JASC 5500
Service difficulty reports · 490
Reports filed under 5500 · Empennage Structure, 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 = '5500' 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 = '5500' 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 DALA2023041202858Unknown · unknownAIRCRAFT 3501, AD/ EM-EO TASK- RH HORIZONTAL STABILIZER LLF LOWER BUSHING PUSHED BACK TO ITS ORIGINAL POSITION. CORRECTIVE ACTION: REPAIR CARRIED OUT AT A350 THS RHS FITTING AS PER PRI ER/A 607336-14 REV 0 DATED: 24 MAR 2023. AWAITING FOR FINAL ER/A . PRI ER/ASDR DALA2023041202857Unknown · unknownAIRCRAFT 3501, AD/ EM-EO TASK- RH HORIZONTAL STABILIZER UPPER BUSHING MIGRATION WAS NOT FOUND TO BE UNIFORM (AA 5510-01108). CORRECTIVE ACTION: REPAIR CARRIED OUT AT A350 THS RHS FITTING AS PER PRI ER/A 607336-14 REV 0 DATED: 24 MAR 2023. AWAITING FOR FINAL ERSDR DALA2023041202856Unknown · unknownAIRCRAFT 3501, AD/ EM-EO TASK- RH LLF UPPER BORE HOLE TO CARRY OUT NEXT OVERSIZE HOLE. CORRECTIVE ACTION: REPAIR CARRIED OUT AT A350 THS RHS FITTING AS PER PRI ER/A 607336-14 REV 0 DATED: 24 MAR 2023. AWAITING FOR FINAL ER/A . PRI ER/A 607336-14 REV 0 DATED: 2SDR DALA2023041202855Unknown · unknownAIRCRAFT 3501, AD/EM-EO TASK - PER WORKCARD 5510-01108-02B FABRICATION OF REPAIR BUSHING REQUIRE ALTERNATIVE MATERIAL AND ALTERNATIVE PROTECTION PROCESS. CORRECTIVE ACTION: REPAIR CARRIED OUT AT A350 THS RHS FITTING AS PER PRI ER/A 607336-14 REV 0 DATED: 24 MASDR DALA2023041202854Unknown · unknownAIRCRAFT 3501, AD/ EM-EO TASK- LH LLF UPPER BORE HOLE TO CARRY OUT NEXT OVERSIZE HOLE. CORRECTIVE ACTION: REPAIR CARRIED OUT AT A350 THS LHS FITTING AS PER PRI ER/A 607336-14 REV 0 DATED: 24 MAR 2023. WAITING FOR FINAL ER/A. PRI ER/A 607336-14 REV 0 DATED: 24 SDR CALA2023040301012Skin · crackedR/H HORIZONTAL STAB LOWER SKIN HAS A 0.750 CRACK LOCAQTED AT ATAB STA 129.50 I/B RIVET ROW 19.00 FROM FRUNT SPAR REF NDTM UAL PART 6 SECTION 55-10-01 REF AAR N/R 974677 REMOVED EXISTING REPAIR BETWEEN STAB STA 138.7 AND 147.9 COTOUT DAMAGED AREA STA 129.5 19INSDR CALA2023040300972Skin · crackedR/H HORIZONTAL STAB LOWER SKIN HAS A 0.750 CRACK LOCAQTED AT ATAB STA 129.50 I/B RIVET ROW 19.00 FROM FRUNT SPAR REF NDTM UAL PART 6 SECTION 55-10-01 REF AAR N/R 974677 THRESHOLDS 56,000 TFC AND REPEAT INSP AT 9,000 F.C INTERVALS PER TABLE 204 WORK ACCOMPLISHESDR AALA202304249920Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER FORWARD SPAR LEFT HAND BULKHEAD FITTING LOCATED AT BS 1016 AND LBL 11.55. REPAIRED PER SOPM 20-43-03, SOPM 20-41-02, AND EA 343695.SDR UIEA2023031400252Unknown · unknownR/H H.STAB (STAB BL 421.5) WEB CRACKED.(<P>R/H H.STAB (STAB BL 421.5) WEB CRACK AREA REPAIRED IAW SRM 55-10-09-2R-12 REPAIR 12.</P>)SDR UIEA2023031400253Unknown · unknownR/H H.STAB (STAB BL 421.5) LWR CHORD CRACKED.(<P>R/H H.STAB (STAB BL 421.5) LOWER CHORD CRACK AREA REPAIRED IAW SRM 55-10-09-2R-12 REPAIR 12.</P>)SDR UIEA2023032000276Stabilizer · unknownEMP RH H STAB STA 560 REAR SPAR STIFFENER CRACK(<P>RH HORIZONTAL STABILIZER REAR SPAR ATT ANGLE REPLACE IAW RI 55-00-16124 REV A</P>)SDR AALA202304248774Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER FIN FORWARD SPAR RIGHT HAND BULKHEAD FITTING LOCATED AT BS 1016 AND RBL 11.55. REPAIRED PER SOPM 20-43-03, SOPM 20-41-02, AND EA 343695.SDR DALA2023032802381Unknown · unknownSHIP 665 TOOL MARK ON STABILIZER STRAP BTW 1480 AND STA 1520 CEILING AREA RBL 16.5 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00235. AREA WAS REPAIRED PER B757-200 SRM. (2688120)SDR EE4Y2023032517508Fitting · unknownDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD TASK CARD 55-320-001_P1-OP-UP/001, IT WAS FOUND THE VERTICAL STABILIZER, RUDDER ATTACHH FITTING NO7 P/N D5537131800400 HINGE WITH PLAY. DUE THIS FACT THE PART WAS REPLACED IAW AIRBUS A320-200 SRM 51-72-1SDR EE4Y2023032517507Fitting · unknownDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD TASK CARD 55-320-001_P1-OP-UP/001, IT WAS FOUND THE VERTICAL STABILIZER, RUDDER ATTACHH FITTING NO5 P/N D5537131800200 HINGE WITH PLAY. DUE THIS FACT THE PART WAS REPLACED IAW AIRBUS A320-200 SRM 51-72-1SDR EE4Y2023032517506Fitting · unknownDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD TASK CARD 55-320-001_P1-OP-UP/001, IT WAS FOUND THE VERTICAL STABILIZER, RUDDER ATTACHH FITTING NO4 P/N D5537131800200HINGE WITH PLAY. DUE THIS FACT THE PART WAS REPLACED IAW AIRBUS A320-200 SRM 51-72-11SDR EE4Y2023032517505Fitting · unknownDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD TASK CARD 55-320-001_P1-OP-UP/001, IT WAS FOUND THE VERTICAL STABILIZER, RUDDER ATTACHH FITTING NO3 P/N D5537131800200 HINGE WITH PLAY. DUE THIS FACT THE PART WAS REPLACED IAW AIRBUS A320-200 SRM 51-72-1SDR EE4Y2023032517504Fitting · unknownDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD TASK CARD 55-320-001_P1-OP-UP/001, IT WAS FOUND THE VERTICAL STABILIZER, RUDDER ATTACHH FITTING NO2 D5537121800000 HINGE WITH PLAY. DUE THIS FACT THE PART WAS REPLACED IAW AIRBUS A320-200 SRM 51-72-11-91SDR EE4Y2023032517503Fitting · unknownDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD TASK CARD 55-320-001_P1-OP-UP/001, IT WAS FOUND THE VERTICAL STABILIZER, RUDDER ATTACHH FITTING NO1 P/N D5537121800000 HINGE WITH PLAY. DUE THIS FACT THE PART WAS REPLACED IAW AIRBUS A320-200 SRM 51-72-1SDR JJBA20230330039Unknown · unknownDENT ON RUDDER 1 LEADING EDGE SKIN BTW RIB ZV 2601.0 AND ZV 2890.0. DENT REDRESSED ON LH RUDDER 1, ON LE SKIN BTW ZIB ZV2601-ZV2890SDR EE4Y2023032317489Hinge Arm · out of limitsITEM 3-32 17489
DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: 553005-01-1-001_P1-OP-UP/003, IT WAS FOUND THE EMPENAGE, RUDDER HINGE ARM N° 4 P/N D5537131420054 AND FITTING P/N P/N D5537131802800 OUT LIMITS, DUE THIS FACT THE PART MUST BE REPLSDR EE4Y2023032317490Hinge Arm · out of limitsDURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: 553005-01-1-001_P1-OP-UP/003, IT WAS FOUND THE EMPENNAGE, RUDDER HINGE ARM N° 1 P/N D5537131620054 AND HINGE ARM N° 7 P/N D5537131720400 OUT LIMITS, DUE THIS FACT THE PARTS MUST BE REPLACED. SEE COOPSDR SWAA2023041919843Seal · crackedTAIL STAB PANEL 333AB HAS A CRACK.<[01] REMOVED AND REPLACED SEAL PER SOPM 20-50-01.;[02] INSPECTEDSDR CALA2023032200821Skin · crackedRH HORIZONTAL STAB LOWER SKIN CRACKED 1" IN LENGTH AT APPROX STA 129.50 I/B OF THE 7TH DRAIN HOLE 17" FROM L.E.M REF BY AIRB ORNE/PEMCO NR.13619.0325 ACCOMPLISHED CUTOUT OF CRACK ON R/H HORIZ STAB LOWER SKIN @ APPR TO VERIFY ENDS OF 1.85"L CRACK & TO VERIFY CSDR CALA2023031700789Skin · crackedRH HORIZONTAL STAB LOWER SKIN CRACKED 1" IN LENGTH AT APPROX STA 129.50 I/B OF THE 7TH DRAIN HOLE 17" FROM L.E.M REF BY AIRB ORNE/PEMCO NR.13619.0325 ACCOMPLISHED CUTOUT OF CRACK ON R/H HORIZ STAB LOWER SKIN @ APPR TO VERIFY ENDS OF 1.85"L CRACK & TO VERIFY CSDR EE4Y2023031017399Fitting · corrodedDESCRIPTION:
DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE ARM#7 WITH CORROSION.
CORRECTIVE ACTION:
REPLACED HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-003. SEE COOPESA WORK ORDER A1M116 SDR EE4Y2023031017398Fitting · noneDESCRIPTION:
DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #3 BEARING WITH PLAY.
CORRECTIVE ACTION:
REPLACED FORK AND END FITTING AT HINGE ARM BR3 IAW A319-SRM TASK 55-36-42-300-008.
SEESDR EE4Y2023031017397Fitting · noneDESCRIPTION:
DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #7 BEARING WITH PLAY.
CORRECTIVE ACTION:
REPLACED FORK AND END FITTING AT HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-008.
SEESDR CALA2023030300608Vortex Gen · missingONE LH AFT BODY VORTEX GENERATOR MISSING. REMOVED BROKEN V.G. AND INSTALLED A NEW V.G. REF. SRM 51-40-02 REMOVED CDL INOP SPEAKER.SDR SWIA2023020010None · damagedLIGHTNING STRIKE DAMAGE ON RH SIDE OF VERTICAL STABILIZER ALONG RIB 10 BETWEEN STRINGERS 1R AND 2R. (C-CHECK RO 2/28/2023) REMOVED LIGHTNING STRIKE AT VERTICAL STAB. R/H SIDE. ALONG RIB 10, STGRGS 1R AND 2R BY INSTALLING BUSHING AND FASTENERS AS REQUIRSDR CALA2023021300406Skin · crackedNDT TASK- INDICATION VERIFICATION, CRACK AT RH HORZ STAB LWR SKI N AT STA 157.10 (MARKED ON SKIN) FOR NDT EVALUATION (REF. AAR NR 99957732). PERFORMED REPAIR ON RH HORZ STAB LWR SKIN AT 157.10, REMOVED AND -801,51-21-72-370-801,27-41-21-000-801,55-10-00-000-80SDR CALA2023020600325Rib · crackedLH STAB LE STA 138.70 RIB CRACKED. 800-4. REF BY AIRBORNE/PEMCO NR.13088.0476. REPAIRED L/H HORIZ STABILIZER RIB STA 138-70 AS PER REF B737 SRM 55-10-09-2R-4 FIG 202 SHEET 1. COMPLETED BY V095648, INSP BY Q9 15, ENTERED BY V928371. RE-INSP BY Q966SDR VNAA202304270016Doubler · corrodedCORROSION ON LIGHTNING PROTECTION STRIP ON RH/LH HORIZONTAL STABILIZER TIP EXTERNAL STRUCTURE (ACCESS PANEL 343BR AND 333BL)SDR HYIA20230203001Not Entered · not enteredDURING ROUTINE INSPECTION IT WAS FOUND THAT THE ELEVATOR TRIM TAB HAS 4 CRACKED HINGES, 2 CRACKED DOUBLERS, AND 2 MISSING RIVETS IN THE AREA BETWEEN LEFT BL5 & RIGHT BL5.SDR SWIA20230129Unknown · damagedLH ELEVATOR HINGE FITTING #3- UPON REMOVAL OF BUSHINGS, FOUND INBD HINGE LUG INNER BORE DAMAGED. (C-CHECK RO 2/8/2023) REMOVED DAMAGE FROM LEFT HAND ELEVATOR HINGE FITTING #3 LUG AND INSTALLED FABRICATED BUSHING. REF EMB, SRM 51-29-00, 55-21-00REP01P.SDR SWAA2023010989184Slider · out of adjustLEFT LOWER AFT STAB SLIDER SEAL TRAILING EDGE NOT ENGAGED CORRECTLY<[01] REMOVED AND PROPERLY REISTALLED SLIDER SEAL PER AMM 55-30-00SDR SWAA2023010989187Slider · out of adjustRIGHT LOWER AFT STAB SLIDER SEAL TRAILING EDGE NOT ENGAGED CORRECTLY<[01] REMOVED AND PROPERLY INSTALLED SLIDER SEAL PER AMM 55-30-00SDR CALA2022121903428Fitting · crackedLH ELEV O/B ACTUATOR FTG FOUND CRACKED. PLEASE PRINT AND ACCOMPLISH OP09 TO REMOVE AND REPLACE CRACKED FTG. TRANSFER REF NON - ROUTINE WO.1318508 AND ORIG BY V924732 LH ELEVATOR OUTBOARD ACTUATOR FITTING REPLACED AND INSTALLED AS PER EA 5510-01896 REV C OP 009SDR FXGA202211112229None · noneMAIN CARGO DOOR LATCHES REPAIR. DURING TORQUE TUBE ISSUES ON ABOVE AIRCRAFT, ALL LATCHES RESULTED WITH GOUGES CAUSED BY THE LOCK PINS. IN ORDER TO CONTINUE WITH LATCHES EVALUATION, IT WILL BE REQUIRED TO BLEND OUT THE LATCHES AND PROVIDE THE THICKNESS OF REMSDR FDEA202210282681Intercostal · crackedINTERCOSTAL P/N AJC 7582-3 IS CRACKED AT AFT UPPER CONRER ACCESED THOUGH PANEL 363 PL. REPAIRED INTERCOSTAL P/N AJC 7582-3 UPPER AFT CORNER REF SRM 55-30-02-2R REPAIR 7 FIGURE 203 AND E.A.#: 1-5530-T0371227 A MAJOR REPAIR.SDR FDEA202210282680Intercostal · crackedINTERCOSTAL P/N AJC 7582-3 IS CRACKED AT FWD UPPER CORNER ACCESED THOUGH PANEL 363 PL. REPAIRED INTERCOSTAL P/N AJC 7582-3 FWD CORNER REF SRM 55-30-02-2R FIGURE 201 REPAIR 7SDR CALA2022102702941Rib · crackedEA 5510-01843 REV H. OP 001: DURING C-SCAN INSP OF LH HORZ P/N: 186A2000-33 S/N 000908, CRACK INDICATION NOTED BEYOND ACCEPTABLE LIMITS AT RIB 129.50, AFT OF DOUBLER LOWER SKIN. REF TO PEMCO NR 12733.0602 REPAIRED DAMAGE AREA AT L/H HORIZ. STAB LWR INSPAR SKINSDR CALA2022102402937None · crackedSTA 92.70 4TH STIFFNER ABOVE CHEM MILL VISUAL CRACK INDICATION. REF BY PEMCO NR.12738.0666. REPAIRED L/H HORIZ STABILIZER IN SPAR RIB 92.7 4TH STIFFNER FROM L/E IAW B737 SRM 55-10-09-2R-4. COMPLETED BY P112, INSP BY Q945 , ENTERED BY V928371. APPROVAL BY Q966.SDR CALA2022102402929None · crackedEA 5510-01843 REV H: STA 129.5 3RD STIFFNER ABOVE CHEM MILL VISUAL CRACK INDICATION. REF BY PEMCO NR.12738.0670. REPAIRED R/H HORZ STABILIZER IN SPAR RIB 129.5 3RD STIFFNER FROM L/E IAW B737 SRM 55-10-09-2R-4. COMPLETED BY P112, INSP BY Q945 , ENTERED BY V9283SDR CALA2022102402928None · crackedSTA 101.90 4TH STIFFNER ABOVE CHEM MILL VISUAL CRACK INDICATION. REF BY PEMCO NR.12738.0667. REPAIRED L/H HORIZ STABILIZER IN SPAR RIB 101.9 4TH STIFFENER FR OM L/E IAW B737 SRM 55-10-09-2R-4.COMPLETED BY P112, INSP BY Q94 5, ENTERED BY V928371. APPROVAL BY Q9SDR CALA2022101402817Vortex Gen · missingONE AFT BODY VORTEX GENERATOR MISSING ABOVE RIGHT HORIZONTAL STABILIZER. REMOVED FASTENERS FROM VORTEX PANEL. REMOVED PANEL FROM A/C SKIN. CLEANED SKIN OF SEALANT, PRIMMED AND PAINTED NEW PANEL. TRANSFERRED HOLES TO NEW PANEL WITH PILOT HOLES BROUGHT HOLES UPSDR CALA2022101402816Vortex Gen · missingONE AFT BODY VORTEX GENERATOR MISSING ABOVE RIGHT HORIZONTAL STABILIZER -- SEE PHOTO; REMOVED AND REPLACED RH SIDE LOWER VORTEX GENERATOR.SDR 2022FA0000611Skin · noneTHIS AIRCRAFT IS IN FOR ANNUAL INSPECTION AND SKIN PANEL P/N 33-6400000-87 IS CRACKED FROM STA 33.9 TO STA 44.4. VERTICAL STABLIZER, LEFT AFT SKIN HAS A VERTICAL CRACK ABOUT 10.5 INCHES ALONG THE LEFT SIDE REAR SPAR RIVET LINE. DURING THE "REAR FUSELAGE AND EMSDR IXXA2022100602Pivot Pin · wornRIGHT OUTER PIVOT PIN AND BEARING ARE WORNSDR CALA2022091402361Rib · corrodedRH ELEVATOR TIP HAS CORROSION (SUPPORT TASK). GENERATED BY V0616 82 AT HAECO LCQ, PER NR 9290678 (30678). CORROSION FOUND TO BE ON R/H ELEVATOR TIP CAP MOUNTING RIB AND T O BE OUT OF LIMITS IAW SRM A320 55-21-12-04-A. REMOVED AND REPLA CED WITH NEW RIB IAW A32
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