JASC 5530
Service difficulty reports · 2,534
Reports filed under 5530 · Vertical Stabilizer, 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 = '5530' 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 = '5530' 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 QXEA200301089Bracket · crackedCONNECTION BRACKET IS CRACKED AT LEFT HAND STABILIZER STATION 716.00 AFT OF FRAME 4 AND STRINGER 4L. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-55-199.SDR 03FDEA01391Panel Support · chafedVERTICAL STAB LT TEE SUPPORT IS CHAFED WHERE PANEL 8603 LWR ATTACHMENT ANGLE, ATTACHES TO THE PANEL SUPPORT. CUT OUT DAMAGED AREA 3 X 1 INCH ON LT VERTICAL STAB SUPPORT AT PANEL 9603'S AFT ATTACH ANGLE MOUNT HOLE. FABRICATED AND INSTALLED REPAIR IAW SRM 55SDR C2XA03TY133Housing · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND VERTICAL STAB SPHERICAL BEARING HOUSING. MAINTENANCE CLEANED AND REPAIRED THE HOUSING IAW EXPRESS JET EC 5510-01061 AND EMB MM 51-50-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BESDR CA030731010Bracket · cracked(CAN) DURING ROUTINE 200 HOUR INSPECTION THE FORWARD LT VERTICAL FIN ATTACHMENT BRACKET APPEARED TO BE CRACKED ALONG THE BASE EXTERNAL SURFACE WHERE IT MATES WITH THE VERTICAL TABS OF THE PART. DISASSEMBLY REVEALED THE CRACK EXTENDED FORWARD AND AFT ALONG THISDR 3983Torque Tube · crackedPILOT NOTED DURING PREFLIGHT INSP ON RAMP, THAT THE UPPER LT VERTICAL STAB WAS BENT IN APPRX 3 INCHES AT THE TOP. VIDEO FOOTAGE OF THE FBO WAS REVIEWED AND IT WAS SEEN THAT THE AIRCRAFT LANDED IN THIS DAMAGE (WAS NOT CAUSED BY PERSONS OR EQUIPMENT ON THE GROUNSDR MALA030332Angle · crackedDURING C-CHECK INSPECTION IN CVG, LT VERTICAL STABILIZER TO FUSELAGE CLOSING ANGLE CRACKED. MAINTENANCE REPAIRED PER EO A55027. REFER TO 409 127862 FOR DETAIL. A/C RELEASE DATE 7/1/2003.SDR CA030702005Fitting · cracked(CAN) DURING PREFLIGHT INSPECTION PILOT NOTICED CRACK, PARALLEL ALONG 90 DEGREES ANGLE.SDR SWAA031346Drag Angle · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL FIN ATTACH CLEVIS DRAG ANGLES CORRODED LT SIDE (2 EA). REMOVED AND REPLACED VERTICAL FIN DRAG ANGLES PER SRM.SDR MALA030308Frame · damagedDURING C-CHECK INSPECTION IN CVG, VERTICAL STAB FRAME ASSEMBLY ITEM NR 1 (HC553314HO138-000) AT RIB 20 WAS DAMAGED DUE TO ITS AFT BUSHING WORN AND CAUSING THE FRAME ASSEMBLY TO DROP AND CHAFE ON RUDDER HINGE ASSEMBLY AT RIB 20. REPLACEMENT OF ITEM 1 & 2 (HC55SDR AUS20030553Hinge · mislocated(AUS) VERTICAL STABILIZER CENTRE HINGE FITTED IN WRONG LOCATION. MANUFACTURING ERROR.SDR CALA0300275Angle · gougedINSPECTION FOUND L-ANGLE AT LT VERTICAL STABILIZER BOTTOM INSIDE PANEL 9507 GOUGED. THE GOUGED SECTION OF L-ANGLE WAS REMOVED AND REPLACED IAW ECRA 5380-01013.SDR SWAA031142Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR PRIMARY LUG AFT FACE CORRODED ON BOTH LT/RT SIDES. REPAIRED VERT STAB PER BFG ER.SDR GTIA030346Fitting · crackedINTERNAL ANGLES ON DORSAL FITTINGS CRACKED BOTH SIDES, STATION 1437. REMOVED LEFT AND RIGHT INTERNAL ANGLES. LOCATED AND DRILLED NEW INNER ANGLE ON LEFT DORSAL FIN. INSTALLED LEFT AND RIGHT INNER ANGLES. (M)SDR MALA030274Angle · crackedDURING C-CHECK INSPECTION IN CVG, LT VERTICAL STAB TO FUSELAGE CLOSING ANGLE CRACKED. MAINTENANCE REPAIRED CRACKED CLOSING ANGLE IAW EO A55024. REF 409 118064 FOR DETAIL. A/C RELEASE DATE 5/21/03.SDR MWEA030184Angle · crackedRIGHT VERTICAL STABILIZER ATTACH ANGLE IS CRACKED IN RADIUS AT FRAME STATION 1437. FABRICATED AND INSTALLED ANGLE AND INSTALLED FILLER AND WASHERS.SDR 03FDEA00353Panel · delaminatedVERTICAL STAB. LE PANEL 321AL DELAMINATEDSDR USAA030029Support Fitting · wornPIT - FOUND TERMINAL SUPPORT FITTING HAS TWO WORN BOLTS, VERTICAL STABILIZER AFT TERMINAL SUPPORT FITTING BOLT HOLES. REWORKED WORN HOLES PER EA 94263A, THIS IS AN INTERIM REPAIR. (M)SDR UPS03840385Fitting · crackedINSPECTION TYPE: C2, LEFT SIDE VERTICAL ATTACH STRAP FOR JACKSCREW TRIM MOTOR SUPPORT BASE CRACKED AT FASTENER HOLE. REMOVED SUPPORT FITTING IAW DC8 SRM 51-1-21 & 51-3-0. LOCATED AND DRILLED UP SUPPORT FITTING 2649617 IAW DC8 SRM 51-1-21 & 51-3-0. INSTALLESDR ASAA0310070Angle · chafedPAE - DURING C-CHECK, FOUND VERTICAL STABILIZER SKATE ANGLE AT BS 1016-1138, CHAFED. REMOVED AND REPLACED SKATE ANGLE PER SRM. (M)SDR AMWA16Structure · damagedON FLIGHT 5437 FROM KANSAS CITY MISSOURI, THE CREW THOUGHT THEY HAD A BIRD STRIKE AND DIVERTED TO SALINA KANSAS DUE TO WEATHER CONDITIONS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. UPON POSTFLIGHT INSPECTION, THE CREW REPORTED DAMAGE TO THE VERTICAL AND SDR C2XA03TY031Housing · corrodedDURING A SCHEDULED 2C INSPECTION THE LT AND RT VERT STAB SPHERICAL BEARING HOUSING HAD LITE CORROSION. MAINTENANCE REWORKED BOTH VERTICAL BEARING HOUSINGS IAW EC 5510-01052 AND EMB 145 AMM 51-50-01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETSDR SWAA030425Beam · crackedDURING SCHEDULED D-CHECK, FOUND VERT STAB RT T/E BEAM CRACKED AT FIN STA 81.8. REMOVED AND REPLACED RT T/E BEAM PER SRM.SDR COMA0360067Bushing · looseTHE LT VERTICAL STABILIZER LUG BUSHING WAS MIGRATED .025 INCH AT THE HORIZONTAL STABILIZER PIVOT POINT. REMOVED THE MIGRATED BUSHING. PERFORMED NDT/LP1 TO ENSURE NO DAMAGE TO LUG BORE. MACHINED AND INSTALLED A 1ST OVERSIZED BUSHING I/A/W REO 601R-55-31-04SDR C2XA03TY016Housing · gougedTYS, During a scheduled inspection the right vertical stab spherical bearing housing support has internal gouges at 1 and 8 oclock position. Maintenance reamed the hole and installed a bushing I/A/W-EMB-EC5510-01049. Aircraft will be released to service upon cSDR CA030211012Skin · cracked(CAN) TWO INCH CRACK FOUND IN LEFT HAND VERTICAL STABILIZER WHILE COMPLYING WITH SB 218SDR SWAA030158Angle · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB LEFT AND RT DRAG ANGLES CORRODED. REMOVED AND REPLACED ANGLES PER SRM.SDR 03FDEA00048Structure · damagedAT 23,000 FT WHILE ACCEL, FELT AIRFRAME VIB AND RETURNED. FOUND NR 1 VERT, LE, FIN ASSY DAMAGED. COAX ENDS PULLED FROM MOUNT, NUMEROUS FIBERGLASS SUPPORTS BROKEN, ANTENNA CONDUIT BENT AND STANDOFFS BROKEN. THIS INCLUDES ANTENNA ITSELF. FOUND STIFFENER 4.5 SDR FFS2003F00009Bolt · undertorquedWHILE PERFORMING AN INSPECTION OF THE TAIL SECTION, THE UPPER FOUR ATTACH BOLTS FOR THE VERTICAL STABILIZER FORWARD SPAR WERE SMOKING AND THE WASHERS WERE LOOSE UNDER THE RT SIDE BOLT HEADS. ALL FOUR BOLTS WERE BELOW MINIMUM TORQUE SPECS.SDR GUU2003F00002Bracket · crackedAT SCHEDULED INSPECTION, THE LT RUDDER TORQUE SHAFT SUPPORT BRACKET WAS FOUND TO BE CRACKED. REMOVED AND REPLACED LT RUDDER TORQUE SHAFT SUPPORT BRACKET.SDR ASAA0280701Frame · chafedOKC - FOUND DURING 30K CHECK, JACKSCREW ACCESS PANEL ON THE VERTICAL STABILIZER HAS CHAFED FRAME MATING FACE. REPLACED FRAME PER SRM 51-30-2 AND 51-30-5. (M)SDR C2XA02TY186Bushing · gougedTYS, During a scheduled inspection, the right hand vertical stab spherical bushings where found gouged. Maintenance reamed the hole for oversized bushing and alodined and installed bushings. I/A/W-EC5510-001045. The repair was satisfactory and the aircraft wasSDR C2XA02TY185Bushing · looseTYS, During a scheduled inspection, the left hand vertical stab spherical bushings where found loose. Maintenance reamed the hole for oversized bushing and alodined and installed bushings. I/A/W-EC5510-001045. The repair was satisfactory and the aircraft was rSDR 02FDEA00929Skin · crackedRT VERTICAL FIN SKIN HAS 2 POSSIBLE CRACKS EMANATING FROM FASTENERS AT BS 1214 COMMON TO SPAR ** SD ** DAMAGE TO RT VERTICAL FIN SKIN AT BS 1214 COMMON TO FRONT SPAR FORGING JUST ABOVE FUSELAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-01, REPAIRED DAMAGE ISDR GTIA021282Former · crackedFTW - FOUND VERTICAL STAB DORSAL FIN CRACKED ON FORMER RIGHT SIDE LOWER ATTACH TO PLATE/STRAP. REMOVED FORMER. LOCATED AND DRILLED NEW FORMER. INSTALLED NEW FORMER, STRAP AND LEFT AND RIGHT PLATES. (M)SDR CA021115016Plate · cracked(CAN) DURING INSPECTION OF AFT FUSELAGE TO FIN ATTACH ADAPTER PLATES AS PER CF-99-11. THE AFT PLATE WAS FOUND CRACKED AT STA 535. ALL ADAPTER PLATES ARE THE POST MODIFICATON TYPE OF A MORE CORROSION RESISTANT MATERIAL. SB 6/516 CALLS UP ONLY A SIMPLE VISUAL ISDR QXEA0201598Attach Angle · crackedPDX- CRACK IN RADIUS OF VERTICAL STABILIZER ATTACH ANGLE AT 32 PERCENT OF VERTICAL STABILIZER SPAR ON THE LT SIDE. REPAIRED IAW FOKKER SRM 55-31-00.SDR QXEA0201597Attach Angle · crackedPDX- CRACK AT FASTENER ON RT SIDE OF VERTICAL STABILIZER ATTACH ANGLE. SECOND FROM THE AFT FASTENER ON THE UPPER FLANGE OF THE ATTACH ANGLE. REPAIRED IAW FOKKER SRM 51-10-4 AND 55-31-00SDR SWAA022218Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER AFT SPAR PRIMARY LUG FACE FITTINGS CORRODED. REPAIRED FITTINGS PER BFG ER.SDR 02FDEA00535Pin · rotatedVERTICAL STABILIZER TO FUSELAGE ATTACHMENT TAPERED PIN & SLEEVE ASSEMBLIES RED INDICATOR MARKS SHOW PIN ROTATION AT ALL SIX LOCATIONS. REMOVED AND REPLACED PINS PER AMM 55-30-11 & EA 6-5530-64304.SDR 02FDEA00480Stringer · crackedCRACKED STRINGER AT VERTICAL FIN STA 20, STR LT RIB NR 2. REPAIRED STR 4 LT AT VERTICAL FIN STA 20, RIB NR 2 IAW SRM 55-30-4 FIG 1. REPAIRED STR 4 LT AT VERTICAL FIN STA 20, RIB NR 2 IAW SRM 55-30-4 FIG 1.SDR 02FDEA00481Stringer · crackedCRACKED STRINGER AT VERT FIN STRINGER 8 AT RIB NR 2 RT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1.SDR CA020718009Fitting · broken(CAN) ON PRE-FLIGHT INSPECTION THE PILOT NOTICED A CRACK ON THE LEFT VERTICAL FIN ATTACH BRACKET. WHEN MAINTENANCE REMOVED THE BRACKET IT WAS FOUND BROKEN THROUGH. THE BRACKET WAS REPLACED WITH NEW AND NEW HARDWARE USED. THE RIGHT BRACKET WAS REMOVED CLEANED ASDR CA020606020Brace · cracked(CAN) DURING INSPECTION IT WAS NOTED THAT THE RH AUX VERTICAL STAB WAS VERY LOOSE. UPON FURTHER INVESTIGATION IT WAS NOTED THAT BOTH THE FORWARD AND AFT AUX VERTICAL STAB BRACE PLATES WERE CRACKED COMPLETELY THROUGH. THE AUX VERTIACL STAB WAS REMOVED FROM THE SDR GUU2002F00006Bolt · loose(BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLT REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLT IAW MFG MM.SDR GUU2002F00010Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GUU2002F00014Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GUU2002F00015Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW BEECH MM.SDR GUU2002F00013Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR GUU2002F00012Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.SDR DL72S020584Skin · crackedFOUND ON E1 LETTER CK 1/2 CRACK VISIBLE VERTICAL STAB AT LWR END SKIN AT AFT SPAR R/H SIDE REPAIRED PER M/M 55-30-000-8 FIG 801
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