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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AMWA42Rib · crackedRIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 FIRST STRG FWD OF AFT SPAR RT SIDE OF VERTICAL STABILIZER.SDR AMWA30Rib · crackedWHILE PERFORMING INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE TO BEECH SRM MANUAL P/N 114-590021-9, 51-70-03.SDR AMWA29Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03.SDR AMWA28Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH SRM P/N 114-590021-9, 51-70-03.SDR AMWA24Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.SDR AMWA23Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.SDR AMWA22Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.SDR AMWA20Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB, STA 39.289 AND STAB 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL REPAIR MANUAL P/N 114-590021-9, 51-70-03.SDR 53738Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STABILIZER, THE RIB FLANGES AT CANTED STAB STA. 39.289 AND STAB STA. 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IAW STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03SDR 03FDEA01241Spar Cap · corrodedMDIS 311 55-30 0008866 05AUG03 BFM CLOSE COMPLY WITH E.A.8-5530-72245. STABILIZER-VERT-REWORK OF CORROSION ON SPARS AMC7107 AND AMC7185 ENT BY3A 60601C RPT BY 3A 60601C. FACT 08AUG03 19 PERCENT 3A29 BFM COMPLIED WITH EA 8-5530-72245 STABILIZER-VERT-REWORK SDR AUS20030757Doubler · corroded(AUS) VERTICAL STABILISER FORWARD SPAR DOUBLER ASSEMBLY CONTAINED EXFOLIATION CORROSION.SDR AWXA200300881Rib · chafedLCQ - MAJOR REPAIR - DURING C-17 CHECK THE FORWARD VERTICAL STABILIZER LT AND RT RIB ASSEMBLIES HAVE CHAFED AREAS AT BS 1006. MAINTENANCE REMOVED VERTICAL STABILIZER LT AND RT RIB ASSEMBLIES; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-30SDR 2003F00551Rib · crackedAT SCHEDULED EMPANNAGE ZONAL INSPECTION, VERTICAL STABILIZER TOP FORWARD RIB SHOWING CRACK ON RIGHT SIDE. STOPPED DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER REPAIR IAW 1900D STRUCTURAL REPAIR MANUAL, CHAPTER 51-70-05. (M)SDR MWEA030261Frame · damagedSTATION 1420 FRAME LOCATED INSIDE THE VERTICAL STABILIZER IS DAMAGED ON BOTH LOWER ENDS. REMOVED AND REPLACED FORMER.SDR 05272003Rib · crackedWHILE INVESTIGATING A SUSPECTED WATER LEAK IN THE BAGGAGE COMPARTMENT MAINTENANCE DISCOVERED AN APPROXIMATELY 2.5 CRACK IN THE RIGHT LOWER VERT STAB LEADING EDGE SKIN P/N 6231276 AT APPROXIMATELY WL 160. AFTER REMOVING SKIN FOR REPLACEMENT IT WAS DISCOVERED TSDR DHL2003604562Frame · crackedVERTICAL STAB L/E FORMER INNER SECTION CRACKED 0.500 AT STA ZFS 104.750 LT SIDE. STOP DRILLED CRACK AT ZFS 104.750 AND FABRICATED REINFORCEMENT IAW SRM 55-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA AND REINFORCEMENT IAW SRM 51-1-8B. INSTALLED REINFORCEMENT IASDR CA030617002Rib · cracked(CAN) DURING ROUTINE INSPECTION OF THE UPPER VERTICAL FIN ATTACHMENT FRAME, AME DISCOVERED RIB TO BE CRACKED. RIB REPLACED AS PER REPAIR MANUAL AND A/C RETURNED TO SERVICE.SDR 2003F00385Rib · crackedAT SCHEDULED ROUTINE INSPECTION, VERTICAL STABLIZER FORWARD TOP RIB HAS TWO CRACKS ON STRESS RELIEF HOLES. REPAIRED VERTICAL STABILIZER FORWARD TOP RIB BY INSTALLING TWO REPAIR DOUBLERS AT THE END OF CRACKS IAW BEECH 1900D STRUCTURAL REPAIR MANUAL 51-70-17, FSDR CA030505009Spar · cracked(CAN) DURING CHANGE OVER CRACKS WERE OBSERVED UNDER THE AFT ATTACHMENT POINT. NEW SPAR MANUFACTURED. NO PARTS AVAILABLE FROM MANUFACTURE. POOR PRODUCT SUPPORT.SDR AUS20030822Spar · corroded(AUS) VERTICAL STABILIZER REAR SPAR ANGLES PNO 101-640010-9 AND PN 10164001010 CONTAINED INTERGRANNULAR CORROSION. CORROSION ORIGINATED FROM RIVETS.SDR DL757030386Panel · puncturedVERTICAL STABILIZER LT LOWER FWD SKIN (FWD TORQUE BOX) WAS DAMAGED DUE TO GROUND DAMAGE. REPAIRED PER ERA 423002-14SDR DLM88030062Spar Cap · damagedDURING HMV-2, REPLACEMENT OF THE RT INNER & OUTER HINGE PLATES, TOOLING DAMAGE WAS INCURRED AT A SINGLE FASTENER LOCATION ON ANGLE PN 3912080504 AND REAR SPAR CAP PN 5911384506.THE HOLE WAS OVERSIZED AND BUSHED ON EACH PART.SDR CALA0200601Spar · crackedINSPECTION FOUND A 10 INCH CRACK IN VERTICAL STABILIZER L/H FRONT SPAR AT LOWER END AT CANTED BULKHEAD STA 1388. INSTALLED DOUBLERS IAW SRM 55-02, FIGURE 26.SDR BX42002F00000Spar · crackedFIN REINFORCEMENT ASSEMBLY (FORWARD SPAR) IS CRACKED AND BROKEN. JUST ABOVE WHERE THE LOWER RIBS ARE RIVETED TO THE REINFORCEMENT. THE REINFORCEMENT IS BROKEN THRU ITS WEB FROM RELIEF TO RELIEF, ONLY THE FLANGES ARE INTACT. THE LOWER FORWARD RIB IS CRACKED SDR 02FDEA00917Stringer · crackedNR 8R STRINGER CRACKED AT RIB IN VERTICAL STABILIZER TUNNEL.SDR DHL2002362516Angle · crackedVERTICAL STAB AT RIB 28, THE VERY TOP OF STAB, THE VERY AFT ANGLE IS CRACKED. REMOVED ANGLE, FABBED ANGLE AND INSTALLEDSDR GTIA021293Spar Cap · crackedFTW - VERTICAL STABILIZER FRONT SPAR CAP RIGHT SIDE CRACKED 2 PLACES STATION 1446 CANT. REMOVED DAMAGED AREA. FABRICATED 8 SPLICE ANGLE. FABRICATED 4 CAP REPAIR SEGMENT. FABRICATED 6 SPLICE. INSTALLED THE 4, 6, 8 AND 10 REPAIR PARTS AND SHIMS. (M)SDR 2002UALA01438Spar Cap · damagedVERTICAL STABILIZER FORWARD SPAR CAP DAMAGED AT APPROX FIN STA 108.00. MAJOR REPAIR ACCOMPLISHED. DAMAGED AREA REMOVED AND EXTRUSION REPAIR ACCOMPLISHED.SDR ABXA020193Rib · crackedVERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED RIGHT SIDE NR 3. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AND 51-30-5.SDR ABXA020192Rib · crackedVERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 1. REPAIRED AREA IAW ABX DC-9 SSRM K05159, SRM 51-30-2 AND 51-30-5.SDR ABXA020191Rib · crackedVERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 4. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AND 51-30-5.SDR ABXA020190Rib · crackedVERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 7. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AND 51-30-5.SDR ABXA020189Rib · crackedVERTICAL REMOVEABLE LEADING EDGE RIB WAS CRACKED, LEFT SIDE NR 12. REPAIRED AREA IAW DC-9 SSRM K05159, SRM 51-30-2 AND 51-30-5.SDR 02FDEA00414Spar · chafedVERT FIN MID SPAR IS CHAFED AT STA 228, LEFT HAND SIDE. REMOVED AND REPLACED VERT FIN PER EA 7-5510-64976.SDR 02FDEA00415Spar · chafedVERT FIN MID SPAR IS CHAFED AT STA 228 RIGHT HAND SIDE. REMOVED AND REPLACED VERT FIN MID SPAR PER EA 7-5510-64975.SDR SWIA200211017Frame · chafedBRACKET AND FRAME CHAFED WHERE RUDDER TRIM CABLES PASS FROM AFT RIGGING BAY INTO VERTICAL STAB. REPAIRED IAW GST-1980/02 AND SB 120-27-0082.SDR O9I2002F00002Rib · crackedDURING A ROUTINE PERIODIC INSPECTION A CRACK WAS FOUND IN VERTICAL STABILIZER BOTTOM RIB (PN 410008197) . THE CRACK RADIATED FROM THE SIDE FLANGE (LEFT) FORWARD RIVET AND EXTENDED TO THE EDGE OF THE RIB. THE TOTAL CRACK LENGTH IS .375 INCH. THE LOWER RIB OSDR AWXA200200371Rib · crackedGYR - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND ON THE VERTICAL STAB TOP LEADING EDGE SUPPORT WEB (RIB), L/H AND R/H SIDES AT FSS 417.169. MAINTENANCE REMOVED DAMAGED RIB, FABRICATED AND INSTALLED A NEW RIB IAW B757-200 SRM 51-40-01, PG. 1.SDR DHL2002807519Rib · crackedVERT STAB L/E - INNER RIB CRACKED .500 AT ZFS 108.000. STOP DRILLED CRACK IAW SRM 55-2-0 FIG 2. FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-0 FIG 2 & SRM 51-1-21 PG 1.SDR 2002807519Rib · crackedVERT STAB L/E INNER RIB CRACKED .500 AT ZFS 108.00. STOP DRILLED CRACK IN VERT STAB L/E INNER RIB AT STA ZFS 108.000 IAW SRM 55-2-0 FIG 2. FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-0 FIG 2 & 51-1-21 PG 1.SDR CA020322005Angle · cracked(CAN) DURING ROUTINE INSPECTION THE RT VERTICAL STABILIZER FORWARD SPAR ATTACH TO FUSELAGE BULKHEAD, FOUND THE RT DRAG ANGLE CRACKED.SDR TSAA0253060Spar · crackedFOUND CRACK IN THE VERTICAL STABILIZER IN SPAR WEB ON THE VERTICAL STABILIZER. TRIMMED OUT CRACK IAW FIGURE 2. FABRICATED A REPAIR DOUBLER AND A FILLER AS SHOWN IN FIGURE 2. INSTALLED REPAIR PARTS AND VERIFIED 8110-3 RECEIVED IAW ECO 3276. AIRCRAFT RETURNESDR TSAA0255063Spar · corrodedFOUND CORROSION ON LEFT REAR SPAR CHORD 6 INCHES UP FROM VERTICAL STABILIZER ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0255064Spar · corrodedFOUND CORROSION ON LEFT REAR SPAR CHORD 46 INCHES UP FROM VERTICAL STABILIZER FIN BETWEEN STATION 99.5 AND 108.7 ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)SDR 02FDEA00212Spar · wornVERT FIN MID SPAR AT FIN STA 230-231 WORN OUT OF LIMITS AT STR 7. REMOVED AND REPLACED MIDSPAR PER EA 7-5510-62791.SDR 02FDEA00213Spar · wornVERT FIN MID SPAR IS WORN OUT OF LIMITS AT STR 7. REMOVED AND REPLACED MID SPAR PER SRM 55-30-6 FIG 3.SDR 02FDEA00081Rib · crackedSTR 5 LT IN VERTICAL STAB CRACKED AT NR 2 RIB FIN STA 6.37. R&R VERT STAB.SDR 02FDEA00061Rib · crackedRIB CRACKED IN VERTICAL STABILIZER LT STR 9, FIN STA 110.4. R&R RIB.SDR 2002FA0000150Rib · crackedDURING ANNUAL INSPECTION THE VERTICAL STABILIZER LOWER FORWARD RIB WAS FOUND CRACKED AT THE 90 DEGREE BEND ADJACENT TO THE FORWARD SPAR. THIS AREA NEEDS CLOSE INSPECTION. 10X MAGNIFYING GLASS SHOULD HELP.SDR 01FDEA01072Stringer · chafedVERTICAL STAB NR 7 STR LT IS CHAFED 3 INCHES FRONT OF SLIDING SEAT TRACK. REPAIRED CHAFFED AREA OF VERTICAL FIN STR 7 MID SPAR STA 229 PER SRM 55-30-06 FIG 3 PER FEDEX EA NR 7-5530-54129.
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