# Service difficulty reports: N281FE, cancelled Dec 19, 2013

A list on [N281FE, cancelled Dec 19, 2013](https://openairdocs.org/deregistered/N281FE-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 · 95 reports

- [SDR FDEA201104271649](https://openairdocs.org/sdr/FDEA201104271649.md): Radar · inoperative · Apr 27, 2011 · N281FE · Boeing 727233 · Weather Radar System
  > WX RADAR SHOWS A RING OF GROUND RETURN AT ALL TILT ANGLES AND RANGES. DOES NOT DEPICT WEATHER RETURNS. REPLACED WX/RADAR R/T IAW AMM 34-41-041-4, AND WX RADAR INDICATOR IAW AMM 34-41-031-4, CK'S GOOD NOW.
- [SDR FDEA200904211367](https://openairdocs.org/sdr/FDEA200904211367.md): Switch · out of adjust · Apr 21, 2009 · N281FE · Boeing 727233 · Landing Gear Position and Warning
  > RIGHT GEAR AFTER DEPARTURE FROM PVD, WHEN FIRST OFFICER MOVED LANDING GEAR LEVER FROM UP TO OFF THE LIGHT REMAINED ILLUMINATED WITH A R GEAR DOOR LIGHT ILLUMINATED ON SECOND OFFICERS DOORS PANEL. COMPLIED WITH QRH AND LEFT HANDLE IN THE UP POSITION WHERE NO L
- [SDR FDEA200902030436](https://openairdocs.org/sdr/FDEA200902030436.md): Hinge · cracked · Feb 3, 2009 · N281FE · Boeing 727233 · Fuselage, Door Hinge
  > MCD AFT HINGE LAST LUG CRACKED FROM EDGE TO FASTENER HOLE. REMOVED MCD AFT UPPER HINGE IAW FX DWG 52FX1433 REV E AND B727 SRM 51-30-2. LOCATED SHAPED AND DRILLED NEW HINGES SEGMENT 48 INCH BY 4 INCH IAW B727 SRM 51-30-5. TREATED AND PRIMED NEW PART IAW B7
- [SDR FDEA200901200269](https://openairdocs.org/sdr/FDEA200901200269.md): Panel · dented · Jan 20, 2009 · N281FE · Boeing 727233 · Fuselage Main, Bulkhead
  > E/E BAY UPPER CHORD SKIN STRUCTURE HAS BULGE AT BS 328 BL 0. EVALUATED BULGE ON NLG WW UPPER SKIN BS 328 BL0 AS AN OIL CANNING DENT. DETERMINED TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. DRILLED 1 INCH ROUND HOLE TO REMOVE DAMAGE IAW B727 SRM 51-10-1.
- [SDR FDEA200901190246](https://openairdocs.org/sdr/FDEA200901190246.md): Web · dented · Jan 19, 2009 · N281FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > E/E BAY UPPER STRUCTURE HAS BULGE AT BS 328 BL0. EVALUATED BULGE ON N/W/W UPPER SKIN BS 328 BL0 AS AN OIL CANNING DENT DETERMINED TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1. DRILLED 1" INCH ROUND HOLE TO REMOVE DAMAGE IAW SRM 51-10-1. FABRICATED REPAIR DOUBL
- [SDR FDEA200901180230](https://openairdocs.org/sdr/FDEA200901180230.md): Spar · cracked · Jan 18, 2009 · N281FE · Boeing 727233 · Wing Spar
  > CRACK ANGLE FALSE SPAR AT NR 7 SPOILER ACTUATOR CUT-OUT. CRACKED ANGLE OUT OF LIMITS IAW SRM 57-10-1 FIG 1. REMOVED SUPPORT FITTING & VERTICAL STRUCTURE IAW DWG SR27-57-038 & SRM 51-30-2. TRIMMED AFT WEB AT CUT LINE IAW DWG SR27-57-038 REV C. REMOVED CRACK
- [SDR 08FDEA03633](https://openairdocs.org/sdr/08FDEA03633.md): Actuator · failed · Aug 28, 2008 · N281FE · Boeing 727233 · Leading Edge Slat Actuator
  > NR 8 SLAT FAILED TO RETRACT NORMALLY. LED AMBER ON FRONT PANEL AND S/O PANEL. REMOVED PANELS ON EACH SIDE OF ACTUATOR. FOUND WIRING CLAMPS LOOSE TIGHTENED. WILL CHANGE ACTUATOR OR SWITCH FOR MOCC. REPLACED NR 8 SLAT ACTUATOR REF MM 27-81-032-4. OPS AND L
- [SDR 08FDEA03522](https://openairdocs.org/sdr/08FDEA03522.md): Pump · malfunctioned · Aug 20, 2008 · N281FE · Boeing 727200 · Engine Fuel Pump
  > AT FL 350 IN STEADY CRUISE FLT, FELT SLIGHT VIBRATION FOLLOWED BY NR 1 EPR ROLL BACK, NR 1 N1,N2 EGT ROLLBACK. N1 STABILIZED AT 26 PERCENT, EGT 180 DEG NR 1 GEN BREAKER LIGHT ON AND NR 1 LOW OIL PRESSURE LIGHT ON. THRUST LEVEL BOUGHT TO IDLE AND DESCENT STAR
- [SDR 06FDEA04254](https://openairdocs.org/sdr/06FDEA04254.md): Control Cable · out of rig · Dec 16, 2006 · N281FE · Boeing 727233 · Main Landing Gear
  > THE L/GEAR EXTENDED IN FLT WITH GEAR HANDLE IN THE OFF POS. THE EXTENSION WAS UNCOMMANDED WHILE THE GEAR WERE UP AND LOCKED AND THE HANDLE IN THE OFF POS. THE A/C WAS CLIMBING THRU 3K FT AT 180 KIAS AND FLAPS 15. THE MAIN GEAR SHOWED DWN AND LOCKED BUT THE
- [SDR 06FDEA2791](https://openairdocs.org/sdr/06FDEA2791.md): Skin · damaged · Aug 2, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL FLUSH REPAIR ON LT LWR FUSELAGE APPROX 3 X 2 INCHES STA 260, S21L TO 22L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED SKIN PER FED EX EA 7-5330-100558.
- [SDR 06FDEA2790](https://openairdocs.org/sdr/06FDEA2790.md): Stringer · corroded · Aug 2, 2006 · N281FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CORROSION FWD CARGO BAY: ON STRINGER 28 AT BS 506, LBL 6. REPAIRED STRINGER PER SRM 53-10-3 FIG 1 DETAIL II.
- [SDR 06FDEA2765](https://openairdocs.org/sdr/06FDEA2765.md): Door · damaged · Aug 1, 2006 · N281FE · Boeing 727200 · Cargo/Baggage Doors
  > EXTERNAL DOUBLER REPAIRS, 6 EACH AT NR 3 CARGO DOOR REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED NR 3 CARGO DOOR PER SRM 51-30-2 AND FED EX MM 52-35-051-4.
- [SDR 06FDEA2750](https://openairdocs.org/sdr/06FDEA2750.md): Threshold · cracked · Jul 31, 2006 · N281FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF STUB FRAME FOUND GALLEY DOOR THRESHOLD WEB CRACKED BS 376 WL 208 RBL 65. REPAIRED THRESHOLD PER FED EX DWG 65-56153 AND SRM 51-30-2.
- [SDR 06FDEA2749](https://openairdocs.org/sdr/06FDEA2749.md): Door Frame · cracked · Jul 31, 2006 · N281FE · Boeing 727200 · Fuselage Main, Structure
  > MAIN CARGO BAY, FWD SERVICE DOOR CUTOUT FWD FRAME IS CRACKED AT BS 380 RBL 65 WL 209. REPAIRED FRAME PER SRM 51-40-3.
- [SDR 06FDEA2710](https://openairdocs.org/sdr/06FDEA2710.md): Skin · damaged · Jul 27, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR APPROX 8" BY 5" ON RIGHT LOWER FWD CORNER OF AFT CARGO DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR, REPAIRED DAMAGE AND INSTALLED NEW REPAIR
- [SDR 06FDEA2709](https://openairdocs.org/sdr/06FDEA2709.md): Stop Fitting · gouged · Jul 27, 2006 · N281FE · Boeing 727233 · Cargo/Baggage Doors
  > AFT LOWER CARGO, AFT NR 2 (FROM BOTTOM) STOP PIN FITTING GOUGED). REPAIRED NR 2 (FROM BOTTOM) CARGO DOOR STOP PIN FITTING IAW FED EX EA 7-5230-100556.
- [SDR 06FDEA2687](https://openairdocs.org/sdr/06FDEA2687.md): Skin · damaged · Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR AT NR 3 CARGO DOOR CUTOUTS, 13 INCHES X 5.5 INCHES STA 1148, STRINGER 23R TO 24R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIRED SKIN PER FEDEX EA 7-5330-100561.
- [SDR 06FDEA2685](https://openairdocs.org/sdr/06FDEA2685.md): Skin · damaged · Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > N01370 EXTERNAL DOUBLER REPAIR APP. 8.5 X 6.5 ON LT LWR FUSELAGESTA 203 STR 23L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPARIED SKIN IAW SRM 53-30-3 FIG 24.
- [SDR 06FDEA2686](https://openairdocs.org/sdr/06FDEA2686.md): Skin · damaged · Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > N01354 EXTERNAL DOUBLER REPAIR APPROX 6 INCHES X 8 INCHES ON RT LOWER FUSELAGE STA 294, WL 168. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXTERNAL DOUBLER INSTALLED PER FED EX EA 7-5
- [SDR 06FDEA2679](https://openairdocs.org/sdr/06FDEA2679.md): Skin · damaged · Jul 25, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR APPROX 22 X 19 INCHES ON RIGHT HAND LOWER FUSELAGE STA 195 - STA 220, STR 19R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER FED EX EA 7-5330-100557.
- [SDR 06FDEA2678](https://openairdocs.org/sdr/06FDEA2678.md): Floorbeam · corroded · Jul 25, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor Beam
  > WHILE WORKING OK TO CLOSE MAIN CARGO AREA FLOORBOARDS, FOUND CORROSION ON PREVIOUS BLEND ON TOP OF FLOORBEAM, AND ONE MISDRILLED HOLE AT; BS 1030, LBL 9, WL 208. CUT OUT CORROSION DAMAGE AND REPAIRED UPPER CHORD OF FLOORBEAM PER SRM 53-10-8 FIG 3.
- [SDR 06FDEA2665](https://openairdocs.org/sdr/06FDEA2665.md): Floorbeam · corroded · Jul 24, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 1030, RBL 10, WL 208. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR PARTS PER SRM 53-10-8 FIG 3.
- [SDR 06FDEA2630](https://openairdocs.org/sdr/06FDEA2630.md): Skin · misrepaired · Jul 19, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL FLUSH REPAIR ON LT LWR FUSELAGE APPROX 3 X 2.5 INCHES STA 220, S21L TO S22L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* FLUSH REPAIR ON LT LWR FUSELAGE STA 220, STR 21L
- [SDR 06FDEA2620](https://openairdocs.org/sdr/06FDEA2620.md): Skin · corroded · Jul 18, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > WHILE WORKING NR N01047 FOUND CORROSION IN FWD CARGO BAY SKIN AT BS 596, LBL 9. *S/D* REMOVED CORROSION FWD CARGO BAY SKIN BS 596 LBL 9 AND REPAIRED IAW SRM 53-30-3, 51-30-2.
- [SDR 06FDEA2618](https://openairdocs.org/sdr/06FDEA2618.md): Skin · dented · Jul 18, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > DENT IN SKIN AT BS 227, WL 178, 3 INCHES BELOW STR 19 LT. *S/D* REMOVED EXISTING REPAIR BS 700 PLUS 10 TO 720 STR 28R AND INSTALLED REPAIR IN SKIN IAW SRM 53-30-3 FIG 1.
- [SDR 06FDEA2619](https://openairdocs.org/sdr/06FDEA2619.md): Unknown · unknown · Jul 18, 2006 · N281FE · Boeing 727200 · Standard Practices/Structures
  > EXTERNAL DOUBLER REPAIR APPROX 12 X 8 INCHES ON RIGHT HAND LOWER FUSELAGE STA 720 STR 2R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR BS 700 PLUS 10 - 720 STR 28
- [SDR 06FDEA2600](https://openairdocs.org/sdr/06FDEA2600.md): Frame · dented · Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, Frame
  > FOUND STA 380 STR 21 RT FRAME INBOARD FLANGE DENTED. REPAIRED DENT AT BS 380 STR 21R IAW SRM 51-40-3.
- [SDR 06FDEA2599](https://openairdocs.org/sdr/06FDEA2599.md): Floorbeam · corroded · Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM AT BS-1110 BL-0 CORRODED ON LOWER FLANGE, UPPER SURFACE. FOUND CORROSION TO BE BEYOND LIMITS, REMOVED DAMAGED SECTION OF FLOORBEAM. FABRICATED REPAIR PARTS, DRILLED, ALODINED, PRIMED REPAIR PARTS AND INSTALLED REF SRM 53-10-1, 51-30-5, 53-10-
- [SDR 06FDEA2598](https://openairdocs.org/sdr/06FDEA2598.md): Stringer · cracked · Jul 17, 2006 · N281FE · Boeing 727233 · Vertical Stabilizer, Spar/Rib
  > FOUND VERTICAL STAB INTERIOR, STR 8L IS CRACKED AT NR 2 RIB. REMOVED DAMAGED AREA OF STR 8L AT NR 2 RIB AND REPAIRED IAW SRM 55-30-4.
- [SDR 06FDEA2597](https://openairdocs.org/sdr/06FDEA2597.md): Frame · dented · Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, Frame
  > DENT ON I/B FRAME FLANGE BS 970 LT AT STR 26L IN AFT CARGO BAY. *S/D* REPAIRED DENT ON I/B FRAME FLANGE BS 970 STR 26L IAW SRM 51-40-3.
- [SDR 06FDEA2596](https://openairdocs.org/sdr/06FDEA2596.md): Frame · dented · Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, Frame
  > DENT ON I/B FRAME FLANGE BS 970 LT BETWEEN STR 23L AND STR 24L IN AFT CARGO BAY. *S/D* REPAIRED DENT ON I/B FRAME FLANGE BS 970 BETWEEN STR 23L AND 24L IAW SRM 51-40-3.
- [SDR 06FDEA2595](https://openairdocs.org/sdr/06FDEA2595.md): Frame · dented · Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, Frame
  > DENT ON INBOARD FRAME AT BS 990 LEFT AT STR 26L IN AFT CARGO BAY. *S/D* REPAIRED DENT IN FRAME BS 990 STR 26L IAW SRM 51-40-3.
- [SDR 06FDEA2601](https://openairdocs.org/sdr/06FDEA2601.md): Floorbeam · misdrilled · Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, Floor Beam
  > FOUND DOUBLE HOLE IN FLOORBEAM AT BS 910 LBL 65 WL 208 TOP FLANGE FWD SIDES COMMON TO CREASE BEAM WEB. CUT OUT DAMAGED SECTION OF FLOORBEAM AND INSTALLED REPAIR ANGLES ON UPPER CHORD AT BS 910, LBL 65, PER SRM 53-10-8 AND DRAWING NR 06-2756.
- [SDR 06FDEA2594](https://openairdocs.org/sdr/06FDEA2594.md): Frame · dented · Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, Frame
  > DENT ON INBOARD FRAME AT BS 1010 LT AT STR 26L IN AFT CARGO BAY.
- [SDR 06FDEA2568](https://openairdocs.org/sdr/06FDEA2568.md): Unknown · unknown · Jul 14, 2006 · N281FE · Boeing 727200 · Standard Practices/Structures
  > EXTERNAL DOUBLER REPAIR APP. 8" X 6" ON R/H LOWER FUSELAGE STA 1156 STRINGER 29R TO 30R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR AT BS 1156 STR 29R TO 30R
- [SDR 06FDEA2567](https://openairdocs.org/sdr/06FDEA2567.md): Skin · dented · Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > A 3 INCH DIAMETER BLENDED AREA WITH ASSOCIATED DENT AND CREASE STA 1270 STRINGER 21L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED BLEND AT STA 1270 STR 21L IAW SRM 53-30-1
- [SDR 06FDEA2566](https://openairdocs.org/sdr/06FDEA2566.md): Frame · dented · Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, Frame
  > DENT ON I/B FRAME FLANGE BS 950F LT BETWEEN STR 23L AND STR 24L IN AFT CARGO BAY. REPAIRED DENT IN FRAME IAW SRM 51-30-5
- [SDR 06FDEA2565](https://openairdocs.org/sdr/06FDEA2565.md): Frame · dented · Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, Frame
  > DENT ON I/B FRAME FLANGE BS 950F LT BETWEEN STR 25L AND STR 26L IN AFT CARGO BAY. REPAIRED FRAME IAW SRM 51-30-5, 51-30-8, 51-10-2
- [SDR 06FDEA2552](https://openairdocs.org/sdr/06FDEA2552.md): Skin · chafed · Jul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN UNDER WING TO BODY FAIRING, IS CHAFED AT LT FWD L/E, BS 720D PLUS 11, STR 19L. *S/D* REPAIRED SKIN UNDER WING TO BODY FAIRING BS 720D 11 STR 19L IAW SRM 53-30-3, 51-30-2, 51-20-1.
- [SDR 06FDEA2551](https://openairdocs.org/sdr/06FDEA2551.md): Skin · chafed · Jul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN UNDER WING TO BODY FAIRING, IS CHAFED AT RT FWD L/E, BS 720D PLUS 11 TP 720E, BELOW STR 17R TO STR 19R. *S/D* REPAIRED SKIN UNDER WING TO BODY FAIRING BS 720D 11 TO BS 720D STR 17R-19R IAW SRM 53-30-3, SRM 51-30-2, SRM 51-20-1.
- [SDR 06FDEA2550](https://openairdocs.org/sdr/06FDEA2550.md): Floorbeam · unknown · Jul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor Beam
  > FLOORBEAM UPPER TEE REPAIR APPROX 12 INCHES LONG ON MAIN CABIN FLOORBEAM STA 1070 RBL 31 TO RBL 42 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* REPAIRED FLOORBEAM T-CAP BS 1070 RBL
- [SDR 06FDEA2549](https://openairdocs.org/sdr/06FDEA2549.md): Skin · misrepaired · Jul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL DOUBLER REPAIR APP 27 X 11 INCHES ON RIGHT HAND LOWER FUSELAGE STA 720 STR 22R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXTERNAL DOUBLER BS 720 STR 22R WAS NOT INSTALLED PE
- [SDR 06FDEA2496](https://openairdocs.org/sdr/06FDEA2496.md): Flap Track · corroded · Jul 10, 2006 · N281FE · Boeing 727233 · Trailing Edge Flaps
  > FOUND CORROSION ON NUMBER 3 FLAP TRACK AFT MOUNTING SURFACE. REMOVED AND REPLACED #3 FLAP TRACK IAW FED EX WORK CARD 27X5705-03
- [SDR 06FDEA2494](https://openairdocs.org/sdr/06FDEA2494.md): Shear Plate · misdrilled · Jul 10, 2006 · N281FE · Boeing 727233 · Vertical Stabilizer
  > FOUND VERT FIN, LT UPPER SHEAR PLATE TO HAVE 3 "SNOWMAN" HOLES. REMOVED AND REPLACED VERT FIN LT UPPER SHEAR PLATE IAW SRM 51-30-2, 51-30-5
- [SDR 06FDEA2493](https://openairdocs.org/sdr/06FDEA2493.md): Fitting · damaged · Jul 10, 2006 · N281FE · Boeing 727233 · Vertical Stabilizer, Attach Fittings
  > FOUND VERT FIN "C" SHAPED SHEAR FITTING TO HAVE 3 "SNOWMAN" HOLES. REMOVED AND REPLACED VERT FIN "C" SHAPED SHEAR FITTING IAW SRM 51-30-2, 51-30-5
- [SDR 06FDEA2499](https://openairdocs.org/sdr/06FDEA2499.md): Skin · damaged · Jul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN UNDER ATC NR 2 ANTENNA, HAS SCRIBE MARKS. REMOVED DAMAGE FROM FUSELAGE SKIN UNDER ATC NR 2 ANTENNA REPAIRED IAW SRM 53-30-3
- [SDR 06FDEA2498](https://openairdocs.org/sdr/06FDEA2498.md): Skin · misrepaired · Jul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FOUND FLUSH DOUBLER REPAIR STA 680-688 STR 28R - 29R, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR BS 680-688 STR 28-29R DID NOT COMPLY WITH APPROVED FAA REP
- [SDR 06FDEA2497](https://openairdocs.org/sdr/06FDEA2497.md): Skin · cracked · Jul 10, 2006 · N281FE · Boeing 727233 · Trailing Edge Flaps
  > FOUND LEFT WING T/E I/B MIDFLAP, CRACKED AT CUTOUT FOR INBOARD PUSHROD IN AFT CHORD. REPAIRED CRACK ON LEFT WING T/E IB MIDFLAP IAW SRM 51-30-2, 51-40-4 FIG 1
- [SDR 06FDEA2495](https://openairdocs.org/sdr/06FDEA2495.md): Beam · chafed · Jul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, Structure
  > MAIN CARGO BAY, LONGITUDINAL BEAM IS CHAFED AT FASTENER HOLES (FROM NUTPLATES) BS 850 TO BS 763 RBL 25 WL 208. FOUND CHAFE AREA TO BE BEYOND LIMITS. REMOVED TRACK EXPANSION LINK AND LONGITUDINAL BEAM, RBL 25, LOCATED AND DRILLED NEW LONGITUDINAL BEAM. INS
- [SDR 06FDEA2471](https://openairdocs.org/sdr/06FDEA2471.md): Carriage · gouged · Jul 7, 2006 · N281FE · Boeing 727233 · Trailing Edge Flaps
  > FOUND RT WING I/B AFT FLAP, I/B CARRIAGE GOUGED. REPAIR ACCOMPLISHED PER FED EX EA 7-5710-100554.

Next page: https://openairdocs.org/deregistered/N281FE-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 = 'N281FE' AND deregistration_id = 'N281FE-2013-12-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N281FE-2013-12-19/reports

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