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 IPXA2016081106917Bracket · crackedVERTICAL RT FILLET PANEL 323AR MOUNT BRACKET 5TH AFT IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-21, AND DWG 19F53570111 ISSUE F.Aug 9, 2016 · N135UP · Airbus A300F4622RSDR DALA2016071405395Support · wornVERTICAL STABILIZER REAR SPAR, UPPER RUDDER HINGE BEARING SUPPORT HAS RADIAL PLAY AT BOTH ATTACH BOLTS. REMOVED AND REPLACED HINGE BEARING SUPPORT IAW DWG 5930608, REV AJ.Jul 12, 2016 · N921DN · Doug MD9030SDR DALA2016071205274Web · crackedVERTICAL STABILIZER HAS A CRACK AT SUPPORT WEB FLANGE AT JACKSCREW GIMBAL NUT, RIGHT ATTACH FITTING. COMPLIED WITH PRI 548544-14, REV 0, 1, 2 AND ERA 548544-14, REV O.Jul 11, 2016 · N915DN · Doug MD9030SDR DALA2016071205273Web · crackedVERTICAL STABILIZER HAS A CRACK AT SUPPORT WEB FLANGE AT JACKSCREW GIMBAL NUT , LEFT ATTACH FITTING. COMPLIED WITH PRI/ERA 548544-14, REV O.Jul 11, 2016 · N915DN · Doug MD9030SDR DALA2017021401204Structure · damagedFASTENERS OF STA 52-267. MEASURED HOLE DIAMETERS OUT OF LIMITS. COMPLIED WITH ERA 5548121-14AD.Jul 8, 2016 · N925DN · Doug MD9030SDR DALA2016070705235Unknown · out of limitsITEM FOUND OUT OF LIMITS. REPAIRED IAW DWG SG09550004.Jul 6, 2016 · N925DN · Doug MD9030SDR GR4D20160718003Fitting · corrodedRIGHT VERTICAL STABILIZER FITTING FOR HORIZONTAL STABILIZER ATTACHMENT BLEEDING RUST FROM PIVOT BORE.Jun 15, 2016 · N401QS · Gulstm GIVSDR GR4D20160718002Fitting · corrodedLEFT VERTICAL STABILIZER FITTING FOR HORIZONTAL STABILIZER ATTACHMENT BLEEDING RUST FROM PIVOT BEARING BORE.Jun 15, 2016 · N401QS · Gulstm GIVSDR DALA2016061404593Structure · crackedCRACK ON LT SIDE OF VERITCAL STABILIZER AT MATING SURFACE OF EMPENNAGE AT BS 116. REPAIRED CRACK ON LT SIDE OF VERTICAL STABILIZER AT MATING SURFACE OF EMPENNAGE BS 1116 IAW SRM 55-30-01, FIG 201, REPAIR 5.Jun 9, 2016 · N966AT · Boeing 717200SDR WVER2016061450502Drag Angle · crackedPOSSIBLE CRACK ON VERTICAL TAIL, LT SIDE, FWD DRAG ANGLE. APPROXIMATELY 1.250 IN LENGTH.Jun 2, 2016 · N505MJ · Cndair CL6002B16SDR SWAA2016062053005Angle · crackedLEFT VERTICAL STABILIZER FIN CLOSURE ANGLE CRACKED BETWEEN BS 1100 TO BS 1129. R & R ANGLE IAW SRM & DWG.Jun 1, 2016 · N640SW · Boeing 7373H4SDR SWAA2016062053004Beam · crackedLEFT T/E BEAM ON VERTICAL STABILIZER CRACKED BETWEEN STA 13 TO STA 32. R & R STABILIZER IAW SRM AND DWG.May 30, 2016 · N640SW · Boeing 7373H4SDR DALA2016051503981Attach Angle · crackedCRACK ON RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE AT DORSAL FIN AREA. REPLACED SAME IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.May 14, 2016 · N923DN · Doug MD9030SDR IPXA2016051103217Fitting · crackedINSPECTION TYPE:2, CONE CRACK IN VERT STABILIZER AFT SPAR NR 4 BANJO FITTING RT SIDE AT LOWER FWD FASTENER HOLE REPAIRED CRACK IAW EO MD11-5530-46641-A.Apr 23, 2016 · N276UP · Doug MD11FSDR IPXA2016051103214Fitting · damagedINSPECTION TYPE:2C, 2 CRACKS IN VERTICAL STABILIZER AFT SPAR NR 4 BANJO FITTING LT SIDE AT LOWER AFT FASTENER HOLE. REPAIRED CRACKS IAW EO MD11-5530-46641-A.Apr 23, 2016 · N276UP · Doug MD11FSDR REXA2016042300642Fitting · wornVERTICAL STAB TO RUDDER, CTR LOWER BEARING FITTING FAILED PRE LOAD CHECK OF NEW BEARING. R & R VERTICAL STAB TO RUDDER CTR BEARING FITTING IAW RIL 0602 REV H.Apr 23, 2016 · N8883E · Cndair CL6002B19SDR KO0R201604210052Inlet · crackedVERTICAL INLET DUCT PLATING CUTOUT IS CRACKED AT YID 279.443, ZID -44.00, XID0.00 TO 9.5, POSITION 6 O'CLOCK.Apr 21, 2016 · N542KD · Doug MD11FSDR DALA2016042103126Nut Plate · wornVERTICAL STABILIZER MID SPAN PANEL HORSE COLLAR NUTPLATES WORN. REPAIRED OVERSIZE FASTENER HOLE IAW PRI 545887-14, REV 0, ER/A 545887-14, REV. O AND REPLACED NUTPLATES IAW SRM 51-41-01. REF LOG NR 2453267 FOR CORRECT MAJOR REPAIR ANNOTATION.Apr 21, 2016 · N921AT · Boeing 717200SDR DALA2016042003043Structure · damagedVERTICAL STABILIZER MID SPAN PANEL FRAME LOWER FASTENER HOLES ELONGATED. REPAIRED IAW REPAIR DWG SG95550001 AND SRM 55-30-01, REPAIR 7.Apr 19, 2016 · N921AT · Boeing 717200SDR DALA2016042703361Panel · crackedON B-CHECK FOUND 12" CRACK IN PANEL 3703A. C/W SECTION I TIME LIMITED REPAIR IAW ERA 545854-14.Apr 11, 2016 · N981DL · Doug MD88SDR AALA201604129023Hinge Fitting · excess playAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 5 RUDDER HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 28, 2016 · N651AW · Airbus A320232SDR AALA201604129021Hinge Fitting · excess playAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 2 RUDDER HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 28, 2016 · N651AW · Airbus A320232SDR ASOA2016032414644Bracket · damagedLIGHTNING STRIKE DAMAGE TO VERTICAL STABILIZER AFT FRAME CONDUIT BRACKET. BLENDED OUT LIGHTNING STRIKE DAMAGE ON AFT FRAME CONDUIT BRACKET IAW SRM 51-12-00. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREA ON AFT FRAME CONDUIT BRACKET IAW NDTM 51-20-006, PARMar 24, 2016 · N608QX · Cndair CL6002C10SDR ASOA2016032414643Support · damagedLIGHTNING STRIKE DAMAGE TO END FRAME SUPPORT FOR VERTICAL AFT FAIRING ATTACHMENT. BLENDED OUT LIGHTNING STRIKE DAMAGE ON BULLET FAIRING AFT FRAME IAW SRM 51-12-00. PERFORMED ULTRASONIC THICKNESS CHECK OF BLENDED AREA INSIDE THE FLANGE COMMON TO REWORKED AREA Mar 24, 2016 · N608QX · Cndair CL6002C10SDR DALA2016032202267Structure · damagedVERTICAL STABILIZER L/E HAS MANY WORN FASTENER HOLES ALONG UPPER EDGE AND MANY OTHERS ON AFT EDGE UPPER END SHOW SIGNS OF LOOSENESS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0220:0593-2005/011 00068, REPAIRED Mar 21, 2016 · N925AT · Boeing 717200SDR AALA201604129024Hinge Fitting · wornAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 7 RUDDER HINGE ARM FITTING BEARING WORN. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 17, 2016 · N651AW · Airbus A320232SDR AALA201604129022Hinge Fitting · excess playAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 3 RUDDER HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 17, 2016 · N651AW · Airbus A320232SDR AALA201604129020Hinge Fitting · excess playAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 1 RUDDER HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 17, 2016 · N651AW · Airbus A320232SDR WVER2016031650602Drag Angle · crackedLEFT FORWARD VERTICAL STABILIZER DRAG ANGLE, IS CRACKED IN RADIUS. REPAIRED IAW REO 670-55-31-018.Mar 16, 2016 · N506MJ · Cndair CL6002C10SDR DALA2016031601961Skate Angle · crackedLT SIDE VERTICAL STABILIZER INNER SKATE ANGLE ATTACH ANGLE CRACKED. REPLACED ANGLE REF DWG NR 5912188 AND SRM 51-40-02.Mar 15, 2016 · N925AT · Boeing 717200SDR REXA2016031400429Hinge Fitting · failedVERTICAL STAB TO RUDDER CTR LOWER BEARING FITTING FAILED PRE LOAD CHECK OF NEW BEARING. REMOVED CTR LOWER HINGE FITTING & INSTALLED NEW FITTING IAW RIL 0602 REV H.Mar 14, 2016 · N8896A · Cndair CL6002B19SDR WVER2016031100010Drag Angle · crackedLEFT VERTICAL STABILIZER FWD ATTACHMENT DRAG ANGLE IS CRACKED.Mar 11, 2016 · N911FJ · Cndair CL6002D24SDR WVER2016031100009Drag Angle · crackedLEFT AFT VERTICAL STABILIZER ATTACHMENT DRAG ANGLE IS CRACKED.Mar 11, 2016 · N911FJ · Cndair CL6002D24SDR WVER2016030400004Drag Angle · crackedRIGHT UPPER TAILCONE, AFT ATTACHMENT DRAG ANGLE IS CRACKED.Mar 4, 2016 · N911FJ · Cndair CL6002D24SDR WVER2016030491103Drag Angle · crackedRIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE IS CRACKED.Mar 4, 2016 · N911FJ · Cndair CL6002D24SDR DALA2016030601680Structure · crackedCRACK ON PREVIOUS REPAIR FWD UPPER CORNER ON ACCESS NR 6301A AT VERTICAL STABILIZER. REPAIR WAS ACCOMPLISHED IAW ETI-88-16-089 R1 & ER/A 543178-14 REV ORIGINAL.Mar 3, 2016 · N991DL · Doug MD88SDR SIMA20160302002Hinge Fitting · wornRUDDER 2, UPPER CTR, & NR 3, LOWER CENTER, HINGE FITTING BEARINGS ON VERTICAL STABILIZER HAS PLAY. R & R RUDDER NR 3, LOWER CTR, HINGE FITTING ON VERTICAL STAB IAW ETN CR-55-026 & NR 2, UPPER CTR, NR 2 RUDDER, PN AV670-21081-015.Mar 2, 2016 · N516AE · Cndair CL6002C10SDR DALA2016030101593Structure · crackedVERTICAL STABILIZER L/E FORWARD TIP HAS CRACK THRU FASTENER HOLE APPROXIMATELY, BS 1460. REPAIRED IAW SRM 55-30-05, FIG 19.Feb 28, 2016 · N911DA · Doug MD9030SDR REXA2016022600309Panel · damagedPANEL 326BL FOUND TO BE SPLIT ON UPPER RT CORNER OF PANEL. REPAIRED PANEL 326BL IAW REO 601R-55-32-233 REV A DATED 05 05 09 & SRM 51-25-01. REINSTALLED PANEL 326BL IAW AMM 55-32-05-400-805.Feb 26, 2016 · N8886A · Cndair CL6002B19SDR DALA2016022401368Scoop · crackedCRACK ON VERTICAL STABILIZER RAM AIR SCOOP LT EDGE. CRACK ON VERTICAL STABILIZER RAM AIR SCOPE LT EDGE WAS REPAIRED, WELDED IAW ER/A 420329-14MA, REV C. THE RIVETS ON NEW FILLER WILL BE INSTALL WHIT NR 20000099368, CARD 3, ZONE 63.Feb 23, 2016 · N991DL · Doug MD88SDR IPXA2016031700864Panel · delaminatedINSPECTION TYPE:C, RT VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL IS DELAMINATED. R & R PANEL IAW SRM 51-40-02-0G AND DWG 175N2001 SHEET.Feb 22, 2016 · N452UP · Boeing 75724APFSDR DALA2016022101382Structure · unknownRT VERTICAL STABILIZER DIRTY HOLE INDICATION. REMOVED VERTICAL STABILIZER L/E AND REPAIRED BOTH LT AND RT STABILIZER SPAR CAP AND L/E SKIN AW SG0955005 AND ERA 543991-14AD.Feb 21, 2016 · N964DN · Doug MD9030SDR UG8A2016030401Attach Fitting · wornTHE LT RUDDER ATTACH POINT NR 3, LOWER BORE ON THE VERTICAL STABILIZER IS WORN BEYOND NOMINAL SIZE. OVERSIZED HOLE OF LT LOWER RUDDER FITTING OF VERTICAL STABILIZER TO FIRST OVERSIZE 0.3125", IAW DWG SE05000102 REV. INITIAL DATED 8 11 2015 WITH FAA APPROVAL Feb 11, 2016 · N473CW · Gulstm GIVSDR WVER0131201600001Drag Angle · crackedLEFT FWD VERTICAL STABILIZER DRAG ANGLE IS CRACKED APPROXIMATELY TWO INCHES.Jan 31, 2016 · N241LR · Cndair CL6002D24SDR DALA2016013100766Former · crackedCRACKED FORMERS ON BS ZFS=23 LT SIDE AND BS ZFS=23 AND 36 AT VERTICAL STABILIZER L/E INTERNAL STRUCTURE. CRACKED FORMERS WERE REPAIRED IAW SRM 55-02D, FIG 27.Jan 30, 2016 · N990DL · Doug MD88SDR DALA2016012900711Angle · crackedCRACKED INNER ANGLE ON DORSAL FIN, REF BS 1427 BETWEEN LONGERONS 1 AND 2 RT. ANGLES WERE REPLACED IAW DWG 5912188 AND SRM 51-30-5.Jan 27, 2016 · N933DL · Doug MD88SDR AALA201602099013Hinge Fitting · excess playAIRCRAFT WAS IN BASE MX. VERTICAL STABILIZER FITTING FOR RUDDER HINGE NR 1 HAS EXCESSIVE PLAY. R & R FITTING SRM 51-72-11 & AMM 55-36-41-400-001-A.Jan 25, 2016 · N676AW · Airbus A320232SDR AALA201602099014Hinge Fitting · excess playAIRCRAFT WAS IN BASE MX. VERTICAL STABILIZER FITTING FOR RUDDER HINGE NR 4, HAS EXCESSIVE PLAY. R & R FITTING IAW SRM 51-72-11 & AMM 55-36-41-400-001-A.Jan 24, 2016 · N676AW · Airbus A320232SDR DALA2016012600645Bushing · scoredVERTICAL STABILIZER GIMBAL PIN BUSHINGS SCORED. REMOVED, CLEANED BORES AND REINSTALLED BUSHINGS IAW B-50PM 20-10-7.Jan 22, 2016 · N939DN · Doug MD9030SDR DALA2015122407711Scoop · crackedVERTICAL STABILIZER L/E, INLET SCOOP CRACKED TOP CENTER, NEXT TO WELD. WELDED IAW SRM 55-05.Dec 23, 2015 · N902DE · Doug MD88
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