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 UF6A990812Fairing · crackedLEFT VERTICAL FAIRING ATTACHMENT TO FUSELAGE IS CRACKED. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW ENGINEERING REPORT NR 99-153. (M)SDR TSAA9953404Skin · crackedFOUND 4.125 INCH CRACK 2 INCH FORWARD OF BS 947 AT STRINGER 24L. SKIN REPAIR IAW SRM 53-30-3 FIGURE 6 SHEET 4 PAGE 12B. AIRCRAFT RETURNED TO SERVICE. (M)SDR CALA9901041Release Mech · out of adjustTHE FORCE REQUIRED TO RELEASE TAILCONE USING BOTH THE INTERIOR TAILCONE RELEASE HANDLE AND THE AFT PASSENGER DOOR EXCEEDED LIMITS. THE TAILCONE RELEASE MECHANISM WAS RIGGED AND TESTED IAW MM 53-53-00.SDR AT9900551Cable · disconnectedTAILCONE UNSAFE LIGHT CAME ON AFTER TAKEOFF. RETURNED TO ATLANTA. RE-INSERTED CABLE BALL END INTO TAILCONE RELEASE HANDLE IAW MM 52-21. RII ACCOMPLISHED.SDR CALA9900969Fillet · corrodedINSPECTION FOUND CORROSION AROUND FASTENER HOLES FOR RT LOWER FILLET PANELS 2213C AND 2208C, STA 806, LONGERON 26R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, 51-30-2, AND 51-30-5.SDR DHL9970317CTail Cone · delaminatedAT C CHECK, TAIL CONE HAS DELAMINATION AT LEFT TOP AREA. REMOVED VERTICAL STABILIZER TAILCONE PER SRM 51-30-2. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1, USED RESIN 50-A AND CLOTH STYLE 720 10 INCH BY 6 INCH, PRIMED ALL REAS PER SRM 51-10-2.SDR CALA9900836Cables · out of adjustTAIL CONE DROP FAILED USING INTERIOR TAIL COMPARTMENT RELEASE HANDLE. THE TAIL CONE INTERIOR PULL WAS ADJUSTED WITHIN LIMITS IAW MM 53-50-00.SDR UF6A990734Fairing · crackedSBN - RIGHT VERTICAL STAB TO FUSELAGE ANGLE CRACKED AROUND AFT RIVET. MAINTENANCE REPAIRED CRACK IAW DER 99-131 AND BAE ATP SRM 51-30-01. (M)SDR UF6A990733Fairing · crackSBN - CRACK ON LEFT VERTICAL STAB FAIRING. MAINTENANCE REPAIRED CRACK IAW DER 99-131 AND BAE ATP SRM 51-30-01. (M)SDR ASAA9980155Lanyard · disconnectedPDX - DURING MAINTENANCE CHECK, THE TAILCONE RELEASE LANYARD WAS FOUND DISCONNECTED FROM THE RETAINER PIN. RECONNECTED LANYARD TO RELEASE MECHANISM RETAINER PIN. (M)SDR RRXA991417Fairing · crackedDURING A MAINTENANCE VISIT, FOUND CABIN AT STA 1688 RT FAIRING (SHROUD) CRACKED AND BROKEN, CARGO CONFIGURATION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FAIRING IAW FAA APPROVED TSDR RRXA991416Fairing · crackedDURING A MAINTENANCE VISIT FOUND CABIN AT STA 1688 LT FAIRING (SHROUD) CRACKED, CARGO CONFIGURATION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FAIRING IAW FAA APPROVED TENNESSEE TECHSDR QXEA9901456Panel · corrodedPDX - THERE IS FRETTING CORROSION ALONG FORWARD AND AFT EDGES OF CUTOUT FOR WING TO FUSELAGE PANEL 261DT. REPAIRED IAW HORIZON AIR EA 2-37-13.SDR QXEA9901455Fairing · corrodedPDX - THERE IS FRETTING CORROSION ALONG FORWARD AND AFT EDGES OF CUTOUT FOR WING TO FUSELAGE FAIRING PANEL 261NT. REPAIRED IAW HORIZON AIR EA 2-37-13.SDR QXEA9901451Fairing · corrodedPDX - THERE IS FRETTING CORROSION ALONG AFT EDGE OF CUTOUT FOR WING TO FUSELAGE FAIRING PANEL 261JT. REPAIRED IAW HORIZON AIR EA 2-37-13.SDR QXEA9901450Fairing · corrodedPDX - THERE IS FRETTING CORROSION ALONG AFT EDGE OF CUT OUT FOR WING TO FUSELAGE FAIRING PANEL 261GT. REPAIRED IAW HORIZON AIR EA 2-37-13.SDR 99FDEA00248Tail Cone · damagedIN FLT HAD LOUD BANG FOLLOWED BY AIRFRAME VIBRATIONS. ON POST FLT PATIO DOORS UNDER NR 2 ENGINE HAD OPENED IN FLT. *S/D* REMOVED AND REPLACED LT AND RT DROOP ELEVATORS AND TAIL CONE ASSY PER MM 27-30-03-4, MM 53-52-00. REPAIRED TAIL MISMATCH COVER ON EA 8-SDR CALA9900739Clip · out of adjustTHE CLIP TENSION AT TAIL CONE RELEASE EXTERIOR HANDLE WAS TOO LOW. A NEW HANDLE RETAINING CLIP WAS INSTALLED AND ADJUSTED IAW MM 53-53-00, PAGE 519.SDR CALA9900730Cables · out of adjustTHE TAIL CONE RELEASE PULL WAS EXCESSIVE USING THE INTERIOR AND EXTERIOR HANDLES AND AFT ENTRY DOOR. THE TAIL CONE CABLES WERE ADJUSTED/TESTED IAW MM 53-53-00, PARAGRAPH 3(A)&(B). DROP TEST PULLED WITHIN ALLOWABLE LIMITS.SDR P5CA9900613Fairing · delaminatedFUSELAGE LOWER SIDE LEFT SIDE AIR CONDITIONING FAIRING PANEL NR 192 HAS DELAMINATION. FIBERGLASS REPAIR PER SRM 51-40-09.SDR P5CA9900611Fairing · brokenRIGHT WING AFT WING TO BODY FAIRING NEAR INBOARD FLAP IS BROKEN. FIBERGLASS REPAIR IAW SRM 51-10-09.SDR DL757991072Radome · brokenON CLIMBOUT ABOUT 13,000 FT, HEARD TWO LOUD BANGING NOISE FOLLOWED BY LOUD AIR NOISE IN NOSE GEAR AREA. FOUND RADOME AND RADAR ANTENNA DAMAGED. MAINT IN PROGRESS.SDR CALA9900527Tail Cone · out of adjustTAIL COMPARTMENT INTERIOR TAIL CONE RELEASE HANDLE PULL TOO HIGH (45 LBS). RIGGED TAIL CONE RELEASE MECHANISM PER MM 53-53-00.SDR 99ZZZX2122Fairing · crackedDURING POST FLIGHT WALK-AROUND, THE RT UPPER WING-TO-FUSELAGE FAIRING (SECOND FROM FORWARD) WAS FOUND BENT BACK AT THE LEADING EDGE, AND CRACKED IN THE AFT CENTER AREA. THE FAIRING ATTACHING HARDWARE WAS STILL INSTALLED. PART REPLACED. INSPECTION OF THE AIRCSDR DL72E990981Fairing · corrodedFUSELAGE FAIRING RT AC BAY FRAME, CORROSION AROUND HINGES FOR ACCESS PANEL 3448 RBL 9 STA 740 TO 774. REMOVED PANEL 3448 DAMAGED T/E. BEGAN FABRICATING REPAIR PER M/M 53-30-1. OK TO PAINT AND INSTALL. COMPLETED FABRICATION PRIOR TO TREAT AND PAINT. INSTALSDR P2EA99165Radome · damagedMDW - PUSH BACK TUG HIT AIRCRAFT DAMAGING RADOME AND FUSELAGE SKIN AT BS 178 AT 6 O'CLOCK POSITION. REPLACED RADOME. FUSELAGE SKIN AT BS 178 REPAIRED BY TWA PER TWA ENG ARA NR'S 13540, 13541, 13542 DATED 5/3/99. (M)SDR CALA9900437Pipe · dentedTAIL CONE RELEASE CABLE GUIDE TUBE LOWER RIGHT HAS SEVERAL DAMAGED AREAS, DENTS, AND SHARP CREASES. REMOVED AND REPLACED PIPE ASSY PER MM 53-50-00.SDR CALA9900436Cable · frayedUPPER LEFT TAILCONE RELEASE CABLE WORN AND FRAYED WHERE IT PASSES OVER UPPER PULLY. REMOVED AND REPLACED PULLY PER MM 53-53-00.SDR CALA9900435Latch · wornUPPER LEFT TAIL CONE LATCH HAS DEEP INDENTATIONS ON BOTH SIDES. REMOVED AND REPLACED LATCH. PERFORMED FUNCTIONAL TEST PER CARD 08-5350-1-0008.SDR CALA9900434Latch · wornUPPER RIGHT TAIL CONE LATCH HAS DEEP INDENTATIONS ON BOTH SIDES. REPLACED LATCH PIN, RIGGED CABLES PER MM 53-33-00 AND TESTED TAIL CONE PER CARD 08-5350-1-0008.SDR VTZA990039Structure · lightning strikeFLT 7534 - IAD-EWR - DURING CRUISE, MADE AN UNSCHEDULED LANDING AT PHL DUE TO LIGHTNING STRIKE AT LEFT WING TIP. AIRCRAFT RELEASED FOR FERRY FLIGHT TO IAD. MAINTENANCE REMOVED AND REPLACED LEFT AILERON, RIGHT PROP, RADOME AND PATCHED RT FLAP AFTER C/W LIGHTISDR CALA9900355Handle · out of adjustTHE TAIL CONE EXTERIOR RELEASE HANDLE CATCHES ON LOWER LIP OF SKIN CUTOUT PREVENTING PULL OF HANDLE. INSPECTED HANDLE AND ADJUSTED CATCH WITHIN LIMITS AND PERFORMED ADJUSTMENT/TEST OF TAIL CONE RELEASE SYSTEM IAW MM 53-53-00.SDR DHL9970115DFairing · crackedAT D-CHECK, LEFT WING FUSE FAIRING HAS CRACK. STOP DRILLED AND INSTALLED DOUBLER REPAIR PER SRM 51-30-2, 6 X 4.SDR UPS99229342Frame · corrodedINSPECTION TYPE:C+SI ON INSPECTION OF UNDERWING FAIRINGS, NR 3430 FOUND TO HAVE A NUMBER OF SMALL GOUGES ON MAIN CENTER FRAME AND CORROSION ON FWD FRAME LOWER CHORD I/B. SMALL GOUGES BLENDED OUT AND FOUND WITHIN LIMITS. FWD FRAME LOWER CHORD REPAIRED IAW SRSDR UPS99229341Fairing · corrodedINSPECTION TYPE:C+SI ON INSPECTION OF FAIRINGS, NR 3335 UPPER SIDE OF FAIRING EXTRUSION FOUND TO BE CORRODED. INTERCOSTAL REPLACED PER SRM 51-10-6 AND 51-30-2.SDR SIMA990774Skin · dentedABI - DURING MBV INSPECTION, A DENT WAS DISCOVERED ON THE RT UPPER TAIL CONE STA 813.5. CUT OUT THE DAMAGED AREA AND RESTORED SURFACE TREATMENT OF THE CUT-OUT. REMOVED FASTENERS AND LIFTED THE VERTICAL STABILIZER FAIRING MOUNT ANGLE TO ALLOW FOR THE INTRODUCSDR DHL9980727CFairing · crackedAT C-CHECK, LT FAIRING PANEL FRAME TO FUSELAGE AT LONGERON APPROX STA 1000 HAS FORMED ANGLE CRACKED AT LOWER SURFACE. STOP DRILLED END OF CRACK, FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 51-21, 1 X 1 X 3.5.SDR CALA9900243Bayonet · wornTHE FORCE REQUIRED TO RELEASE TAIL CONE USING EXTERNAL HANDLE WAS LOW. THE LEFT LOWER TAIL CONE BAYONET WAS REMOVED AND REPLACED DUE TO WEAR. AN ADJUSTMENT/TEST OF THE TAIL CONE RELEASE MECHANISM WAS PERFORMED IAW MM 53-53-00.SDR CALA9900229Release Mech · failed testTHE TAIL CONE RELEASE PULL WAS LOW AT 15 POUNDS DURING TEST. THE TAIL CONE WAS REMOVED AND A NEW TAIL CONE WAS INSTALLED AND RIGGED IAW MM 53-53-00. OPERATIONAL CHECKS WERE GOOD.SDR SIMA990391Fairing · chafedABI - DURING AN MBV INSPECTION, A CHAFE WAS DISCOVERED AT LT STABLIZER TO FUSELAGE FILLET FAIRING CONTACT AREA. BLENDED CHAFE AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. APPLIED PROTECTIVE TREATMENT INCLUDING TOP COAT TO BLENDED ASDR AWXA9900060Fitting · damagedTOP OF RIGHT WING FILLET AREA, STA 663 SPLICE FITTING HAS A HOLE/DRILL START WBL 71.24. REMOVED FASTENER ON FITTING, SPOT FACED HOLE TO REMOVE DAMAGE, SHOT PEENED PER BAC 5730, ALODINED AND PRIMED PER SRM 51-10-2 IAW AND ER 2-57-31-17. REINSTALLED FASTENER ISDR 99ZZZX1364Skin · crackedPILOT REPORTED FLUTTER/VIBRATION IN-FLIGHT. UPON INVESTIGATION, DISCOVERED TAILCONE CRACKED CIRCUMFERENTIALLY APPROXIMATELY 60 PERCENT, ABOUT 18 INCHES IN FROM TIP OF TAIL CONE. FURTHER INVESTIGATION REVEALED SEVERAL SMALLER CRACKS BEGINNING AT STIFFENER FASSDR SWAA990187Radome · bird strikeAFTER TAKEOFF AT 1500 FT, LARGE BIRD HIT RADOME. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RADOME ASSY AS PER MM. C/W BIRD STRIKE INSPECTION COMPLIED WITH PER MM 05-51-37. NO OTHER DEFECTS NOTED. A/C OK FOR CONTINUED SESDR CA990323025Cowl · separated(CAN) DURING FLIGHT, THE FORWARD BELLY COWLING SEPARATED FROM THE AIRCRAFT AND LANDED IN A FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. SUBSEQUENT INVESTIGATION REVEALED THAT 4 LATCHES WERE WORN AND MAY NOT HAVE BEEN POSITIVELY ENGAGED. THE LATCHES AND COWLISDR CALA9900070Handle · out of adjustTHE TAIL CONE EXTERIOR RELEASE HANDLE FAILED PULL TEST. THE HANDLE FAILED LOW AT 18 POUNDS. THE TAIL CONE EXTERIOR RELEASE HANDLE WAS RIGGED AND FELL WITHIN TEST LIMITS IAW MM 53-53-00.SDR P5CA9900034Fairing · damagedRIGHT BODY FAIRING PANEL 194B FOUND DAMAGE. REPAIRED PER SRM 51-48-14.SDR USAA990037Fairing · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION STA 980 RT SIDE KEEL BEAM FAIRING FLANGE NEAR SCREW HOLE. REPAIRED PER SRM 53-50-12 AND E.O. 5195T055, PART 2, STEPS 2, 4. (X)SDR USAA990035Fairing · corrodedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION STA 1000 LEFT OF KEEL BEAM OF FAIRING FLANGE. REPAIRED PER SRM 53-50-12, PAGE 107. (X)SDR P5CA9900036Fairing · damagedFUSELAGE FAIRING PANEL 194B FOUND 1.5 INCH HOLE. REPAIRED PER SRM 51-40-12 FIG 10.SDR UF6A990114Empennage · damagedORD - DAMAGE TO RIGHT HAND EMPENNAGE AREA. DAMAGE LOCATED BETWEEN STA 441.5AS TO STA 378AS. MAINTENANCE REPAIRED DAMAGE TO RIGHT HAND EMPENNAGE IAW DER REPORT NR 99-009. ACFT TT: 14,110 HOURS. (X)
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