# Service difficulty reports: N168FE, cancelled Jun 28, 2007

A list on [N168FE, cancelled Jun 28, 2007](https://openairdocs.org/deregistered/N168FE-2007-06-28.md).

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

- [SDR 04FDEA03385](https://openairdocs.org/sdr/04FDEA03385.md): Switch · malfunctioned · Dec 7, 2004 · N168FE · Boeing 72722 · Leading Edge Slat Position Indicating System
  > AT 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 DECLAR
- [SDR 03FDEA02042](https://openairdocs.org/sdr/03FDEA02042.md): Bellcrank · damaged · Dec 4, 2003 · N168FE · Boeing 727100 · Cargo/Baggage Doors
  > COMPLY 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.
- [SDR 03FDEA01639](https://openairdocs.org/sdr/03FDEA01639.md): Duct · loose · Sep 26, 2003 · N168FE · Boeing 727100 · Engine Bleed Air System
  > ON 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 HOT
- [SDR 01FDEA00262](https://openairdocs.org/sdr/01FDEA00262.md): Support · cracked · Apr 7, 2001 · N168FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR 01FDEA00261](https://openairdocs.org/sdr/01FDEA00261.md): Seat Track · corroded · Apr 7, 2001 · N168FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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.
- [SDR 01FDEA00260](https://openairdocs.org/sdr/01FDEA00260.md): Floorbeam · corroded · Apr 7, 2001 · N168FE · Boeing 72722 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR 01FDEA00259](https://openairdocs.org/sdr/01FDEA00259.md): Floorbeam · corroded · Apr 7, 2001 · N168FE · Boeing 72722 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR 01FDEA00227](https://openairdocs.org/sdr/01FDEA00227.md): Skin · corroded · Mar 24, 2001 · N168FE · Boeing 72722 · Fuselage Main, Structure
  > N 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.
- [SDR 01FDEA00229](https://openairdocs.org/sdr/01FDEA00229.md): Support Fitting · cracked · Mar 24, 2001 · N168FE · Boeing 72722 · Vertical Stabilizer, Spar/Rib
  > N 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.
- [SDR 01FDEA00228](https://openairdocs.org/sdr/01FDEA00228.md): Rib · cracked · Mar 24, 2001 · N168FE · Boeing 72722 · Vertical Stabilizer, Spar/Rib
  > DURING 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.
- [SDR 01FDEA00230](https://openairdocs.org/sdr/01FDEA00230.md): Intercostal · cracked · Mar 24, 2001 · N168FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR 00FDEA00896](https://openairdocs.org/sdr/00FDEA00896.md): Downlock Switch · faulty · Dec 21, 2000 · N168FE · Boeing 72722 · Landing Gear Position and Warning
  > ON 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.
- [SDR 00FDEA00320](https://openairdocs.org/sdr/00FDEA00320.md): Warning Light · illuminated · May 5, 2000 · N168FE · Boeing 72722 · Leading Edge Slat Position Indicating System
  > AFT T/O WITH FLAPS FULLY RETRACTED, NR 2 LEADING EDGE FLAP AND LEADING EDGE (AMBER) LIGHT ILLUM ON FWD PANEL.
- [SDR 98FDEA00650](https://openairdocs.org/sdr/98FDEA00650.md): Doubler · corroded · Oct 13, 1998 · N168FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > WHILE WORKING NR0186, FOUND INTERNAL DOUBLER AT BS 961 TO 990, STR 28 TO 29 RT TO BE CORRODED AND OUT OF LIMITS PER SRM.
- [SDR 98FDEA00649](https://openairdocs.org/sdr/98FDEA00649.md): Chord · corroded · Oct 13, 1998 · N168FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > WHILE 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.
- [SDR 98FDEA00644](https://openairdocs.org/sdr/98FDEA00644.md): Stringer · corroded · Oct 8, 1998 · N168FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > UPON 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.
- [SDR 98FDEA00640](https://openairdocs.org/sdr/98FDEA00640.md): Beam · corroded · Oct 7, 1998 · N168FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > WHILE 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.
- [SDR 98FDEA00619](https://openairdocs.org/sdr/98FDEA00619.md): Stringer · corroded · Oct 5, 1998 · N168FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > NR 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.
- [SDR 98FDEA00618](https://openairdocs.org/sdr/98FDEA00618.md): Stringer · corroded · Oct 5, 1998 · N168FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > CORROSION (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.
- [SDR 98FDEA00597](https://openairdocs.org/sdr/98FDEA00597.md): Keel Beam · corroded · Sep 28, 1998 · N168FE · Boeing 72722 · Fuselage Main, Keel
  > CORROSION 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.
- [SDR 98FDEA00596](https://openairdocs.org/sdr/98FDEA00596.md): Beam · corroded · Sep 28, 1998 · N168FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR 98FDEA00595](https://openairdocs.org/sdr/98FDEA00595.md): Keel Beam · corroded · Sep 28, 1998 · N168FE · Boeing 72722 · Fuselage Main, Keel
  > CORROSION 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.
- [SDR 96FDEA01694](https://openairdocs.org/sdr/96FDEA01694.md): Switch Spacer · missing · Nov 27, 1996 · N168FE · Boeing 72722 · Leading Edge Slat Control System
  > NR 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 MAINT
- [SDR 96FDEA01179](https://openairdocs.org/sdr/96FDEA01179.md): Gusset · cracked · Jun 25, 1996 · N168FE · Boeing 727123 · Fuselage Miscellaneous Structure
  > CABIN 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.
- [SDR 96FDEA01181](https://openairdocs.org/sdr/96FDEA01181.md): Bell Frame · crack · Jun 24, 1996 · N168FE · Boeing 727123 · Fuselage Main, Frame
  > FORWARD 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.
- [SDR 96FDEA01180](https://openairdocs.org/sdr/96FDEA01180.md): Floor Beam · corrosion · Jun 24, 1996 · N168FE · Boeing 72722 · Fuselage Main, Floor Beam
  > MAIN 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.

## 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 = 'N168FE' AND deregistration_id = 'N168FE-2007-06-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N168FE-2007-06-28/reports

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