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 GUUA94955040511ARib · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STABILIZER LT SIDE, 1 CRACK AT CSS 54.026. STOP DRILLED CRACK AND INSTALLED REPAIR STRAP.Apr 5, 2011 · N69549 · Beech 1900DSDR DALA1123059878Angle · chafedVERTICAL STABILIZER REAR SPAR Z-ANGLE FOR ACCESS PANEL 6404A IS CHAFED THROUGH AT FASTENER HOLE. REMOVED DAMAGED ANGLE. RECEIVED REPAIR MATERIAL. FABRICATED, DRILLED, FITTED, TREAT & PRIME & INSTALLED IAW DC-9 SRM 51-70-5, 51-10-3, 51-30-5 & 51-31-0.Mar 29, 2011 · N787NC · Doug DC951SDR GUUA95755032411BRib · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL CANTED STABILIZER RIB CRACKS AT RIGHT NR 4 STRINGER AT STATION 89.184. STOP DIRILLED CRACK AT RIGHT VERTICAL STABILIZER RIB NR 4 STRINGER AND INSTALLED REPAIR DOUBLERS.Mar 24, 2011 · N87557 · Beech 1900DSDR GUUA95755032411ARib · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL CANTED STABILIZER RIB CRACKS AT LEFT NR 2, 3 AND 4 STRINGERS AND RIGHT NR 3 STRINGER AT STATION 54.026. STOP DIRILLED ALL CRACKS VERTICAL STABILIZER RIBS LEFT AND RIGHT SIDE AND INSTALLED REPAIR DOUBLEMar 24, 2011 · N87557 · Beech 1900DSDR DALA1114999877Rib · crackedLT SIDE VERTICAL STABILIZER STA ZFS43 HAS A CRACK FROM FASTENER HOLE. AT FIFTH OPEN HOLE 3 INCHES LONG FROM THE BOTTOM OF THE RIB (LT) THAT EXTENDS ON OTBD FLANGE FWD AND TERMINATES AT OPEN HOLE OF RIB SUPPORT, STA ZFS43 IAW SPM 06-10-01.001. FABBED REPAIR PFeb 21, 2011 · N786NC · Doug DC951SDR CA110211013Rib · crackedWHILE DOING PHASE INSP, THE SQUEEZE TEST FOUND CRACKED FWD TABS ON SEVERAL VERTICAL STABILIZER NOSE RIBS. THE SAME DEFECTS WERE FOUND ON 2 OTHER ACFT OUT OF 9 ACFT THAT WERE CHECKED. SOME OF THE TABS APPEAR TO HAVE BEEN BROKEN FOR AN EXTENDED TIME. REPAIRS AFeb 11, 2011 · Gulstm 690SDR DALA1106059857Frame · crackedAFT ACCY COMPARTMENT ABOVE Y-DUCT WHERE VERT STABILIZER LT ATTACH BOLT FITTING IS LOCATED, FRAME HAS 2 EACH CRACKS. REMOVED CRACKED FRAME IAW SRM 51-30-5. LOCATED, DRILLED AND INSTALLED NEW FRAME, CUSTOMER FURNISHED PART IAW SRM 51-10-4 & 51-30-5.Jan 25, 2011 · N766NC · Doug DC951SDR FDEA201101060058Rib · corrodedVERTICAL STABILIZER, RIB 1 TOP SURFACE HAS CORROSION (ABOUT 4 SQ INCHES) RT STRINGER 5 RT TO STR 7 RT. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW SRM 53-31-19, PG 209-211, FIG 203.Jan 6, 2011 · N423FE · Airbus A310203SDR FDEA201101060045Spar · crackedCRACK AT FRONT SPAR CONNECTING SECTION AT RIB 1,2.5 INCH LONG. REMOVED TRANSVERSE FITTING AT VERTICAL STAB FWD SPAR RIB 1 AND REMOVED CONNECTION SECTION AT RIB 1 IAW SRM 51-72-10 PG 1-3. CLEANED AREA IAW AMM 12-21-11. REPROTECTED AREA IAW SRM 51-75-10 PG 3Jan 6, 2011 · N443FE · Airbus A310203SDR FDEA201101060025Angle · corrodedVERTICAL STABILIZER REAR SPAR FWD FACE RIB 9, HORIZ ANGLE HAS CORROSION ABOUT 3 SQ INCHES. REMOVED HORIZONTAL ANGLE AT FWD FACE OF RIB 9 IAW SRM 51-40-21, PG 22 PARA 7. REMOVED CORROSION IAW SRM 51-74-10, PG 205, PARA 3. NOMINAL THICKNESS IS 0.063, REMAINJan 6, 2011 · N443FE · Airbus A310203SDR FDEA201101060023Rib · corrodedVERTICAL STABILIZER INTERIOR DIAGONAL ANGLE AT RT JOINT OF RIB 9 AND STR 2 HAS CORROSION ABOUT 4 SQ INCHES. REMOVED DIAGONAL BRACE AT RIB 10 AND REAR SPAR ON VERTICAL STABILIZER IAW SRM 51-72-10, PG 1-3. REMOVED CORROSION IAW SRM 51-76-10, PG 205, PARA 6. Jan 6, 2011 · N443FE · Airbus A310203SDR FDEA201101050014Rib · corrodedVERTICAL STABILIZER RIB 1 WEB TOP SURFACE HAS CORROSION ( ABOUT 4 - SQUARE INCHES) RT STRINGER 5R TO STRINGER 7R VERT STAB RT SIDE REMOVED CORRODED SECTION ON RIB1 WEB BETWEEN STR 5R AND 7R IAW SRM 55-31-19, PG 209 - 210 FIG 203. FABRICATED AND INSTALLED REJan 5, 2011 · N423FE · Airbus A310203SDR FDEA201101050013Spar · gougedBETWEEN AFT SPAR AND RUDDER RIB STA 97.354 LT SIDE HAS 2 GOUGES. REPAIRED DAMAGE IAW EA F-5530-143212. STABILIZER-VERTICAL-ELONGATED HOLES IN TRAILING RIB. MAJOR REPAIR.Jan 5, 2011 · N993FD · Boeing 7572Q8SDR DALA1103270961Spar · crackedVERTICAL STAB LT SPAR CHORD ZFS 52 DAMAGED HOLE. REPAIRED IAW ERA 488672-14.Jan 3, 2011 · N961DL · Doug MD88SDR DALA1516370907Spar · not reportedVERTICAL STABILIZER FRONT SPAR RT CHORD ZFS=52 REPAIRED IAW ERA 484065-14.Dec 30, 2010 · N907DL · Doug MD88SDR DALA1034440947Spar · damagedVERTICAL STABILIZER FRONT SPAR RT CHORD ZFS=52, OVERSIZED HOLES REPAIRED IAW ERA 487648-14 REV A.Nov 22, 2010 · N947DL · Doug MD88SDR DALA1029309003Spar · damagedELONGATED HOLE ON VERTICAL STAB LT FRONT SPAR CHORD FLANGE ZFS=66.500. REPAIR PER ERA 485915-14 REV ORG. (DLM88102899)Oct 23, 2010 · N903DE · Doug MD88SDR DALA1027880908Spar · crackedVERT STAB FRONT SPAR CHORD BHEC REVEALED CRACK INDICATION AT RT SIDE VERT STAB FRONT SPAR CHORD FORWARD FLANGE AT FIRST FASTENER HOLE BELOW ZFS 52. REPAIRED PER ERA 486620-14 REV ORIG ON N/R 103. (DLM88102844)Oct 18, 2010 · N908DL · Doug MD88SDR K11A2010121472601Rib · crackedVERTICAL STAB RIB CRACKED, LT SIDE AT STA 133.8.Oct 9, 2010 · N726CK · Boeing 7272M7SDR USAA2010090791930Fitting · wornSAL - Q4 - MAJOR REPAIR - WEAR ON FRONT SPAR ATTACH FITTING LEFT AFT LUG AFT FACE ON VERTICAL STABILIZER AT LBBL 11.55. REPAIRED FRONT SPAR ATTACH FITTING LEFT AFT LUG AFT FACE ON VERTICAL STABILIZER AT LBBL 11.55 IAW EA 133018.Sep 2, 2010 · N530AU · Boeing 7373B7SDR DALA1020580928Spar · damagedDURING FASTENER REMOVAL FOR ACCOMPLISHMENT OF EA 09-482741-14MA, OPN 8901 HAD ELONGATED HOLE ON VERTICAL STABILIZER LT FRONT SPAR CHORD COMMON TO CHORD AND OVERLYING SKIN PERFORMED TIME LIMITED REPAIR IAW ERA 484939-14 REV ORIG REPAIR LIMITED TO 24 MONTHS UNLEAug 19, 2010 · N928DL · Doug MD88SDR EE4Y1010346Stringer · cracked(EE4Y) EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, ST STA 157 STR 7L CRACKED.Aug 17, 2010 · N762AT · Boeing 7272B7SDR EE4Y1010345Stringer · crackedEMPENNAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8R AT STA 180 CRACKED.Aug 17, 2010 · N762AT · Boeing 7272B7SDR EE4Y1010344Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 6L CRACKED AT STA 180.Aug 17, 2010 · N762AT · Boeing 7272B7SDR EE4Y1010343Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY,STR 5L AT STA 22.5 AND STA 157 WITH CRACK.Aug 17, 2010 · N762AT · Boeing 7272B7SDR EE4Y1010342Stringer · crackedEMPENAGE VERTICAL STABILIZER CAVITY,STR 9L CRACKED AT STA 110.Aug 17, 2010 · N762AT · Boeing 7272B7SDR EE4Y1010341Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8L CRACKED AT STA 157, STA 133 AND STA 22.5.Aug 17, 2010 · N762AT · Boeing 7272B7SDR QXEA2010080500455Spar · damagedC5 CHECK- HORIZONTAL STAB FWD SPAR HAS SEVERAL SMOKING RIVETS ON THE INBD RT AND LT SIDES. REPLACED RIVETS IAW SRM 51-42-45. CLEANED AND INSPECTED AREA FOUND NO FURTHER LOOSE RIVETS. FOUND STAINING TO BE FROM WATER SEEPING FROM THE L/E. NO DAMAGE CAUSED TO TAug 1, 2010 · N410QX · Bombdr DHC8402SDR IPXA10561087Rib · chafedINSPECTION TYPE:C3, VERTICAL STAB (LOWER END) FIXED TO FUSE IS CHAFED ON THE FWD BULKHEAD FWD SKIN FSS 69.750-92.250. REMOVED END, REPLACED RIB ALODINED AND PRIMED IAW SRM 51-40-01-0G, SRM 51-20-00-0.Jul 12, 2010 · N421UP · Boeing 75724APFSDR FDEA201007082406Spar · corrodedVERTICAL STAB T/E PANEL ATTACH ANGLEAT RT SIDE HAS APPROX 2 SQ INCH OF VISIBLE CORROSION BETWEEN RIB 9 AND AT RIB 10 AT STA 286 AND 309 (2 EA LOCATIONS) BETWEEN RIB. REMOVED CORROSION FROM VERTICAL STAB T/E PANEL ATTACH ANGLE RT SIDE BETWEEN RIB 9 AND RJul 8, 2010 · N402FE · Airbus A310203SDR CA100608009Spar · crackedAFT ATTACH POINT SPAR RADIUS FOUND CRACKED ON A WALK AROUND - VERTICAL FIN.Jun 3, 2010 · Airtrc AT802ASDR DALA1012880906Spar · crackedVERT STAB LT SPAR CHORD CRACK. REPAIRED IAW ERA 482730-14 ON NR 73. (DLM88101466)May 20, 2010 · N906DL · Doug MD88SDR DALA1012870906Spar · crackedVERT STAB RT SPAR CHORD 2 HOLES CRACKED BELOW ZFS 52. REPAIRED ON NR 72 IAW ERA 482731-14. (DLM88101465)May 20, 2010 · N906DL · Doug MD88SDR DLM88101232Spar · damagedVERTICAL STAB FRONT SPAR UPPER RT CHORD HAD OVERSIZED HOLES AND WAS REPAIRED IAW ERA 482312-14.May 14, 2010 · N929DL · Doug MD88SDR 2010FA0000334Stiffener · corrodedDURING REPLACEMENT OF RUDDER HINGE BRACKETS ON VERTICAL STABILIZERS REAR SPAR, EXFOLIATION CORROSION WAS FOUND ON THE LOWER BRACKET (P/N: 6931050-10) OF THE UPPER RUDDER HINGE POINT, LOWER BRACKET (P/N: 6931050-12) & UPPER BRACKET (P/N: 6931050-11) OF THE MIDDApr 9, 2010 · N365QS · Cessna 680CESDR DLM88100782Spar · crackedVERTICAL STABILIZER FRONT SPAR CHORD ZFS52 FATIGUE CRACKS.Mar 22, 2010 · N915DL · Doug MD88SDR DLM88100184Spar · crackedTHE FIRST FASTENER HOLE BELOW ZFS-52 ON THE RT CHORD OF VERTICAL STABILIZER FRONT SPAR WAS FOUND WITH A CRACK INDICATION. THE INSP IS BEING ACCOMPLISHED IAW EO 09-470871-12. REPAIRED IAW ER/A 479449-14 REV ORIG.Jan 24, 2010 · N957DL · Doug MD88SDR USAA2010012590179Spar · crackedSAL - Q4 - MAJOR REPAIR - CRACK ON VERTICAL STABILIZER LEFT SPAR CHORD ASSEMBLY BETWEEN STAB STA 237.5 TO STAB STA 255.9, WL 175. REPAIRED VERTICAL STABILIZER LEFT SPAR CHORD IAW EA 132834.Jan 4, 2010 · N450UW · Boeing 7374B7SDR 2010FA0000022Spar · crackedTOP RUDDER ATTACH BRACKET CRACKED OUT OF REAR SPAR ON THE VERTICAL FIN. NOTICED CRACK AT ANNUAL INSPECTION. POSSIBLY INSTALL A HEAVIER REAR SPAR OR BEEF UPS IN THAT AREA.Jan 4, 2010 · N4999X · Ayres S2RSDR ABXR200912180048Rib · crackedDURING A ROUTINE HEAVY MX VISIT HAD CRACK INDICATION AT A FASTENER FOR 2 EACH RIBS ON THE RT SIDE OF THE LWR SECTION OF THE VERTICLE STAB. STOP DRILLED CRACK IAW SRM 55-02, FIG 27, FABRICATED REPAIR DOUBLERS USING .0407075-T6 IAW SRM 55-31-00. ITEM WAS RETURDec 18, 2009 · N327US · Doug DC933FSDR DLM88091858Spar · crackedVERTICAL STABILIZER FRONT SPAR CHORD BHEC CRACK INDICATION AT RT SIDE SECOND FASTENER ABOVE ZFS 52 REF EA 09-470871-12. REPAIRED PER ER/A 478340-14 ORIG.Nov 22, 2009 · N930DL · Doug MD88SDR DLM88091749Spar · crackedCRACK INDICATION FOUND AT TWO HOLES COMMON TO THE VERTICAL STABILIZER FRONT SPAR LIGHT AND RT CHORDS, AT LOWER SKIN PANEL. THE TWO DAMAGED HOLES ARE EXACTLY SITUATED AT THE UPPER MOST LOCATION OF THE SKIN PANEL (6TH HOLE FROM BOTTOM OF THE INSPECTION AREAS ON Nov 3, 2009 · N924DL · Doug MD88SDR FDEA200911023791Spar Cap · crackedCRACK INDICATION FOUND DURING HFEC INSP ON LT OF THE LWR VERTICAL STABILIZER FWD FLANGE OF UPPER REAR SPAR CAP. REPAIR CARRIED OUT ON LT LWR VERTICAL STABILIZER FWD OF UPPER REAR SPAR CAP IAW SRM 55-30-02. REPAIR 3 REV 41 AND EA 1-5530-135661. REPAIR CLASSINov 2, 2009 · N598FE · Doug MD11FSDR CA091022005Spar · corroded(CAN) DURING A VERTICAL STAB SPAR INSPECTION PER CESSNA CARAVAN 208B SUPPLEMENTAL INSPECTION NUMBER 55-30-01, PART OF A 20,000 HOUR INSPECTION, FRETTING DAMAGE WAS FOUND AT VERTICAL STABILIZER REAR SPAR WEB AT W.L. 134.00. THERE WAS NO CORROSION DETECTED WHEREOct 13, 2009 · Cessna 208BSDR FDEA200909153299Fitting · crackedLWR VERT STAB, RT SIDE FWD FLANGE OF UPPER REAR SPAR CAP BETWEEN FIRST AND SECOND LOWEST FASTENER FOUND APPROX 1 INCH CRACKED. RT LWR VERTICAL STABILIZER FWD FLANGE UPPER REAR SPAR CAP AREA REPAIRED IAW SRM 55-30-02, FIGURE 201, REPAIR 3, REVISION 41. FABRSep 15, 2009 · N522FE · Doug MD11FSDR SWAA095656Spar · corrodedDURING SCHEDULED MV1 CHECK, FOUND RT VERTICAL STABILIZER AFT SPAR CORRODED AT STA 209.90. REMOVED AND REPLACED VERTICAL STABILIZER PER MM.Sep 1, 2009 · N657SW · Boeing 7373L9SDR DLM88091422Spar · crackedDURING INSPECTION PER EO 09-470871-12 FOUND RT VERTICAL SPAR CHORD CRACKED AT ONE FASTENER HOLE ABOVE ZFS=52. HOLE WAS OVER SIZED AND BUSHED PER ER/A 476785-14 ORIG.Aug 31, 2009 · N956DL · Doug MD88SDR DLM88091421Spar · crackedDURING L/C INSP PER EA 09-470871-12 FOUND RT SPAR CHORD OF VERTICAL STABILIZER ABOVE ZFS=52 WAS CRACKED IN ONE FASTENER HOLE. A/C WAS GROUNDED AND PART REPAIRED PER ER/A 476845-14 ORIG. ALSO VERTICAL LEADING EDGE WAS FOUND WITH SKIN FASTENER HOLES ELONGATED Aug 31, 2009 · N956DL · Doug MD88SDR IPXA09556543Skin · puncturedINSPECTION TYPE:C2 VERT STAB ACCESS PANEL 322BL INNER SKIN PUNCTURED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER, PREPARED SURFACE FOR BONDING POTTED CORE. INSTALLED DOUBLER AND CURED, REV B757-5530-34101. THIS REPAIR IS TIME LIMITED UNTIL JUNE29,2011.Jun 17, 2009 · N467UP · Boeing 75724APFSDR GUUA95055061509ASpar Cap · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED SURFACE CORROSION ON VERTICAL STABILIZER LT AND RT SPAR CAPS, LT CAP BETWEEN CSS 39.289 AND 46.289 AND RT CAP BETWEEN CSS 53.026 AND 55.026. CLEANED CORROSION AND INSTALLED REPAIR STRAP IN CORRODED AREA BETWEEN CSS 53.Jun 15, 2009 · N87550 · Beech 1900D
Back to JASC 5531