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 DHL2005781550Frame · crackedDURING A "C" CHECK, FOLLOWING DISCREPANCIES WERE NOTED;VERT STAB FIN STA 180 STR 6R IS CRACKED AT FRAME ATTACH BOLT. REMOVED PANEL NR 9504 FOR ACCESS TPM FOR SHEET METAL REPAIR IAW B727 SRM 51-30-2. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED STIFFENER ANDFeb 16, 2005 · N781DH · Boeing 727227SDR 05FDEA00261Rib · corrodedVERTICAL STAB R&L TIP ATTACH FLANGES CORRODED AROUND HOLES AND UNDER NUT PLATES. REMOVED AND REPLACED RIB FLANGES IAW A310-200 SRM 51-72-10. APPLIED SURFACE PROTECTION IAW A310-200 SRM 51-73-10.Feb 7, 2005 · N405FE · Airbus A310203SDR 05FDEA00194Stringer · crackedSTRINGER CRACKED IN VERTICAL FIN AT FIN STA 180.6 STRINGER 3 LEFT. *S/D* FABRICATED AND INSTALLED REPAIR PARTS PER SRM 55-30-4 FIG 1.Jan 28, 2005 · N235FE · Boeing 727200SDR 05FDEA00193Stringer · crackedSTRINGER CRACKED IN VERTICAL FIN AT VERT FIN STA 110.4 STRINGER 7 LEFT. *S/D* REPAIRED PER SRM 55-30-4.Jan 28, 2005 · N235FE · Boeing 727200SDR 05FDEA00109Spar · crackedVERTICAL STABILIZER AFT CENTER SPAR HAS CRACK STATION ZFR 328, YV237.628. REMOVED PANEL AND WEB IAW DC10 SRM 51-35-01 VOL 2. REPAIRED CENTER SPAR DOUBLER IAW FEDEX EA 8-5530-83960, STABILIZER - VERTICAL AFT CENTER SPAR DOUBLER CRACK-REPAIR. REINSTALLED PANEJan 17, 2005 · N395FE · Doug DC1010SDR SWAA043647Spar · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR LT AND RT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED STAB PER ER.Dec 16, 2004 · N682SW · Boeing 7373Y0SDR QXEA200400808Frame · crackedPDX - VERTICAL STABILIZER FRAME 4 IS CRACKED AT STRINGER RT 4 IN AFT FUSELAGE SECTION. REPAIRED IAW RD 8-55-199.Nov 20, 2004 · N368PH · Dhav DHC8102SDR SWAA043111Spar · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR RT AND LT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STAB PER ER.Oct 26, 2004 · N601WN · Boeing 7373H4SDR SWAA043105Spar · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR RT AND LT PRIMARY CLEVIS FWD LUGS CORRODED. REPAIRED VERTICAL STAB PER ER.Oct 25, 2004 · N397SW · Boeing 7373H4SDR 04FDEA02967Spar Cap · corrodedEMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE FOUND CORRODED. EMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE CORROSION AREA REPAIRED AS PER FEDEX EAOct 22, 2004 · N602FE · Doug MD11FSDR 04FDEA02964Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR ZFR 328.0 LT SKIN EXTERIOR SURFACE FOUND CORRODED. CORROSION REMOVED & WITHIN LIMIT AS PER SRM55-00-01VOL1.Oct 21, 2004 · N602FE · Doug MD11FSDR 04FDEA02962Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BERWEEN ZFR 400.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED. FOUND WITHIN LIMIT AS PER FEDEX EA #1-5530-81581.Oct 21, 2004 · N602FE · Doug MD11FSDR 04FDEA02963Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR, ZID 92.50 LT SKIN EXTERIOR SURFACE FOUND CORRODED. CORROSION AREA REPAIRED AS PER FEDEX EA 1-5530-81582.Oct 21, 2004 · N602FE · Doug MD11FSDR 04FDEA02961Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BETWEEN ZID 92.50 TO ZFR 424.219 LT SKIN EXTERIOR SURFACE FOUND CORRODED. REMOVED & REPAIRED AS PER FEDEX EA 1-5530-81581.Oct 21, 2004 · N602FE · Doug MD11FSDR 04FDEA02960Spar · corrodedEMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR BERWEEN ZFR 389.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5530-81580.Oct 21, 2004 · N602FE · Doug MD11FSDR ASAA0480505Frame · gougedOKC - C-CHECK, VERTICAL STABILIZER PANEL 6308C, CUT OUT JAMB GOUGED AROUND LAND ORDERED AND INSTALLED NEW FRAME IAW SRM 51-30-2.Sep 24, 2004 · N973AS · Doug DC983SDR USAA040807Spar · crackedPIT, Q5, ANGLE SUPPORT .7500 INCH CRACK, VERT STAB SPAR ANGLE FOR RIB 163.90 FRONT LT SIDE. INSTALLED DOUBLER AND SHIM IAW EA 79100.Sep 9, 2004 · N383US · Boeing 7373B7SDR DHL2004801511Frame · crackedITEM REF. NR 2094: VERTICAL STAB L/E FORMER CRACKED 0.500 AT ZRS 173.000 (LT). REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21.PERFOMED STOP DRILL AND FABRICATED ANGLE. DOUBLER IAW SRM 55-2-0 PAGE 7,8 CLEANED TREATED AND PRIMED IAW SRM 51-1-8BSep 2, 2004 · N801DH · Doug DC873FSDR DHL2004801512Rib · crackedVERTICAL STABILIZER L/E FORMER CRACKED 0.500 AT ZRS 104.000 (LT). MED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL- 2024-T3, 0.032") IAW SRM 55-2-0 PAGE 7,8.CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51Sep 2, 2004 · N801DH · Doug DC873FSDR M562004F00000Spar · corrodedVERTICAL STABILIIZER REAR SPAR RT CHORD CORROSION BETWEEN FIN STA 66.35 AND 90.30. CORROSION ON SURFACE ONLY FROM .018 INCH TO .084 INCH DEEP. BLENDING CORROSION IAW MFG ENGINEERING INSTRUCTIONS.Jul 21, 2004 · N37NY · Boeing 7374Y0SDR 2004F00352Spar · crackedVISUAL INSPECTION OF VERTICAL FIN ATTACHMENT REVEALED APPARENT CRACK IN FRONT SPAR REINFORCING ANGLE AT RIGHT LOWER ATTACHMENT BUSHING. CRACK WAS VERIFIED BY DYE PENETRANT INSPECTION. (M)Jun 24, 2004 · N3536B · Piper PA31350SDR IXXA060322SSpar · corrodedDURING ROUTINE C CHECK FOUND VERTICAL STABILIZER RIGHT SIDE REAR SPAR INTERNAL AREA CORRODED AT STATION ZV299. REPAIRED PER ALL APPLICABLE DATA.Jun 10, 2004 · N41CX · Doug DC862FSDR SO1550Rib · crackedDURING HIDDEN DAMAGE INSPECTION AFTER BIRDSTRIKE ON VERTICAL STABILIZER LEADING EDGE, FOUND FORMING RIB ASSY CRACKED. REPLACED WITH NEW PART.Jun 10, 2004 · N1951F · Cessna 172NSDR ABXA040186Rib · crackedREMOVEABLE VERTICAL LEADING EDGE SECTION 5TH RIB UPON RIGHT SIDE CRACKED AT AFT END. REPAIRED RIB IAW DC-9 SSRM K05159.May 13, 2004 · N976AX · Doug DC941SDR ABXA040185Rib · crackedREMOVEABLE VERTICAL LEADING EDGE SECTION 6TH RIB UP ON RIGHT SIDE CRACKED AT AFT END. REPAIRED RIB IAW DC-9 SSRM K05159.May 13, 2004 · N976AX · Doug DC941SDR ABXA040187Rib · cracked2ND RIB DOWN FROM REMOVEABLE VERTICAL LEADING EDGE SECTION CRACKED ON RIGHT AFT SIDE. REPAIRED IAW ABX SSRM K05159 DRAWING.May 13, 2004 · N976AX · Doug DC941SDR 04FDEA01152Rib · corrodedVERTICAL STABILIZER TRAILING EDGE ON RIGHT SIDE EDGE FOR ACCESS PANEL ATTACHMENT STRUCTURE, PROPAGATION OF CORROSION NOTED FROM RIB 12-17, AS MARKED. REMOVED CORROSION IAW A310-200 SRM 51-74-10. REPAIRED IAW FEDEX EA 6-5530-77658 AND SRM A310-200 51-74-10 ANMay 4, 2004 · N428FE · Airbus A310203SDR 04FDEA00736Spar · chafedVERTICAL STAB MID SPAR CHAFED AT PANEL 9601 (LT SIDE). REPAIRED DAMAGED AREA ON VERTICAL STAB MID SPAR BEHIND PANEL 9601 PER FED EX EA 7-5530-76229 AND SRM 55-30-6 FIG 3.Mar 23, 2004 · N282FE · Boeing 727200SDR 04FDEA00735Spar · chafedVERTICAL STAB MID SPAR CHAFED AT PANEL 9602 (RT SIDE). REPAIRED THE RT VERTICAL MID SPAR AT PANEL 9602 IAW FED EX EA 7-5530-76229 AND SRM 55-30-6 FIG 3.Mar 23, 2004 · N282FE · Boeing 727200SDR GTIA040393Rib · corrodedFTW - FOUND VERTICAL STAB LOWER DORSAL FIN ACCESS PANEL SUPPORT MATING SURFACES CORRODED, SEVERAL NUTPLATES CORRODED AND MISSING. AFTER FURTHER EVALUATION, FOUND RIB CRACKED. DORSAL FIN PANEL SUPPORT FOUND TO BE OUT OF LIMITS. FABRICATED NEW PANEL SUPPORT. Mar 22, 2004 · N836NK · Doug DC983SDR DHL2004803516Frame · crackedVERTICAL STABILIZER L/E FORMER CRACKED 0.500 (LT SIDE) AT ZFS 86.000. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3AL 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLEDMar 19, 2004 · N803DH · Doug DC873SDR DHL2004803510Frame · crackedVERTICAL STABILIZER L/E FRAME CRACKED 2.000 AT FS 98.000 (LT SIDE). PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGMar 19, 2004 · N803DH · Doug DC873SDR DHL2004803509Frame · crackedVERTICAL STAB L/E FRAME CRACKED 2.000 AT STA 105.000 (RT SIDE). STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAWMar 19, 2004 · N803DH · Doug DC873SDR DHL2004803512Rib · crackedVERTICAL STABILIZER L/E FORMER CRACKED 0.500 STA. XFS 110.000 (LT SIDE). PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) UAW SRN 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLMar 19, 2004 · N803DH · Doug DC873SDR SWAA040408Spar · corrodedDURING SCHEDULED D CHECK, FOUND CORROSION ON VERTICAL STAB FRONT SPAR RT LUG FORWARD AND AFT FACES. REPAIRED STAB PER EO.Feb 8, 2004 · N665WN · Boeing 7373Y0SDR 04FDEA00332Stringer · crackedVERTICAL STAB LT STRINGER CRACKED, FIN STA 157.2 STR NR 7 FROM TOP, AT BOLT HOLE. REPAIRED CRACKED STRINGER NR 7L FIN STA 157.2 PER SRM 55-30-4 FIG 1.Feb 6, 2004 · N288FE · Boeing 727200SDR QXEA200400033Frame · crackedPDX - VERTICAL STABILIZER FRAME NR 4 HAS A CRACK APPROXIMATELY 3.4 INCH LONG WHERE FRAME MEETS UP WITH THE 4TH STRINGER FROM THE TOP RIGHT SIDE OF FUSELAGE. REPAIRED IAW RD 8-55-199.Jan 2, 2004 · N354PH · Dhav DHC8202SDR QXEA200400032Frame · crackedPDX - VERTICAL STABILIZER FRAME NR 4 HAS A CRACK IN IT WHERE FRAME MEETS UP WITH THE FOURTH STRINGER FROM THE TOP LEFT OF FUSELAGE. REPAIRED IAW RD8-55-199.Jan 2, 2004 · N354PH · Dhav DHC8202SDR AMWA110Rib · crackedDURING INSPECTION FOUR CRACKS FOUND ON THIS RIB, TWO ON THE LT SIDE AND TWO ON THE RT SIDE LOCATED ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46 & 101-640000-38. LT STRINGER P/N 101-640000-39 & 101-640000-45.Dec 22, 2003 · N139ZV · Beech 1900DSDR AMWA109Rib · crackedDURING INSPECTION, FIVE CRACKS FOUND IN THIS RIB, THREE ON THE RT SIDE AND TWO ON THE LT SIDE LOCATED ON THE STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-45, 101-640000-42 & 101-640000-38. LT STRINGER P/N 101-640000-43, 10Dec 22, 2003 · N139ZV · Beech 1900DSDR AMWA107Rib · crackedDURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON THE LT SIDE AT STRINGER TO RIB INTERSECTION STRINGER. P/N 101-640000-39.Dec 22, 2003 · N139ZV · Beech 1900DSDR AMWA108Rib · crackedDURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON RT SIDE ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46.Dec 22, 2003 · N139ZV · Beech 1900DSDR 03FDEA02168Stringer · crackedVERTICAL FIN STR 8L AT FIN STA 180 IS CRACKED.Dec 11, 2003 · N287FE · Boeing 727200SDR 03FDEA02166Stringer · crackedVERTICAL FIN STR 8L AT FIN STA 133 IS CRACKED ** SD ** COMINGDec 11, 2003 · N287FE · Boeing 727200SDR LR7A03111Longeron · crackedDURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND FS 902 DORSAL FIN LONGERON CRACKED AT LBL 13 & RBL 13, WL 285. REPAIRED IAW LAC MEA 382-53-03-076. NR 2054.Dec 4, 2003 · N405LC · Lkheed 382GSDR AMWA87Rib · crackedDURING THE D-6 INSPECTION THERE WAS TWO CRACKS FOUND ON THE RIB ON RT SIDE AT STRINGER. CRACK LOCATED AT END OF RIVET ON JOGGLE OVER STRINGER. RIB NR 3 FROM TOP. REPAIRED CRACKS IAW BMM. P/N 101-640000-25, 39.289Nov 26, 2003 · N138YV · Beech 1900DSDR AMWA86Rib · crackedDURING THE D-6 INSPECTION THERE WERE TWO CRACKS FOUND AT THE LOWER RT SIDE VERTICAL RIB ON JOGGLE THROUGH RIVET HOLE. REPAIRED CRACKS IAW BMM. P/N 101-640000-21, 54.026Nov 26, 2003 · N138YV · Beech 1900DSDR AMWA85Rib · crackedDURING THE D-6 INSPECTION. THERE WAS TWO CRACKS FOUND AT THE UPPER RIB LT AT BOTH SLOTS FOR STRINGER. REPAIRED CRACKS IAW BMM. P/N 101-640000-17,69.184Nov 26, 2003 · N138YV · Beech 1900DSDR AMWA84Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB., THE RIB FLANGES AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE LEFT SIDE AT THE CENTER STRINGER. REPAIRED CRACKS TO RIB FLANGE IAW BMM P/N 114-590021-9, 51-70-03.Nov 14, 2003 · N10675 · Beech 1900DSDR AMWA83Rib · crackedWHILE PERFORMING AND INSPECTION IN THE VERT. STAB., THE RIB FLANGES AT CANTED STAB STA 54.026 WERE FOUND CRACKED IN FOUR PLACES ON THE LEFT AND TWO PLACES ON THE RIGHT. REPAIRED CRACKS TO RIB FLANGE IAW BMM P/N 114-590021-9, 51-70-03Nov 14, 2003 · N10675 · Beech 1900D
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