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 MALA070107Panel · debondedDURING N4K CHECK IN CWA, FOUND 6 DENTS ON CENTER BELLY WING FUSELAGE PANEL DISBONDED. REPAIRED IAW EO NR S51031 AND SRM 51-70-50.SDR UPS07M51049Bracket · crackedINSPECTION TYPE:C EMP - FWD TAIL CONE, RIGHT UPPER ALIGNMENT PIN MOUNTING BRACKET CRACKED. EMP FWD TAIL CONE AFT FUSE FIXED FAIRING 317AR REMOVED PER AMM20-50-02 R.50. EMP FWD TAIL CONE RIGHT UPPER ALIGNMENT PIN MOUNTING CRACKED AREA CUT OFF PER EN 1600-07. SDR 2007UALA02994Radome · contaminatedFLIGHT DIVERTED DUE TO INOPERABLE WEATHER RADAR. UNRELIABLE WEATHER RADAR CELLS. RADOME FAILED MOISTURE TEST, REPLACED RADOME WEATHER RADAR.SDR TRAX200701012Drag Angle · crackedRHS VERT STAB AND FUSELAGE ATTACHMENT ANGLE CRACKED ON T/E, ABOVE THE FWD OF TAIL CONE. REMOVED AND REPLACED RS VERT STAB DRAG ANGLE PER REO 670-55-31-018SDR TRAX200701011Drag Angle · crackedLT VERT STAB AND FUSELAGE ATTACHMENT ANGLE CRACKED ON T/E, ABOVE THE FWD OF TAIL CONE. REMOVED AND REPLACED LT VERT STAB DRAG ANGLE IAW REO 670-55-31-018SDR UIEA200700266Fairing · puncturedLOWER BODY FAIRING PANELS 194C AND 194B HAVE A PUNCTURED HOLE. PANEL 194B AREA OF PUNCTURE IS 2.750 BY .750 INCHES AND 194C IS 1.250 BY .750 INCHES. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-09 FIG 11 AND 747-200 SRM 51-40-12. ALSO, REF: ATSDR TRAX200700937Cover · missingRIGHT ENG MISSING INSPECTION COVER ON TOP LEFT SIDE OF TAIL CONE. FLTS 4672, 4713 CX.SDR UPS07450189Skin · dentedINSPECTION TYPE:C EMP RIGHT TAIL CONE SKIN SURFACE FOUND A DENT MARK AT STA 2755 BETWEEN 17R & 18R. EMP RIGHT TAIL CONE SKIN BS 2750 TO 2762 STR 17R - 18R AREA REPAIRED AS PER SRM 53-30-03 FIG 1A.SDR ZZDA2007206Strap · corrodedSTRAP ON FAIRING SUPPORT STA 851 RT SIDE CORRODED. INSTALLED STRAP ON FAIRING SUPPORT STA 851 RT SIDE IAW B717 SRM 51-41-02. MATERIAL USED 7075-T6 100" SIZE 6'.3" X 2".SDR VNAA0706003Radome · damagedCREW REPORTED A LIGHTNING STRIKE WHILE IN FLIGHT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE RADOME IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 53-81-01-400SDR QXEA200700945Panel · corrodedC4 PDX - SURFACE CORROSION AT AFT OUTBOARD CORNER OF APERTURE FOR PANEL 144JZ STATION X783. REPAIRED IAW SRM 51-14-00.SDR FDKA200705246Latch · crackedRADOME LATCH HOUSINGS ARE CRACKED. THE DAMAGED PARTS HAVE BEEN REMOVED AND REPLACED.SDR ASAA0741694Stringer Clip · corrodedAFT CARGO PIT CLIP CORRODED. REPLACED WITH MADE REPAIR PART IAW SRM 51-40-02.SDR UPS07549796Radome · failedPILOT REPORT - DURING CLIMB HEARD SINGLE THUMP ON LOWER RIGHT SIDE OF NOSE OF A/C. RADOME SUSTAINED STRUCTURAL FAILURE. [SUP 05-18-07] R & R NOSE RADOME IAW AMM 53-12-01-4 AND PERFORMED WEATHER RADAR TEST. ALL CHECKS NORMAL.SDR FDKA200705237Flange · crackedTAIL CONE FAIRING DOOR, 313CL, INNER FLANGE IS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER TO REPAIR THE DAMAGE.SDR SIMA200712702Radome · erodedCONTINUOUS NOISE FROM FRONT OF AIRCRAFT NOSE, VIBRATION NOTED, POST FLIGHT INSPECTION REVEALED RADOME EROSION TAPE DELAMINATED. REMOVED AND REPLACED EROSION TAPE IAW AMERICAN EAGLE PROCEDURES. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. RETURNESDR 07FDEA01691Hinge Fitting · crackedTAIL CONE COMPARTMENT, LT HINGE FITTING FOUND CRACKED, VIEWED FROM AFT ACCESSORY COMPARTMENT. [SUP 05-14-07] REMOVED & REPLACED AS PER DAC DWG AJC7346 AND SRM 51-31-01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 2007UALA01340Tail Cone · puncturedTAIL CONE 18 INCH PUNCTURE AT STA 1898. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: MANUFACTURED & INSTALLED STRUCTURAL FILLERS AND DOUBLER REPAIR.SDR VNAA0704012Radome · damagedCREW REPORTED A LIGHTNING STRIKE TO THE AIRCRAFT NOSE ON DESCENT. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. AIRCRAFT WAS FERRIED TO DAYTON FOR REPAIR. MAINTENANCE INSPECTED AND REPAIRED ALL DAMAGE. MAINTENANCE ALSO REMOVED AND REPLACED SDR VNAA0704008Radome · damagedCREW REPORTED A LIGHTNING STRIKE ON DESCENT. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTION. AIRCRAFT WAS FERRIED TO DAYTON FOR REPAIR. MAINTENANCE INSPECTED AND REPAIRED ALL DAMAGE. MAINTENANCE ALSO REPLACED THE RADOME INSDR UIEA200700200Keelbeam · corrodedKEEL BEAM PNL NR 191KK EXTERNAL AND INTERIOR SURFACE CORROSION REVEALED. KEEL BEAM PANEL NR 191KK OUT OF LIMIT HINGE AREA REPAIRED AS PER SRM 51-40-03 FIG 1 AND SKIN REPAIRED AS PER SRM 51-40-02 FIG 1.SDR 07FDEA01442Fairing · crackedCRACK FOUND ON NR 1 PYLON LOWER FAIRING. REPAIR ON GOING AS SRM REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.SDR 07FDEA01433Fairing · crackedFAIRING PANEL TO PYLON COWL OF RT CORE WITH 2 CRACKS REPAIRED THE CRACKS IAW SRM 54-56-10 CONFIG. 2 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MINOR.SDR UPS07549609Radome · damagedINSPECTION TYPE:N/A RADOME HAS SEVERAL NICKS & GOUGES, POSSIBLE DELAMINATION. INSPECTED PER SRM 53-10-72-1A. DAMAGE IS OUT OF LIMITS. RADOME UNLOCKED. UPON FURTHER INSPECTION DAMAGE WAS TO THE SURFACE COATING AND BOOT. REPAIRED BOOT AND APPLIED SURFACE COSDR UPS07549669Tail Cone · damagedINSPECTION TYPE:C HOLE IN TAILCONE STA 1893 LBL 8. COMPLIED WITH EA NR 757-5381-27-A1656. NO DEVIATIONS AND UPS RAA NR 757-53-20242.SDR 2007UALA01046Seal · damagedNOTICEABLE HI FREQUENCY LO AMPLITUDE VIBRATION DURING CLIMB. REPLACED BLADE SEAL AND RESEALED BODY WING FAIRING.SDR TAMF20070002SWeb · crackedDURING INSPECTION CHECK WAS FOUND A CRACK AT AFT WING FAIRING WEB STA 1080 BL 62-70-LT. DAMAGED AREA WAS REPAIRED IAW EWO 767 53-035 AND MFG SERVICE REQUEST 1-311853573. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.SDR QXEA200700553Radome · damagedC3 OKC - NOSE RADOME HAS EVIDENCE OF LIGHTNING STRIKE BURN THROUGH WITH DISBONDING ON INTERNAL SURFACE. REPAIRED IAW SRM 53-81-80.SDR MALA070048Skin · puncturedAIRCRAFT WAS STRUCK BY A MANLIFT IN MSP CAUSING A PUNCTURE IN THE AFT LT TAIL CONE SKIN AT STATION 825. PERMANENT REPAIR COMPLETED IAW MAL EO#S53418.SDR 07FDEA01129Fairing · damagedREPAIR DAMAGE TO FAIRING 577EL REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW EA 6-5317-106416 AND RAS/DAHAM/4021689/2007 ISS.ASDR 07FDEA01089Doubler · corrodedSEVERAL AREAS OF CORROSION ON C95, ON INTERNAL DOUBLER BETWEEN C94-C95, P14-P16 LT AND ON EXTERNAL SKIN BETWEEN C95-C96, P15 LT ON FUSELAGE TAIL CONE, LISTED IN DR 0534-01-16-0200. REPAIR PERFORMED BY BLEND OUT, REPLACEMENT, CUT OUT WITH EXTERNAL AND INTERNALSDR TAMF20070001SFairing · crackedDURING INSPECTION, FOUND A CRACK AT AFT WING FAIRING WEB STA 1080, BL 62-70, LT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-303353670 AND EWO 767-53-031. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.SDR FDKA200703143Panel · crackedUPPER FLANGE FOR FUSELAGE OVERWING PANEL NR 194 IS CRACKED. THE DAMAGE HAS BEEN REPAIRED.SDR UPS07M49793Frame · damagedINSPECTION TYPE:C TAIL CONE ACCESS CUTOUT AFT FRAME DAMAGED AS MARKED. DAMAGED AREA ON BEAM, CHANNEL REMOVE. FOUND BEYOND LIMIT. MAT'L THK 0.04 0"X0.063" THK REMAIN 0.027"X0.040" THK REMOVED 0.013"X0.023" SRM 53-00-01VIR R38. DAMAGED BEAM, CHANNEL REMOVED SDR UPS07M49780Frame · scratchedINSPECTION TYPE:C TAIL CONE RIGHT ABOVE FLOOR PANEL FRAME SCRATCH AS MARKED. SCRATCH MARK REMOVED, FOUND BEYOND LIMIT. MATL THK 0.040" THK REMN 0.07", THK REMV 0.013" PER SRM 53-00-01VIR38. DAMAGED SUPPORT REMOVED PER SRM 51-35-01VIIR38. NEW SUPPORT FAB USSDR UPS07M49778Skin · chafedINSPECTION TYPE:C FWD TAIL CONE RIGHT RETRACTABLE DOOR INTERIOR FWD SECT REAR OF SAFETY BARRIER STOWAGE ANGLE SKIN CHAFED AS MARKED. CHAFED AREA REMOVED FOUND EXCEED LIMIT MATL THK 0.020" THK REMAIN 0.000" THK REMOVED 0.020" AREA 2" X 1" PER SRM 53-00-01VIR38SDR UPS07M49770Support Angle · dentedINSPECTION TYPE:C TAIL CONE ACCESS PANEL SUPPORT ANGLE RIGHT DENTED. SUPPORT DENTED AREA SMOOTHED & MEASURED D/Y 0.75"X0.040"=18.75 BEYOND LIMIT SRM 51-80-01VIIR38. SUPPORT ANGLE FAB BOEING DWG AKC7546. HEAT TREAT PER DPS 7.00-1 & HARDNESS VALUE HRB 58.5 PESDR UPS07M49678Structure · dentedINSPECTION TYPE:C FWD TAIL CONE: LT RETRACTABLE DOOR EXTERIOR FIN FOUND DENT AS MARKED NR 6660. DENT AREA FOUND BEYOND LIMIT PER SRM 51-81-01 VOLIR38. DAMAGED AREA TRIMMED PER SRM 52-00-01VOLIR38. HFEC INSP C/OUT PER DAC NDTSPM REV13 06-10 -01.001. FOUND NSDR MWEA070045Release Mech · failedTAIL CONE FAILED TO DROP WHEN USING AFT PRESSURE BULKHEAD DOOR PULL PER TASK 53-52-00-03. CLEANED AND ADJUSTED RELEASE CLIPS IN AFT ACCESSORY COMPARTMENT.SDR CA070320010Radome · burned(CAN) DURING CRUISE AIRCRAFT STRUCK BY LIGHTENING. MAINTENANCE INSPECTION FOUND SCORCH MARKS ON RADOME, ALONG CENTER EDGES OF NLG DOORS, AND ALONG FORWARD FUSELAGE UP TO WING ROOT FAIRINGS. ALSO MINOR BURN MARK ON RT WINGLET TIP. NO DAMAGE TO ANY STATIC DISCHASDR 2007FA0000264Fairing · departedON MARCH 6, 2007, DURING A FLIGHT, THE SUBJECT AIRCRAFT EXPERIENCED AN IAPPARENT IN-FLIGHT STRUCTURAL FAILURE OF THE RIGHT WING-TO FUSELAGE FORWARD FAIRING. THE INCIDENT OCCURRED AT FLIGHT LEVEL 400 AT 90 DME ON THE (LNK) VOR 220 RADIAL AT .85 MACH. AFTER ONSDR MWEA070041Latch · brokenAFT TAIL CONE DOOR ARMING, DISARMING GUARD WILL NOT REMAIN DOWN AND LOCKED ON PLACE. REMOVED AND REPLACED LATCH.SDR MWEA070040Release Mech · out of adjustTAIL CONE DID NOT DEPLOY WHEN THE AFT PRESSURE BULKHEAD DOOR TEST WAS PERFORMED. CLEANED AND ADJUSTED RELEASE CLIP.SDR IXXA07SMN107SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND TAIL CONE LOWER SKIN CORRODED STATION XFS 1813.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMEDSDR SIMA200704403Clamp · out of adjustNOSE VIBRIBATION IN FLIGHT. READJUSTED RADOME ATTACHMENT CLAMPS, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE.SDR DHL2007802532Fillet · delaminatedFOUND FUSELAGE LWR FILLET PANEL NR 732 DELAMINATED (STA 990.000 - 1050.000). REMOVED AND REPLACED LWR FILLET PANEL NR 732 IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).SDR COMA0760103Fairing · looseFLIGHT 7451 - AFTER TAKEOFF FROM CVG A LOUD RUMBLING NOISE WAS EMANATING FROM UNDER THE FLOOR AREA, FLIGHT RETURNED TO CVG FOR INVESTIGATION. RESEALED THE BELLY FAIRINGS.SDR ZZDA070123123Radome · dentedAIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. RADOME ASSEMBLY DENTED. REPLACED RADOME ASSEMBLY PER 717 AMM CHAPTER 53-51-01 REV 27 DATED 01/01/07.SDR ZZDA070123100Radome · crackedAIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. RIGHT AND LEFT RADOME LATCH ASSEMBLIES AND FORWARD LOWER SKIN CRACKED AND BROKEN BEYOND REPAIR. REPLACED RIGHT AND LEFT RADOME LATCH ASSEMBLIES AND FORWARD LOWER SKIN AT STA 37.0 PER MDC DRAWING 5911400 REV CM DSDR ASMF200701005Fairing · damagedAIRCRAFT WAS HIT IN THE RT LOWER WING BY A BAGGAGE CONVEYOR, CAUSING A DAMAGE OF 2 X 2 INCHES WITH .3125 INCH DEPTH IN THE MLG FAIRING. DUE, IT WAS A NON PRESSURIZED AREA, HI-SPEED TAPE WAS INSTALLED IAW MGMYPTA 10-24-1 AND AIRCRAFT WAS DISPATCHED. DURING OVE
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