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 QXEA0001178Spar Cap · scratchedYYC- VERTICAL STAB FWD SPAR CAP ANGLES SCRATCHED. REPAIRED IAW DHC-8 RD 8-55-584.Apr 27, 2000 · N829PH · Dhav DHC8102SDR CALA0000578Angle · crackedDORSAL FIN FUSELAGE RT SIDE ANGLE IS CRACKED AT CENTER (1). REMOVED AND REPLACED ANGLE PER SRM 51-30-02, 51-10-04, 51-10-03,AND 51-30-04.Apr 27, 2000 · N71828 · Doug DC982SDR C2XA00IA105Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310--1-32, AND THE AIRCRAFT WApr 17, 2000 · N12957 · Emb EMB145SDR C2XA00IA104Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01032, AND THE AIRCRAFTApr 17, 2000 · N12957 · Emb EMB145SDR AALA20000679Angle · crackedTUL- LEFT VERTICAL STABILIZER TO FUSELAGE CORD ANGLE CRACKED THROUGH 2 FASTENERS IN VERTICAL LEG STA 1381. REPAIRED CORD ANGLE PER ESO 11697 DATED 4-14-00. (X)Apr 17, 2000 · N719AA · Boeing 727227SDR CALA0000454Angle · crackedINSPECTION FOUND LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1474 - 1485. THERE WERE FIVE CRACKS TOTALING 8 INCHES IN COMBINED LENGTH. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-01.Apr 11, 2000 · N12811 · Doug DC982SDR 0001289929Angle · crackedVERTICAL STABILIZER LOWER ATTACH ANGLE CRACKED AT RIGHT SIDE, NEAR AFT END. REPAIRED DAMAGED AREA AND CONFIRMED. REPAIRED IAW SRM 53-05 AND EA 99-175537. LP''S 1424295, 1423937Apr 11, 2000 · N8923E · Doug DC931SDR RRXA003841Frame · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO VERTICAL STAB TOP "A" FRAME AT STA. ZR329.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM Apr 10, 2000 · N500MH · Doug DC871FSDR QXEA0001080Angle · crackedPDX - RT VERTICAL STABILIZER CONNECTION ANGLE HAS CRACKS OFF TWO HI-LOCKS. REPAIRED IAW HORIZON AIR EA 4-55-170 AND FOKKER SRM 51-31-02.Apr 7, 2000 · N494US · Fokker F28MK4000SDR C2XA00IA088Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01032, AND THE AIRCRAFT WApr 4, 2000 · N13956 · Emb EMB145SDR C2XA00IA089Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01032, AND THE AIRCRAFT Apr 4, 2000 · N13956 · Emb EMB145SDR ABXA000262Angle · crackedDURING D-CHECK INSPECTION, FOUND LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED AT STATION 1109. REPAIRED ANGLE IAW ABX REA D953-36544-MR.Apr 3, 2000 · N939AX · Doug DC932SDR MWEA00256Skin · gougedVERTICAL SKIN IS GOUGED FROM RIGHT LOWER HORIZONTAL TO VERTICAL FAIRING. FABRICATED AND INSTALLED NEW SKIN PANEL.Apr 3, 2000 · N900ME · Doug DC915SDR QXEA0001079Angle · crackedPDX - RT VERTICAL STABILIZER CONNECTION ANGLE APPEARS TO HAVE CRACKS OFF OF TWO HI LOCKS. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 2, SRM 55-31-01 AND SRM 51-31-05.Apr 2, 2000 · N494US · Fokker F28MK4000SDR SWAA000584Mount · corrodedDURING SCHEDULED D CHECK, FOUND CORROSION DAMAGE IN VERTICAL STABILIZER RT FWD MOUNT LUG BORE. REPAIRED LUG PER ER 00-0278.Mar 28, 2000 · N507SW · Boeing 7375H4SDR AALA2000204Flange · damagedTUL - VERTICAL STABILIZER FIN STATION 242, STRINGER 7 RIGHT. SCREW HEAD WORN DEEP INTO FLANGE. REPAIRED STRINGER IAW ECO 11697, DATED 1-21-00. OVERSIZE HOLE TO .25 INCH. FABRICATE REPAIR STRAP 17-7 PH BY .063 THK. CONDITION TH1050. CAD PLATE, PRIME, INSTMar 28, 2000 · N887AA · Boeing 727223SDR AALA2000205Flange · damagedTUL - VERTICAL STABILIZER FIN STATION 242, STRINGER 7 LEFT, SCREW HEAD WORN DEEP INTO FLANGE. REPAIRED STRINGER IAW ESO 11697 DATED 1-21-00. OVERSIZE HOLE TO .25 INC. FABRICATE REPAIR STRAP, 17-7PHX .063 THK. CONDITION TH1050. CAD PLATE AND PRIME INSTALL SMar 28, 2000 · N887AA · Boeing 727223SDR 00FDEA00172Web · crackedDURING ROUTINE INSP, WEB INSIDE VERTICAL STABILIZER AT FIN STA 110.4 FOUND CRACKED. REPAIRED IAW SRM 53-10-9 FIG 4.Mar 27, 2000 · N186FE · Boeing 72722SDR GAIA0097Plate · crackedDURING HEAVY C-CHECK AT TIMCO/OSC, FOUND VERTICAL STAB REAR FITTING SPLICE PLATE CRACKED THREE INCHES AT AFT SIDE OF 1342 BULKHEAD LBL 16. REPAIRED IAW SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 20, 2000 · N6808 · Boeing 727223SDR DL72K000621Panel · damagedAT HMV A TEMP REPAIR WAS INSTALLED ON LT SIDE OF VERT STAB AT L/E STA 1298 JUST FWD OF L/E PNL 9525. TEMP REPAIR WAS REMOVED AND DAMAGE CUT OUT AND PERM REPAIR INSTALLED PER MM 54-30-0 FIG 802.Mar 20, 2000 · N410DA · Boeing 727232SDR DL73K000526Fitting · corrodedCORROSION WAS FOUND ON THE FORWARD AND AFT FACE OF BOTH THE INNER LUGS OF THE VERTICAL STABILIZER ATTACH FITTING. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED AND PAINTER PER ERA 334169-14. THE DAMAGE WAS FOUND AT HMV.Mar 17, 2000 · N302DL · Boeing 737232SDR DL72L000620Web · crackedWEB CRACKED LT LOWER CORNER INSIDE OF VERT, MARKED. STOP DRILLED CRACK AND MADE REPAIR PARTS PER SRM 53-10-4D. CHEMICAL TREAT PER PS 900-2-4-1 NR 2. OK TO IST DOUBLER. REPAIRED PER SRM 53-10-4D.Mar 16, 2000 · N510DA · Boeing 727232SDR 2000UALA00135Fitting · corrodedDURING THE HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE LUG HOLE AND SURFACE OF THE VERTICAL STABILIZER UPPER CLOSURE RIB FITTING. THE LUG BORE WAS OVERSIZED AND THE SURFACE SPOTFACED TO REMOVE CORROSION. AN OVERSIZED BUSHING WAS INSTALLED TO RESTORE Mar 15, 2000 · N7466U · Boeing 727222SDR AALA2000505Casting · corrodedTUL - FOUND RIGHT AND LEFT BORES AND FACES PITTED OF SIDE LOAD CASTING, LOCATED ON VERTICAL STAB BETWEEN STAB HINGE BEARING LUGS. INSTALLED NEW SIDE LOAD CASTING PER SRM 51-01. (M)Mar 7, 2000 · N484AA · Doug DC982SDR UPS00832204Strap · corrodedINSPECTION TYPE: C123, INSIDE VENT STAB LOWER ACCESS HOLE FUSELAGE BACKSTRAP DOUBLER HAS AREAS OF EXCESSIVE CORROSION.Mar 4, 2000 · N804UP · Doug DC873FSDR 20001115SH011Structure · damagedTAIL OF AIRCRAFT DAMAGED WHILE BEING TOWED OUT OF HANGAR 3. RUDDER SEPARATED INTO 2 PIECES BY A HORIZONTAL TEAR. 1 FOOT SECTION OF REAR SPAR VERTICAL STAB MISSING. ON THE RT SIDE, THE SKIN COMPOSITE MATERIAL IS RIPPED FROM THE STABILIZER FRAME. THE WIDTH OMar 3, 2000 · N838AB · Airbus A310324SDR CA000308003Bolt · broken(CAN) REAR/TOP ATTACHMENT BOLT OF VERTICAL FIN ASSY WAS FOUND BROKEN (STILL IN PLACE) ON 600 HOUR CHECK. THE OTHER 3 BOLTS WERE FOUND BELOW MINIMUM TORQUE VALUE.Mar 2, 2000 · Bell 206BSDR 20000619AP009Panel · damagedDURING PREFLIGHT, FOUND DAMAGE TO THE TAILCONE AND PANEL NR 9779, DIRECTLY IN FRONT OF THE TAILCONE ON THE LEFT SIDE OF THE VERTICAL STABILIZER. A/C WAS FERRIED TO IND FOR MAINTENANCE. PANEL AND TAILCONE REPAIRED PER SRM 51-40-09. (M)Mar 1, 2000 · N765AT · Boeing 727264SDR DL72L000513Web · crackedAT HMV2 FOUND WEB CRACKED INSIDE VERT STAB AT BOTTOM LT SIDE OF S-DUCT STA 1303. REMOVED STIFFENER FROM STA 1303, STA 1323. FABD REPAIR AND STOPPED DRILLED PER SRM 53-10-4D, CHEM TREAT PER PS 900-2-4-1 NR 2, DYE CKD PER PS 900-6-3 NR 1, REPAIRED PER SRM 53-1Feb 21, 2000 · N506DA · Boeing 727232SDR DL72L000512Web · crackedAT HMV2 FOUND WEB CRACKED INSIDE VERT STAB AT BOTTOM RT SIDE OF S-DUCT STA 1303. REMOVED NR 2 ANTI ICE DUCT AT STA 1303 - 1280, FABD REPAIR AND STOPPED DRILLED CRACK PER SRM 53-10-4D, CHEM TREATED PER PS 900-2-4-1 NR 2, DYE CKD PER PS 900-6-3 NR 1, INSTALLED Feb 21, 2000 · N506DA · Boeing 727232SDR USAA000304Angle · crackedPIT - FOUND 2 INCH CRACK, AT STATION 1463 RT, VERT FIN DRAG ANGLE. INSTALLED DOUBLER PER SRM 53-05-23A-23. (M)Feb 18, 2000 · N814US · Doug DC981SDR AALA2000410Structure · corrodedTUL - FOUND VERTICAL STAB HINGE PLATE CENTER SECTION, RIGHT INBOARD FACE AND LEFT INBOARD FACE CORRODED. MACHINED AND SPOT FACED RT INBOARD AND LEFT INBOARD SURFACE OF HINGE PLATE CENTER SECTION PER ESO 80559 DATED 2/11/00. LEFT MACHINED TO THICKNESS .631, RFeb 16, 2000 · N476AA · Doug DC982SDR USAA000305Angle · crackedPIT - FOUND 3 INCH CRACK AT STATION 1437 LT VERT FIN ANGLE. INSTALLED DOUBLER PER SRM 53-05 FIG 23B AND 54099 ALSO EA 49714. (M)Feb 16, 2000 · N814US · Doug DC981SDR AALA2000409Structure · corrodedTUL - FOUR HINGE PLATES, FACES AND BORES CORRODED. REFACED INBOARD AND OUTBOARD FACES AND REBORED 1.435 INCH TO REMOVE CORROSION. INSTALLED NEW BUSHINGS AND HONED PER SRM 55-02 PAGE 68. (M)Feb 15, 2000 · N476AA · Doug DC982SDR DL767000308Bolt · damagedWHILE PERFORMING OPN 5940 RC587 FOUND TENSION TIE BOLTS ROTATING AT FS 1702. UPON INSPECTION FOUND BOTH BARREL NUTS L/R AFT POSTION AT FS 1702 HAD FAILED. FOUND TO BE HEAVILY RUSTED. ENGRG ISSUED ERA 373376-14 TO C/W E0 1-74297-12. BOLT AND NUT REPLACEMENTFeb 14, 2000 · N102DA · Boeing 767232SDR 2000UALA00071Fitting · corrodedDURING A HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON THE LUG HOLE OF THE VERTICAL STABILIZER UPPER CLOSURE RIB FITTING (P/N 65-4233-16). THE CORROSION WAS REMOVED BY SPOTFACING AND OVERSIZING OF THE LUG BORE. A BUSHING WAS INSTALLED TO RESTORE THE HOLE TOFeb 11, 2000 · N7467U · Boeing 727222SDR MWEA00058Skin · crackedFOUND CRACK IN AFT LEFT SIDE OF VERTICAL STABILIZER ABOVE TRAILING EDGE OF RUDDER. MAINTENANCE FABRICATED AND INSTALLED SKIN REPAIR DOUBLER.Feb 9, 2000 · N800ME · Doug DC914SDR 2000ZZZX310Frame · misdrilledDOUBLE-DRILLED HOLE TO THE VERTICAL STABILIZER FRAME AT STA YV 247.750, ZV 140.825. REPAIRED DOUBLE-DRILLED HOLE ON VERTICAL STABILIZER FRAME AT STA YV 247.750, ZV 140.825 PER EIA ECRA 941-52-053-2 REV A.Feb 8, 2000 · N941F · Doug DC933FSDR LR7A0012Angle · crackedDURING SCHEDULED C2 INSPECTION PER JOB CARD HSP57110, FOUND FS 902 RT DORSAL FIN EXTERNAL LONGERON CRACKED IN RADIUS ADJACENT TO FASTENER HOLES. REPAIRED PER SRM SMP 583-51-70-1.Feb 6, 2000 · N401LC · Lkheed 382GSDR 0000832293Web · corrodedDURING ''H'' CHECK, FOUND CORROSION ON VERTICAL STABILIZER TENSION TIE WEB, FORWARD HORIZONTAL LUG LOWER SURFACE AROUND FASTENER HOLES. REPAIRED PER EA22-170771.Jan 28, 2000 · N293US · Boeing 727251SDR C2XA00IA024Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER 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 EC5330-01101Jan 27, 2000 · N14952 · Emb EMB145LRSDR DL72L000286Angle · wornSUPPORT ANGLE WORN VERT STAB LT SIDE JUST FWD OF SLIDING SEAL. REMOVED DAMAGED AREA AND DRILLED UP REPAIR PER SRM 55-30-6D. INSTALLED REPAIR PER SRM 55-30-6D.Jan 27, 2000 · N507DA · Boeing 727232SDR CALA0000087Clip · crackedINSPECTION FOUND A 1 INCH CRACK IN CLIP AT VERTICAL STABILIZER LOWER LT AFT CORNER JUST FORWARD OF RUDDER LEADING EDGE. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.Jan 26, 2000 · N14839 · Doug DC982SDR ABXA000088Fairing · corrodedWHILE COMPLYING WITH A C-CHECK INSPECTION, FOUND LOWER RIGHT SIDE HORSE COLLAR CORRODED. REPLACED LOWER RIGHT SIDE HORSE COLLAR IAW DC9 MM 55-10-0 AND DC9 SRM 51-30-1.Jan 26, 2000 · N980AX · Doug DC932SDR C2XA00IA008Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE, IAW CONTINENTLAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, ANDJan 14, 2000 · N13949 · Emb EMB145LRSDR C2XA00IA007Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE 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 EC5330-01101, AND Jan 14, 2000 · N13949 · Emb EMB145LRSDR TWAA0000304Angle · crackedDURING CHECK-C MAINT, FOUND THE RT AFT VERTICAL STABILIZER ATTACH ANGLE CRACKED APPROX .75 INCH IN AT STA 1104. RT VERT STAB ANGLE AT STA 1104 REPAIRED PER SRM 53-05, FIG 23.Jan 5, 2000 · N924L · Doug DC932SDR C2XA00IA002Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE 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 EC5330-01101, AND Jan 5, 2000 · N14947 · Emb EMB145SDR C2XA00IA001Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE 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 EC5330-01101, AND TJan 5, 2000 · N14947 · Emb EMB145SDR USAA010001Skin Tie · crackedVERTICAL STABILIZER SKIN TIE CRACKED AT FASTENER LEFT SIDE AT INTERSECTION OF RIB NR 3 AND STR 8L (JUST ABOVE). FOUND DURING C-CHECK. REPLACED SKIN TIE TO VERTICAL STABILZIER LEFT SIDE AT INTERSECTION OF RIB NR 3 AND STR 8 LEFT. MATERIAL USED, 7075-T6, 0.0Jan 3, 2000 · N925TS · Boeing 727227
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