# Service difficulty reports: N169FE, cancelled Jun 7, 2004

A list on [N169FE, cancelled Jun 7, 2004](https://openairdocs.org/deregistered/N169FE-2004-06-07.md).

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

- [SDR 02FDEA00290](https://openairdocs.org/sdr/02FDEA00290.md): Hydraulic Line · leaking · Apr 25, 2002 · N169FE · Boeing 72722 · Hydraulic System, Main
  > HYDRAULIC A-QTY TO ZERO IN FLT. REMOVED AND REPLACED NR 1 ENG A-SYSTEM HYDRAULIC PRESS LINE. REMOVED AND REPLACED 1 & 2 ENGINE HYD PUMP CASE DRAIN FILTERS PER MM 29-11-041-2.
- [SDR 00FDEA00887](https://openairdocs.org/sdr/00FDEA00887.md): Sensor · failed · Dec 19, 2000 · N169FE · Boeing 72722 · Stall Warning System
  > 00-366 AFT T/O STICK SHAKER ACTIVATED. PULLED AC STALL WARN NR 1 CIRCUIT BREAKER & RETURN FOR LAND. R&R RIGHT ANGLE OF ATTACK SENSOR IAW 727 MM 34-18-51, NR 1 STALL WARNING SYS OPERATIONAL CHECK NORMAL IAW 727 MM 34-18-0. OK TO CONTINUE.
- [SDR 98FDEA00612](https://openairdocs.org/sdr/98FDEA00612.md): Floorbeam · corroded · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > BS 680 CORROSION ON BOTTOM SIDE OF FLOORBEAM LWR FLANGE AT SEV AREAS. BLENDED OUT CORROSION PER EA 7-5310-29662 DATED 9-14-98. INSTALLED.071 7075-T6 ANGLES ON FWD AND AFT FLANGES PER AARD 53-10-7-2 AND EA 7-5310-29662.
- [SDR 98FDEA00611](https://openairdocs.org/sdr/98FDEA00611.md): Frame · cracked · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > AFT CARGO FWD DOOR PORTAL FRAME CRACKED AT LOWER FWD DOOR STOP, OUTBD LWR FAST. REMOVED AND REPLACED AFT CARGO FWD DOOR PORTAL FRAME PER SRM 51-10-1.
- [SDR 98FDEA00610](https://openairdocs.org/sdr/98FDEA00610.md): Skin · corroded · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN 25 PERCENT LOBE OF MATERIAL BETWEEN STR 25R-26R, BS 360. CUT OUT CORROSION, INSTALLED DOUBLER AND FILLER ON OUTSIDE OF SKIN EXTENDING 3 ROWS BELOW SKIN LAP PER EA 7-5330-29666. DATED 9/18/98 AND SRM 53-30-3.
- [SDR 98FDEA00609](https://openairdocs.org/sdr/98FDEA00609.md): Floorbeam · damaged · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > UPPER LOBE FLOORBEAM HAS DOUBLER DRILL HOLE BS 990. CUT OUT DAMAGE, INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.
- [SDR 98FDEA00608](https://openairdocs.org/sdr/98FDEA00608.md): Floorbeam · damaged · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM HAS ONE DOUBLE DRILL HOLE BS 1010, RBL 63. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-07-02 FIG 3 AND EA 7-5310-29648.
- [SDR 98FDEA00607](https://openairdocs.org/sdr/98FDEA00607.md): Floorbeam · damage · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FLOORBEAM CUT ACROSS TOP FLANGE BS 1130, RBL 63. BLENDED OUT DAMAGE AND INSTALLED.080 STRAP OF 7075-T6 ALUM PER AARD 53-10-07-01 AND 7-5310-29698.
- [SDR 98FDEA00606](https://openairdocs.org/sdr/98FDEA00606.md): Floorbeam · damaged · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM CUT ACROSS TOP FLANGE BS 1050, RBL 63. CUT OUT DAMAGE, INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.
- [SDR 98FDEA00605](https://openairdocs.org/sdr/98FDEA00605.md): Floorbeam · damaged · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM CUT ACROSS TOP FLANGE AT STR 970, RBL 63. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.
- [SDR 98FDEA00603](https://openairdocs.org/sdr/98FDEA00603.md): Floorbeam · corroded · Sep 25, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > UPPER LOBE, BS 1050 HEAVY CORROSION ON LWR FWD LEG OF FLOORBEAM AT LBL 29. BLENDED OUT CORROSION IN AREA NOTED PER SRM 51-10-6. BLENDED AREA OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER ON FLOORBEAM PER AARD 53-10-07-2.
- [SDR 98FDEA00613](https://openairdocs.org/sdr/98FDEA00613.md): Floorbeam · corroded · Sep 16, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM BS 1050, LWR CHORD HAS CORROSION FROM RBL 24- RBL 43. INSTALLED FLOORBEAM REPAIR LWR CHORD PER SRM 53-10-8 PG 11-17.
- [SDR 98FDEA00602](https://openairdocs.org/sdr/98FDEA00602.md): Floorbeam · corroded · Sep 16, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > UPPER LOBE HEAVY CORROSION ON UPPER SURFACE OF LWR FLANGE OF FLOORBEAM BS 1050, RBL 39. INSTALLED FLOORBEAM LWR CHORD REPAIR PER SRM 53-10 8 PG 11-17.
- [SDR 98FDEA00601](https://openairdocs.org/sdr/98FDEA00601.md): Floorbeam · misdrilled · Sep 14, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > UPPER LOBE FLOORBEAM BS 1070, RBL 625 HAS DOUBLE DRILL HOLE IN FLOORBEAM. CUT OUT AREA OF DAMAGE AND REPAIR PER AARD 53-10-07.
- [SDR 98FDEA00559](https://openairdocs.org/sdr/98FDEA00559.md): Floorbeam · corroded · Sep 9, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR 0936 - UPPER LOBE, FLOORBEAM BS 680 CORROSION ON UPPER FLANGE LBL 10- RBL 6. CORROSION REMOVAL OUT OF LIMITS AT LBL 5 FWD SIDE OF FLANGE. INSTALLED ANGLE DOUBLER PER AARD 53-10-07-2.
- [SDR 98FDEA00557](https://openairdocs.org/sdr/98FDEA00557.md): Skin · damaged · Sep 9, 1998 · N169FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR 0698 - LFEC IND 10 PERCENT MATERIAL LOSS JUST ABOVE STR 23 LT, 2 AFT OF BS 360 FRAME. DAMAGED AREA, REMOVED AND REPLACED DOUBLER INSTALLED PER SRM 53-30-3 PG 14B-14D.
- [SDR 98FDEA00556](https://openairdocs.org/sdr/98FDEA00556.md): Skin · corroded · Sep 9, 1998 · N169FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR 0342 - UPPER LOBE BS 886 HEAVY CORROSION AT WINDOW BELT AND ON SKIN 8 ABOVE STR 14L. REMOVED CORROSION FRAME WAS TAKEN OUT OF LIMITS. WINDOW FRAME REPLACED FOR EA 7-5330-29636 AND SRM 51-30-2 DOUBLER INSTALL PER EA 7-5330-29636.
- [SDR 98FDEA00549](https://openairdocs.org/sdr/98FDEA00549.md): Skin · damaged · Aug 26, 1998 · N169FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > LOW FREQ EDDY CURRENT IND 15 PERCENT MATERIAL LOSS BS 360 AFT FASTENER ROW STR 4 RT BOTTOM OF SKIN LAP TO ONE INCH BELOW. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 5.
- [SDR 98FDEA00550](https://openairdocs.org/sdr/98FDEA00550.md): Floorbeam · corroded · Aug 18, 1998 · N169FE · Boeing 72722 · Fuselage Main, Floor Beam
  > UPPER LOBE BS 380 HEAVY CORROSION ON FLOORBEAM AT LBL 34. REMOVED CORROSION PER SRM 51-10-6. CORROSION REMOVAL OUT OF LIMITS. INSTALLED REPAIR PER AARD 53-10-07-2 PG 1 AND 2 FIG 3.
- [SDR 97FDEA00299](https://openairdocs.org/sdr/97FDEA00299.md): Engine · failed · May 21, 1997 · N169FE · Boeing 72722 · Engine (Turbine/Turboprop)
  > PASSING 16,000 FEET ON DESCENT POWER AT IDLE, NR 2 ENGINE FLAMED OUT. ONLY ABNORMAL INDICATION WAS ZERO OIL PRESSURE. QUANTITY OK WITH N1 ROTATION. NO N2 WAS OBSERVED. FOUND OIL SCREEN FULL OF METAL. REMOVED AND REPLACED NR 2 ENGINE PER WORK CARD 70T0502 A
- [SDR 96FDEA00194](https://openairdocs.org/sdr/96FDEA00194.md): Fitting · cracked · Feb 7, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CRACK IN HOLES NR 2 AND NR 4 OF ROW 2, FWD O/B FLANGE, AT BS 870 JUST BELOW STR 9R. REPAIRED CRACK IN HOLES NR 2 AND NR 4 OF ROW 2 FWD O/B FLANGE, AT BS 870 JUST BELOW STR 9R PER FEDEX EA 7-5310-26957.
- [SDR 96FDEA00193](https://openairdocs.org/sdr/96FDEA00193.md): Skin · corroded · Feb 6, 1996 · N169FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN INTERIOR AT BS 875 TO 878 BELOW STR 9R. REPAIRED CORROSION ON INTERIOR SKIN AT BS 875 TO 878 BELOW STR 9R PER FEDEX EA 7-5310-26957.
- [SDR 96FDEA00192](https://openairdocs.org/sdr/96FDEA00192.md): Fitting · cracked · Feb 6, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DURING UT INSPECTION, CRACK INDICATION FOUND AT FUSE BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6. REPAIRED CRACK AT BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6 PER FEDEX EA'S 7-5310-26957 AND 7-5310-26913.
- [SDR 96FDEA00183](https://openairdocs.org/sdr/96FDEA00183.md): Stiffener · corroded · Feb 2, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-03-1/2), ON VERTICAL STIFFENER BS 336 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.
- [SDR 96FDEA00182](https://openairdocs.org/sdr/96FDEA00182.md): Stiffener · corroded · Feb 2, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION (C53-111-03-1/2), ON VERTICAL STIFFENER BS 319 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.
- [SDR 96FDEA00167](https://openairdocs.org/sdr/96FDEA00167.md): Fitting · cracked · Feb 1, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CRACK IN AFT FLANGE OF TERMINAL FITTING AT BS 870 STR 13R. HFEC DAMAGE FABRICATED REPAIR PARTS AND INSTALLED PER EWO NR 96-2-43.
- [SDR 96FDEA00157](https://openairdocs.org/sdr/96FDEA00157.md): Rib · corroded · Jan 31, 1996 · N169FE · Boeing 72722 · Leading Edge Devices
  > CORROSION ON NR 6 K-FLAP MOST OUTBOARD RIB WHERE LANDING LIGHT CONDUIT ATTACHES TO RIB UPPER BOLT HOLE. REMOVED CORROSION, REPAIRED PER EWO NR 96-2025.
- [SDR 96FDEA00156](https://openairdocs.org/sdr/96FDEA00156.md): Hinge · corroded · Jan 31, 1996 · N169FE · Boeing 72722 · Ailerons
  > RIGHT WING OUTBOARD AILERON INBOARD HINGE FITTING IS CORRODED (NR 2 HINGE FITTING). REMOVED CORROSION, FABRICATED REPAIR ANGLE ON FLANGE ON RIGHT WING OUTBOARD AILERON HINGE FITTING IAW FEDEX EA 7-5750-26969.
- [SDR 96FDEA00155](https://openairdocs.org/sdr/96FDEA00155.md): Skin · dented · Jan 31, 1996 · N169FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DENT TO SKIN DUE TO TOOL BOX AT STA 1083 AND BETWEEN STR 28 - 29L. REPAIRED DAMAGED SKIN AT BS 1083, BETWEEN STR 28 - 29L PER FEDEX SRM 53-30-3 PER ENGINE REPAIR REQUEST REPLY. MFG PART NUMBER M502776.
- [SDR 96FDEA00137](https://openairdocs.org/sdr/96FDEA00137.md): Fitting · corrosion · Jan 26, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION ON STR TO FRAME TIE AT BS 360 STR 20L. REMOVED AND REPLACED STR TIE AT BS 360 20L, DUE TO CORROSION OUT OF LIMITS.
- [SDR 96FDEA00136](https://openairdocs.org/sdr/96FDEA00136.md): Fitting · cracked · Jan 26, 1996 · N169FE · Boeing 72722 · Vertical Stabilizer
  > LT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IS CRACKED. REPAIRED LT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IAW FEDEX EA 7-5510-26907.
- [SDR 96FDEA00135](https://openairdocs.org/sdr/96FDEA00135.md): Stringer · delamination · Jan 26, 1996 · N169FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > DELAMINATION OF SKIN LAP STRINGER 19L BS 360 TO 368. REMOVED FASTENERS IN SKIN LAP AT STR 19L. UPON REMOVAL OF FASTENERS FOUND NO FURTHER INDICATIONS OF DELAMINATION. INSTALLED NEW STR TIE AND INSTALLED STR 19 SPLICE. ALL WORK DONE IAW FEDEX SRM 53-10-3.
- [SDR 96FDEA00077](https://openairdocs.org/sdr/96FDEA00077.md): Fitting · cracked · Jan 19, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DURING UT INSP, CRACK IND FOUND AT FUSE BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6. REPAIRED CRACK AT BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6 PER FEDEX EA'S 7-5310-26957 AND 7-5310-26913.
- [SDR 96FDEA00076](https://openairdocs.org/sdr/96FDEA00076.md): Fitting · cracked · Jan 19, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CRACK IN AFT FLANGE OF TERMINAL FITTING AT BS 870 STR 13R. HFEC DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER EWO NR 96-2043.
- [SDR 96FDEA00075](https://openairdocs.org/sdr/96FDEA00075.md): Skin · lightning strike · Jan 19, 1996 · N169FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES AT BS 706, 793, 824 AND 888 BETWEEN STR 4 AND 5. REPAIRED LIGHTNING STRIKES AT BS 750, 793, 824 BY INSTALLING NEW FASTENERS. REPAIRED BS 888 BY CUTTING OUT DAMAGED AREA AND FABRICATING REPAIR PARTS. INSTALLED IAW 53-30-3.
- [SDR 96FDEA00074](https://openairdocs.org/sdr/96FDEA00074.md): Skin · chafing · Jan 19, 1996 · N169FE · Boeing 72722 · Trailing Edge Flaps
  > RT WING I/B FOREFLAP IS CHAFING APPROX 24 INCHES O/B FROM I/B LEADING EDGE. REPAIRED DAMAGE AREA ON RT WING I/B FOREFLAP APPROX 24 INCHES O/B FROM I/B LEADING EDGE.
- [SDR 96FDEA00078](https://openairdocs.org/sdr/96FDEA00078.md): Skin · corroded · Jan 18, 1996 · N169FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN INTERIOR AT BS 875 TO 878 BELOW STR 9R. REPAIRED CORROSION ON INTERIOR SKIN AT BS 875 TO 878 BELOW STR 9R PER FEDEX EA 7-5310-26957.
- [SDR 96FDEA00067](https://openairdocs.org/sdr/96FDEA00067.md): Te Skin · disbonded · Jan 18, 1996 · N169FE · Boeing 72722 · Trailing Edge Flaps
  > RIGHT WING INBD FORE FLAP UPPER SURFACE HAS DISBOND ON T/E AREA MARKED. REPAIRED RT WING INBOARD FORE FLAP IAW SRM 51-40-6.
- [SDR 96FDEA00066](https://openairdocs.org/sdr/96FDEA00066.md): Stringer · corroded · Jan 18, 1996 · N169FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > CORROSION (C53-224-03-1/2) ON STR 22R, BS 396. REMOVED CORROSION AT BS 396, STR 22R. REMOVED IN A 1 INCH BY 2 INCH AREA. ORIGINAL METAL THICKNESS IS.040 INCH. REMOVED.009 INCH, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED AND INSTALLED RE
- [SDR 96FDEA00065](https://openairdocs.org/sdr/96FDEA00065.md): Stiffener · corroded · Jan 17, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION (C53-111-03-1/2), ON VERTICAL STIFFENER BS 319 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.
- [SDR 96FDEA00060](https://openairdocs.org/sdr/96FDEA00060.md): Skin · gouged · Jan 17, 1996 · N169FE · Boeing 72722 · Trailing Edge Flaps
  > THERE'S A GOUGE ON THE RT WING FOREFLAP UPPER SURFACE ABOVE THE NR 8 FLAP TRACK. REMOVED AND REPLACED DAMAGE ON O/B RT WING FOREFLAP IAW FEDEX SRM 51-40-6.
- [SDR 96FDEA00064](https://openairdocs.org/sdr/96FDEA00064.md): Stiffener · corroded · Jan 15, 1996 · N169FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-03-1/2), ON VERTICAL STIFFENER, BS 336 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.

## 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 = 'N169FE' AND deregistration_id = 'N169FE-2004-06-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N169FE-2004-06-07/reports

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