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 QXEA0101223Flange · scratchedPDX-LEFT HAND STABILIZER FORWARD SPAR UPPER FLANGE HAS TOOL SCRATCH NEAR RIB 8, STATION YH77.500. REPAIRED IAW DHC-8 RD8-55-626.Jul 17, 2001 · N375PH · Dhav DHC8202SDR QXEA0101222Structure · gougedPDX-THREE TOOLING GOUGES ON LOWER RIGHT HAND VERTICAL STABILIZER LEADING EDGE MOUNTING FLANGE. REPAIRED IAW DHC-8 RD8-55-584.Jul 17, 2001 · N375PH · Dhav DHC8202SDR QXEA0101205Flange · tool damagePDX-SEVERAL TOOLING GOUGES AND SCRATCHES ON LEFT HAND VERTICAL STABILIZER LEADING EDGE MOUNT FLANGE. REPAIRED IAW DHC-8 RD8-55-584.Jul 17, 2001 · N375PH · Dhav DHC8202SDR QXEA011205Flange · gougedPDX-SEVERAL TOOLING GOUGES AND SCRATCHES ON LEFT HAND VERTICAL STABILIZER LEAD EDGE MOUNT FLANGE. REPAIRED IAW DHC-8 RD8-55-584.Jul 17, 2001 · N375PH · Dhav DHC8202SDR 01FDEA00598Structure · chafedCHAFE AT VERT STAB L/E RIGHT FRONT SPAR FIN BS 55.8 TO 47.0 O/B SIDE.Jul 17, 2001 · N236FE · Boeing 727247SDR QXEA0101283Structure · crackedYYC-RUDDER COVE CRACKED ON VERTICAL STABILIZER AT RIB 3.4. REPAIRED IAW FOKKER SRM 51-00-03, PAGE 17, SRM 55-31-01, PAGE 2, AND SRM 51-31-01, PAGE 7.Jul 7, 2001 · N487US · Fokker F28MK4000SDR QXEA0101141Structure · crackedPDX - SMALL CRACK FOUND IN SHEET METAL ON RIGHT SIDE OF FORE RUDDER CENTER HINGE AREA. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1.Jul 3, 2001 · N348PH · Dhav DHC8202SDR T212003F00000Structure · crackedAT DAILY INSPECTION CHECK, CRACKS WERE FOUND, THROUGH INSPECTION PLATE, AT TOP OF VERTICAL FIN. CRACK ABOUT 1.5 INCH LONG ON NOSE RIB (PN105-3040120/ 1053041415), WHERE THE TAIL ROTOR GEAR BOX ATTACHED, ALSO RIVET MISSING. PROBABLE CAUSE, VIBRATION.Jun 22, 2001 · N727WW · Bolkms BO105LSA3SDR DL72W011020Skin · crackedLWR END OF VERT STAB SKIN CRACKED R/H SIDE STA 1342 REPAIR PER M/M 55-30-000-8 FIG 801Jun 20, 2001 · N293WA · Boeing 727247SDR OLJ2001F00000Stud · departedRIGHT HAND VERTICAL FIN DEPARTED AIRCRAFT DURING FLIGHT. CAUSE: FATIGUE ON ONE STUD LEADING TO FAILURE OF OTHER STUDS.Jun 14, 2001 · N896LL · Aerosp SA365N1SDR 2001FA0000098Rib · brokenUPPER RUDDER RIB WAS FOUND BROKEN AT THE OPENING FOR UPPER HINGE BOLT INSTALLATION ACCESS. THIS TYPE OF DAMAGE IS A REOCCURRING PROBLEM DUE TO A LACK OF PROPER GUST LOCKS FOR THE RUDDERS, WIND SLAPPING OF THE RUDDER WITH THE ARM OF THE BALANCE WEIGHT CAUSING Jun 6, 2001 · N5838A · Cessna 172SDR 2001FA0000091Fitting · crackedDURING ROUTINE 100 HR INSPECTION, MINOR CORROSION WS FOUND ON BOTH LEFT AND RIGHT VERTICAL STABILIZER ATTACH FITTINGS, APPROX BS 200.4. UPON REMOVAL OF CORROSION, A CRACK WS FOUND IN THE RADIUS OF THE RIGHT FITTING APPROXIMENTLY .7500 OF THE WAY ACROSS AND APPMay 25, 2001 · N714TD · Cessna 152SDR UPS01235908Web · crackedINSPECTION TYPE:C STRUCTURE ABOVE NR 2 ENGINE, WEB CRACKED AT BS 1388 APPROX RT SIDE. NEW WEB INSTALLED IAW SRM 51-30-02 & BOEING DRAWING 65-17555.May 11, 2001 · N906UP · Boeing 72730CSDR AALA20011156Plate · corrodedTUL - FOUND 4 INCH BY 4 INCH CORROSION ON ALL 4 VERTICAL STABILIZER HINGE PLATES FOR HORIZONTAL STABILIZER. REMOVED PLATES AND REPLACED SRM 51-01. (M)May 8, 2001 · N3515 · Doug DC982SDR USAA010505Fitting · crackedSJO - FOUND HINGE RIB FITTING CRACKED .75 INCH, VERT FS 23.27. DAMAGE REMOVED. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE PER EA 70830. (M)May 7, 2001 · N270AU · Boeing 7372B7SDR QXEA0100768Rivet · looseYYC - VERTICAL STABILIZER LEFT-HAND SIDE ABOVE TAIL CONE HAS LOOSE RIVETS. INSTALLED FASTENERS IAW FOKKER SRM 51-32-04 AND HORIZON AIR EA 4-55-289.May 6, 2001 · N486US · Fokker F28MK4000SDR GAIA01166STStringer · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE LEFT VERTICAL STABILIZER INTERIOR STRINGER 3RD BAY DOWN FROM PANEL 9504 IS CRACKED. ACCOMPLISHED VERTICAL STAB STRINGER REPAIR STRINGER 8L FIN STATION 60 IAW B727 SRM 55-30-4 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223SDR COMA0160366Bushing · scoredLEFT AND RIGHT VERTICAL STABILIZER BUSHINGS ARE MIGRATED. REMOVED AND REPLACED LT AND RT VERTICAL STABILIZER BUSHINGS IAW WVAC EO 601R-55-2429.Apr 30, 2001 · N929CA · Cndair CL6002B19SDR ZW0A0100814Attach Angle · crackedDURING CHECK-C MAINT THE DORSAL FIN ATTACH ANGLE WAS CRACKED ON LT SIDE, STA 1405 TO 1427. REPLACED ATTACH ANGLE WITH NEW. INSTALLED RIVETS PER SRM 51-30-2.Apr 25, 2001 · N904TW · Doug DC982SDR RRXA11012Tab · debondedDURING A MAINTENANCE VISIT FOUND DEBONDED DAMAGE TO LH ELEVATOR IB CORNER OF GEARED TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-9A, DC-8 MM 27-30-3.Apr 23, 2001 · N602AL · Doug DC873FSDR 2001UALA00441Fitting · corrodedVERTICAL STABILIZER ATTACH POINT LEFT HAND FORWARD FAIL SAFE LUG IS CORRODED. LUG WAS REAMED TO REMOVE CORROSION AND THE BUSHING WAS REPLACED. MAJOR REPAIR ACCOMPLISHED.Apr 7, 2001 · N311UA · Boeing 737322SDR 2001UALA00440Fitting · corrodedVERTICAL STABILIZER ATTACH POINT LEFT HAND FAIL SAFE LUG ON FUSELAGE SIDE IS CORRODED. LUG REAMED TO REMOVE CORROSION AND A BUSHING WAS MANUFACTURED AND INSTALLED. MAJOR REPAIR ACCOMPLISHED.Apr 7, 2001 · N311UA · Boeing 737322SDR 2001UALA00439Fitting · corrodedVERTICAL STABILIZER LEFT HAND ATTACH LUGS ARE CORRODED. LUGS WERE REAMED TO REMOVE CORROSION AND BUSHINGS WERE MANUFACTURED AND INSTALLED. MAJOR REPAIR ACCOMPLISHED.Apr 7, 2001 · N311UA · Boeing 737322SDR 2001UALA00438Fitting · corrodedVERTICAL STABILIZER RIGHT HAND ATTACH LUGS ARE CORRODED. BUSHINGS REMOVED AND FITTINGS WERE REAMED TO REMOVE THE CORROSION. MAJOR REPAIR ACCOMPLISHED.Apr 7, 2001 · N311UA · Boeing 737322SDR 2001UALA00437Fitting · corrodedVERTICAL STABILIZER RIGHT HAND REAR ATTACH FITTING AFT FAIL SAFE LUG IS CORRODED. FAIL SAFE LUG BORE REAMED AND BUSHING INSTALLED. MAJOR REPAIR ACCOMPLISHED.Apr 7, 2001 · N311UA · Boeing 737322SDR 2001UALA00436Fitting · corrodedVERTICAL STABILIZER RIGHT HAND FORWARD FAIL SAFE LUG IS CORRODED. BORE OF FAIL SAFE LUG REAMED AND BUSHING INSTALLED. MAJOR REPAIR ACCOMPLISHED.Apr 7, 2001 · N311UA · Boeing 737322SDR QXEA0100611Angle · crackedYYC- CRACKED ANGLE ON VERTICAL STAB ABOVE RIB 3 AND 2 BELOW RUDDER. REPAIRED IAW FOKKER SRM 55-31-04 AND 51-31-01.Apr 5, 2001 · N493US · Fokker F28MK4000SDR AALA20010724Hinge Fitting · corrodedTUL - FOUND TWO RIGHT OUTBOARD, TWO RIGHT INBOARD, TWO LEFT OUTBOARD, TWO LEFT INBOARD VERTICAL STABILIZER HINGE PLATES CORRODED. REMOVED AND REPLACED 2 RIGHT OUTBOARD, 2 RIGHT INBOARD, 2 LEFT OUTBOARD, 2 LEFT INBOARD VERTICAL STABILIZER HINGE PLATES PER SRM Apr 3, 2001 · N7514A · Doug DC982SDR UPS01235559Hinge · crackedINSPECTION TYPE: C & SI, UPPER RUDDER HINGE SUPPORT FITTING IN VERT STAB HAS SUSPECT CRACK AL ONG LH FLANGE AT FWD END. REPLACED RUDDER HINGE SUPPORT FITTING IAW SMRO EO 2001-010-003 UPS ENGINEERING FILE 727-27-20001Mar 27, 2001 · N926UP · Boeing 72731CSDR CA010504007Fitting · corroded(CAN) DURING MID-LIFE STRUCTURAL INSPECTION THE ABOVE CLEAT WAS FOUND TO BE EXFOLIATED IN VARIOUS SPOTS BETWEEN THE WEBS. IT IS LIKELY THAT STANDING WATER COULD SIT IN THE WEB AREAS AND SPEED UP THE CORROSION PROCESS. THE VERTICAL STAB WAS REMOVED TO OBTAIN ACMar 23, 2001 · Stbros SD360SDR COMA0160335Bushing · wornLEFT VERTICAL STAB PIVOT POINT BUSHING WORN. REMOVED AND REPLACED BUSHING IAW CRJ AMM 20-26-00-910-803, REAMED BUSHING IAW CRJ DRAWING 600-21061. MACHINED FLANGE IAW WVAC EO 601R-55-2325.Mar 23, 2001 · N797CA · Cndair CL6002B19SDR EIA2001120Structure · corrodedMZJ-EAC - FOUND VERTICAL STAB INTERIOR CORROSION ON FORWARD FLANGE OF T-CHORD AT FIN STATION 570 RIGHT. FABRICATED AND INSTALLED CHORD PER B747 SRM 51-30-02 AND 51-10-02. (M)Mar 21, 2001 · N3203Y · Boeing 747128SDR CA010323005Adapter · failed(CAN) LOWER LT MOUNTING / MATING SURFACE INCORRECTLY MACHINED. SURFACE WAS MACHINED CYLINDRICALLY INSTEAD OF SPHERICAL CONVEX. IF INSTALLED THE MATING SURFACES WOULD NOT MATCH CAUSING STRESS AND POSSIBLE FAILURE OF THE MOUNT. CONCERNED THAT MORE WERE PRODUCED Mar 14, 2001 · Dhav DHC6SDR ABXA010091Attach Angle · crackedA CRACK WAS FOUND ON RIGHT SIDE OF VERTICAL STABILIZER, STABILIZER TO FUSELAGE ATTACH ANGLE. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED ATTACH ANGLE IAW ABX REA D953-40145.Mar 12, 2001 · N987AX · Doug DC932SDR DHL2001806533Angle · crackedC-CHECK - VERT. STAB. LE INNER RIB REINFORCING ANGLE CRACKED 1/2 INCH ZF 86.000 RT. REMOVED CRACK REINFORCING ANGLE IAW SRM 51-1-21 PAGE 1. FABRICATED ANGLE IAW SRM 55-1-1 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 5-1-8B. INSTALLED ANGLE IAW SRM 51-1-21 PAGMar 10, 2001 · N806DH · Doug DC873FSDR 01FDEA00188Fitting · corrodedTRANSVERSE LOAD FITTING HAS INTERGRANULAR CORROSION, TOP LT AND RT ATTACH POINT TO FWD VERTICAL STAB FRONT SPAR.Feb 28, 2001 · N442FE · Airbus A310203SDR UPS01835315Angle · corrodedINSPECTION TYPE:C2, 3 VERTICAL STAB LT SKATE ANGLE IS CORRODED BEYOND LIMITS AT STA 1766. REPAIRED ANGLE IAW SRM 53-2-5 FIG 16A.Feb 22, 2001 · N811UP · Doug DC873FSDR COMA0160265Bushing · scoredLT AND RT BUSHINGS (P/N 600-21061-5) IN VERTICAL STABILIZER WAS FOUND TO BE SCORED DURING INCORPORATION OF COMAIR EO 55-007. REPLACED LT AND RT BUSHING IN VERTICAL STABILIZER WITH (P/N 600-21061-7) IAW CRJ AMM 20-26-00-910-803, CRJ DRWG 600-23068 AND WVAC EO Feb 18, 2001 · N912CA · Cndair CL6002B19SDR TWAA0103011Attach Angle · crackedDURING CHECK-C MAINT IN THE VERT STAB FOUND CRACK IN RT AFT VERTICAL ATTACH ANGLE. CUT OUT CRACKED AREA AND FABRICATED FILLER AND REPAIR ANGLE AND INSTALLED PER SRM 53-05, FIG 23.Feb 14, 2001 · N983Z · Doug DC931SDR COMA0160225Bushing · wornLT AND RT VERTICAL STAB BUSHINGS ARE WORN/SCORED AT HORIZONTAL STAB PIVOT POINT. REMOVED WORN/SCORED BUSHINGS. VERIFIED LT LUG BORE 1.7005 AND RT LUG BORE 1.7002 TO BE WITHIN LIMITS. MACHINED FLANGE OF NEW BUSHING (P/N 600-21061-7) TO .086 IAW WVAC 601R-55-Feb 10, 2001 · N920CA · Cndair CL6002B19SDR COMA0160221Bushing · wornLT AND RT VERTICAL STAB BUSHINGS ARE WORN/SCORED AT HORIZONTAL STAB PIVOT POINT. REMOVED WORN/SCORED BUSHINGS. VERIFIED LT LUG BORE 1.7005 AND RT LUG BORE 1.7002 TO BE WITHIN LIMITS. MACHINED FLANGE OF NEW BUSHING (P/N 600-21061-7) TO .086 IAW WVAC EO 601R-Feb 10, 2001 · N920CA · Cndair CL6002B19SDR COMA0160173Bushing · wornRIGHT VERTICAL STABILIZER STAB BUSHING WORN. REMOVED AND REPLACED BUSHING (P/N 600-21061-7), MACHINED BUSHING FLANGE THICKNESS TO .077 INCH AND REAMED INSIDE DIAMETER TO 1.5002 IAW CRJ AMM 20-26-00-910-803, DRAWING 600-21061 AND WVAC EO 601R-55-21-2175.Jan 29, 2001 · N937CA · Cndair CL6002B19SDR UPS01234900Support Bracket · corrodedINSPECTION TYPE:C, VERT STAB, FAIRING SUPPORT AT JUNCTION OF TENSION TIE RIB AND VERT STAB FRONT SPAR IS WORN DUE TO FRETTING CORROSION LT. REPLACED FAIRING SUPPORT STRUCTURE IAW BOEING INST DRG 65-17485 & SRM 51-30-02.Jan 26, 2001 · N943UP · Boeing 72722CSDR ABXA0100019Fairing · delaminatedLEFT UPPER HORSECOLLAR WAS FOUND DELAMINATED. MAINTENANCE INSPECTED AND REPLACED THE HORSECOLLAR IAW DC-9 SRM 51-30-1.Jan 19, 2001 · N963AX · Doug DC941SDR ABXA0100018Fairing · corrodedRIGHT UPPER HORSECOLLAR HORIZONTAL FAIRING FOUND WORN AND CORRODED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT UPPER HORSECOLLAR FAIRING IAW DC-9 MM 55-10-00.Jan 19, 2001 · N963AX · Doug DC941SDR QXEA0100061Flange · tool damagePDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING SCRATCH ON LEFT HAND FLANGE. REPAIRED IAW DHC-8 51-10-00 AND SRM 51-20-16.Jan 12, 2001 · N824PH · Dhav DHC8102SDR QXEA0100060Flange · tool damagePDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING SCRATCH ON RIGHT HAND FLANGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-10-00.Jan 12, 2001 · N824PH · Dhav DHC8102SDR QXEA0100059Flange · tool damagePDX- VERTICAL STAB LEADING EDGE SPAR ATTACH FLANGE FOR LEADING EDGE 321GT HAS TOOLING GOUGES. REPAIRED IAW DHC-8 SRM 51-10-00 AND SRM 51-20-16.Jan 12, 2001 · N824PH · Dhav DHC8102SDR COMA0160118Bushing · wornVERTICAL STABILIZER LEFT HAND PIVOT POINT BUSHING WAS FOUND TO BE WORN. PERFORMED A MAJOR REPAIR BY REPLACING WORN VERTICAL STABILIZER LT PIVOT POINT BUSHING. (P/N 600-2061-7) IAW WVAC EO 601R-55-7103, CRJ AMM 20-26-00-910-003 AND CRJ DRAWING 600-21029.Jan 12, 2001 · N915CA · Cndair CL6002B19SDR CA010111007Plate · worn(CAN) ON ANNUAL INSPECTION EXCESSIVE WEAR WAS NOTICED BETWEEN THE STAP PART NR 555.30.12.211 AND PLATE PART NR 553.52.12.074. THESE PARTS ENGAGE AND PREVENT FLUTTER OF THE FAIRING. THE STRAP IS RIVETED TO THE TOP OF REAR SPAR ON THE VERTICAL STABILIZER. THE PLJan 3, 2001 · Pilats PC1245
Back to JASC 5530