N700UW

Service difficulty reports · 298

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 = 'N700UW' AND registry_match = 'registration'
  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.

SDR AALA202112277053Thrust Reverser · fault messageAIRCRAFT WAS GROUNDED: #2 ENGINE THRUST REVERSER UNLOCK EICAS DURING TAKEOFF POWER APPLICATION, LOW SPEED REJECT LESS THAN 40 KNOTS IAS. MAINTENANCE PERFORMED. TSM 78-3100-810-864-A THRUST REVERSER INDICATION FAILURE. FOUND ALL BLOCKER DOORS FLUSH WITH FAN CODec 25, 2021 · N700UW · Airbus A319112 · Engine Thrust ReverserSDR AALA202110283560Switch · dirtyAIRCRAFT WAS NOT GROUNDED: DOOR 1R INDICATES OPEN WHEN CLOSED. REMOVED DEBRIS FROM DOOR SWITCH, CLEANED SURROUNDING AREA, AND ACCOMPLISHED DOOR INDICATION DISAGREE TEST IAW TSM 52-11-00, OPS CHECK GOOD.Oct 25, 2021 · N700UW · Airbus A319112 · Door Warning SystemSDR AALA202106219015Sliding Window · out of adjustAIRCRAFT WAS NOT GROUNDED: FIRST OFFICER WINDOW STUCK IN OPEN POSITION. ADJUSTED SLIDING WINDOW AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 56-12-11.Jun 20, 2021 · N700UW · Airbus A319112 · Flight Compartment WindowsSDR AALA202106189011Engine · stalledAIRCRAFT WAS GROUNDED: AT THE TOP OF DECENT INTO PHL THE LEFT ENGINE EXPERIENCED A ROLL BACK STALL WITH A SLIGHT DIP IN N1 RPM. THE ENGINE DID NOT SHUT DOWN BUT FAILED TO RECOVER QUICKLY SO THE PILOT PULLED THE THROTTLE BACK MANUALLY AND THE ENGINE RECOVERED SJun 16, 2021 · N700UW · Airbus A319112 · Engine (Turbine/Turboprop)SDR AALA202106149003Torque Shaft · defectiveAIRCRAFT WAS GROUNDED: FLIGHT CONTROL FLAPS LOCKED - WING TIP BRAKE ON. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BOS WHERE IT LAND SAFELY WITHOUT FURTHER INCIDENT. REPLACED TORQUE SHAFT 6254CM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PERJun 13, 2021 · N700UW · Airbus A319112 · Trailing Edge Flap Control SystemSDR AALA202106079025Sensor · defectiveAIRCRAFT WAS GROUNDED: #1 ENGINE STALL AT FL340 AFTER LEVEL OFF. ACCOMPLISHED QRH PROCEDURE AND ALL SYSTEMS NORMAL AND FLIGHT CONTINUED DFW WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED T12 (AALA202106039008) AND T25 (AALA202106079025) SENSORS PER May 31, 2021 · N700UW · Airbus A319112 · Engine Indicating SystemSDR AALA202106039008Sensor · defectiveAIRCRAFT WAS GROUNDED: #1 ENGINE STALL AT FL340 AFTER LEVEL OFF. ACCOMPLISHED QRH PROCEDURE AND ALL SYSTEMS NORMAL AND FLIGHT CONTINUED DFW WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT: REPLACED T12 (AALA202106039008) AND T25 (AALA202May 31, 2021 · N700UW · Airbus A319112 · Engine (Turbine/Turboprop)SDR AALA202104069002Warning Message · false activationAIRCRAFT WAS NOT GROUNDED: AUXILIARY POWER UNIT DISCHARGE LIGHT ILLUMINATED ON AUXILIARY POWER UNIT FIRE PANEL. REMOVED AND REPLACED AUXILIARY POWER UNIT FIRE BOTTLE PER AMM 26-22-41.Apr 5, 2021 · N700UW · Airbus A319112 · Extinguishing SystemSDR AALA202103319010Slide · no testAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 SLIDE RAFT DOES NOT PASS THE LIGHT TEST. REPLACED SLIDE PER AMM 25-62-44-400-007-A.Mar 30, 2021 · N700UW · Airbus A319112 · Escape SlideSDR AALA202103319009Slide · no testAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 SLIDE RAFT DOES NOT PASS THE LIGHT TEST. REPLACED SLIDE PER AMM 25-62-44-400-803-A.Mar 30, 2021 · N700UW · Airbus A319112 · Escape SlideSDR AALA202103319008Slide · no testAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DOES NOT PASS THE LIGHT TEST. REPLACED SLIDE PER AMM 25-62-44-400-007-A.Mar 30, 2021 · N700UW · Airbus A319112 · Escape SlideSDR AALA202103319007Power Supply · no testAIRCRAFT IN BASE MAINTENANCE: IWHILE PERFORMING A TEST OF THE EMERGENCY LIGHTING SYSTEM FAULT MESSAGE FOR INT LOAD FAULT AT EPSU AFT L (13WL) OCCURRED. REPLACED POWER SUPPLY 13WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38-400-001-A.Mar 30, 2021 · N700UW · Airbus A319112 · Emergency LightingSDR AALA202103319006Power Supply · no testAIRCRAFT IN BASE MAINTENANCE: DONT PASS OPERATIONAL TEST EMERGENCY LIGHTING SYSTEM DUE TO SHOWTHE MESSAGE INT AND EXT LOAD ON ESPU FWD L IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT 11WL, PASSENGER / CREW DOORS 831 SLIDE RAFT (AALA202103319008) ANDMar 30, 2021 · N700UW · Airbus A319112 · Emergency LightingSDR AALA202103229010Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND L= 0.122 INCH CRACK ON RIGHT FITTING AT FR1 AND Y0. PERFORMED REPAIR, REPLACING CONTINUITY FITTING RIGHT LOCATED ON FRAME 1 TO FRAME 2 AND LEVEL OF Y0 IAW EA# 311074.Mar 19, 2021 · N700UW · Airbus A319112 · Fuselage Main, StructureSDR AALA202103229011Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND L= 0.082 INCH CRACK ON RIGHT CENTER WINDSHIELD FRAME AT FR2 AND Y0. PERFORMED REPAIR ON WINDOW CENTER POST RIGHT FROM LOWER INBOARD RADIUS AT LOWER ATTACHMENT INTERNAL AREA SIDE IN COCKPIT IAW EA 311073.Mar 18, 2021 · N700UW · Airbus A319112 · Fuselage Main, StructureSDR AALA202103189009Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL #2 AT THE REAR SPAR AND RIB 7. REPAIRED SKIN PANEL PER EA 325539.Mar 17, 2021 · N700UW · Airbus A319112 · Wing, Plate/SkinSDR AALA202103189001Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING HAS ELONGATED HOLE / WORN. REPLACED HINGE FITTING PER CMM 52-81-18-400-809-A01.Mar 17, 2021 · N700UW · Airbus A319112 · Landing Gear DoorsSDR AALA202103159016Skin · wornAIRCRAFT IN BASE MAINTENANCE: WORN SKIN PANEL AT FR25 BETWEEN S42L AND S43L. REPAIRED PANEL PER SRM 53-00-11-300-029.Mar 14, 2021 · N700UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR AALA202103159011Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR HINGE FITTING #3 HAS OVERSIZED HOLES ON BOTH LUGHS. REPLACED ELEVATOR PER AMM 27-34-41-400-001.Mar 12, 2021 · N700UW · Airbus A319112 · Elevator StructureSDR AALA202103099007Hinge Fitting · looseAIRCRAFT IN BASE MAINTENANCE: LOOSE BEARING HINGE INBOARD THRUST REVERSER, UPPER ATTACHMENT ON ENGINE 2. REPLACED THRUST REVERSER COWL FITTING ON RIGHTHAND PYLON PER AMM 54-57-17-000-003-A.Mar 8, 2021 · N700UW · Airbus A319112 · Engine Thrust ReverserSDR AALA202102249001Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SUPPORT ANGLE PRESSURE BULKHEAD FR 46 AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE PRESSURE BRACKET AND FASTENERS LOCATED BULKHEAD FR46 AFT CARGO COMPARTMENT IAW A319 SRM 51-72-11-911-001 AND DWG D93570727.Feb 23, 2021 · N700UW · Airbus A319112 · Fuselage Main, BulkheadSDR AALA202102239008Support Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT SUPPORT ANGLE CORRODED. LOCATED AT DOOR CUT OUT BETWEEN FRAME 55A AND FRAME 56. REPLACED SUPPORT ANGLE PER SRM 51-42-11-801 AND DWG D53477100.Feb 22, 2021 · N700UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202102229007Attach Bolt · corrodedAIRCRAT IN BASE MAINTENANCE: CORROSION ON LEFT WING SLAT TRACK #1 MID AFT ATTACHMENT BOLT. REPLACED BOLT PER 26C51057005.Feb 21, 2021 · N700UW · Airbus A319112 · Leading Edge DevicesSDR AALA202102229006Attach Bolt · corrodedAIRCRAT IN BASE MAINTENANCE: CORROSION ON LEFT WING SLAT TRACK #11 LOWER ATTACHMENT BOLT. REPLACED BOLT PER 26C51057005.Feb 21, 2021 · N700UW · Airbus A319112 · Leading Edge DevicesSDR AALA202102189005Slide · deformedAIRCRAFT IN BASE MAINTENANCE: DEFORMATION ESCAPE SLIDE COMPARTMENT ASSEMBLY OF 841 DOOR IN PASSENGER CABIN (1 EA). REPLACED ESCAPE SLIDE ASSEMBLY ON DOOR 841 AT FORWARD GALLEY AREA.Feb 17, 2021 · N700UW · Airbus A319112 · Escape SlideSDR AALA202102149005Support Fitting · migratedAIRCRAFT IN BASE MAINTENANCE: FOUND MIGRATED PASSENGER CREW DOOR 842 HINGE ARM UPPER SUPPORT FITTING BEARING IN PASSENGER CABIN. REPLACED PASSENGER CREW DOOR 842 HINGE ARM UPPER SUPPORT FITTING IN PASSENGER CABIN IAW AMM 52-13-31-400-002-A STEP 4.F.Feb 13, 2021 · N700UW · Airbus A319112 · Passenger/Crew DoorsSDR AALA202102159033Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING SLAT TRACK #12 LOWER FORWARD ATTACHMENT BOLT. REPLACED BOLT PER TASK CARD 26C5005705.Feb 12, 2021 · N700UW · Airbus A319112 · Leading Edge DevicesSDR AALA202103159015Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LATERAL WINDSHIELD FRAME CRACKED. REPAIRED WINDOW FRAME PER ENGINEERING AUTHORIZATION 311076.Jan 31, 2021 · N700UW · Airbus A319112 · Fuselage Main, StructureSDR AALA202103159014Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LATERAL WINDSHIELD FRAME CRACKED. REPAIRED WINDOW FRAME PER ENGINEERING AUTHORIZATION 311075.Jan 31, 2021 · N700UW · Airbus A319112 · Fuselage Main, StructureSDR AALA202103169002Frame · crackedAIRCRAFT WAS GROUNDED: CRACK FOUND ON FRAME 43 RH BETWEEN STR 21R AND STR 22R IN PASSENGER CABIN, L=0.096. REPLACED FRAME 43 RH BETWEEN STR 21R AND STR 22R IN PASSENGER CABIN.Jan 29, 2021 · N700UW · Airbus A319112 · Fuselage Main, FrameSDR AALA202103044088Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 65 AND S26R. REPLACED STRINGER PER SRM 51-72-11.Jan 28, 2021 · N700UW · Airbus A319112 · Fuselage Main, Longeron/StringerSDR AALA202102269001Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231YG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV I.Jan 27, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202102109011Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: FOUND DELAMINATED FLOOR PANEL 241EF AT FR36 AND BL Y254, MEASURING L= 10 INCHES W= 3 INCHES. REMOVED AND REPLACED FLOOR PANEL REF A319 SRM 53-02-00-300-011 AND IRM 9701 REV I.Jan 27, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202102109009Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231WG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.Jan 27, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202102109008Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231MF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.Jan 27, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202102099011Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON FLOOR BEAM BETWEEN FR68 AND FR69 AT AFT GALLEY AREA. L=1.464 BY W=0.727 BY D=0.061 INCHES CORRODED AREA. REPLACED FLOOR BEAM -Y1162.5 BETWEEN FR68 TO FR69 AT AFT GALLEY AREA PER SRM 51-42-11-801.Jan 27, 2021 · N700UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202102089008Dummy Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: RAIL DUMMY AT FR 16 FORWARD GALLEY AREA CORROSION MEASURING L=0.466 INCHES W=0.340 INCHES D=0.059 INCHES. REPLACED RAIL DUMMY PER SRM 51-72-11-911-001 AND DWG # 53112825..Jan 27, 2021 · N700UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202103229018Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL #2 AT THE FRONT SPAR AND RIB 20. REPAIRED SKIN PANEL PER EA 325539.Jan 26, 2021 · N700UW · Airbus A319112 · Wing, Plate/SkinSDR AALA202103229014Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL #2 AT THE REAR SPAR AND RIB 13. REPAIRED SKIN PANEL PER EA 325539.Jan 26, 2021 · N700UW · Airbus A319112 · Wing, Plate/SkinSDR AALA202103029024Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 261PF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV I.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029023Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 261AG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV I.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029022Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231CF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV I.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029021Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 261DF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV I.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029020Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231EF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV I.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029019Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 221DF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV I.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029017Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATED/DISBONDED AREA FOUND ON FLOOR PANEL 251LF, L= 20 IN, W= 2.5 IN. REMOVED AND REPLACED FLOOR PANEL 251LF PER SRM 53-02-00-300-011.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029018Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATED/DISBONDED AREA FOUND ON FLOOR PANEL 261BG, L= 19 IN, W= 10.50 IN. REMOVED AND REPLACED FLOOR PANEL 261BG PER SRM 53-02-00-300-011.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029016Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATED/DISBONDED AREA FOUND ON FLOOR PANEL 251FF, L= 8 IN, W = 3.5 IN. REMOVED AND REPLACED FLOOR PANEL 251FF PER SRM 53-02-00-300-011.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029015Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATED/DISBONDED AREA ON FLOOR PANEL 252FG, L= 18 IN, W= 3 IN. REMOVED AND REPLACED FLOOR PANEL 252FG PERSRM 53-02-00-300-011.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor PanelSDR AALA202103029014Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATED/DISBONDED AREA ON FLOOR PANEL 232AH, L= 11 IN, W= 10 IN. REMOVED AND REPLACED FLOOR PANEL 232AH PER SRM 53-02-00-300-011.Jan 25, 2021 · N700UW · Airbus A319112 · Fuselage Floor Panel
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