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 0700396732Skin · damagedDURING "L" CHECK WHILE REPLACING DAMAGED TAIL CONE FOUND SKIN PANEL WITH ELONGATED FASTENER HOLES AT BS 2701-2742 SECTION 48. REPAIRED PER EA 67-208732.SDR UPS07448961Support · corrodedINSPECTION TYPE:C FX REAR BODY FAIRING SUPPORT LWR SURFACE FOUND CORROSION AT STA 1520 TO STA 1525 CENTER SUPPORT. BODY FAIRING SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.SDR CA070105001Radome · bird strike(CAN) AFTER DEPARTURE CREW WITNESSED A BIRD STRIKE ON THE NOSE OF THE AIRCRAFT. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT AND LAND OVERWEIGHT (ESTIMATED AT 49200 LBS). AIR TRAFFIC CONTROL WAS NOTIFIED BUT EMERGENCY EQUIPMENT WAS NOT REQUIRED. MAINTENANCE INSDR AALA20070051Control Cable · frayedTUL - DURING SCHEDULED MAINTENANCE, FOUND TAIL CONE JETTISON HOIST CONTROL CABLE FRAYED. REPLACED TAIL CONE JETTISON HOIST CONTROL CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR BIOR061211001Fairing · corrodedDURING A PHASE 4 INSPECTION PAINT BLISTERS WERE NOTED ON THE LT AND RT WING ROOT FAIRING LOWER AFT PANELS P/N 101-420024-43 AND 101-420024-8. UPON FURTHER INSPECTION BOTH PANELS WERE FOUND TO BE CORRODED THRU IN SEVERAL PLACES FROM THE INSIDE OUT. AFTER REMOVSDR 06FDEA04201Frame · damagedLEFT FWD TAILCONE FRAME ALIGNMENT PIN HOLE (CTR POS) ELONGATED. DAMAGED FRAME AT L/H FWD TAILCONE REMOVED AS PER SRM 51-31-01 VOL.II. HOLES ON NEW FRAME PICKED-UP AS PER SRM 51-31-01 VOL.II AND DWG AKC 7520. NEW FRAME AT L/H FWD TAILCONE INSTALLED AS PESDR 06FDEA04170Frame · crackedRT FWD TAILCONE FRAME ALIGNMENT PIN HOLE (CTR POS) FOUND WITH CRACK. REPAIRED AS PER SRM 53-00-01 FIG.9 VOL. I AND SRM 53-30-00 FIG.12 VOL.I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA04105Intercostal · damagedFOUND ONE EACH INTERCOSTAL DAMAGED AT FORWARD LOWER RT AREA OF TAILCONE, INTERCOASTAL P/N AKC7549-9. NEW INTERCOSTAL INSTALLED AS PER SRM 51-31-01 VOL 2.SDR 06FDEA04101Skin · damagedFOUND SKIN DAMAGED AT FORWARD LOWER RT AREA OF FORWARD TAILCONE, SKIN P/N AKC7541-41). SNRM N02226: NEW SKIN REPLACED AS PER SRM 51-31-01 VOL2 (MAJOR REPAIR).SDR 06FDEA04100Frame · crackedFOUND ONE FRAME CRACKED AT FORWARD LOWER RT AREA OF FORWARD TAILCONE, (FRAME P/N AKC7520U5). FRAME REPLACED AS PER SRM 51-31-01 VOL 2.SDR 06FDEA04104Intercostal · damagedFOUND ONE EACH INTERCOASTAL DAMAGED AT FORWARD LOWER RT AREA OF TAILCONE, INTERCOASTAL P/N AKC7549-5. DAMAGED INTERCOASTAL REPLACED AS PER SRM 51-31-01 VOL2.SDR 06FDEA04103Frame · damagedFOUND ONE EACH FRAME DAMAGED AT FORWARD LOWER RT AREA OF TAILCONE, FRAME P/N AKC7522-7. DAMAGED FRAME REPLACED AS PER SRM 51-35-01 VOL2.SDR 06FDEA04102Stiffener · crackedFOUND ONE EACH STIFFENER INSIDE FRAME CRACKED AT FORWARD LOWER RT AREA OF FORWARD TAILCONE, STIFFENER P/N AKC7520-9. NEW STIFFENER INSTALLED AS PER SRM 51-35-01 VOL2.SDR IXXA06SMN402SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE TAIL CONE LEFT SIDE EXTERIOR SKIN CRACKED AT STATION 1756.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREASDR AALA20060783Radome · damagedBNA - ON POST FLIGHT FOUND BIRD STRIKE ON RADOME. RADOME PUNCTURED AND RADAR ANTENNA DENTED. REPLACED RADOME AND RADAR ANTENNA. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR QXEA20060289Radome · chafedC3 PDX - AT FS 169.00 BOTH THE RIGHT AND LEFT SPACERS ON THE RADOME ARE CHAFING ON THE BULKHEAD. REPAIRED IAW SRM 51-25-01 AND 53-81-80.SDR UIEA200600259Fairing · crackedDURING VISUAL INSPECTION FOUND (1)BODY FAIRING 293C & 293D INNER SURFACE CRK (2) FOUND BODY FAIRING 194B, 193C, 193D, 193G,WITH DENT MARKS CAUSED BY TIRE BLOWN. COMPOSITE REPAIR CARRIED OUT AS PER SRM 51-40-12 FIG 9.SDR UIEA200600258Fairing · dentedDURING VISUAL INSPECTION OF BODY FAIRING 194C FOUND DENT MARKS CAUSED BY TIRE BLOWN. COMPOSITE REPAIR CARRIED OUT AS PER SRM 51-40-15 FIG 7.SDR 06FDEA03220Hinge Fitting · crackedEMPENNAGE, FORWARD TAILCONE LEFT FORWARD HINGE FITTING FOUND CRACKED (LOCATED AT AFT ACCESSORY COMPARTMENT AFT BULKHEAD AREA). REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR UPS06M48197Stiffener · crackedINSPECTION TYPE:C FX-RT WING TO FX FAIRING CUT-OUT LOWER SIDE AT Y=1236.800 FOUND SUPPORT FITTING CRACKED. CRACKED STIFFENER INTERNAL SUPPORT AND CRACKED STIFFENER REMOVED PER SRM 51-31-01 VII R.38. NEW STIFFENER FASTENER HOLES PICK-UP PER DWG AYB7104 AND SRSDR UPS06M48196Support Fitting · crackedINSPECTION TYPE:C FX-RT WING TO FX FAIRING CUT-OUT LOWER SIDE AT Y=1216.200 FOUND SUPPORT FITTING CRACKED. CRACKED FITTING ON FX-RHW TO FX FAIRING CUTOUT LOWER SIDE AT Y=1216.20 0 AND ATTACHED INTERNAL FITTING REMOVED PER SRM 51-31-01 V.II R.38. HOLE S PICK-SDR EIA2006210Support · crackedCRACK ON BODY FAIRING SUPPORT LT BS 1480 WL 140. REPAIRED AS PER EN-EA-53-1067.SDR MALA060561Fairing · damagedLT FAIRING PANEL 197BL SUSTAINED DEER STRIKE AND REQUIRES REPAIR. REPAIRED IAW EOS51031. THIS IS A MAJOR REPAIR.SDR VNAA0608040Radome · delaminatedTHE CREW REPORTED A LIGHTNING STRIKE ON THE LT SIDE OF NOSE. MAINTENANCE PERFORMED AN EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. RADOME WAS REPLACED AND DAMAGE TO NOSE GEAR DOORS AND FUSELAGE WERE REPAIRED. AIRCRAFT WAS RELEASED FOR SERVICE.SDR A6WA200640338Fairing · looseVERY NOTICEABLE RUMBLE AND VIBRATION COMING FROM NOSE AREA DURING CLIMB-OUT. ALTITUDE 12,000 TO 13,000 FT ASL, GEAR UP. LASTED APPROXIMATELY 30 SECONDS THEN DISAPPEARED. VIBRATION FELT THROUGH FLOOR AREA IN COCKPIT. FOUND BELLY FAIRING LOOSE. RESEALED IAWSDR UPS06247849Fairing · corrodedINSPECTION TYPE:C BODY FAIRING 3430 HAS AREA OF LIGHT SURFACE CORROSION LWR DOOR CUTOUT FRAME. PLEASE REMOVE ANCHOR NUTS, REMOVE CORROSION, REINSPECT AND RECTIFY AS NECESSARY. FRAME AND SUPPORT BRACKET REPAIRED IAW SRM 51-40-04 AND 51-30-02.SDR UPS06447938Support · corrodedINSPECTION TYPE:C FX AIR CONDITIONING BAY FAIRING SUPPORT FLOATING NUT AT SURFACE FOUND SURFACE CORROSION AT STA 1045 RBL 10 TO RBL 57. CORROSION BLEND OUT 0.029" BY 1/2" BY 20" EXCEED SRM LIMIT. FX BS 1045 BL0 - RBL57 FAIRING SUPPORT REPAIRED AS PER SRM 51-SDR UPS06447926Support · corrodedINSPECTION TYPE:C FX FRONT BODY FAIRING SUPPORT LOWER SURFACE CORROSION AT STA983 LBL20 TO RBL10. CORROSION BLEND OUT 0.025" X 1/2" X 10" EXCEED SRM LIMIT. FX BS983 LBL22 TO RBL33 BODY FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.SDR UPS06447914Support · corrodedFX AIR CONDITIONING BAY FAIRING SUPPORT FLOATING NUT AT SURFACE FOUND CORROSION AT STA 1013 TO 1017 O/B SIDE. CORROSION BLEND OUT 0.050" BY 1/2" BY 8" EXCEED SRM LIMIT. FX BS1005-1018 RBL75 FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.SDR ASMF200608010Radome · damagedDURING FINAL APPROACH, A HAIL STORM WAS REPORTED BY CAPTAIN AND A MISSED APPROACH WAS PERFORMED. DURING MAINTENANCE REVIEW, THE RADOME WAS DETECTED DAMAGED AND OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK DENTS WERE DETECTED IN HSDR MALA060505Rail · brokenDURING MAINTENANCE WALK AROUND FOUND TAIL FRAME RAIL BROKEN. THIS FRAME WORK WHICH THE AFT TAIL NAV LIGHTS MOUNT TO. BROKEN RAIL CAUSED DAMAGE TO THE LT AIRBRAKE AS WELL. REPLACED AIRBRAKE, REAR NAV LIGHT AND TAIL BOOM ASSEMBLY.SDR UIEA200600194Fairing · departedDURING WALK AROUND, FOUND 1-EACH FILLET FAIRING DAMAGED ON RIGHT WING (OVERWING). REMOVED AND REPLACED FILLET FAIRING AS PER MM 53-51-01.SDR A6WA200640292Fairing · looseUNUSUAL VIBRATION IN AIRFRAME AND YOKE WHEN FLAPS EXTENDED AND RETRACTED. FOUND FORWARD AND AFT MOUNTS OF RIGHT AND LEFT BELLY FAIRING TO HAVE EXCESS MOVEMENT. SEALANT BROKEN AND BELLY FAIRING LOOSE. (M)SDR AALA20060463Pin · inoperativeSTL - TAIL CONE JETTISON SYSTEM INSPECTION AND OPERATIONAL CHECK FAILED FIRST DROP FROM AFT PASSENGER DOOR. ADJUSTED AND LUBRICATED PUSH PIN. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DLM88060520Skin · delaminatedTAIL CONE DELAMINATION/SPONGY APPEARS TO BE SKYDROL SOAKED. REPLACED TAIL CONE DUE TO LIGHTNING STRIKE DAMAGE PER M/M 53-53-00-401-2 P/N INSTALLED 5940163-1.SDR U5QA06003Radome · debondedNOSE RADOME DELAMINATION LARGE AREA ON NOSE.REQUIRED OVERHAULSDR LR7A06062Panel · delaminatedDURING SCHEDULED C7 CHECK PER JOB CARD HC3212 FOUND RT MWW OUTBOARD PANEL (HONEYCOMB) DELAMINATED MORE THAN 30 PERCENT OF AREA AT FS 491 - FS 617, WL 159 - WL 190, RBL 100. FABRICATED AND INSTALLED PANEL IAW LAC MEA 382-53-06-045.SDR QXEA200601638Tail Cone · dentedPDX: DENT IN RT TAIL FUSELAGE BAY, 5 INCHES LONG, 1 INCH WIDE AND .019 INCHES DEEP FS X910.0 BETWEEN STRINGER 21R AND 22R ON RT SIDE OF TAIL FUSELAGE. MAINTENANCE REPAIRED IAW Q400 NDTM PART 6, 51-00-01, HORIZON EA 6-55-146, AND RD 8/4-55-0271.SDR QXEA200601434Fairing · dentedPDX - C4 THE METAL PORTION OF THE LEFT WING TO FUSELAGE FAIRING HAS A SERIES OF DENTS. RUNNING VERTICALLY AT ABOUT STATION X320, BETWEEN STRINGER 6L AND 9L. REPAIRED IAW HORIZON AIR EA 2-53-748 AND RD 8-53-9081.SDR DLM88060464Tail Cone · deployedTAIL CONE INADVERTENTLY DEPLOYED. ADJ SPRING CAM RELEASE CABLE. REINSTALLED TAIL CONE PER MM 53-53-00. ADJ OF TAIL CONE RELEASE MECHANISM CAM OK PER MM.SDR UPS06146993Fairing · ground damageA/C WAS STRUCK BY ANOTHER A/C WHILE PARKED. THIS CAUSED SIGNIFICANT DAMAGE TO THE TAIL CONE EXHAUST FAIRING. ITEM IS DEFERRED IAW UPS FERRY FLIGHT. APU HAS BEEN DEFERRED AND STA FR 101 HAS BEEN BLOCKED OFF PER AIRBUS NTO 13-2006-92071-1. FERRY FLT CLEARS DSDR MWEA060052Crank Assy · defectiveTAIL CONE FAILED THE PULL TEST AND THE TAIL CONE DID NOT DEPLOY WHEN USING THE VENTRAL STAIR DOOR. REMOVED AND REPLACED CRANK ASSEMBLY.SDR MWEA060049Frame · crackedLOWER FUSELAGE FILLET FAIRING FRAME IS CRACKED, JUST FORWARD OF LEFT INBOARD FORWARD CORNER OF LEFT MAIN LANDING GEAR. FABRICATED AND INSTALLED DOUBLER AND STIFFENER.SDR QXEA200601310Skin · dentedYYC - C4 FUSELAGE EXTERIOR, TAIL CONE LEFT HAND SIDE SKIN AT STATION X 718 AND Z 155 IS DENTED. REPAIRED IAW RD8-55-1689 AND EA 2-55-123.SDR VNAA0605007Radome · dentedDURING WALKAROUND INSPECTION THE CREW DISCOVERED A DENT IN THE LT FORWARD FUSELAGE AFT OF THE RADOME. MAINTENANCE FOUND THE DENT -ACCEPTABLE AS IS- AFTER INSPECTION IAW BOMBARDIER REO 670-53-11-141. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR UPS06246808Fairing · delaminatedDELAM ON L/AFT WING TO BODY FAIRING PANEL NR 3510 JUST AFT OF HYD SYS BAY REF EO B727-5350-24306. PERFORMED INTERIM REPAIR PER EO B727-5350-24306 STEP 6. DEFERRED FOR REPEAT INSPECTION EVERY 30 DAYS AND PERM BY C-CK. NR D 325051 ASSIGNED INSTALLATION OF PANSDR UPS06846873Skin · crackedINSPECTION TYPE:C3 AFTER REMOVAL OF TAIL CONE FOUND EXTERIOR SKIN DENTED, CRACKED, AND BROKEN OUT FWD END. REMOVED DAMAGED SKIN AT TAIL CONE EXTERIOR STA 1990 IAW SRM 53-02-00-0. RECEIVED, DRILLED UP NEW SKIN IAW SRM 53-02-00-0 AT TAIL CONE EXTERIOR SKIN STASDR VNAA0604010Structure · lightning strikeTHE CREW REPORTED TAKING A LIGHTNING STRIKE IN FLIGHT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. MINOR DAMAGE WAS FOUND ON THE TOP VHF ANTENNA, LOWER TAIL STATIC DISCHARGER, AND THE TAIL COSDR CA060413008Fairing · chafed(CAN) RT HORZ STAB TO BODY SEAL FAIRING LOWER IB GUIDE CHAFED AT FORWARD END. (TC NR 20060413008)SDR DLM88060266Release Cable · dislodgedTAIL CONE UNSAFE MSG AT FL 220. FOUND UPPER RELEASE CABLE (INNER RELEASE CABLE) TRIPPED. REINSTALLED CABLE. NO MSG ON EOAP.
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