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 FDEA200911234112Angle · corrodedRT WING-TO-BODY FAIRING, RT PACK AIR INLET DOOR (BOTTOM) HAS 33 SMALL CORRODED RIVET HEADS AND ANGLE EXFOLIATING AT STA 860 TO STA 900, RBL 20. EVALUATE AND RECTIFY. STA 860, RBL 20, CORRODED ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. ANGLE FASDR FDEA200911204090Frame · corrodedRT LWR FUSELAGE WING TO BODY FAIRING FRAME FS 900 CORRODED WITH CORRODED FASTENERS. REMOVED CORROSION WING TO BODY FRAME STA. 900 FOUND OUT OF LIMITS IAW SRM 53-00-71 DET. 7 REPLACED FRAME, DRILLED AND INSTALLED IAW SRM 51-40-02 THIS IS A MAJOR "A" REPAIR NO SDR QXEA2009111600957Strap · corrodedSTRAP CORRODED FOR AFT FAIRINGS 195DL AND 196DR. REPLACED STRAP WITH SERVICEABLE STRAP.SDR FDEA200911023766Strap · corrodedRT WING-TO-BODY FAIRING, RT PACK AIR INLET DOOR PANEL "BOTTOM" HAS ONE LOOSE FASTENER AT BS 875.25, RBL 25 AND FOUR CORRODED PLATES FOR NUTPLATES. REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-40-02 REV. 98. PARTS FABRICATED AND PART MARK AS PER DRAWING 149NSDR WRLA20091101301Fitting · crackedCRACK - ONE CLIP CRACKED ABOUT 1 INCH Y=1341, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY=1. FABRICATED PART IAW EGAT EI W2009P53B-1375 REV 00. INSTALLED WITH NEW PARTS IAW MD11 SRM 51-33-01.SDR WRLA20091101300Fitting · crackedCRACK- ONE CLIP CRACKED ABOUT .5 INCH, Y=1401, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY =1. REPLACED WITH NEW CLIP IAW MD11 SRM 51-35-01 FIG 2 AND SRM 51-33-01 FIG 2 REV 41.SDR WRLA20091101298Bracket · damagedCRACK - BRACKET TAIL CONE WORK PLATFORM DOOR LOCK/UNLOCK SENSOR SUPPORT ATTACHED AFT FUSELAGE BULKHEAD AFT FACE, Y=2164, Z=73, LENGTH =.5 INCH. REPLACED DAMAGE BRACKET IAW MD11 SRM 51-33-01 REV 41.SDR WRLA20091101296Bracket · crackedCRACK - BRACKET OF TAIL CONE WORK PLATFORM LIGHT BOTH OF AFT FUSELAGE BULKHEAD ABOUT 1 INCH QTY = 2EA. REPLACED NEW BRACKET IAW MD11 SRM 51-35-01 REV 41.SDR WRLA20091101285Angle · crackedCRACK - ANGLE, C/T WING TO BODY FAIRING SUPPORT STRUCTURE STA Y=1361, RT FUSELAGE L=1". REPLACED WITH NEW ANGLE IAW MD-11 SRM 51-33-01 AND SRM 51-35-01 REV 41. COND CHECK NORMAL AND JOB COMPLETED.SDR WRLA20091101284Web · crackedCRACK - WEB, LT WING TO BODY FAIRING SUPPORT STRUCTURE, L=1.5", Y=1341. REPAIRED WEB CRACK AREA IAW MD11 SRM 53-00-00 FIG 204 REV 41.SDR VNAA2009102600009Radome · damagedCREW REPORTED A BIRD STRIKE IN DCA. MAINTENANCE INSPECTED PER THE AIRCRAFT MAINTENANCE MANUAL. THE RADOME WAS REMOVED AND REPLACED AND CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.SDR DLM88091603Lever · wornDURING HMV WEAR WAS FOUND ON LEVER OF TAIL CONE UPPER RT LATCH. LEVER OF TAIL CONE RT UPPER LATCH WAS REPLACED IAW CMM 53-50-01.SDR DLM88091600Clamp · wornDURING HMV WORN CLAMPS WERE FOUND FOR TAIL CONE RELEASE CABLE STA 1510. CLAMPS WERE REPLACED IAW AMM 20-30-01-201.SDR DLM88091599Pin · wornDURING HMV A WORN PIN OF TAIL CONE INTERNAL RELEASE MECHANISM WAS FOUND. PIN WAS REPLACED IAW AMM 20-30-01-201.SDR DLM88091597Latch · corrodedDURING HMV CORROSION WAS FOUND ON HOUSING OF LATCH ASSY TO ATTACH TAIL CONE STA Y=1510 7 HRS POSITION. LATCH PIN WAS REPLACED IAW AMM 53-53-00-501.SDR ASAA0976705Support · corrodedFRETTING ON LOWER WING TO BODY FAIRING SUPPORT FRAME BS 727 BL 0 RBL 20. REMOVED AND REPLACED WITH FABRICATED SUPPORT FRAME.SDR WRLA20090924252Support · corrodedEXFOLIATION - LOWER FUSELAGE FS 987.5, LBL 9 TO RBL 9 THE T-SUPPORT OF FAIRING EXFOLIATED. REPLACED THE EXFOLIATED FAIRING SUPPORT WITH NEW PARTS PER WOA 747-400 SRM 51-40-02 REV 73.SDR SIMA200926603SUPFairing · crackedDURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT OVERWING FAIRING 172CR CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED RIGHT OVERWING FAIRING 172CR IAW CRJ 700 ETA CR-5300-088. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200926604SUPFairing · crackedDURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OVERWING FAIRING 172CL CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED LEFT OVERWING FAIRING 171CL IAW CRJ 700 ETA CR-5300-088. RESTORED PROTECTIVE FINISH IAW SRM 51-25-01, 51-25-06 AND ETN GN-51-002R3. AISDR SIMA200926604Fairing · crackedDURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OVERWING FAIRING 172CL CRACKED. AIRCRAFT REMOVED FROM SERVICE.SDR SIMA200926603Fairing · crackedDURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT OVERWING FAIRING 172CR CRACKED. AIRCRAFT REMOVED FROM SERVICE.SDR WRLA20090921207Support · crackedCRACK - FOUND LONGERON BOX SKIN CRACK OF LT BODY FAIRING PANEL AT LT STA 1372 WL 128. REMOVED THE LT WING I/B FORE FLAP RUBBER STRIPE AND FAIRING PANEL 293JL REF TO JOB CARD ATTACHING SHEET 074003 ITEM 01, 02 & 03. REMOVED LT LONGERON BOX SKIN PER WOA 747-40SDR WRLA20090921206Support · crackedCRACK - FOUND LONGERON BOX SKIN CRACK OF RT BODY FAIRING PANEL AT RT STA 1372 WL 128. REMOVED THE RT WING I/B FORE FLAP RUBBER STRIPE AND FAIRING PANEL 294JR REF TO JOB CARD ATTACHING SHEET 074002 ITEM 01, 02 & 03. REMOVED RT LONGERON BOX SKIN PER WOA 747-40SDR ASAA0946593Support · damagedELONGATED HOLE IN AFT FAIRING SUPPORT LEFT SIDE. REPLACED ATTACHED SUPPORT.SDR 2009F00079Panel · corrodedCORROSION ON RT LWR LOBE AFT PANEL.SDR ASAA0976525Support · chafedFAIRING SUPPORT STRUCTURE TEE CHORD CHAFED ON LWR SURFACE. REMOVED AND REPLACED TEE CHORD.SDR ASAA0996584Tail Cone · dentedLEFT SIDE OF TAIL CONE DENTED. REPAIRED DENT ON LT OF TAIL CONE.SDR HVUA001Arm · shearedDURING ROUTINE INSP, FOUND (2) OF THE (3) BOLTS SECURING NOSE GEAR STEERING ARM SHEARED OFF. THE AN6H-40 WAS SECURING THE ARM ALONG WITH ONE AN3H5A. MFG ON LATER SN USED AN4H BOLTS RATHER THEN AN3H BOLTS. OVER STEER CAM WAS SEIZED TOGETHER. THE STEERING ARM (SDR FDEA200908313196Frame · corrodedLT FWD WING-TO-BODY FAIRING SPLICE FRAME BETWEEN BS 800 TO BS 820, BL 0 HAS EXFOLIATION CORROSION. EVALUATE AND RECTIFY. LT FWD WING TO BODY FAIRING SPLICE FRAME AT BS 800 TO BS 820, BL 0, UPPER INTERCOSTAL FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 9SDR VNAA2009082400005Radome · damagedCREW REPORTED A LIGHTNING STRIKE IN VPS. MAINTENANCE INSPECTED THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED THE RADOME AND STATIC WICKS. THE SRM AND REO’S WERE USED TO REPAIR RIVETS. OTHER CHECKS WERE MADE PER THE AISDR CALA2009082400471Skin · dentedDENT ON APU TAIL CONE AREA AT STA 1920, 11 O`CLOCK POSITION. DIMENSIONS ARE .130 INCH DEEP 3 X 2.25 INCH FX STA 1913 TO STA 1920 BETWEEN STR 0-STR 12AL. SKIN REPAIRED PER SRM 53-00-01 FIG 201, REPAIR 14 AND HFEC NO CRACK FOUND.SDR FDEA200908173029Support Angle · corrodedRT WING-TO-BODY FAIRING INTERCOSTAL SUPPORT ANGLE TO FAIRING HAS CORROSION AT STA 900, RBL 19.0 INCH. CORROSION ON INTERCOSTAL CLIP FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED INTERCOSTAL CLIP IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSISDR VNAA2009080300007Radome · damagedCREW REPORTED A POSSIBLE LIGHTNING STRIKE AFTER ARRIVAL CLT. MAINTENANCE INSPECTED PER THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED THE RADOME AND STATIC WICKS. OPERATION CHECKS PER AIRCRAFT MANUAL WERE ACCOMPLISHED. AIRCRAFT RELEASED SDR 2009FA0000750Seal · mismanufacturedON DEPARTURE, THE RT WING FUSELAGE FAIRING TO WING SEAL STRIP CAME LOOSE, CAUSING THE STRIP TO LIFT UP AND BEAT AGAINST THE WIND FAIRING CREATING A VERY LOUD NOISE IN THE CABIN AND SOME VIBRATION. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCISDR VNAA2009072800005Radome · damagedON PRE FLIGHT INSPECTION CREW REPORTED A LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT IN OAJ. MAINTENANCE INSPECTED AND REPLACED STATIC DISCHARGERS AND RADOME. ALL WORK WAS DONE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.SDR FDEA200907172651Frame · corrodedLT CHORD ON FAIRING STRUCTURE FROM STA 1120 TO STA 1138, LBL 8.0" HAS CORROSION. CORROSION FOUND EXCEEDED SRM REPAIRABLE LIMITS ; LOWER CHORD REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA..SDR A6WA200940415Seal · looseON CLIMBOUT, NOTICED VIBRATION IN BOTH CONTROL COLUMNS AND AN ASSOCIATED LOW PITCH BUZZ. VIBRATION AND BUSS REMAINED CONSTANT REGARDLESS OF AIRSPEED PITCH OR CONTROL COLUMN MOVEMENT. FA REPORTED SIMILAR BUZZ AND VIBRATION IN PASSENGER CABIN. VIBRATION AND BSDR QXEA2009071300531Radome · not bondedFLIGHT 2302, CONTINUOUS LOUD SQUEAL ON COMM 1 AND 2 WHILE IN THE CLOUDS, UNABLE TO HEAR CENTER FOR 25 MIN. DIVERTED TO GEG AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED STATIC WICKS AND BONDING JUMPERS, NO DEFECTS NOTED. FOUND INSUFFICIENT BONDING BETWEENSDR UALA2009071302021Radome · dentedFOUND DENT AT 10 O'CLOCK POSITION AT 18 INCHES FROM RADOME AFT EDGE. AREA COVERED WITH TAPE. INSPECTED RADOME. DENT IS WITHIN LIMITS. REPLACED RADOME.SDR IPXA09556736Filler · crackedINSPECTION TYPE: C2 FAIRING SUPPORT STUCTURE HAS CRACK AT FASTENER HOLE BS1020 UNDER PNL NR 191DL. REPLACED FILLER IAW SRM 51-40-02.SDR DLM88091108Rod End · corrodedDURING HMV4 CORROSION WAS FOUND ON ROD ENDS OF TAILCONE RELEASE MECHANISM STA 1510 CANT. SURFACE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3SDR FDEA200907032474Structure · corrodedWING-TO-BODY FAIRING LOWER CHORD AT STA 900 HAS INTERGRANULAR CORROSION FROM RBL 33 TO LBL 22. CORROSION FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR CA090821008Skin · wornDURING ELEVATOR TAB CONTROL SYS RIGGING, MX FOUND ELEVATOR TRIM TAB CONTROL CABLES RUBBING ON FUSELAGE TAILCONE SKIN AT CUT OUT HOLES. TRIM CABLES, PULLEYS AND CABLE RUNS WERE INSPECTED AND FOUND CORRECT, NO DAMAGE OR DEFECTS. ENGINEERING WAS ADVISED AND ISSUESDR UALA2009062901860Panel · delaminatedWING TO BODY PANEL AFT OF THE LT BODY GEAR HAS DELAMINATION ROUGHLY 3FT BY 1FT. REMOVED PANEL FOR REPAIR. SENT TO SHOP FOR REPAIR. PANEL FLAMED SPRAYED. PREPPING FOR PAINT REMOVE AND REPLACE. INSTALLED REPAIRED PANEL.SDR FDEA200906252288Support · corrodedWING-TO-BODY FAIRING SUPPORT FRAME (ENTIRE FRAME) HAS CORROSION AT STA 900. CORROSION ON SUPPORT FRAME AT STA 900 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 SDR FDEA200906252287Web · corrodedWING-TO-BODY LOWER FAIRING; VERTICAL WEB AT STA 860, RBL 3.0 NR TO LBL 3.0 NR HAS INTERGRANULAR CORROSION. CORROSION ON VERTICAL WEB OF WING-TO-BODY LOWER FAIRING STRUCTURE AT STA 860 FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. WEB REMOVED AND REPLACED IAW SRSDR FDEA200906242264Support Bracket · corrodedLT WING TOP WING TO BODY FAIRING SUPPORT BRACKET AT STA 940 WITH CORROSION. EVALUATE AND RECTIFY. RE-WORKS CORRODED AREA FOUND TO EXCEEDED ALLOWABLE LIMITS IAW SRM 51-00-71 REV. 97. MATERIALS REMOVED = 0.055 INCH, MATERIALS REMAINED = 0.025 INCH, MATERIALS SDR AXSA189WA6/17/09Fairing · departedAPPROX 20 MILES SOUTH, DURING DESCENT THE PILOT NOTED A LOUD NOISE AND THE ACFT SHUTTERED. ALL INSTUMENTS AND FLIGHT CONTROLS REMAINED NORMAL. THE PILOT SLOWED TO 160KTS AS A PRECAUTION AND LANDED WITHOUT INCIDENT. VISUAL INSP REVEALED THAT THE AFT AERODYNAMICSDR CA090618011Spring · damaged(CAN) AD 006-12-99 WAS CARRIED OUT IN 2000. NO FAULTS FOUND. NO REPEAT INSP REQUIRED IAW AD. REMOVED TAILCONE TO DO A GENERAL INTERNAL INSP. VISUAL SAW UPPER ANGLE , AND LOWER DIAPHRAGM CRACKED IAW THE AD SUGGESTS. REF SB 53-JA-990842 PARTS 2 AND 3. ORDERSDR A6WA200940303Drag Angle · damagedMWC 137953-7 - FOUR FWD MISALIGNED BOLT HOLES ON LT AND RT TAILCONE DRAG ANGLES. TRIMMED DRAG ANGLES, FABRICATED AND INSTALLED FILLERS AND REPAIR ANGLES IAW EO 601R-53-16986. (K)
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