# Service difficulty reports: N314NE, cancelled Feb 26, 2004 A list on [N314NE, cancelled Feb 26, 2004](https://openairdocs.org/deregistered/N314NE-2004-02-26.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 82 reports - [SDR EISA20010109](https://openairdocs.org/sdr/EISA20010109.md): Engine · inoperative · Jul 26, 2001 · N314NE · Boeing 727223 · Compressor Bleed Control > JUST 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 PRBC - [SDR EISA20010104](https://openairdocs.org/sdr/EISA20010104.md): Light · inoperative · Jul 6, 2001 · N314NE · Boeing 727223 · Landing Gear Position and Warning > DURING APPROACH NOSE GEAR DOWN AND LOCKED LIGHT INOP. WOULD NOT PRESS TO TEST. RELAMPED BULB. - [SDR EISA20010021](https://openairdocs.org/sdr/EISA20010021.md): Seat Track · corroded · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings > DURING 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 FIG - [SDR EISA20010020](https://openairdocs.org/sdr/EISA20010020.md): Angle · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Leading Edge Devices > DURING 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. - [SDR EISA20010019](https://openairdocs.org/sdr/EISA20010019.md): Seat Track · corroded · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings > DURING 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- - [SDR EISA20010018](https://openairdocs.org/sdr/EISA20010018.md): Seat Track · corroded · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings > DURING 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, 51 - [SDR EISA20010017](https://openairdocs.org/sdr/EISA20010017.md): Seat Track · corroded · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings > DURING 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 - [SDR EISA20010016](https://openairdocs.org/sdr/EISA20010016.md): Skin · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Cargo/Baggage Doors > DURING 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 LETT - [SDR EISA20010015](https://openairdocs.org/sdr/EISA20010015.md): Mount Bracket · damaged · Feb 2, 2001 · N314NE · Boeing 727223 · Engine Mount Section > DURING 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. - [SDR EISA20010014](https://openairdocs.org/sdr/EISA20010014.md): Frame · punctured · Feb 2, 2001 · N314NE · Boeing 727223 · Cargo/Baggage Doors > DURING 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. - [SDR EISA20010013](https://openairdocs.org/sdr/EISA20010013.md): Seat Track · corroded · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings > DURING 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 51-3 - [SDR EISA20010012](https://openairdocs.org/sdr/EISA20010012.md): Skin · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Wing, Plate/Skin > DURING 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. - [SDR EISA20010011](https://openairdocs.org/sdr/EISA20010011.md): Attach Fitting · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Wing, Control Surface Attach Fittings > DURING 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. - [SDR EISA20010010](https://openairdocs.org/sdr/EISA20010010.md): Skin · damaged · Feb 2, 2001 · N314NE · Boeing 727223 · Elevator, Tab Structure > DURING 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. - [SDR EISA20010009](https://openairdocs.org/sdr/EISA20010009.md): Skin · delaminated · Feb 2, 2001 · N314NE · Boeing 727223 · Trailing Edge Flaps > DURING 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. - [SDR EISA20010008](https://openairdocs.org/sdr/EISA20010008.md): Frame · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Main, Frame > DURING 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, 51 - [SDR EISA20010007](https://openairdocs.org/sdr/EISA20010007.md): Frame · damaged · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Main, Frame > DURING ROUTINE C-CHECK INSPECTION FOUND ELONGATED HOLE AT BS 870. REAMED HOLE PER SB 53-0194 TO 402. - [SDR EISA20010006](https://openairdocs.org/sdr/EISA20010006.md): Support Fitting · damaged · Feb 2, 2001 · N314NE · Boeing 727223 · Wing, Control Surface Attach Fittings > DURING 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. - [SDR EISA20010005](https://openairdocs.org/sdr/EISA20010005.md): Former · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Leading Edge Devices > DURING 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. - [SDR EISA20010004](https://openairdocs.org/sdr/EISA20010004.md): Stiffener · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Leading Edge Slat Actuator > DURING 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. - [SDR EISA200120025](https://openairdocs.org/sdr/EISA200120025.md): Frame · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Main, Frame > DURING 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. - [SDR EISA20010024](https://openairdocs.org/sdr/EISA20010024.md): Angle · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Miscellaneous Structure > DURING 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. - [SDR EISA20010023](https://openairdocs.org/sdr/EISA20010023.md): Frame · damaged · Feb 2, 2001 · N314NE · Boeing 727223 · Fuselage Main, Frame > DURING 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. - [SDR EISA20010022](https://openairdocs.org/sdr/EISA20010022.md): Angle · cracked · Feb 2, 2001 · N314NE · Boeing 727223 · Wing Miscellaneous Structure > DURING 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. - [SDR EISA2000054](https://openairdocs.org/sdr/EISA2000054.md): Brake · damaged · Jun 9, 2000 · N314NE · Boeing 727223 · Landing Gear Brake System > FLT 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) - [SDR EISA2000016](https://openairdocs.org/sdr/EISA2000016.md): Engine · leaking · Feb 15, 2000 · N314NE · Boeing 727223 · Turbine Engine Oil System > NR 2 ENGINE OIL LOSS IN FLIGHT. PRECAUTIONARY SHUTDOWN OF ENGINE. (M) - [SDR EISA2000030](https://openairdocs.org/sdr/EISA2000030.md): O-Ring · worn · Feb 11, 2000 · N314NE · Boeing 727223 · Engine Oil Distribution (Airframe Furnished) > NR 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) - [SDR EISA99081](https://openairdocs.org/sdr/EISA99081.md): Skin · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Wing, Plate/Skin > DURING 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 51-3 - [SDR EISA99080](https://openairdocs.org/sdr/EISA99080.md): Seat Track · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings > DURING 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) - [SDR EISA99079](https://openairdocs.org/sdr/EISA99079.md): Seat Track · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings > DURING 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) - [SDR EISA99078](https://openairdocs.org/sdr/EISA99078.md): Rib · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Leading Edge Devices > DURING 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) - [SDR EISA99077](https://openairdocs.org/sdr/EISA99077.md): Rib · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Trailing Edge Flaps > DURING 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) - [SDR EISA99076](https://openairdocs.org/sdr/EISA99076.md): Tie Clip · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage Miscellaneous Structure > DURING 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) - [SDR EISA99075](https://openairdocs.org/sdr/EISA99075.md): Angle · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage Miscellaneous Structure > DURING 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) - [SDR EISA99074](https://openairdocs.org/sdr/EISA99074.md): Stiffener · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage Miscellaneous Structure > DURING 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) - [SDR EISA99073](https://openairdocs.org/sdr/EISA99073.md): Frame · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Fuselage Main, Frame > DURING 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) - [SDR EISA99072](https://openairdocs.org/sdr/EISA99072.md): Exit Case · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Turbine Engine Bypass Section > DURING 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) - [SDR EISA99071](https://openairdocs.org/sdr/EISA99071.md): Exit Case · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Turbine Engine Bypass Section > DURING 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) - [SDR EISA99070](https://openairdocs.org/sdr/EISA99070.md): Support · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Drag Control Actuator > DURING 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) - [SDR EISA99068](https://openairdocs.org/sdr/EISA99068.md): Skin · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Elevator, Plate/Skin > DURING 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) - [SDR EISA99067](https://openairdocs.org/sdr/EISA99067.md): Skin · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Leading Edge Devices > DURING 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) - [SDR EISA99066](https://openairdocs.org/sdr/EISA99066.md): Rib · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Leading Edge Devices > DURING 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) - [SDR EISA99065](https://openairdocs.org/sdr/EISA99065.md): Rib · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Leading Edge Devices > DURING 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) - [SDR EISA99064](https://openairdocs.org/sdr/EISA99064.md): Case · cracked · Mar 27, 1999 · N314NE · Boeing 727223 · Turbine Engine Bypass Section > DURING 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 MA - [SDR EISA98182](https://openairdocs.org/sdr/EISA98182.md): Fire Loop · failed · Jul 23, 1998 · N314NE · Boeing 727223 · Fire Detection > ON 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) - [SDR EISA98167](https://openairdocs.org/sdr/EISA98167.md): Strut · overheat · Jul 7, 1998 · N314NE · Boeing 727223 · Smoke Detection > AT 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 S - [SDR EISA97280](https://openairdocs.org/sdr/EISA97280.md): Switch · malfunctioned · Dec 13, 1997 · N314NE · Boeing 727223 · Stabilizer Position Indicating > TAKEOFF, AURAL WARNING SOUNDS AT ALL TIMES. REMOVED AND REPLACED UPPER STABILIZER TRIM SWITCH. (X) - [SDR EISA97167](https://openairdocs.org/sdr/EISA97167.md): Connector · loose · Jul 26, 1997 · N314NE · Boeing 727223 · Engine Oil Temperature > ON 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) - [SDR EISA96283](https://openairdocs.org/sdr/EISA96283.md): Adc · inoperative · Dec 13, 1996 · N314NE · Boeing 727223 · Air Data Computer > F/O'S AIRSPEED AND ALTIMETER INTERMITTENTLY INOP. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. OPS CHECK NORMAL. (M) - [SDR EISA96284](https://openairdocs.org/sdr/EISA96284.md): Clip · cracked · Nov 1, 1996 · N314NE · Boeing 727223 · Fuselage Miscellaneous Structure > DURING 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) Next page: https://openairdocs.org/deregistered/N314NE-2004-02-26/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N314NE-2004-02-26/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.