JASC 5531

Service difficulty reports · 1,234

Reports filed under 5531 · Vertical Stabilizer, Spar/Rib, 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 = '5531'
  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 CA090422002Frame · cracked(CAN) DURING O/H OF ACFT, TECH FOUND SMOKING RIVETS ON THE ACFT FRAME AT VERTICAL FIN ATTACH BRACKET, REMOVED BRACKET AND 6 OF 6 HOLES WERE CRACKED, BRACKET REPAIRED.Apr 20, 2009 · Dhav DHC2MK3SDR FDEA200904131269Spar Cap · crackedCRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON RIGHT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP. CRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON RIGHT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE Apr 13, 2009 · N605FE · Doug MD11FSDR GUUA91255040609BSpar · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED VERTICAL STABILIZER RT SPAR HAS CORROSION BETWEEN CSS 11.500 TO 24.973, CSS 39.289 TO CSS 69.184 AND APPROX 3.5 INCHES ABOVE CSS 69.184. CLEANED CORROSION AND INSTALLED REPAIRS STRAPS IN CORRODED AREAS BETWEEN CSS 11.50 TApr 6, 2009 · N45AR · Beech 1900DSDR GUUA91255040609ASpar · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED VERTICAL STABILIZER LT SPAR HAS CORROSION BETWEEN CSS 11.50 TO CSS 24.973,CSS 24.973 TO CSS 39.289 AND CSS 39.289 TO CSS 69.184. CLEANED CORROSION AND INSTALLED REPAIR STRAPS IN CORRODED AREAS BETWEEN CSS 11.50 TO CSS 69Apr 6, 2009 · N45AR · Beech 1900DSDR MALA090050Spar · dentedDENT NOTED ON LT VERTICAL STAB AT STA 781.35 11 INCH FWD OF VERTICAL REAR SPAR. REPAIRED IAW S55017.Apr 4, 2009 · N437XJ · Saab 340BSDR FDEA200903190970Spar Cap · crackedCRACK INDICATION APPROXIMATELY 1 INCH LENGTH FOUND ON THE LT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 55-20-00 FIG. 3 VOL. I REV. 40. CATEGORY 'B' REPAIR INITIAL INSPECTION TO BE CARRIED OUT AT 5400Mar 19, 2009 · N588FE · Doug MD11FSDR FDEA200903190969Spar Cap · crackedCRACK INDICATION APPROXIMATELY 1 1/4 INCH LENGTH FOUND ON THE RT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAP. CARRIED OUT REPAIR AS PER SRM 55-20-00 FIG. 3 VOL. I REV. 40. CATEGORY 'B' REPAIR INITIAL INSPECTION TO BE CARRIEMar 19, 2009 · N588FE · Doug MD11FSDR FDEA200903160924Spar Cap · crackedCRACK INDICATION APPROXIMATELY 1.5 INCH FOUND ON RIGHT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAPS AREA. REPAIRED AS PER SRM 55-20-00 FIGURE 3 VOLUME I REVISION 40. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 REVISION 107.Mar 16, 2009 · N599FE · Doug MD11FSDR CALA2009020400080Bulkhead · wornVERTICAL STABILIZER FORWARD BULKHEAD HAS WEAR SPOTS AT FORWARD SIDE WHERE DORSAL FIN CONTACTS. REPAIRED PER ECRA 5530-01528.Feb 3, 2009 · N13720 · Boeing 737724SDR GUUA95455020209ASpar · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED VERTICAL STABILIZER RT TRAILING EDGE SPAR ANGLE SHOW SIGNS OF EXFOLIATION AT STA 61. BLENDED OUT CORROSION, FABRICATED AND INSTALLED REPAIR STRAP.Feb 2, 2009 · N87554 · Beech 1900DSDR GUUA95455012809BSpar · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED VERTICAL STABILIZER RT TRAILING EDGE SPAR ANGLE SHOW SIGNS OF EXFOLIATION AT STA 12. BLENDED OUT CORROSION, FABRICATED AND INSTALLED REPAIR STRAP.Jan 28, 2009 · N87554 · Beech 1900DSDR DHLA2009770AT526Frame · wornEMPENNAGE VERTICAL STABILIZER ACTUATOR RT ACCESS PANEL FRAME "T" SHAPE SUPPORT WORN AND LOOSE. REPAIRED VERTICAL STABILIZER MID SPAR CHORD RIGHT SIDE FROM FIN STA 222 TO FIN STA 235 IAW B727 SRM 55-30-6 FIG 3Jan 6, 2009 · N770AT · Boeing 7272B7SDR FDEA200901060045Rib · brokenVERTICAL STABILIZER RIB NR 8 IS BROKEN AT THE LEFT REAR EDGE AT THE ATTACHMENT POINT TO THE REAR SPAR. COMPLIED WITH E.A. 6-5530-127910 REV. A.Jan 6, 2009 · N436FE · Airbus A310203SDR CA081223005Rib · cracked(CAN) CRACK 35 MM LONG ON RIB OF VERTICAL STAB AT WL 396.Dec 8, 2008 · Cndair CL2156B11215SDR DHLA2009770AT528Frame · wornEMPENNAGE VERTICAL STABILIZER ACTUATOR LT ACCESS PANEL FRAME "T" SHAPE SUPPORT WORN AND LOOSE. REPAIRED VERTICAL STABILIZER MID SPAR CHORD SECTION FROM FIN STA 222 TO FIN STA 241 IAW COOPESA EO COO-2-55-499-08 DTD 12/22/08 DOCUMENTED ON FAA FORM 8110-3.Dec 8, 2008 · N770AT · Boeing 7272B7SDR FDEA200811295035Spar · corrodedRT THS REAR SPAR UPPER TEE CAP UPPER SURFACE HAS CORROSION BETWEEN RIB 14 - 15. REMOVED CORROSION IAW A300-600 SRM 51-74-10. ORIG THICKNESS .080 IAW AIRBUS DWG A55177703. MAT REMAINING .054. FOUND AREA TO BE OUT OF LIMITS IAW A300-600 SRM 55-10-00 PG 106 TNov 29, 2008 · N716FD · Airbus A300B4622SDR FDEA200811285034Spar Cap · corrodedR/H THS REAR SPAR UPPER TEE CAP HAS CORROSION AT RIB 3. REMOVED PANELS & NECESSARY SUB STRUCTURE TO FACILITATE MANTENANCE IAW SRM 51-40-21; ( RE-INSTALLED IAW SRM 51-40-21). REMOVED & RE-INSTALLED THE ELEVATOR PRESSURE & RETURN LINES & ELEVATOR CONTROL RODNov 28, 2008 · N716FD · Airbus A300B4622SDR DHLA2009743545Stringer · crackedVERTICAL STABILIZER, LT SIDE, AT FIN STA 133, STR 9 CRACKED AT WL 359. ACCOMPLISHED REPAIR TO STRINGER PER B727 SRM 55-30-3 FIG 2.Nov 24, 2008 · N743DH · Boeing 727225SDR AALA200810322Frame · crackedVERTICAL STABLIZER, LEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER RIGHT SIDE ZFS 30.00. REPAIRED PER AARD 55-30-00-2.Nov 13, 2008 · N948TW · Doug DC983SDR AALA200810325Frame · crackedLEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER LEFT STATION ZFS 36.500. INSTALLED REPAIR DOUBLER PER AARD 55-30-00-2.Nov 13, 2008 · N948TW · Doug DC983SDR CALA0801042Rib · crackedVERTICAL STABILIZER LEADING EDGE RIB AT STATION 235.90 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11.Nov 7, 2008 · N62631 · Boeing 737524SDR CALA0801041Rib · crackedVERTICAL STABILIZER LEADING EDGE RIB AT STATION 273.35 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11.Nov 7, 2008 · N62631 · Boeing 737524SDR CALA0801040Rib · crackedVERTICAL STABILIZER LEADING EDGE RIB AT STATION 292.07 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11.Nov 7, 2008 · N62631 · Boeing 737524SDR CALA0801039Rib · crackedVERTICAL STABILIZER LEADING EDGE RIB AT STATION 189.09 IS CRACKED ON RIGHT SIDE. REMOVED AND REPLACED CRACKED RIB AT STATION 189.09 PER SRM 51-40-02.Nov 6, 2008 · N62631 · Boeing 737524SDR DLM88081391Spar · crackedVERTICAL STABILIZER FRONT SPAR RT CHORD CRACKED THROUGH THREE FASTENER HOLES AT ZFS=52. DAMAGE CUT OUT OF FLANGE AND REINFORCED WITH A REPAIR ANGLE.Oct 20, 2008 · N941DL · Doug MD88SDR 08FDEA04101Spar Cap · crackedHFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK ON LEFT SIDE RADIUS OF LOWER FORWARD SPAR CAP AT LOWER VERTICAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 29, 2008 · N606FE · Doug MD11FSDR AALA200802556Spar · crackedRT VERTICAL STABILIZER FORWARD SPAR TANG CRACKED ON AFT SIDE OF CANTED FRAME AT STATION 1388. INSTALLED REPAIR ANGLE IN ACCORDANCE WITH AARD 55-30-00-08.Sep 24, 2008 · N571AA · Doug DC983SDR 08FDEA03974Spar Cap · crackedHFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK INDICATION ON RIGHT SIDE RADIUS OF LOWER SPAR CAP AT LOWER VERTICAL STABILIZER. REPAIRED AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11FSDR 08FDEA03973Spar Cap · crackedHFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK INDICATION ON ONE FASTENER TO EDGE OF LEFT LOWER FORWARD SPAR CAP FORWARD FLANGE AT LOWER VERTICAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 22, 2008 · N606FE · Doug MD11FSDR UPS08853529Rib · crackedINSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR EFN89419911115. ORIGINAL N/R 480 775. VERTICAL STABILIZER L/E LOWER SECTION NR 25 RIB CRACKED AFT LT FLANGE. RFTS N894UP-9-20284 RIVETS INSTALLED IN FREE STANDING LEG OF REPAIR. REMOVED RIVETS AND INSTALSep 21, 2008 · N894UP · Doug DC873FSDR CALA0800870Spar · corrodedVERTICAL STABILIZER HAS CORROSION AT FIN STATION 163.90 - 191.50 LEFT-SIDE AT REAR SPAR. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER EC/RA 5530-01510.Sep 5, 2008 · N76355 · Boeing 7373T0SDR AALA200802156Fitting · damagedAFW VERTICAL STABILIZER RIB FITTING AT RUDDER STATION 380.769 WAS DAMAGED FROM STATIC DISCHARGE. REPAIRED PER MRB 767 3269.Aug 5, 2008 · N328AA · Boeing 767223SDR KCSA081304Spar · corrodedVERTICAL STAB LEADING EDGE SPAR AT BL-0 FIN STA-225 SKIN DAMAGED (B)Jun 30, 2008 · N712CK · Boeing 747122SDR COEA0804911Spar · corrodedFOUND DURING HEAVY CHECK AT COE. FOUND LEVEL 2 CORROSION AROUND THE RIVET FILLED TOOLING HOLE ON THE AFT SURFACE OF VERTICAL STAB REAR SPAR. LOCATED IN THE CENTERLINE OF THE SHEAR WEB BETWEEN STIFFENERS (P/N`S S55371300230 AND S55371300225). REPAIRED PER SRJun 11, 2008 · N911FX · Aerosp ATR42300SDR COEA0809911Spar · corrodedFOUND DURING HEAVY CHECK AT COE. AFT SURFACE OF VERTICAL STAB REAR SPAR HAS AREAS OF SURFACE CORROSION BETWEEN LOWER & UPPER RUDDER ATTACH FITTINGS. REPAIRED PER SRAS DO/TS-2656/08-4694, NOTE DO/TS-2665/08-10353. CORROSION REMOVED FROM THE RIVET HOLE AREA PMay 30, 2008 · N911FX · Aerosp ATR42300SDR UPS08M53521Spar · corrodedINSPECTION TYPE:N/A VERTICAL STABILIZER FRONT SPAR RT AT STA ZFS 353.295 FOUND SURFACE CORROSION. SURFACE CORROSION ON VERTICAL STABILIZER FRONT SPAR RT AT STA ZFS 353.295 REMOVED AS PER SRM 51-21-01 VOL II REV 35. REWORKED AREA MATERIAL ORIGINAL THICKNESS 0May 20, 2008 · N296UP · Doug MD11FSDR 08FDEA01765Stringer · crackedSTRINGER 8R CRACKED AT RIB NR 8 STRINGER 8R, FIN STA 157.200 CRACK TERMINATES IN FASTENER HOLD AND HFEC INSPECTED AREA AND VERIFIED IAW NDTM 51.00.00 PART 6. FABRICATED REPAIR ANGLE IAW SRM 55.30.5 FIGURE 7. TREATED AND PRIMED AREA IAW SRM 51.10.2. INSTALLEMay 5, 2008 · N203FE · Boeing 7272S2FSDR 08FDEA01764Stringer · crackedSTRINGER 8L CRACKED AT RIB NR 8 STRINGER 8L, FIN STA 157.200 CRACK TERMINATES IN FASTENER HOLE AND HFEC INSPECTED AREA AND VERIFIED IAW NDTM 51.00.00 PART 6. FABRICATED REPAIR ANGLE IAW SRM 55.30.5 FIGURE 1. TREATED AND PRIMED PARTS IAW SRM 51.10.2. INSTALLMay 5, 2008 · N203FE · Boeing 7272S2FSDR UPS08M53543Spar · corrodedINSPECTION TYPE:N/A VERTICAL STABILIZER FRONT SPAR RT CUTOUT AT STA ZFS 516-443 APPROX FOUND MINOR CORROSION AS MARKED. VERTICAL STABILIZER FRONT SPAR RT CUTOUT STA ZFS 516.443 APPROX MINOR CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 35, Apr 3, 2008 · N295UP · Doug MD11FSDR USAA920080713Rib · crackedMIA - MAJOR REPAIR - PAINT LINE - VERTICAL STABILIZER HINGE RIB CRACKED. REPAIRED VERTICAL STABILIZER HINGE RIB IAW USAIRWAYS EA 100364.Mar 28, 2008 · N456UW · Boeing 7374B7SDR SWAA081323Fitting · corrodedDURING SCHEDULED 12Y CHECK, FOUND VERTICAL STABILIZER SPAR RT AND LT AFT OUTBOARD LUG FITTINGS CORRODED. REPAIRED FITTINGS PER MM.Mar 10, 2008 · N629SW · Boeing 7373H4SDR EPUA031608Rib · crackedCRACK DISCOVERED DURING ROUTINE INSP ON VERT STAB RIB FLANGE AT RIB STRINGER INTERSECTION 39.5 AND RIB 54.026 CANT STAB STA, RT SIDE. REPAIRED CRACK IAW WITH APPROVED DATA, AIRCRAFT RETURNED TO SERVICE.Mar 8, 2008 · N404GV · Beech 1900CSDR ABXR080086Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080085Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080082Rib · crackedRIB CRACKED AT FASTENER LEFT SIDE VERT STABILIZER LEADING EDGE ZFS 93. REPAIRED RIB IAW DC9 SRM D05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080084Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT VERT STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080081Rib · crackedRIB CRACKED AT FASTENER LEFT SIDE OF VERTICAL STAB LEADING EDGE XFS 148. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080078Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080077Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080076Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F
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