILCONE FRAME INTERFERING WITH A RELEASE CAM. THE TAILCONE RING WAS ROUTED AND A DOUBLER WAS INSTALLED IAW DWG 991157.SDR V0XD20160207015Bracket · crackedAFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE, LT BRACKET CRACKED FS 939.00. R & R LT ANGLE, PN SH670-39189-1, IAW SRM 51-42-06, 51-45-00 & 51-25-16.SDR DALA2016020400944Gauge · inoperativeTAIL CONE NITROGEN BOTTLE PRESSURE GAUGE NOT INDICATING PRESSURE. R & R BOTTLE.SDR DXTA2016012306168Fan · failedWHILE SITTING IN COCKPIT PRIOR TO ENGINE START, HEARD AN AUDIBLE POP WITH SIMULTANEOUS INDICATIONS OF THE RADOME FAN CAUTION LIGHT, FLASHING MASTER CAUTION, BOTH PFDS, MFD & FMS WENT BLANK BUT WERE BACK LIT. 45 SECONDS LATER A LOUD BUZZING NOISE CAME ACROSS SDR DALA2016012500566Structure · crackedMAINTENANCE FOUND 4 CRACKS EMINATING FROM THE 5:00 POSITION TAILCONE ALIGNMENT PIN HOLE. A REPAIR WAS INSTALLED IAW ER/A 497316-14MA, REV ORIG.SDR REXA2016011600039Channel · crackedACCESS PANEL 195DL HAS ONE EACH ANGLE & STIFFENER CRACKED. REPAIRED ACCESS PANEL 195DL BY REMOVING & REPLACING FAIRING C CHANNEL, PN CC690-39251-1, IAW SRM 51-42-13-001-001-A01, 51-40-11-001-001-A01 & INCORPORATE IS670538200021 IAW EO R53572. REMOVED ORANGE SDR V0XD20160117348Attach Bracket · crackedCRACK IN ATTACH BRACKET ON AFT WING TO BODY FAIRING STRUCTURE AT FS 909.00. REPAIRED CRACK BY CUTTING OUT DAMAGE. FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-53-82-478 REV A DATED 2014 11 12.SDR SIMA20160112010Support · crackedRIGHT WING TO FUSELAGE FAIRING, UPPER SUPPORT CRACKED. REPAIRED IAW SRM 53-23-12.SDR SIMA20160112011Attach Angle · crackedRIGHT WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE NR 4 CRACKED AT THE AFT END. INSTALLED NEW SECTION ANGLE IAW ETN-EM-53-142 & SRM 51-40-02.SDR SIMA20160112009Support · crackedRIGHT WING TO FUSELAGE PANEL, LOWER FWD SUPPORT CRACKED. COMPLETED REPAIR IAW ETN-EM-53-142 R2. SEE NRTC E488775 FOR LEAK CHECK.
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