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"

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SDR HAIHEEA9280Stabilizer Assy · corrodedSTAB LOWER AFT CORNER SEPARATED ON L/H AND R/H SIDES. CORRODEDMar 31, 1997 · N3178K · Bell 206L1SDR HAIHEEA9268Stabilizer Assy · defectiveCANNOT INSTALL ANGLES DUE TO INSERTS NOT PROPERLY INSTALLED.Mar 31, 1997 · N21497 · Bell 206L3SDR HAIHEEA9258Stabilizer Assy · separationSTABILIZER SEPARATED AT "T" EDGE.Mar 31, 1997 · N5737T · Bell 206L1SDR DL72W970587Stringer · crackedFOUND VERTICAL FIN LT SIDE, 3RD STR FROM REAR SPAR CRACKED 3RD BAY, ABOVE FIN ACCESS PNL 9504. REPAIRED PER M/M 55-33-00, FIG 803.Mar 26, 1997 · N2820W · Boeing 727247SDR 97FDEA00184Fitting · corrodedNR 0467 008, WHILE WORKING CARD NR 7-5530-7-2310 F, FOUND CORROSION ON LT AND RT AFT CLOSURE RIB FITTING; CORROSION LOCATED AROUND BUSHING OUTSIDE DIAMETER. *S/D* REMOVED AND REPLACED LT AND RT AFT CLOSURE RIB FITTINGS IAW FED-EX EA NR 7-5510-32916.Mar 18, 1997 · N243FE · Boeing 727277SDR DL72S970454Stringer · crackedFOUND ON LETTER CHECK, .75 INCH CRACK IN VERTICAL STABILIZER S-9 AT FOURTH BULKHEAD ABOVE CRAWL-WAY OPENING. REPAIRED PER MM 55-30-0.Mar 10, 1997 · N521DA · Boeing 727232SDR CALA9700520Angle · crackedINSPECTION FOUND AN 8 INCH CRACK IN COWL TO VERTICAL STABILIZER Z-ANGLE AT ACCESS 364QR. THE CRACKED AREA WAS REMOVED, A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 55-31-01 AND 51-31-01.Mar 9, 1997 · N68041 · Doug DC1010SDR HALA97103Angle · crackedLEVE 2 CORROSION, CRACKS, CHAFED DAMAGE AND WEAR ON FORE AND AFT ATTACH ANGLE 'S' FORWARD CURVED PANEL AT VERTICAL STAB TO FUSELAGE STATION 1258 A/C CENTERLINE ABOVE STRINGER 1. REMOVED AND REPLACED DAMAGED ATTACH ANGLES WITH REPAIR PARTS FABRICATED, PER 55-0Mar 6, 1997 · N709HA · Doug DC951SDR HALA97102Angles · corrodedFS 1257 VERT STABILZER INTERNAL, LEVEL 2 CORROSION, ON ANGLE FROM LEFT TO RIGHT SIDE OF STABILIZER ACCESS THROUGH SKIN OPENINGS FOR LEFT AND RIGHT VERTICAL STABILZER FRONT SPAR OPENINGS. REMOVED AND REPLACED ANGLES PER SRM 55-02 FIG 1 AND 51-10-03. (M)Mar 6, 1997 · N709HA · Doug DC951SDR DL72S970400Chord · crackedFOUND THE VERTICAL STAB BULKHEAD CHORD CRACKED AT STA 157.200, STR 10 LEFT. REPAIRED PER M/M 55-30-0.Mar 4, 1997 · N529DA · Boeing 727232SDR DL72S970399Stringer · crackedFOUND THREE VERTICAL STABILIZER STRINGERS CRACKED AT STR 9 LEFT STA 157.200, STR 9 LEFT STA 110.400 AND STR 6 LEFT STA 6.372. REPAIRED PER M/M 55-30-0.Mar 4, 1997 · N529DA · Boeing 727232SDR VJ970139Angle · delaminatedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THAT DURING INSPECTION FOR COMPLIANCE OF AD 89-08-10 IAW ASB 52-154 AND ASB 53-223. DETERMINED REPAIR INSTALLED IS A SINGLE SPLICE ATTACH ANGLE. REMOVED LT AND RT VERTICAL Feb 27, 1997 · N921VV · Doug DC932SDR USAA970076Drag Angle · crackedPIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AT RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE STA 1087. INSTALLED DOUGLAS PER SRM 53-05 FIG 23B. (M)Feb 26, 1997 · N959VJ · Doug DC931SDR F3LA97093Skate Angle · crackedRIGHT VERTICAL STAB AFT MOUNT LUG INBOARD SKATE ANGLE CRACKED. REMOVED RIGHT VERTICAL STAB AFT MOUNTING LUG INBOARD SKATE ANGLE. FABRICATED REPAIR ANGLE FROM MATERIAL OF 7075-0 .071 AND HEAT TREATED BY GIDDENS INDUSTRIES, INC TO 7075-T6, PO NR 1ML212756. INFeb 26, 1997 · N205AU · Boeing 737201SDR HEEA979131Stabilizer Assy · crackedSTAB HAS A CRACK LEFT AFT AROUND RIVET AND CORROSION UNDER SHIM TOP LEFT.Feb 21, 1997 · N6095S · Snias AS350B2SDR ABXA9700487Bracket · corrodedDURING C-INSPECTION, FOUND UPPER RUDDER HINGE BRACKET CORRODED AT THE RIGHT AND LEFT ATTACH BOLTS. REPLACED RUDDER HINGE BRACKET IAW DC9 MAINTANCE MANUAL CHAPTERS 55-50-0 AND 20-16-0.Feb 21, 1997 · N985AX · Doug DC932SDR VJ970127Dorsal Fin · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, TWO L-ANGLES CRACKED IN SIDE DORSAL FIN AT STATION 1074 BOTH APPROXIMATELY 1 INCH IN LENGTH. REMOVED CRACKED L-ANGLES FROM INTERIOR OF DORSAL FIN FS 1074, FABRICATED AND REPFeb 20, 1997 · N919VV · Doug DC932SDR 97ZZZX1359Web · mismanufacturedUPON RECEIVING PART (NEW) FROM SIKORSKY, FOUND PYLON WEB MADE OF WRONG ALLOY OR NOT HEAT TREATED CORRECTLY. METAL TOO SOFT.Feb 20, 1997 · Skrsky S76SDR DL72S970281Stringer · crackedS-8L CRACKED AT FIN STA 110.40. FABRICATED REPAIR PER M/M 55-30-0 FIG 803, STOP DRILLED CRACKS AND INSTALLED REPAIR PER M/M 55-30-0 FIG 803.Feb 15, 1997 · N409DA · Boeing 727232SDR IXXA9700035Angle · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE RIGHT HAND VERTICAL STABILIZER BASE ATTACH ANGLE AT FUSELAGE STATION 1593 TO 1604. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF A REPAIR ANGLE IN ACCORDANCE WITHFeb 12, 1997 · N51CX · Doug DC862SDR CALA9700167Fitting · crackedINSPECTION FOUND A 1 INCH CRACK AT BOTTOM AFT FACE OF VERTICAL STABILIZER LT AFT OUTBOARD FITTING TO LUG. THE CRACKED FITTING WAS REMOVED, A NEW FITTING WAS DRILLED AND INSTALLED IAW SRM 51-10-7 AND 51-30-2.Feb 5, 1997 · N14233 · Boeing 737217SDR AALA970295Stringer · corrodedTUL - VERT FIN STATION 87 STRINGER 3R CORRODED AT ATTACH POINT TO NR 5 RIB. REPAIRED STRINGER 3R VERT FIN STATION 87 IAW ESO 11697 AND SRM 51-40-4. (M)Feb 5, 1997 · N843AA · Boeing 727223SDR AALA970292Stringer · corrodedTUL - VERT FIN STRINGER 1L, CORRODED UNDER LEVELING COMPOUND AT RIB NR 5 ATTACH POINT. CUT OUT DAMAGED AREA, DRILLED UP AND INSTALLED REPAIR ANGLES AND CLIPS AND FILLER PER SRM 55-30-4. (M)Feb 5, 1997 · N843AA · Boeing 727223SDR USAA970043Angle · crackedPIT - DURING B-CHECK, FOUND .75 INCH CRACK AT LEFT VERTICAL STABILIZER DRAG, DORSAL FIN, ANGLE JUST AFT OF STATION 1076. REPAIRED FOR MFG DRWG ANGLE AND DOUBLERS PE EA 46217. (M)Jan 31, 1997 · N912VJ · Doug DC931SDR 97ZZZX1274Vertical Fin · crackedDAILY INSPECTION FOUND CRACK ON LEFT AUXILIARY VERTICAL FIN AT ATTACH POINT (4 INCH) SPIDER. THIS IS A PROBLEM THAT WAS CORRECTED MANY YEARS AGO ON 206L-1 SERIES.Jan 28, 1997 · N355AL · Bell 206L3SDR DL72S970144Stringer · crackedA 1 INCH VISIBLE CRACK IN VERT STAB S-8L, 1 INCH VISIBLE CRACK IN VERT STAB S-9L, 1 INCH VISIBLE CRACK IN VERT STAB S-7L. REPAIRED PER M/M 55-30-0.Jan 24, 1997 · N404DA · Boeing 727232SDR DL72S970143Vert Stab Web · crackedA 1.5 INCH CRACK IN VERT STAB WEB STA 1303 ACROSS TOP OF NR 2 ENG S-DUCT LOWER RT CORNER. REPAIRED PER M/M 53-11-0.Jan 24, 1997 · N404DA · Boeing 727232SDR DL72S970141Stringer · crackedFOUND DURING F-2 LETTER CHECK, VERTICAL STAB STR 7 LEFT STA 133.8 CRACKED 1 INCH, STR 8 LEFT STA 157.2 CRACKED 1 INCH AND STR 9 LEFT STA 133.8 CRACKED 1 INCH. REPAIRED PER M/M 55-30-0.Jan 24, 1997 · N404DA · Boeing 727232SDR DHL9774113CStringer · crackedAT C-CHECK, VERTICAL STAB INTERIOR, FIN STA 157.2 STR 8 TO FRAME IS CRACKED. CUT OUT DAMAGED AREA AT FLANGE OF STRINGER 8, CUT NEW ANGLE AND INSTALLED REPAIR PER SRM 55-30-4. REPAIR 1 BY 12, STRAP 12.Jan 23, 1997 · N741DH · Boeing 7272Q9SDR P5CA9700214Web · damageGOUGES/CRACK ON WEB AT STA 82-8 LT VERTICAL STAB. BLENDED GOUGES SRM 51-10-01. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-02.Jan 22, 1997 · N858FT · Boeing 747123SDR 97ZZZM438Rib · chafedVERTICAL STABILIZER LEADING EDGE STRUCTURE BEHIND ACCESS NR 325AL AND AR HAS TWO HOT AIR LINES PASSING THROUGH A DIAPHRAMS LIGHTNING HOLE AND CHAFING ON BOTH LEFT AND RIGHT SIDES. RIGHT SIDE HAS FLANGE OF HOLE WORN AWAY. REPAIRED VERTICAL STABILIZER LEADING Jan 17, 1997 · N612AW · Bag BAE146300ASDR TWAA9710010Hinge Plate · corrodedMCI - DURING OP-16, FOUND CORROSION AT VERTICAL STABILIZER HORIZONTAL STABILIZER LT HINGE PLATE, INBOARD AND OUTBOARD, AND AT CHAMBER BORE HOLE. REPLACED HINGE PLATES PER SRM 51-01 AND SRM 51-30-0. (M)Jan 16, 1997 · N906TW · Doug DC982SDR TWAA9806001Angle · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND A CRACK IN THE VERT STAB TO FUSELAGE ATTACH ANGLE, LEFT STATION 1437. INSTALLED NEW ANGLE PER SRM 51-01, AND FASTENERS PER SB 53A223 AND TWA STD PRACTICES. (M)Jan 15, 1997 · N906TW · Doug DC982SDR 97ZZZM373Angle · corrodedDURNG C-1 CHECK AT AERO CORP 31J, THE RIGHT VERTICAL STABILIZER LOWER MOUNT HORIZONTAL ATTACH ANGLE WAS FOUND TO BE CORRODED BEYOND ALLOWABLE LIMITS. REMOVED AND FABRICATED NEW SUPPORT BRACKET PER BAC PRING 69-39677, MATERIAL 7075 T-6 .365 DIM, 5.5 INCH BY 2.Jan 9, 1997 · N1PC · Boeing 7372P6SDR UPS97222107Intercostal · crackedINSPECTION C-CHECK, INTERCOSTAL IS CRACKED RT SIDE FIN STA 22.5 B.S.1367. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-40-3 AND 51-30-02.Jan 6, 1997 · N954UP · Boeing 727185CSDR UPS97222087Intercostal · crackedINSPECTION C-CHECK, LT INTERCOSTAL IS CRACKED BS 1367 FIN STA 22.5. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-3 AND 51-30-02.Jan 6, 1997 · N954UP · Boeing 727185CSDR UPS97221985Torque Box · corrodedINSPECTION TYPE: C. VERTICAL FIN TORQUE BOX RT HORIZONTAL CHORD BS 1342 FIN STA ZERO IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED PER DHC SK-954-576 REF. ENRG FILE NR 727-55-0339.Jan 6, 1997 · N954UP · Boeing 727185CSDR DHL9774011CVert Stab · crackedAT C-CHECK, VERTICAL STAB HAS CRACK ON LOWER LT FASTENERS. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 5 BY 4.Jan 3, 1997 · N740DH · Boeing 7272Q9SDR C2XA97IA004Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE ANGLE USING A SPLICE REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 2, 1997 · N16710 · Emb EMB120RTSDR C2XA97IA003Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE PEFORMED A SPLICE REPAIR OF THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 2, 1997 · N16710 · Emb EMB120RTSDR 97ZZZM197Beam · corrodedFOUND CORROSION ON TRAILING EDGE BEAM ON VERTICAL FIN 4H SIDE ATT FIN STATION 127.10 RUD STATION 60.15 (MARKED). REPAIRED TRAILING EDGE BEAM PER TRAMCO EWO 96-09-29. (M)Dec 19, 1996 · N464AT · Boeing 7372L9SDR DL72W962768Stringer · crackedFOUND DURING MV2, JUST INSIDE ACCESS 9504 ON RT SIDE 2ND FROM TOP STRINGER, CRACK AT RIB ATTACH BOLT. FABRICATED AND DRILLED REPAIR PARTS PER M/M 55-30-0 PG. 803. INSTALLED REPAIR PER M/M 55-30-0.Dec 16, 1996 · N2817W · Boeing 727247SDR 9626279618Fitting · crackedDURING ACCEPTANCE CHECK, FOUND VERTICAL STABILIZER LOWER LEADING EDGE FORWARD LEFT ANCHOR WITH AN 8 INCH CRACK AT FS 1089, LONGERON 2L. REPLACED FITTING PER EA 99-097758.Dec 9, 1996 · N618NW · Doug DC932SDR ABXA9700158Fairing · delaminatedWHILE COMPLYING WITH A C INSPECTION, FOUND THE LEFT UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING DELAMINATED. REPLACED LEFT HAND UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING IAW ABD JOB CARD NR 40232.Dec 7, 1996 · N935AX · Doug DC933FSDR ABXA9700153Fairing · delaminatedWHILE COMPLYING WITH A C INSPECTON, FOUND THE RIGHT UPPER HORIZONTAL TO VERTICAL STABLIZER FAIRING DELAMINATED. REPLACED THE RIGHT UPPER HORIZONTAL TO VERTICAL STABLIZER FAIRING IAW ABX JOB CARD NR 40232.Dec 3, 1996 · N935AX · Doug DC933FSDR CA961120041Fasteners · broken(CAN) ON ANNUAL INSPECTION FASTENERS IN THE VERTICAL STABILIZER ATTACH FITTINGS WERE FOUND LOOSE. SEVERAL OF THE FASTENERS WERE IN FACT BROKEN OFF. FASTENERS HAD BEEN PREVIOUSLY INSTALLED AS PER AD 80-19-14AND SB 600-88A.Nov 22, 1996 · Piper PA60600SDR DL72S962560Stringer · crackedSTRINGER CRACKED ON VERT STAB STA 157.2 STR 4 LT. REPAIRED PER M/M 55-30-0 FIG 803.Nov 21, 1996 · N528DA · Boeing 727232SDR DL72S962559Stringer · crackedSTRINGER CRACKED ON VERT STAB STR 9 STA 44 RT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.Nov 21, 1996 · N528DA · Boeing 727232SDR UPS96221695Chord · crackedINSPECTION TYPE-C, VERTICAL STAB RT LOWER TORQUE BOX CHORD CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED REPAIR PARTS IAW DHC SK947-123 AND SRM 51-30-2 REF ENGINEERING FLIE NR 727-55-0338.Nov 2, 1996 · N947UP · Boeing 72725CSDR USAA960706Angle · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 1.5 INCH CRACK IN LEFT DRAG ANGLE AT FS 1095 LEFT VERTICAL FIN. INSTALLED DOUBLER PER SRM 53-05 FIG 23B. (M)Oct 28, 1996 · N958VJ · Doug DC931
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