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 ABXR080075Rib · crackedRIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 23. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080083Rib · 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 ABXR080080Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 74. REPAIRED LEFT AND RIGHT RIBS IAW DC9 SSRM K05159.Feb 14, 2008 · N208US · Doug DC933FSDR ABXR080079Rib · crackedRIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 80. REPAIRED RIB IAW DC9 SSRM K05159.Feb 14, 2008 · N208US · Doug DC933FSDR USAA920080405Rib · crackedMCN - MAJOR REPAIR - C20 CHECK - VERTICAL STABILIZER LEADING EDGE RIB IS CRACKED, STABILIZER STATION 86.12. REPAIRED VERTICAL STABILIZER LEADING EDGE RIB, STABILIZER STATION 86.12 IAW USAIRWAYS EA 100232.Feb 11, 2008 · N313AW · Boeing 7373S3SDR USAA920080314Rib · crackedC4 CHECK, VERTICLE STABILIZER RIB CRACKED, BS1 1767.7. REPLACED VERTICLE STABILIZER RIB CRACKED, BS1 1767.7 IAW B767 SRM 55-30-09.Jan 25, 2008 · N252AU · Boeing 7672B7ERSDR 2008UALA00257Spar · gougedLEFT SIDE OF VERTICAL STABILIZER LOWER INTERSPAR SKIN IS GOUGED. REPLACED LOWER INTERSPAR SKIN.Jan 14, 2008 · N385UA · Boeing 737322SDR DHL2008765019Stringer · crackedDURING C CHECK, VERTICAL STABILIZER NR 8 STRINGER CRACKED FIN STATION 133. REMOVED PREVIOUS REPAIR FROM AREA IAW SRM 51-30-2. FABRICATED 2 EACH REPAIR ANGLES IAW SRM 55-30-5 FIGURE 1 AND 55-30-2 FIGURE 2. HFEC VERIFIED CRACK TERMINATES IN FASTENER HOLE IAW Jan 9, 2008 · N765AT · Boeing 727264SDR HSYA20080102Rib · crackedDURING SCHEDULED MX - SIM TASK 55-30-00 (1200 FLT HR/ 24 MO) REF. B1900 STRUCTURAL INSPECTION MANUAL, MX PERFORMED A VISUAL INSPECTION OF THE VERTICAL STABILIZER STRUCTURAL COMPONENTS AND FOUND RIB, AT CANTED STAB. STA. 69.184, CRACKED ON THE RT SIDE FLANGE ATJan 6, 2008 · N101UE · Beech 1900CSDR 07FDEA05098Spar · crackedVERTICAL STAB TIP L/E SPAR, CLOSER WEB HAS CRACK RUNNING THROUGH UPPER MOST FASTENER HOLE OF RIGHT SIDE TERMINAL FITTING LOCATION, 4.5" RBL. FABED DOUBLER, APPLIED ALODINE AND PRIMER AND INSTALLED REF DWG 65-17484, SRM 51- 10-2. CLASSIFIED AS A MINOR REPAIRDec 19, 2007 · N268FE · Boeing 727233SDR USAA920071151Spar · crackedCLT - MAJOR REPAIR - C16 CHECK, CRACKED VERTICLE STABILIZER LEFT AFT SPAR CHORD, RUDDER STATION 18. REPLACED VERTICLE STABILIZER LEFT AFT SPAR CHORD, RUDDER STATION 18 I/A/W B737 SRM 55-30-13.Nov 2, 2007 · N307AW · Boeing 7373G7SDR LR7A07111Longeron · crackedDURING SCHEDULED C-7 CHECK PER JOB CARD HC5511 FOUND LT & RT DORSAL FIN LOWER LONGERON REPAIR DOUBLER FOUND CRACKED AT FS 850. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA382-53-00-087 AND MEA382-53-00-088.Oct 1, 2007 · N404LC · Lkheed 382GSDR CA070921002Rib · cracked(CAN) CRACK FOUND IN VERTICAL STABILIZER AT RIB CSS 11.500. CRACK REPAIRED IAW SRM 51-70-17-001. CRACKED RIB REPAIR (NON-PRESSURIZED AREA). (TC NR 20070921002)Sep 19, 2007 · Beech 1900CSDR CA070906001Spar · cracked(CAN) CRACKS DISCOVERED ON BOTH SIDES OF STABILIZER THROUGH LOWER DOUBLER AT SPAR. FOUR RIVETS FOUND MISSING FROM FORWARD SPAR ATTACHMENT OF LOWER STABILIZER FRAME. (VISISBLE UPON REMOVAL ONLY) SUSPECT INCORRECT SHIMMING AT THIS TIME. (TC NR 20070906001)Aug 27, 2007 · Snias AS350BASDR UPS07850663Spar Cap · corrodedINSPECTION TYPE:C2 CORROSION ON VERTICAL STAB REAR SPAR CAP, RIGHT SIDE NEAR STA ZR=100. REPAIRED DAMAGED SPAR CAP ON VERTICAL STAB REAR SPAR CAP AT STA ZR=100 IAW SAA EA 008-5520-01-A1067, UPS RAA DC8-55-20108, AND FAA FORM 8100-9.Aug 22, 2007 · N801UP · Doug DC873FSDR UPS07850662Spar Cap · corrodedINSPECTION TYPE:C2 EXFOLIATING CORROSION ON VERTICAL STAB RIGHT AFT SPAR AT STA ZV299. REPAIRED DAMAGED VERTICAL STAB SPAR CAP AT STA ZV299 IAW SAA EA 008- 5520-01-A1074, UPS RAA DC8-55-20110, AND FAA FORM 8100-9.Aug 22, 2007 · N801UP · Doug DC873FSDR UPS07850661Spar Cap · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON INBOARD FACE OF VERTICAL STAB REAR SPAR LEFT CAP ABOVE NR 2 RUDDER HINGE ARM. REPAIRED DAMAGED VERTICAL STAB SPAR CAP ABOVE NR 2 RUDDER HINGE ARM IAW SAA EA 008-5520-01-A1073, UPS RAA DC8-55-20109, AND FAA FORM 8100-9.Aug 14, 2007 · N801UP · Doug DC873FSDR UPS07850660Spar Cap · corrodedINSPECTION TYPE:C2 CORROSION ON INBOARD FACE OF VERTICAL STAB REAR SPAR CAP RIGHT SIDE AT 6 BOLTS ABOVE 2ND HINGE ARM. REPAIRED DAMAGED AREA OF THE VERTICAL STAB REAR SPAR CAP IAW SAA EA 008-5520-01-A1073, UPS RAA DC8-55-20109, AND FAA FORM 8100-9.Aug 14, 2007 · N801UP · Doug DC873FSDR USAA070551Rib · chafedVERTICAL FIN FWD RIB BOTTOM LEFT & RIGHT SIDE AT STA 1007.55 CHAFED. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-09, 51-70-11; EA 98755, DEFECT SIZE: 8 AND 12 INCHES.Jul 17, 2007 · N417US · Boeing 737401SDR SWAA073357Rib · crackedDURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER RIB CRACKED AT STA 292.70. REMOVED AND REPLACED RIB PER SRM.Jul 6, 2007 · N650SW · Boeing 7373H4SDR 07FDEA02372Rib · crackedVERTICAL STABLIZER RIB NUMBER 2 LT OTBD CHORD CRACKED AT STRINGER 7. REMOVED DAMAGE, FABRICATED REPAIR PARTS, SENT TO HEAT TREAT, TRACKING NR 2007-06-203, DRILLED, TREATED, AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS REF SRM 55-30-5 FIG 1.Jul 5, 2007 · N481FE · Boeing 727227SDR DHL2007783522Support Angle · crackedVERTICAL STAB INTERNAL WEB LT UPPER ANGLE IS CRACKED STA 1323, SHORT WEB ANGLE W/L 259. REMOVED DAMAGED ANGLE VERITCAL STAB INTERIOR WEB IAW B727 SRM 51-30-2, FIG 7. VERIFIED MATERIAL TO BE 7075T6 IAW HARDNESS TESTER B727 SRM 51-10-3, FIG 2. FABRICATED NEW Jun 20, 2007 · N783DH · Boeing 727227SDR 07FDEA01802Rib · damagedVERTICAL STAB RT SIDE AT INTERSECTION OF ACCESS PANELS 323AL AND 323BR APPROX 2.5 INCHES FROM VERTICAL LOWER RIB EDGE 2 EACH WEAR MARKS APPROX .200 IN DIAMETER AND .050 DEEP BLENDED CHAF MARKS IAW A310 SRM 51-73-10 CHECKED LIMITS IA W A310 SRM 55-30-00 (OUT OFMay 15, 2007 · N410FE · Airbus A310203SDR 07FDEA01801Rib · damagedVERTICAL STAB RT SIDE AT INTERSECTION OF ACCESS PANELS 323AL AND 323BR APPROX 2.5 INCHES FROM VERTICAL LOWER RIB EDGE 2 EACH WEAR MARKS APPROX .200 IN DIAMETER AND .050 DEEP BLENDED CHAF MARKS IAW A310 SRM 51-73-10 CHECKED LIMITS IAW A310 SRM 55-30-00 (OUT OF May 15, 2007 · N410FE · Airbus A310203SDR CA070529005Spar · cracked(CAN) DURING AN ANNUAL/100 HOUR INSPECTION FIN AFT SPAR WAS FOUND CRACKED. MFG SINGLE ENGINE CUSTOMER CARE SERVICE INFORMTION LETTER SE 80-85 ADDRESSES THIS PROBLEM. SERVICE KIT SK 185-25A INSTALLED THIS DATE. (TC NR 20070529005)May 11, 2007 · Cessna A185FSDR F3LA200700098Rib · scratchedDURING C-3 CHECK, INSPECTION REPORTED LE OF VERTICAL STAB FIN HAD DEEP SCRATCH MARKS (TOOL MARKS) BETWEEN PANELS NR 322BL AND 322CL ON ATTACHMENT BRACKET WHERE PANEL 322BL ATTACHES. REPLACED RIB FOR VERT STAB LE BETWEEN PANELS 322BL AND 322CL IAW SRM 51-42-11Apr 25, 2007 · N801FR · Airbus A318111SDR DJFA2007039Rib · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A CRACK IN A VERTICAL STABILIZER RIB ABOVE THE ELEVATOR BELLCRANK MOUNTING BRACKET. CRACK WAS .5" LONG AND TERMINATED TO A TOOLING HOLE. CRACK WAS REPAIRED IAW ENGINEERING DATA.Mar 30, 2007 · N789TA · Beech 400ASDR 06FDEA04166Stringer · crackedVERTICAL STAB INTERIOR, STR 9 LT IS CRACKED AT RIB STA 110.4 REPAIRED PER FED EX EA 7-5530-100611.Dec 2, 2006 · N241FE · Boeing 727227SDR CA061124007Spar Cap · cracked(CAN) CRACK FOUND IN LT HAND SPAR CAP 1.5 IN. FROM BOTTOM. (TC NR 20061124007)Nov 24, 2006 · Gulstm 690SDR 06FDEA04091Rib · corrodedVERTICAL STAB FRONT SPAR FWD FACE ENTIRE LENGTH OF RT VERT STAB L/E HAS CORROSION UNDER NUT PLATES AND FASTENER HOLES. REMOVED CORROSION FROM RIB12-26 RT CHORD FLANGE CHECKED AND FOUND TO BE IN LIMITS IAW A310/200 SRM'S 51-74-10, 55-31-21.Nov 22, 2006 · N418FE · Airbus A310203SDR CA061027002Spar · cracked(CAN) DURING ANNUAL X-RAY INSPECTION OF THE VERTICAL STABILIZER, A CRACK WAS DETECTED ON THE LEFT HAND SIDE OF THE VERTICAL STABILIZER CENTRE SPAR AT THE 4TH FASTENER ABOVE THE DOUBLER. THE CRACK APPEARS TO RUN INTO THE RADIUS OF THE CENTRE SPAR. THE AIRCRAFT Oct 23, 2006 · Gulstm 690ASDR QXEA200602729Frame · crackedC3 PDX - 1/4 INCH CRACK IN FLANGE RADIUS OF EMPENNAGE OBLIQUE FRAME AT STATION X935, 11 O`CLOCK POSITION LEFT HAND SIDE OF CUTOUT FOR V-STAB FORWARD TUNNEL. REPAIRED IAW SRM 51-42-05, 51-40-10.Oct 7, 2006 · N414QX · Bombdr DHC8402SDR 06FDEA03434Stringer · crackedVERTICAL STAB, CRACK IN STR 8R, AT RIB NR 2. REMOVED DAMAGE ON VERTICAL STA STR 8R AT RIB NR 2 AND REPAIRED IAW SRM 55-30-4 FIG 1.Sep 26, 2006 · N285FE · Boeing 727233SDR 06FDEA03401Stringer · crackedFOUND VERTICAL STAB, CRACK IN STR 7R, AT RIB, FIN STA 133.8. REMOVED DAMAGE ON STR 7R AT RIB FIN STA 133.8 AND REPAIRED IAW SRM 55-30-4 FIG 1.Sep 22, 2006 · N285FE · Boeing 727233SDR QXEA200602518Spar · damagedC4 YYC - FORE RUDDER CENTER HINGE AREA, SPAR WEB HAS AREA OF TOOLING DAMAGE. REPAIRED IAW RD8-55-1742.Sep 11, 2006 · N357PH · Dhav DHC8202SDR K11A2008122372311Rib · corrodedUPPER CLOSURE RIB HAS CORROSION ON BOTTOM OF HORIZONTAL FLANGE, VERTICAL STAB STA 297.Sep 9, 2006 · N723CK · Boeing 7272H3SDR 06FDEA03162Rib · chafedVERT STAB RT AND LT FIN STA 55.9 PANEL SUPPORT RIB CHAFED. BLENDED DAMAGE, OUT OF LIMITS. FABRICATED REPAIR STRAP AND INSTALLED PER FED EX EA 7-5530-100583.Sep 1, 2006 · N282FE · Boeing 727233SDR LR7A06147Longeron · crackedDURING SCHEDULED C 2 CHECK PER JOB CARD HC5321, FOUND LT DORSAL FIN LONGERON CRACKED AT FS 836. REPAIRED LONGERON IAW LAC MEA 382-53-06-063.Aug 7, 2006 · N406LC · Lkheed 382GSDR 06FDEA2598Stringer · crackedFOUND VERTICAL STAB INTERIOR, STR 8L IS CRACKED AT NR 2 RIB. REMOVED DAMAGED AREA OF STR 8L AT NR 2 RIB AND REPAIRED IAW SRM 55-30-4.Jul 17, 2006 · N281FE · Boeing 727233SDR SWAA062297Web · chafedDURING SCHEDULED 18Y CHECK, FOUND VERTICAL STAB FWD WEB COMMON TO DORSAL FIN CHAFED. REPAIRED WEB PER SRM.Jul 5, 2006 · N346SW · Boeing 7373H4SDR 06FDEA2446Spar · chafedFOUND VERTICAL STAB LT MID SPAR CHORD FIN STA 225.71 CHAFED.Jul 3, 2006 · N281FE · Boeing 727233SDR DJFA2006275Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT A VERTICAL STABILIZER SUPPORT RIB WAS FOUND CRACKED. SUPPORT RIB PART NUMBER 45A23324-003 WAS REPLACED REFERENCING THE BEECHJET 400A STRUCTURAL REPAIR MANUAL.Jun 21, 2006 · N898TA · Beech 400ASDR 06FDEA2031Spar · corrodedFOUND VERT STAB SPAR BOX, LWR VERT STAB ATTACH BEAM HAS 11 AREAS OF CORROSION ON UPPER SURFACE REF N00367. REMOVED CORROSION IAW A310 SRM 51-74-10 1 EA AREA OUT OF LIMITS, REPAIRED AREA NR 11 IAW A310 SRM 55-31-19.May 26, 2006 · N427FE · Airbus A310203SDR TSAA0651039Spar · corrodedVERTICAL STABILIZER RIGHT T/E REAR SPAR CORROSION (3 AREAS).May 24, 2006 · N810AL · Boeing 7372Y5SDR 06FDEA1945Spar · chafedVERT FIN, LT MID SPAR HAS CHAFING DAMAGE AT FIN STA 225.71. REPAIRED PER FED EX EA 7-5530-100551,May 17, 2006 · N493FE · Boeing 727227SDR USAA060685Spar · gougedVERTICAL FIN FRONT SPAR RT AT FS 182 GOUGED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 97657, DEFECT SIZE: 3.9 INCH.May 10, 2006 · N529AU · Boeing 7373B7SDR USAA060684Spar · gougedVERTICAL FIN FRONT SPAR LT CHORD AT FS 182 GOUGED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 97657, DEFECT SIZE: 2.2 BY .4 INCH.May 10, 2006 · N529AU · Boeing 7373B7SDR 06FDEA1638Rib · gougedN00712 WHILE WORKING CARD NO. 73C023-00 (TAIL 43), FOUND VERT. FIN TENSION TIE RIB, LT VERT AFT BOLT HOLE HAS A GOUGE. REPAIRED BOLT HOLE IAW EA 7-5530-100866.Apr 29, 2006 · N493FE · Boeing 727200SDR 06FDEA1227Spar · chafedVERTICAL STAB JACKSCREW COMPARTMENT LWR MID SPAR CHORD CHAFED JUST FWD OF STAB SLIDING SEAL, FIN STA 230, LT SIDE. *S/D* REPAIRED PER FED EX EA 7-5530-96617.Mar 24, 2006 · N492FE · Boeing 727200SDR 06FDEA1226Spar · chafedVERTICAL STAB JACKSCREW COMPARTMENT LWR MID SPAR CHORD CHAFED JUST FWD OF STAB SLIDING SEAL, FIN STA 230, RT SIDE. *S/D* REPAIRED PER FED EX EA 7-5330-96617.Mar 24, 2006 · N492FE · Boeing 727200
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