JASC 5553

Service difficulty reports · 586

Reports filed under 5553 · Vertical Stabilizer, Attach Fittings, 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 = '5553'
  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 USAA2009091592539Lug · corrodedSAL - Q6 - MAJOR REPAIR - CORROSION ON AFT LUG OF VERTICAL STABILIZER FIN ATTACH FITTING. REPAIRED AFT LUG OF VERTICAL STABILIZER FIN ATTACH FITTING IAW US AIRWAYS EA 132580.Jul 26, 2009 · N454UW · Boeing 7374B7SDR FDEA200907132599Fitting · crackedDURING OPEN HOLE INSP ON RT SIDE BANJO FITTING FASTENER HOLE COMMON TO REPAIR DOUBLER, CRACKED FOUND ON AFT FLANGE LOWEST FASTENER HOLE BANJO FITTING LAYER AT 3 AND 6 O'CLOCK POSITION. REPAIR CARRIED OUT IAW EA 1-5530-132118. REPAIR CATEGORY B, ACCOMPLISH INJul 13, 2009 · N617FE · Doug MD11FSDR FDEA200907132598Fitting · crackedDURING OPEN HOLE INSP CRACKED FOUND ON LT SIDE BANJO FITTING SECOND FASTENER HOLE COMMON TO BANJO FITTING AND CARRY THROUGH STRUCTURE AFT ROW ON BANJO FITTING LAYER. REPAIR CARRIED OUT IAW EA 1-5530-132118. REPAIR CATEGORY B, ACCOMPLISH INITIAL INSP WITHINJul 13, 2009 · N617FE · Doug MD11FSDR 2009FA0000721Attach Fitting · damagedCOMPIED WITH AD72-07-09 DATED 10/17/74 BY INSP AND FOUND SIGNS OF WORKING AT LEFT SIDE AND RIGHT SIDE AFT VERTICAL FIN ATTACHMENT BOLTS. PERFORMED DYE PENETRANT INSP IAW PARA C,1, D, 1 AND 2 WITH NO CRACKS FOUND. CHECKED ATTACHMENT HOLES FOR EXCESSIVE ELONGAJul 10, 2009 · N42154 · Cessna 182LSDR C2XA09SH190Attach Fitting · looseSHV - DURING C-CHECK VERTICAL STABILIZER ATTACHMENT AT FR 75 HAS WORKING HARDWARE AND FASTENERS. MAINTENANCE REMOVED AND INSTALLED NEW VERTICAL STABILIZER ATTACHMENT AT FR 75 IAW EC5310-01317A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jul 5, 2009 · N13958 · Emb EMB145LRSDR FDEA200906302401Fitting · crackedCRACKED INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON FIRST LAYER (SKIN) AT RT SIDE BANJO FITTING, AFT ROW LOWEST NR 4 FASTENER HOLE. REPAIR CARRIED OUT AS PER EA 1-5530-132118, REPAIR CATEGORY B, ACCOMPLISH INITIAL INSPECTIJun 30, 2009 · N617FE · Doug MD11FSDR FDEA200906302400Fitting · crackedVERTICAL STABILIZER LT NR 4 FWD BANJO FITTING FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-20-00 FIGURE 3 VOLUME I, REVISION 40. REPAIR CATEGORY B, DAMAGE TOLERANCE INSPECTION REQUIREMENT INITIAL 5400 CYCLE, REPETITIVE 2700 CYCLE AS PER DRAWING NR SN1Jun 30, 2009 · N617FE · Doug MD11FSDR DL757091174Flange · gougedBOTTOM OF LT VERTICAL BODY TO FIN FLANGE IS GOUGED WHERE ACCESS PANEL 322AL SEATS / COMPLIED WITH ER/A 475625-14 REV ORIG DATED 07/08/09 AT SAA SAT ON N/R CARD 127112Jun 4, 2009 · N615DL · Boeing 757232SDR QXEA2009050700315Angle · damagedLEFT SIDE CONNECTING ANGLE FOR THE VERTICAL STAB TO THE FUSELAGE IS POSSIBLY CRACKED APPROX 1 INCH AT VERTICAL STAB STRINGER DATUM 67.5 PERCENT. HFEC INSPECTED SUSPECTED CRACK IAW NDTM 51-20-006. CONFIRMED CONNECTING ANGLE IS CRACKED. DRILLED OUT FASTENERS May 6, 2009 · N600QX · Cndair CL6002C10SDR QXEA2009042000276Angle · crackedTHE AFT CONNECTING ANGLE ON THE LT SIDE FOR THE VERT STAB TO THE FUSELAGE IS CRACKED AT THE FWD END APPROX. .75 INCH AT VERTICAL STAB STRINGER DATUM 67.5 PERCENT. HFEC IAW NDTM PART 1, 51-20-006 CONFIRMED AND MARKED CRACK. MAPPED AREA FOR ENGINEERING. REMOVApr 19, 2009 · N601QX · Cndair CL6002C10SDR QXEA2009042000275Angle · crackedTHE LT SIDE CONNECTING ANGLE FOR THE VERTICAL STAB TO THE FUSELAGE IS CRACKED APPROX 1 FT AT VERTICAL STAB STRINGER DATUM 67.5 PERCENT. HFEC IAW NDTM PART 1 51-20-006. CONFIRMED AND MARKED CRACK. MAPPED AREA FOR ENGINEERING. REMOVED FASTENERS FROM AFFECTEDApr 19, 2009 · N601QX · Cndair CL6002C10SDR DLM88090651Attach Angle · crackedVERTICAL STAB INTERNAL ATTACH ANGLE CRACKED AT FASTENER HOLE FWD END OF RAM AIR SCOOP. REPLACED INTERNAL ATTACH ANGLE PER 51-30-02.Apr 5, 2009 · N966DL · Doug MD88SDR RMXA029H325622609Fitting · corrodedUPON REMOVAL OF THE AIRFRAME VERTICAL FIN ASSY, THE UPPER VERTICAL FIN FWD ATTACH STEEL FITTING SEPARATED FROM THE UPPER VERTICAL FIN. INSP REVEALED THAT ALL RIVETS ATTACHING THE FITTING TO THE FIN WERE CORRODED BEYOND RETENTION. ALSO FOUND THE SHIN OF THE FINFeb 26, 2009 · N5230J · Snias AS350B3SDR CA090212001Spar · failedON TAXI OUT, R RUDDER TEST FAILED. RUDDER PEDAL APPEARS TO BIND. UNABLE TO ACHIEVE MORE THAN HALF DEFLECTION. INITIAL INSPECTION FOUND CTR PCA (LT HYD SYS) FULLY RETRACTED IN THE LT RUDDER DEFLECTION POSITION, WITH ONLY LT HYD SYS PRESSURIZED, RUDDER APPROX Feb 11, 2009 · Boeing 767333SDR 2009FA0000067Attach Fitting · looseUPON REMOVAL OF VERTICAL FIN FROM HORIZONTAL STABILIZER FOR ROUTINE MX, THE VERTICAL FIN ATTACH BRACKET IN THE STABILIZER WAS FOUND LOOSE AND HAD ELONGATED MOST ALL OF THE MOUNTING HOLES IN THE STABILIZER SPAR. WITH THE TAIL FULLY ASSEMBLED, NO LOOSENESS HAD BFeb 5, 2009 · N660K · Ayres S2RT660SDR ASOA200900088Drag Angle · crackedRT DRAG ANGLE (VERTICAL - FUSELAGE) APPEARS CRACKED. PERFORMED REPAIR TO CRACKED LT DRAG ANGLE (VERTICAL FUSELAGE) AS PER REO 670-55-31-018 STEPS 1-5. PERFORMED EDDY CURRENT INSPECTION DRAG ANGLE IAW NDTM 51-20-006. ANGLE IS CONFIRMED CRACKED AND MARKED. Jan 19, 2009 · N717EV · Cndair CL6002C10SDR AALA2009012200005Lug · corrodedNUMBER 5 VERTICAL STABILIZER PIVOT LUG HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 5 LUG.Jan 7, 2009 · N434AA · Doug DC983SDR AALA2009012200004Lug · corrodedNUMBER 6 VERTICAL STABILIZER PIVOT LUG HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 6 LUG.Jan 7, 2009 · N434AA · Doug DC983SDR AALA2009012200003Lug · corrodedNUMBER 7 VERTICAL STABILIZER PIVOT LUG HAS PITTING ON FACE. INSTALLED A SERVICEABLE NUMBER 7 LUG.Jan 7, 2009 · N434AA · Doug DC983SDR FDEA200811134875Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION. COMPLIED WITH EA 6-5510-125488.Nov 13, 2008 · N453FE · Airbus A310222SDR FDEA200811134874Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION. COMPLIED WITH EA 6-5510-125488.Nov 13, 2008 · N453FE · Airbus A310222SDR FDEA200811134873Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. FREE OF CRACK AT THE REWORKED AREA. REMAINING THICKNESS IS 0.481 INCH, IT IS WITHIN LIMIT PER SRM 55-30-0Nov 13, 2008 · N453FE · Airbus A310222SDR 08FDEA04875Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION.Nov 13, 2008 · N453FE · Airbus A310222SDR 08FDEA04874Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION.Nov 13, 2008 · N453FE · Airbus A310222SDR 08FDEA04873Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION.Nov 13, 2008 · N453FE · Airbus A310222SDR CA081002007Fitting · fractured(CAN) ACFT BROUGHT TO MX DUE TO ACFT NOT RESPONDING CORRECTLY, VERTICAL STABILATOR WAS INSPECTED AND A FRACTURE WAS FOUND IN THE BRACKET. IT APPEARED TO BE A STRESS FRACTURE IN THE FITTING. WE WOULD LIKE ALL CESSNA OWNERS TO UNDERSTAND THAT IF THE TAIL HITS Sep 24, 2008 · Cessna 152SDR 08FDEA03853Attach Fitting · corrodedVERT STAB ATTACH FITTING CORROSION L AND R SIDE. COMPLIED WITH EA 6-5536-110931 RII:680053. COMPLIED WITH EA 6-5536-110931.Sep 12, 2008 · N426FE · Airbus A310203SDR CALA0800660Fitting · corrodedAFT RIGHT OUTBOARD VERTICAL STABILIZER FORWARD FAIL-SAFE LUG INSIDE DIAMETER HAS CORROSION. OVERSIZED BORE TO REMOVE ALL CORROSION DAMAGE, INSPECTED REWORKED AREA, INSTALLED REPAIR BUSHING AND REINSTALLED DRAG ANGLE PER ECRA 5342-01054.Jul 1, 2008 · N16646 · Boeing 737524SDR CALA0800659Lug · gougedAFT RIGHT-HAND OUTBOARD VERTICAL STABILIZER FORWARD FUSELAGE FITTING BUSHING IS GOUGED. REMOVED BUSHING, REWORKED LUG AND INSTALLED OVERSIZED REPAIR BUSHING PER ECRA 5342-01053.Jul 1, 2008 · N16646 · Boeing 737524SDR CALA0800658Fitting · corrodedAFT LEFT-HAND OUTBOARD VERTICAL STABILIZER FORWARD FAIL-SAFE LUG INSIDE DIAMETER HAS CORROSION. OVERSIZED BORE TO REMOVE ALL CORROSION DAMAGE, INSPECTED REWORKED AREA, INSTALLED REPAIR BUSHING AND REINSTALLED DRAG ANGLE PER ECRA 5342-01054.Jul 1, 2008 · N16646 · Boeing 737524SDR NWAA082669881Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN THE RT DORSAL FIN ATTACH ANGLE AT BS 1266. REPAIRED PER EA 98-213301. (A)Jun 6, 2008 · N676MC · Doug DC951SDR MWEA080054Attach Angle · crackedRIGHT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE IS CRACKED IN THE RADIUS BETWEEN CANTED FRAMES 1474 AND 1485. FABRICATED AND INSTALLED DOUBLER.Apr 12, 2008 · N823ME · Doug MD88SDR TRAX200800333Drag Angle · crackedLHS VERTICAL STAB-TO-FUSELAGE DRAG ANGLE CRACKED AT AFT END. REPAIRS PERFORMED IAW REO 670-55-31-018, REO 670-55-31-031, AND REO 670-55-31-031AFeb 26, 2008 · N354CA · Cndair CL6002C10SDR TRAX200800328Drag Angle · crackedRT VERTICAL STAB-TO-FUSELAGE DRAG ANGLE CRACKED AT AFT END.Feb 26, 2008 · N354CA · Cndair CL6002C10SDR SWAA080252Attach Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER PRIMARY FITTING ATTACH LUGS CORRODED. REPAIRED FITTING PER SWA EA.Jan 10, 2008 · N691WN · Boeing 7373G7SDR SWAA076312Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND LT VERTICAL STABILIZER LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.Dec 17, 2007 · N691WN · Boeing 7373G7SDR SWAA076313Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.Dec 17, 2007 · N691WN · Boeing 7373G7SDR SWAA075860Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT VERTICAL STABILIZER FITTING LUG FACES CORRODED. REPAIRED FITTING PER ER.Nov 26, 2007 · N669SW · Boeing 7373A4SDR SWAA075692Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT VERTICAL STABILIZER FITTING BODY FRONT SPAR CLEVIS AFT LUG FACE CORRODED. REMOVED AND REPLACED FITTING PER SRM.Nov 13, 2007 · N669SW · Boeing 7373A4SDR SWAA075279Fitting · corrodedDURING SCHEDULED 18Y CHECK, FOUND VERTICAL STABILIZER FITTING FWD AND AFT LUG FACES CORRODED. REPAIRED FITTING PER EA.Oct 24, 2007 · N501SW · Boeing 7375H4SDR SWAA075082Rod End · brokenDURING SCHEDULED 14Y CHECK, FOUND VERTICAL STABILIZER STANDBY ACTUATOR, INPUT ROD END BROKEN. REMOVED AND REPLACED ROD END PER MM.Oct 15, 2007 · N371SW · Boeing 7373H4SDR ASAA0782082Attach Angle · crackedRIGHTHAND SIDE OF VERTICAL STABILIZER EXTERNAL VERTICAL TO FUSELAGE JOIN STRAP (ATTACH ANGLE) IS CRACKED. REPLACED DAMAGED SECTION OF JOIN STRAP PER SRM 53-05.Oct 5, 2007 · N958AS · Doug DC983SDR SWAA074894Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND VERTICAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.Oct 1, 2007 · N329SW · Boeing 7373H4SDR SWAA074831Fitting · corrodedDURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER FWD ATTACH FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.Sep 26, 2007 · N656SW · Boeing 7373H4SDR 07FDEA04118Attach Fitting · gougedDEEP GOUGE ON LT MIDDLE VERTICAL STABILIZER TO FUSELAGE ATTACH FITTING, OUTBOARD SIDE AFT AREA. REPAIR PERFORMED BY SMOOTH BLEND OUT AND NDT INSPECTION FOR CRACK FREE CONDITION IAW EA 6-5319-82881 AND RAS/DAHAM/4019574/2005 ISSUE A.Sep 20, 2007 · N803FD · Airbus A310324SDR ABXA070310Attach Angle · crackedVERTICAL STABILIZER RIGHT ATTACH ANGLE COMMON TO FUSELAGE CRACKED - AFT. REPAIRED RIGHT VERTICAL STABILIZER ATTACH ANGLE IAW DC9 SRM 53-05.Sep 2, 2007 · N930AX · Doug DC933FSDR N93A28082007Attach Fitting · corrodedDURING 5000 LANDING INSPECTION FOUND 714 BULKHEAD VERTICAL STAB ATTACH FITTINGS CORRODED.Aug 28, 2007 · N495QS · Gulstm GIVSDR USAA070633Lug · corrodedPITTED & CORRODED VERT FWD FACE OF L4 LUG ON FUSELAGE. REMOVED BUSHING & BLENDED LUG TO REMOVE CORROSION, TREATED & REPLACED PER EA 98800; CORR TASK C55-70, DEFECT SIZE: .25 INCH.Aug 8, 2007 · N425US · Boeing 737401SDR USAA070632Lug · corrodedAFT FACE OF L6 LUG ON FUSELAGE VERT STAB LUG CORRODED. REMOVED LUG BUSHING, CORROSION, TREATED & REPLACED PER EA 98800; CORR TASK C55-706-11, DEFECT SIZE: .25 INCH.Aug 8, 2007 · N425US · Boeing 737401SDR USAA070631Lug · corrodedPITTING ON FWD FACE OF L6 LUG ON FUSELAGE CORRODED. REMOVED BUSHING, CLEANED CORROSION & RE-INSTALLED PER EA 98800; CORR TSK C55-706-11, DEFECT SIZE: .25 INCH.Aug 8, 2007 · N425US · Boeing 737401
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