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.

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 5Aug 14, 2007 · N801UP · Doug DC873FSDR 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.Aug 2, 2007 · N907DA · Doug MD9030SDR 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 ACCOMPLISJul 18, 2007 · N11535 · Emb EMB145LRSDR 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.Jun 3, 2007 · N906DA · Doug MD900SDR DLM88070675Access Panel · corrodedCORROSION ON ACCESS 6301A VERTICAL STAB L/E. REPAIRED IAW SRM 51-30-1, NR T0056168.May 29, 2007 · N946DL · Doug MD88SDR 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.May 15, 2007 · N210FE · Boeing 7272S2FSDR 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.May 12, 2007 · N402QX · Bombdr DHC8402SDR 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.May 11, 2007 · N402QX · Bombdr DHC8402SDR 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.May 9, 2007 · N210FE · Boeing 7272S2FSDR 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.Apr 29, 2007 · N626AW · Airbus A320231SDR N93A19042007Angle · crackedDURING 5000 LANDING INSPECTION MAINTENANCE FOUND 793 BULKHEAD CAP ANGLE CRACKED.Apr 19, 2007 · N493QS · Gulstm GIVSDR DL738070506Beam · damagedTHE VERTICAL STABILIZER LT TRAILING EDGE BEAM HAS TWO HOLES MISDRILLED. THE DAMAGED HOLES WERE OVERSIZED.Apr 10, 2007 · N373DA · Boeing 737832SDR 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 FABRICATEMar 30, 2007 · N789TA · Beech 400ASDR 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.Mar 18, 2007 · N367PH · Dhav DHC8202SDR 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.)Mar 16, 2007 · N816FD · Airbus A310304SDR DALA1104281401Barrel Nut · missingJOINT BARREL NUT /BOLT ASSY OF VERTICAL FIN MISSING, REPLACED IAW EA 01-074297-12, ME05.Mar 2, 2007 · N140LL · Boeing 767332SDR 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.Jan 25, 2007 · N229DE · Doug DC915FSDR 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.Dec 28, 2006 · N524FX · Bombdr BD1001A10SDR TRAX200601139Drag Angle · crackedLT SIDE VERTICAL STAB TO FUSELAGE DRAG ANGLE HAS POSSILBLE CRACK (MARKED).Dec 14, 2006 · N723EV · Cndair CL6002C10SDR 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.Dec 12, 2006 · N614QX · Cndair CL6002C10SDR 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.Dec 9, 2006 · N614QX · Cndair CL6002C10SDR 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.Dec 8, 2006 · N614QX · Cndair CL6002C10SDR 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 ORDec 2, 2006 · N557J · Socata TB9SDR 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.Nov 14, 2006 · N361PH · Dhav DHC8202SDR 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.Nov 9, 2006 · N342SW · Boeing 7373H4SDR 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.Oct 31, 2006 · N413QX · Bombdr DHC8402SDR 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.Oct 25, 2006 · N406US · Boeing 737401SDR 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 6Sep 29, 2006 · N285FE · Boeing 727233SDR 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 51-30-02Sep 29, 2006 · N285FE · Boeing 727233SDR MWEA060203Doubler · chafedVERTICAL STABILIZER LEFT SIDE IS CHAFED JUST ABOVE HORIZONTAL STABILIZER. FABRICATED AND INSTALLED DOUBLER.Sep 18, 2006 · N814ME · Doug DC981SDR 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.Sep 12, 2006 · N357PH · Dhav DHC8202SDR 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.Sep 9, 2006 · N357PH · Dhav DHC8202SDR QXEA200602519Hinge · wornC4 YYC - FORE RUDDER TRAILING EDGE LOWER MAIN HINGE IS WORN AROUND TOP BUSHING HOLE. REPAIRED IAW RD8-55-1128.Sep 8, 2006 · N357PH · Dhav DHC8202SDR QXEA200602523Hinge Fitting · wornC4 YYC - VERTICAL STAB LOWER HINGE FITTING HAS WEAR AROUND FORE RUDDER ATTACH HOLE. REPAIRED IAW RD8-55-752.Sep 7, 2006 · N357PH · Dhav DHC8202SDR 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.Sep 3, 2006 · N61304 · Boeing 7373T0SDR 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, 51-30-5Jul 10, 2006 · N281FE · Boeing 727233SDR 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 TOWJul 4, 2006 · Cessna 150MSDR 1264060606Angle · crackedDURING 5000 LDG INSPECTION FOUND 793 BULKHEAD CAP ANGLE CRACKED AT UPPER VERT STAB ATTACH BOLT HOLES.Jun 6, 2006 · N464QS · Gulstm GIVSDR 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.May 8, 2006 · N355PH · Dhav DHC8202SDR C2XA06TY026Housing · gougedLT VERT STAB SPHERICAL BEARING HOUSING GOUGED. REAMED RT AND LT HOUSING AND INSTALLED BEARINGS IAW COEX EC5510-01138.May 1, 2006 · N11121 · Emb EMB145XRSDR 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.Apr 29, 2006 · N493FE · Boeing 727200SDR 06FDEA1561Tie · corrodedFOUND RT FWD HORIZONTAL TENSION TIE O/B FITTING LUG, O/B FACE IS CORRODED. REPAIRED PER EA 7-5530-96626.Apr 20, 2006 · N485FE · Boeing 727200SDR 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 RETURNApr 20, 2006 · N14116 · Emb EMB145XRSDR 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 TApr 20, 2006 · N14116 · Emb EMB145XRSDR 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.Apr 3, 2006 · N777AU · Boeing 7374B7SDR 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.Apr 3, 2006 · N777AU · Boeing 7374B7SDR 06FDEA1296Attach Fitting · corrodedVERTICAL LEADING EDGE LOWER LEFT ATTACH FITTING HAS CORROSION REF N00327. REPAIRED FITTING IAW EA 6-5530-99020.Apr 3, 2006 · N455FE · Airbus A310222SDR 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.Apr 3, 2006 · N455FE · Airbus A310322SDR 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.Mar 30, 2006 · N929UA · Boeing 737522SDR 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 DOMar 24, 2006 · N722CX · Doug DC872
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