N186FE, cancelled Jun 27, 2007

Service difficulty reports · 21

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 = 'N186FE' AND deregistration_id = 'N186FE-2007-06-27'
  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 04FDEA03234Attach Fitting · damagedMAIN FRAME MLG FWD TRUNNION ATTACH FITTING OVERSIZE HOLE REWORK C/W EA 7-5710-55408 ENT BY: 497236 RPT BY: 497236 FACT 26NOV04 15:03 COMPLIED WITH EA 7-5710-55408 HOLES OVERSIZED TO .875 AND REPAIR BUSHINGS INSTALLED RII:497228 ENT BY: 497236 RPT BY: 497236.Nov 26, 2004 · N186FE · Boeing 72722 · Wing, Landing Gear Attach FittingsSDR 04FDEA03170Hinge · gougedDOOR MAIN CARGO DOOR UPPER HINGE LOBE GOUGE REPAIR P/N B27-53-070-19. ENT BY: 497207 RPT BY: 497207 FACT 20 NOV 04 00:49 BFM U COMPLIED WITH EA NR 7-5210-82074 DOOR, MAIN CARGO DOOR UPPER HINGE LOBE GOUGE REPAIR P/N B27-53-070-19 ENT BY: 497212 RPT BY: 49721Nov 19, 2004 · N186FE · Boeing 72722 · Cargo/Baggage DoorsSDR 04FDEA03103Seat Track · gougedFWD CARGO SEAT TRACK RT SIDE AT PFM BOX HAS A GOUGED/WORN LOBE. REMOVED FWD CARGO SEAT TRACK RT SIDE AT PFM BOX IAW SRM 51-30-02. CHECKED LIMITS IAW SRM 53-10-05. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SECTION OF SEAT TRACK UNDER TRAVELER NR T4/469064. Nov 12, 2004 · N186FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03087Seat Track · corrodedRT UPPER LOBE BS480, RBL40, SEAT TRACK CORRODED AROUND RIVET. FABRICATED SEAT TRACK IAW SRM 53-10-5 PG 4, WITH MAT ID AND MPN 60-6549/7075-T6511. LOCATED AND DRILLED HOLES IAW SRM 51-30-0. (TRAVELER NR T4/470482) AND ALODINED AND PRIMED IAW SRM 51-10-2 PG Nov 11, 2004 · N186FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00416Skin · dentedSKIN DENTED AT BS 720, STR 16R.Jun 16, 2002 · N186FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 02FDEA00418Skin · corrodedCORROSION STR 19L TO 23L, BS 350-360 SKIN BULGING AROUND FASTENERS. REMOVED AND REPLACED SKIN PER EA 7-5330-64974 & SRM 53-30-3.Jun 15, 2002 · N186FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00447Fitting · corrodedLEFT WING O/B AILERON FITTING CORRODED ON TOPSIDE OF FITTING. REMOVED AND REPLACED FITTING PER MM 27-10-131-4.Jun 12, 2002 · N186FE · Boeing 727200 · AileronsSDR 01FDEA00012Actuator · failed01-002 DURING CLIMBOUT, LANDING GEAR SELECTOR IN OFF POSITION. RED DOORS LIGHT ILLUMINATED, WITH AMBER RT MLG DOOR LIGHT. REPLACED DOOR ACTUATOR PER B727 MM 32-32-081-4. LEAK & OPS CK OK. REMOVED GEAR PINS.Jan 6, 2001 · N186FE · Boeing 72722 · Landing Gear ActuatorSDR 00FDEA00208Skin · crackedDURING ROUTINE INSP, EXT FUSELAGE SKIN FOUND CRACK IN THE A ROW AT 9/32 FASTENER HOLE AT BS 440, STR 4L.Apr 3, 2000 · N186FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 00FDEA00183Channel · corrodedAFT BAG BIN FLOOR SUPPORT CHANNEL CORRODED BEYOND ALLOWED LIMITS, ON LWR SURFACE, AT FASTENER HOLES BENEATH RT FLOOR TRACK BS 960. *S/D* REMOVED ANGLE, FAB AND INSTALLED NEW ANGLE IAW SRM 51-20-1 & 51-30-2.Mar 27, 2000 · N186FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 00FDEA00174Attach Fitting · corrodedDURING ROUTINE INSP, THE LEFT O/B AILERON, I/B ATTACH FITTING WAS FOUND TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED PER IAW MM 27-10-031-2.Mar 27, 2000 · N186FE · Boeing 72722 · Wing, Control Surface Attach FittingsSDR 00FDEA00173Attach Fitting · corrodedDURING ROUTINE INSP, RIGHT O/B AILERON, I/B ATTACH FITTING WAS FOUND TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED PER IAW MM 27-10-031-2.Mar 27, 2000 · N186FE · Boeing 72722 · Wing, Control Surface Attach FittingsSDR 00FDEA00172Web · crackedDURING ROUTINE INSP, WEB INSIDE VERTICAL STABILIZER AT FIN STA 110.4 FOUND CRACKED. REPAIRED IAW SRM 53-10-9 FIG 4.Mar 27, 2000 · N186FE · Boeing 72722 · Vertical StabilizerSDR 00FDEA00182Skin · crackedDURING ROUTINE INSP, FUSELAGE SKIN FOUND CRACKED AT LAP JOINT, STR 20L, BS 1185. *S/D* FAB FILLER, DOUBLER AND INSTALLED IAW SRM 53-30-3 FIG 3A.Mar 27, 2000 · N186FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 97FDEA00866Skin · corrodedCORROSION (C53-100-01) ON EXTERIOR SKIN FROM BS 1149 TO BS 1153, RBL 2, WL 148. *S/D* REMOVED SECTION OF SKIN (9.7 X 7.5) AT BS 1149 TO 1159, RBL 2 LBL 2, WL 148, APPLIED SKIN PATCH IAW FDE SRM 53-30-3.Nov 26, 1997 · N186FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 97FDEA00863Skin · dentedDENTED EXTERIOR SKIN AT BS 1135 BETWEEN STRINGERS 18L AND 19L, LBL 65, WL 192. *S/D* ACCESSED DAMAGED AREA AND INSTALLED COUNTERSINK WASHERS, FABRICATED PARTS AND INSTALLED FASTENERS AND ALL ACCESSED PARTS PER FEDEX SRM 53-30-03.Nov 24, 1997 · N186FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 97FDEA00862Frame · crackedBS 500 FRAME IS CRACKED UNDER FLOOR SUPPORT AT RBL 9, WL 156. *S/D* REPAIRED FRAME AT BS 500, RBL 9, WL 156 UNDER FLOOR SUPPORT IAW FEDEX SRM 51-40-3.Nov 24, 1997 · N186FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00857Crease Beam · corrodedNR 0125 003 CORROSION (C53-224-06) ON CREASE BEAM VERTICAL FLANGE BS 310-346, LBL 62, WL 209. REMOVED OLD CORRODED CREASE BEAM AND DRILLED AND INSTALLED FASTENERS IN NEW CREASE BEAM BS 285 - BS 360, LBL 62, WL 208 IAW FEDEX SRM 51-30-2, 53-10-1, 51-30-5.Nov 24, 1997 · N186FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00856Stringer · corrodedWHILE WORKING CUSTOMER CARD NR NR0154, FOUND CORROSION ON STR 30, BS 1148, WL 142. *S/D* REMOVED DAMAGED STRINGER AT BS 1138 TO BS 1158, STR 30, WL 142 AND REPAIRED IAW FED SRM 53-10-3.Nov 24, 1997 · N186FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 97FDEA00851Skin · corrodedCORROSION (C53-100-01) ON EXTERIOR SKIN AT BS 1080 BETWEEN STR 27L AND 28L, WL 144, LBL 12 TO LBL 24. *S/D* REPAIRED SKIN AT BS 1080 BETWEEN STR 27L AND 28L, LBL 12 TO LBL 24 PER FEDEX SRM 53-30-3.Nov 21, 1997 · N186FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 97FDEA00850Frame · crackedBS 680 FRAME HAS CRACK EMANATING FROM RADIUS IN CUTOUT FOR STR 26 RT. *S/D* STOP DRILLED CRACK AT BS 680, STR 26 RT PER FEDEX SRM 51-10-1 AND REPAIRED CRACK PER FEDEX SRM 51-40-3.Nov 21, 1997 · N186FE · Boeing 72722 · Fuselage Main, Frame
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