# Service difficulty reports: N280FE, cancelled Dec 19, 2013

A list on [N280FE, cancelled Dec 19, 2013](https://openairdocs.org/deregistered/N280FE-2013-12-19.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 · 62 reports

- [SDR FDEA201109244102](https://openairdocs.org/sdr/FDEA201109244102.md): Pin · out of adjust · Sep 24, 2011 · N280FE · Boeing 727233 · Flight Compartment Windows
  > CAPTAINS SLIDING WINDOW WILL NOT CLOSE. ADJUSTED GUIDE PIN ON PILOT'S SLIDING WINDOW IAW MM 56-12-011-5. OPS CHECK OF PILOT'S SLIDING WINDOW COMPLIED WITH IAW MM 26-12-011-5. OPS CHECK NORMAL. ACFT OK TO CONTINUE. ADJUSTED GUIDE PIN ON PILOT'S SLIDING WIND
- [SDR FDEA201109143874](https://openairdocs.org/sdr/FDEA201109143874.md): Sliding Window · out of adjust · Sep 14, 2011 · N280FE · Boeing 727233 · Flight Compartment Windows
  > CAPTIANS SLIDING WINDOW WILL NOT CLOSE. ADJUSTED CAPT'S SLIDING WINDOW. ADJUSTMENT ROD IAW MM REF 56-12-011-5-0. OPS CHECKED GOOD. OK FOR FLIGHT.
- [SDR FDEA200905031496](https://openairdocs.org/sdr/FDEA200905031496.md): Angle · corroded · May 3, 2009 · N280FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > ANGLE AT BS 740 AND STRINGER'S 27L TO 28L IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGED ANGLE AND FABRICATED A NEW ONE, HEAT TREATED TO T6 CONDITION AND INSTALLED IAW SRM 53-10-1, 51-10-6, 51-30-2 AND DWG 69-43695.
- [SDR FDEA200905031495](https://openairdocs.org/sdr/FDEA200905031495.md): Stiffener · corroded · May 3, 2009 · N280FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD PIT, CORROSION ON OTBD SIDE OF VERTICAL STIFFENER AT BS 740, BETWEEN STRINGERS 26L AND 25L. REMOVED AND REPLACED DAMAGED CHORD WITH NEW PART IAW DWG 65-15940, SRM 51-30-5 AND SRM 51-30-2.
- [SDR FDEA200904301481](https://openairdocs.org/sdr/FDEA200904301481.md): Skin · chafed · Apr 30, 2009 · N280FE · Boeing 727233 · Emergency Exits
  > RIGHT AFT OVERWING HATCH LOWER SKIN CHAFED ON THE EDGE. BURNISHED AREA AND FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER USING 2024T-3.063 PO NR 9008186 DIMS 12 INCH BY 5 INCH AND FILLER USING 2024T-3.050 PO NR 9008452 DIMS 1 INCH BY 1 I
- [SDR FDEA200904251415](https://openairdocs.org/sdr/FDEA200904251415.md): Structure · cracked · Apr 25, 2009 · N280FE · Boeing 727233 · Leading Edge Devices
  > NR 7 SLAT TRAILING EDGE CHORD IS CRACKED AT INBD UPSTOP PAD REMOVED PANEL FOR ACCESS IAW B727 SRM 51-30-2, CUT OUT DAMAGED AREA DIM 29 1/2 INCH IAW B727 SRM 51-40-4. FABRICATED REPAIR PARTS FROM BAC 1514-1559 PO NR 2903470 DIM 29 1/2 INCH AND SPLICE 11 1/2
- [SDR FDEA200904251414](https://openairdocs.org/sdr/FDEA200904251414.md): Skin · corroded · Apr 25, 2009 · N280FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > AFT CARGO COMPARTMENT, FUSELAGE SKIN IS CORRODED NEXT TO STRINGER 29 L AT BS 1145 FOUND CORROSION OUT OF LIMITS IAW SRM 53-30-1, CUT OUT DAMAGED AREA. REMOVED PREVIOUS REPAIR AND U CHANNEL IAW SRM 51-30-2 FIG 3. CUT OUT DAMAGED AREA IAW SRM 53-30-2 FABRICAT
- [SDR FDEA200904241398](https://openairdocs.org/sdr/FDEA200904241398.md): Structure · cracked · Apr 24, 2009 · N280FE · Boeing 727233 · Trailing Edge Flaps
  > LEFT INBOARD MIDFLAP LOWER TRAILING EDGE CHORD CRACKED AT WBL100. CUT OUT DAMAGED AREA DIM 48 INCH, FABRICATED NEW CHORD, SPLICE ANGLE AND INSTALLED REPAIR PARTS IAW SRM 51-40-2, 57-50-2 AND 51-30-2.
- [SDR FDEA200904241397](https://openairdocs.org/sdr/FDEA200904241397.md): Seat Track · corroded · Apr 24, 2009 · N280FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK STA 783-804 LBL 25. REMOVED CORROSION ON SEAT TRACK AND FOUND OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW SEAT TRACK SECTION USING BAC1506-1108 PO NR 29034128 DIMS 110 INCH BY 4 INCH AND INSTALLED IAW SRM 51-30-2 AND
- [SDR FDEA200904211374](https://openairdocs.org/sdr/FDEA200904211374.md): Bracket · cracked · Apr 21, 2009 · N280FE · Boeing 727233 · Wing, Attach Fittings
  > LT WING L/E CAVITY NR 1 SLAT ACT ATTACH BRACKETS HAVE BOTH INSIDE PLATES CRACKED. REMOVED 2 EA WEB AND STEEL DOUBLERS ON NR 1 SLAT ACTUATOR. BRACKETS IAW EA 7-5750-126809. FABRICATED 2 EA WEBS & STEEL DOUBLERS IAW EO 7-5750-126809 HEAT TREAT WEBS FROM "O" TO
- [SDR FDEA200904201366](https://openairdocs.org/sdr/FDEA200904201366.md): Stringer · corroded · Apr 20, 2009 · N280FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD PIT, FWD SIDE OF BS 720 STRINGER 28 LEFT CORRODED. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1, CUT OUT DAMAGED SECTION IAW SRM 53-10-1 FIG 1, FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG 1, TREATED AND PRIMED REPAIR PARTS IAW S
- [SDR FDEA200904201365](https://openairdocs.org/sdr/FDEA200904201365.md): Skin · corroded · Apr 20, 2009 · N280FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD PIT STA 720 STRINGER 28L SKIN CORRODED. REMOVED CORROSION IAW SRM 51-10-6, AREA FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1, CUT OUT DAMAGED AREA IAW SRM 53-30-2 FIG 1, FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1 AND 53-10-2, TREATED AND PRIMED REPAI
- [SDR FDEA200904171328](https://openairdocs.org/sdr/FDEA200904171328.md): Seat Track · corroded · Apr 17, 2009 · N280FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION AT OUTER FLANGE, LBL 45 STA 640-680. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792 PO NR 9006020 APPROX LENGTH 18 FT IAW SRM 53-10-5 FIG 1 AND 53-10-5. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. IN
- [SDR FDEA200904161324](https://openairdocs.org/sdr/FDEA200904161324.md): Intercostal · corroded · Apr 16, 2009 · N280FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT, CORROSION ON INTERCOSTAL AT BS 580 BETWEEN STRINGERS 28R AND 27R REMOVED INTERCOSTAL IAW B727 SRM 51-30-2. REMOVED CORROSION ON SKIN IAW SRM 51-10-6. FOUND OUT OF LIMITS IAW SRM 53-10-1. FABRICATED INTERCOSTAL. CUT OUT DAMAGED AREA O
- [SDR FDEA200904151308](https://openairdocs.org/sdr/FDEA200904151308.md): Skin · damaged · Apr 15, 2009 · N280FE · Boeing 727233 · Leading Edge Devices
  > NR 5 SLAT OUTBD LOWER SURFACE IS DAMAGED ROUTED OUT EDGE IAW SRM 51-10-1. AREA FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 2. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR IAW SRM 57-50-3 FIG 1. ALODINED AND PRIMED DOUBLER IAW SRM 51-10-
- [SDR FDEA200904151306](https://openairdocs.org/sdr/FDEA200904151306.md): Doubler · cracked · Apr 15, 2009 · N280FE · Boeing 727233 · Fuselage Main, Structure
  > AFT AIRSTAIR AREA - LOWER RT TORQUE BOX LIGHTNING HOLE HAS 2 STOP-DRILLED CRACKS AT BS 1243 CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED 2 EA DOUBLERS IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. ALODINED AND PRIMED PARTS AND AREA IAW SRM 51-10-2. INSTA
- [SDR FDEA200904111268](https://openairdocs.org/sdr/FDEA200904111268.md): Angle · cracked · Apr 11, 2009 · N280FE · Boeing 727233 · Leading Edge Devices
  > NR 2 SLAT LOWER TRAILING EDGE CHORD ANGLE IS CRACKED AT INBD UPSTOP PAD CUT OUT DAMAGED AREA DIM 25 5/8 INCH IAW SRM 51-10-1. FABRICATED ANGLE SECTION FROM BAC 1514-1559 PO NR 8307196 DIM 25 5/8 INCH AND SPLICE FROM BAC 1514-1559 PO NR 8307196 DIM 11 1/2 INC
- [SDR FDEA200904081229](https://openairdocs.org/sdr/FDEA200904081229.md): Skin · dented · Apr 8, 2009 · N280FE · Boeing 727233 · Cargo/Baggage Doors
  > PROTRUDING DENT, EXTERIOR SKIN OF C-3 DOOR, TOP OF DOOR BETWEEN RIBS, BS 1110 CHECKED DENT LIMITS AND FOUND OUT OF LIMITS IAW SRM 52-00-2. CUT OUT DAMAGED AREA IAW SRM 52-00-3. FABRICATED DOUBLER REPAIR IAW SRM 52-00-3 FIG 3. TREATED AND PRIMED DOUBLER REPA
- [SDR 07FDEA01483](https://openairdocs.org/sdr/07FDEA01483.md): Control Valve · failed · Apr 12, 2007 · N280FE · Boeing 727200 · Cabin Pressure Control System
  > S/O REPERTED HEARING A SLIGHT POP PASSING 2000FT AFTER RIGHT PACK WAS TURNED ON.NORMAL INDICATION RIGHT PACK MATCHED LEFT PACK TEMP BUT AIR MIX VALVE STAYED COLD ON RIGHT PACK.CABIN STARTED A HIGHER THAN NORMAL CLIMB 71500 FT/MIN IN MAN PRESSURIZATION WIT
- [SDR 07FDEA00130](https://openairdocs.org/sdr/07FDEA00130.md): Engine · failed · Jan 18, 2007 · N280FE · Boeing 727200 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED DURING CLIMB-OUT AT APPROX 1500 FT ABOVE GROUND. NOTED HIGH EGT (AROUND 780 C), EPR 0, N1 AND N2 WINDMILLING. OIL QTY 3 GALS ENGINE FAILED WITH A LOUD BANG AND SPARKS REPORTED TRAILING AIRCRAFT BY TOWER. VISUAL INSPECTION OF ENGINE REVEA
- [SDR 06FDEA04242](https://openairdocs.org/sdr/06FDEA04242.md): Retaining Nut · missing · Dec 14, 2006 · N280FE · Boeing 727233 · Trailing Edge Flap Control System
  > ON CLIMB-OUT WHEN FLAP HANDLE WAS RAISED FROM 5 DEG TO 2 DEG, OBSERVED THE INBD FLAP GAUGE STOPPED AT 3/4 DEG. INBD FLAPS INDICATOR REMAINED AT 3-4 DEG FOR LNDG. QRH ACCOMPLISHED. INSP ALL FLAPS AND DISCOVERED LT INBD FLAP INBD JACKSCREW FAIRING END RETAI
- [SDR 06FDEA03629](https://openairdocs.org/sdr/06FDEA03629.md): Attach Fitting · cracked · Oct 13, 2006 · N280FE · Boeing 727233 · Leading Edge Devices
  > LT WING NR 4 FLAP TRACK FALSE SPAR ATTACH FITTING CRACKED AND SEVERAL FASTENERS LOOSE. FABED NEW WEB SECTION, DOUBLER, ANGLE, AND SPLICES; AND INSTALLED IAW DWG SR27-57-038 REV C AND EA 7-5750-102761, (WING SPOILER SUPPORT BEAM-REPAIR) EA ATTACHED TO SNRM N008
- [SDR 06FDEA03627](https://openairdocs.org/sdr/06FDEA03627.md): Spar · failed · Oct 13, 2006 · N280FE · Boeing 727233 · Wing Spar
  > RT WING FALSE SPAR FASTENERS LOOSE AT NR 5 FLAP TRACK ATTACH AREA REMOVED DAMAGED ANGLE AND WEB, FABRICATED NEW WEB SECTION, DOUBLER AND ANGLE SECTION WITH SPLICE ANGLES IAW DWG. SR 27-57-038 REV C. AND EA 7-5750-102761. ALL PARTS ALODINED AND PRIMERED IAW SRM
- [SDR 06FDEA03620](https://openairdocs.org/sdr/06FDEA03620.md): Floorbeam · corroded · Oct 11, 2006 · N280FE · Boeing 727200 · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE CORRODED TOP SIDE BS 620 LBL 10. REMOVED DAMAGED UPPER TEE IAW B 727 SRM 53-10-8 FIG. 3. FABRICATED AND INSTALLED REPAIR PARTS IAW B 727 SRM 53-10-8 FIG. 3.
- [SDR 06FDEA03619](https://openairdocs.org/sdr/06FDEA03619.md): Floorbeam · corroded · Oct 11, 2006 · N280FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE CORRODED BODY STATION 680 BUTT LINE 0 RBL 55. REMOVED CORRODED FLOORBEAM TEE STA 680 IAW B727 SRM 53-10-8.
- [SDR 05FDEA02123](https://openairdocs.org/sdr/05FDEA02123.md): Seat Track · corroded · Jul 27, 2005 · N280FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 344-480 RBL 45 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.
- [SDR 05FDEA02120](https://openairdocs.org/sdr/05FDEA02120.md): Floorbeam · corroded · Jul 27, 2005 · N280FE · Boeing 727200 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA. 720A RBL 18-22 HAS CORROSION ON UPPER CAP. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 3 THIS IS A MAJOR REPAIR.
- [SDR 05FDEA02006](https://openairdocs.org/sdr/05FDEA02006.md): Seat Track · corroded · Jul 21, 2005 · N280FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 690-740 IS CORRODED LBL 24. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2
- [SDR 05FDEA02005](https://openairdocs.org/sdr/05FDEA02005.md): Seat Track · corroded · Jul 21, 2005 · N280FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 45 690-740 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2
- [SDR 05FDEA01972](https://openairdocs.org/sdr/05FDEA01972.md): Seat Track · corroded · Jul 17, 2005 · N280FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 344-480 RBL 24 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2
- [SDR 05FDEA01971](https://openairdocs.org/sdr/05FDEA01971.md): Seat Track · corroded · Jul 17, 2005 · N280FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 45 STA 740-757 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2
- [SDR 05FDEA01970](https://openairdocs.org/sdr/05FDEA01970.md): Seat Track · corroded · Jul 17, 2005 · N280FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BL 0 STA 480-600 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2
- [SDR 05FDEA01969](https://openairdocs.org/sdr/05FDEA01969.md): Seat Track · corroded · Jul 17, 2005 · N280FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BL 0 STA 600-720 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2
- [SDR 05FDEA01968](https://openairdocs.org/sdr/05FDEA01968.md): Seat Track · corroded · Jul 17, 2005 · N280FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 45 STA 480-690 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2
- [SDR 04FDEA00782](https://openairdocs.org/sdr/04FDEA00782.md): Fitting · cracked · Mar 31, 2004 · N280FE · Boeing 727200 · Ailerons
  > LEFT WING INBOARD AILERON HINGE FITTING AND WEB IS CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-1, REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-10-1 AND BOEING DWG 65-21709.
- [SDR 04FDEA00764](https://openairdocs.org/sdr/04FDEA00764.md): Hinge · gouged · Mar 27, 2004 · N280FE · Boeing 727200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR, DOOR HINGE LUG MINOR GOUGE REPAIR BS 616.5. COMPLIED WITH EA 7-5230-75124 DOOR - MAIN CARGO DOOR DOOR HINGE LUG MINOR GOUGE REPAIR FS 616.5 AT MAE.
- [SDR 03FDEA01584](https://openairdocs.org/sdr/03FDEA01584.md): Handle · inoperative · Sep 19, 2003 · N280FE · Boeing 727200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR LIGHT ILLUMINATED AIRBORNE. RETURNED TO DLH. LANDING OK AND PRESSURIZATION OK. FOUND SHORT IN LIGHT IN VENTRAL DOOR STAIR HANDLE AFT COMPARTMENT ON A/C. REPAIRED AS REQUIRED. OPS CHECK NORMAL.
- [SDR 03FDEA01303](https://openairdocs.org/sdr/03FDEA01303.md): Switch · failed · Aug 14, 2003 · N280FE · Boeing 727200 · Leading Edge Slat Control System
  > DURING FLAP RETRACTION L/E FLAP AMBER LIGHT REMAINED ILLUMINATED 26 S/O PANEL SHOWED 237 L/E SLAT NOT RETRACTED. REMOVED AND REPLACED BOTH RETRACT & EXTEND SWITCHES ON NR 7 SLAT ACTUATOR IAW 727-200 M/M 27-82-011-4. TESTED AS PER SAME REFER. OPS CHECKS GOOD
- [SDR 03FDEA01177](https://openairdocs.org/sdr/03FDEA01177.md): Proximity Sensor · out of adjust · Jul 30, 2003 · N280FE · Boeing 727200 · Door Warning System
  > LEVEL FL 190 280 KTS OCN LT TURB MAIN CARGO DOOR WARNING LIGHT ILLUMINATED STEADY THEN WENT DIM AND EXTINGUISHED AFTER 30 SEC AS WE COMPLIED WITH RED TABS. CHECKED OPERATION AND INDICATION OF MAIN CARGO DOOR, ONLY DISCREPANCY NOTED WAS INCORRECT ADJUSTMENT
- [SDR 01FDEA00804](https://openairdocs.org/sdr/01FDEA00804.md): Rib · cracked · Sep 4, 2001 · N280FE · Boeing 727233 · Wing, Rib/Bulkhead
  > LT WING LEAD EDGE RIB CRACKED FOR ACTUATOR ROD END CUTOUTS FOR NR 2 SLAT WS 640, WBL 540. REMOVED AND REPLACED RIBS PER SRM 57-30-4.
- [SDR 01FDEA00805](https://openairdocs.org/sdr/01FDEA00805.md): Pin · corroded · Sep 4, 2001 · N280FE · Boeing 727233 · Fuselage, Wing Attach Fittings
  > CORROSION ON LT AFT TERMINAL PIN BS 870. REMOVED AND REPLACED TERMINAL PIN PER 57-41-001-4.
- [SDR 01FDEA00806](https://openairdocs.org/sdr/01FDEA00806.md): Pressure Panel · cracked · Sep 4, 2001 · N280FE · Boeing 727233 · Fuselage Main, Bulkhead
  > RT NOSE WHEEL WELL SHELF WEB CRACKED AT LIGHTENING HOLE BS 291, WL 156, RBL 18. REMOVED AND REPLACED WEB PER SRM 51-20-1.
- [SDR 01FDEA00808](https://openairdocs.org/sdr/01FDEA00808.md): Skin Panel · cracked · Sep 4, 2001 · N280FE · Boeing 727233 · Nacelle/Pylon, Plate/Skin
  > UPPER O/B SKIN PANEL CRACKED ON NR 3 PYLON BS 1203 AT WL 240. REMOVED AND REPLACED PANEL PER SRM 51-20-1.
- [SDR 01FDEA00807](https://openairdocs.org/sdr/01FDEA00807.md): Cargo Track · corroded · Sep 4, 2001 · N280FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CARGO TRACK NR 6 AT BS 420 TO 440. REMOVED AND REPLACED TRACK PER SRM 53-10-5.
- [SDR 01FDEA00809](https://openairdocs.org/sdr/01FDEA00809.md): Rib · cracked · Sep 4, 2001 · N280FE · Boeing 727233 · Leading Edge Devices
  > RT WING NR 5 SLAT ACTUATOR ATTACH RIBS CRACKED WS 408 AND 411, WBL 320 AND 322. ROUTED OUT CRACKS PER SRM 57-50-1.
- [SDR 01FDEA00821](https://openairdocs.org/sdr/01FDEA00821.md): Skin Panel · cracked · Sep 4, 2001 · N280FE · Boeing 727233 · Nacelle/Pylon, Plate/Skin
  > N 925 UPR O/B SKIN PANEL CRACKED ON #3 PYLON BS 1203 AT WL 240. R&R PNL PER SRM 51-20-1.
- [SDR 01FDEA00819](https://openairdocs.org/sdr/01FDEA00819.md): Web · cracked · Sep 4, 2001 · N280FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > N 1481 RH NOSE WHEEL WELL SHELF WEB CRACKED AT LIGHTNING HOLE BS 291, WL 156, RBL 18. R&R WEB PER SRM 51-20-1.
- [SDR 01FDEA00817](https://openairdocs.org/sdr/01FDEA00817.md): Rib · cracked · Sep 4, 2001 · N280FE · Boeing 727233 · Wing, Control Surface Attach Fittings
  > N 1494 LH WING L/E RIB CRACKED FOR ACTUATOR ROD END CUT-OUTS FOR #2 SLAT AT WS 640, WBL 540. R&R RIBS PER SRM 57-30-4.
- [SDR 01FDEA00782](https://openairdocs.org/sdr/01FDEA00782.md): Pin · cracked · Aug 28, 2001 · N280FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > FLANGE ON RT FWD TERMINAL PIN CRACKED BS 740. REMOVED AND REPLACED PIN PER MM 57-41-001-4.
- [SDR 01FDEA00781](https://openairdocs.org/sdr/01FDEA00781.md): Skin · corroded · Aug 28, 2001 · N280FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > A.5 INCH CRACK AND CORROSION ON SKIN AT BS 680-720 AT STR 28R.

Next page: https://openairdocs.org/deregistered/N280FE-2013-12-19/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 = 'N280FE' AND deregistration_id = 'N280FE-2013-12-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N280FE-2013-12-19/reports

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