N166FE, cancelled Aug 21, 2007

Service difficulty reports · 71

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 = 'N166FE' AND deregistration_id = 'N166FE-2007-08-21'
  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 05FDEA02718Radar · failedWX RADAR FAILED 5 MIN AFTER T/O CYCLED C/B NO JOY TURNED RT ON AND OFF SEVERAL TIMES REMAINED FAILED. REPLACED WX R/T, GRD OPS CK NORMAL MM 34-41-041. REMOVAL/INSTALLATION, OFF MFG 622-5132-101, POS ONL SRL 2652 TAG A03946 ON MFG 622-5132-101 SRL 3939 TAG AAug 30, 2005 · N166FE · Boeing 72722 · Weather Radar SystemSDR 05FDEA02694Stall Warning · malfunctionedON TAXI OUT, NR 1 STALL WARNING STICK SHAKER ACTIVATED MOMENTARILY THEN STOPPED. ABOUT 3 MINUTES LATER, IT REACTIVATED AND PULLED THE NR 1 STALL WARNING C\B TO DEACTIVATE. ON TAXI IN SMOKE BEGAN TO EMANATE FROM BEHIND GLARE SHIELD. EVACUATED AIRCRAFT. REMOAug 27, 2005 · N166FE · Boeing 72722 · Stall Warning SystemSDR 04FDEA03450Structure · crackedN01259 RT HAND HORIZONTAL STAB L/E UPPER CHORD CRACKED ON LWR SURFACE BETWEEN L/E STAB STA 1.0 TO L/E STAB STA 72.0. FOUND RT HORIZ STAB L/E UPR CHORD OUT OF LIMITS. TRIMMED OUT SEGMENT OF CHORD, FABRICATED NEW CHORD FROM REF. PO 179160, SPLICE FROM BAC1490Dec 20, 2004 · N166FE · Boeing 727100 · Horizontal Stabilizer StructureSDR 04FDEA03436Skin · crackedEXTERNAL SKIN CRACKED AT AFT LWR CARGO DOOR CUTOUT 10 INCHES AFT OF THE FWD LWR CORNER 2 INCHES BELOW LWR EDGE. REPAIRED CRACKED SKIN, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX EA 7-5330-82517.Dec 17, 2004 · N166FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA03411Spar · crackedWHILE ACCESSING FRONT SPAR WEB FOR UPR SPAR REPAIR, LWR FRONT SPAR VERTICAL FLANGE CRACKED BETWEEN LT L/E STA 109 & 119. REPAIRED IAW SRM 55-10-5.Dec 14, 2004 · N166FE · Boeing 727100 · Horizontal Stabilizer, Spar/RibSDR 04FDEA03404Web · corrodedCORROSION LT HORIZONTAL STAB FIXED L/E INTERNAL VERTICAL WEB L/E STA 29. *S/D* REPAIRED PER SRM 55-10-1 FIG 1, 51-30-2, 51-10-1, 55-10-4, 51-30-5.Dec 10, 2004 · N166FE · Boeing 727100 · Horizontal Stabilizer StructureSDR 04FDEA03401Skin · damagedCOMPLY WITH EO 7-5330-7-2319 PART 5 BS 441 AT STR 19-20 RT AND STR 20-21 RT. *S/D* REPAIRED FUSE SKIN BS 441 STR 19-21 RT IAW EO 7-5330-7-2319 AND EA 7-5330-82513.Dec 9, 2004 · N166FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA03181Skin · gougedUPPER EXTERNAL SKIN BS 761, 2 INCHES ABOVE STR 4 LT IS GOUGED. BLENDED GOUGE ON SKIN BS 761, 2 INCHES ABOVE STR 4 LT, OUT OF LIMITS. REPAIRED DAMAGE SKIN AT BS 761 STR 4 LT PER SRM 53-30-3 FIG 5.Nov 22, 2004 · N166FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA03164Skin · corrodedCORROSION BS 480 STR 4R - STR 6R UNDER FWD SIDE OF THE SPLICE. FOUND VISUALLY, DURING DETAILED VISUAL INSPECTION. CORROSION NOT FOUND DURING LOW FREQUENCY INSPECTION. CORROSION BS 480 STR 4R TO 6R UNDER FWD SIDE OF SPLICE REPAIR ON W/C N01202 AND EO 7-533Nov 18, 2004 · N166FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA03165Hinge · corrodedCORROSION ON LT WING NR 1 K-FLAP O/B BULLNOSE HINGE LUG AROUND FASTENERS UPPER SURFACE.Nov 18, 2004 · N166FE · Boeing 727100 · Leading Edge DevicesSDR 04FDEA03163Attach Fitting · damagedLT WING FIXED TRAILING EDGE O/B AILERON O/B ATTACH FITTING.Nov 18, 2004 · N166FE · Boeing 727100 · Wing, Control Surface Attach FittingsSDR 04FDEA03109Frame · corrodedCORROSION LT FWD EMERGENCY ESCAPE DOOR UNDER SIDE OF LWR FRAME BACK SIDE OF OUTER SKIN 7 INCH UP FROM LWR AFT CORNER.Nov 15, 2004 · N166FE · Boeing 72722 · Emergency ExitsSDR 04FDEA03108Frame · dentedFRAME BS 1010 LT BETWEEN STR 24 AND 25 DENTED.Nov 15, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03107Floorbeam · damagedCORROSION MECHANICAL DAMAGE ON FLOORBEAM BS 680 UPPER CHORD LWR SURFACE AT LBL 64 WL 208.Nov 15, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03106Frame · dentedAFT CARGO FRAME DENTED AT BS 970, STR 26R.Nov 15, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03100Structure · crackedLT WING I/B MID FLAP TRAILING EDGE CHORD CRACKED AT THE I/B AFT FLAP ACTUATION ROD CUT OUT. REPAIRED PER SRM 51-40-4, 51-30-2, OHM 20-50-01, 20-50-02.Nov 12, 2004 · N166FE · Boeing 72722 · Leading Edge DevicesSDR 04FDEA03076Spar · crackedN01167 CORROSION ON LT. HORIZ. STAB UPPER SPAR AT STAB STA. 198. REPAIRED PER SRM 55-10-5 FIG 1Nov 11, 2004 · N166FE · Boeing 727100 · Horizontal Stabilizer, Spar/RibSDR 04FDEA03082Frame · dentedFRAME BS 990 LT AT STR 24 DENTED. REPAIRED PER SRM 51-40-3.Nov 11, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03081Skin · bulgedRT HORIZ STAB UPPER SKIN HAS SHEARED FASTENER AND SKIN BULGE 31 INCH FROM TRAILING EDGE AND 30 INCH FROM I/B EDGE. RT HORIZONTAL STAB UPPER SKIN FOUND TO BE CORRODED BEYOND LIMITS AND WILL BE REPLACED ON FED EX W/C N01050.Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Plate/SkinSDR 04FDEA03077Stringer · gougedMAIN CARGO BAY HAS 2 GOUGES ON STR 16R AT BS 554 AND BS 557. GOUGES ON STR 16R BS 554 AND BS 557 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REPAIRED STR 16R IAW SRM 53-10-3.Nov 11, 2004 · N166FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 04FDEA03079Floorbeam · corrodedFLOORBEAM CORRODED RBL 18, W/L 200. REPAIRED PER SRM 53-10-8Nov 11, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03075Skin · corrodedRT HORIZ STAB UPPER SKIN LOWER SURFACE HAS CORROSION (C55-300-10(2)) EMANATING FROM BONDED DOUBLERS 33 INCHES FROM AFT EDGE AND 30 INCH FROM I/B EDGE. RT HORIZONTAL STAB UPPER SKIN LOWER SURFACE FOUND TO BE OUT OF LIMETS REPAIRED PER FED-EX EA 7-5510-82519 ANNov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Plate/SkinSDR 04FDEA03074Spar · corrodedCORROSION LT HORIZONTAL STAB UPPER FRONT SPAR CHORD INTERNAL SURFACE IN AREAS FROM STAB STA 4.45 TO STAB STA 33. REPAIRED IAW SRM 51-10-6. 51-30-2, 51-10-2, 55-10-5.Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Spar/RibSDR 04FDEA03073Spar · corrodedCORROSION ON LT HORIZONTAL STAB INTERNAL UPPER FRONT SPAR CHORD STAB STA 64. REPAIRED IAW SRM 51-10-6, 51-30-2, 51-10-2, 55-10-5.Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Spar/RibSDR 04FDEA03071Floorbeam · corrodedCORROSION AT FLOORBEAM UPPER AND LOWER SURFACE BS 344 LBL 10 - RBL 10. REPAIRED FLOORBEAM BS 344 LBL 10 - RBL10 PER SRM 53-10-1 AND FEDEX SR 27-53-007.Nov 10, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03068Floorbeam · damagedMECHANICAL DAMAGE ON FLOORBEAM STA 700 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8Nov 10, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03062Hinge Fitting · corrodedCORROSION ON RT WING O/B AILERON I/B CTR FITTING A/C SIDE IS CORRODED ON LOWER SURFACE. REPAIRED PER MM 27-10-031-2, SRM 51-30-2, 51-30-5.Nov 9, 2004 · N166FE · Boeing 72722 · Wing, Control Surface Attach FittingsSDR 04FDEA03056Frame · dentedFRAME BS 1030 LT AT STR 24 AND 25, DENTED. REPAIRED FRAME PER SRM 51-40-3.Nov 9, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03055Floorbeam · damagedMECHANICAL DAMAGE ON FLOORBEAM BS 720 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8Nov 9, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03032Frame · dentedAFT CARGO FRAME DENTED AT BS. 1010 STR 26R. REPAIRED PER SRM 51-40-3Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, FrameSDR 04FDEA03029Frame · dentedAFT CARGO FRAME DENTED AT BS 1030, STR 26R. REPAIRED PER SRM 51-40-3.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03028Frame · dentedAFT CARGO FRAME DENTED AT BS 990 STR 26 LT. REPAIRED PER SRM 51-40-3, 51-10-2 AND 51-30-2.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03027Skin · dentedBS 294, STR 21 RT, DENTS AROUND 3 FASTENERS. REPAIRED PER SRM 53-30-1, 53-30-3.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 04FDEA03045Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM AT BS 620 BL O - LBL 8 (C53-111-01(3)). CORROSION REMOVED ON FLOORBEAM FOUND TO BE OUT OF LIMITS. FLOORBEAM TO BE REPAIRED ON N00920.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03044Web · crackedFUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED AT STA 880-890, LBL 47, WL 206. REPLACED VERTICAL WEB PER SRM 51-10-2, 51-30-2 & SRM 51-30-5.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 04FDEA03047Floorbeam · corrodedCORROSION (C53-224-01) AT FLOORBEAM UPPER CHORD AT BS 620, LBL 45-65, WL 208.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03046Floorbeam · corrodedCORROSION FLOORBEAM STA 620 LWR CHORD LWR SURFACE CORRODED LBL 8 AROUND NUTPLATE HOLE. REPAIRED PER SRM 53-10-1, 53-10-8Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03043Stringer · gougedMAIN CARGO BAY HAS GOUGE ON STRINGER 9R AT BS 600.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 04FDEA03042Web · crackedFUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED, STA 880-890 RBL 47, WL 206. REPAIRED PER SRM 51-30-2, 51-30-5, 51-10-3, 51-10-2Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 04FDEA03041Stringer Clip · crackedSTRINGER CLIP CRACKED, STR 5L, BS 1010. REPLACED PER SRM 51-30-2, 51-30-5Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Attach FittingsSDR 04FDEA03040Seat Track · gougedSEAT TRACK GOUGED AT BS 740, RBL 45, WL 208. REPAIRED SEAT TRACK PER SRM 53-10-5.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03039Stringer Clip · crackedSTRINGER CLIP CRACKED BS 1108 LT STR 20. REPLACED STRINGER CLIP PER SRM 51-30-2.Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Attach FittingsSDR 04FDEA03038Door Frame · damagedBS 1108 AFT CARGO DOOR FRAME AT STR 26 HAS A OPEN HOLE IN UPPER FLANGE. REPAIRED AFT CARGO DOOR FRAME PER FED EX EA 7-5310-825111.Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, StructureSDR 04FDEA03037Stringer · gougedGOUGE ON UNDERSIDE FLANGE OF STR 19 RT, BS 488, WL 174. REPAIRED STR 19 RT IAW SRM 53-10-3 FIG 1 AND 53-10-1.Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 04FDEA03036Frame · dentedFWD CARGO STA 540 FRAME DENTED AT STR 24 LT & 25 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-1, 51-20-4, 53-10-1.Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, FrameSDR 04FDEA03035Frame · dentedFWD CARGO FRAME STA 660 DENTED STR 24 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-4 AND 53-10-1.Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, FrameSDR 04FDEA03034Frame · dentedTOP FLANGE OF FRAME AT BS 640, RBL 32, WL 150 IS DENTED. REPAIRED PER SRM 53-10-1, 51-30-5, 51-20-4, 51-30-2, 51-10-1, 53-10-2 AND 51-40-3Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, FrameSDR 04FDEA03033Rib · crackedRT ELEVATOR NR 5 HINGE SUPPORT RIB ELEVATOR STA 136.50 PREVIOUS REPAIR AT I/B LOWER FLANGE IS CRACKED. REPLACED PER E.O. 7-5510-7-5001 PT 2.Nov 8, 2004 · N166FE · Boeing 727100 · Elevator, Spar/RibSDR 04FDEA03031Frame · dentedFRAME DENTED AT BS 1090, STR 23 LT. REPAIRED PER SRM 51-40-3.Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, FrameSDR 04FDEA03030Frame · dentedAFT CARGO FRAME DENTED AT BS 990, STR 26R. REPAIRED PER SRM 51-40-3.Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Frame
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