JASC 5220
Service difficulty reports · 7,388
Reports filed under 5220 · Emergency Exits, 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 = '5220' 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 = '5220' 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 USAA2012062800007Door Frame · corroded3S CHECK - CORROSION ON FORWARD CURVE EDGE OF THE LEFT AFT EMERGENCY EXIT DOOR (834) AT FR40. REPLACED FORWARD CURVE EDGE OF THE LEFT AFT EMERGENCY EXIT DOOR (834) AT FR40 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D52279010.SDR USAA2012062600011Door Frame · corroded3S CHECK - CORROSION ON CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4. REPLACED CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4 IAW A320 SRM 51-72-11 DRAWING D52279010.SDR N6WA2012061102Cover · inoperativeRT OVERWING EXIT HANDLE COVER WILL NOT CLOSE. REPLACED RT OVER WING HANDLE COVER IAW AMM 25-26-09. OPS CHECKED GOOD.SDR YENA20120611527Release Cable · defectiveFLT 6405 JFK-LCQ DURING HEAVY MAINTENANCE, RIGHT OVERWING EXIT CABLE FAILS TEST. RIGHT EMERGENCY SLIDE RELEASE CABLE REPLACED, RIGGED & OPS CHECKED ON CARD A320-53-1227-02. REF N/R 29840.SDR YENA20120611526Release Cable · defectiveFLT JFK-LCQ, DURING HEAVY MAINTENANCE, THE LEFT OVERWING EXIT CABLE FAILS TEST. LEFT EMERGENCY SLIDE CABLE RELEASE, RIGGED & OPS CHECKED ON CARD A320-53-1227-01. REF NR 29841.SDR USAA2012061100027Reservoir · low pressureFLIGHT ATTENDANT REPORTED PANEL INDICATIONS: DOOR DISARMED WHEN HANDLE WAS IN ARMED POSITION, AND CHECK SLIDE PRESSURE. ECAM IN FLIGHT DECK NORMAL THROUGHOUT FLIGHT.SDR AALA20120609006Pan · crackedCABIN SIDEWALL LEFT AFT OVERWING EXIT DOOR HAS CRACK IN DOOR PAN ON THE AFT SIDE AT 2ND FROM BOTTOM STOP PAD BRACKET. STOP DRILLED CRACK INSTALLED REPAIR DOUBLER PER SRM 52-05-00 FIGURE 51.SDR AALA20120609005Pan · crackedCABIN SIDEWALL LEFT AFT OVERWING EXIT DOOR HAS CRACK IN DOOR PAN ON AFT SIDE AT TOP STOP FITTING. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 52-05-00 FIGURE 51.SDR AALA20120607009Structure · crackedRIGHT FORWARD OVERWING EXIT DOOR CRACKED ON UPPER AFT CORNER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05-00.SDR AALA20120607008Structure · crackedRIGHT FORWARD OVERWING EXIT DOOR CRACKED ON UPPER FORWARD CORNER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05-00.SDR KCSA20120606005Battery Pack · dischargedRIGHT EMERGENCY DOOR BATTERY WILL NOT TEST. REMOVED AND REPLACED RIGHT UPPER DECK DOOR EMERGENCY BATTERY PACK IAW MM 52-23-14. OPS CHECK NORMAL.SDR USAA2012060500015Actuator · low pressurePRE-FLIGHT: SLIDE PRESSURE FOR DOOR 2L SHOWS LOW AND DOOR WILL NOT ARM. CHARGED SLIDE PRESSURE FOR DOOR 2L IAW AIRBUS MAINTENANCE MANUAL 52-22-00.SDR USAA2012062800006Angle · cracked2S CHECK - CRACK ON FRAME SEGMENT 1 OF LEFT AFT EMERGENCY EXIT DOOR (834) BETWEEN FR39 TO FR40, S14L TO S18L. REPLACED FRAME SEGMENT 1 OF LEFT AFT EMERGENCY EXIT DOOR (834) BETWEEN FR39 TO FR40, S14L TO S18L IAW EO 5210Y288.SDR USAA2012062600023Angle · cracked2S CHECK - CRACK ON SEGMENT ANGLE ON EMERGENCY EXIT DOOR 844 BETWEEN FR39 TO FR40, BETWEEN BEAM 1 TO BEAM 3 & BETWEEN S14R TO S18R. REPLACED SEGMENT ANGLE ON EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.SDR V0XR20120604J0046Insulation · damagedRT OVERWING EMERGENCY EXIT DOOR HAS 6 PIECES OF INSULATION SATURATED, OR DAMAGED BEYOUND SERVICEABLE LIMITS. R & R DAMAGED INSULATION IAW AMM 25-82-02-400-803.SDR USAA2012070200019Door Frame · cracked3S CHECK - CRACK ON INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.SDR USAA2012070200018Door Frame · cracked3S CHECK - CRACK ON INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.SDR USAA2012062900015Angle · corroded3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF LEFT FORWARD EMERGENCY EXIT HATCH (833) BETWEEN FR38 TO FR39 & BETWEEN BEAM 4 AND EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.SDR USAA2012062900014Angle · corroded3S CHECK - CORROSION ON T-SECTION ANGLE OF AFT LOWER VERTICAL FRAME OF LEFT FORWARD EMERGENCY EXIT HATCH (833) BETWEEN FR38 TO FR39 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.SDR USAA2012062900013Angle · corroded3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF LEFT AFT EMERGENCY EXIT HATCH (834) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.SDR USAA2012062900012Angle · corroded3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF RIGHT AFT EMERGENCY EXIT HATCH (844) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.SDR USAA2012062900011Angle · corroded3S CHECK - CORROSION ON T-SECTION ANGLE OF AFT LOWER VERTICAL FRAME OF RIGHT AFT EMERGENCY EXIT HATCH (844) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.SDR USAA2012062800017Door Frame · cracked3S CHECK - CRACK IN INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 843 IAW EO 5210Y228.SDR USAA2012062800016Door Frame · cracked3S CHECK - CRACK IN INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.SDR USAA2012062600010Door Frame · corroded3S CHECK - CORROSION ON CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4. REPLACED CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4 IAW A320 SRM 51-72-11 DRAWING D52279010.SDR USAA2012060100001Damper · low pressureDOOR 3L DOOR DAMPER HAS LOW PRESSURE. MAINTENANCE ADJUSTED DOOR 3L DAMPER.SDR USAA2012053100001Retainer · corrodedC2 CHECK - GALVANIC CORROSION FOUND ON AFT RIGHT EMERGENCY EXIT HATCH UNDER PRESSURE SEAL. REMOVED CORROSION AND REPLACED SEAL RETAINERS ON AFT RIGHT EMERGENCY EXIT HATCH IAW B737-400 SRM 51-40-02.SDR USAA2012062800003Angle · cracked2S CHECK - CRACK ON SEGMENT ANGLE OF LEFT AFT EMERGENCY EXIT DOOR (834) BETWEEN FR40 TO FR41, BEAM 1 TO BEAM 3. REPAIRED SEGMENT ANGLE OF LEFT AFT EMERGENCY EXIT DOOR (834) IAW EO 5210Y228.SDR USAA2012062200007Angle · cracked2S CHECK - CRACK IN EMERGENCY EXIT DOOR 844 FORWARD SEGMENT ANGLE BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED EMERGENCY EXIT DOOR 844 FORWARD SEGMENT ANGLE IAW EO 5210Y228.SDR USAA2012052900003Retainer · corrodedC2 CHECK - RIGHT AFT CABIN OVERWING EMERGENCY EXIT DOOR FIXED PRESSURE SEAL TRIM RETAINER HAS GALVANIC CORROSION AT LOWER JAM. REMOVED & REPLACED EMERGENCY EXIT DOOR RT AFT FIXED PRESSURE SEAL TRIM RETAINER AT LOWER JAM IN ACCORDANCE WITH B737 SRM 51-40-02.SDR USAA2012053100002Retainer · corrodedC2 CHECK - EXFOLIATION CORROSION ON LOWER ANGLE SEAL RETAINER OF AFT LEFT EMERGENCY EXIT HATCH. REPLACED LOWER ANGLE SEAL RETAINER OF AFT LEFT EMERGENCY EXIT HATCH IAW B737-400 SRM 51-40-02.SDR N6WA2012052302Escape Hatch · unsecureCREW ESCAPE HATCH NOT CLOSED PROPERLY. REINSTALLED COCKPIT EMERGENCY ESCAPE HATCH IAW AMM 52-22-00.SDR USAA2012052300021Frame · crackedC11 CHECK - CRACK IN UPPER SEGMENT FRAME AT RIGHT AFT EMERGENCY EXIT DOOR 844. REPLACED UPPER SEGMENT FRAME AT RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EA 139940.SDR USAA2012052300018Structure · crackedC11 CHECK - 1/2 CRACK FOUND AT AFT SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR 844. REPLACED AFT SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EA 139940.SDR USAA2012052300017Structure · crackedC11 CHECK - 1/2 CRACK FOUND AT FORWARD SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR 844. REPLACED FORWARD SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EA 139940.SDR USAA2012052300016Beam · crackedC11 CHECK - 1/2 CRACK FOUND AT LOWER BEAM FLANGE AREA OF RIGHT AFT EMERGENCY EXIT DOOR 844. REPLACED LOWER BEAM OF RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EA 139940.SDR USAA2012052300015Beam · crackedC11 CHECK - 1/2 CRACK FOUND AT LOWER BEAM FLANGE AREA OF RIGHT AFT EMERGENCY EXIT DOOR 844. REPLACED LOWER BEAM OF RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EA 139940.SDR UALA2012052102846Door · leakingAFT OVERWING EMERGENCY EXIT WINDOW AT ROW 21 ON THE RIGHT SIDE IS LEAKING WATER. PRESSURIZED ACFT TO 3 LBS NO LEAKS NOTED CLEANED AREA OF WATER. NO OTHER LEAKS NOTED AT THIS TIME, FLASH RAIN STORM AT TIME OF LEAK.SDR AALA20120530004Pan · crackedCABIN SIDEWALL RIGHT FORWARD OVERWING EXIT DOOR HAS A CRACK IN DOOR PAN NEXT TO STOP PAD BRACKET AT UPPER FORWARD CORNER. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 52-05-00 FIGURE 51 AND COMP-52-024000.SDR N6WA2012051801Snap Ring · missingSNAP RING ON RT LIFE LINE MISSING. INSTALLED SNAP RING ON RT LIFE LINE IAW AMM 25-63-04.SDR USAA2012051400022Actuator · low pressureCIDS CAUTION: CHECK DOOR R3 PRESSURE. SERVICED R3 DOOR ACTUATOR PER AMM TASK 52-22-00-614-002-A. OPS CHECKED GOOD.SDR UALA2012051102749Handle · damagedDURING EXTERIOR WALK AROUND, FOUND LEFT FORWARD EMERGENCY OVERWING ESCAPE DOOR HANDLE PUSHED IN. REMOVED LT FWD EMERGENCY HATCH PER MM AND ROUTED TO SHOP FOR REPAIR.SDR N6WA2012051001Hook And Loop · wornRT EMERGENCY EXIT PANEL COVER WON'T STAY ON. R & R HOOK AND LOOP ON RT EXIT PLANEL COVER IAW AMM 25-26-04.SDR USAA2012051000021Angle · crackedBC1 CHECK - 5 EA CRACKS ON SEGMENT ANGLE APPROX 1/8 INCH IN LENGTH ON FORWARD LEFT EMERGENCY EXIT DOOR 833. REPLACED SEGMENT ANGLE ON FORWARD LEFT EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.SDR USAA2012051000020Angle · crackedBC1 CHECK - 10 EA CRACKS ON SEGMENT ANGLE APPROX 1/8 INCH IN LENGTH ON AFT RIGHT EMERGENCY EXIT DOOR 844. REPLACED SEGMENT ANGLE ON AFT RIGHT EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.SDR USAA2012051600015Frame · crackedC11 CHECK - CRACK ON AFT FRAME SEGMENT OF LEFT AFT EMERGENCY EXIT DOOR AT STA 1792. REPLACED AFT FRAME SEGMENT OF LEFT AFT EMERGENCY EXIT DOOR IAW EO 5210Y228.SDR USAA2012051600014Frame · crackedC11 CHECK - CRACK ON FORWARD FRAME SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR AT STA 1738. REPLACED FORWARD FRAME SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR IAW EO 5210Y228.SDR USAA2012051600013Frame · crackedC11 CHECK - CRACK ON AFT FRAME SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR AT STA 1738. REPLACED AFT FRAME SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR IAW EO 5210Y228.SDR USAA2012050700014Cylinder · low pressureCIDS CAUTION LIGHT ILLUMINATED ON FLIGHT ATTENDANT PANEL. FOUND R2 ASSIST PRESSURE LOW - CHARGED R2 DOOR ASSIST CYLINDER IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-A.SDR SIMA20120501005Skin · gougedLEFT OVERWING EMERGENCY ESCAPE HATCH SKIN GOUGED AT LOWER FWD END NEAR METAL CLIP.(MARKED) REPAIRED LT OVERWING EMERGECY ESCAPE HATCH SKIN GOUGE AT LOWER FWD END NEAR METAL CLIP IAW EO EM-52MR-310.
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