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 GUU2002F00011Bolt · 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.May 21, 2002 · N81538 · Beech 1900DSDR GUU2002F00009Bolt · loose(BOLT) AT 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.May 20, 2002 · N81546 · Beech 1900DSDR GUU2002F00008Bolt · loose(BOLT) AT 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.May 15, 2002 · N48544 · Beech 1900DSDR GUU2002F00007Bolt · loose(BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.May 14, 2002 · N47542 · Beech 1900DSDR ASAA0280146Web · chafedPAE - DURING 30K-CHECK, FOUND VERTICAL STABILIZER BULLET FAIRING WEB CHAFED AROUND EDGES WHERE PANEL 6308C TO UPPER TIP BULLET FAIRING IS INSTALLED. REPLACED WEB PER SRM 51-10-4. (M)Apr 25, 2002 · N973AS · Doug DC983SDR ABXA010850Angle · crackedRIGHT VERTICAL STABILIZER ATTACH ANGLE WAS CRACKED ON THE AFT END. REPAIRED AREA IAW DC-9 SRM 53-05.Apr 15, 2002 · N989AX · Doug DC932SDR 02FDEA00241Fitting · corroded#1 RUDDER HINGE FITTING HAS CORROSION AT LWR HINGE PIN ATTACH. R&R FITTING.Apr 10, 2002 · N410FE · Airbus A310203SDR CA020517008Crossbeam · cracked(CAN) DURING INTERNAL STRUCTURAL INSPECTION OF THE TAIL AREA, A 5/8 INCH CRACK WAS FOUND ON THE RUDDER CONTROL CROSS BEAM SUPPORT (EMPENNAGE).THE PROBABLE CAUSE MAY BE THAT ON THE LOWER LT OUTBOARD RIVETS WITH BELLOW MINIMUM EDGE DISTANCE. IN ADDITION, THE RIVApr 4, 2002 · Cndair CL6001A11SDR 2002FA0000449Stabilizer · crackedDURING A ROUTINE INSPECTION WE FOUND THE UPPER AND LOWER VERTICAL STABILIZERS TO HAVE CRACKS IN THE MOUNTING BORE EMANATING FROM THE BOLT HOLES THAT ATTACH THE STABILIZERS TO THE TORQUE TUBE.THE BORE HAS A CASTED LOOKING FITTING FOR EACH OF THE TWO MOUNTING BOApr 4, 2002 · N959SD · Doug 600NSDR 2002FA0000447Stabilizer · crackedDURING A ROUTINE INSPECTION WE FOUND THE UPPER AND LOWER VERTICAL STABILIZERS TO HAVE CRACKS IN THE MOUNTING BORE EMANATING FROM THE BOLT HOLES THAT ATTACH THE STABILIZER TO THE TORQUE TUBE.THE BORE HAS A CASTED LOOKING FITTING FOR EACH OF THE TWO MOUNTING BOLApr 4, 2002 · N957SD · Doug 600NSDR 2002F00509Frame · crackedAT C-CHECK FOUND VERTICAL STABILIZER FRAME CRACKED AT LEFT SIDE STATION 180.6 STRINGER 6. (M)Mar 6, 2002 · N801EA · Boeing 727225SDR 2002F00320Structure · crackedDURING 100 HOUR INSPECTION 2 IDENTICAL CRACKS WERE NOTICED ON THE UPPER VERTICAL STABILIZER, DIRECTLY ABOVE THE RUDDER AND MIGRATING FORWARD APPROXIMATELY 4.5 INCHES. AFTER CONTACTING MANUFACTURER, IT WAS SUGGESTED THAT THE BOTTOM FAIRING OF THE VERTICAL STABMar 1, 2002 · N562NA · Pilats PC1245SDR ALG2002F00025Spacer · spinningREMOVING STABILIZER FROM AIRCRAFT AND NOTED SPACER SPINNING. WHILE STARTING TO REPAIR SPACER, BUBBLED PAINT WAS NOTED BY TIP CAP AND ON TRAILING EDGE CAPS. SPACER SPINNING IN HONEYCOMB, THE SPACER IS MANUFACTURED SMOOTH WITH NO SERATIONS TO PREVENT SPINNINFeb 17, 2002 · N567AL · Bell 407SDR QXEA0200349Boss · wornPDX - PIP PIN BOSS HAS STEP WEAR AT THE RT SIDE OF THE UPPER REMOVABLE FALSE RIB FOR PANEL 55F. REPAIRED IAW HORIZON AIR EA 4-55-301.Feb 14, 2002 · N480AU · Fokker F28MK4000SDR CA020228003Panel · cracked(CAN) VERTICAL STAB LEADING EDGE PANELS 322AL, 322CL AND 322BL CRACKED. PANEL 322AL CRACKED APPROXIMATELY 4 INCHES FROM LOWER EDGE LT SIDE. PANEL 322CL CRACKED APPROXIMATELY 4 INCHES FROM LOWER EDGE LT SIDE. ALSO 322BL. PRODUCTION PERMIT RAISED FOR REPAIR IF BFeb 12, 2002 · Airbus A320211SDR SWAA020325Tee Chord · crackedDURING SCHEDULED D CHECK, FOUND VERTICAL FIN LT TEE CHORD CRACKED AT RUDDER STA 13.33. REPAIRED TEE CHORD PER SRM.Feb 9, 2002 · N528SW · Boeing 7375H4SDR 0200419870Frame · crackedDuring Mck in ATL, a crack was found in the area of the Verticle Access Cover, the crack was on the LH side of former P/n 9911986-11. Repaired per EA.98-185563.Feb 8, 2002 · N779NC · Doug DC951SDR 0200459981Stabilizer · crackedDuring overnight in MSP, a crack was found on the verticle stabilizer front spar left lower chord.Repaired per EA 99-187946Feb 4, 2002 · N994Z · Doug DC931SDR COMA0260083Bushing · scoredTHE R/H VERTICAL STABILIZER BUSHING WAS SCORED AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE SCORED BUSHING. MACHINED FLANGE OF NEW BUSHING P/N 600-21061-7S/B I/A/W WVAC EO 601R-55-2952.INSTALLED THE NEW BUSHING I/A/W CRJ AMM 20-26-00-910-803. REAMED THE BFeb 1, 2002 · N952CA · Cndair CL6002B19SDR 02FDEA00118Fitting · corrodedVERT STAB TENSION TIE FITTING LT AFT VERTICAL BOLT HOLE CORRODED. REMOVED AND REPLACED TIE PER MM 55-30-051-4.Jan 30, 2002 · N244FE · Boeing 727277SDR 02FDEA00117Tie · corrodedN 1259 VERT STAB TENSION TIE FITTING RH AFT VERTICAL BOLT HOLE CORRODED. R&R TIE PER MM 55-30-051-4.Jan 30, 2002 · N244FE · Boeing 727277SDR CALA0200015Bracket · crackedINSPECTION FOUND A 1/2" CRACK IN VERTICAL STABILIZER R/H SIDE SUPPORT BRACKET FOR UPPER FAIRING ABOVE JACKSCREW. A DOUBLER WAS INSTALLED ON THE SUPPORT BRACKET IAW SRM 51-30-2.Jan 11, 2002 · N72825 · Doug DC982SDR CALA0200007Hinge · corrodedINSPECTION FOUND LEFT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238.Jan 9, 2002 · N72825 · Doug DC982SDR CALA0200006Hinge · corrodedINSPECTION FOUND RIGHT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238.Jan 9, 2002 · N72825 · Doug DC982SDR COMA0260008Bushing · mislocatedTHE R/H SIDE VERTICAL STABILIZER HAS A MIGRATING BUSHING AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE MIGRATING BUSHING. MACHINED AND CADMIUM PLATED A NEW NOMINAL SIZE BUSHING I/A/W WVAC EO 601R-55-2910. INSTALLED THE NEW BUSHING I/A/W CRJ AMM 20-26-00-910Dec 28, 2001 · N713CA · Cndair CL6002B19SDR TX22002F00000Bearing · failedDURING REMOVAL OF THE HORIZONTAL STABILIZER HINGE PINS TO COMPLY WITH THE AD AND SB. FOUND RIGHT HINGE BEARING TO HAVE FAILED WITH PIECES MISSING. LEFT BEARING WAS CRACKED. DURING FURTHER INSPECTION FOUND NUMEROUS BUSHINGS AND ATTACH HARDWARE IN THE HORIZONDec 27, 2001 · N400RG · Boeing 72722SDR 2002FA0000020Bracket · crackedVERICAL STAB BRACKET CRACKED, OCCURRED DURING NORMAL OPERATING CONDITIONS AND WAS DISCOVERED AT APPROX 3130 AC TT.Dec 18, 2001 · N6249Y · Piper PA23250SDR 2002FA0000019Bracket · crackedVERTICAL STAB BRACKET CRACKED, OCCURRED DURING NORMAL OPERATING CONDITIONS AND WAS DISCOVERED AT APPROX. 3130 ACTT.Dec 18, 2001 · N6249Y · Piper PA23250SDR 2002F00131Support Bracket · crackedVERTICAL STABILIZER AFT WEB SUPPORT BRACKET IS CRACKED OUT AROUND FASTENERS AT FIN WL 58.18 AND BS 1088. (M)Dec 17, 2001 · N54SW · Boeing 7372H4SDR QXEA0102154Rivet · loosePDX - LT SIDE OF VERTICAL STABILIZER CONNECTION ANGLE HAS SIX LOOSE/SMOKING RIVETS LOCATED AT RIBS 6.0 AND 7.0. REPAIRED IAW FOKKER SRM 51-30-02.Dec 11, 2001 · N488US · Fokker F28MK4000SDR QXEA0102153Rivet · loosePDX - VERTICAL STABILIZER RT CONNECTION ANGLE HAS SIX SMOKING/LOOSE RIVETS AT RIB 6.0 AND 7.0. REPAIRED IAW FOKKER SRM 51-31-02.Dec 11, 2001 · N488US · Fokker F28MK4000SDR 2001FA0000518Rivet · brokenRIVET HEAD MISSING ON EXTENSION FITTING OF VERTICAL STABILIZER FORWARD SPAR JUST ABOVE AREA WHERE SPAR IS BOLTED TO FUSELAGE BULKHEAD. THERE IS NO EVIDENCE OF CORROSION OR CRACKING OF STRUCTURE IMMEDIATELY SURROUNDING RIVET LOCATION. RIVET APPEARS TO HAVE FAOct 31, 2001 · N145Z · Beech 58PSDR 01FDEA00919Frame · crackedVERTICAL STABILIZER MAIN BOX INTERIOR CHORD IS CRACKED AT FIN BS 157.2, STR 8 LT. REMOVED AND REPLACED CHORD PER SRM 55-30-5 FIG 1 & EA 7-5530-59891.Oct 25, 2001 · N279FE · Boeing 727233SDR 0103679998Support Fitting · crackedDuring H ck at ATL base maintenance, two 1.00" cracks were found on verticle stabilizer actuator support fittings. Both cracks emenated from the end fastener hole forward the edge of the firrigns flange. The repair involved the installation of a repair doublerOct 17, 2001 · N8934E · Doug DC931SDR MWEA011350Angle · corrodedEXFOLIATION CORROSION ON AFT END OF VERTICAL STABILIZER ATTACH ANGLE LEFT SIDE, STATION 1121. FABRICATED AND INSTALLED ANGLE REPAIR.Sep 27, 2001 · N401ME · Doug DC932SDR UPS01836926Fitting · corrodedINSPECTION TYPE:C2 VERTICAL STAB REAR SPAR FWD SIDE FITTING IN 4TH LIGHTENING HOLE FROM THE TOP IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 36480113, AND SRM 51-1-20D.Sep 15, 2001 · N852UP · Doug DC873FSDR CA010907009Support Bracket · broken(CAN) BRACKET INSPECTED IN ACCORDANCE WITH THE DC3 SUPPLEMENTAL INSPECTION DOCUMENT 53.03.01. BASE FLANGE BROKEN AS DESCRIBED IN THE SID. REPLACEMENT BRACKET FABRICATED AND INSTALLED AS ORIGINAL. TO BE INSPECTED IN ACCORDANCE WITH THE SID ON A CONTINUING BASISSep 5, 2001 · Doug DC3G202ASDR DHL2001727522Bracket · crackedVERTICAL STABILIZER TOP SIDE SUPPORT BRACKET FOR HORIZONTAL STAB POSITION INDICATOR IS CRACKED AT LT AND RT ATTACH POINT. REMOVED SUPPORT BRACKET PER SRM 51-30-2. INSTALLED NEW SUPPORT BRACKET PER SRM 51-30-2.Aug 23, 2001 · N727DH · Boeing 727228SDR 0104069868Hinge · corrodedDuring Mck in Atl, two verticle stabilizer hinge plates for the horizontal stabilizer were found corroded. The right outboard outer lug, and the right outboard inner lug had corrosion on the surface around the bore.Repaired per EA 98-185043Aug 17, 2001 · N777NC · Doug DC951SDR GAIA01272STWeb · crackedDURING AN LTC INSPECTION, IT WAS DISCOVERED STATION 1300 LEFT AND RIGHT CORNERS ON WEB HAVE .5 INCH CRACK. ACCOMPLISHED UPPER TORQUE BOX WEB REPAIR IAW B727 SRM 55-30-2, FIG 2 AND 51-40-2, FIG 1. (M)Aug 6, 2001 · N278US · Boeing 727251SDR 01FDEA00641Shear Tie · crackedCRACKED SHEAR TIE FOR VERTICAL STAB SKIN AT RIB NR 3 BETWEEN STR 6R & 7R. *S/D* REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-2.Aug 3, 2001 · N236FE · Boeing 727247SDR QXEA0101321Structure · corrodedPDX - LIGHT CORROSION BELOW VERTICAL STABILIZER LEADING EDGE, RIGHT-HAND FASTENER HOL AT X813.823, Z335.5. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26.Aug 2, 2001 · N349PH · Dhav DHC8202SDR CALA0100695Plate · corrodedINSPECTION FOUND I/B AND O/B LEFT VERTICAL STABILIZER SUPPORT PLATES FOR HORIZONTAL STABILIZER PIVOT BOLT CORRODED IN AND AROUND BOLT HOLES. THE SUPPORT PLATES WERE REMOVED AND REPLACED IAW WORK CARD 08-5530-1-0005.Jul 26, 2001 · N76823 · Doug DC982SDR CALA0100673Plate · corrodedINSPECTION FOUND I/B AND O/B RT VERTICAL STABILIZER SUPPORT PLATES CORRODED. THE I/B AND O/B RT VERTICAL STABILIZER SUPPORT PLATES WERE REMOVED AND REPLACED IAW EA SA003-5530-01238, SRM 51-10-2.Jul 24, 2001 · N76823 · Doug DC982SDR CA010906017Bolt · loose(CAN) DURING H-CHECK AND ACCOMPLISHING AIRCRAFT MAINTENANCE MANUAL TASK 53-51-00-210-009 FOUND THREE BOLTS LOOSE AS WELL AS CORRODED NUT FOR THE TAIL CONE ATTACHMENT.BOLTS RETORQUED AND NUTS REPLACED.Jul 19, 2001 · Airbus A320211SDR 2001F00414Rub Strip · bulgedVERTICAL STABILIZER, LEFT UPPER SIDE RUB STRIP, SHOWS BULGES IN SEVERAL AREAS. REPAIRED VERTICAL FIN TRACK OUTBOARD LEFT SIDE IAW SRM 51-30-2 AND AVHM-245RO-1 REVISION R1. (M)Jul 18, 2001 · N355QS · Boeing 72721SDR QXEA0101227Flange · gougedPDX-FOUR TOOLING GOUGES ON UPPER HALF OF VERTICAL STABILIZER FORWARD LEADING EDGE MOUNT FLANGE. REPAIRED IAW DHC-8 RD8-55-584.Jul 17, 2001 · N375PH · Dhav DHC8202SDR QXEA0101226Flange · gougedPDX-NUMEROUS TOOL GOUGES/SRATCHES ON UPPER HALF OF VERTICAL STABILIZER FORWARD SPAR RIGHT HAND LEADING EDGE MOUNT FLANGE. REPAIRED IAW DHC-8 RD8-55-584.Jul 17, 2001 · N375PH · Dhav DHC8202SDR QXEA0101225Flange · damagedPDX-TOOL SCRATCH ON RIGHT HAND SIDE OF VERTICAL STABILIZER TOP RIB MOUNT FLANGE STATION AT 325AT. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 55-30-16.Jul 17, 2001 · N375PH · Dhav DHC8202SDR QXEA0101224Flange · scratchedPDX-RIGHT HAND STABILIZER FORWARD SPAR LOWER EDGE FLANGE HAS SMALL SCRATCH NEAR RIB 8 STATION YH77.500. REPAIRED IAW DHC-8 RD8-55-626.Jul 17, 2001 · N375PH · Dhav DHC8202
Back to JASC 5530