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 QXEA0000582Skin · chafedPDX - SERVICE/EMERGENCY DOOR OUTER SKIN CHAFED FORWARD EDGE UPPER PART. REPAIRED IAW FOKKER SRM 51-10-04.SDR AWXA0000081Seal · leakingLEFT AFT OVERWING EXIT HAS VERY LOUD AIR LEAK. FOUND SMALL SEALANT VOID AT TOP CENTER SPLICE OF DOOR CUTOUT, CLEANED OUT AND RESEALED DOOR FOR FIRST OCCURRENCE. OPS CK GOOD. FOUND 6 SECTION OF DOOR SEAL PULLED FROM CHANNEL ON SECOND OCCURRENCE. REINSTALLEDSDR QXEA0000583Structure · crackedPDX - SERVICE/EMERGENCY DOOR UPPER FORWARD DOOR CORNER PROFILE CRACKED AT FOUR CHERRY RIVETS. REPAIRED IAW FOKKER SRM 51-31-01.SDR QXEA0000411Button · failedPDX - SERVICE EMERGENCY DOOR FAILED EMERGENCY RELEASE TEST. EMERGENCY RELEASE BUTTON DID NOT RELEASE MECHANISM WHEN ACTUATED. CLEANED AND LUBED.SDR 2000ZZZX293Structure · damagedPREVIOUSLY PLUGGED HOLE WITH SHORT EDGE DISTANCE AND GOUGE ON THE RT FORWARD EMERGENCY EXIT DOOR. REPAIRED PREVIOUSLY PLUGGED HOLE WITH SHORT EDGE DISTANCE AND GOUGE ON THE RT FORWARD EMERGENCY EXIT DOOR PER EIA ECRA 941-52-058-2.SDR QXEA0000587Structure · gougedPDX - SERVICE/EMERGENCY DOOR LIGHTNING HOLE FLANGE BY EMERGENCY RELEASE BUTTON HAS GOUGES AND BARE METAL. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 8 AND SRM 51-10-04.SDR QXEA0000409Skin · crackedPDX - RIGHT-HAND EMERGENCY EXIT DOOR TOP FORWARD CORNER SKIN HAD APPROXIMATELY 1 INCH CRACK. REPAIRED IAW FOKKER SRM 52-02-03, PAGE 5 AND SRM 51-31-05.SDR ABXA000087Pan · crackedLEFT MAIN ENTRY DOOR PAN CRACKED AT TOP HINGE CUT OUT. FABRICATED DOOR REPAIR ANGLE IAW DC9 SRM 52-05 FIGURE 47. INSTALLED DOOR REPAIR ANGLE IAW DC9 SRM 51-30-5 AND 51-30-1 AND 52-05 FIGURE 4.SDR CALA0000059Bracket · corrodedINSPECTION FOUND CORROSION AROUND FASTENER HOLE AT RT LOWER CORNER OF RT AFT EMERGENCY EXIT DOOR. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND 51-30-2. A BRACKET WAS INSTALLED IAW SRM 51-10-4 AND 51-30-1.SDR QXEA0000410Skin · crackedPDX - LEFT-HAND OVERWING AFT EMERGENCY EXIT DOOR TOP FORWARD CORNER SKIN HAD APPROXIMATLEY 1 INCH CRACK. REPAIRED IAW 52-02-03.SDR 2000ZZZM97Seal · failedAFTER T/O, THE FLT CREW EXPERIENCED PRESS DIFFICULTY. CAPT WAS NOTIFIED BY THE SENIOR F/A OF A LOUD SQUEAL COMING FROM LEFT FWD EMERGENCY EXIT DOOR. A DECISION WAS MADE TO LAND THE A/C. A/C WAS LANDED W/O FURTHER INCIDENT UNDER NORM CONDITIONS. AFTER LANDISDR DHL200071718DStop · crackedAT D CK, CABIN INTERIOR, RT FWD OVERWING EXIT CUTOUT HAS CRACKED PRESSURE STOP PAD AT AFT LOWER CORNER. REMOVED AND REPLACED PRESSURE STOP PADS, IAW B727 MM 52-20-0. REF: N/R 3280.SDR DHL200071717DStop · crackedAT D CK, CABIN INTERIOR, LT FWD OVERWING EXIT CUTOUT HAS CRACKED PRESSURE STOP PAD AT FWD LOWER CORNER. REMOVED AND REPLACED PRESSURE STOP PAD PER B727 MM 52-20-0, REF: N/R 3279.SDR SWAA000030Stop · out of rigDURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR RELEASE HANDLE DIFFICULT TO OPERATE. ADJUSTED STOP PINS PER MM.SDR TWAA0000808Flange · corrodedDURING CHECK-C MAINT, FOUND RT AFT OVERWING EMERGENCY EXIT, PRESSURE SEAL FLANGE BOTTOM SIDE WITH CORROSION FROM 6 INCHES UP ON EACH SIDE TO BOTTOM. REMOVED CORROSION BY SANDING PER SRM 51-10-6, PAGE 147. ALODINED AND PRIMED BARE AREA PER SRM 51-10-2 PAGE 1.SDR AALA996050Connector · failedUPON LANDING, TAILCONE UNSAFE LIGHT APPEARED. TAXIED CLEAR AT RUNWAY. F/A REPORTED TAILCONE WAS ATTACHED. INSPECTED ALL LOCKS AND CABLES. ALL SECURED, NO DEFECTS NOTED. CLEANED CANNON PLUG TO UNLATCH SWITCH. OPS CHECK GOOD. (M)SDR AWXA9900437Door · out of adjustAFT ENTRY DOOR EICAS MESSAGE DURING CLIMB. CABIN DOOR HANDLE COULD NOT BE LATCHED UNTIL A/C WAS DEPRESSURIZED PER QRH PROCEDURE WAS ACCOMPLISHED. ADJUSTED L4 PASSENGER DOOR IAW MM 52-11-00, OPS CK GOOD.SDR MWEA99820Frame · crackedVENTRAL DOOR FRAME LOWER RIGHT HAND CORNER HAD A CRACK. MTC REPAIRED CRACKED MEMBER IAW DC9- SRM 53-01 FIG 2 SHEET NR 4.SDR ABXA9900838Bracket · crackedDURING C-CHECK, FOUND INTERIOR BRACKET IN LOWER LEFT CORNER OF THE RIGHT FORWARD EMERGENCY EXIT DOOR CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-5.SDR ABXA9900781Pan · crackedDURING C-CHECK, FOUND RIGHT FORWARD OVERWING EXIT DOOR PAN CRACKED. REPLACED DOOR ASSEMBLY.SDR ABXA9900780Pan · crackedDURING C-CHECK, FOUND LEFT AFT EMERGENCY EXIT DOOR PAN CRACKED. REPLACED DOOR ASSEMBLY.SDR ABXA9900779Pan · crackedDURING C-CHECK, FOUND LEFT FORWARD EMERGENCY EXIT PAN CRACKED. REPLACED DOOR ASSEMBLY.SDR MWEA99771Beam · chafedLEFT LOWER CORNER OF AFT EXIT DOOR WAS CHAFED. MAINTENANCE FITTED AND INSTALLED NEW BEAM.SDR CA991116007Seal · displaced(CAN) IN CRUISE FLIGHT AT 8,000 FEET, CABIN PRESSURE WAS LOST AND AIR COULD BE HEARD EXITING FROM THE EMERGENCY EXIT DOOR AREA. MAINTENANCE FOUND A SMALL SECTION OF DOOR SEAL DISPLACED FROM ITS TRACK.SDR UPS99830979Fasteners · missingINSPECTION TYPE:N/A, AFT RT EMERGENCY EXIT DOOR LWR EDGE HAS SEVEN MISSING FASTENERS. *S/D* REMOVED R5 DOOR, REPLACED NUT PLATE CHANNEL AND INSTALLED SCREWS IAW SRM 51-3-0. REINSTALLED DOOR REF LG 416910 ITEM 2.SDR UPS99430980Skin · crackedINSPECTION TYPE:N/A, R3 DOOR HAD A 5 INCH CRACK ON SKIN AND WAS LEAKING. FABRICATED AND INSTALLED DOUBLER PER SRM 52-00-03.SDR QXEA9902215Skin · chafedPDX - LEFT AFT OVERWING EMERGENCY EXIT BOTTOM FORWARD CORNER CHAFED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 3, FIGURE 1.SDR QXEA9902214Skin · chafedPDX - LEFT OVERWING EMERGENCY EXIT BOTTOM AFT CORNER CHAFED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 3, FIGURE 1 AND SRM 52-01-01, PAGE 9.SDR QXEA9902213Skin · crackedPDX - LEFT AFT OVERWING EMERGENCY EXIT TOP FORWARD CORNER CHAFED/CRACKED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-02-03, PAGE 5.SDR QXEA9902212Skin · crackedPDX - LEFT AFT OVERWING EMERGENCY EXIT TOP AFT CORNER CHAFED/CRACKED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-02-03, PAGE 5.SDR SWAA991747Sensor · activatedABORTED TAKEOFF, PSEU LIGHT ILLUMINATED WHEN FLAP EXTENDED AND THRUST POWER APPLIED. C/W BITE CK, FAULT INFO SHOWED OVERWING DOORS DISAGREE PROBLEM. CYCLED BOTH OVERWING DOORS AND C/W FIM TASK. OPS CK GOOD.SDR MWEA99674Pan · crackedCRACK ON INNER PAN LOWER FORWARD CORNER OF RIGHT AFT OVERWING EMERGENCY EXIT DOOR. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR.SDR 20000424AP026Skin · crackedFOUND DURING D-CHECK, LEFT AFT OVERWING EXIT DOOR FOUND CRACK IN DOOR UNDER BOTTOM PLATE THAT WAS REMOVED FOR CORROSION. STOP DRILLED CRACK IAW DC-8 SRM 52-20-0. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21D. (M)SDR MWEA99666Door · crackedAFT VENTRAL DOOR HAS CRACK IN THE RADIOUS, RIGHT SIDE JUST ABOVE THE FIRST OFFICERS SEAT. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS.SDR DL757992098Assist Bottle · low pressureON LAYOVER, FOUND DOOR ASSIST POWER RESERVOIR AT DOOR 2R PRESSURE LOW. REPLACED DOOR BOTTLE PER MM.SDR USAA991004Skin · disbondedDURING A-2 CHECK VISUAL INSPECTION, FOUND A 12 INCH BY 36 INCH DISBONDED AREA AT SLIDE DOOR COVERING OUTER SKIN AND LEFT A/C RT OFF WING SLIDE DOOR. REMOVED AND REPLACED SLIDE. (X)SDR SWAA991498Handle · brokenDURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY DOOR HANDLE COVERPLATE BROKEN. REMOVED AND REPLACED HANDLE PER MM.SDR CALA9901130Casting · crackedINSPECTION FOUND A 1 INCH CRACK IN RT FORWARD OVERWING DOOR INNER UPPER CASTING. THE CASTING WAS REMOVED AND A NEW CASTING WAS INSTALLED IAW SRM 51-30-2, FIGURE 1.SDR SWIA971564Door · not latchedUNABLE TO PRESSURIZE CABIN. RETURNED TO SLC. LATCHED RIGHT FOWARD EMERGENCY EXIT. EXIT NOW SECURE. NO OTHER PRESSURIZATION PROBLEMS.SDR SWAA991403Stops · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT EMERGENCY OVERWING EXIT DOOR LOWER STOPS CRACKED. REMOVED AND REPLACED STOPS PER MM.SDR SWAA991320Door · gougedDURING SCHEDULED C2 CHECK, FOUND 2 EACH SMALL GOUGES ON RT EMERGENCY OVERWING DOOR AT FWD SKIN. REPAIRED SKIN PER SRM.SDR CALA9900867Press Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD RT OVERWING EXIT LOWER PRESSURE PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-10-1, PAGE 5. A DOUBLER WAS INSTALLED IAW SRM 51-40-3, PAGE 1, 51-10-2, PAGE 1, AND 51-30-2, PAGE 1.SDR RRXA991170Emergency Exit · unsecuredCABIN DOOR WARNING LIGHT CAME ON DURING ROTATION TO TAKEOFF ACCOMPANIED BY LOW RUSHING AIR NOISE. FOUND RT FWD OVERWING HATCH UNLOCKED, LOCKED WINDOW. OPS CK'D OK.SDR DL76L991470Step · missingON ARRIVAL, FOUND RT AFT OVERWING EXIT DOOR STEP MISSING. REF IPC 52-21-01-02 ITEM 75. A/C MTC FERRY HAM ATL AFTER INTERIM REPAIRS MADE.SDR 99T64R368ARDoor · corrodedFORWARD RIGHT O/W EXIT DOOR CORROSION WINDOW FRAME INTERNAL STATION 730. REMOVED CORROSION FILLED WITH HYSOL EA 9309NA. FAIRED TO ORIGINAL THICKNESS. TREATED AND FINISHED IAW DC-8 SRM 51-1-8 PER EO NR 99-061. (M)SDR 99T64R260ARWindow Frame · corrodedNR 2633 - AFT LT OVER WING DOOR, WINDOW FRAME CORRODED STA 798 - STA 822.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL 9309NA, FAIR TO ORIGINAL THICKNESS, TREATED AND PRIMED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROSDR 99T64R251ARWindow Frame · corrodedNR 2286 - FORWARD LT O/W EXIT DOOR, CORROSION WINDOW FRAME INTERNAL. STA 717-742. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL EA 9309NA TO FRAME, FAIRED TO ORIGINAL THICKNESS OF FRAME. TREATED AND PRIMED PER EO 99-061 WITH APPROVED FAA FORM 8110SDR 99T64R250ARWindow Frame · corrodedNR 2285 - AFT RIGHT O/W EXIT DOOR, CORROSION WINDOW FRAME INTERNAL. STA 798 - STA 822.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL EA 9309NA TO FRAME, FAIRED TO ORIGINAL THICNESS OF FRAME. TREATED AND PRIMES PER EO 99-061 WITH APPROVED FAA FSDR A6WA9900056Seal · failedDEN - FLT 7075 - SMELL BURNING INSULATION OF ELECTRICAL WIRES INSIDE COCKPIT. FOUND ESCAPE HATCH SEAL LEAKING WATER WHICH SHORTED SEVERAL OVERHEAD PANELS. REMOVED AND REPLACED OVERHEAD ESCAPE HATCH SEAL AND AFFECTED PANELS. AIR RETURN TO DENVER. (X)SDR SWAA990898Stops · wornDURING SCHEDULED TRANSITION CHECK, FOUND WORN STOP PADS AT LT AND RT OVERWING EMERGENCY EXIT DOORS. REMOVED AND REPLACED STOPS PER MM.
Back to JASC 5220