N113FE, cancelled Apr 23, 2014

Service difficulty reports · 23

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 = 'N113FE' AND deregistration_id = 'N113FE-2014-04-23'
  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.

SDR 99FDEA00387Air Dist · fumesAIRCRAFT NEEDS INSP FOR ODOR. CVG FIRE DEPT FOUND FUMES EMANATING FROM CRATE IN NR 2 CONTAINER. RAMP AGENT REMOVED CRATE. INSP AC COMP AND FOUND NO CONTAMINATION OR DEFECTS. FUMES FROM SOLID OBJECTS IN CRATE.Sep 15, 1999 · N113FE · Boeing 72722C · Air Distribution SystemSDR 98FDEA00750Connector · loose98-303 NR 2 COWL ANTIICE TEMP OFF SCALE AT OVER 250C. NR 2 COWL VALVE STUCK. FOUND CANNON PLUG OFF ANTI DUCT TEMP SENSOR. LOCK WIRED ELECT CONN TO SENSOR PER MM 30-21-051. PERF FUNCTION TEST PER MM 30-21-00. SYSTEM OPER NORM WITH NR 2 ENG RUNNING.Dec 19, 1998 · N113FE · Boeing 72722C · Air Intake Anti/De-Ice SystemSDR 98FDEA00599Switch · failedON APPROACH WITH GEAR LEVER DOWN, NOSE GEAR IND UNSAFE. DURING GO-AROUND LIGHT WENT OUT AND GREEN NOSE GEAR DOWN CAME ON. REPLACED NOSE LAND GEAR POSITION SWITCH AND OPER CK GOOD PER MM 32-61-21.Sep 29, 1998 · N113FE · Boeing 72722C · Landing Gear Position and WarningSDR 97FDEA00778Retract Mech · failedDURING GEAR EXTENSION, THE NOSE GEAR DOOR LIGHT FLICKERED OFF AND ON AND NEVER TURNED GREEN. RECYCLED GEAR AND GOT A GREEN DOWN AND LOCKED INDICATION. CLEANED NOSE GEAR DOOR SWITCH PLUNGERS AND C/P'S ON GEAR UPLOCK AND DOWNLOCK MICROSWITCHES. GREASED TRUNNIOct 28, 1997 · N113FE · Boeing 72722C · Landing Gear Door Retract SectionSDR 97FDEA0765Actuator · stickingNOSE GEAR SLOW TO SHOW DOWN AND LOCKED (GREEN). RED LIGHT REMAINS ON LONGER THAN NORMAL. INSPECTED AND FOUND RT DOOR PLUNGER STICKING. REPLACED PLUNGER, OPS CK GOOD.Oct 15, 1997 · N113FE · Boeing 72722C · Landing Gear Door ActuatorSDR 96FDEA01508Bellframe · dentedMAIN CABIN STA 520 AT STR 6R BELLFRAME DENTED, NR0760 MAIN CABIN STA 520 4 INCHES BELOW STR 6R TO BELL FRAME DENTED NR0261. MAIN CABIN STA 520 BETWEEN STR 7 TO 8R BELLFRAME CRACKED AND DENTED NR0262. REPAIRED PER EA 7-5310-28854 NR 0260, 0261 AND 0262.Sep 18, 1996 · N113FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA01509Bellframe · dentedMAIN CABIN STA 580 BELLFRAME DENTED AND DISTORTED AT FLOOR LEVEL RIGHT SIDE ABOVE STR 17R. CUT OUT DAMAGE AND REPAIRED PER SRM 51-40-3 FIG 1.Sep 17, 1996 · N113FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA01507Fitting · corrodedUPPER LOBE MAIN CARGO FLOOR LT BARRIER NET FITTING 9G CORRODED AND CRACKED IN NUMEROUS PLACES STA 365 LBL 60. REMOVED DAMAGED FITTING, FABRICATED NEW FITTING PER EA 7-5320-28860. INSTALLED NEW FITTING PER SRM 51-10-1.Sep 11, 1996 · N113FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01505Seat Track · corrosionUPPER LOBE CORROSION AT LBL 35 FROM FS 540 TO 560. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-1.Sep 11, 1996 · N113FE · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA01506Floor Beam · corrodedUPPER LOBE, CORROSION ON FLOOR BEAM STA 681 UPPER CHORD, LBL 45 ON BOTTOM OF AFT FLANGE AT FLOOR BOARD ATTACH HOLE. REMOVED CORROSION, INSTALLED REPAIR STRAP PER B727 AARD 53-10-07-2 FIG 1.Sep 10, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01502Floor Beam · corrodedUPPER LOBE CORROSION AT FS 480 LBL 10 TOP FLOOR BEAM. REMOVED CORROSION PER SRM 51-10-6 OUT OF LIMITS PER SRM 53-10-1. INSTALLED FLOOR BEAM REPAIR STA 480 LBL 4 TO 22 PER SRM 53-10-8.Sep 8, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01494Floor Beam · corrodedSTA 640 BL 0 LBL 60 FLOOR BEAM IS CORRODED ON UPPER FLANGE TOP AND BOTTOM SIDES. FLOOR BEAM HAS BEEN REPAIRED PER SRM 53-10-8 FIG 15.Sep 7, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01504Floor Beam · corrosionHEAVY CORROSION ON MAIN CARGO FLOOR BEAM STA 480. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-10-08.Sep 6, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01501Skin · corrodedCORROSION ON FUSE SKIN BETWEEN STR 4 TO 6L AT STA 680 TO 700. CUT OUT DAMAGED SECTION OF FUSE SKIN, INSTALLED REPAIR DOUBLER PER SRM 53-30-3.Sep 6, 1996 · N113FE · Boeing 72722C · Fuselage Main, Plate/SkinSDR 96FDEA01499Floor Beam · corrodedUPPER LOBE STA 640 FLOOR BEAM CORRODED ON BOTTOM OF UPPER CHORD, FWD AND AFT FLANGES BETWEEN RBL 45 TO 65. REMOVED CORROSION PER SRM 51-10-6 FOR A SMOOTH BLEND OUT. INSTALLED 2 REINFORCEMENT REPAIR STRAPS TO LWR SIDE OF FLOOR BEAM STA 640 UPPER CHORD PER FESep 4, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01510Web · corrodedCENTER WING BOX 3RD BAY WEB AT STA 870 RBL 25.08 TO 45.61 POPPED FASTENER. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER EA 7-5771-28858.Aug 29, 1996 · N113FE · Boeing 72722C · Wing, Center BoxSDR 96FDEA1500Floor Beam · corrodedUPPER LOBE STA 680 FLOOR BEAM WAS CORRODED. CORROSION WAS REMOVED ON NR0484 LBL 50, MATERIAL REMOVED EXCEEDED SRM 53-10-1 LIMIT MEASURES .121. ACCOMPLISHED REPAIR AS PER SRM 53-10-8 FIG 8.Aug 28, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01503Floor Beam · corrosionUPPER LOBE STA 680 FLOOR BEAM WAS CORRODED. CORROSION WAS REMOVED ON NR0484 LBL 5, MATERIAL REMOVAL EXCEEDED SRM 53-10-1 LIMITS MIN .140 MINIMUM PER SRM IS .150. FABRICATED AND INSTALLED DOUBLERS PER SRM 53-10-8 PG 33, REF S/O'S W45M AND W45U FOR DOUBLERS. Aug 28, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01498Floor Beam · corrodedCABIN FLOOR BEAM CORRODED AROUND HOLE LWR SURFACE OF UPPER FLANGE STA 440 RBL 35 MKD. CUT OUT DAMAGED SECTION OF FLOOR BEAM UPPER CHORD, FWD ANGLE, INSTALLED FLOOR BEAM REPAIR ANGLES PER SRM 53-10-8 FIG 8.Aug 28, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01497Floor Beam · corrodedFLOOR BEAM AT STA 344 TOP SURFACE CORRODED FROM LBL 55 RBL 15. REMOVED DAMAGED SECTION OF UPPER CHORD, INSTALLED REPAIR CHORD AND ANGLES PER FEDEX SRD NR SR 27-53-007.Aug 27, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01496Floor Beam · crackedSTA 680 LBL 48 FLOOR BEAM IS CRACKED AROUND CORRODED FASTENER HOLE. REMOVED CORROSION PER 51-10-6, INSTALLED REPAIR PER SRM 53-10-8.Aug 27, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01495Floor Beam · corrodedSTA 680 BL 0 LBL 60 FLOOR BEAM IS HEAVY CORRODED BL 0 TO LBL 50 MEDIUM CORROSION 50 TO 60 LBL. REMOVED CORROSION PER 51-10-6 INSTALLED REPAIR PER SRM 53-10-8 FIG 8.Aug 27, 1996 · N113FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA00719Strut · reqd serviceNOSE GEAR DOORS WOULD NOT RETRACT ON TAKEOFF. RECYCLED THE GEAR AND TRIED AGAIN, STILL NO GEAR DOORS RETRACTED. WE OBSERVED AIR SPEED LIMITS, LIGHT EXTINGUISHED EN ROUTE. FOUND NOSE STRUT DEFLATED. RESEALED UPPER GLAND NUT PER MM 32-21-1 AND SERVICED SAME,Mar 30, 1996 · N113FE · Boeing 72722 · Nose/Tail Landing Gear Strut/Axle
Back to N113FE, cancelled Apr 23, 2014