# Service difficulty reports: N279FE, cancelled Mar 19, 2013

A list on [N279FE, cancelled Mar 19, 2013](https://openairdocs.org/deregistered/N279FE-2013-03-19.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 · 56 reports

- [SDR FDEA200902230670](https://openairdocs.org/sdr/FDEA200902230670.md): Structure · cracked · Feb 23, 2009 · N279FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING INBD MID FLAP REAR CHORD CRACKED AT 2ND CUTOUT FROM INBD WBL 96. REMOVED MID FLAP LWR SKIN FOR ACCESS, REMOVED DAMAGED EXTRUDED SECTION. FABRICATED NEW EXTRUDED SECTION USING 7075T-6 PO NR 8306161 DIMS 48 INCH LONG AND INSTALLED NEW EXTRUDED SECTION,
- [SDR FDEA200902120511](https://openairdocs.org/sdr/FDEA200902120511.md): Intercostal · damaged · Feb 12, 2009 · N279FE · Boeing 727233 · Cargo/Baggage Doors
  > MCD INNER CENTER BEAM HAS MISDRILLED HOLE AND GOUGED INTO INTERCOSTAL REMOVED DAMAGE INTERCOSTAL IAW SRM 51-30-2, FABRICATED NEW INTERCOSTAL IAW HAYES INTERNATIONAL CORP DRAWING NR 52FX518 REV A, HEAT TREATED PART IAW FAS ENGINEERING REPORT NR 2-37153-801 REV
- [SDR FDEA200902060476](https://openairdocs.org/sdr/FDEA200902060476.md): Skin · cracked · Feb 6, 2009 · N279FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > TWO CRACKS ON FWD ENTRY DOOR HINGE CUT OUT BODY SKIN EDGE RADII, LOWER HINGE. REPAIRED CRACKS IAW EO 7-5330-7-2345F PART 2.
- [SDR FDEA200901310407](https://openairdocs.org/sdr/FDEA200901310407.md): Skin · cracked · Jan 31, 2009 · N279FE · Boeing 727233 · Leading Edge Devices
  > RIGHT WING NR 8 SLAT OTBD TRACK SKIN IS CRACKED. STOP DRILLED CRACK IAW DRAWING SR27-57-034 REV A AND SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071 DIM 9 1/2" BY 6" IAW DRAWING SR27-57-034 REV A. INSTALLED DOUBLER IAW DRAWING SR27-57-034 REV A A
- [SDR FDEA200901290389](https://openairdocs.org/sdr/FDEA200901290389.md): Structure · corroded · Jan 29, 2009 · N279FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > POSSIBLE CORROSION AT DOG HOUSE LOWER LEFT CHORD STA 312 UNDER LEVELING COMPOUND. REMOVED LEVELING COMPOUND AND CORROSION FROM AREA IAW SRM 51-10-6 AND SOPM 20-30-03, FOUND CHORD OUT OF LIMITS IAW SRM 53-10-1 FIG 1, REMOVED AND REPLACED CHORD IAW SRM 51-30-
- [SDR FDEA200901290386](https://openairdocs.org/sdr/FDEA200901290386.md): Angle · cracked · Jan 29, 2009 · N279FE · Boeing 727233 · Wing, Attach Fittings
  > RIGHT WING LOWER CHORD ANGLE CRACKED AT NR 8 SPOILER FITTING.
- [SDR FDEA200901290385](https://openairdocs.org/sdr/FDEA200901290385.md): Angle · cracked · Jan 29, 2009 · N279FE · Boeing 727233 · Wing Miscellaneous Structure
  > LEFT WING LOWER CHORD ANGLE CRACKED AT NR 7 SPOILER FITTING.
- [SDR FDEA200901290384](https://openairdocs.org/sdr/FDEA200901290384.md): Skin · canning · Jan 29, 2009 · N279FE · Boeing 727233 · Cargo/Baggage Doors
  > C1 DOOR LOWER AFT SKIN IS OIL CANNED. CUT OUT DAMAGED AREA IAW 52-00-03 FIG 3. FABRICATED DOUBLER REPAIR IAW SRM 52-00-03 FIG 3 AND 52-30-01 FIG. 7. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.
- [SDR FDEA200901290383](https://openairdocs.org/sdr/FDEA200901290383.md): Structure · cracked · Jan 29, 2009 · N279FE · Boeing 727233 · Trailing Edge Flaps
  > CRACK ON LEFT INBD MID FLAP CHORD AT WBL 114. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED LOWER SECTION USING EXTRUSION AND SPLICE IAW SRM 51-40-3 FIG 1 AND 57-50-2 FIG 5. INSTALLED REPAIR PARTS IAW SRM 51-30-2.
- [SDR FDEA200901290382](https://openairdocs.org/sdr/FDEA200901290382.md): Frame · gouged · Jan 29, 2009 · N279FE · Boeing 727233 · Fuselage Main, Frame
  > FWD PIT FRAME AT BS 520 STRINGER 22L IS GOUGED AT RADIUS. CUT OUT DAMAGED IAW SRM 51-40-3 FIG. 1. FABRICATED REPAIR DOUBLER, STRUCTURAL FILLER, AND 1 FILLER IAW SRM 53-10-2 FIG. 3 AND 51-40-3 FIG. 1. HEAT TREATED PART FROM 7075-O TO 7075-T6 IAW FAS ENGINEERIN
- [SDR FDEA200901290380](https://openairdocs.org/sdr/FDEA200901290380.md): Skin · gouged · Jan 29, 2009 · N279FE · Boeing 727233 · Trailing Edge Flaps
  > RIGHT WING INBD FORE FLAP IS GOUGED AT OTBD LEADING EDGE IN TWO PLACES. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR PARTS IAW SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. INSTALLED NEW REPAIR IAW SRM 51-30-2.
- [SDR FDEA200901280343](https://openairdocs.org/sdr/FDEA200901280343.md): Angle · cracked · Jan 28, 2009 · N279FE · Boeing 727233 · Spoilers
  > LEFT WING LOWER CHORD ANGLE CRACKED AT NR 7 SPOILER FITTING. REMOVED AND DISCARDED DOUBLER IAW FEDEX DRAWING SR27-57-038 REV C. TRIMMED WEB AND LOWER CHORD IAW FEDEX DRAWING SR27-57-038 REVC. FABRICATED NEW WEB FROM 7075-T6 0.032 DIM. 12 1/8" BY 9 1/2".
- [SDR FDEA200901280347](https://openairdocs.org/sdr/FDEA200901280347.md): Frame · cracked · Jan 28, 2009 · N279FE · Boeing 727233 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE NOSE COWL AFT EDGE IS CRACKED AND SECTION TORN AT 4 O'CLOCK POSITION BS 1200 CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED REPAIR PARTS AND 1 FILLER IAW SRM 54-10-2 FIG 1 AND 54-10-3 FIG 3. INSTALLED REPAIR PARTS IAW SRM 51-30-2.
- [SDR FDEA200901280344](https://openairdocs.org/sdr/FDEA200901280344.md): Skin · damaged · Jan 28, 2009 · N279FE · Boeing 727233 · Emergency Exits
  > LEFT AFT EMERGENCY EXIT HATCH HAS DEEP SCRATCH ON OUTER SKIN. CUT OUT DAMAGED AREA IAW SRM 52-00-03 FIG 3. FABRICATED REPAIR DOUBLER IAW SRM 52-00-03 FIG 3 AND 52-20-01 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.
- [SDR FDEA200901280342](https://openairdocs.org/sdr/FDEA200901280342.md): Angle · cracked · Jan 28, 2009 · N279FE · Boeing 727233 · Wing Miscellaneous Structure
  > RIGHT WING LOWER CHORD ANGLE CRACKED AT NR 8 SPOILER FITTING. REMOVED AND DISCARDED DOUBLER IAW DRAWING SR27-57-038 REV C. TRIMMED WEB AND LOWER CHORD IAW DRAWING SR27-57-038 REV C. FABRICATED NEW INBD WEB, FABRICATED NEW INBD LOWER CHORD, FABRICATED NEW ST
- [SDR FDEA200901280345](https://openairdocs.org/sdr/FDEA200901280345.md): Skin · damaged · Jan 28, 2009 · N279FE · Boeing 727233 · Emergency Exits
  > RIGHT FWD EMERGENCY EXIT HATCH OUTER SKIN HAS DEEP SCRATCH. CUT OUT DAMAGED AREA DIM 4 1/4 BY 1 1/4 INCH IAW B727 SRM 52-00-03 FIG 3. FABRICATED DOUBLER REPAIR MAT USED 2024-T3 0.080" PO NR 9008077 DIM 11 1/8 BY 7" IAW B727 SRM 52-00-03 FIG 3 AND 52-20-01
- [SDR FDEA200901090107](https://openairdocs.org/sdr/FDEA200901090107.md): Actuator · failed · Jan 9, 2009 · N279FE · Boeing 727233 · Leading Edge Slat Actuator
  > AFTER TAKEOFF WHILE RAISING FLAPS NR 1 LEADING EDGE DEVICE REMAINED EXTENDED AT 2 DEG AND 0 DEG FLAP SETTING. RAN QRH PROBLEM REMAINED. RETURNED TO BASE FOR NORMAL LANDING. LEADING EDGE DEVICE RETRACTED ON SCHEDULE AFTER LANDING CLEAN UP. VISUAL INSPECTION
- [SDR FDEA200901080103](https://openairdocs.org/sdr/FDEA200901080103.md): Actuator · failed · Jan 8, 2009 · N279FE · Boeing 727233 · Leading Edge Slat Actuator
  > AFTER TAKEOFF WHILE RAISING FLAPS NR 1 LEADING EDGE DEVICE REMAINED EXTENDED AT 2 DEG AND 0 DEG FLAP SETTING. RAN QRH PROBLEM REMAINED. RETURNED TO BASE FOR NORMAL LANDING. LED RETRACTED ON SCHEDULE AFTER LANDING CLEAN UP. VISUAL INSPECTION OF NR 1 LEADING
- [SDR 07FDEA01502](https://openairdocs.org/sdr/07FDEA01502.md): Connector · damaged · Apr 12, 2007 · N279FE · Boeing 727200 · Detection System
  > NR 1 ENG FIRE DETECTION A LOOP INOP. MEL 03APR07 00:03 YOW ACN RELEASED FOR SERVICE PER MEL/CDL: 26-06-B. REMOVABLE ON P6 AREA, APU START PANEL, L/E ANNUNC. PANEL, GEN. FAULT ANNUNC. PANEL. REMOVED RELAY R730, DEPINNED PIN 9 FROM D5220J, DEPINNED PINS 6
- [SDR 06FDEA03463](https://openairdocs.org/sdr/06FDEA03463.md): Switch · sticking · Sep 27, 2006 · N279FE · Boeing 727233 · Landing Gear Position and Warning
  > DURING GEAR EXTENSION NOSE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER EXTENSION WITH DOOR LIGHT ON S/O PANEL. LIGHT WENT OUT AFTER 2 MINUTES. INSPECTED SWITCH ASSY ON NOSE WHEEL GEAR DOOR SWITCH. FOUND PLUNGERS STICKING. CLEANED AND LUBED SWITCH. OPS CHEC
- [SDR FDEA200607212648](https://openairdocs.org/sdr/FDEA200607212648.md): Warning Light · illuminated · Jul 21, 2006 · N279FE · Boeing 727233 · Door Warning System
  > MAIN CARGO DOOR "B" LT ILLUMINATED IN FLIGHT, FL250 WITH VENT DOOR WARNING LT IN GALLEY AREA ILLUMINATED.
- [SDR 06FDEA2648](https://openairdocs.org/sdr/06FDEA2648.md): Warning Light · illuminated · Jul 21, 2006 · N279FE · Boeing 727233 · Door Warning System
  > MAIN CARGO DOOR "B" LT ILLUMINATED IN FLIGHT, FL250 WITH VENT DOOR WARNING LT IN GALLEY AREA ILLUMINATED.
- [SDR 06FDEA1420](https://openairdocs.org/sdr/06FDEA1420.md): Fitting · loose · Apr 12, 2006 · N279FE · Boeing 727233 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FAILED TO MAKE STANDARD EPR ON TAKEOFF ROLL TARGET EPR 2.08, MADE ONLY 1.8 WITH THRUST LEVER AT FORWARD STOP. ENGINE WAS VERY SLOW TO ACCELERATE. NO OTHER PARAMETERS EXCEEDED. RUNWAY 27, WEATHER: 190/4KTS, 1ONM VIS, TEMP19*C, DEW POINT 11*C, 30.
- [SDR 04FDEA01001](https://openairdocs.org/sdr/04FDEA01001.md): Web · corroded · Apr 17, 2004 · N279FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > CENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE.
- [SDR 04FDEA001000](https://openairdocs.org/sdr/04FDEA001000.md): Bracket · cracked · Apr 17, 2004 · N279FE · Boeing 727200 · Spoilers
  > NR 8 SPOILER INBOARD STOP BRACKET LWR MOUNTING CRACKED. REMOVED AND REPLACED STOP BRACKET IAW SRM 51-30-2 AT MAE.
- [SDR 04FDEA001001](https://openairdocs.org/sdr/04FDEA001001.md): Floor Panel · corroded · Apr 17, 2004 · N279FE · Boeing 727200 · Fuselage Floor Panel
  > CENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE.
- [SDR 04FDEA00849](https://openairdocs.org/sdr/04FDEA00849.md): Duct · cracked · Apr 7, 2004 · N279FE · Boeing 727200 · Engine Exhaust System
  > COMPLY WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR. COMPLIED WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR AT MAE.
- [SDR 02FDEA00755](https://openairdocs.org/sdr/02FDEA00755.md): Door Seal · defective · Oct 23, 2002 · N279FE · Boeing 727200 · Landing Gear Doors
  > ON APPROACH TO CID-EXTENDED LAND GEAR, NOSE DOOR AMBER LT ON S/O PANEL & RED DOORS LIGHT ON. ELECTED TO DO MISS APPROACH & RECYCLE GEAR. LT WENT OUT. ON RE-EXTENSION RED GEAR DOOR LT WENT OUT. BELOW 200 KTS ON RECYCLE. CHECKED QRH. NO OTHER PROBLEM. FOU
- [SDR 02FDEA00201](https://openairdocs.org/sdr/02FDEA00201.md): Wire · chafed · Mar 14, 2002 · N279FE · Boeing 727233 · Hydraulic Power System Wiring
  > HYD A-SYS OVERHEAT LIGHT CAME ON. BOTH PUMPS WERE OFF PER CK LIST. REPEAT WRITEUP. REMOVED AND REPLACED CHAFED WIRE WITH TEFLON TAPE PER CHAPTER 20 STANDARD PRACTICES.
- [SDR 01FDEA00965](https://openairdocs.org/sdr/01FDEA00965.md): Floorbeam · corroded · Nov 6, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01, 1) ON TOP OF FLOORBEAM AT FASTENER HOLES BS 312, LBL 3 TO LBL 50, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8, FIG 9.
- [SDR 01FDEA00959](https://openairdocs.org/sdr/01FDEA00959.md): Beam · chafed · Nov 3, 2001 · N279FE · Boeing 727233 · Horizontal Stabilizer Structure
  > LT HORIZ STAB LOWER TRAILING EDGE BEAM HAS CHAFE DAMAGE AND MISSING SPACER.
- [SDR 01FDEA00952](https://openairdocs.org/sdr/01FDEA00952.md): Floorbeam · corroded · Nov 2, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01) ON TOP OF FLOORBEAM BS 344, RBL 3 - LBL 31, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10-6.
- [SDR 01FDEA00935](https://openairdocs.org/sdr/01FDEA00935.md): Stringer · damaged · Oct 29, 2001 · N279FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L EDGE DAMAGE BS 480, WL 149. REMOVED AND REPLACED STRINGER PER EA 7-5310-59896.
- [SDR 01FDEA00932](https://openairdocs.org/sdr/01FDEA00932.md): Floorbeam · corroded · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 1070, LBL 45, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3.
- [SDR 01FDEA00921](https://openairdocs.org/sdr/01FDEA00921.md): Beam · chafed · Oct 26, 2001 · N279FE · Boeing 727233 · Horizontal Stabilizer Structure
  > LEFT HORIZ STAB LOWER TRAILING EDGE BEAM HAS CHAFE DAMAGE AND MISSING SPACER BLOCK AT THE 3RD RUB PAD FROM O/B END. REMOVED AND REPLACED BEAM PER EA 7-5510-60563.
- [SDR 01FDEA00927](https://openairdocs.org/sdr/01FDEA00927.md): Floorbeam · corroded · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01, 2) ON LWR CHORD OF FLOORBEAM, BS 1110, RBL 41, WL 200. REMOVED AND REPLACED CORROSION PER EA 7-5310-59897.
- [SDR 01FDEA00922](https://openairdocs.org/sdr/01FDEA00922.md): Floorbeam · corroded · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION C53-224-01,1 ON TOP CHORD OF BS 720A FLOORBEAM RBL 7 OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM PER EA 7-5310-60567.
- [SDR 01FDEA00958](https://openairdocs.org/sdr/01FDEA00958.md): Floorbeam · corroded · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 1970, LBL 45, WL 208.
- [SDR 01FDEA00928](https://openairdocs.org/sdr/01FDEA00928.md): Skin · dented · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EMPENNAGE SKIN DENT AT BS 1338, 38' BELOW VERT STAB LT SIDE. REMOVED AND REPLACED SKIN PER SRM 51-40-2.
- [SDR 01FDEA00929](https://openairdocs.org/sdr/01FDEA00929.md): Skin · cracked · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CRACK IND IN EXTERNAL FUSE SKIN AFT I/B CORNER. REMOVED AND REPLACED SKIN PER DWG SR 27-53-024 & EA.
- [SDR 01FDEA00923](https://openairdocs.org/sdr/01FDEA00923.md): Floorbeam · corroded · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER CHORD OF FLOORBEAM BS 1050, RBL 35 AND RBL 55, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 & 51-30-2.
- [SDR 01FDEA00925](https://openairdocs.org/sdr/01FDEA00925.md): Keelbeam · corroded · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM AT BS 934, STR 29 RIGHT O/B. REMOVED AND REPLACED BEAM PER DWG SR 27-53-023.
- [SDR 01FDEA00926](https://openairdocs.org/sdr/01FDEA00926.md): Frame · dented · Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Frame
  > FRAME DENTED BS 660 JUST ABOVE STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-40-3.
- [SDR 01FDEA00920](https://openairdocs.org/sdr/01FDEA00920.md): Stringer · cracked · Oct 25, 2001 · N279FE · Boeing 727233 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN STA 110.4, STR 9 LT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1 & EA 7-5530-59892.
- [SDR 01FDEA00919](https://openairdocs.org/sdr/01FDEA00919.md): Frame · cracked · Oct 25, 2001 · N279FE · Boeing 727233 · Vertical Stabilizer
  > VERTICAL STABILIZER MAIN BOX INTERIOR CHORD IS CRACKED AT FIN BS 157.2, STR 8 LT. REMOVED AND REPLACED CHORD PER SRM 55-30-5 FIG 1 & EA 7-5530-59891.
- [SDR 01FDEA00918](https://openairdocs.org/sdr/01FDEA00918.md): Stringer · cracked · Oct 25, 2001 · N279FE · Boeing 727233 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN BS 157.2, STR 8 RT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 & EA 7-5530-59891.
- [SDR 01FDEA00916](https://openairdocs.org/sdr/01FDEA00916.md): Spar · cracked · Oct 25, 2001 · N279FE · Boeing 727233 · Wing Spar
  > RIGHT WING I/B MIDFLAP, AFT FLAP CONTROL ROD CUT OUT IN THE LWR SPAR CHORD CRACKED. REMOVED AND REPLACED CHORD PER SRM 51-40-4, 51-30-2.
- [SDR 01FDEA00917](https://openairdocs.org/sdr/01FDEA00917.md): Skin · chafed · Oct 25, 2001 · N279FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > BS 720, STR 19 LT FUSELAGE EXTERNAL SKIN CHAFED. REMOVED AND REPLACED SKIN PER SRM 53-30-3.
- [SDR 01FDEA00956](https://openairdocs.org/sdr/01FDEA00956.md): Floorbeam · corroded · Oct 21, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON LOWER CHORD OF FLOORBEAM AROUND NUT PLATE HOLES. REMOVED AND REPLACED FLOORBEAM PER EA 7-5310-59894.
- [SDR 01FDEA00801](https://openairdocs.org/sdr/01FDEA00801.md): Switch · failed · Sep 5, 2001 · N279FE · Boeing 727233 · Leading Edge Slat Control System
  > 01-299 DUR DEPART #2 L/E DEVICE FAILED TO RETRACT. R&R #2 LED SWITCH PER MM 27-82-001. OPS CK OK.

Next page: https://openairdocs.org/deregistered/N279FE-2013-03-19/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 = 'N279FE' AND deregistration_id = 'N279FE-2013-03-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N279FE-2013-03-19/reports

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