N168FE, cancelled Jun 28, 2007

Service difficulty reports · 26

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 = 'N168FE' AND deregistration_id = 'N168FE-2007-06-28'
  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 04FDEA03385Switch · malfunctionedAT FL280, LE AMBER LIGHT ILLUMINATED (WING ANTI-ICE ON). NO ROLL OR DIRECTIONAL CENTRAL PROBLEM NOTED. NR 2 FLAP ON FE PNL L AMBER. SLOWED DOWN TO 230 KTS, CLOSED WING ANTI-ICE. LIGHT STAYED ON, RECEIVED QRH. DID NOT CHANGE CONFIG. DESCENDED T0 200 DECLARDec 7, 2004 · N168FE · Boeing 72722 · Leading Edge Slat Position Indicating SystemSDR 03FDEA02042Bellcrank · damagedCOMPLY WITH EA 7-5230-73854A DOOR MAIN CARGO DOOR TORQUE TUBE ELONGATED HOLES REPAIR BS 489 THROUGH BS 610. COMPLIED WITH EA 7-5230-73854A DOOR-MAIN CARGO DOOR TORQUE TUBE ELONGATED HOLES REPAIR BS 489 THRU BS 610, AT MAE.Dec 4, 2003 · N168FE · Boeing 727100 · Cargo/Baggage DoorsSDR 03FDEA01639Duct · looseON CLIMBOUT NR 3 GENERATOR BREAKER TRIPPED. OBSERVED GENERATOR DRIVE OIL TEMP PEGGED ON THE HIGH SIDE. COMPLIED WITH CSD HIGH OIL TEMP PROCEDURE AND CSD FAILED TO DISCONNECT. TEMP REMAINED HIGH THRU THE FLIGHT. FOUND CSD EJECTOR LINE LOOSE AT VALVE AND HOTSep 26, 2003 · N168FE · Boeing 727100 · Engine Bleed Air SystemSDR 01FDEA00262Support · crackedDURING ROUTINE INSP, FLOORBEAM SUPPORT STRAP AT BS 304, STR 18R, RBL 35 FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.Apr 7, 2001 · N168FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 01FDEA00261Seat Track · corrodedDURING ROUTINE INSP, FWD LWR CARGO BIN LT SEAT TRACK FOUND CORRODED AT BS 680. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.Apr 7, 2001 · N168FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 01FDEA00260Floorbeam · corrodedDURING ROUTINE INSP, BS 660 FLOORBEAM FOUND CORRODED AT NR 5 SEAT TRACK. CUT OUT DAMAGED AREA. FAB AND INSTALL REPAIR PER IAW BAC 727 SRM 53-10-8.Apr 7, 2001 · N168FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 01FDEA00259Floorbeam · corrodedDURING ROUTINE INSP, BS 640 FLOORBEAM FOUND CORRODED AT 5 SEAT TRACK. CUT OUT DAMAGED AREA. FAB AND INSTALL REPAIR PER IAW BAC 727 SRM 53-10-8.Apr 7, 2001 · N168FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 01FDEA00227Skin · corrodedN 164 DUR ROUTINE INSP, FUSELAGE SKIN FND CORRODED AT BS 400, STR 3R AND 4R. ** S/D ** STRIPPED AREA. LFEC IND NO CORROSION LOSS PER LOSS IAW 727 NDT MANUAL PART 6. TREATED, PRIMED AND REPAIR PER IAW BAC 727 SRM 51-20-151-7.Mar 24, 2001 · N168FE · Boeing 72722 · Fuselage Main, StructureSDR 01FDEA00229Support Fitting · crackedN 650 DUR ROUTINE INSP, UPR AND LWR LUGS OF THE UPR RUDDER ROD SUPPORT FITTING LOCATED ON THE VERTICAL STABILIZER REAR SPAR FND CRACKED. ** S/D ** HFEC IND NO CRACKS PER IAW 727 NDT MANUAL PART 6.Mar 24, 2001 · N168FE · Boeing 72722 · Vertical Stabilizer, Spar/RibSDR 01FDEA00228Rib · crackedDURING ROUTINE INSP HFEC IND THE LWR RUDDER, THRUST HINGE RIB FITTING WAS CRACKED AT FWD RIGHT SIDE. *S/D* REMOVED AND REPLACED RUDDER THRUST HINGE RIB PER IAW FEDEX EO 7-5550-7-2303C PART 2.Mar 24, 2001 · N168FE · Boeing 72722 · Vertical Stabilizer, Spar/RibSDR 01FDEA00230Intercostal · crackedDURING ROUTINE INSP, INTERCOSTAL AT BS 738 AT THE NR 5 SEAT TRACK FOUND CRACKED. *S/D* STOP DRILLED INTERCOSTAL. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-2.Mar 24, 2001 · N168FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 00FDEA00896Downlock Switch · faultyON APRROACH IN INDIANA, NO GREEN LIGHT ON NOSE GEAR INDICATOR. RECYCLED GEAR NOSE GEAR IND SHOW GREEN AFT A DELAY. ** S/D ** CLEAN & TREAT DOWN & LOCK POSITION SWITCH PER 727-100 32-21-041-2.Dec 21, 2000 · N168FE · Boeing 72722 · Landing Gear Position and WarningSDR 00FDEA00320Warning Light · illuminatedAFT T/O WITH FLAPS FULLY RETRACTED, NR 2 LEADING EDGE FLAP AND LEADING EDGE (AMBER) LIGHT ILLUM ON FWD PANEL.May 5, 2000 · N168FE · Boeing 72722 · Leading Edge Slat Position Indicating SystemSDR 98FDEA00650Doubler · corrodedWHILE WORKING NR0186, FOUND INTERNAL DOUBLER AT BS 961 TO 990, STR 28 TO 29 RT TO BE CORRODED AND OUT OF LIMITS PER SRM.Oct 13, 1998 · N168FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00649Chord · corrodedWHILE WORKING NR 0213 FOUND CORROSION ON FAIL-SAFE CHORD, BS 380 BETWEEN STR 25 TO 26 RT. *S/D* REPAIRED FAIL-SAFE CHORD BS 380 BETWEEN STR 25-26 RT IAW FEDEX SRM 51-40-3.Oct 13, 1998 · N168FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00644Stringer · corrodedUPON REMOVAL OF LT KEEL BEAM ON NR 0190, FOUND CORROSION IN STR AT BS 1080, LBL 8, WL 138, STR 29L. *S/D* REPAIRED STR 29L, BS 1082-1098, LBL 8, WL 138 PER FED-EX SRM 53-10-3.Oct 8, 1998 · N168FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 98FDEA00640Beam · corrodedWHILE WORKING NR 424, FOUND CORROSION ON 25 G-BEAM AT BS 264, WL 208, RBL 8 TO BE OUT OF LIMITS. *S/D* REMOVED AND REPLACED 25 G-BEAM, BS 264, WL 208, LBL 18 TO RBL 26 IAW FED-EX DRAWING 65-17593 AND FED-EX SRM 51-30-2.Oct 7, 1998 · N168FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00619Stringer · corrodedNR 0211 CORROSION (C53-224-03-1/2) TOP OF STR 26 FROM BS 381-400, LBL 29, WL 156 IN FWD E/E BAY. REMOVED AND REPLACED STR 26L FROM BS 384-413, LBL 29, WL 156 PER FEDEX SRM 53-10-3.Oct 5, 1998 · N168FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 98FDEA00618Stringer · corrodedCORROSION (C53-224-03-1/2) ON UPPER SURFACE OF STR 26R, BS 380, RBL 16, WL 152. *S/D* REMOVED AND REPLACED CORRODED STR BS 360-385, STR 26R, WL 152 PER FED-EX SRM 53-10-3.Oct 5, 1998 · N168FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 98FDEA00597Keel Beam · corrodedCORROSION ON RT KEEL BEAM AT BS 1040, WL 138, AFT CARGO BAY. *S/D* REMOVED AND REPLACED RT KEEL BEAM AT BS 1040 TO BS 961 WL 138 PER FEDEX EA 7-5330-42225.Sep 28, 1998 · N168FE · Boeing 72722 · Fuselage Main, KeelSDR 98FDEA00596Beam · corrodedCORROSION UNDER NUT PLATE ON FLANGE OF LONGITUDINAL BEAM BS 798, LBL 25, WL 208. *S/D* REMOVED AND REPLACED LONGITUDINAL BS 798, LBL 25, WL 208 PER FED-EX SRM 51-30-2, BOEING DWG 65-16279.Sep 28, 1998 · N168FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00595Keel Beam · corrodedCORROSION ON LT KEEL BEAM AT BS 1030, WL 138, LBL 12 IN THE AFT CARGO BAY. *S/D* REMOVED AND REPLACED LT KEEL BEAM AT BS 961-1087, WL 138, LBL 8 PER FEDEX.Sep 28, 1998 · N168FE · Boeing 72722 · Fuselage Main, KeelSDR 96FDEA01694Switch Spacer · missingNR 2 LEADING EDGE FLAP FAILED TO RETRACT AFTER TAKEOFF. FOLLOWED CHECKLIST WITH NO RESULTS, RETURNED TO PORTLAND. REMOVED AND REPLACED NR 2 FLAP SWITCH, FOUND SPACER MISSING. INSTALLED SPACER, OPERATIONAL CHECK SEVERAL TIMES OPERATIONAL CHECK GOOD PER MAINTNov 27, 1996 · N168FE · Boeing 72722 · Leading Edge Slat Control SystemSDR 96FDEA01179Gusset · crackedCABIN INTERIOR - FS 783.5 RIB SUPPORT GUSSET BELOW FLOOR LEVEL, IS CRACKED AT LOWER INBOARD CORNER, JUST ABOVE WING SKIN, CRACK APPROX 1 INCH. CRACKED GUSSET REMOVED, DOUBLER INSTALLED AS PER BOEING SB 727-53-0197.Jun 25, 1996 · N168FE · Boeing 727123 · Fuselage Miscellaneous StructureSDR 96FDEA01181Bell Frame · crackFORWARD CARGO CRACK IN BELL FRAME, STA 680 BETWEEN STR 26-27L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-40-4, PG 12-17.Jun 24, 1996 · N168FE · Boeing 727123 · Fuselage Main, FrameSDR 96FDEA01180Floor Beam · corrosionMAIN CARGO CORROSION ON FLOOR BEAM AT SCREW HOLES FROM LBL 45 - 54, STA 344. REMOVED CORROSION PER SRM 53-10-1. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8 AND EA 7-5310-28760, DATE 6-24-96.Jun 24, 1996 · N168FE · Boeing 72722 · Fuselage Main, Floor Beam
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