JASC 5531

Service difficulty reports · 1,234

Reports filed under 5531 · Vertical Stabilizer, Spar/Rib, newest first.

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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"

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SDR HALA9787Rib · crackedVERT STAB L/E INTERNAL NR 9 RIB CRACKED AT BOTTOM CORNER LEFT SIDE. STOP DRILLED CRACK, FABRICATED, TREATED, AND INSTALLED DOUBLER PER SRM 51-10-3, 55-02 FIG 19, 51-30-2. (M)Feb 25, 1997 · N709HA · Doug DC951SDR HALA9786Rib · crackedVERT STABILIZER L/E INTERNAL NR 11 RIB CRACKED AT BOTTOM CORNER LEFT SIDE. STOP DRILLED CRACK, FABRICATED, TREATED AND INSTALLED DOUBLER PER SRM 51-10-3, 55-02 FIG 19, 51-30-2. (M)Feb 25, 1997 · N709HA · Doug DC951SDR HALA97117Rib · crackedVERTICAL STABILIZER L/E INTERNAL NR 10 RIB CRACKED AT BOTTOM FASTENER LEFT SIDE. STOP DRILLED CRACK, FABRICATED, TREATED, AND INSTALLED DOUBLER PER SRM 51-10-3, 55-02, FIG 19, 51-30-2. (M)Feb 25, 1997 · N709HA · Doug DC951SDR CALA9700225Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN TOP RIB AND A .25 INCH CRACK IN 7TH RIB FROM BOTTOM OF VERTICAL STABILIZER LEADING EDGE. BOTH CRACKS WERE STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 55-01, FIGURE 2.Feb 11, 1997 · N12532 · Doug DC932SDR ABXA9700594Rib · crackedDURING C-INSPECTION, FOUND VERTICAL STAB LEADING EDGE 4TH RIB CRACKED RIGHT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.Feb 5, 1997 · N949AX · Doug DC931SDR ABXA9700593Rib · crackedDURING C-INSPECTION, FOUND VERTICAL STAB LEADING EDGE LOWER SECTION 5 RIB CRACKED, LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.Feb 5, 1997 · N949AX · Doug DC931SDR ABXA9700592Rib · crackedDURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 3 RIB CRACKED LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.Jan 31, 1997 · N949AX · Doug DC931SDR ABXA9700591Rib · crackedDURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 7 RIB CRACKED LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.Jan 31, 1997 · N949AX · Doug DC931SDR ABXA9700590Rib · crackedDURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 8 CANTED RIB CRACKED LT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.Jan 31, 1997 · N949AX · Doug DC931SDR 97ZZZM259Spar · crackedDURING B-1/B-2 INSPECTION, THE VERTICAL STABILIZER RT FRONT SPAR RAIL AT WL 151 WAS FOUND TO BE CRACKED. REPLACED RAIL WITH NEW UNIT. AIRCRAFT WILL BE RETURNED TO SERICE AT END OF INSPECTION.Jan 31, 1997 · N8042W · Cvac 440SDR UPS97222086Spar Chord · corrodedINSPECTION C-CHECK, RT VERTICAL FIN SPAR CHORD IS CORRODED BEYOND LIMITS AT FIN STA 22.5. CUT OUT DAMAGE ON CHORD AND REPAIRED IAW BOEING DWG 65-68408 AND SRM 51-30-2.Jan 6, 1997 · N954UP · Boeing 727185CSDR UPS97222081Spar · corrodedINSPECTION TYPE: C. LT VERTICAL FIN SPAR CHORD IS CORRODED BEYOND LIMITS FIN. STA. 22.5. CUT OUT DAMAGE AND REPAIRED IAW BOEING DWG. 65-68408 AND SRM 51-30-2.Jan 6, 1997 · N954UP · Boeing 727185CSDR UPS97221983Interspar Skin · corrodedINSPECTION TYPE: C B.S. 1342 LT INTERSPAR SKIN IS CORRODED BEYOND LIMITS AT TERMINAL FITTING. CUTOUT DAMAGE, FABRICATED REPAIR PART AND INSTALLED PER DHC SK 954-578 REF. ENGINEERING FILE NR 727-55-0340.Jan 6, 1997 · N954UP · Boeing 727185CSDR AU970933Spar · cracked(AUS) FIN REAR SPAR CRACKED ALLOWING TOP AND MIDDLE RUDDER ATTACHMENT BRACKETS TO SEPARATEJan 1, 1997 · Piper PA36375SDR GTIA9700087Rib · crackedMHV - VERTICAL STABILIZER LE PANEL RT SIDE HAS 5 RIBS CRACKED THROUGH FASTENER HOLES AT EDGE OF PANEL. LEFT SIDE HAS 3 RIBS CRACKED THROUGH FASTENER HOLES AT EDGE OF PANEL. FABRICATED AND INSTALLED PARTS IAW 55-02 FIG 14, 51-10-3, 51-20-0, 51-30-0. ALL CRADec 20, 1996 · N928ML · Doug DC931SDR 97ZZZX710Rib · corrodedFOUND HEAVY TO SEVERE CORROSION, POPPED RIVETS, THROUGHOUT THE VERT FIN. CESSNA DID NOT PRIME ANY INTERNAL PARTS DURING MANUFACTURE RESULTING IN AN UNSAFE CONDITION. REPLACED PART, CLEANED, TREATED, AND PRIMED WITH EPOXY PRIMER. RECOMMEND CESSNA DO LIKEWISEDec 18, 1996 · N64688 · Cessna 172PSDR 9626369981Rib · crackedDURING PERIODIC CHECK, FOUND MULTIPLE VERTICAL STABILIZER RIBS CRACKED AT AFT ATTACH POINTS. REPAIRED PER EA 99-111928.Dec 11, 1996 · N994Z · Doug DC931SDR ABXA9700160Screw · rustedWHILE COMPLYING WITH A C INSPECTION, FOUND THE VERTICAL STABILIZER CENTER ATTACH FITTINGS HAVE HEAVY RUST ON EIGHT EACH FASTENERS, AT FUSELAGE FRAME AT STATION 1104. REPLACED RUSTED FASTENERS IAW DC-9 SRM CHAPTER 51-30-1.Dec 5, 1996 · N935AX · Doug DC933FSDR CKSA96287Spar · corrodedDURING C-4 CHECK INSPECTION, FOUND LEFT VERTICAL STABILIZER REAR SPAR CORRODED AT STA ZR180. REPAIRED IAW SKETCH AIA/E/2386 TREATED AND PRIMED IAW DC-8 SRM 51-1-8. REPAIR ACCOMPLISHED IAW EA 96-326 AND AIA 8110-3 DATED 11-15-96. CORROSION CARD NR 6000-0551,Nov 24, 1996 · N811CK · Doug DC863FSDR CKSA96229Spar · corrodedDURING C-4 CHECK INSPECTION, FOUND LEFT VERTICAL STAB REAR SPAR CORRODED AT STA ZR132. REPAIRED IAW AIA/E/2386 SKETCH NR C-4 CHECK WORK CARD NR 3014. NON-ROUTINE TASK CARD NR 87304.Nov 24, 1996 · N811CK · Doug DC863FSDR DL72P962564Rib · crackedVERTICAL RIB INSIDE PLATE 9504 CRACKED LEFT AND RIGHT SIDE JUST ABOVE S-DUCT. REPAIRED PER SRM 53-10-4.Nov 6, 1996 · N8890Z · Boeing 727225SDR ABXA9700711Spar Cap · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE VERTICAL STABILIZER REAR SPAR CAPS CORRODED AT STATIONS ZRS 4, 8 AND 10. REPAIRED VERTICAL STAB REAR SPAR CAPS IAW ABX REA D957-16873-MR.Oct 22, 1996 · N964AX · Doug DC941SDR 96ZZZM1532Rib · crackedMCI - DURING OP-16, FOUND LOWER LEADING EDGE PANEL VERTICAL STABILIZER LOWER ENDS OF RIBS CRACKED, LEFT AND RIGHT SIDE. REPAIRED PER SRM 55-30-102, FIGURE 201.Oct 14, 1996 · N959U · Doug DC982SDR ZIAA96070Spar · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. VERT STAB AFT SPAR ZR 218-281. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (C)Oct 13, 1996 · N799AL · Doug DC862SDR MWEA96585Rib · crackedDURING D-CHECK, FOUND VERTICAL STAB LEADING EDGE STA ZV147 UPPER RIB CRACKED AT AFT END. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 55-01 FIG 2, SHEET 3.Oct 11, 1996 · N80ME · Doug DC914SDR MWEA96539Rib · crackedDURING D-CK, FOUND VERTICAL STABILIZER LEADING EDGE UPPER RIB CRACKED NEAR MOUNTING FLANGE AND RIB CRACKED AT LT SIDE OF VOR ANTENNA BOX. INSTALLED ANGLE REPAIR IAW SRM 55-02, FIG 19.Oct 11, 1996 · N80ME · Doug DC914SDR ABXA9700641Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, UPPER RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 3, 1996 · N942AX · Doug DC931SDR ABXA9700640Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, CANTED RIB RIGHT SIDE. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 3, 1996 · N942AX · Doug DC931SDR ABXA9700639Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, LOWER RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 3, 1996 · N942AX · Doug DC931SDR ABXA9700638Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, SECOND FROM BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 3, 1996 · N942AX · Doug DC931SDR ABXA9700637Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, FOURTH FROM BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 3, 1996 · N942AX · Doug DC931SDR ABXA9700636Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, FIFTH FROM BOTTOM RIGHT. \N\N\N\N\N REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 3, 1996 · N942AX · Doug DC931SDR ABXA9700635Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, LOWER LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 3, 1996 · N942AX · Doug DC931SDR ABXA9700634Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, SECOND FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 3, 1996 · N942AX · Doug DC931SDR ABXA9700645Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, FOURTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 2, 1996 · N942AX · Doug DC931SDR ABXA9700644Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, SEVENTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 2, 1996 · N942AX · Doug DC931SDR ABXA9700643Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, EIGHTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 1, 1996 · N942AX · Doug DC931SDR ABXA9700642Rib · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, SEVENTH FROM BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.Oct 1, 1996 · N942AX · Doug DC931SDR UPS96221424Rib · crackedINSPECTION TYPE: C. B/S 1367, FIN STA 22.5 RT RIB IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED AN INSTALLED REPAIR PARTS IAW SRM 51-40-3 AND 51-30-2.Sep 19, 1996 · N950UP · Boeing 72725CSDR 97ZZZM519Rib · crackedFIN STATION 35, STRINGER NR 4 SECOND BAY UP FROM THE BOTTOM, RIB CRACKED WITH PREVIOUS ANGLE REPAIR, STOP DRILL IS NET .25 INCH AND CRACKED ON FORWARD SIDE OF RIB RUNS TO THE SIDE OF STOP DRILL. CRACK RUNS PAST ANGLE DOUBLER RT SIDE OF VERTICAL STABILIZER. RSep 14, 1996 · N553NA · Boeing 7272J7SDR MWEA96502Spar Cap · crackedDURING INSP, A 1.25 INCH CRACK FOUND IN RT ELEVATOR UPPER SPAR CAP AT STA XE151. COMPLETED A REPAIR IAW SRM 55-02 FIG 9, CONFIGURATION -503.Sep 12, 1996 · N209ME · Doug DC932SDR 96ZZZX5527Rib · crackedMAJOR INSPECTION, FOUND VERT PYLON RIB CRACKED, NORMAL WEAR AND TEAR.Aug 15, 1996 · N376AL · Skrsky S76ASDR 96ZZZX5522Rib · crackedMAJOR INSPECTION, VERTICAL PYLON RIB CORRODED INNER GRANULAR, CRACKED, NORMAL WEAR AND TEAR.Aug 15, 1996 · N376AL · Skrsky S76ASDR UPS96220817Midspar · corrodedINSPECTION TYPE: SI. CORROSION RT FIN MID-SPAR HAS FRETTING CORROSION AT ACCESS PANEL 9602 FIN STA 226.7 FIN W.L. 168.39 AND BS 1495.75. CORROSION REMOVAL OUT OF LIMITS, REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PARTS PER TRAMCO E.W.O. 96-2402.Jul 31, 1996 · N920UP · Boeing 727180CSDR MWEA96311Ribs · crackedDURING D-CHECK, THREE RIBS WERE FOUND CRACKED THROUGH THE AFT FASTENER HOLES IN THE VERTICAL STABILIZER LEADING EDGE. REPAIRED THE CRACKED RIBS WITH ANGLE DOUBLERS IAW SRM 55-01, FIG 2 SHEET 3.Jul 31, 1996 · N501ME · Doug DC932SDR AALA961151Rib · drill marksAFW - FOUND VERTICAL STABILIZER RIB AT STATION 206 HAS DRILL MARKS. (M)Jul 31, 1996 · N662AA · Boeing 757223SDR UPS96220939Rib · crackedINSPECTION TYPE-C, FS 1352 FIN STA 22.5 LT RIB IS CRACKED. CUTOUT DAMAGED AREA PER SRM 51-40-3, FAB'D AND INSTALLED ANGLE DOUBLER PER SRM 51-40-3 AND 51-30-2.Jul 30, 1996 · N951UP · Boeing 72725CSDR UPS96220944Spar Skin · corrodedINSPECTION TYPE-C, RT VERT STAB INNER SPAR SKIN CORRODED BEYOND LIMITS STA 1342. REMOVED DAMAGED SKIN, FAB'D AND INSTALLED REPAIR PARTS PER DHC SK 951-982.Jul 29, 1996 · N951UP · Boeing 72725CSDR UPS96220935Doubler · crackedINSPECTION TYPE-C, LT INNER SPAR SKIN, INTERNAL DOUBLER CRACKED. REMOVED, FAB'D AND INSTALLED INNER SPAR SKIN INTERNAL DOUBLER PER BOEING DWG 65-17509 AND UPS SRM 51-30-02.Jul 20, 1996 · N951UP · Boeing 72725CSDR UPS96220938Spar Skin · corrodedINSPECTION TYPE-C, LT INNER SPAR SKIN IS CORRODED BEYOND LIMITS STA 1342 LT. REMOVED DAMAGE, FABRICATED AND INSTALLED INNER SPAR SKIN DOUBLERS AND REPAIR DOUBLERS PER BOEING DWG 65C-29055 AND 951-982.Jul 18, 1996 · N951UP · Boeing 72725C
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