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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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 INSDR 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 WITHINSDR 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 ELONGASDR 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.SDR 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 INSPECTISDR 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 SN1SDR 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 127112SDR 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 SDR 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. REMOVSDR 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 AFFECTEDSDR 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.SDR 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 FINSDR 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 SDR 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 BSDR 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. SDR AALA2009012200005Lug · corrodedNUMBER 5 VERTICAL STABILIZER PIVOT LUG HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 5 LUG.SDR AALA2009012200004Lug · corrodedNUMBER 6 VERTICAL STABILIZER PIVOT LUG HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 6 LUG.SDR AALA2009012200003Lug · corrodedNUMBER 7 VERTICAL STABILIZER PIVOT LUG HAS PITTING ON FACE. INSTALLED A SERVICEABLE NUMBER 7 LUG.SDR FDEA200811134875Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION. COMPLIED WITH EA 6-5510-125488.SDR FDEA200811134874Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION. COMPLIED WITH EA 6-5510-125488.SDR 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 55-30-0SDR 08FDEA04875Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION.SDR 08FDEA04874Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION.SDR 08FDEA04873Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION.SDR 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 SDR 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.SDR 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.SDR 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.SDR 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.SDR NWAA082669881Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN THE RT DORSAL FIN ATTACH ANGLE AT BS 1266. REPAIRED PER EA 98-213301. (A)SDR MWEA080054Attach Angle · crackedRIGHT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE IS CRACKED IN THE RADIUS BETWEEN CANTED FRAMES 1474 AND 1485. FABRICATED AND INSTALLED DOUBLER.SDR 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 670-55-31-031ASDR TRAX200800328Drag Angle · crackedRT VERTICAL STAB-TO-FUSELAGE DRAG ANGLE CRACKED AT AFT END.SDR SWAA080252Attach Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER PRIMARY FITTING ATTACH LUGS CORRODED. REPAIRED FITTING PER SWA EA.SDR SWAA076312Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND LT VERTICAL STABILIZER LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.SDR SWAA076313Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.SDR SWAA075860Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT VERTICAL STABILIZER FITTING LUG FACES CORRODED. REPAIRED FITTING PER ER.SDR SWAA075692Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT VERTICAL STABILIZER FITTING BODY FRONT SPAR CLEVIS AFT LUG FACE CORRODED. REMOVED AND REPLACED FITTING PER SRM.SDR SWAA075279Fitting · corrodedDURING SCHEDULED 18Y CHECK, FOUND VERTICAL STABILIZER FITTING FWD AND AFT LUG FACES CORRODED. REPAIRED FITTING PER EA.SDR SWAA075082Rod End · brokenDURING SCHEDULED 14Y CHECK, FOUND VERTICAL STABILIZER STANDBY ACTUATOR, INPUT ROD END BROKEN. REMOVED AND REPLACED ROD END PER MM.SDR 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.SDR SWAA074894Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND VERTICAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.SDR SWAA074831Fitting · corrodedDURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER FWD ATTACH FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.SDR 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.SDR ABXA070310Attach Angle · crackedVERTICAL STABILIZER RIGHT ATTACH ANGLE COMMON TO FUSELAGE CRACKED - AFT. REPAIRED RIGHT VERTICAL STABILIZER ATTACH ANGLE IAW DC9 SRM 53-05.SDR N93A28082007Attach Fitting · corrodedDURING 5000 LANDING INSPECTION FOUND 714 BULKHEAD VERTICAL STAB ATTACH FITTINGS CORRODED.SDR 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.SDR 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.SDR 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.
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