JASC 5553
Service difficulty reports · 586
Reports filed under 5553 · Vertical Stabilizer, Attach Fittings, 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 = '5553' 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 = '5553' 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 SWAA042130Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS CORRODED. REPAIRED VERTICAL STAB PER ER.SDR SWAA042129Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL FIN BODY FITTING LUGS CORRODED. REPAIRED VERTICAL FIN PER ER.SDR UPS04842793Attach Angle · crackedINSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE HAS POPPED RIVET, LT SIDE, STA 1766. REMOVED PAINT IAW SRM 51-20-00. FOUND CRACK, NDT VERIFIED. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-26, 51-1SDR UPS04842792Attach Angle · crackedINSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1750 RT SIDE. STRIPPED PAINT IAW MM51-20-00. NDT VERIFIED CRACK. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG.16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-11, 51-1-26.SDR DL73S040658Fitting · corrodedVERTICAL STABILIZER NR 5 FIN LUG AFT FACE CORRODED. REPAIRED IAW ERA 091628-14.SDR CA040629009Bolt · undertorqued(CAN) IN REFERENCE TO AN MAINTENANCE ALERT, AN INSPECTION WAS CARRIED OUT TO THE VERTICAL STABILIZER FRONT SPAR ATTACHMENT BOLTS FOR SECURITY AND TORQUE OF AIRCRAFT. ONE AIRCRAFT WAS FOUND WITH BOLT TORQUE UNDER THE SPECIFIED TORQUE ON THE RT SIDE UPPER AND LSDR DL73S040571Attach Fitting · damagedVERTICAL STABILIZER ATTACH LUG FOUND TO HAVE A THINNER FLANGE THAN BLUEPRINT. AREA REPAIRED IAW ERA 090968-14AD.SDR SWAA041052Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR RIGHT AND LEFT PRIMARY CLEVIS AFT LUGS, CORRODED. REPAIRED VERTICAL STAB LUGS PER ER.SDR MWEA040039Frame · crackedAFT ACCESSORY CANTED FRAME WEB HAS A CRACK LOCATED JUST RIGHT OF FORWARD VERTICAL STABILIZER FRONT ATTACH TANG. FABRICATED AND INSTALLED DOUBLER.SDR SWAA040624Attach Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR PRIMARY LUG AND AFT FACE CHAMFER CORRODED. REPAIRED VERTICAL STAB LUG PER ER.SDR GTIA040183Attach Angle · crackedFTW - FOUND RIGHT SIDE DORSAL FIN ATTACH ANGLE CRACKED THROUGH VERTICAL LEG AND INTO 1ST ROW OF FAST ON HORIZONTAL LEG AND GOUGED AND BROKEN FAST. DYE PEN INSPECTION SHOWS NO CRACKS. REMOVED RIGHT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND RSDR GTIA040182Attach Angle · crackedFTW - FOUND LEFT SIDE DORSAL FIN ATTACH ANGLE CRACKED AND GOUGED THROUGH VERTICAL LEG INTO 1ST ROW OF HORIZONTAL. REMOVAL LEFT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND INNER ATTACH ANGLE LEFT SIDE CRACKED SEVERAL PLACES. REMOVED LEFT INNERSDR C2XA04TY006Attach Fitting · gougedDURING A SCHEDULED INSPECTION, GOUGES WERE FOUND ON THE INNER BEARING MATING SURFACES AT THE HORIZONTAL STABILIZER ATTACH POINT. MAINTENANCE ACCOMPLISHED A REAM TO FIRST OVERSIZE REPAIR IAW EC5530-01062, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELESDR SWAA032832Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING FRONT SPAR LEFT AND RIGHT AFT BODY CLEVICES CORRODED. REPAIRED FITTING PER BFG ER.SDR SWAA032655Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB LT ATTACH FITTING AFT BODY LUG CORRODED. REPAIRED LUG PER SRM AND BFG ER.SDR ABXA030464Angle · crackedEXTERIOR SURFACE OF VERTICAL STABILIZER AT FORWARD RIGHT FUSELAGE ATTACH POINT HAD CRACK. REMOVED AND REPLACED VERTICAL ATTACH ANGLE IAW DC-9 SRM.SDR DL73S031028Fitting · corrodedCORROSION DAMAGE WAS FOUND ON THE VERTICAL STAB NR 2 FIN LUG AND THE NR 11 BODY CLEVIS LUG. CORROSION WAS REMOVED AND REWORKED PER ERA 385810-14.SDR ABXA030433Attach Angle · crackedVERTICAL STABILIZER RIGHT ATTACH ANGLE WAS CRACKED AT 99. REPAIRED CRACK ON VERTICAL STABILIZER RIGHT ATTACH ANGLE AND SEAM SEALED IAW DC-9 SRM.SDR 2003FA0001130Bracket · crackedFOUND LT REAR VERTICAL FIN BRACKET CRACKED AT BASE (FITTING).SDR AWXA200301307Fitting · corrodedDURING C-17 CHECK THE VERTICAL STABILIZER RT AFT ATTACH DRAG FITTING AT THE FORWARD FUSELAGE LUG WAS FOUND PITTED. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STABILIZER RT AFT ATTACH DRAG FITTING IAW B737-300 SRM 51-40-02 PG 38 FIG 8 & 12.SDR USAA030178Fitting · corrodedFOUND FITTING CORRODED 2.5 INCHES AROUND, VERT STAB AFT RT OUTBOARD LUG AFT CLEVIS AND T-FITTING. REMOVED AND REPLACED BUSHING/OVERSIZE PER EA 76801. CORROSION LEVEL 1, STAK NR C55-706-11. (M)SDR USAA030184Fitting · corrodedFOUND FITTING CORODED 1 INCH BETWEEN LAYERS, VERT STAB RT AFT OUTBOARD ATTACH POINT BETWEEN T-FITTING AND CLEVIS. OVERSIZED PART, REMOVED AND REPLACED BUSHING PER SRM 55-30-90 AND EA 76801. CORROSION LEVEL 1, TASK NR C55-706-11. (M)SDR USAA030177Fitting · corrodedFOUND FITTING WITH CORROSION AND PITTING .5 INCH, 5-7 O'CLOCK, VERT STAB AFT OUTBOARD LUG FORWARD CLEVIS BETWEEN CLEVIS AND T-FITTING. REMOVED AND REPLACED BUSHING/OVERSIZE PER EA 76801. CORROSION LEVEL 1, TASK NR C55-706-11. (M)SDR USAA030176Fitting · corrodedFOUND FITTING CORRODED AND PITTING 1 INCH, VERTICAL STAB AFT OUTBOARD LUG AFT CLEVIS BETWEEN CLEVIS AND T-FITTING 3-6 O'CLOCK. REMOVED AND REPLACED BUSHING PER EA 76801. (M)SDR USAA030175Fitting · corrodedPIT FOUND FITTING CORRODED 1 INCH LONG INSIDE RADIUS BORE, VERT STAB AFT RT OUTBOARD LUG FWD CLEVIS BETWEEN CLEVIS AND T-FITTING. REMOVED AND REPLACED BUSHING/OVERSIZE PER EA 76801. (M)SDR CA030807007Fitting · cracked(CAN) UPON REMOVAL OF VERTICAL STABILIZER THE REAR DORSAL FIN ATTACH BRACKET WAS FOUND TO BE CRACKED. THE LT RADIUS HAD FAILED BELOW THE FASTNER ATTACHMENT.SDR 2003FA0000853Attach Fitting · crackedON ANNUAL INSPECTION FOUND LEFT VERTICAL FIN ATTACH POINT OUTBOARD EAR BROKEN OFF. ALSO FOUND A STEEL TAPERED SHIM (.018 TO .065) UNDER THE RIGHT THREE OF THE FOUR AFT FIN ATTACH FITTING BOLTS. TECH SUPPORT FOUND NO REF TO ANY SUCH PART. REMOVED SHIM AND RESDR CALA0300416Bushing · corrodedINSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHING CORRODED AT LT O/B AFT LOCATION. THE BUSHING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-52274.SDR CALA0300415Bushing · corrodedINSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT RT I/B FORWARD AND AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED IAW SOPM 20-50-03.SDR CALA0300410Bushing · corrodedINSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT LT I/B FORWARD AND AFT AND RT I/B AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED AND HONED TO SIZE IAW DRAWING NR 65-46872.SDR CALA0300409Bushing · corrodedINSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT LT O/B FORWARD AND AFT AND RT O/B FORWARD AND AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED AND HONED TO SIZE PER DRAWING 65-46872.SDR AUS20030768Adapter · cracked(AUS) FORWARD VERTICAL FIN ATTACHMENT BRACKET CRACKED THROUGH BOLT MOUNTING HOLE.SDR DL73S030479Attach Fitting · corrodedFUSELAGE ATTACH FITTINGS: VERTICAL STABILIZER CLEVIS LUGS - CORROSION. THE NR 11 CLEVIS LUG FWD FACE WAS FOUND GOUGED. THE DAMAGE WAS CLEANED UP USING A SPOTFACE, WITH A MIN REMAINING LUG THICKNESS OF 0.940 INCH IAW DAL ER/A 412535-14, INITIAL RELEASE.SDR ABXA030183Attach Angle · crackedVERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED, LEFT SIDE OF VERTICAL AFT END. REPAIRED ANGLE IAW DC-9 SRM 53-05.SDR ABXA030176Attach Angle · crackedRIGHT AFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS CRACKED. REPAIRED ANGLE IAW DC-9 SRM 53-05.SDR MALA030257Angle · crackedLEFT VERTICAL STABILIZER TO FUSELAGE CLOSING ANGLE CRACKED. MAINTENANCE REPAIRED PER EO A53112.SDR GTIA030272Angle · crackedRIGHT INNER DORSAL FIN ANGLE CRACKED AT FS 1437. REMOVED RIGHT DORSAL FIN INNER ANGLE. LOCATED AND DRILLED NEW DORSAL FIN INNER ANGLE. INSTALLED INNER DORSAL FIN ANGLE. (M)SDR DL733030330Fitting · misalignedVERTICAL STABILIZER REAR TERMINAL FITTING LUGS WERE DETERMINED TO HAVE UNDERGONE PREVIOUS REWORK WHICH LEFT THE LUG THICKNESS LESS THAN BLUEPRINT SPECIFICATIONS AT EACH OF THE FOUR LUGS. AREA INSPECTED AND NEW BUSHINGS WERE FABRICATED PER DAL ER/A 384672-14 TSDR GTIA030227Angle · crackedFTW - FOUND DORSAL FIN AT BOTH LT AND RT SIDE CRACKED. REMOVED BOTH LT AND RT SIDE. LOCATED AND DRILLED ANGLE 5912188036. INSTALLED ANGLE P/N 5912158036. FABRICATED LOCATED AND DRILLED NEW 5910242-121. INSTALLED NEW 5910242-121. (M)SDR GTIA030202Angle · crackedFTW - FOUND RIGHT DORSAL FIN ATTACH ANGLE INNER ANGLE CRACKED IN RADIUS. REMOVED RIGHT DORSAL FIN ATTACHED INNER ANGLE. DRILL AND LOCATE NEW INNER ANGLE. INSTALLED NEW INNER ANGLE. UPON REMOVAL OF RIGHT DORSAL FIN ANGLE FOUND LEFT GUSSET TO BE CRACKED. RESDR DL733030146Fitting · corrodedCORROSION WAS FOUND IN THE BORES OF BOTH THE REAR SPAR LT AND RT PRIMARY AND FAIL-SAFE FIN LUGS. THE BORES WERE ENLARGED TO REMOVE CORROSION. ALSO, THE FORWARD FACE OF THE LHS PRIMARY FIN LUG WAS SPOTFACED TO REMOVE CORROSION. REPAIR BUSHINGS WERE INSTALLEDSDR DHL2003804894Angle · corrodedVERT STAB AND RT FUSE- ATTACHING ANGLE CORRODED BETWEEN STA 1766.000 - STA 1800.382 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 PG 44A-44B, FIG 16A. REMOVED CORROSION ON ANGLE IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUTSDR DHL2003804892Angle · corrodedCORROSION ON JOINT ANGLE BETWEEN FUSELAGE AND VERTICAL STABILIZER, STA 1766.000, L-3L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 PG 44A-44B FIG 16A. REMOVED CORROSION ON ANGLE IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUSDR COMA0360058Bushing · looseDURING LUBRICATION OF HORIZONTAL STABILIZER PIVOT POINT, THE VERTICAL STABILIZER RT FITTING WAS FOUND TO HAVE BUSHING MIGRATED.PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED BUSHING ON VERTICAL STABILIZER RT FITTING, FABRICATED BUSHING PN 601R55310025 FROM BUSHSDR 2003F00454Fitting · corrodedAT C-CHECK, FOUND VERTICAL STAB AT FIN STATION 316, HORIZONTAL STAB HINGE FITTING BEARING HOLE, RIGHT SIDE HAS CORROSION ON INSIDE DIAMETER. REWORKED VERTICAL STAB HORIZONTAL STAB HINGE FITTING BEARING HOLE AT RIGHT SIDE AND INSTALLED NEW BEARING. (M)SDR 2003F00453Fitting · corrodedAT C-CHECK, FOUND VERTICAL STAB AT FIN STATION 316, HORIZONTAL STAB HINGE FITTING BEARING HOLE, LT SIDE, HAS CORROSION ON INSIDE DIAMETER. REWORK VERTICAL STAB, HORIZONTAL STAB HINGE FITTING BEARING HOLE AT LEFT SIDE AND INSTALLED NEW BEARING. (M)SDR SWAA030126Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL FIN LT FWD, RT FWD AND RT AFT CLEVIS LUG FACES CORRODED. REPAIRED THE VERTICAL FIN LUG FACES PER SWA ER.SDR DL733030066Fitting · corrodedCORROSION WAS FOUND ON THE AFT FACE OF THE RT REAR SPAR PRIMARY FITTING LUG. THE AFT SIDE OF THE LUG WAS SPOT FACED .005 INCH TO REMOVE THE CORROSION. A REPAIR BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR GTIA030005Attach Angle · crackedFTW - FOUND LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE CRACKED, APPROXIMATELY 1 INCH. REMOVED LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE. NEW FORMED ANGLE. INSTALLED LEFT VERTICAL DORSAL FIN, INNER ATTACH ANGLE. (M)SDR ASOA02645Angle · crackedDURING HANGAR INSPECTION IN MCN, THE VERTICAL STABILIZER RIGHT ATTACH ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT ATTACH ANGLE IAW ASA EO120-55-0009. (M)
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