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 C2XA98IA004Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER RIGHT SIDE DRAG ANGLE CRACKED. MAINTENANCE REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW EC5530-01013. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 8, 1998 · N27707 · Emb EMB120RTSDR DL72W980119Stringer · crackedTHE 3RD BAY DOWN INSIDE ACCESS 9504 ON LT SIDE STRINGER HAS .25 INCH CRACK EMANATING FROM BELOW BOLT HEAD. DYE CHECKED AREA PER PS 900-6-3. AREA VERIFIED AS CRACKED. STOP DRILLED ENDS OF CRACKS. DYE CKD TO VERIFY CRACK END. FAB REPAIR PARTS PER M/M 55-30-Jan 6, 1998 · N297WA · Boeing 727247SDR DL72W980118Stringer · crackedTHE 3RD BAY DOWN INSIDE ACCESS 9504 STRINGER IS CRACKED ON LT SIDE. STOP DRILLED CRACK, DYE CKD TO VERIFY CRACK END, FAB REPAIR PARTS PER M/M 55-30-0 FIG 803. INSTALLED REPAIR.Jan 6, 1998 · N297WA · Boeing 727247SDR DL72W980110Stringer · crackedSTRINGER CRACKED INSIDE VERTICAL STAB RT SIDE 3RD BAY UP FROM LOWER WEB. REPAIRED PER M/M 55-30-0 FIG 803.Jan 5, 1998 · N297WA · Boeing 727247SDR HEEA0012417Fin Assembly · looseFIN ASSY HAS LOOSE STRINGER.Dec 31, 1997 · N467PH · Bell 407SDR DL72S980108Web · crackedWEB CRACKED VERTICAL STAB INTERIOR, WEB CRACKED LT SIDE OF VERTICAL, APPROX STA 1303 ABOVE S-DUCT. REPAIRED PER SRM 53-10-4.Dec 22, 1997 · N403DA · Boeing 727232SDR DL72S980107Web · crackedWEB CRACKED VERTICAL STAB INTERIOR, WEB CRACKED RT SIDE OF VERTICAL APPROX STA 1303. REPAIRED PER SRM 53-10-4.Dec 22, 1997 · N403DA · Boeing 727232SDR ASAA9780281Shim · brokenOAK - DURING 30K CHECK, BROKEN SHIM WAS FOUND ON LT HORIZONTAL STABILIZER PIVOT SUPPORT FITTING THROUGH-BOLT. TRIMMED SHIM IAW ASA EA 5530-01042. AIRCRAFT TT: 54,110 HOURS. ACFT TC: 28,793. (X)Dec 9, 1997 · N955AS · Doug DC982SDR CALA9701705Angle · crackedINSPECTION FOUND A .75 INCH CRACK EXTENDING FROM FASTENER IN RT AFT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1474. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 23.Dec 1, 1997 · N14880 · Doug DC981SDR 97ZZZX5100Hinge · seizedFOUND THE RUDDER TOP HINGE BOLT SEIZED IN THE HINGE BEARING AND COULD NOT BE FREED. BOTH HINGE ASSEMBLIES (THE RUDDER AND VERTICAL STABILIZER) HAD TO BE REPLACED. THE CORROSION WAS SEVERE AND THERE WAS NO EVIDENCE OF LUBRICATION.Nov 25, 1997 · N272HJ · Piper PA31310SDR ABXA9701838Angle · crackedDURING C-CHECK, FOUND A LOWER LT ATTACH ANGLE CRACKED ON VERTICAL STAB AFT SPAR. REPLACED ANGLE IAW DC9 SRM 51-30-5.Nov 17, 1997 · N984AX · Doug DC932SDR DL72W972276Stringer · crackedFOUND ON B-2 LETTER CK, CRACK AT BOLT HOLE OF VERTICAL STAB STRINGER S-9 AT STAB STA 133.80 RT SIDE. REPAIRED PER MM 55-30-0.Nov 6, 1997 · N2812W · Boeing 727247SDR ABXA9701795Angle · crackedDURING C-CHECK, FOUND L-ANGLE WHERE THE VERTICAL STAB JOINS THE FUSELAGE, LEFT SIDE HAS A 3 INCH CRACK IN THE RADIUS. REPAIRED ANGLE IAW DC9 SRM 53-05.Nov 6, 1997 · N984AX · Doug DC932SDR MZZA97315Fitting · wornKUL - NRC: 844297 - Q-CHECK - VERTICAL STABLIZER LOWER RUDDER TAB SUPPORT FITTING HAS WORN TAB ROD BOLT HOLES. WORN HOLES REAMED TO 0.620 INCH AND BUSHINGS FABRICATED AND INSTALLED IAW ECRA 5530-01195. TAB RODS RE-INSTALLED AND TAB RIGGING/FUNCTIONS CHECK CNov 5, 1997 · N69741 · Boeing 727224SDR CALA9701571Bracket · corrodedINSPECTION FOUND MOUNT BRACKET FOR VERTICAL STABILIZER PANEL 374ER CORRODED. THE MOUNT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-31-01.Nov 3, 1997 · N14090 · Doug DC1030SDR ASAA9710107Angle · wornSEA - DURING C-CHECK, THE RIGHT VERTICAL FIN SKATE ANGLE WAS FOUND TO BE WORN. REPAIRED PER EA 5530-01041. (M)Oct 31, 1997 · N730AS · Boeing 737290CSDR ABXA9701771Angle · corrodedVERTICAL STABILIZER, TO FUSELAGE ATTACH ANGLE CRACKED AND GOUGED ON RT AFT SIDE AT REAR SPAR. REPAIRED IAW DC8 SRM 53-2-5, 51-1-8 AND ABX REA D853-19535MR.Oct 30, 1997 · N828AX · Doug DC863SDR DL72S972262Web · crackedWEB - CRACKED VETICAL STAB INTERIOR FS 1303 WEB CRACKED AT STRINGER CUTOUT, RH SIDE FABRICATED REPAIR DOUBLER AND DRILLED PE R SRM 53-10-4 FIG 17BEGAN INSTALLING DOUBLER PER SRM 53-10-4 FIG 17.STOP DRILLEDCRACK AND DYE CHECKED PER SRM 53-10-4. COMPLETED INSTAOct 27, 1997 · N518DA · Boeing 727232SDR DL72S972261Web · crackedWEB - CRACKED VERT STAB INTERIOR FS1303 WEB CRACKED A T LOWER LH CORNER FABRICATED REPAIR DOUBLER AND DRILLED PE R SRM 53-10-4 FIG 17DYE CHECKED AND STOP DRILLED CRACK PER SRM 53-10-4. OK TO INSTALL REPAIR. INSTALLED REPAIR PER SRM 53-10-4 FIG 17Oct 27, 1997 · N518DA · Boeing 727232SDR DL72E972331Stringer · crackedSTRINGER CRACKED VERT STAB INTERIOR STRINGER 1R AT RIB NR 4. STOP DRILLED CRACKS PER M/M 55-30-0 FIG 803. FABRICATED REP AIR PER M/M 55-30-0 PG 803 FIG 803. OK TO INSTALL. INSTALLED REPAIR PER M/M 55-30-0 PG 803 FIG 803.Oct 27, 1997 · N831WA · Boeing 727247SDR DL72S972157Stringer · crackedVERT FIN STR 9L IS CRACKED AT FIN STA 133.800. REPAIR PER MM 55-30-0.Oct 25, 1997 · N411DA · Boeing 727232SDR DL72S972156Stringer · crackedVERT FIN STR 9L CRACKED AT FIN STA 157.200. REPAIR PER MM 55-30-0.Oct 25, 1997 · N411DA · Boeing 727232SDR UPS97425182T-Fitting · crackedINSPECTION TYPE-C, FOUND T-FITTING CRACKED AT FIN STA 143 2ND RIB FROM BELOW. INTERNAL LT SIDE JUST AFT OF FRONT SPAR FROM VERT STAB. REPLACED T-FITTING AT FIN STA 143 LT ACC SRM 51-30-02.Oct 24, 1997 · N677UP · Boeing 747123FSDR USAA970306Frame · crackedPIT - DURING C-2 CHECK, FOUND 1.5 INCH CRACK EXTENDED INTO RADIUS AT TAIL COMPARTMENT, AFT LEFT SIDE OF CANTED FRAME 1388, VERTICAL STAB FRONT SPAR. REPLACED SRO 955003, -5, -7, -9, -3 7075-T6 ANGLES AND DOUBLERS PER SRM 55-02 FIG 26 PAGE 99-101. (M)Oct 23, 1997 · N803US · Doug DC981SDR UPS97824881Doubler · corrodedINSPECTION TYPE-C, LT VERT STAB PANEL BELOW VHF ANTENNA AND FWD OF AFT SPAR HAS SEVERE CORROSION. REPAIRED IAW DHC SK 801-001.Oct 22, 1997 · N801UP · Doug DC873FSDR DL72S972073Chord · crackedFOUND ON F-2 LETTER CK, LT ATTACH CHORD CRACKED .75 INCH AT VERTICAL STAB S-7L. REPAIRED PER MM 55-30-0.Oct 16, 1997 · N524DA · Boeing 727232SDR CA971113072Adapter · cracked(CAN) INSPECTION AT HMV FOUND THE FORWARD VERTICAL STABILIZER ATTACHMENT ADAPTER CRACKED. THE CRACK ORIGINATED AT THE RIGHT HAND BOLT HOLE EXTENDING .375 INCH INBOARD ON THE LOWER FACE AND .125 INCH VERTICALLY UP THE INBOARD SIDE OF THE BOLT HOLE. DEFECT IS Oct 16, 1997 · Dhav DHC6300SDR CALA9701536Plate · crackedINSPECTION FOUND VERTICAL STABILIZER UPPER LT REINFORCEMENT PLATE JUST FOWARD OF TENSION TIE FORWARD ATTACH BOLT AREA CRACKED. THE CRACK WAS 1.5 INCH LONG. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.Oct 10, 1997 · N33785 · Boeing 727232SDR CALA9701535Bulkhead · crackedINSPECTION FOUND VERTICAL STABILIZER LEADING EDGE LOWER PANEL UPPER ATTACH BULKHEAD CRACKED AT ATTACH HOLES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.Oct 10, 1997 · N33785 · Boeing 727232SDR ABXA9701599Angle · corrosionLT FUSELAGE TO VERTICAL STAB ATTACH ANGLE IS CORRODED FROM THE REAR SPAR TO THE CENTER SPAR OF VERTICAL STAB. REPAIRED ATTACH ANGLE IAW SRM 53-2-5, 51-1-20D AND 51-1-21.Oct 10, 1997 · N843AX · Doug DC861SDR HEEA0011348Stabilizer Assy · separatedSTABILIZER ASSY SEPARATED AT OUTER EDGES.Oct 9, 1997 · N6160Y · Bell 206L3SDR ABXA9701676Angle · crackedDURING C-CHECK, FOUND THE LT VERTICAL STABILIZER FUSELAGE ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC9 SRM 53-05.Oct 9, 1997 · N954AX · Doug DC941SDR SIMA972814Web · corrosionABI - WEB REINFORCEMENT AT FS 287 HAD CORROSION BEYOND LIMITS. REMOVED AND REPLACED WEB REINFORCEMENT IAW SAAB SRM 51-40-21. AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 8, 1997 · N359SB · Saab 340BSDR HEEA0011313Fin Assy · separatedFIN ASSY CORRODED AND SEPARATED BEYOND REPAIR.Oct 8, 1997 · N5742H · Bell 206L1SDR HEEA0011312Fin · corrodedVERT FIN CORROSION AND SEPARATED BEYOND REPAIR.Oct 8, 1997 · N2753F · Bell 206B3SDR TWAA9805804Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND VERTICAL FIN TO FUSELAGE ATTACH ANGLE CRACKED JUST FORWARD OF LEFT FIN ACCESS PLATE, AT DORSAL FIN FITTING AREA. REMOVED AND REPLACED ANGLE PER SRM 51-01 PAGE 1 ITEM C. (M)Oct 7, 1997 · N993Z · Doug DC931SDR DL72W971970Stringer · crackedVERT STAB STR 9L IS CRACKED AT FIN STA 133.800. REPAIRED PER M/M 55-30-0.Oct 3, 1997 · N2811W · Boeing 727247SDR DL72W971968Stringer · crackedFOUND DURING D2 LETTER CHECK, VERT STAB STR 9L CRACKED AT FIN STA 133.800. REPAIRED PER M/M 55-30-0.Oct 3, 1997 · N2811W · Boeing 727247SDR DL72S972238Web · crackedA 1.5 INCH CRACK UPPER RT CUTOUT 1303 WEB ABOVE S-DUCT. A 1 INCH CRACK LOWER RT CUTOUT 1303 WEB ABOVE S-DUCT. A 1 INCH CRACK LOWER LT CUTOUT 1303 WEB. A 1 INCH CRACK UPPER LT CUTOUT 1303 WEB. FOUND DURING B2 LETTER CHECK, INSTALLED PERM REPAIR PER SRM 53-1Oct 3, 1997 · N493DA · Boeing 727232SDR CA971010004Doubler · damaged(CAN) DURING MANUFACTURING AND INSTALLATION OF THE DORSAL FIN, A RIVET AT THE REAR PRESSURE BULKHEAD (STN 345.0) WAS DRILLED THROUGH THE SKIN, DOUBLER AND FLANGE ANGLE ADJACENT TO A BULKHEAD ATTACHMENT RIVET. AIRCRAFT TT: 2,277 HOURS.Oct 3, 1997 · Cessna 550SDR HEEA0011189Fin Assy · mis drilledFIN ASSY MIS-DRILLED HOLES.Oct 2, 1997 · N3207Q · Bell 206L3SDR HEEA0011188Vertical Fin · corrodedVERTICAL FIN CORRODED AT TOP.Oct 2, 1997 · N2275Q · Bell 206B3SDR DL72W971945Stringer · crackedFOUND DURING A2 LETTER CHECK, VERT STAB STR 96 CRACKED AT FIN STA 180.6. REPAIR PER M/M 55-30-0.Oct 1, 1997 · N296WA · Boeing 727247SDR QXEA9800101Angle · crackedPDX - CRACKS LOCATED ON THE RIGHT CONNECTION ANGLE IN THE RADIUS AND THROUGH UPPER RIVETS ADJACENT TO 16 PERCENT FRONT SPAR. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.Sep 30, 1997 · N486US · Fokker F28MK4000SDR HEEA0011125Fin Assy · crackedFIN ASSY CRACKED.Sep 30, 1997 · N5005F · Bell 206L1SDR HEEA0011124Fin Assy · groovedFIN ASSY GROOVED BEYOND LIMITS.Sep 30, 1997 · N6160Y · Bell 206L3SDR 98ZZZM43Rivets · looseVERTICAL STAB TO FUSELAGE CLOSING ANGLE ON LEFT AND RIGHT SIDES AT AFT ENDS HAVE RIVETS WORKING, 3 ON THE LEFT AND 2 ON THE RIGHT CIRCLED IN BLACK PEN. REMOVED RIVETS ON LEFT AND RIGHT VERTICAL STAB TO FUSELAGE CLOSING ANGLES, 3 ON LEFT AND 2 ON RIGHT. INSTASep 30, 1997 · N615AW · Bag BAE146300ASDR CA971007014Skin · damaged(CAN) INSPECTION OF FINS FOUND THAT TWO GRINDING MARKS WERE MADE DURING MANUFACTURE AT AFT BOTTOM SECTION OF FORMERS FOR INSTALLATION OF FAIRINGS. AN ASB WILL BE ISSUED TO COVER.Sep 29, 1997 · Bell 407SDR CKSA97537Angle · crackedDURING CPCP CHECK INSPECTION, FOUND FS 1343 AT S11L INTERIOR VERTICAL STAB ATTACH ANGLE CRACKED. REMOVED CRACKED ATTACH ANGLE. INSTALLED NEW ATTACH ANGLE IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C55-395-11 PART 1 OF 1. NON-ROUTINE TASK Sep 17, 1997 · N727CK · Boeing 72722CSDR DL72S971821Web · crackedWEB CRACKED PAST STOP DRILL AT STA 1303 RT SIDE INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 17.Sep 12, 1997 · N528DA · Boeing 727232
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