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.

SDR UF6A990750Angle · crackedSBN - UPPER ATTACHMENT ANGLE ON THE VERTICAL STABILIZER AT THE LOWER RUDDER HINGE POINT IS CRACKED AT RIB 29.53. MAINTENANCE FABRICATED ANGLE PER SAMPLE AND INSTALLED. ALL WORK WAS DONE IAW BAE SRM 55-30-00, 51-30-01, AND 51-10-06. (M)Jul 20, 1999 · N859AW · Bag ATPSDR UF6A990731Shroud · crackedSBN - CRACK IN UPPER LEFT CORNER OF SHROUD AT LOWER HINGE POINT AT RIB STATION 29.53. MAINTENANCE REPLACED SHROUD IAW BAE ATP SRM 55-30-00 AND 51-10-03. TREATED AND PRIMED IAW BAE SRM 51-30-01. (M)Jul 14, 1999 · N859AW · Bag ATPSDR UF6A990730Angle · crackedSBN - LOWER ATTACHMENT ANGLE ON VERTICAL STAB AT RUDDER LOWER HINGE POINT CRACKED AT RIB STATION 29.53. MAINTENANCE REPLACED CHANNEL IAW BAE ATP SRM 55-30-00. TREATED AND PRIMED IAW BAE SRM 51-30-01. (M)Jul 14, 1999 · N859AW · Bag ATPSDR UF6A990729Channel · crackedSBN - CRACK ON LEFT SIDE CHANNEL OF BOTTOM RUDDER HINGE BOX, AROUND RIB STATION 29.53. MAINTENANCE REPLACED CHANNEL IAW BAE ATP SRM 55-30-00, 51-10-03. TREATED AND PRIMED IAW BAE SRM 51-10-06. (M)Jul 14, 1999 · N859AW · Bag ATPSDR UF6A990728Angle · crackedSBN - VERTICAL STAB LOWER ATTACHMENT ANGLE BETWEEN VERTICAL WEB AND HINGE BOX WEB IS CRACKED. MAINTENANCE REPAIRED CRACKED IAW BAE ATP SRM 55-30-00, 51-10-06 AND 51-30-01. (M)Jul 14, 1999 · N859AW · Bag ATPSDR UF6A990727Angle · crackedSBN - ANGLE CRACKED ON VERTICAL STAB AT RIB 47.78. MAINTENANCE REPAIRED CRACK IAW BAE ATP SRM 51-30-01 AND 51-10-06. (M)Jul 14, 1999 · N859AW · Bag ATPSDR C2XA99IA370Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE FORWARD LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-0110Jul 10, 1999 · N13936 · Emb EMB145SDR C2XA99IA369Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE FORWARD RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-011Jul 10, 1999 · N13936 · Emb EMB145SDR C2XA99IA351Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER FORWARD RIGHT DRAG ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURNJun 30, 1999 · N14939 · Emb EMB145SDR C2XA99IA350Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER FORWARD LEFT DRAG ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN Jun 30, 1999 · N14939 · Emb EMB145SDR DL72S991415Fitting · corrodedRHS BOLT HOLES FOR THE VERT FIN FITTING ATTACH TO TENSION TIE RIB WAS FOUND WITH CORROSION. REWORKED PER ERA 333260-14, REV B.Jun 23, 1999 · N536DA · Boeing 727232SDR 99ZZZX3487Bolt · damagedDURING ANNUAL INSPECTION, VERTICAL FIN WAS HAND FLEXED AT TOP. MOVEMENT WAS APPARANT. NOISE FROM LOWER ATTACHMENT WAS NOTED. REMOVED FOUR REAR SPAR ATTACHING BOLTS AN4-61 FOUND MARKING FROM MOVEMENT. REPLACED WITH NEW AN4-6A BOLTS AND HARDWARE. TORQUE TO Jun 10, 1999 · N94D · Piper PA32R301TSDR CA990614071Stabilizer · cracked(CAN) SEE SKETCHJun 4, 1999 · Wsk M18DROMADERSDR DL72S991233Skin · crackedSKIN CRACKED FS 1340 VENTRAL STAB SKIN IS CRACKED RT SIDE. FABRICATED DOUBLER PER M/M 55-30-0 FIG 801. PERFORMED DYE CHECK PER PS 900-6-3 NR 1. NO CRACKS FOUND PAST FASTENER HOLE. OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 PG 801.Jun 2, 1999 · N521DA · Boeing 727232SDR AT9900431Angle · crackedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND A CRACK ON THE RIGHT SIDE VERTICAL STABILIZER ANGLE ADJACENT TO THE ACME SCREW NUT MOUNT AT BS 1251. REMOVED OLD FITTING, FABRICATED REPAIR ANGLE, FORMED, DRILLED AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-6Jun 2, 1999 · N867AT · Doug DC932SDR UPS99229921Gusset · crackedINSPECTION TYPE: C & SI, VERT STAB MAIN BOX INTERIOR 9TH COMPARTMENT FROM TOP, RIB TO SKIN ATTACH GUSSET CRACKED AT S7 RT. GUSSET REPLACED IAW SRM 51-20-1 FIG 7.May 26, 1999 · N927UP · Boeing 72731CSDR C2XA99IA292Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC553May 23, 1999 · N14933 · Emb EMB145SDR C2XA99IA291Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC553May 23, 1999 · N14933 · Emb EMB145SDR 99FDEA00200Support · crackedANGLE RIB SUPPORT CRACKED IN VERTICAL STAB LT CORNER. INSTALLED DOUBLER PER SRM 51-40-3 AND 53-10-9 PG 11. FABRICATED, DRILLED, PRIMED AND SEALED ACCESS HOLE DOUBLER PER SRM 51-40-2. OPS CHECK PERF ON CARD 70C027-00.May 19, 1999 · N149FE · Boeing 72722SDR 99FDEA00190Support · crackedNR 924 - ANGLE RIB SUPPORT CRACKED IN VERTICAL STAB LEFT CORNER. INSTALLED DOUBLER PER SRM 51-40-3 AND 53-10-9 PG 11. FABRICATED, PRIMED AND SEALED ACCESS HOLE DOUBLER PER SRM 51-40-2, OPS CK PER ON CARD 70C027-00.May 19, 1999 · N149FE · Boeing 72722SDR UF6A990549Angle · crackedSBN - LEFT SIDE OF VERTICAL STABILIZER HAS A CRACK LOCATED ON THE TOP FAIRING ANGLE. MAINTENANCE FABRICATED ANGLE TO NEST IN THE END OF THE FAIRING. ANGLE WAS MADE 2024-T3, .071 INCH THICK. ALL WORK WAS PERFORMED IAW ENGINEERING ORDER NR 99-091. (M)May 15, 1999 · N857AW · Bag ATPSDR DL72S991022Stringer · crackedVERT STAB S7 WAS FOUND CRACKED AT STA 157.2 DURING INSPECTIONS PER SI 4-59253-12AD. REPAIRED PER ERA 333133-14AD.May 10, 1999 · N8873Z · Boeing 727225SDR CALA9900507Stringer · crackedVERTICAL STABILIZER INNER COMPARTMENT NR 8 RIB RT STRINGER NR 8 CRACKED AT ATTACH BOLT (2). STOP DRILLED CRACK, FABRICATED ANGLE AND FILLER REPAIR, TREATED AND PRIMED REPAIR PARTS, INSTALLED PER SRM 55-30-4, 55-30-9 AND 51-30-2.May 10, 1999 · N79749 · Boeing 727224SDR CALA9900505Shield Plate · crackedVERTICAL STABILIZER INNER COMPARTMENT SHIELD PLATE AT I/B 1 AND LEFT HAND STRINGER NR 7 AREA HAS A SMALL CRACK (.25). REMOVED FASTENERS, FABRICATED ANGLE PER SRM 55-30-6. TREATED, PRIMED AND INSTALLED DOUBLER PER SRM 51-10-2 AND 55-30-6 PG 2A.May 10, 1999 · N79749 · Boeing 727224SDR TWAA9907103Angle · crackedDURING CHECK-C MAINT, FOUND LOWER RT VERTICAL STABILIZER MOUNT ANGLE CRACKED 2 PLACES AFT END BELOW RUDDER. ACCOMP NDT HFEC FOR CRACK CONTAINMENT AFTER SECTION CUT OUT. TRIMMED OUT CRACK PER SRM 53-05.May 8, 1999 · N960TW · Doug DC982SDR DL72S991123Stringer · crackedFOUND DURING MV2 CORROSION VISIT NRC 210, STR 9 CRACKED AT FIN STA 157.2 INSIDE VERT STAB CRAWLWAY (3RD STR FROM BOTTOM, 3RD BAY UP FROM DOOR). REPAIRED PER M/M 55-30-0 FIG 803.May 7, 1999 · N534DA · Boeing 727232SDR CALA9900465Angle · crackedHOU - RIGHT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-30-2. (M)Apr 30, 1999 · N35836 · Doug DC982SDR CALA9900464Angle · crackedHOU - LEFT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. (M)Apr 30, 1999 · N35836 · Doug DC982SDR UPS99829541Web · corrodedINSPECTION TYPE:C2 VERT STAB BASE, FS 1781 THROUGH 1818, RT WEB BETWEEN THE CENTER AND REAR SPARS HAS HEAVY EXFOLIATION CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 51-1-9A. CPCPApr 23, 1999 · N880UP · Doug DC873FSDR RAAA99B2042Web · corrodedDURING SCHEDULED C-CHECK, FOUND VERTICAL STABILIZER CLOSURE WEB CORRODED INSIDE LOWER END AT ATTACH ANGLE INSIDE AND AFT NR 2 PYLON ACCESS PANEL AND AT LOWER END FASTENERS ABOVE NR 2 ENGINE MOUNT. REPAIRED IAW RAA ECO 99-4 REFERENCE DWG 65-22913 65-17551 M5Apr 21, 1999 · N832RV · Boeing 72722CSDR AU990446Bracket · corroded(AUS) LOWER RUDDER ATTACHMENT BRACKET CRACKED IN HORIZONTAL PLANE.Apr 20, 1999 · Cessna 210JSDR UPS99229366Angle · crackedINSPECTION TYPE:SI, VERTICAL FIN STA 180.6, STR 7, ANGLE IS CRACKED AT FASTENER HOLE. REMOVED FASTENERS COMMON TO REPAIR, FABRICATED REPAIR PARTS, ALODINED AND PRIMED PARTS. INSTALLED REPAIR PARTS IAW SRM 55-30-02, 55-30-05.Apr 13, 1999 · N937UP · Boeing 72725CSDR DL72S990821Stringer · crackedVERTICAL STAB S7 WAS FOUND CRACKED AT STA 157.2 DURING INSP PER SI 4-59253-12AD. REPAIRED PER ERA 333025-14A.DApr 13, 1999 · N8875Z · Boeing 727225SDR LR7A99135Web · crackedDURING C CHECK/BRIDGING INSPECTION PER HST5505, FOUND FS 1095 VERTICAL STAB WEB CRACKED AT VSS 9 TO 12. REPAIRED IAW DWG R99-0002-8 AND MPP L100-404-99-061. NR 545.Apr 11, 1999 · N404LC · Lkheed 382GSDR C2XA99IA221Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE TO BE CRCKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF THE DRAG IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01101, AND THE AIRApr 11, 1999 · N12934 · Emb EMB145SDR C2XA99IA220Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01101, ANDApr 11, 1999 · N12934 · Emb EMB145SDR CALA9900359Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN LT AND RT DRAG ANGLES BELOW NR 2 ENGINE AT THIRD BANJO FITTING. THE CRACKS WERE STOP DRILLED AND REPAIR ANGLES WERE INSTALLED IAW SRM 55-20-00, FIGURE 3.Apr 6, 1999 · N14063 · Doug DC1030SDR TWAA9906310Angle · crackedDURING CHECK-C MAINT, FOUND A .1875 IN CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE AT STA 1421. REMOVED AND REPLACED ATTACH ANGLE PER SERVICE BULLETIN 53-223 PER MD9-AD-13.Apr 5, 1999 · N953U · Doug DC982SDR TWAA9905402Angle · crackedDURING CHECK-C MAINT, FOUND .1875 INCH CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE AT STA 1421. REMOVED AND REPLACED ATTACH ANGLE PER SB 53-223 AND PER MD9-AD-13.Apr 5, 1999 · N953U · Doug DC982SDR TWAA9905101Angle · crackedDURING CHECK-C MAINT, FOUND .1875 INCH CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE, STA 1421. REMOVED AND REPLACED ATTACH ANGLE PER SERVICE BULLETIN 53-223, AND PER MD9-AD-13.Apr 5, 1999 · N953U · Doug DC982SDR TWAA9906309Angle · crackedDURING CHECK-C MAINT, FOUND .1875 IN CRACK AT THE LT DORSAL FIN ATTACH ANGLE AT STA 1421. INSTALLED NEW ATTACH ANGLE PER SERVICE BULLETIN 53-223 AND SR09530162.Apr 4, 1999 · N953U · Doug DC982SDR TWAA9905403Angle · crackedDURING CHECK-C MAINT, FOUND .1875 INCH CRACK AT THE LT DORSAL FIN ATTACH ANGLE STA 1421. INSTALLED NEW ATTACH ANGLE PER SB 53-223 AND SRO9530162.Apr 4, 1999 · N953U · Doug DC982SDR TWAA9904903Angle · crackedDURING CHECK-C MAINT CHECK, FOUND .75 INCH CRACK AT THE LT DORSAL FIN ATTACH ANGLE AT STA 1421. INSTALLED NEW ATTACH ANGLE PER SVC BULLETIN 53-2234, SB 09530162.Apr 4, 1999 · N953U · Doug DC982SDR TWAA9906307Angle · crackedDURING CHECK-C MAINT, FOUND INSIDE ANGLE AT STA 1421 WAS CRACKED ON RT SIDE. INSTALLED NEW ANGLE AT STA 1421, PER SRM 51-10-4 AND 51-30-2.Apr 2, 1999 · N953U · Doug DC982SDR C2XA99IA207Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL FIN TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRApr 1, 1999 · N13935 · Emb EMB145SDR C2XA99IA206Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL FIN TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THApr 1, 1999 · N13935 · Emb EMB145SDR QXEA9900557Shroud · dentedYXX - VERTICAL STABILIZER RIGHT-HAND TRAILING EDGE SHROUD BETWEEN RIB 8 AND RIB 9 DENTED. REPAIRED IAW DASH 8 RD 8-555-718.Mar 30, 1999 · N816PH · Dhav DHC8102SDR DHL9970168DFitting · corrodedAT D-CHECK, VERTICAL FIN RT HORIZ STAB STAINLESS RUB BLOCK STRIP OVER VERTICAL FIN BULGED. REMOVED AND REPLACED VERTICAL FITTING PER SRM 55-30-2.Mar 26, 1999 · N701DH · Boeing 72730CSDR DHL9970161DFitting · corrodedAT D-CHECK, VERTICAL FIN LT HORIZONTAL STAB STAINLESS RUB BLOCK STRIP ON VERT FIN BULGED. REMOVED VERTICAL FITTING AND FOUND CORRODED. REPLACED FITTING SUPORT PER SRM 55-30-2.Mar 26, 1999 · N701DH · Boeing 72730CSDR C2XA99IA199Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTENENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFMar 21, 1999 · N15932 · Emb EMB145
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