N123DN, cancelled Feb 28, 2018
Service difficulty reports · 40
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N123DN' AND deregistration_id = 'N123DN-2018-02-28' 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 n_number = 'N123DN' AND deregistration_id = 'N123DN-2018-02-28' 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 RYNA201207250031Connector · looseFOUND EMERGENCY LIGHTING WIRE HARNESS CONNECTOR LOOSE UNDER SEAT 26B AND 25F. RECONNECTED CONNECTOR AND SECURED WIRE HARNESS UNDER SEAT 26B AND25F AND EMERGENCY LIGHTING OPS CHECK GOOD PER MM 33-51-00.SDR RYNA201206150026Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE AT ALL PASSENGER SEATS AND LOWER EXIT SIGNS AT ALL DOORS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT SEATS 2A, 29A, AND 45G PER AMM 33-51-09. OPERATIONAL CHECKED NORMAL.SDR RYNA201203200015Actuator Valve · inoperativeNR 2 ENGINE WILL NOT START- ENGINE VALVE LIGHT ILLUMINATED ON OVERHEAD PANEL. EICAS MESSAGE "RIGHT ENGINE VALVE-NO START". REMOVED AND REPLACED ENGINE CONDITIONER CONTROL FUEL ACTUATOR PER MM 76-11-01 PG 401, OPS CHECK NORMAL.SDR RYNA2011082000018Battery Pack · inoperativeRIGHT/LEFT AFT, L1 AND R1 EMERGENCY EXIT THRESHOLD LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-07. OPERATIONAL CHECKED GOOD.SDR RYNA2010002260005Battery Pack · dischargedTHE FOLLOWING ITEMS WERE NOTED REGARDING THE EMERGENCY LIGHTING SYSTEM DURING THE INSPECTION AND TESTING OF THE C-CHECK ON AIRCRAFT N123DN: EMERGENCY LIGHT OUTSIDE R1 DOOR INOPERABLE AND 3 RT OVERWING. EMERGENCY EXIT SIGN INOPERABLE LEFT AND RIGHT SIDE O/H FSDR RYNA201002040003Strap · crackedDURING THE ACCOMPLISHMENT OF EO RN767-53-02 RELATED TO BOEING SB 767-53A0100 AND AD 2004-19-06-R1 .1875 INCH CRACK WAS FOUND ON THE RT REAR BULKHEAD SIDE FITTING FAIL-SAFE STRAP. ACCOMPLISHED REPAIR ON RT SIDE PER EO RN767-53-02 AND BOEING SB 767-53A0100.SDR RYNA2010002040002Strap · crackedDURING THE ACCOMPLISHMENT OF EO RN767-53-02 RELATED TO BOEING SB 767-53A0100 AND AD 2004-19-06 R1 A .0937 INCH CRACK WAS FOUND ON THE LT REAR BULKHEAD SIDE FITTING FAIL-SAFE STRAP. ACCOMPLISHED REPAIR ON LT SIDE PER EO RN767-53-02 AND BOEING SB 767-53A0100.SDR RYNA200910300021Unknown · malfunctionedDURING CLIMB EICAS E/E LIGHT ILLUMINATED, CABIN CONTINUED SLIGHT CLIMB. PERFORMED AIR TURNBACK. PLACARD THE LOWER LOBE ELECTRONIC EQUIPMENT ACCESS DOOR ITEM DEFERRED PER MEL 52-71-1 ITEM IS A CATEGORY C. ADDITIONALLY PERFORMED CABIN PRESSURE CONTROL BITE CHSDR RYNA200909180019Structure · crackedPERFORMING FLEET CAMPAIGN DIRECTIVE (FCD) 53-205 FOUND CRACKING WITHIN STA 287 AT WL 159 WHICH EXTENDS APPROXIMATELY 0.375 INCHES ABOVE WL 159 AND APPROXIMATELY 0.750 INCHES BELOW WL 159. FERRY WAS AGREED TO UNDER THE LIMITATIONS: FLIGHT TO BE CONDUCTED USINSDR RYNA200908210016Proximity Sensor · faultyDURING PREFLIGHT INSPECTION THE PILOT’S OVERHEAD EMERGENCY ADVISORY LIGHT CAME ON. PLACARD THE PILOT’S OVERHEAD EMERGENCY ADVISORY LIGHT PER MEL 52-71-1 DMI REFERENCE 60510. REMOVED AND REPLACED SENSOR 192 PER AMM 52-71-01 PAGE 412-414. OPS CHECK GOOD, CLESDR RYNA200906170007B-Nut · looseLEFT HYDRAULIC SYSTEM PRESSURE, RUDDER RATIO, LEFT HYDRAULIC QUANTITY, YAW DAMPER, AND SPOILER EICAS MESSAGES. TIGHTENED B NUT THAT BACKED OFF ON NR 1 ENGINE HYDRAULIC PUMP. REMOVED AND REPLACED PRESSURE, CASE DRAIN AND RETURN FILTERS.SDR RYNA200800044Fan Blade · out of balanceDURING CLIMB AND LEVEL OFF AT F/L 370 RIGHT ENGINE VIBRATION REACHED 3.9 UNITS. THE AIRCRAFT DIVERTED TO ATLANTA FOR MAINTENANCE TO DELTA AIRLINES MAINTENANCE CENTER. ACCOMPLISHED BORESCOPE INSPECTION, FAN BLADE LUBRICATION, RIGGED VSV & VBV SYSTEM AND BALANSDR RYN2008F00010Radio · failedACFT DIVERTED DUE TO LOSS OF THE RT HF COMMUNICATION SYSTEM. THE LT HF IS ALREADY ON DEFERRAL PER MEL 23-11-1-2. TROUBLESHOOTING IN WORK (ISSUED MEL 23-11-1-2OH DMI NR62632). (S)SDR DL76S071016Window · crackedF/O WINDSHIELD CRACKED AND IS ARCHING. REPLACED R1 WINDOW WINDOW HEAT CONTROL UNIT PER AMM. BITE CHECKED CONTROL UNIT IT VERIFIED GOOD.SDR DL76S060877Floorbeam · corrodedCORROSION WAS FOUND AROUND THE NUT PLATES ON THE LOWER TEE OF THE 1502 FLOORBEAM. THE CORROSION WAS REMOVED AND REPAIR PARTS INSTALLED PER BOEING INSTRUCTIONS AS CONTAINED IN 456631-14.SDR DL76S060876Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT THE NR 3 VHF ANTENNA, FS 1197+90, AT STR 39L 39R. REPAIR INVOLVED CUTTING OUT THE DAMAGE AND INSTALLATION OF BOEING APPROVED REPAIR PARTS PER ERA 455968-14.SDR DL76S060875Fitting · corrodedCORROSION WAS IDENTIFIED ON THE INBOARD FORWARD SURFACE OF THE REAR SPAR BULKHEAD TERMINAL FITTING. THE BOEING APPROVED REPAIR INVOLVED REMOVING BOLTS FOR ACCESS AND LIGHT BLENDING OF THE SURFACE TO REMOVE THE CORROSION PER ERA 456629-14.SDR DL76S060873Spar · crackedTHE NUMBER 1 PYLON UPPER SPAR FITTING, RHS AT ATTACH FITTING HOLE SHOWED A CRACK INDICATION. THE SUBJECT HOLE WAS OVERSIZED, AND THE BOEING APPROVED REPAIR INVOLVED INSTALLATION OF A STRAIGHT SHANK FREEZE PLUG PER ERA 456634-14.SDR DL76S060871Bulkhead · damagedDURING ACCOMPLISHMENT OF THE SIP MOD ON THE AIRCRAFT, AN EXISTING FREEZE PLUG REPAIR WAS FOUND ON THE NR 1 PYLON LHS UPPER ATTACH HOLE FOR GSE FITTING. THE PLUG WAS COMMON TO THE BULKHEAD FLANGE AND SIDE LOAD FITTING. THE SIDE LOAD FITTING WAS REPLACED AS PASDR DL76S060870Spar · damagedDURING ACCOMPLISHMENT OF EO 01-074906-03 THE NUMBER 2 PYLON SPLICE PLATE UPPER OUTBOARD HOLE WAS FOUND TO ALREADY BE OVERSIZED TO BEYOND MAX EO LIMIT. THE BOEING APPROVED REPAIR INVOLVED INSTALLATION OF AN OVERSIZED FASTENER PER ERA 456537-14.SDR DL76S060869Fitting · damagedTHE NUMBER 2 PYLON UPPER SPAR FITTING WAS FOUND TO HAVE A PREVIOUSLY OVERSIZED HOLE, AT THE AFT OUTER PERIMETER FASTENER. A BOEING APPROVED REPAIR WAS INSTALLED AT THE SUBJECT LOCATION, PER ERA 456536-14.SDR DL76S060868Skin · misrepairedA PREVIOUS REPAIR FOUND ON THE FUSELAGE SKIN AT 500 AND S36L DOES NOT CONFORM TO SRM AND NO RECORDS WERE FOUND. REPAIR WAS REMOVED AND A BOEING APPROVED REPAIR WAS INSTALLED PER ERA 456627-14.SDR DL76S060658Frame · crackedFUSELAGE FRAME FS 883.5 RHS LOWER INNER CHORD CRACK. CRACK WAS LOCATED ON THE LOWER END OF THE .25 RADIUS TRANSITION BETWEEN CHORD FLANGES.SDR DL76S060649Frame · crackedCRACKS WERE FOUND ON THE INNER CHORD OF THE FS 903 FRAME, RT SIDE. DAMAGE WAS CUT OUT AND A REPAIR ANGLE WAS INSTALLED.SDR DL76S060583Fitting · misalignedTHE NR 1 PYLON INBOARD PITCH LOAD FITTING UPPER LINK BUSHING HAS MIGRATED 0.004 INCH. THE MIGRATED BUSHING WAS REPLACED. AD 2004-16-12, B767-57-0053.SDR DL76S060701Linkage · misinstalledDURING INSPECTION OF THE LT OFF WING ESCAPE SLIDE PER JIC 6075 THE TECHNICIAN FOUND THAT THE INTEGRATOR LOCK HANDLE HAD TO BE FORCED INTO THE SAFETY POSITION. UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT SLIDE DOOR OPENING ACTUATOR LINKAGE LEVER WAS INSTSDR DL76S020312Light · inoperativeSVC CHECK FOUND EMERGENCY OVERHEAD LIGHT AT ROW 17 LT SIDE INOP. REPLACED EMERGENCY LIGHT ASSY AT ROW 17 LT SIDE, CHECKS OK.SDR DL76S011436Battery Pack · dischargedRT EMERGENCY ESCAPE SQUIB WILL NOT TEST. REPLACED RT BATTERY PACK TEST OK.SDR DL76S001594Battery · dischargedEMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY INOP. REPLACED BATTERY.SDR DL76S990685Power Supply · inoperativeDURING ROUTINE MAINTENANCE, THE LEFT AND RIGHT EMERGENCY EXIT THRESHOLD LIGHTS FOUND INOP. REPLACED POWER SUPPLY, OPS CK NORMAL.SDR DL76S980655Wedge · delaminatedWINGS NR 1 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 1 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 4 AREA OF DELAMINATION ON THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364345-14AD.SDR DL76S980654Wedge · delaminatedWINGS NR 2 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 2 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 7 BY 4.5 AREA OF DELAMINATION ON THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364346-14AD.SDR DL76S980653Wedge · delaminatedWINGS NR 8 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 5 BY 9 AREA OF DELAMINATION ON THE UPPER SKIN. THE DELAMINATION WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364347-14AD.SDR DL76S980652Skin · delaminatedWINGS LEADING EDGE SLAT NR 11, TRAILING EDGE WEDGE, SKIN DELAMINATION REPAIR. THE UPPER SKIN OF THE NR 11 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 6 AREA OF DELAMINATION. THE DAMAGE WAS TRIMMED OUT AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER SDR DL76S970585Battery Pack · dischargedRIGHT AND LEFT AFT SERVICE DOOR INTERIOR EMERGENCY EXIT LIGHT SIGNS INOP. REPLACED BATTERY PACK, CHECKS GOOD.SDR DL76S970341Skin · delaminationTHE NR 10 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED AT THE INBD CORNER. THE DAMAGE CUTOUT MEASURES 8 FWD-AFT AND 6 INBD-OUTBD. DAMAGE REPAIRED PER ER/A 361270-14AD.SDR DL76S961847Te Wedge · delaminatedTHE NRS 10, 11, 12 LEADING EDGE SLATS' TRAILING EDGE WEDGES WERE FOUND TO HAVE AREAS OF DELAMINATION. THE AREAS MEASURE 4 INCHES BY 6 INCHES, 2 INCHES BY 3 INCHES, AND 10 INCHES BY 6 INCHES, RESPECTIVELY. REPAIRED IN ACCORDANCE WITH B767-300 SRM, 57-43-02, FSDR DL76S960203Check Valve · crackedINFLIGHT GOT EICAS FOR LT SYS HYDRAULIC'S, FOLLOWED IMMEDIATELY BY LEFT HYDRAULIC SYS PRESSURE MESSAGE. STATUS PAGE SHOWS LT QTY AT 0.04. FOUND CHECK VALVE AT GROUND HYD SERV QUICK DISCONNECT LEAKING.SDR DL76S952151Skin · lightning strikeFOUND DURING LETTER CHECK, LIGHTNING STRIKES ABOVE COCKPIT SECTION OF FUSELAGE. BURNISHED OUT DAMAGES, FOUND ONE LIGHTING STRIKE OUT OF LIMITS. REPLACED RIVETS STA 355 BETWEEN STR 3 AND 4R STA 400 STR 4R, STA 484 STR 3R. DYE CHECKED AREAS, TREATED AND PAINTSDR DL76S950698Skin · lightning strikeDURING LETTER CHECK, FOUND SEVERAL LIGHTNING STIKES TO FUSELAGE SKIN. RT SIDE REPAIRED PER SRM 53-00-01 ITEM 3.
Back to N123DN, cancelled Feb 28, 2018