# Service difficulty reports: N186FE, cancelled Jun 27, 2007

A list on [N186FE, cancelled Jun 27, 2007](https://openairdocs.org/deregistered/N186FE-2007-06-27.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 04FDEA03234](https://openairdocs.org/sdr/04FDEA03234.md): Attach Fitting · damaged · Nov 26, 2004 · N186FE · Boeing 72722 · Wing, Landing Gear Attach Fittings
  > MAIN 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.
- [SDR 04FDEA03170](https://openairdocs.org/sdr/04FDEA03170.md): Hinge · gouged · Nov 19, 2004 · N186FE · Boeing 72722 · Cargo/Baggage Doors
  > DOOR 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: 49721
- [SDR 04FDEA03103](https://openairdocs.org/sdr/04FDEA03103.md): Seat Track · gouged · Nov 12, 2004 · N186FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > FWD 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.
- [SDR 04FDEA03087](https://openairdocs.org/sdr/04FDEA03087.md): Seat Track · corroded · Nov 11, 2004 · N186FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > RT 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
- [SDR 02FDEA00416](https://openairdocs.org/sdr/02FDEA00416.md): Skin · dented · Jun 16, 2002 · N186FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > SKIN DENTED AT BS 720, STR 16R.
- [SDR 02FDEA00418](https://openairdocs.org/sdr/02FDEA00418.md): Skin · corroded · Jun 15, 2002 · N186FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > CORROSION STR 19L TO 23L, BS 350-360 SKIN BULGING AROUND FASTENERS. REMOVED AND REPLACED SKIN PER EA 7-5330-64974 & SRM 53-30-3.
- [SDR 02FDEA00447](https://openairdocs.org/sdr/02FDEA00447.md): Fitting · corroded · Jun 12, 2002 · N186FE · Boeing 727200 · Ailerons
  > LEFT WING O/B AILERON FITTING CORRODED ON TOPSIDE OF FITTING. REMOVED AND REPLACED FITTING PER MM 27-10-131-4.
- [SDR 01FDEA00012](https://openairdocs.org/sdr/01FDEA00012.md): Actuator · failed · Jan 6, 2001 · N186FE · Boeing 72722 · Landing Gear Actuator
  > 01-002 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.
- [SDR 00FDEA00208](https://openairdocs.org/sdr/00FDEA00208.md): Skin · cracked · Apr 3, 2000 · N186FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DURING ROUTINE INSP, EXT FUSELAGE SKIN FOUND CRACK IN THE A ROW AT 9/32 FASTENER HOLE AT BS 440, STR 4L.
- [SDR 00FDEA00183](https://openairdocs.org/sdr/00FDEA00183.md): Channel · corroded · Mar 27, 2000 · N186FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR 00FDEA00174](https://openairdocs.org/sdr/00FDEA00174.md): Attach Fitting · corroded · Mar 27, 2000 · N186FE · Boeing 72722 · Wing, Control Surface Attach Fittings
  > DURING 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.
- [SDR 00FDEA00173](https://openairdocs.org/sdr/00FDEA00173.md): Attach Fitting · corroded · Mar 27, 2000 · N186FE · Boeing 72722 · Wing, Control Surface Attach Fittings
  > DURING 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.
- [SDR 00FDEA00172](https://openairdocs.org/sdr/00FDEA00172.md): Web · cracked · Mar 27, 2000 · N186FE · Boeing 72722 · Vertical Stabilizer
  > DURING ROUTINE INSP, WEB INSIDE VERTICAL STABILIZER AT FIN STA 110.4 FOUND CRACKED. REPAIRED IAW SRM 53-10-9 FIG 4.
- [SDR 00FDEA00182](https://openairdocs.org/sdr/00FDEA00182.md): Skin · cracked · Mar 27, 2000 · N186FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR 97FDEA00866](https://openairdocs.org/sdr/97FDEA00866.md): Skin · corroded · Nov 26, 1997 · N186FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > CORROSION (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.
- [SDR 97FDEA00863](https://openairdocs.org/sdr/97FDEA00863.md): Skin · dented · Nov 24, 1997 · N186FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DENTED 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.
- [SDR 97FDEA00862](https://openairdocs.org/sdr/97FDEA00862.md): Frame · cracked · Nov 24, 1997 · N186FE · Boeing 72722 · Fuselage Main, Frame
  > BS 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.
- [SDR 97FDEA00857](https://openairdocs.org/sdr/97FDEA00857.md): Crease Beam · corroded · Nov 24, 1997 · N186FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 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.
- [SDR 97FDEA00856](https://openairdocs.org/sdr/97FDEA00856.md): Stringer · corroded · Nov 24, 1997 · N186FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > WHILE 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.
- [SDR 97FDEA00851](https://openairdocs.org/sdr/97FDEA00851.md): Skin · corroded · Nov 21, 1997 · N186FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > CORROSION (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.
- [SDR 97FDEA00850](https://openairdocs.org/sdr/97FDEA00850.md): Frame · cracked · Nov 21, 1997 · N186FE · Boeing 72722 · Fuselage Main, Frame
  > BS 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.

## 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 = 'N186FE' AND deregistration_id = 'N186FE-2007-06-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N186FE-2007-06-27/reports

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