JASC 5530
Service difficulty reports · 2,534
Reports filed under 5530 · Vertical Stabilizer, 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 = '5530' 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 = '5530' 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 USAA2009022090391Bearing · excess playSAL - C8 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE ARM BEARING NR 1 VERTICAL STABILIZER. REPLACED ATTACH FITTING HINGE ARM BEARING NR 1 OF VERTICAL STABILIZER IAW A320 AMM 55-36-41.SDR 2009FA0000085Hinge · corrodedDURING THE REMOVAL OF THE RUDDER, LWR STABILIZER HINGE ASSY WAS FOUND WITH HEAVY CORROSION. THIS CORROSION WAS NOT VISIBLE WITHOUT REMOVING THE RUDDER. (K)SDR FDEA200901190233Fitting · damagedEXISTING FASTENER HOLE REPAIR AT VERTICAL STABILIZER AT RIGHT AND LEFT NR 4 BANJO FITTING AND PYLON CARRY THRU CAP. EXISTING FASTENER HOLE REPAIR AT VERTICAL STABILIZER AT RIGHT AND LEFT NR 4 BANJO FITTING AND PYLON CARRY THRU CAP EVALUATED AND FOUND PREVIOUSSDR LR7A2009020200004Bracket · crackedDURING SCHEDULED C-9 CHECK PER JOB CARD HST2708, FOUND RUDDER LOWER AND CENTER AUX BEAMS CRACKED AT FS 1157, VSS0-15, BL0 AND FS 1175.5, VSS0-73, BL0. REPAIRED CENTER BEAM IAW SMP583 FIG 51-140-19 REF FIG 55-50-02 ITEM 11. FABRICATED AND INSTALLED LWR BEAM ISDR AALA200910630Lug · corrodedTAIL, NUMBER 8 VERTICAL STABILIZER PIVOT LUG HAS CORROSION. INSTALLED A SERVICABLE NUMBER 8 LUG.SDR USAA2008123092351Hinge Fitting · wornSAL - MAJOR REPAIR - C7 CHECK - NR 6141112, NR 5 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2985 / RIB7 HAS EXCESSIVE PLAY. REPLACED NR 5 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2985 / RIB7 IAW A319 AMM 55-36-41.SDR USAA2008123092350Hinge Fitting · wornSAL - MAJOR REPAIR - C7 CHECK - NR 6141111, NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2632 / RIB6 HAS EXCESSIVE PLAY. REPLACED NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2632 / RIB6 I/A/W A319 AMM 55-36-41.SDR CA081210012Bracket · cracked(CAN) FOUND CRACK IN BRACKET LOCATED ON THE FORWARD SIDE OF THE VERTICAL STAB ATTACH FITTING AT FS 521.75. THREE CRACKS EXTEND FROM THE RIGHT OUTBOARD ATTACHMENT BOLT HOLE. THE ATTACHING BOLTS RUNS HORIZONTALLY FWD AND AFT THROUGH THE RUDDER STOP BRACKET, VSDR A6WA200840626Visor · crackedVERTICAL STAB. LT UPPER VISOR CRACKED AND BENT. CRACK .250 LONG. VERTICAL STAB LT UPPER VISOR REPLACED IAW CRJ 200SDR DL757081534Structure · damagedDURING AGING AIRCRAFT INSPECTION, FOUR AREAS OF TOOLING DAMAGE WERE FOUND ON THE VERTICAL STABILIZER CHORD. BOEING WAS CONTACTED FOR APPROVAL TO LEAVE THE BLENDED MARKS AS IS. THE REPAIR IS DOCUMENTED IN ER/A 471254-14.SDR ASOA200801331Drag Angle · crackedLEFT SIDE VERTICAL STABILIZER HAS A CRACK IN THE FORWARD DRAG ANGLE AS MARKED. PERFORMED EDDY CURRENT INSPECTION ON DRAG ANGLE. END OF CRACK MARKED. CUT AWAY DAMAGE PER REO 670-55-31-018. PERFORMED ET INSPECTION OF CUT LINE. NO DEFECTS NOTED. REPAIRED PESDR ASOA200801330Drag Angle · crackedRIGHT SIDE VERTICAL STABILIZER HAS A CRACK IN THE FORWARD DRAG ANGLE AS MARKED. REMOVED EXISTING FASTENERS FROM REPAIR AREA AND CUT AWAY DAMAGE. PERFORMED ET INSPECTION. NO DEFECTS NOTED. FABRICATED FILLERS IAW REO 670-55-31-018. FINAL TRIMMED DOUBLER,SDR GLB2008F00027Stabilizer · damagedMAJOR REPAIR ACFT N122UX WHILE TAXIING THE ACFT TO THE GATE THE PILOTS STRUCK A JETWAY WITH THE TAIL OF THE ACFT DAMAGING THE VERTICAL AND HORIZONTAL STABILIZERS. THE VERTICAL STABILIZER WAS DAMAGED AND TWISTED TO THE LT FROM VERTICAL STABILIZER POSITION CSS SDR ASA2008F00007Drag Angle · crackedCRACKED DRAG ANGLE RT LOWER VERT STAB (MARKED). PERFORMED EDDY CURRENT INSPECTION OF RT V/ STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE IS VERIFIED CRACKED AND END OF CRACK IS MARKED 9/4/08 VTJ7010159. GUT AWAY DAMAGED AREA OF RT DRAG ANSDR ASA2008F00006Drag Angle · crackedCRACKED DRAG ANGLE LEFT LOWER VERT STAB (MARKED). PERFORMED EDDY CURRENT INSPECTION OF LEFT V/STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE IS VERIFIED CRACKED AND END OF CRACK IS MARKED. PERFORMED CUTOUT OF DAMAGED AREA LOCATED OF LT LSDR C2XA08TY090Bearing · corrodedA/C WAS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE LT SPHERICAL BEARING. MX REMOVED THE CORROSION REMOVED SPHERICAL HOUSING AND REAM TO THE 1ST OVERSIZE TO INSTALL A NEW BUSHION. REPLACED THE BEARING. INSTALL THE SPHERICAL BEARING AND PERFORMED ALL CSDR UPS08553061Support · chafedINSPECTION TYPE-C2, VERTICAL STAB LWR LEADING EDGE FAIRING SUPPORT RIB IS CHAFED, BS 1681. REMOVED & REPLACED RIB.SDR 2008FA0000515Inlet · crackedDURING SCHEDULED INSP, FOUND VERTICAL STABILIZER L/E AT HEAT EXCHANGER INLET IS CRACKED APPROX 6.5 INCHES LONG ON LT SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 55-05 FIG 3. (K)SDR 08FDEA02996Support Angle · crackedVERTICAL STABILIZER RIGHT TRAILING EDGE SUPPORT IS CRACKED BELOW THE NR 2 RUDDER HINGE FITTING. REMOVED DAMAGE IAW SRM 51-70-10, REPAIR I. FABRICATED A REPAIR ANGLE AND FILLER IAW SRM 51-70-10, REPAIR I. ALODINED AREA AND REPAIR PARTS IAW SRM 51-21-10. PRISDR 08FDEA02997Support Angle · crackedVERTICAL STABILIZER RIGHT TRAILING EDGE SUPPORT IS CRACKED BELOW THE NR 2 RUDDER HINGE FITTING. REMOVED DAMAGE IAW SRM 51-70-10, REPAIR I. FABRICATED A REPAIR ANGLE AND FILLER IAW SRM 51-70-10, REPAIR I. ALODINED AREA AND REPAIR PARTS IAW SRM 51-21-10. PRISDR TRAX200800886Drag Angle · crackedRIGHT SIDE VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. REFER TO STEPS 2-9 ON M-234 FORM ATTACHED FOR WORK ACCOMPLISHED DK 7022603. REMOVED RT VERTICAL DRAG ANGLE PAINT IAW CRJ 700 SRM 51-26-00. (S)SDR TRAX200800885Drag Angle · crackedSUSPECT CRACK ON LT SIDE VERTICAL STAB TO FUSELAGE DRAG ANGLE. (B) REFER TO STEPS 3-9 ON M-234 FOR WORK ACCOMPLISHED DK 7022603. REFER TO STEP NUMBER THREE ON M-234 FOR WORK ACCOMPLISHED FOR THIS STEP.SDR 08FDEA02479Skin · delaminatedTAIL CONE: VERTICAL STAB PNL 9703 HAS NUMEROUS PUNCTURES AND DELAM. REPAIRED PANEL NR 9703. REF SRM 51-40-9 PAR 3, 4 PAGES 2A-6. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR TRAX200800722Drag Angle · crackedLT DRAG ANGLE APPEARS CRACKED PERFORMED ET INSPECTION OF SUSPECT CRACK IAW NDTM 51-20-006. FOUND ANGLE TO BE CRACKED. MARKED END OF CRACK. (B)SDR TRAX200800721Drag Angle · crackedRT DRAG ANGLE (EMPENAGE-VERTICAL) APPEARS CRACKED. PERFORMED ET INSPECTION OF SUSPECT CRACK IAW NDTM 51-20-006. FOUND ANGLE TO BE CRACKED. MARKED END OF CRACK. (B)SDR TRAX200800616Drag Angle · crackedVERTICAL STAB LOWER LT DRAG ANGLE IS CRACKED CUT AWAY DAMAGE FROM VERTICAL STAB LOWER LT DRAG ANGLE IAW REO 670-53-31-018. INSTALLED DOBLER AND FILLER, FILLET SEAL REPAIR PARTS AND FINAL PAINT AND LT DRAG ANGLE. ALL WORK DONE IAW REO 670-53-31-018. (B)SDR TRAX200800617Drag Angle · crackedVERTICAL STAB LOWER RT DRAG ANGLE IS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF RIGHT V/STAB TO FUSELAGE DRAG ANGLE TO LOCATE END OF CRACK IAW NDTM 51-20-006 END OF CRACK IS MARKED. CUT AWAY DAMAGE FROM VERTICAL STAB LOWER RT DRAG ANGLE IAW REO 670-55-31-SDR 2008UALA01852Structure · wornCROWN AREA DORSAL FIN LANDING AT BS 867-883 WORN AT RBL 1-4. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED EXTERNAL DOUBLER AND STRAPS. REPAIR CONSISTED OF 0.050 INCH DOUBLER FROM BS 857 TO BS 907 FROM STRINGER S-2L TO S-2R. INSTALLED WEAR STRIPS ON SDR USAA920080711Hinge Fitting · wornSAL - MAJOR REPAIR - C6 CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 5, VERTICAL STABILIZER STATION 2985/RIB 7. REPLACED RUDDER HINGE FITTING NR 5, VERTICAL STABILIZER STATION 2985/RIB 7 IAW A320 AMM 55-36-41.SDR USAA920080709Hinge Fitting · wornSAL - MAJOR REPAIR - C6 CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 3, VERTICAL STABILIZER STATION 2279/RIB 5. REPLACED RUDDER HINGE FITTING NR 3, VERTICAL STABILIZER STATION 2279/RIB 5 IAW A320 AM 55-36-41.SDR USAA920080708Hinge Fitting · wornSAL - MAJOR REPAIR - C6 CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 4, VERTICAL STABILIZER STATION 2632/RIB 6. REPLACED RUDDER HINGE FITTING NR 4, VERTICAL STABILIZER STATION 2632/RIB 6 IAW A320 AMM 55-36-41.SDR 08FDEA00779Tip Cap · crackedVERTICAL STABILIZER TIP IS CRACKED AND DELAMINATED AT THE FWD HOIST POINT HOLE. REPAIRED VERTICAL STAB TIP ERROSION DAMAGE BY REMOVING DAMAGE SKIN PLYS, APPLING A WET LAYUP FIBERGLASS REPAIR AND REFINISHING IAW SRM 55-34-11.SDR HALA0800346Scoop · corrodedLEVEL 2 CORROSION VERTICAL STAB RAM AIR INLET SCOOP 2 REPAIR DOUBLERS LEFT AND RIGHT SIDE. REPAIR IN WORK.SDR HALA0800349Structure · corrodedLEVEL 1 CORROSION ON VERTICAL STAB FWD LOWER L/E NUT PLATES (9EA). REPAIR IN WORK.SDR DLM90080238Lug · corrodedRT O/B VERT STAB LUG CORRODED. RT O/B VERT STAB LUG REPAIRED, IAW DAL ER/A 466168-14 DATE 02/15/08 REV A.SDR DLM90080237Lug · corrodedRT INBOARD VERTICAL STAB LUG CORRODED. REPAIRED RT INBOARD VERTICAL STAB LUG, IAW DAL ER/A 466168-14 DATED 02/15/08 REV A.SDR DLM90080199Lug · corrodedLT O/B VERTICAL STABILIZER LUG CORRODED. REPAIRED LEFT OUTBOARD VERTICAL LUG (STAB), IAW MD90 SRM 55-30-05.SDR DLM90080198Lug · corrodedLT INBOARD VERTICAL STABILIZER LUG CORRODED. REPAIRED LT INBOARD VERTICAL STAB LUG, IAW MD90 SRM 55-30-05.SDR DLM90080056Bushing · corrodedVERTICAL STABILIZER RT I/B HORIZONTAL STABILIZER MOUNT LVG/BUSHING CORRODED/PITTED. REPAIRED HORIZONTAL STABILIZER MOUNT LUG IAW MD90 SRM 55-30-05 VOL.I.SDR SWAA076382Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER AFT INBOARD FAIL SAFE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.SDR SWAA076381Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND LT VERTICAL STABILIZER AFT INBOARD FAIL SAFE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.SDR TRAX200701926Angle · crackedLT VERTICAL STAB TO FUSELAGE ANGLE T/E CRACKED. NEEDS PAINT REMOVED FOR FURTHER EVALUATION.SDR TRAX200701656Drag Angle · crackedVERTICAL STAB-TO-FUSELAGE LT DRAG ANGLE CRACKED AT AFT END.SDR USAA920070977Hinge Fitting · wornSAL - MAJOR REPAIR - C-07 CHECK - RUDDER HINGE NR 4 FITTING WORN, VERTICAL STABILIZER STATION 2632 / RIB 6. REPLACED RUDDER HINGE NR 4 FITTING VERTICAL STABILIZER STATION 2632 / RIB 6 IAW A320 AMM 27-21-00 AND 55-36-41.SDR USAA920070976Hinge Fitting · wornSAL - MAJOR REPAIR - C-07 CHECK - RUDDER HINGE NR 3 FITTING WORN, VERTICAL STABILIZER STATION 2279 / RIB 5. REPLACED RUDDER HINGE NR 3 FITTING VERTICAL STABILIZER STATION 2279 / RIB 5 IAW A320 AMM 27-21-00 AND 55-36-41.SDR USAA920070975Hinge Fitting · wornSAL - MAJOR REPAIR - C-07 CHECK - RUDDER HINGE NR 1 FITTING WORN, VERTICAL STABILIZER STATION 780 / RIB 2. REPLACED RUDDER HINGE NR 1 FITTING VERTICAL STABILIZER STATION 780 / RIB 2 IAW A320 AMM 27-21-00 AND 55-36-41.SDR 2007UALA04117Hinge Fitting · damagedFOUND LIGHTNING STRIKE DAMAGE IS AT VERTICAL STAB REAR SPAR UPPER RUDDER HINGE FITTING AT RUB STA 522. REMOVED AND REPLACED HINGE FITTING. A/C OK FOR SERVICESDR 2007FA0000875Bolt · looseLOSE VERTICAL ATTACH BOLTS ON AFT BULKHEAD.SDR DLM90071421Angle · crackedVERTICAL STABILIZER ANGLE IS CRACKED ON RT SIDE BELOW INLET SCOOP. REMOVE AND REPLACE ANGLE IAW MD-90 SRM 51-30-05 ON N/R 3000-0048 AT HMV-2 IN OKC.SDR 07FDEA03329Structure · corrodedUPPER HOIST POINT OF DORSAL FIN IS DAMAGED BY EROSION. SURFACE REPAIRED AS PER GUIDELINES OF SRM 51-77-11 PARA 3 A., USING PASTE ADHESIVE AS PER SRM 51-77-10 PARA 5 B (1) IAW. EA 6-5318-92211 AND RAS/DAHAM/4020086/2005 ISS A.
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