# Service difficulty reports: N254FE, cancelled Apr 25, 2013

A list on [N254FE, cancelled Apr 25, 2013](https://openairdocs.org/deregistered/N254FE-2013-04-25.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 · 58 reports

- [SDR 08FDEA00322](https://openairdocs.org/sdr/08FDEA00322.md): Power Unit · malfunctioned · Jan 29, 2008 · N254FE · Boeing 727233 · Fire Detection
  > SHORTLY AFTER TAKEOFF LIGHT IN APU FIRE HANDLE FLICKERED FOR SEVERAL MINUTES, FOLLOWED BY A STEADY LIGHT. NO OTHER FIRE INDICATIONS WERE NOTED. APU FIRE HANDLE PULLED, BOTTLE BLOWN. REMOVED AND REPLACED OPERATING POWER UNIT FOR APU FIRE DETECTION IAW B727-2
- [SDR 07FDEA02925](https://openairdocs.org/sdr/07FDEA02925.md): Web · corroded · Aug 15, 2007 · N254FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT BETWEEN BS 580-600 S28R OUTER WEB LOWER ANGLE HAS SURFACE CORROSION. REMOVED AND REPLACED WEB IAW SRM 51-30-2. FABRICATED WEB ON TRAVELER T7/695113.
- [SDR 07FDEA02923](https://openairdocs.org/sdr/07FDEA02923.md): Web · cracked · Aug 15, 2007 · N254FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > CABIN FS 1183 BULKHEAD LT OB FLOOR WEB HAS CRACKS. REMOVED AND REPLACED FLOOR WEB IAW SRM 51-30-2. FABRICATED NEW FLOOR WEB.020 ON TRAVELER T7/1695713 IAW SRM 51-30-6 TABLE 1.
- [SDR 07FDEA02922](https://openairdocs.org/sdr/07FDEA02922.md): Skin · dented · Aug 15, 2007 · N254FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXT FUSELAGE SKIN DENT APPROX STA 1153 BETWEEN S-17L - S-19L, REPAIRED IAW SRM 53-30-3.
- [SDR 07FDEA02924](https://openairdocs.org/sdr/07FDEA02924.md): Door Frame · cracked · Aug 15, 2007 · N254FE · Boeing 727233 · Fuselage Main, Structure
  > LT AFT SERVICE DOOR FWD UPPER CAM ROLLER FRAME HAS A CRACK. REMOVED AND REPLACED FWD FRAME IAW SRM 51-30-2.
- [SDR 07FDEA02824](https://openairdocs.org/sdr/07FDEA02824.md): Panel · corroded · Aug 10, 2007 · N254FE · Boeing 727233 · Wing, Plate/Skin
  > RT WING T/E LOWER HINGE PANEL 8506R INNER SURFACE HAS CORROSION AROUND EDGE REPAIRED IAW SRM 51-20-151-7.
- [SDR 07FDEA02823](https://openairdocs.org/sdr/07FDEA02823.md): Support · cracked · Aug 10, 2007 · N254FE · Boeing 727233 · Wing Miscellaneous Structure
  > LT WING AT T/E REAR SPAR AREA APROX RS STA 383 UPPER FIXED PANEL LOWER C CHANNEL BRACKET MOUNT SUPPORT HAS A CRACK AT FWD SECTION ABOVE NR 3 TRANS ASSY. REMOVED AND REPLACED C CHANNEL SUPPORT IAW SRM 51-30-2. C CHANNEL SUPPORT, FABRICATED ON TRAVELER NR T7
- [SDR 07FDEA02822](https://openairdocs.org/sdr/07FDEA02822.md): Skin · cracked · Aug 10, 2007 · N254FE · Boeing 727233 · Landing Gear Doors
  > LT MLG FLYING DOOR UPPER MID INNER SKIN EDGE CRACKED REPAIRED IAW SRM 51-40-2.
- [SDR 07FDEA02756](https://openairdocs.org/sdr/07FDEA02756.md): Rib · cracked · Aug 3, 2007 · N254FE · Boeing 727233 · Wing, Rib/Bulkhead
  > RT WING L/E SLAT NR 5 INBD END PORK CHOP SEAL MOUNTING PLATE DEFORMED AND CRACKED. REMOVED CRACKED RIB, FABBED NEW RIB ON TRAVLER T/682663. INSTALLED NEW RIB.
- [SDR 06FDEA03609](https://openairdocs.org/sdr/06FDEA03609.md): Valve · leaking · Oct 11, 2006 · N254FE · Boeing 727233 · Aircraft Fuel System
  > NR 1 ENG FAILED DURING FLIGHT. 1ST INDICATION WAS EXCESSIVE NR 1 FUEL FLOW AND 2 KNOB DIFF BETWEEN NR 1 THRUST LEVER AND NR 2/3. JUST PRIOR TO FAILURE, NR 1 EPR 1.6 (2/3 EPRS 1.8). NR 1 N1 80 NR 2/3 N1S 85) N2 86 (NR 2/3 N2S 88/90) NR 1 FF 4000 (2/3 3400).
- [SDR 05FDEA03008](https://openairdocs.org/sdr/05FDEA03008.md): Indicator · inoperative · Sep 20, 2005 · N254FE · Boeing 727233 · Airspeed/Mach Indicator
  > CAPTAINS AIRSPEED INDICATOR DID NOT INDICATE AIRSPEED ON T/O. ACN RELEASED FOR SERVICE PER MEL/CDL: 20-01 CATEGORY: X RVSM ITEM "MEL 20-01: DO NOT OPERATE AIRCRAFT WITHIN RVSM AIRSPACE." "NO RVSM OPERATIONS". R/R CADC PER M/M 34-12-011-4, OPS CHECK GOOD. DE
- [SDR 05FDEA01587](https://openairdocs.org/sdr/05FDEA01587.md): Connector · dirty · Jun 7, 2005 · N254FE · Boeing 727200 · Door Warning System
  > ON T/O MCD A LIGHTS ON FWD ILLUM. FOLLOWED QRH RED TABS AND RETURNED TO AFW. A LIGHT WENT OUT ON FINAL. MAIN CARGO DOOR WARNING LIGHT SYSTEM (A OR B) INOP. VERIFY DOOR CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT. CLEANED CONNECTOR ON SYS-A MICROSWITCH PER S
- [SDR 05FDEA01371](https://openairdocs.org/sdr/05FDEA01371.md): Skin Panel · gouged · May 18, 2005 · N254FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > COMPLY WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. COMPLIED WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. THIS IS A MAJOR REPAIR.
- [SDR 05FDEA01360](https://openairdocs.org/sdr/05FDEA01360.md): Fairing · cracked · May 17, 2005 · N254FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING LOWER T/E FLAP TRACK SKATE FAIRING BEHIND MLG STRUT IS CRACKED. REMOVED AND REPLACED SKATE FAIRING IAW SRM 51-30-2.
- [SDR 05FDEA01359](https://openairdocs.org/sdr/05FDEA01359.md): Floorbeam · damaged · May 17, 2005 · N254FE · Boeing 727233 · Fuselage Main, Floor Beam
  > FLOORBEAM LBL 7-RBL 40 UPPER CHORD REQUIRES MAJOR REPAIR. REMOVED AND REPLACED UPPER T-CHORD IAW SRZ 53-034E REPAIR NR 7.
- [SDR 05FDEA01358](https://openairdocs.org/sdr/05FDEA01358.md): Insulation · damaged · May 17, 2005 · N254FE · Boeing 727233 · Cargo Compartments
  > EQUIPMENT AND FURNISHINGS INSULATION BLANKETS. PARTIAL REPLACEMENT STA 360-1183, MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81692.
- [SDR 05FDEA01289](https://openairdocs.org/sdr/05FDEA01289.md): Retainer · corroded · May 15, 2005 · N254FE · Boeing 727233 · Landing Gear Doors
  > LT NOSE GEAR AFT DOOR SEAL RETAINER CORRODED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2.
- [SDR 05FDEA01288](https://openairdocs.org/sdr/05FDEA01288.md): Insulation · damaged · May 15, 2005 · N254FE · Boeing 727233 · Accessory Compartment
  > COMPLY WITH EA 7-2580-81691 "EQUIPMENT AND FURNISHINGS. INSULATION BLANKETS, PARTIAL REPLACEMENT, STA 178-294, LOWER SECTION 41 INCH.
- [SDR 05FDEA01260](https://openairdocs.org/sdr/05FDEA01260.md): Angle · corroded · May 12, 2005 · N254FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > STA 740 STR 27R CORROSION FOUND ON LOWER LEG OF ANGLE. REMOVED AND REPLACED ANGLE IAW EA 7-5310-55482 ON N/R CARD S00011.
- [SDR 05FDEA01259](https://openairdocs.org/sdr/05FDEA01259.md): Doubler · corroded · May 12, 2005 · N254FE · Boeing 727233 · Fuselage Main, Bulkhead
  > FUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION. COMPLIED WITH EA 7-5310-55482 FUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION AT MAE. THIS IS A MAJOR REPAIR.
- [SDR 05FDEA01231](https://openairdocs.org/sdr/05FDEA01231.md): Clip · corroded · May 10, 2005 · N254FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > RT MLG WHEEL WELL ABOVE UPLOCK MECHANISM WEB UPPER SURFACE BETWEEN STA 930 - 940 SURFACE CORROSION. REMOVED AND REPLACED CLIP IAW SRM 51-30-2.
- [SDR 05FDEA01226](https://openairdocs.org/sdr/05FDEA01226.md): Seat Track · damaged · May 6, 2005 · N254FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BL 0 STA 720F HAS AN EXISTING SPLICE REPAIR AND DOES NOT MEET REQUIREMENTS OF DWG 2902. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF TRACK WITH REPAIR ANGLES IAW SRM 51-10-5 FIG 1.
- [SDR 05FDEA01225](https://openairdocs.org/sdr/05FDEA01225.md): Panel · cracked · May 6, 2005 · N254FE · Boeing 727200 · Flight Compartment Equipment
  > BELOW CAPTAINS PEDALS RACEWAY (PANEL) HAVE CRACKS. REMOVED AND REPLACED RACEWAYS (PANELS) IAW SRM 51-30-2.
- [SDR 05FDEA01212](https://openairdocs.org/sdr/05FDEA01212.md): Support Angle · cracked · May 5, 2005 · N254FE · Boeing 727200 · Wing Miscellaneous Structure
  > LEFT WING LOWER FIXED T/E PANEL SUPPORT ANGLE CRACKED AT STA WS 522. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2.
- [SDR 05FDEA01211](https://openairdocs.org/sdr/05FDEA01211.md): Gate · corroded · May 5, 2005 · N254FE · Boeing 727200 · Service Doors
  > GALLEY DOOR LWR FLAPPER ASSY INNER STRUCTURE HAS CORROSION (MAG ALLOY ASSY). REMOVED AND REPLACED GALLEY DOOR LWR GATE IAW OHM 52-16-01.
- [SDR 05FDEA01210](https://openairdocs.org/sdr/05FDEA01210.md): Hinge · cracked · May 5, 2005 · N254FE · Boeing 727200 · Trailing Edge Flaps
  > RIGHT WING NR 8 FLAP TRACK FAIRING AFT I/B END IS CRACKED AND FWD FITTING IS GOUGED. REMOVED AND REPLACED FITTING IAW SRM 51-30-2.
- [SDR 05FDEA01209](https://openairdocs.org/sdr/05FDEA01209.md): Bracket · cracked · May 5, 2005 · N254FE · Boeing 727200 · Cargo/Baggage Doors
  > UPPER AFT DOOR BEARING GUIDE BRACKET ON AFT LWR CARGO DOOR FRAME IS CRACKED. REMOVED AND REPLACED DOOR GUIDE BRACKET IAW SRM 51-30-2.
- [SDR 05FDEA01208](https://openairdocs.org/sdr/05FDEA01208.md): Floorbeam · damaged · May 5, 2005 · N254FE · Boeing 727200 · Fuselage Main, Floor Beam
  > EVALUATE PREVIOUS REPAIR STA 1070 MCD FLOORBEAM RBL 12--RBL 62 UPPER CHORD FOR REPAIR STATUS (MAJOR/MINOR) AND FAA APROVAL. EVALUATED PREVIOUS REPAIR, FOUND TO BE IAW SR 27-53-034 REP NR 5 AND A MAJOR REPAIR IAW FED EX GMM 6-2-100.
- [SDR 05FDEA01204](https://openairdocs.org/sdr/05FDEA01204.md): Stringer · corroded · May 4, 2005 · N254FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CORROSION, STRINGER END TO FWD LWR FUEL TANK CHORD FITTING STA 740 STR 26L. REMOVED DAMAGED AREA IAW SRM 53-10-3 FIG 1 MATERIAL BAC 1498- 147-7075-T6 BATCH 27819 AND SPLICE MAT BMC 1498-131-7075-T6 BATCH 32659. LOCATED AND DRILLED IAW SRM 51-30-5, INSTALLED
- [SDR 05FDEA01202](https://openairdocs.org/sdr/05FDEA01202.md): Skin · gouged · May 4, 2005 · N254FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSE SKIN AT BS 1228 STR 22L HAS DEEP GOUGED MARK MEASURED 1.5 INCH LONG. FABBED REPAIR PLATE IAW SRM 53-30-3 FIG 1 AND INSTALLED REPAIR PLATE IAW SRM 51-30-2. THIS IS A MAJOR REPAIR AT MAE ON N/R N00818.
- [SDR 05FDEA01201](https://openairdocs.org/sdr/05FDEA01201.md): Stringer · damaged · May 4, 2005 · N254FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > EVALUATE PREVIOUS REPAIR STA 1120 STR 22 FOR REPAIR STATUS (MAJOR/MINOR) AND FAA APPROVAL. REMOVED DAMAGE SECTION OF STRINGER, FABBED FILLER AND SPLICES AND INSTALLED REPAIR IAW SRM 53-10-3 FIG 1 DETAIL I. THIS IS A MAJOR REPAIR ON N/R N00228 AT MAE.
- [SDR 05FDEA01199](https://openairdocs.org/sdr/05FDEA01199.md): Mount Bracket · cracked · May 3, 2005 · N254FE · Boeing 727200 · Leading Edge Devices
  > NR 1 SLAT OUTBOARD TRACK MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.
- [SDR 05FDEA01198](https://openairdocs.org/sdr/05FDEA01198.md): Strap · cracked · May 3, 2005 · N254FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > SUBFLOOR BEAM STRAP STA 312-344 RBL 25 IS CRACKED 3EA PLACES. REMOVED AND REPLACED STRAP IAW SRM 51-30-2.
- [SDR 05FDEA01197](https://openairdocs.org/sdr/05FDEA01197.md): Retainer · cracked · May 3, 2005 · N254FE · Boeing 727200 · Leading Edge Devices
  > NR 3 SLAT INBOARD MOLDED SEAL RETAINER CRACKED ON SEVERAL AREAS. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2.
- [SDR 05FDEA01196](https://openairdocs.org/sdr/05FDEA01196.md): Antenna · corroded · May 3, 2005 · N254FE · Boeing 727200 · VHF Communications System
  > LOWER AFT VHF ANTENNA HAS CORROSION ON ITS BASE. REMOVED AND REPLACED LWR AFT VHF ANTENNA IAW MM 23-21-031-2, OPS CHECKS GOOD.
- [SDR 05FDEA01179](https://openairdocs.org/sdr/05FDEA01179.md): Floor Panel · corroded · Apr 29, 2005 · N254FE · Boeing 727200 · Fuselage Floor Panel
  > CORROSION ON LEFT TRANS PANEL FWD PIT STA 540-545. REMOVED AND REPLACED TRANSITIONAL PANEL IAW SRM 51-30-2 AT MAE ON N/R N00892.
- [SDR 05FDEA01102](https://openairdocs.org/sdr/05FDEA01102.md): Seat Track · damaged · Apr 22, 2005 · N254FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 244 TO 480 RBL 45, HAS EXISTING BLEND REPAIRS AND AN EXISTING SPLICE REPAIR AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK IAW SRM 51-30-2. FAB'D SEAT TRACK ON TRAVELER NR T5/510065. LOCATED AND DRILLED IAW SRM 53-10-5 FIG 3.
- [SDR 05FDEA01060](https://openairdocs.org/sdr/05FDEA01060.md): Seat Track · damaged · Apr 21, 2005 · N254FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, STA 344 - 480 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002, LBL 45. REMOVED SEAT TRACK STA 344 - 480 LBL 45 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NR T5/510063, BATCH NR 888841, PO NR MST0017183. LOCATE
- [SDR 05FDEA01059](https://openairdocs.org/sdr/05FDEA01059.md): Seat Track · damaged · Apr 21, 2005 · N254FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, STA 344, LBL 24 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK STA 344 - 480 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NRT5/510064, BATCH NR 888841, P.O. NR MST0017183. LOCATED AND DRILLED
- [SDR 05FDEA01058](https://openairdocs.org/sdr/05FDEA01058.md): Strap · chafed · Apr 21, 2005 · N254FE · Boeing 727233 · Fuselage Main, Frame
  > MAIN DECK CARGO, AT STA 1030 AND 1050 STR 6L, LINER FRAME ASSY HAS CHAFED INTO THE FRAME STRAP'S AND HARDWARE. GOUGE OUT OF LIMITS IAW BOEING SRM 53-10-1. REMOVED AND REPLACED STRAP IAW BOEING SRM 51-30-2.
- [SDR 02FDEA00822](https://openairdocs.org/sdr/02FDEA00822.md): Shear Tie · corroded · Nov 12, 2002 · N254FE · Boeing 727200 · Fuselage Main, Structure
  > CORROSION ON SHEAR TIE BS 580 JUST O/B OF STR 28R. R&R SHEAR TIE PER SRM 51-30-2, 51-10-6, 51-20-1, 51-30-5.
- [SDR 02FDEA00816](https://openairdocs.org/sdr/02FDEA00816.md): Frame · corroded · Nov 11, 2002 · N254FE · Boeing 727200 · Fuselage Main, Frame
  > CORROSION ON FRAME BS 420, STR 23R. R&R FRAME PER SRM 51-40-3.
- [SDR 02FDEA00851](https://openairdocs.org/sdr/02FDEA00851.md): Keelbeam · damaged · Nov 10, 2002 · N254FE · Boeing 727200 · Fuselage Main, Keel
  > COMPLY WITH EO REV C1 PT5 KEELBEAM CHORD REPAIR BS 980-1007, STR 29L. REPAIRED KEELBEAM BS 980-1007, STR 29L IAW EO.
- [SDR 02FDEA00821](https://openairdocs.org/sdr/02FDEA00821.md): Frame · corroded · Nov 8, 2002 · N254FE · Boeing 727200 · Fuselage Main, Frame
  > CORROSION ON FRAME BS 720E, STR 27R TO 28R. R&R FRAME PER SRM 53-10-4 FIG 11.
- [SDR 02FDEA00818](https://openairdocs.org/sdr/02FDEA00818.md): Floorbeam · corroded · Nov 7, 2002 · N254FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LOWER CHORD BS 1070, RBL 46, WL 200. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8.
- [SDR 02FDEA00805](https://openairdocs.org/sdr/02FDEA00805.md): Stringer · corroded · Nov 7, 2002 · N254FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 29L, BS 1000 TO 1018. R&R STRINGER PER EO 7-5310-7-2356.
- [SDR 02FDEA00806](https://openairdocs.org/sdr/02FDEA00806.md): Keelbeam · corroded · Nov 7, 2002 · N254FE · Boeing 727200 · Fuselage Main, Keel
  > CORROSION ON KEELBEAM BS 1000, STR 29L. R&R KEELBEAM PER EO 7-5310-7-2356.
- [SDR 02FDEA00807](https://openairdocs.org/sdr/02FDEA00807.md): Skin · dented · Nov 6, 2002 · N254FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > DENT IN ETERNAL FUSELAGE SKIN AT BS 1045 JUST BELOW STR 20L. R&R SKIN PER SRM 53-30-3.
- [SDR 02FDEA00800](https://openairdocs.org/sdr/02FDEA00800.md): Frame · dented · Nov 5, 2002 · N254FE · Boeing 727200 · Fuselage Main, Frame
  > DENT ON FRAME AT STR 23R ASSOCIATED WITH E&E CATWALK. REPAIRED FRAME IAW SRM 51-40-3.
- [SDR 02FDEA00799](https://openairdocs.org/sdr/02FDEA00799.md): Stringer · dented · Nov 5, 2002 · N254FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > DENT IN STR AT BS 392. REPAIRED STR 23R BS 392 IAW SRM 53-10-3, 51-10-2.

Next page: https://openairdocs.org/deregistered/N254FE-2013-04-25/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 = 'N254FE' AND deregistration_id = 'N254FE-2013-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N254FE-2013-04-25/reports

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