# Service difficulty reports: N240FE, cancelled Apr 25, 2013

A list on [N240FE, cancelled Apr 25, 2013](https://openairdocs.org/deregistered/N240FE-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.

- [SDR 08FDEA02376](https://openairdocs.org/sdr/08FDEA02376.md): Aoa · damaged · Jun 22, 2008 · N240FE · Boeing 727227 · Stall Warning System
  > STALL WARNING ACTIVATED AT ROTATION. AIRCRAFT FLYING NORMALLY. STAYED ON UNTIL CIRCUIT BREAKER PULLED. AMBER WINDSHEAR LIGHT CAME ON. REMOVED AND REPLACED AOA VANE AND SYSTEM OPS CKS NORMAL IAW 727 M/M 34-18-051-4 AND REINSTALLED S/OS HAND MIKE AND BOOM M
- [SDR 07FDEA00541](https://openairdocs.org/sdr/07FDEA00541.md): Unknown · none · Feb 22, 2007 · N240FE · Boeing 727277 · Cargo/Baggage Doors
  > DOORS, MAIN CARGO LWR AFT CORNER EXTERNAL SKIN PERMANENT REPAIR P/N 52FX1435-2. COMPLIED WITH EA 7-5230-102022 DOORS MAIN CARGO, LWR AFT CORNER EXTERNAL SKIN PERMANENT REPAIR P/N 52FX14 35-2.
- [SDR 07FDEA00540](https://openairdocs.org/sdr/07FDEA00540.md): None · none · Feb 22, 2007 · N240FE · Boeing 727227 · Nacelle/Pylon, Main Frame
  > NACELLES AND PYLONS MINOR DEVIATION TO SRM S DUCT HOUSING SKIN REPAIR. COMPLIED WITH EA 7-5410-102026 THIS ITEM CLEARED BY REPAIR PER SRM 54-10-3 FIG 4 WITH MINOR DEVIATION DOCUMENTED BY THIS EA.
- [SDR 06FDEA1661](https://openairdocs.org/sdr/06FDEA1661.md): Engine · failed · Apr 29, 2006 · N240FE · Boeing 727227 · Engine (Turbine/Turboprop)
  > ATTEMPTED TAKEOFF ON 18L HAD SLIGHT COMPRESSOR STALL ON POWER APPLICATION. ABORTED TAKEOFF AND CHECKED ENGINE CONDITIONS ELECTED SECOND ATTEMPT DUE TO CROSSWINDS. ON SECOND ATTEMPT HAD ANOTHER COMPRESSOR STALL. 1ST STALL OCCURRED AT 1.5 EPR AND SECOND STALL
- [SDR 05FDEA04109](https://openairdocs.org/sdr/05FDEA04109.md): Union · leaking · Dec 3, 2005 · N240FE · Boeing 727200 · Hydraulic System, Main
  > AFTER T/O WHEN GEAR LVR WAS RAISED TO THE UP POS THE HYD SYS (A) RESERVOIR WENT TO ZERO. THE GEAR REMAINED DOWN AND FLAPS STAYED AT 15 DEG. REMOVED AND REPLACED PACKING AND UNION FOR THE OB TE FLAP CONTROL VALVE IAW IPC REF 27-50-00-30AZZ ITEM 145. LEAK AN
- [SDR 05FDEA00501](https://openairdocs.org/sdr/05FDEA00501.md): Oil Filter · bypassing · Mar 12, 2005 · N240FE · Boeing 727200 · Turbine Engine Oil System
  > DESCENDING THROUGH 20,000 FEET, THE NR 1 LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED; ENGINE OIL PRESSURE READ 45 PSI (MATCHED NR 2 AND NR 3). SHUT DOWN NR 1 ENGINE IAW QRH PROCEDURES. NO OTHER PROBLEMS NOTED.
- [SDR 05FDEA00047](https://openairdocs.org/sdr/05FDEA00047.md): Shear Tie · damaged · Jan 7, 2005 · N240FE · Boeing 727200 · Fuselage Main, Structure
  > REPAIR SHEAR TIE AT BS 380 BETWEEN STR 14 & 15 LT TO ACCOMPLISH 9G MOD. REPAIRED PER SRM 53-10-4.
- [SDR 05FDEA00048](https://openairdocs.org/sdr/05FDEA00048.md): Shear Tie · damaged · Jan 7, 2005 · N240FE · Boeing 727200 · Fuselage Main, Structure
  > REPAIR SHEAR TIE AT BS 380 BETWEEN STR 15 & 16 LT TO ACCOMPLISH 9G BARRIER MOD.
- [SDR 04FDEA02842](https://openairdocs.org/sdr/04FDEA02842.md): Channel · corroded · Sep 29, 2004 · N240FE · Boeing 727277 · Fuselage Miscellaneous Structure
  > FWD LWR CARGO A/C COMPT STR 27L BETWEEN F/S 720F TO 740, PROTECTIVE FINISH PEELING AND MINOR SURFACE CORROSION IN HAT CHANNEL. REMOVED CORROSION IAW SRM 51-10-6 PG 6, PARG 4. ORIG MAT.095, AFTER REWORK.075.020 MAT LOSS, FOUND TO BE OUT OF LIMITS IAW SRM
- [SDR 04FDEA02840](https://openairdocs.org/sdr/04FDEA02840.md): Floorbeam · corroded · Sep 28, 2004 · N240FE · Boeing 727277 · Fuselage Main, Floor Beam
  > BFM CLOSER C/W WITH EA7-5321-82044 FUSELAGE, FLOORBEAM UPPER CORD REPAIR STA 950 AT BL 21.0 ENT BY: 497236 RPT BY: 497236 FACT 28SEP04 23:10. BFM U COMPLIED WITH EA 7-5321-82044. REMOVED CORROSION, TREATED AREA AND INSTALLED REPAIR ANGLE ENT BY: 497236 RPT
- [SDR 04FDEA02839](https://openairdocs.org/sdr/04FDEA02839.md): Support Beam · corroded · Sep 28, 2004 · N240FE · Boeing 727277 · Wing, Landing Gear Attach Fittings
  > CLOSER COMPLY WITH EA NR 7-5710-82041 WINGS, LEFT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. BFM U COMPLIED WITH EA7-5710-82041 REAMED HOLE, FLAP PEENED AREA, INSTALLED REPAIR BUSHING AND WASHER ENT BY: 497236 RPT BY: 497236.
- [SDR 04FDEA02838](https://openairdocs.org/sdr/04FDEA02838.md): Beam · corroded · Sep 28, 2004 · N240FE · Boeing 727200 · Wing, Landing Gear Attach Fittings
  > COMPLY WITH EA 7-5710-82042 WINGS RIGHT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. COMPLIED WITH EA 7-5710-82042 REAMED HOLE, FLAP PEENED AND INSTALLED REPAIR BUSHING.
- [SDR 04FDEA02837](https://openairdocs.org/sdr/04FDEA02837.md): Skin · damaged · Sep 28, 2004 · N240FE · Boeing 727200 · Nacelle/Pylon, Plate/Skin
  > COMPLY WITH EA 7-5450-80610 PYLON STRUCTURE NR 1 ENG PYLON UPPER SKIN REPAIR. COMPLIED WITH EA 7-5450-80610, REPLACED SKIN SECTION AND INSTALLED EXT SPLICE DOUBLER.
- [SDR 04FDEA02803](https://openairdocs.org/sdr/04FDEA02803.md): Floor Support · corroded · Sep 22, 2004 · N240FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT FLOOR SUPPORT BEAM CORRODED UNDER NUTPLATE STA. 1110, RBL 6. REMOVED CORROSION, MATERIAL OUT OF LIMITS IAW SRM 53-10-5 FIG.6,PG.16 AND SRM 51-10-6. REMOVED DAMAGED AREA FROM STA 1105 TO 1115 RBL, FABRICATED 4 EA ANGLES (SPLICES). REPAIR AN
- [SDR 04FDEA02801](https://openairdocs.org/sdr/04FDEA02801.md): Intercostal · cracked · Sep 22, 2004 · N240FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > FWD CARGO, INTERCOSTAL IS CRACKED AT STRINGER 25L STA.624. REMOVED INTERCOSTAL IAW SRM 51-30-2. FABRICATED,TREATED AND PRIMED NEW INTERCOSTAL IAW SRM 51-20-1 FIG.6, 51-30-5 AND 51-10-2. INSTALLED IAW SRM 51-30-2. FABRICATED INTERCOSTAL USING 2024-T3.050,
- [SDR 04FDEA02800](https://openairdocs.org/sdr/04FDEA02800.md): Stringer · corroded · Sep 22, 2004 · N240FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > NUMEROUS AREAS OF CORROSION FOUND AT FWD PIT BILGE AREA FROM STA 560 TO STA 580 AT STR 28L. REMOVED DAMAGED AREA FROM STA 550 - 590 IAW SRM 51-10-3 FIG 1 PG 4. FABBED 2EA STRINGERS FROM BAC1498-142 7075-T62, BATCH 318127, FABBED 3EA SPLICES FROM BAC1498-132
- [SDR 04FDEA00601](https://openairdocs.org/sdr/04FDEA00601.md): O-Ring · failed · Mar 5, 2004 · N240FE · Boeing 727200 · Trailing Edge Flap Control System
  > A-SYSTEM HYDRAULICS FAILED IN FLIGHT. IN CRUISE FLT LVL 220, NOTICED A-SYSTEM QUANTITY DECREASING, LEAK CONTINUED TILL CHECKLIST DIRECTED A-PUMPS TO BE TURNED OFF. FOUND O-RING FAILURE AT UPPER PORT OF FLAP CONTROL VALVE. REPLACED O-RING PER 727-200 MM 20-1
- [SDR 03FDEA01597](https://openairdocs.org/sdr/03FDEA01597.md): Door · false indication · Sep 20, 2003 · N240FE · Boeing 727200 · Door Warning System
  > RED GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION AND HANDLE PLACED IN OFF POSITION. LIGHT EXTINGUISHED WHEN GEAR HANDLE PLACED IN UP POSITION. COMPLIED WITH ALL APPLICABLE CHECK LIST. PUT IN GEAR PINS, CYCLED GEAR DOORS, ALL INDICATIONS NORMAL, REF PER
- [SDR 03FDEA01401](https://openairdocs.org/sdr/03FDEA01401.md): Packing · leaking · Sep 1, 2003 · N240FE · Boeing 727200 · Turbine Engine Reduction Gear
  > AFTER T/O NR 1 ENG EPR LOW WITH A HI FF AT FL200 NR 1 ENG THROTTLE LEVER 3 INCHES FWD OF NR 2 & 3 THROTTLE LEVERS W/ ALL EPR'S MATCHING & NR 1 FF GAUGE 3000 LBS/HR MORE THAN NR 2 & 3 FF GAUGES. ALL ENG INST IN GREEN. CL THRU FL230, NR 1 EPR INDIC 0 & NR 1 FF
- [SDR 02FDEA00242](https://openairdocs.org/sdr/02FDEA00242.md): Fitting · cracked · Apr 9, 2002 · N240FE · Boeing 727277 · Fuselage Miscellaneous Structure
  > BS 1185, LBL 24, WL 292 BULKHEAD TO SPAR FITTING CRACKED AT FWD HORZ FASTENER HOLE. REMOVED AND REPLACED FITTING PER SRM & MM.
- [SDR 02FDEA00235](https://openairdocs.org/sdr/02FDEA00235.md): Skin · worn · Apr 8, 2002 · N240FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > N 279 FASTENERS AROUND DRAIN HOLE 11" ABOVE LH AFT NLG DOOR WORN. ** S/D ** COMING
- [SDR 02FDEA00234](https://openairdocs.org/sdr/02FDEA00234.md): Skin · chafed · Apr 6, 2002 · N240FE · Boeing 727277 · Electrical/Electronic Compartment Doors
  > MAIN E/E BAY DOOR SKIN IS CHAFED AT LEFT AFT EDGE. R&R SKIN PER SRM.
- [SDR 02FDEA00306](https://openairdocs.org/sdr/02FDEA00306.md): Frame · dented · Mar 28, 2002 · N240FE · Boeing 727277 · Cargo/Baggage Doors
  > N 697 MAIN CARGO DOOR AFT SIDE FRAME DENTED ABOVE CENTERING GUIDE RAMP. ** S/D ** COMING
- [SDR 02FDEA00226](https://openairdocs.org/sdr/02FDEA00226.md): Door Frame · dented · Mar 28, 2002 · N240FE · Boeing 727277 · Cargo/Baggage Doors
  > MAIN CARGO DOOR AFT SIDE FRAME DENTED ABOVE CENTERING GUIDE RAMP. REMOVED AND REPLACED FRAME PER EA 7-5230-64028.
- [SDR 02FDEA00222](https://openairdocs.org/sdr/02FDEA00222.md): Skin · dented · Mar 27, 2002 · N240FE · Boeing 727277 · Cargo/Baggage Doors
  > NR 2 CARGO DOOR OUTER SKIN HAS THREE LARGE DENTS FWD OF AFT EDGE 6 INCHES FROM BOTTOM. REMOVED AND REPLACED SKIN PER EA 75230-64035.
- [SDR 02FDEA00233](https://openairdocs.org/sdr/02FDEA00233.md): Web · corroded · Mar 25, 2002 · N240FE · Boeing 727277 · Galley Doors
  > FWD GALLEY DOOR INTERNAL WEB ABOVE CENTER PRESSURE PANEL UPPER SURFACE OF WEB HAS CORROSION. REMOVED AND REPLACED WEB PER SRM 51-20-1, 51-10-1.
- [SDR 00FDEA00886](https://openairdocs.org/sdr/00FDEA00886.md): Controller · faulty · Dec 19, 2000 · N240FE · Boeing 727277 · Cabin Pressure Controller
  > 00-365 FLT 1239/19 AIR TURN-BACK SEA. AC WILL NOT PRESSURIZE. WITH REF TO B727-200 MM 21-31-00-0 INSP AIRFRAME. RESET & PRESSURE TEST C/W CHECKS OK.
- [SDR 00FDEA00786](https://openairdocs.org/sdr/00FDEA00786.md): Switch · malfunctioned · Nov 22, 2000 · N240FE · Boeing 727277 · Landing Gear Position and Warning
  > WHEN PUTTING GEAR HANDLE FROM UP TO OFF, DOOR LIGHT ILLUMINATED WITH RIGHT MAIN DOOR LIGHT ILLUMINATED ON S/O PANEL. COMPLETED RED TABS HANDLE TO OFF, LIGHT OUT. *S/D* REMOVED AND REPLACED DOOR WARN SWITCH PER MM 32-62-011-4 & OPS CK NORMAL PER MM 32-62-011
- [SDR 98FDEA00167](https://openairdocs.org/sdr/98FDEA00167.md): Fire Warn Light · malfunction · Mar 10, 1998 · N240FE · Boeing 727277 · Fire Detection
  > BOTH MASTER FIRE WARNING LIGHTS ILLUMINATE INTERMITTENTLY. ALL FIRE WARNING LIGHTS OFF PRIOR TO TAKEOFF. ONCE AIRBORNE APU FIRE LIGHT CAME ON STEADY. MASTER FIRE WARNING LIGHTS STARTED FLICKERING. REPLACED APU FIRE BOTTLE. FOUND CORROSION ON PLUG D-4858P
- [SDR 98FDEA00116](https://openairdocs.org/sdr/98FDEA00116.md): Fire Light · malfunctioned · Feb 18, 1998 · N240FE · Boeing 727277 · Fire Detection
  > RED LIGHT ON IN AUXILIARY POWER UNIT FIRE HANDLE IN FLIGHT. TOOK OFF AT 0334Z AND NOTICED THE AUXILIARY POWER UNIT RED LIGHT ON AT 0400Z, FLIGHT LEVEL 310. PULLED THE HANDLE AND DISCHARGED THE AGENT. RED LIGHT REMAINED ON BUT WITH VARIATION OF INTENSITY. L
- [SDR 97FDEA00382](https://openairdocs.org/sdr/97FDEA00382.md): Bolt · jammed · Jul 2, 1997 · N240FE · Boeing 727277 · Elevator Tab Control System
  > BEFORE TAKEOFF CHECK, ELEVATOR JAMMED PULLING AFT ON YOKE. OPENED ACCESS PANELS 9115, 9118, BOUND BOLT AT FORWARD END OF FORWARD TAB ROD ON LEFT HAND ELEVATOR POWER CONTROL UNIT WORKED LOOSE. INSTALLED BOLT, WASHERS, NUT AND SAFETY PER MAINTENANCE MANUAL 27-
- [SDR 97FDEA00227](https://openairdocs.org/sdr/97FDEA00227.md): Chord · corroded · Apr 10, 1997 · N240FE · Boeing 727277 · Fuselage Miscellaneous Structure
  > NR 0302 005. CORROSION (C53-100-01(1)) ON MID LT NOSE CHORD BS 344-350, LBL 16, WL 170. REMOVED AND REPLACED MID LT NOSE CHORD PER BAC DWG 65-18415 AND FED-EX SRM 51-30-2.
- [SDR 97FDEA00229](https://openairdocs.org/sdr/97FDEA00229.md): Keel Beam · corroded · Apr 9, 1997 · N240FE · Boeing 727277 · Fuselage Main, Keel
  > NR 0250 004, CORROSION (C53-113-01-1) ON KEEL BEAM AT BS 720F, RBL 7, WL 149. *S/D* REMOVED CORROSION, SPOT FACED, FLAP PEENED AND INSTALLED STRAP AT BS 720F, RBL 7, WL 149 IAW FED-EX EA 7-5310-32976.
- [SDR 97FDEA00211](https://openairdocs.org/sdr/97FDEA00211.md): Foreflap · delaminated · Apr 1, 1997 · N240FE · Boeing 727277 · Trailing Edge Flaps
  > NR 0349 003, LEFT WING I/B UPPER SURFACE STAINLESS STEEL RUB STRIP DISBONDED. *S/D* REMOVED, REPAIRED AND INSTALLED ON LEFT WING I/B FOREFLAP, I/B UPPER SURFACE STAINLESS STEEL RUB STRIP IAW FED-EX SRM 51-40-6. FUNCTIONAL TEST LEFT WING I/B FOREFLAP OK IAW
- [SDR 97FDEA00208](https://openairdocs.org/sdr/97FDEA00208.md): Frame · damage · Mar 31, 1997 · N240FE · Boeing 727277 · Fuselage Main, Frame
  > NR 0244 002, DENT IN FRAME AT BS 720A, RBL 15, WL 155. BLENDED OUT DENT AND REPAIRED FRAME BS 720A, RBL 15, WL 155. ALL WORK ACCOMPLISHED PER FED-EX 727 SRM 51-10-2, 51-10-6, 53-10-4. FABRICATED REPAIR PART PER FED-EX SRM 53-10-4.
- [SDR 97FDEA00207](https://openairdocs.org/sdr/97FDEA00207.md): Wedge · punctured · Mar 31, 1997 · N240FE · Boeing 727277 · Trailing Edge Flaps
  > NR 0106 001, RIGHT WING I/B MIDFLAP TRAILING EDGE WEDGE PUNCTURED ON LOWER SURFACE 25 FROM INBOARD END. *S/D* REMOVED RIGHT WING I/B AFT FLAP, REPAIRED PUNCTURE ON RIGHT WING I/B MID FLAP T/E WEDGE, INSTALLED RIGHT WING I/B AFT FLAP, REPAIR PERFORMED IAW FED
- [SDR 97FDEA00042](https://openairdocs.org/sdr/97FDEA00042.md): Accessory Unit · failed · Jan 12, 1997 · N240FE · Boeing 727277 · Landing Gear Position and Warning
  > LANDING GEAR WOULD NOT RETRACT UNLESS WE USED LATCH LEVER RELEASE. REMOVED AND REPLACED GEAR ACCESSORY UNIT IAW 32-09-121 PG 401, FUNCTIONAL TEST GOOD IAW 32-09-122 PG 501 TO 505.
- [SDR 97FDEA00037](https://openairdocs.org/sdr/97FDEA00037.md): Sensor · dirty · Jan 11, 1997 · N240FE · Boeing 727277 · Landing Gear Position and Warning
  > GEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF. RETRACTED GEAR USING LEVER LOCK OVERRIDE. GEAR EXTENDED NORMALLY FOR LANDING. FOUND ICE ON AIR GROUND SAFETY SENSOR. CLEANED AND LUBED AS REQUIRED.
- [SDR 95FDEA00010](https://openairdocs.org/sdr/95FDEA00010.md): Accessory Unit · false warning · Jan 12, 1995 · N240FE · Boeing 727277 · Landing Gear Position and Warning
  > AFTER T/O FROM MEM AT GEAR RETRACTION, THE L/MAIN GEAR RED LIGHT WOULD NOT EXTINGUISH. CHECKLIST PROCEDURE ACCOMPLISHED. ALL GREEN ALL GEAR DOOR LIGHTS AND THE NOSE AND R/MAIN RED LIGHT EXTINGUISHED. THE L/MAIN RED LIGHT STILL WOULD NOT EXTINGUISH. FLT CON

## 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 = 'N240FE' AND deregistration_id = 'N240FE-2013-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N240FE-2013-04-25/reports

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