N281FE, cancelled Dec 19, 2013

Service difficulty reports · 95

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201104271649Radar · inoperativeWX 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.Apr 27, 2011 · N281FE · Boeing 727233 · Weather Radar SystemSDR FDEA200904211367Switch · out of adjustRIGHT 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 LApr 21, 2009 · N281FE · Boeing 727233 · Landing Gear Position and WarningSDR FDEA200902030436Hinge · crackedMCD 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 B7Feb 3, 2009 · N281FE · Boeing 727233 · Fuselage, Door HingeSDR FDEA200901200269Panel · dentedE/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. Jan 20, 2009 · N281FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA200901190246Web · dentedE/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 DOUBLJan 19, 2009 · N281FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200901180230Spar · crackedCRACK 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 CRACKJan 18, 2009 · N281FE · Boeing 727233 · Wing SparSDR 08FDEA03633Actuator · failedNR 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 LAug 28, 2008 · N281FE · Boeing 727233 · Leading Edge Slat ActuatorSDR 08FDEA03522Pump · malfunctionedAT 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 STARAug 20, 2008 · N281FE · Boeing 727200 · Engine Fuel PumpSDR 06FDEA04254Control Cable · out of rigTHE 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 Dec 16, 2006 · N281FE · Boeing 727233 · Main Landing GearSDR 06FDEA2791Skin · damagedEXTERNAL 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.Aug 2, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2790Stringer · corrodedCORROSION FWD CARGO BAY: ON STRINGER 28 AT BS 506, LBL 6. REPAIRED STRINGER PER SRM 53-10-3 FIG 1 DETAIL II.Aug 2, 2006 · N281FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA2765Door · damagedEXTERNAL 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.Aug 1, 2006 · N281FE · Boeing 727200 · Cargo/Baggage DoorsSDR 06FDEA2750Threshold · crackedAFTER 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.Jul 31, 2006 · N281FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA2749Door Frame · crackedMAIN CARGO BAY, FWD SERVICE DOOR CUTOUT FWD FRAME IS CRACKED AT BS 380 RBL 65 WL 209. REPAIRED FRAME PER SRM 51-40-3.Jul 31, 2006 · N281FE · Boeing 727200 · Fuselage Main, StructureSDR 06FDEA2710Skin · damagedEXTERNAL 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 REPAIRJul 27, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2709Stop Fitting · gougedAFT 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.Jul 27, 2006 · N281FE · Boeing 727233 · Cargo/Baggage DoorsSDR 06FDEA2687Skin · damagedEXTERNAL 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.Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2685Skin · damagedN01370 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.Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2686Skin · damagedN01354 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 7-5Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2679Skin · damagedEXTERNAL 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.Jul 25, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2678Floorbeam · corrodedWHILE 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.Jul 25, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2665Floorbeam · corrodedCORROSION 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.Jul 24, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2630Skin · misrepairedEXTERNAL 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 21LJul 19, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2620Skin · corrodedWHILE 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.Jul 18, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2618Skin · dentedDENT 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.Jul 18, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2619Unknown · unknownEXTERNAL 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 28Jul 18, 2006 · N281FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA2600Frame · dentedFOUND STA 380 STR 21 RT FRAME INBOARD FLANGE DENTED. REPAIRED DENT AT BS 380 STR 21R IAW SRM 51-40-3.Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA2599Floorbeam · corrodedFOUND 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-Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 06FDEA2598Stringer · crackedFOUND 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.Jul 17, 2006 · N281FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 06FDEA2597Frame · dentedDENT 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.Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2596Frame · dentedDENT 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.Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2595Frame · dentedDENT 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.Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2601Floorbeam · misdrilledFOUND 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.Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 06FDEA2594Frame · dentedDENT ON INBOARD FRAME AT BS 1010 LT AT STR 26L IN AFT CARGO BAY.Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2568Unknown · unknownEXTERNAL 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 30RJul 14, 2006 · N281FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA2567Skin · dentedA 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 53-30-1Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2566Frame · dentedDENT ON I/B FRAME FLANGE BS 950F LT BETWEEN STR 23L AND STR 24L IN AFT CARGO BAY. REPAIRED DENT IN FRAME IAW SRM 51-30-5Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2565Frame · dentedDENT 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, 51-10-2Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2552Skin · chafedFUSELAGE 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.Jul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2551Skin · chafedFUSELAGE 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.Jul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2550Floorbeam · unknownFLOORBEAM 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 RBLJul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2549Skin · misrepairedEXTERNAL 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 PEJul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2496Flap Track · corrodedFOUND CORROSION ON NUMBER 3 FLAP TRACK AFT MOUNTING SURFACE. REMOVED AND REPLACED #3 FLAP TRACK IAW FED EX WORK CARD 27X5705-03Jul 10, 2006 · N281FE · Boeing 727233 · Trailing Edge FlapsSDR 06FDEA2494Shear Plate · misdrilledFOUND 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, 51-30-5Jul 10, 2006 · N281FE · Boeing 727233 · Vertical StabilizerSDR 06FDEA2493Fitting · damagedFOUND 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, 51-30-5Jul 10, 2006 · N281FE · Boeing 727233 · Vertical Stabilizer, Attach FittingsSDR 06FDEA2499Skin · damagedFOUND FUSELAGE SKIN UNDER ATC NR 2 ANTENNA, HAS SCRIBE MARKS. REMOVED DAMAGE FROM FUSELAGE SKIN UNDER ATC NR 2 ANTENNA REPAIRED IAW SRM 53-30-3Jul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2498Skin · misrepairedFOUND 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 REPJul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2497Skin · crackedFOUND 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 1Jul 10, 2006 · N281FE · Boeing 727233 · Trailing Edge FlapsSDR 06FDEA2495Beam · chafedMAIN 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. INSJul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, StructureSDR 06FDEA2471Carriage · gougedFOUND RT WING I/B AFT FLAP, I/B CARRIAGE GOUGED. REPAIR ACCOMPLISHED PER FED EX EA 7-5710-100554.Jul 7, 2006 · N281FE · Boeing 727233 · Trailing Edge Flaps
Back to N281FE, cancelled Dec 19, 2013