N311EA, cancelled Feb 23, 2004
Service difficulty reports · 58
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 = 'N311EA' AND deregistration_id = 'N311EA-2004-02-23' 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 = 'N311EA' AND deregistration_id = 'N311EA-2004-02-23' 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 WRNA200300011Pressure Switch · leakingDURING CLIMB/CRUISE FULL FIRE INDICATION ON ENG NR 3, LOOP A&B ON, FIRE HANDLE ON, FIRE BELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATIONS OFF IMMEDIATELY AFTER ENGINE SHUTDOWN. FIRE BOTTLE NOT FIRED. APPROX 8800 GALS. OF FUEL DUMPED. A/C RETURNED TO FIELD, LANDEDSDR WRNA200300010Fire Loop · false activationAFTER TAKE OFF AND DURING CLIMB OUT A FULL FIRE INDICATION ON NR 3 ENGINE. LOOP A & B ON, FIRE HANDLE ON, FIREBELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATION OFF IMMEDIATLY AFTER ENGINE SHUTDOWN. FIRE BOTTLES NOT FIRED. FUEL DUMPED (APPROX. 8800 GALLONS) AIRCRAFSDR WRNA200200007Fire Loop · shortedEnroute to BDL @ approx. 270fl, A&B fire loop on #1 engine came on. Engine fire lights came on and fire bell. Bell silenced, #1 engine shutdown per procedures. Alt fire bottle discharged, light remained in handle, Main bottle discharged light remained on. FuelSDR WRNA200200006Duct · detachedAircraft at F/L 280 outflow valves full closed cabin climbing at 2,000 ft/min. Manual and stby control no help. Aircraft returned to departing airport. Fuel dumped (42K lbs.) to make max landing wt. Aircraft landed normal.Corrective Action: Mx found duct out oSDR WRNA200200004Computer · unserviceableDuring Climb to cruise altitude Both Mach Feel Fail Lights came on. Fuel dump procedures carried out for Max landing wt (26K lbs dumped). Aircraft landed normal and returned to base.Corrective Action: Removed and replaced Trim Augmentation Computer. Op's checkSDR WRNA00023Cover · out of positionAT 27,000 FEET NR 2 PACK WATER SEPARATOR COVER BLEW OFF. CREW UNABLE TO MAINTAIN PRESSURIZATION ON NR 3 PACK ONLY. AIRCRAFT RETURNED TO BQN. FUEL DUMPED. AIRCRAFT LANDING NORMAL. WATER SEPARATOR COVER REINSTALLED, CLAMP SECURED AND TORQUED IAM MM 21-51-07SDR WRNA200100018Cover · separatedAT 27,000 FEET NR 2 PACK WATER SEPARATOR COVER BLEW OFF. CREW UNABLE TO MAINTAIN PRESSURIZATION ON NR 3 PACK ONLY. AIRCRAFT RETURNED TO BQN. FUEL DUMPED. AIRCRAFT LANDING NORMAL. WATER SEPARATOR COVER REINSTALLED AND CLAMP SECURED AND TORQUED IAM MM 21-51SDR 20010529SG003Engine · vibrationENGINE SHUTDOWN FOR HIGH VIBRATION INDICATION AT FL350. IN CRUISE INDICATION 3 AND AMBER LIGHT. BOTH A AND B PICKUPS. LOW SELECTION INDICATES THIS PROBLEM. TEST CARRIED OUT IAW 71-00-00 TEST 16. ALL TRIM WEIGHTS REMOVED. EPR 1.53=1.3 UNITS 90 PERCENT N1=SDR WRN2001F00000Turbine Blades · failedINSPECTION REVEALED IP TURBINE BLADE FAILURE. REMOVED AND REPLACED ENGINE IAW TRADEWINDS CARD L2-130-A01 AND FORMS TWM-7103B AND TWM-7103BB. AIRCRAFT RUN AND LEAK CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2001F00004O-Ring · pinchedNR 3 ENGINE OIL QUANTITY DROPPED TO 1 QUART, OIL PRESSURE FLUCTUATED BUT DID NOT DROP BELOW 35 PSI. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND DAMAGED (PINCHED) O-RING AT NR 3 ENGINE OIL PRESSURE FILTER BOWL CAP. REMOVED AND REPLACED O-RING IAW MM 72-01-00. RSDR WRN2001F00001Compressor · stalledON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR TWO ENGINE FERRY BEING ACCOMPLISHED IAW LOCKHEED MM AND TRADEWINDS GMM FOR ENGINE CHANGE AT MAINSDR 20010509SG004Compressor · stalledON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR TWO ENGINE FERRY BEING ACCOMPLISHED IAW LOCKHEED MM AND TRADEWINDS GMM FOR ENGINE CHANGE AT MX BSDR 20000516AP005Card · malfunctionedNR 2 ENGINE FILTER PRESSURE LIGHT, ALSO ENGINE VIB FILTER PRESSURE LIGHT CAME ON DURING CRUISE. NR 2 ENGINE SHUTDOWN. A/C CAME IN WITH NORMAL APPROACH AND LANDING. REMOVED AND REPLACED PRESSURE FILTER AND FINE SCAVENGE FILTER IAW 72-01-00. LEAK CHECKS GOODSDR 20000615AP019Doubler · corrodedDURING INSPECTION OF FESC, CORROSION FOUND BETWEEN FS 315 AND 297 FORWARD OF NOSE WHEEL AREA, SURROUNDING FORWARD LAV VENTILATION DUCT. REMOVED AND REPLACED CORRODED DOUBLER. CLEANED AND PAINTED AREA. DWG NR 1548569. (M)SDR 20000405AP001Doubler · corrodedDURING INSPECTION OF FESC, FOUND CORROSION BETWEEN FS 315 AND 297 FORWARD OF NOSE WHEEL AREA, SURROUNDING FORWARD LAV. VENTILATION DUCT REMOVED AND REPLACED CORRODED DOUBLER. CLEANED AND PAINTED AREA. (M)SDR 2000ZZZM250Oil Pump · failedNR 2 ENGINE RAPID LOSS OF OIL QTY ENGIEN RAN APPROXIMATELY 2 MINUTES PRIOR TO SHUTDOWN WINDMILLED WITH NO OIL QTY 23 MINUTES OIL PRESSURE NR 2 LIGHT ON. RETURNED TO BQN, LANDING NORMAL. REMOVED AND REPLACED PRIMARY OIL PUMP ASSEMBLY IAW MM 72-63-03. RUN ANDSDR 98ZZZM404Hyd Line · leakingSYSTEM 'C' HYD RSVR QTY LOW AND DECREASING. SWITCHING PUMP OFF DID NOT STOP FLUID LOSS. REF MANUAL GEAR EXTENSION, ATM TURNED OFF FLUID LOSS STOPPED AT AROUND THREE-EIGHTHS TANK QTY. AIRCRAFT LANDING NORMAL. FOUND PIN HOLE LEAK IN HYD C-CHECK SYSTEM RETURNSDR 98ZZZM193Actuator · failedAFTER TAKEOFF DURING FLAP RETRACTION FLAP/SLAT LOCK LIGHT ON, L/E TRANS LIGHT REMAINED ON. GREEN SLAT LIGHTS ON LEFT WING. NO LIGHTS ON RT WING. AIRCRAFT RETURNED TO BASE. LANDING NORMAL. REMOVED AND REPLACED NR 7 SLAT ACT IAW 27-81-21. REMOVED AND REPLASDR 97ZZZX3958Tire · failedON TAKEOFF ROLL, NR 6 TIRE BLEW. TIRE RUBBER DAMAGED HYDRAULIC LINE AND T/E WING PANEL. ACFT DUMPED FUEL AND RETURNED TO BASE. LANDING NORMAL. NR 5 AND NR 6 TIRES REPLACED. PANEL P/N 1529072-191 LOCATION NR 541BB WAS REPLACED PER SRM 57-34-00, NOTE 12. PSDR 97ZZZX3800Rudder Stud · shearedBQN - DURING TAXI, CREW NOTICED A BINDING WITHIN THE RUDDER PEDALS FOLLOWED BY A 'POP' SOUND FROM UNDERNEATH COCKPIT FLOOR. AIRCRAFT RETURNED TO GATE. BQN MAINTENANCE FOUND A RUDDER LINKAGE STUD SHEARED ON THE RIGHT HAND SIDE. REMOVED AND REPLACED STUD AND SDR 97ZZZX3393Brace Assy · crackedRIGHT MLG DOWNLOCK JURY BRACE FOUND CRACKED UPON MAINTENANCE WALK-AROUND. REMOVED AND REPLACED DOWNLOCK JURY BRACE IAW 32-11-14. AIRCRAFT RETURNED TO SERVICE. (X)SDR 97ZZZM707Actuator · failedAFTER TAKEOFF, LEFT GEAR INTRANS DOOR, F/E LEFT GEAR OR DOOR LIGHTS ON GEAR RETRACTED. AIRCRAFT DUMPED FUEL AND RETURNED TO BQN WITH A NORMAL LANDING. WHEN AIRCRAFT RETURNED TO GATE, MAINTENANCE NOTED LEFT GEAR DOOR OPEN. MX TROUBLESHOT AND FOUND MLG DOOR ASDR 97ZZZM674Water Separator · failed ductAPPROX 20 MINUTES AFTER TAKEOFF, LOST CONTROL OF CABIN PRESSURE DUE TO LEAK AT 28,000 FEET. A LOUD NOISE OCCURRED AT THE SAME TIME. RETURNED TO GSO, LANDING NORMAL. INSPECTION FOUND NR 2 WATER SEPARATOR HAD BLOWN DUCT. REMOVED AND REPLACED WATER SEPARATOR SDR 97ZZZM570Panels · missingAFTER APPROXIMATELY 125 NM, AFTER TAEKOFF, A SUDDEN VIBRATION WAS FELT. AIRCRAFT RETURNED TO BASE. LANDING WAS NORMAL. AFTER LANDING, INSPECTION REVEALED PANELS 198K AND 196B WERE MISSING. RIGHT WING TO FUSE PANELS REINSTALLED. AIRCRAFT RETURNED TO SERVICSDR 97ZZZM569Panels · missingAFTER APPROXIMATELY 125 NM, AFTER TAEKOFF, A SUDDEN VIBRATION WAS FELT. AIRCRAFT RETURNED TO BASE. LANDING WAS NORMAL. AFTER LANDING, INSPECTION REVEALED PANELS 198K AND 196B WERE MISSING. RIGHT WING TO FUSE PANELS REINSTALLED. AIRCRAFT RETURNED TO SERVICSDR 97ZZZM571Actuator · failedON GEAR RETRACTION, RIGHT GEAR DOOR LIGHT ON, WITH RED DOOR AND RED INTRANSIT LIGHT ON. FUEL JETTISON FROM 76,000 LBS TO 30,000 LBS. AIRCRAFT LANDED NORMALLY. RIGHT DOOR ACTUATOR REMOVED AND REPLACED IAW 32-33-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SESDR 96ZZZX5798Line · crackedA-HYD SYS RAPIDLY DEPLETED AT 33,000 FEET. SYS SHUTDOWN IAW FLIGHT MANUAL. AIRCRAFT LANDED NORMALLY. FOUND HYD LINE IN NR 1 PYLON AREA LEAKING. REPAIRED LINE IAW REV MM ATA 20. AIRCRAFT RETURNED TO SERVICE.SDR 96ZZZX5797Pdu Motor · crackedA-HYD RESERVOIR QTY LOW AND LOW QTY LIGHT ON. TURNED OFF HYD PUMP - LEAK STOPPED. AIRCRAFT LANDED NORMAL. FOUND SLAT A-SYS PDU HYD MOTOR HOUSING CRACKED. REMOVED AND REPLACED MOTOR IAW MM 27-80-10. AIRCRAFT RETURNED TO SERVICE.SDR 96ZZZM1536Lock Actuator · failedMAIN GEAR DOOR LIGHT AND RED INTRANSIT LIGHT CAME ON DURING CLIMB-OUT. AIRCRAFT RETURNED TO AIRPORT. LANDING NORMAL. REMOVED AND REPLACED MAIN GEAR DOOR LOCK ACTUATOR IAW 32-33-08 OF THE MM. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR 96ZZZM371Prox Logic Box · malfunctionedNOSE GEAR OR DOOR LIGHT AND RED INTRANSIT LIGHT CAME ON DURING CLIMB, RETURNED TO AIRPORT. LANDING WAS NORMAL. ADJUSTED NOSE GEAR UPLOCK SENSOR IAW 32-61-04. REMOVED AND REPLACED PROX LOGIC BOX IAW 31-22-01. INSTALLED PROX LOGIC CARD IAW 31-22-02, CARRIED SDR DLSP96004Skin · crackedATL - DURING CONTRACT MAINTENANCE AT DALA, THE FUSELAGE SKIN WAS FOUND WITH AN APPROXIMATE 1 INCH LONG CRACK RUNNING HORIZONTALLY FROM THE FORWARD EDGE OF THE SKIN AT FS 1363 LOCATED MIDWAY BETWEEN STR 18 AND STR 19. THE CRACK IS SIMILAR TO THOSE ADDRESSED INSDR DLSP96003Angle · oversize holesATL - DURING CONTRACT MAINTENANCE AT DALA, C/W AD 94-05-01, REPLACEMENT OF FUSELAGE LT AND RT WING TO FUSELAGE AT TACH UPPER ROOT JOINT FAIL-SAFE ANGLE, SEVERAL HOLES WERE FOUND OVERSIZED AND OUT-OF-ROUND. REAMED HOLES TO A ROUND CONDITION PER DL ERA 273277-1SDR DLSP96002Skin · crackedATL - DURING CONTRACT MAINTENANCE WITH DALA, FOUND FUSELAGE SKIN AT FS 1363 CRACKED IN THE TYPICAL MANNER DEPICTED IN THE L1011 SRM 53-11-00, FIGURE 826, REPAIR. THE SUBJECT CRACK IS APPROXIMATELY 12 INCHES IN LENGTH AND HAD BEEN PREVIOUSLY REPAIRED PER SRM 5SDR DLSP96001Skin · crackedATL - DURING CONTRACT MAINTENANCE AT DALA, THE FUSELAGE SKIN AT FS 1363 IS CRACKED IN THE TYPICAL MANNER DEPICTED IN SRM 53-11-00, FIGURE 826, REPAIR. THE CRACK IS APPROXIMATELY 2.25 INCHES LONG, LOCATED BETWEEN STR 21 AND STR 22. THE SUBJECT CRACK WAS PREVISDR 96ZZZM283Press Ctlr · failedAIRCRAFT DEPARTED BQN EN ROUTE TO GSO, CREW EXPERIENCED DIFFICULTY WITH CABIN PRESSURIZATION. C/B 3X14 PULLED AND RESET TO NO AVAIL. AIRCRAFT RETURNED TO BQN. LANDING NORMAL. AFT OUTFLOW VALVE OK IN ALL MODES, FORWARD VALVE INOP IN ALL MODES. T/S PER 21-5SDR 95ZZZM520Angle · crackedDURING NORMAL SERVICING OF ATM, MAINTENANCE NOTICED A CRACK LOCATED AT FS 1363 WL 147 (APPROXIMATELY) ON THE RIGHT SIDE. ANGLE 1561639-101 REPAIRED IAW SRM 53-11-00 FIG 822. AIRCRAFT RETURNED TO SERVICE. (M)SDR 95ZZZM506Pin · crackedWHILE PERFORMING ROUTINE MAINTENANCE, MECHANIC FOUND LEFT MLG RETRACT ACTUATOR PIN CRACKED AT AFT HOUSING. MLG PIN WAS REMOVED AND REPLACED IAW 32-11-27. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 95ZZZX4103Bulkhead · crackedACCOMPLISHED AD 95-12-24. DISCOVERED CRACKS ON RIGHT LOWER OUTBOARD SECTION OF FS 1363 BULKHEAD BY VISUAL INSPECTION. PERFORMED BOLT HOLE EDDY CURRENT INSPECTION IAW SB 093-53-268. TWO CRACKS WERE FOUND ON THE BULKHEAD CAP AT BL 42.5. LOCKHEED NOTIFIED AND SDR 95ZZZW622Spar Web · crackedWING REAR SPAR AND WEB UPPER CAP REPLACEMENT IWS 228-423. REPAIR CARRIED OUT BY DELTA AIRLINES IAW ERA 280196-14AD REV B DATED 3-29-94. REFERENCED BY FAA FORM 8110-3 DATED 3-31-95. (W)SDR 95ZZZW621Spar Web · crackedWING REAR SPAR AND WEB UPPER CAP REPLACEMENT IWS 228-423. REPAIR CARRIED OUT BY DELTA AIRLINES IAW ERA 280196-14AD REV B DATED 3-29-94. REFERENCED BY FAA FORM 8110-3 DATED 3-31-95. (W)SDR DALR950002Fitting · crackedATL - DURING LETTER CHECK AT DALR, THE NLG SHOCK STRUT SUPPORT FITTING ON THE RBL 22 BULKHEAD WAS FOUND CRACKED NEAR FS 449. CRACKS WERE REPAIRED PER DER APPROVED DATA, EL ERA 270628-14. TT, 38155 HRS. CYCLES, 18905. (X)SDR DALR950006Fitting · corrodedATL - DURING LETTER CHECK AT DALR, CORROSION WAS FOUND IN THE RIGHT WING REAR SPAR TO FUSELAGE UPPER WING ROOT TENSION FITTING BOLT HOLE. THE BOLT HOLE WAS OVESIZED TO CLEAN UP CORROSION PER DL ERA 270605-14. TT 38155 HRS. CYCLES, 18905. (X)SDR DALR950013Wing Skin · crackedATL - DURING LETTER CHECK, COMPLYING WITH AD 94-05-01 AND AD 93-17-01. AT THE REPLACEMENT OF THE LEFT WING INBOARD REAR SPAR SECTION, A CRACK WAS FOUND IN THE UPPER WING SKIN AT APPROXIMATELY IWS 332 AT A FASTENER HOLE. THE HOLE WAS OVERSIZED TO REMOVE THE CSDR DALR950005Spar Cap · crackedATL - DURING LETTER CHECK AT DALR. THE CENTER WING FS 1163 INTERMEDIATE SPAR UPPER CAP WAS FOUND WITH A CRACK IN ITS LEFT SIDE OUTBOARD END. THIS CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPISHED PER DL ERA 270580-14. TT, 38155 SDR DALR950004Spar Cap · crackedATL - DURING LETTER CHECK AT DALR, WING CENTER SECTION FS 1043 INTERMEDIATE SPAR UPPER CAP HAS A CRACK IN THE LEFT SIDE OUTBOARD END. THE CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPLIHSED PER DL ERA 270578-14. TT, 38155 HRS. CYSDR DALR950003Spar Cap · crackedATL - DURING LETER CHECK AT DALR. THE WING CENTER SECTION INTERMEDIATE SPAR UPPER CAP AT FS 1103 WAS FOUND CRACKED AT THE LEFT SIDE OUTBOARD END. THE CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPLISHED PER DL ERA 270579-14. TT, 3SDR DALR950001Fitting · corrodedATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 AND AD 93-17-10 DURING THE REPLACEMENT OF THE INBOARD LEFT AND RIGHT REAR SPAR WEB AND REWORK OF THE UPPER 1.1250 INCH (2 TOTAL) AND INBOARD .6250 INCH (4 TOTAL) HOLES AT THE MLG BACKUP FITTING IWSSDR DALR950008Skin · crackedATL - DURING LETTER CHECK A DALR. THE FUSELAGE SKIN WAS FOUND CRACKED AT THE LOWER RIGHT SIDE OF THE FS 983 PRESSURE BULKHEAD UNDER THE FUSELAGE-TO-WING BOX LONGERON. THE SKIN WAS FOUND WITH A 1.5 INCH LONG CRACK IN THE SECOND FASTENER ROW FORWARD OF THE BULSDR DALR950010Doubler · crackedATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 FUSELAGE NLG WHEELWELL MOD. FS 328 PER DL EO.7-53207-3AD. AN ADDITIONAL CRACK WAS FOUND THAT WAS BEYOND THE SCOPE OF THE E.O. THE CRACK LIES IN THE SKIN DOUBLER AT THE FORWARD LEFT CORNER OF THE SDR DALR950009Longeron · corrodedATL - DURING LETTER CHECK AT DALR. CONSIDERABLE CORROSION WAS FOUND AT FS 328 ON THE VERTICAL FLANGE OF THE LBL 22 NLG WHEELWELL SIDEWALL LOWER LONGERON. A NEW SECTION OF LONGERON WAS SPLICED IN PER DL ERA 270527-14. TT, 38155 HRS. CYCLES, 18905. (X)
Back to N311EA, cancelled Feb 23, 2004