# Service difficulty reports: N166FE, cancelled Aug 21, 2007

A list on [N166FE, cancelled Aug 21, 2007](https://openairdocs.org/deregistered/N166FE-2007-08-21.md).

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

Page 1 of 2 · 71 reports

- [SDR 05FDEA02718](https://openairdocs.org/sdr/05FDEA02718.md): Radar · failed · Aug 30, 2005 · N166FE · Boeing 72722 · Weather Radar System
  > WX 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 A
- [SDR 05FDEA02694](https://openairdocs.org/sdr/05FDEA02694.md): Stall Warning · malfunctioned · Aug 27, 2005 · N166FE · Boeing 72722 · Stall Warning System
  > ON 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. REMO
- [SDR 04FDEA03450](https://openairdocs.org/sdr/04FDEA03450.md): Structure · cracked · Dec 20, 2004 · N166FE · Boeing 727100 · Horizontal Stabilizer Structure
  > N01259 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 BAC1490
- [SDR 04FDEA03436](https://openairdocs.org/sdr/04FDEA03436.md): Skin · cracked · Dec 17, 2004 · N166FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERNAL 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.
- [SDR 04FDEA03411](https://openairdocs.org/sdr/04FDEA03411.md): Spar · cracked · Dec 14, 2004 · N166FE · Boeing 727100 · Horizontal Stabilizer, Spar/Rib
  > WHILE 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.
- [SDR 04FDEA03404](https://openairdocs.org/sdr/04FDEA03404.md): Web · corroded · Dec 10, 2004 · N166FE · Boeing 727100 · Horizontal Stabilizer Structure
  > CORROSION 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.
- [SDR 04FDEA03401](https://openairdocs.org/sdr/04FDEA03401.md): Skin · damaged · Dec 9, 2004 · N166FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > COMPLY 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.
- [SDR 04FDEA03181](https://openairdocs.org/sdr/04FDEA03181.md): Skin · gouged · Nov 22, 2004 · N166FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > UPPER 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.
- [SDR 04FDEA03164](https://openairdocs.org/sdr/04FDEA03164.md): Skin · corroded · Nov 18, 2004 · N166FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > CORROSION 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 7-533
- [SDR 04FDEA03165](https://openairdocs.org/sdr/04FDEA03165.md): Hinge · corroded · Nov 18, 2004 · N166FE · Boeing 727100 · Leading Edge Devices
  > CORROSION ON LT WING NR 1 K-FLAP O/B BULLNOSE HINGE LUG AROUND FASTENERS UPPER SURFACE.
- [SDR 04FDEA03163](https://openairdocs.org/sdr/04FDEA03163.md): Attach Fitting · damaged · Nov 18, 2004 · N166FE · Boeing 727100 · Wing, Control Surface Attach Fittings
  > LT WING FIXED TRAILING EDGE O/B AILERON O/B ATTACH FITTING.
- [SDR 04FDEA03109](https://openairdocs.org/sdr/04FDEA03109.md): Frame · corroded · Nov 15, 2004 · N166FE · Boeing 72722 · Emergency Exits
  > CORROSION LT FWD EMERGENCY ESCAPE DOOR UNDER SIDE OF LWR FRAME BACK SIDE OF OUTER SKIN 7 INCH UP FROM LWR AFT CORNER.
- [SDR 04FDEA03108](https://openairdocs.org/sdr/04FDEA03108.md): Frame · dented · Nov 15, 2004 · N166FE · Boeing 72722 · Fuselage Main, Frame
  > FRAME BS 1010 LT BETWEEN STR 24 AND 25 DENTED.
- [SDR 04FDEA03107](https://openairdocs.org/sdr/04FDEA03107.md): Floorbeam · damaged · Nov 15, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION MECHANICAL DAMAGE ON FLOORBEAM BS 680 UPPER CHORD LWR SURFACE AT LBL 64 WL 208.
- [SDR 04FDEA03106](https://openairdocs.org/sdr/04FDEA03106.md): Frame · dented · Nov 15, 2004 · N166FE · Boeing 72722 · Fuselage Main, Frame
  > AFT CARGO FRAME DENTED AT BS 970, STR 26R.
- [SDR 04FDEA03100](https://openairdocs.org/sdr/04FDEA03100.md): Structure · cracked · Nov 12, 2004 · N166FE · Boeing 72722 · Leading Edge Devices
  > LT 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.
- [SDR 04FDEA03076](https://openairdocs.org/sdr/04FDEA03076.md): Spar · cracked · Nov 11, 2004 · N166FE · Boeing 727100 · Horizontal Stabilizer, Spar/Rib
  > N01167 CORROSION ON LT. HORIZ. STAB UPPER SPAR AT STAB STA. 198. REPAIRED PER SRM 55-10-5 FIG 1
- [SDR 04FDEA03082](https://openairdocs.org/sdr/04FDEA03082.md): Frame · dented · Nov 11, 2004 · N166FE · Boeing 72722 · Fuselage Main, Frame
  > FRAME BS 990 LT AT STR 24 DENTED. REPAIRED PER SRM 51-40-3.
- [SDR 04FDEA03081](https://openairdocs.org/sdr/04FDEA03081.md): Skin · bulged · Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > RT 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.
- [SDR 04FDEA03077](https://openairdocs.org/sdr/04FDEA03077.md): Stringer · gouged · Nov 11, 2004 · N166FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > MAIN 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.
- [SDR 04FDEA03079](https://openairdocs.org/sdr/04FDEA03079.md): Floorbeam · corroded · Nov 11, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED RBL 18, W/L 200. REPAIRED PER SRM 53-10-8
- [SDR 04FDEA03075](https://openairdocs.org/sdr/04FDEA03075.md): Skin · corroded · Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > RT 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 AN
- [SDR 04FDEA03074](https://openairdocs.org/sdr/04FDEA03074.md): Spar · corroded · Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Spar/Rib
  > CORROSION 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.
- [SDR 04FDEA03073](https://openairdocs.org/sdr/04FDEA03073.md): Spar · corroded · Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Spar/Rib
  > CORROSION 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.
- [SDR 04FDEA03071](https://openairdocs.org/sdr/04FDEA03071.md): Floorbeam · corroded · Nov 10, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION 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.
- [SDR 04FDEA03068](https://openairdocs.org/sdr/04FDEA03068.md): Floorbeam · damaged · Nov 10, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor Beam
  > MECHANICAL DAMAGE ON FLOORBEAM STA 700 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8
- [SDR 04FDEA03062](https://openairdocs.org/sdr/04FDEA03062.md): Hinge Fitting · corroded · Nov 9, 2004 · N166FE · Boeing 72722 · Wing, Control Surface Attach Fittings
  > CORROSION 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.
- [SDR 04FDEA03056](https://openairdocs.org/sdr/04FDEA03056.md): Frame · dented · Nov 9, 2004 · N166FE · Boeing 72722 · Fuselage Main, Frame
  > FRAME BS 1030 LT AT STR 24 AND 25, DENTED. REPAIRED FRAME PER SRM 51-40-3.
- [SDR 04FDEA03055](https://openairdocs.org/sdr/04FDEA03055.md): Floorbeam · damaged · Nov 9, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor Beam
  > MECHANICAL DAMAGE ON FLOORBEAM BS 720 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8
- [SDR 04FDEA03032](https://openairdocs.org/sdr/04FDEA03032.md): Frame · dented · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO FRAME DENTED AT BS. 1010 STR 26R. REPAIRED PER SRM 51-40-3
- [SDR 04FDEA03029](https://openairdocs.org/sdr/04FDEA03029.md): Frame · dented · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Frame
  > AFT CARGO FRAME DENTED AT BS 1030, STR 26R. REPAIRED PER SRM 51-40-3.
- [SDR 04FDEA03028](https://openairdocs.org/sdr/04FDEA03028.md): Frame · dented · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Frame
  > AFT CARGO FRAME DENTED AT BS 990 STR 26 LT. REPAIRED PER SRM 51-40-3, 51-10-2 AND 51-30-2.
- [SDR 04FDEA03027](https://openairdocs.org/sdr/04FDEA03027.md): Skin · dented · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > BS 294, STR 21 RT, DENTS AROUND 3 FASTENERS. REPAIRED PER SRM 53-30-1, 53-30-3.
- [SDR 04FDEA03045](https://openairdocs.org/sdr/04FDEA03045.md): Floorbeam · corroded · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FOUND 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.
- [SDR 04FDEA03044](https://openairdocs.org/sdr/04FDEA03044.md): Web · cracked · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FUEL 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.
- [SDR 04FDEA03047](https://openairdocs.org/sdr/04FDEA03047.md): Floorbeam · corroded · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01) AT FLOORBEAM UPPER CHORD AT BS 620, LBL 45-65, WL 208.
- [SDR 04FDEA03046](https://openairdocs.org/sdr/04FDEA03046.md): Floorbeam · corroded · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM STA 620 LWR CHORD LWR SURFACE CORRODED LBL 8 AROUND NUTPLATE HOLE. REPAIRED PER SRM 53-10-1, 53-10-8
- [SDR 04FDEA03043](https://openairdocs.org/sdr/04FDEA03043.md): Stringer · gouged · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > MAIN CARGO BAY HAS GOUGE ON STRINGER 9R AT BS 600.
- [SDR 04FDEA03042](https://openairdocs.org/sdr/04FDEA03042.md): Web · cracked · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FUEL 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, 51-10-2
- [SDR 04FDEA03041](https://openairdocs.org/sdr/04FDEA03041.md): Stringer Clip · cracked · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED, STR 5L, BS 1010. REPLACED PER SRM 51-30-2, 51-30-5
- [SDR 04FDEA03040](https://openairdocs.org/sdr/04FDEA03040.md): Seat Track · gouged · Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK GOUGED AT BS 740, RBL 45, WL 208. REPAIRED SEAT TRACK PER SRM 53-10-5.
- [SDR 04FDEA03039](https://openairdocs.org/sdr/04FDEA03039.md): Stringer Clip · cracked · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED BS 1108 LT STR 20. REPLACED STRINGER CLIP PER SRM 51-30-2.
- [SDR 04FDEA03038](https://openairdocs.org/sdr/04FDEA03038.md): Door Frame · damaged · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Structure
  > BS 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.
- [SDR 04FDEA03037](https://openairdocs.org/sdr/04FDEA03037.md): Stringer · gouged · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > GOUGE 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.
- [SDR 04FDEA03036](https://openairdocs.org/sdr/04FDEA03036.md): Frame · dented · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Frame
  > FWD 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.
- [SDR 04FDEA03035](https://openairdocs.org/sdr/04FDEA03035.md): Frame · dented · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Frame
  > FWD 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.
- [SDR 04FDEA03034](https://openairdocs.org/sdr/04FDEA03034.md): Frame · dented · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Frame
  > TOP 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 51-40-3
- [SDR 04FDEA03033](https://openairdocs.org/sdr/04FDEA03033.md): Rib · cracked · Nov 8, 2004 · N166FE · Boeing 727100 · Elevator, Spar/Rib
  > RT 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.
- [SDR 04FDEA03031](https://openairdocs.org/sdr/04FDEA03031.md): Frame · dented · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Frame
  > FRAME DENTED AT BS 1090, STR 23 LT. REPAIRED PER SRM 51-40-3.
- [SDR 04FDEA03030](https://openairdocs.org/sdr/04FDEA03030.md): Frame · dented · Nov 8, 2004 · N166FE · Boeing 727100 · Fuselage Main, Frame
  > AFT CARGO FRAME DENTED AT BS 990, STR 26R. REPAIRED PER SRM 51-40-3.

Next page: https://openairdocs.org/deregistered/N166FE-2007-08-21/reports.md?page=2

## 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 = 'N166FE' AND deregistration_id = 'N166FE-2007-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N166FE-2007-08-21/reports

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