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 C2XA10TY077Housing · out of limitsTYS - LT AND RT SPHERICAL BEARING HOUSING OUT OF LIMITS. REAMED LT AND RT VERTICAL STAB. SPHERICAL BEARING HOUSING TO FIRST OVERSIZE.May 5, 2010 · N11150 · Emb EMB145XRSDR DLM88100994Structure · crackedBHEC INSPECTION OF FASTENER HOLES ON VERTICAL STAB RT SIDE INDICATIONS OF CRACKING IN HOLE NR 7 AT ZFS52. STEPPED UP HOLE BELOW ZFS52 RT SIDE TO .250" COMP-LIED WITH PRI 481680-14 REV 2 4/24/2010 1000 EST.Apr 25, 2010 · N929DL · Doug MD88SDR C2XA10TY060Hinge Fitting · corrodedLT & RT VERTICAL STAB HINGE FITTINGS CORRODED IN SEVERAL AREAS AS MARKED & LOOSE FIT WITHIN BEARINGS. REAMED HOUSING INSTALLED NEW BUSHINGS AND BEARINGS IAW 55-30-02.Apr 21, 2010 · N12167 · Emb EMB145XRSDR IPXA10559029Strap · corrodedINSPECTION TYPE: C4, VERTICAL STAB FAIRING 326B HAS CORROSION ON INNER SURFACE STRAP. REMOVED, FABRICATED AND INATALLED REPLACEMENT STRAP IAW SRM 51-40-02.Mar 23, 2010 · N451UP · Boeing 75724APFSDR IPXA10559120Strap · gougedINSPECTION TYPE:C3, VERTICAL FIN L/E PANEL NR 321BL FWD MATING SURFACE IS GOUGED ON A/C SIDE, REMOVED, FABRICATED AND INSTALLED STRAP IAW SRM 51-40-02.Mar 16, 2010 · N458UP · Boeing 75724APFSDR FDEA201003110774Fitting · cracked02 CRACKS APPROX .3125 INCH AND .1875 INCH AT 5:00 AND 7:00 O'CLOCK RESPECTIVELY ON FASTENER HOLE OF VERTICAL STABILIZER LT SIDE FWD FLANGE OF NR 4 BANJO FITTING. REPAIR CARRIED OUT IAW EA NR 1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100Mar 11, 2010 · N601FE · Doug MD11FSDR FDEA201003110773Fitting · cracked02 CRACKS APPROX .1250 INCH AND .1875 INCH AT 1:00 AND 7:00 O'CLOCK RESPECTIVELY ON FASTENER HOLE OF VERTICAL STABILIZER RT SIDE FWD FLANGE OF NR 4 BANJO FITTING. REPAIR CARRIED OUT IAW EA NR1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REMar 11, 2010 · N601FE · Doug MD11FSDR FDEA201003110772Fitting · crackedCRACK FOUND APPROX 1.5 INCH ON VERTICAL STABILIZER RT SIDE FWD FLANGE OF NR 4 BANJO FITTING RADIUS. REPAIR CARRIED OUT IAW EA NR 1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.Mar 11, 2010 · N601FE · Doug MD11FSDR FDEA201003110771Fitting · crackedCRACK FOUND PROPAGATED 1.3 INCH UPWARD FROM STOP DRILL HOLE ON LT NR 4 BANJO AFT FLANGE OF REAR SPAR. REPAIR CARRIED OUT IAW EA NR 1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.Mar 11, 2010 · N601FE · Doug MD11FSDR FDEA201003110770Fitting · crackedCRACK FOUND PROPAGATED 0.4 INCH DOWNWARD FROM STOP DRILL HOLE ON RT NR 4 BANJO AFT FLANGE OF REAR SPAR. REPAIR CARRIED OUT IAW EA NR 1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.Mar 11, 2010 · N601FE · Doug MD11FSDR USAA2010031090557Hinge Fitting · excess playSAL - S2 - MAJOR REPAIR - EXCESSIVE PLAY ON HINGE BEARING NR 7 OF VERTICAL STABILIZER AT RIB 11 VERTICAL STABILIZER STATION 5605. REPLACED HINGE FITTING NR 7 OF VERTICAL STABILIZER RIB 11 VERTICAL STABILIZER STATION 5605 & PERFORMED OPERATIONAL TEST IAW 55-36Feb 19, 2010 · N626AW · Airbus A320231SDR USAA2010031090555Hinge Fitting · excess playSAL - S2 - MAJOR REPAIR - EXCESSIVE PLAY ON HINGE BEARING NR 5 OF VERTICAL STABILIZER AT RIB 7 VERTICAL STABILIZER STATION 2985. REPLACED HINGE FITTING NR 5 OF VERTICAL STABILIZER RIB 7 VERTICAL STABILIZER STATION 2985 & PERFORMED OPERATIONAL TEST IAW 55-36-4Feb 19, 2010 · N626AW · Airbus A320231SDR USAA2010030890539Hinge Fitting · excess playSAL - S2 - MAJOR REPAIR - EXCESSIVE PLAY ON NR 1 HINGE BEARING OF VERTICAL STABILIZER. REPLACED NR 1 HINGE FITTING OF VERTICAL STABILIZER IAW A320 AMM 55-36-41.Feb 19, 2010 · N626AW · Airbus A320231SDR 2010FA0000098Nut · brokenONE OF THE 4 BOLTS HOLDING THE REAR ATTACHMENT BRACKET ON VERTICAL STABILIZER, HAD A BROKEN/ SPLIT NUT. PROBABLE CAUSE COULD HAVE BEEN FROM CORROSION FOUND BETWEEN THE NUT AND WASHER CAUSING STRUCTURAL LOSS OF THE NUT. INSPECTED NUTS FOR CORROSION AND REPALCJan 28, 2010 · N21462 · Cessna 182PSDR AALA20100224TUL10Structure · crackedFOUND CRACK INDICATION AT STATION 1809.5 RIGHT FORWARD CHORD FASTENER HOLE. THE HOLE WAS OVERSIZED TO 0.2782 INCH IN ORDER TO REMOVE ANY CRACK INDICATIONS. BOEING REQUIRED AN INSURANCE CUT OF AT LEAST 0.030 INCH. THE INSURANCE CUT RESULTED IN A FINAL HOLE SJan 18, 2010 · N371AA · Boeing 767323SDR DALA100519751Former · looseDURING "L" CHECK FOUND 3 EA BLIND FASTENERS LOOSE IN VERTICAL STABILIZER FORMER. REPAIRED IAW SRM 55-30-0, SRM 55-31-0 & SRM 51-30-8.Jan 16, 2010 · N751NW · Doug DC941SDR C2XA10TY010Housing · damagedTYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT AND RT SPHERICAL BEARING HOUSING WITH PITTING AND SCRATCHES. MAINTENANCE REAMED THE SPHERICAL HOUSING TO THE 1ST REWORK AND INSTALL BUSHIONS IAW EMB SRM 55-30-02. ALL WORK WAS ACCOMPLISHED Jan 13, 2010 · N13965 · Emb EMB145LRSDR TIMA201000007Hinge · corrodedFOUND INTERGRANULAR CORROSION ON HINGE.Dec 18, 2009 · N194GA · Beech 1900CSDR TIMA201000006Hinge · corrodedFOUND INTERGRANULAR CORROSION ON HINGE.Dec 18, 2009 · N194GA · Beech 1900CSDR 2010FA0000083Hinge · corrodedFOUND INTERGRANULAR CORROSION ON HINGE.Dec 18, 2009 · N194GA · Beech 1900CSDR 2010F00018Hinge · corrodedFOUND INTERGRANULAR CORROSION ON HINGE.Dec 18, 2009 · N194GA · Beech 1900CSDR ABXR200912180049Structure · crackedDURING A HEAVY MX VISIT CRACK INDICATION WITH EDDY CURRENT VERT STAB L/E UPPER SECTION. STOP DRILLED CRACK IAW SRM 55-02 FIG 27. FABRICATED REPAIR PARTS OUT OF 2024-T3 .050 AND .040. ITEM RETURNED TO SERVICE.Dec 18, 2009 · N327US · Doug DC933FSDR SWIA200923279Nut · corrodedC-CHECK, VERTICAL STABILIZER ATTACHMENT HINGE NUT CORRODED. (NDT INSP) REPLACED NUT PER AMM.Dec 15, 2009 · N958SW · Cndair CL6002B19SDR A6WA201040138Bracket · crackedNUT BRACKET UNDER PANEL 326CL, LT SIDE OF VERTICAL STAB, CRACKED. REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE PN 600-21137-5 BRACKET.Dec 7, 2009 · N432AW · Cndair CL6002B19SDR C2XA09SH372Rivet · looseSHV - DURING C-CHECK (FRAME 81) VERTICAL STAB BASE AND DRAG ANGLE ON LT SIDE HAS (3) WORKING RIVETS. MAINTENANCE REMOVED AND REPLACED THE (3) WORKING RIVETS AT FRAME 81 VERTICAL STAB BASE AND DRAG ANGLE ON LT SIDE IAW EMB-145 SRM 51-20-03 AND CPM 51-21-07. TOct 21, 2009 · N11164 · Emb EMB145XRSDR FDEA200910153590Fitting · crackedCRACK INDICATION FOUND APPROX 0.50" IN LENGTH DURING HFEC ON LT SIDE OF THE LWR VERTICAL STABILIZER FWD FLANGE OF UPPER REAR SPAR CAP. REPAIR CARRIED OUT IAW EA 1-5530-135612, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 108.Oct 15, 2009 · N628FE · Doug MD11FSDR DLM88091629Structure · crackedACCOMPLISHMENT OF EA 09-470871-12, REV A. OPN 0101 HFEA SHOWS 2ND, 3RD AND 6TH HOLES LT SIDE WITH CRACK INDICATIONS. 2ND AND 3RD HOLES RECHECK OK AFTER REMOVAL OF NUTPLATE GANG CHANNEL. 6TH HOLE REPAIRED IAW ER/A 477465-14 REV 0.Oct 12, 2009 · N918DL · Doug MD88SDR C2XA09SH324Housing · out of limitsSHV - DURING C-CHECK BOTH LT AND RT VERTICAL STAB SPHERICAL BEARING HOUSING OUT OF LIMITS IAW EMB-145XR SRM 55-30-02. MAINTENANCE PERFORMED WORK ON BOTH LT AND RT VERTICAL STAB SPHERICAL BEARING HOUSINGS IAW SRM 55-30-02. THE AIRCRAFT WAS APPROVED FOR RETURNOct 11, 2009 · N21130 · Emb EMB145XRSDR C2XA09TY248Fitting · damagedFRM 75 UPPER FITTING HAS OVERSIZED HOLE ON RT O/B HOLE. REMOVED, REPAIRED AND INSTALLED FITTING IAW EC5530-01187, EMB 145 SRM 51-40-02 AND EC5310-01317.Sep 29, 2009 · N12924 · Emb EMB145LRSDR CA090910003Bolt · crackedIGX POWER VISUAL INSP OF NAS BOLT - CRACKED (APPARANT) UNDER HEAD IN RADIUS. IPC DOES NOT INDICATE A CHAMBERED WASHER TO BE INSTALLED AS IS INDUSTRY PRACTICED WITH NAS BOLTS. NOTE THERE IS NO CHAMBER ON THE FITTINGS PN C3TF6-3. BOTH ATTACH BOLTS TO BE REPLASep 2, 2009 · Dhav DHC3SDR SWAA095640Attach Fitting · wornDURING SCHEDULED MV1 CHECK, FOUND RT VERTICAL STABILIZER AFT FAIL SAFE ATTACH LUG WORN. REPAIRED LUG PER SWA EA.Aug 29, 2009 · N657SW · Boeing 7373L9SDR SWAA095616Fitting · corrodedDURING SCHEDULED MV1 CHECK, FOUND RT VERTICAL STABILIZER FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.Aug 29, 2009 · N657SW · Boeing 7373L9SDR CA090826008Hinge Bracket · crackedBRACKET REMOVED FOR COMPLIANCE WITH AD 78-08-03 (HINGE BRACKET ASSY). CRACKS FOUND IN BRACKET OFF OF ANCHOR NUT RIVET HOLES. UPON FURTHER INSP, CRACKS FOUND ALSO IN SIMILAR LOCATION ON REAR VERTICAL FIN SPA (PN 17067-02). SERVICEABLE VERTICAL FIN ASSY INSTALAug 19, 2009 · Piper PA23160SDR CA090901007Bolt · brokenONE OF THE 4 VERTICAL FIN ATTACHMENT (NAS6604-30) BOLTS FOUND BROKEN (BOTTOM AFT BOLT). REMAINING 3 BOLTS WERE NOT FINGER LOOSE, BUT WERE NOT AT MAXIMUM TORQUE. THE NUTS WERE NOT BOTTOMED ON THE SHANK OF THE BOLTS. FRETTING DAMAGE TO TAIL FIN FLANGE BUSHINGSAug 12, 2009 · Bell 427SDR AC2A2009081282853Bolt · brokenDURING PRE-FLIGHT INSP, PIC FOUND THE VERTICAL STABILIZER TO HAVE UP AND DOWN PLAY.Aug 12, 2009 · N427MH · Bell 427SDR DLM88091125Hinge · corrodedVERTICAL FIN LEFT AND RIGHT O/B PIVOT FITTING PLATES CORRODED. FOUND DURING REMOVAL OF HORIZONTAL FOR UPPER SKIN REPLACEMENT DUE TO TIME LIMITED REPAIR OF CRACK. REPLACED BOTH OUTBOARD PLATE SETS PER ERA 475781-14. THESE PLATES WERE SUBJECT TO SB MD80-55-054Jul 8, 2009 · N999DN · Doug MD88SDR FDEA200906262326Fitting · crackedVERTICAL STABILIZER RT NR 4 FWD BANJO FITTING FOUND WITH CRACK. REPAIR CARRIED OUT AS PER SRM 55-20-00 FIGURE 3 VOLUME I, REVISION 40. REPAIR CATEGORY B DAMAGED TOLERANCE INSPECTION REQUIREMENT INITIAL 5400 CYCLE, REPETITIVE 2700 CYCLE AS PER DRAWING NR Jun 26, 2009 · N617FE · Doug MD11FSDR C2XA09TY125Fitting · wornDURING C-CHECK FRAME 75 TO VERTICAL STAB SPAR FITTING WAS FOUND FRETTING. MX REMOVED AND REPLACED THE VERTICAL STAB SPAR FITTING IAW EC 5310-01317. ACFT STILL IN C-CHECK.Jun 23, 2009 · N13935 · Emb EMB145EPSDR IPXA09555838Panel · delaminatedINSPECTION TYPE:C4 REMOVE THE VERTICAL STAB LT SIDE FORWARD LOWER PANEL TO FACILITATE REPAIR ON CARD 803048. REMOVED DELAMINATED PANEL, REPAIR UNSUCCESSFUL REPLACED PANEL IAW SRM 51-40-02-0G.May 5, 2009 · N443UP · Boeing 75724APFSDR C2XA09SH150Hinge · excess playSHV - DURING C-CHECK RUDDER ONE UPPER CENTER HINGE POINT HAS VERTICAL PLAY. MAINTENANCE REMOVED AND REPLACED RUDDER ONE UPPER CENTER HINGE POINT IAW EMB-145XR AMM 55-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 3, 2009 · N18101 · Emb EMB145XRSDR C2XA09SH149Hinge · excess playSHV - DURING C-CHECK RUDDER ONE LOWER CENTER HINGE POINT HAS VERTICAL PLAY. MAINTENANCE REMOVED AND REPLACED RUDDER ONE LOWER CENTER HINGE POINT IAW EMB-145XR AMM 55-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 3, 2009 · N18101 · Emb EMB145XRSDR USAA2009041690907Hinge Fitting · excess playSAL - BC2 - MAJOR REPAIR - EXCESSIVE PLAY ON NR 4 VERTICAL STABILIZER RUDDER HINGE FITTING AT THE FORK END AT VERT STAB STA 2632. REPLACED NR 4 VERTICAL STABILIZER RUDDER HINGE FITTING IAW A319 AMM 55-36-41.Apr 7, 2009 · N840AW · Airbus A319132SDR USAA2009041690906Hinge Fitting · excess playSAL - BC2 - MAJOR REPAIR - EXCESSIVE PLAY ON NR 3 VERTICAL STABILIZER HINGE FITTING AT THE FORK END AT VERTICAL STABILIZER STATION 2279. REPLACED NR 3 VERTICAL STABILIZER RUDDER HINGE FITTING IAW A319 AMM 55-36-41.Apr 7, 2009 · N840AW · Airbus A319132SDR C8GA20090111Structure · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT VERTICAL STAB HINGE PIN BEARING HOLE IS PITTED. REMOVED PITTING FROM THE LT BEARING HOLE BY REAMING AND INSTALLED REPAIR SLEEVE PN 69-65750-5. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVIMar 23, 2009 · N287SC · Boeing 7272A1SDR MZZA2009030400027Failsafe · corrodedVERTICAL STABILIZER REAR SPAR RT FAIL SAFE CHORD HAS CORROSION AT FIN STA185. 663. REPAIR CARRIED OUT IAW EC/RA 5530-01526 PART 1 INTERIM REPAIR. REFER L/P 7907827 FOR DIP ISSUED.Mar 3, 2009 · N14235 · Boeing 737824SDR A6WA200940089Structure · crackedVERTICAL STAB, LT UPPER VISOR IS CRACKED. VERTICAL STAB, LT UPPER VISOR REPLACED IAW SRM 51-41-04. (K)Feb 27, 2009 · N450AW · Cndair CL6002B19SDR USAA2009022090390Bearing · excess playSAL - C8 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE ARM BEARING NR 3 VERTICAL STABILIZER. REPLACED ATTACH FITTING HINGE ARM BEARING NR 3 OF VERTICAL STABILIZER IAW A320 AMM 55-36-41.Jan 26, 2009 · N648AW · Airbus A320232SDR USAA2009022090389Bearing · excess playSAL - C8 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE ARM BEARING NR 5 VERTICAL STABILIZER. REPLACED ATTACH FITTING HINGE ARM BEARING NR 5 OF VERTICAL STABILIZER IAW A320 AMM 55-36-41.Jan 26, 2009 · N648AW · Airbus A320232SDR USAA2009021990384Bearing · excess playSAL - C8 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE ARM BR NR 4 RIB NR 6. REPLACED ATTACH FITTING HINGE ARM BEARING NR 4 OF VERTICAL STABILIZER IAW A320 AMM 55-36-41.Jan 26, 2009 · N648AW · Airbus A320232SDR USAA2009021990383Bearing · excess playSAL - C8 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE ARM BR NR 2 RIB NR 4. REPLACED ATTACH FITTING HINGE ARM BEARING NR 2 OF VERTICAL STABILIZER IAW A320 AMM 55-36-41.Jan 26, 2009 · N648AW · Airbus A320232
Back to JASC 5530