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 UPS07850539Stiffener · corrodedINSPECTION TYPE:C2 SMALL HORIZ STIFFENER CORRODED/EXFOLIATED INSIDE VERT STAB REAR SPAR, THROUGH ACCESS PNL 55. REMOVED DAMAGED STIFFENER ON VERT STAB INSIDE ACCESS PNL 55 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPAIR STIFFENER IAW SRM 51-01-21 AND DWG 5SDR DLM90071013Hinge · corrodedVERT TO HORIZ STAB RT O/B HINGE PLATES HAS CORROSION ON I/B AND O/B SURFACES AND PITTING CORROSION IN BORES. REPAIRED RT O/B HINGE PLATE IAW MD-90 SRM 55-30-05 PARA 5.SDR C2XA07TY038Hinge Bracket · out of limitsTYS - DURING A CURRENT C-CHECK INSPECTION THE VERTICAL STAB HINGE FITTING SPHERICAL BEARING HOUSING ON THE LT AND RT WERE OUT OF LIMITS. MAINTENANCE REAMED BOTH SIDES OF VERTICAL STAB AND REPLACED NEW BUSHINGS IAW EMB 145 SRM 55-30-02. ALL WORK WAS ACCOMPLISSDR DLM90070760Attach Fitting · corrodedRT I/B VERTICAL STAB TO HORIZONTAL ATTACH PLATE HAS CORROSION ON PLATE FACE AND BORE. REPAIRED RT I/B VERTICAL STAB TO HORIZONTAL HINGE IAW MD90 SRM 55-30-05 PAR 5.SDR DLM88070675Access Panel · corrodedCORROSION ON ACCESS 6301A VERTICAL STAB L/E. REPAIRED IAW SRM 51-30-1, NR T0056168.SDR 07FDEA01822Stiffener · crackedANGLE CRACKED ON THE VERTICAL STAB LEADING EDGE WEB LOCATED ON THE UPPER RIGHT ON THE AFT SIDE OF WEB AND THE UPPER STAB BULKHEAD REMOVED AND REPLACED STIFFENER ANGLE ON VERTICAL STAB. REFERENCE SRM 51-30-02, PG 3.SDR QXEA200700811Hinge Bracket · chafedC4 PDX - LOWER HINGE BRACKET ON VERTICAL STAB HAS A CHAFED AREA WHERE THE FORE RUDDER LINK ATTACHES. REPAIRED IAW RD8/4-55-335 AND SRM 51-14-01, 51-26-10.SDR QXEA200700812Hinge Bracket · chafedC4 PDX - UPPER HINGE BRACKET ON VERTICAL STAB HAS A CHAFED AREA WHERE FORE RUDDER ATTACHES. REPAIRED IAW RD8-4-55-331/3.SDR 07FDEA01723Web · crackedVERTICAL STAB ELEVATOR FEEL CONTROL UNIT PLATFORM ASSY FWD LT VERTICAL WEB CRACKED ON INTERNAL SIDE AT THE 2 MOST FWD LWR FASTENERS. REPLACED LT VERTICAL WEB ON VERT STAB ELEVATOR FEEL CONTROL UNIT PLATFORM. REF SRM 51-30-2 PG 1-12.SDR AWXA200700546Hinge Fitting · wornCREW REPORTED CLIMBING THROUGH FL 220 AT 340 KTS A/C VIBRATION FELT ON THE HORIZONTAL AXIS. MX REPLACED THE RUDDER HINGE ARM FITTINGS: NR 1, NR 2, NR 3, NR 4, NR 5, AND NR 7. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR N93A19042007Angle · crackedDURING 5000 LANDING INSPECTION MAINTENANCE FOUND 793 BULKHEAD CAP ANGLE CRACKED.SDR DL738070506Beam · damagedTHE VERTICAL STABILIZER LT TRAILING EDGE BEAM HAS TWO HOLES MISDRILLED. THE DAMAGED HOLES WERE OVERSIZED.SDR DJFA2007040Bracket · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A SMALL CRACK ON THE RIB SUPPORT BRACKET FOR A RIB IN THE VERTICAL STABILIZER. THE CRACK WAS APPROX .25 INCH LONG TRANSECTING A NUTPLATE RIVET. MAINTENANCE IS REPLACING THE BRACKET. MAINTENANCE FABRICATESDR QXEA200700408Bracket · missingC4 PDX - INTERIOR OF VERTICAL STABILIZER LEADING EDGE UNDER PANEL 321CL. THE BRACKET FOR THE HOT AIR DUCTING IS MISSING A FASTENER. REPAIRED IAW RD8-55-1813.SDR 07FDEA00955Attach Fitting · damagedV/S TAPERED ATTACH FITTINGS LT REAR, RT REAR AND RT CENTER BRONZE PLATING MISSING. PARTS REPLACED IAW AMM 55-30-11/401, P/N A555-72151-000-00 (1 EA.) AND P/N A555-72201-000- 00 (2 EA.)SDR DALA1104281401Barrel Nut · missingJOINT BARREL NUT /BOLT ASSY OF VERTICAL FIN MISSING, REPLACED IAW EA 01-074297-12, ME05.SDR ABXA070033Fitting · crackedRIGHT KEEL BEAM CLOSE-OUT PANEL STRUCTURE, FORWARD LOWER FITTING, CRACKED ON INTERIOR SECTION. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-3 AND 51-30-1.SDR 3002009512280Structure · damagedBIRD STRIKE HIT LT HORZ STAB AND VERTICAL STAB, LEADING EDGE FOR THE LT STAB, LEADING EDGE ACCESS PANEL, UPPER AND LOWER HORSE COLLAR DAMAGED. NO DAMAGE FOUND TO STAB ACTUATOR. FOUND BIRD PARTS INSIDE PANELS.SDR TRAX200601139Drag Angle · crackedLT SIDE VERTICAL STAB TO FUSELAGE DRAG ANGLE HAS POSSILBLE CRACK (MARKED).SDR QXEA200603321Attach Fitting · crackedYYC C3 - VERTICAL STAB LOWER LEFT SIDE, FUSELATE TO STAB ATTACH CHORD HAS SUSPECT CRACK IN RADIUS AFT END BELOW REAR SPAR. REPAIRED IAW REO 670-55-31-013.SDR QXEA200603320Attach Angle · looseYYC C3 - VERTICAL STAB HAS AREA OF LOOSE RIVETS ON RIGHT SIDE, LOWER ATTACH ANGLE BELOW RUDDER. REPAIRED IAW CRJ 700 SRM 51-42-10-001-001-A01.SDR QXEA200603319Attach Angle · looseYYC C3 - VERTICAL STAB HAS 3 LOOSE RIVETS ON LEFT SIDE LOWER ATTACH ANGLE BELOW RUDDER. REPAIRED IAW CRJ700 SRM 51-42-10-001-001-A01, 51-21-11-001-001-A012 AND 51-25-01-001-001-A01.SDR 2006FA0001188Rivet · looseDURING THE PRE-FLIGHT INSPECTION FOR A LOCAL TRAINING FLIGHT, THE BLIND RIVETS LOCATED HALFWAY UP VERTICAL FIN WERE FOUND TO BE MAKING ALUMINUM OXIDE (DIRT TRAILS) ON BOTH SIDES OF THE VERTICAL FIN. THIS CONDITION IS INDICATIVE OF A POTENTIALLY LOOSE RIVET ORSDR QXEA200603143Support Beam · corrodedC4 PDX - AVIONICS RACK VERTICAL SUPPORT BEAM AT STATION X202 AND STRINGER 31L HAS CORROSION ON FORWARD SIDE AT BASE. REPAIRED IAW SRM 51-40-00, 51-20-00, AND 51-20-11.SDR SWAA064321Beam · crackedDURING SCHEDULED 18Y CHECK, FOUND VERTICAL STAB RIGHT LOWER MID T/E BEAM CRACKED AT LOWER SECTION. REMOVED AND REPLACED STAB LOWER MID T/E BEAM SECTION PER SRM.SDR QXEA200603458Access Panel · crackedC3 PDX - SUSPECT CRACK ON WEB IN LEFT FORWARD CORNER OF BACK UP STRUCTURE FOR FORWARD VERTICAL STAB INTERNAL ACCESS PANEL. REPAIRED IAW SRM 51-40-07, 51-42-05.SDR USAA061262Skate Angle · wornVERTICAL STAB FWD END OF SKATE ANGLE HAS WEAR. FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-10-02, DEFECT SIZE: 1 X 2 INCHES.SDR 06FDEA03483Angle · crackedFOUND VERTICAL STAB, CRACK IN ANGLE, ATTACHED TO UNDER SIDE OF STR 11R, 4" AFT OF TOP OF 1342 BULKHEAD. REMOVED CRACKED ANGLE AT FIN STA. 13.746 UNDER STR 11R, 4" AFT OF BS 1342 BULKHEAD, FABRICATED REPLACEMENT ANGLE FROM .040" 7075-T6 LOT #694306 PER DWG 6SDR 06FDEA03481Bulkhead · crackedFOUND VERTICAL STAB, CRACK IN WEB 3" BELOW STR 11L, 8" AFT OF TOP OF 1342 BULKHEAD. BULKHEAD REMOVED, FABRICATED AND INSTALLED WEB PER SRM 51-30-02SDR MWEA060203Doubler · chafedVERTICAL STABILIZER LEFT SIDE IS CHAFED JUST ABOVE HORIZONTAL STABILIZER. FABRICATED AND INSTALLED DOUBLER.SDR QXEA200602522Hinge · gougedC4 YYC - VERTICAL STAB CENTER HINGE FITTING LOWER HAS GOUGE ON LEFT HAND SIDE OF FORE RUDDER ATTACH. REPAIRED IAW RD8-55-1749, SRM 51-20-11, 51-20-16, 51-20-36.SDR QXEA200602536Bolt · shearedC4 YYC - BLEED AIR PIPE MOUNT PYLON ASSY, FORWARD ANGLE CRACKED AND 2 MOUNT BOLTS SHEARED. REPAIRED IAW SRM 51-40-11, AND EA 2-55-145, AND RD8-55-1747.SDR QXEA200602519Hinge · wornC4 YYC - FORE RUDDER TRAILING EDGE LOWER MAIN HINGE IS WORN AROUND TOP BUSHING HOLE. REPAIRED IAW RD8-55-1128.SDR QXEA200602523Hinge Fitting · wornC4 YYC - VERTICAL STAB LOWER HINGE FITTING HAS WEAR AROUND FORE RUDDER ATTACH HOLE. REPAIRED IAW RD8-55-752.SDR CALA0600330Fitting · corrodedINSPECTION FOUND LEFT AFT FWD, RIGHT AFT FWD, AND RIGHT AFT O/B VERTICAL STABILIZER DRAG ANGLE FITTINGS CORRODED AT STA 1088, S2L AND S2R. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-73744.SDR 06FDEA2494Shear Plate · misdrilledFOUND VERT FIN, LT UPPER SHEAR PLATE TO HAVE 3 "SNOWMAN" HOLES. REMOVED AND REPLACED VERT FIN LT UPPER SHEAR PLATE IAW SRM 51-30-2, 51-30-5SDR CA060707005Fitting · corroded(CAN) DURING 100 HOUR INSPECTION AME FOUND WHAT APPEARED TO BE A CRACK IN THE RADIUS OF THE LT FLANGE OF THE LT FITTING ATTACHING THE VERTICAL FIN TO THE HORIZONTAL STABILIZER. WHEN THE PART WAS REMOVED FROM THE AIRCRAFT THE LT FLANGE WAS FOUND TO BE BENT TOWSDR 1264060606Angle · crackedDURING 5000 LDG INSPECTION FOUND 793 BULKHEAD CAP ANGLE CRACKED AT UPPER VERT STAB ATTACH BOLT HOLES.SDR QXEA200601322Hinge · wornYYC - C4 VERTICAL STAB TOP SAFETY HINGE FOR THE FORE RUDDER ATTACHMENT HAS DEEP WEAR MARK ON TOP SURFACE. REPAIRED IAW RD8-57-752.SDR C2XA06TY026Housing · gougedLT VERT STAB SPHERICAL BEARING HOUSING GOUGED. REAMED RT AND LT HOUSING AND INSTALLED BEARINGS IAW COEX EC5510-01138.SDR 06FDEA1637Rib · gougedN00638, WHILE WORKING CARD NR 73C023-00 (TAIL 43). FOUND VERT FIN TENSION TIE RIB. RT AFT VERT BOLT HOLE HAS GOUGE. REPAIRED BOLT HOLE PER FED EX EA 7-5530-100866.SDR 06FDEA1561Tie · corrodedFOUND RT FWD HORIZONTAL TENSION TIE O/B FITTING LUG, O/B FACE IS CORRODED. REPAIRED PER EA 7-5530-96626.SDR C2XA06SH050Hinge Fitting · corrodedSHV - MAJOR - DURING C-CHECK THE RIGHT VERTICAL STABILIZER BEARING HOUSING WAS FOUND TO BE SCRATCHED AND CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA BY OVERSIZING THE HOUSING TO 58.000 (-0, +0.030) MM IAW EC 5510-0117. THE AIRCRAFT WAS APPROVED FOR RETURNSDR C2XA06SH049Hinge Fitting · corrodedSHV - MAJOR - DURING C-CHECK THE LEFT VERTICAL STABILIZER BEARING HOUSING WAS FOUND TO BE SCRATCHED AND CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA BY OVERSIZING THE HOUSING TO 58.000 (-0, +0.30) MM IAW EC5510-01117. THE AIRCRAFT WAS APPROVED FOR RETURN TSDR USAA060556Skate Angle · wornRT VERT STAB SKATE ANGLE HAS WEAR. REMOVED DAMAGE, INSTALLED FABRICATED REPAIR PARTS IAW TR 53-20-05, DEFECT SIZE: 3 X 1 INCH.SDR USAA060555Skate Angle · wornRT VERT STAB SKATE ANGLE WEAR. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW TR 53-20-05, DEFECT SIZE: 3 X 1 INCH.SDR 06FDEA1296Attach Fitting · corrodedVERTICAL LEADING EDGE LOWER LEFT ATTACH FITTING HAS CORROSION REF N00327. REPAIRED FITTING IAW EA 6-5530-99020.SDR 06FDEA1294Access Panel · damagedVERTICAL STAB L/E FRONT SPAR ACCESS PNL ON RT SIDE HAS 2 HOLES DOUBLE DRILLED. COMPLIED WITH EA 6-5530-97607 PART 1.SDR 2006UALA00622Bushing · damagedFOUND VERTICAL STAB LT PRIMARY FWD LUG BUSHING SPUN WHILE MACHINING. DAMAGE REMOVED AND A NEW REPAIR BUSHING WAS INSTALLED PER AAR EA I060151. RESULTING BORE SIZE WAS 1.6048 IN.SDR IXXA06SMN101SVent · crackedDURING ROUTINE C-CHECK INSPECTION, REMOVED THE FWD BUFFET VENT TRIMMER VALVE AND PLUG OUTLET ON FUSELAGE. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7. REMOVED FWD BUFFET VENT TRIMMER VALVE IAW DC-8 MM 38-20-11 PAGES 201-202. REMOVED EXISTING INTERNAL DO
Back to JASC 5530