N314NE, cancelled Feb 26, 2004

Service difficulty reports · 82

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 = 'N314NE' AND deregistration_id = 'N314NE-2004-02-26'
  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 EISA20010109Engine · inoperativeJUST AFTER ROTATION, SEVERAL COMPRESSOR STALLS WERE HEARD. GAUGES FOR #1 ENGINE SHOWED SOME FLUCTUATION; ENG. FAIL LIGHT FLASHED. ACCOMPANIED BY AUTO PACK TRIP. AIR TURN BACK TO INDIANAPOLIS.CORRECTIVE ACTION:INSP. INLET AND EXHAUST, NO DAMAGE NOTED, R/R PRBCJul 26, 2001 · N314NE · Boeing 727223 · Compressor Bleed ControlSDR EISA20010104Light · inoperativeDURING APPROACH NOSE GEAR DOWN AND LOCKED LIGHT INOP. WOULD NOT PRESS TO TEST. RELAMPED BULB.Jul 6, 2001 · N314NE · Boeing 727223 · Landing Gear Position and WarningSDR EISA20010021Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SEAT TRACK AT RBL 45.50 BS 700. REMOVED CORRODED SECTION, FABRICATED SEAT TRACK LOCATED HOLES, ALODINED, PRIMED, AND INSTALLED SEAT TRACK SPLICE IAW SRM 51-10-2, 51-10-6, 53-10-1, 51-10-5 FIG 1, 53-10-2 FIGFeb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA20010020Angle · crackedDURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED IN LEFT WING LEADING EDGE OF NR 3 KRUEGER FLAP. REMOVED ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE, ALODINED AND PRIMED IAW SRM 51-40-3 FIG 1, 51-30-2.Feb 2, 2001 · N314NE · Boeing 727223 · Leading Edge DevicesSDR EISA20010019Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SCREW HEADS ON SEAT TRACK RBL 24.50 FROM BS 480 TO BS 680. REMOVED SEAT TRACK, FABRICATED, TRIMMED, DRILLED, ALODINED, PRIMED, AND INSTALLED SEAT TRACK SPLICE, AT RBL 24.50 FROM BS 480 TO BS 680 IAW SRM 53-Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA20010018Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AROUND SCREW HEADS ON SEAT TRACK LBL 24.50 FROM BS 640 TO BS 720. REMOVED CORRODED SEAT TRACK FABRICATED, TRIMMED, DRILLED, ALODINED, PRIMED, AND INSTALLED, SEAT TRACK SPLICE IAW SRM 53-10-1, 53-10-5 FIG 7, 51Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA20010017Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AROUND FASTENER HEADS ON SEAT TRACK FROM BS 480 TO BS 580. REMOVED CORRODED SEAT TRACK SECTION, FABRICATED SEAT TRACK, SPLICE DRILLED, DEBURRED, COUNTER SUNK, ALODINED, PRIMED, AND INSTALLED SEAT TRACK SPLICE Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA20010016Skin · crackedDURING ROUTINE C-CHECK FOUND SEVERAL CRACK INDICATIONS ON EXTERNAL SKIN AND DOUBLER AT MAIN CARGO DOOR. STEP REAMED HOLES, FABRICATED FREEZE PLUG BUSHINGS, AND RADIUS FILLER, ALODINED, PRIMED, AND INSTALLED IAW FVC DRAWING 53-0066-1, ATLANTA ACO APPROVAL LETTFeb 2, 2001 · N314NE · Boeing 727223 · Cargo/Baggage DoorsSDR EISA20010015Mount Bracket · damagedDURING ROUTINE C-CHECK INSPECTION FOUND NR 3 ENGINE AFT MOUNT LOWER FLANGE HAS ELONGATED HOLES. FABRICATED FREEZE PLUGS, STAP, ALODINED, PRIMED, AND INSTALLED REPAIR IAW EOI-DAL-00-0081H, AND SRM 51-10-2, 51-30-2.Feb 2, 2001 · N314NE · Boeing 727223 · Engine Mount SectionSDR EISA20010014Frame · puncturedDURING ROUTINE C-CHECK INSPECTION FOUND AFT UPPER CORNER AFT CARGO DOOR HAS HOLE IN FRAME. REMOVED AND REPLACED CORNER BRACE IAW SRM 51-20-4, 51-30-2.Feb 2, 2001 · N314NE · Boeing 727223 · Cargo/Baggage DoorsSDR EISA20010013Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON SEAT TRACK FROM BS 580 TO BS 620 LBL 45.50. REMOVED CORRODED SEAT TRACK, FABRICATED TRACK SPLICE, DRILLED DEBURRED, COUNTERSUNK, ALODINED, PRIMED, AND INSTALLED IAW 53-10-1, 53-10-5 FIG 7, 51-10-2, AND 51-3Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA20010012Skin · crackedDURING ROUTINE C-CHECK INSPECTION FOUND SKIN CRACKED ON LEFT WING ABOVE NR 4 SLAT. ROUTED OUT CRACK, FABRICATED REPAIR DOUBLER, PRIMED, ALODINED, AND INSTALLED DOUBLER IAW SRM 57-30-4, 51-10-2, 51-30-2.Feb 2, 2001 · N314NE · Boeing 727223 · Wing, Plate/SkinSDR EISA20010011Attach Fitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACKS AT TOP OF LEFT WING AT NR 2, 3, AND 4 SPOILER ATTACH POINTS. STOP DRILLED CRACKS, FABRICATED, INSTALLED, ALODINED, AND PRIMED REPAIR DOUBLERS, IAW SRM 51-10-2, 51-30-4 FIG 10, AND 51-30-2.Feb 2, 2001 · N314NE · Boeing 727223 · Wing, Control Surface Attach FittingsSDR EISA20010010Skin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND HOLE IN LT ELEVATOR TAB UPPER SURFACE. CLEANED PREPPED AND POTTED .250 DIAMETER AREA, ALODINED, PRIMED, AND PAINTED. WEIGHT AND BALANCE IAW SRM 51-40-6 FIG 35, 51-10-2, 51-80-9 PG 1, 51-80 FIG 2, AND M/M 27-30-1.Feb 2, 2001 · N314NE · Boeing 727223 · Elevator, Tab StructureSDR EISA20010009Skin · delaminatedDURING ROUTINE C-CHECK INSPECTION FOUND NR 4 AFT FLAP TRAILING EDGE DELAMINATED. REMOVED DELAMINATED AREAS OF FLAP TRAILING EDGE, CLEANED, PREPPED, ALODINED, PRIMED, AND BONDED FIBERGLASS OVERLAYS IAW SRM 51-10-2, 57-50-1 FIG 3, 51-40-6 FIG 37.Feb 2, 2001 · N314NE · Boeing 727223 · Trailing Edge FlapsSDR EISA20010008Frame · crackedDURING ROUTINE C-CHECK INSPECTION FOUND BS 620 FRAME WEB HAS CRACK STARTING AT LOWER TOOLING HOLE AND EXTENDING DOWN THROUGH FASTENER HOLE. CORRECTIVE ACTION: FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER IAW SRM 51-10-2, 51-30-2, 51Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Main, FrameSDR EISA20010007Frame · damagedDURING ROUTINE C-CHECK INSPECTION FOUND ELONGATED HOLE AT BS 870. REAMED HOLE PER SB 53-0194 TO 402.Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Main, FrameSDR EISA20010006Support Fitting · damagedDURING ROUTINE C-CHECK INSPECTION FOUND OUTBOARD TRACK SUPPORT HAS ELONGATED HOLE. REAMED FITTING IAW SB 57-0134, ALODINED AND PRIMED IAW SRM 51-10-2.Feb 2, 2001 · N314NE · Boeing 727223 · Wing, Control Surface Attach FittingsSDR EISA20010005Former · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT NR 4 SLAT ACTUATOR INBOARD FORMER. STOP DRILLED CRACK, FABRICATED, REPAIR DOUBLER, ALODINED, PRIMED, AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3, 51-30-2, 51-10-2.Feb 2, 2001 · N314NE · Boeing 727223 · Leading Edge DevicesSDR EISA20010004Stiffener · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND CRACK AT NR 2 SLAT ACTUATOR STIFFENER. REMOVED CRACKED STIFFENER, FABRICATED STIFFENER, DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-2, 51-10-2, SB 57-0130, BSOPM 20-42-02.Feb 2, 2001 · N314NE · Boeing 727223 · Leading Edge Slat ActuatorSDR EISA200120025Frame · crackedDURING ROUTINE C-CHECK, INSPECTION FOUND CRACK AT BS 298 RBL 14. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-10-1 PARA 9, 51-40-3 FIG 1, 51-10-2, 51-30-2, M/M 20-10-20.Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Main, FrameSDR EISA20010024Angle · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACKED ANGLE UNDER FLOOR PANEL AT BS 300 RBL 10. REMOVED ANGLE, FABRICATED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLE IAW SRM 51-30-2, 51-10-6, 51-40-4.Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA20010023Frame · damagedDURING ROUTINE C-CHECK INSPECTION FOUND HOLE IN FRAME AT STRINGER 17L. FABRICATED REPAIR DOUBLER, ALODINED, REPAIRED, AND INSTALLED REPAIR IAW SRM 51-30-2, 51-10-2, 53-10-4 FIG 1.Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Main, FrameSDR EISA20010022Angle · crackedDURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED AT STATION 92L WING ROOT. FABRICATED REPAIR ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLE IAW SRM 51-30-2, 51-10-2, 51-40-3 FIG 1.Feb 2, 2001 · N314NE · Boeing 727223 · Wing Miscellaneous StructureSDR EISA2000054Brake · damagedFLT 746 - SAT - DURING TAXI OUT, BRAKES LOCKED AND AIRCRAFT CAME TO A STOP. NO ACTION WOULD RELEASE BRAKES. SERVICED DE-BOOST CYL AND CHANGED NR 1 BRAKE ASSY AND TIRE ASSY. (M)Jun 9, 2000 · N314NE · Boeing 727223 · Landing Gear Brake SystemSDR EISA2000016Engine · leakingNR 2 ENGINE OIL LOSS IN FLIGHT. PRECAUTIONARY SHUTDOWN OF ENGINE. (M)Feb 15, 2000 · N314NE · Boeing 727223 · Turbine Engine Oil SystemSDR EISA2000030O-Ring · wornNR 2 ENGINE LOSING 1 QUART OF OIL EVERY 5-7 MINUTES. IN FLIGHT SHUT DOWN NR 2 ENGINE. REMOVED AND REPLACED O-RING ON OIL LINE FROM ENGINE OIL BYPASS SWITCH TO OIL PUMP. LEAK CHECKS GOOD IAW MM 79-2-0. (M)Feb 11, 2000 · N314NE · Boeing 727223 · Engine Oil Distribution (Airframe Furnished)SDR EISA99081Skin · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND 5 INCH CRACK ON RIGHT WING LEADING EDGE AT WS 456 ABOVE FUELING BAY. TRIMMED OUT DAMAGED AREA PER SRM 57-30-4. FABRICATED FILLER AND DOUBLER PER SRM 57-30-4. INSTALLED REPAIR PER SRM 57-30-4 AND 51-3Mar 27, 1999 · N314NE · Boeing 727223 · Wing, Plate/SkinSDR EISA99080Seat Track · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND LEFT OUTBOARD SEAT TRACK CRACKED AT BS 620-720. REMOVED DAMAGED SEAT TRACK FROM BS 620-720. FABRICATED NEW SEAT TRACK FROM 60-13201 EXTRUSION PER SAMPLE AND INSTALLED PER SRM 51-30-2. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA99079Seat Track · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND RIGHT OUTBOARD SEAT TRACK CRACKED AT BS 520. REMOVED DAMAGED SEAT TRACK FROM BS 480-580. FABRICATED NEW SEAT TRACK FROM 60-13201 PER SAMPLE AND INSTALLED PER SRM 51-30-2. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA99078Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND INBOARD RIB AND RIB ATTACH ANGLE AT NR 1 SLAT ACTUATOR ATTACH POINT CRACKED. REMOVED AND REPLACED SLAT WITH A SERVICEABLE UNIT PER MM 27-81-11. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Leading Edge DevicesSDR EISA99077Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND NR 4 SLAT OUTBOARD SUPPORT RIB CRACKED. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Trailing Edge FlapsSDR EISA99076Tie Clip · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND STRINGER TIE CRACKED AT BS 675, 527L. REMOVED DAMAGED PART, FABRICATED AND INSTALLED NEW STRINGER TIE PER SRM 53-10-3. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA99075Angle · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SUPPORT ANGLE CRACKED AT FS 720B, 525L. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-3 AND 53-10-4. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA99074Stiffener · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACKED STIFFENER ON FORWARD SIDE OF NR 2 ENGINE FIREWALL AT BS 1342.4, PREVIOUS REPAIR. REMOVED OLD REPAIR, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-40-3. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA99073Frame · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND FRAME CRACKED AND DEFORMED AT BS 440, WL 210. TRIMMED DAMAGED SECTION PER SRM 51-40-3. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage Main, FrameSDR EISA99072Exit Case · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED RIGHT SIDE AT 2 O'CLOCK POSITION. REMOVED AND REPLACED FAN EXIT CASE PER 727 OVERHAUL MANUAL 72-00-34. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Turbine Engine Bypass SectionSDR EISA99071Exit Case · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED AROUND STATOR ON LEFT SIDE AT 9 O'CLOCK POSITION JUST ABOVE CASE LINE. REMOVED AND REPLACED FAN EXIT CASE PER 727 OVERHAUL MANUAL 72-00-34. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Turbine Engine Bypass SectionSDR EISA99070Support · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACK AT NR 13 SPOILER ACTUATOR INBOARD SUPPORT ANGLE ON REAR SPAR. REMOVED CRACKED SUPPORT AND FABRICATED NEW PAR PER SRM 51-10-1. INSTALLED SUPPORT PER SRM 51-10-1 AND 51-30-2. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Drag Control ActuatorSDR EISA99068Skin · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND A 2.5 INCH CRACK IN SKIN ON LEFT ELEVATOR LOWER SURFACE, 20 INCH AFT OF PANEL NR 9308. STOP DRILLED CRACK PER SRM 55-20-3. FABRICATED AND INSTALLED DOUBLER PER SRM 55-20-3. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Elevator, Plate/SkinSDR EISA99067Skin · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SKIN CRACKED ON NR 1 SLAT TRAINING EDGE AREA OUTBOARD SIDE AT OUTBOARD TRACK. REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER PER SRM 57-50-3. INSTALLED REPAIR PER SRM 57-50-3 AND 51-30-2. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Leading Edge DevicesSDR EISA99066Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND INBOARD RIB AND RIB ATTACH ANGLE CRACKED AT NR 1 SLAT ACTUATOR. REMOVED AND REPLACED SLAT WITH A SERVICEABLE UNIT PER MM 27-81-11. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Leading Edge DevicesSDR EISA99065Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND NR 4 SLAT OUTBOARD SUPPORT CRACKED. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3. (M)Mar 27, 1999 · N314NE · Boeing 727223 · Leading Edge DevicesSDR EISA99064Case · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED AROUND STATOR ON LEFT SIDE AT 9 O'CLOCK POSITION AND RIGHT SIDE AT 2 O'CLOCK POSITION JUST ABOVE CASE SPLIT LINE. REMOVED AND REPLACED FAN EXIT CASE PER 727 OVERHAUL MAMar 27, 1999 · N314NE · Boeing 727223 · Turbine Engine Bypass SectionSDR EISA98182Fire Loop · failedON PRE-FLIGHT, FOUND NR 1 ENGINE FIRE LIGHT WOULD NOT ILLUMINATE WHEN TESTED. FIRE BELL WORKED OK. GENERATED FROM PILOT REPORT. CORRECTIVE ACTION: REMOVED AND REPLACED NR 1 ENGINE FIRE LOO PER MM CHAPPTER 26-11-12. OPS CHECK GOOD. (X)Jul 23, 1998 · N314NE · Boeing 727223 · Fire DetectionSDR EISA98167Strut · overheatAT 1,000 FEET, AGL ON REDUCED POWER TAKEOFF OUT OF DFW, AIRCRAFT INDICATED NR 1 STRUT OVERHEAT. LIGHT EXTINGUISHED 2 MINUTES AFTER THROTTLE RETARDED. GENERATED FROM PILOT REPORT. REMOVED NR 1 STRUT PANELS AND INSPECTED. NO DEFECTS NOTED. ALSO, TIGHTENED SJul 7, 1998 · N314NE · Boeing 727223 · Smoke DetectionSDR EISA97280Switch · malfunctionedTAKEOFF, AURAL WARNING SOUNDS AT ALL TIMES. REMOVED AND REPLACED UPPER STABILIZER TRIM SWITCH. (X)Dec 13, 1997 · N314NE · Boeing 727223 · Stabilizer Position IndicatingSDR EISA97167Connector · looseON CLIMB-OUT LAX, NR 2 ENGINE OIL TEMP EXCEEDED THE RED LINE. ACCOMPLISHED ABNORMAL HIGH ENGINE OIL TEMP CHECKLIST, PERFORMED ENGINE FAILURE/FIRE/DAMAGE CHECKLIST NR 2 ENGINE. FOUND OIL TEMP XMITTER CANNON PLUG LOOSE, RECONNECTED PLUG. (M)Jul 26, 1997 · N314NE · Boeing 727223 · Engine Oil TemperatureSDR EISA96283Adc · inoperativeF/O'S AIRSPEED AND ALTIMETER INTERMITTENTLY INOP. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. OPS CHECK NORMAL. (M)Dec 13, 1996 · N314NE · Boeing 727223 · Air Data ComputerSDR EISA96284Clip · crackedDURING A SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS AT VARIOUS STATIONS CRACKED FROM BS 560 TO 1050. REPLACED CLIPS PER SRM 51-10-1 AND 51-30-2. (M)Nov 1, 1996 · N314NE · Boeing 727223 · Fuselage Miscellaneous Structure
Back to N314NE, cancelled Feb 26, 2004