N246FE, cancelled Jul 28, 2009

Service difficulty reports · 57

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 = 'N246FE' AND deregistration_id = 'N246FE-2009-07-28'
  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 08FDEA04015Transmitter · malfunctionedWITH T/O PWR SET ENGINE NR 3 N1 WAS 87 PECENT WITH EPR SET AT STD PWR 2.12, DEFERED EPR INDICATION. REMOVED AND REPLACED THE EPR TRANSMITTER.Sep 24, 2008 · N246FE · Boeing 727277 · Engine Pressure Ratio (EPR)SDR 08FDEA00089Frame · crackedLOWER FWD CARGO, SPLICE FRAME AT ST 580, STR 22L IS CRACKED. VERIFIED BY HFEC. REMOVED 53FX1350 SPLICE FRAME, FABRICATED AND INSTALLED NEW SPLICE FRAME IAW FEDEX DRWG 53FX1350 REV A AND 727-200 SRM 51-30-2.Jan 10, 2008 · N246FE · Boeing 727277 · Fuselage Main, FrameSDR 07FDEA02786Smoke Detector · failedDESCENT BELL SOUNDED MAIN FIRE LIGHT ILLUMINATED, SMOKE ILLUMINATED. EMERGENCY DECLARED. FUMES WERE PRESENT IN THE COCKPIT. ALL EMERGENCY QRH CHECKLIST ACCOMPLISHED. WHILE ENTERING A/C NOTICED NO ODOR OF ANY SORT, INSPECTED A/C FOR ANY SIGNS OF HEAT STRAug 7, 2007 · N246FE · Boeing 727277 · Smoke DetectionSDR 07FDEA00627Receptacle · crackedTHREE RECEPTACLES DEFECTIVE ON NR 3 PYLON STRUCTURE WHERE PANEL 5402 MOUNTS TO PYLON. REPLACED THE DEFECTIVE RECEPTACLES AT PYLON PANEL 5502 MOUNT AREA. IAW 727-200 SRM 51-30-2. REINSTALLED PANEL 5502.Dec 22, 2006 · N246FE · Boeing 727277 · Nacelle/Pylon, Main FrameSDR 06FDEA04305Beam · crackedNR 3 CARGO DOOR, LWR BEAM CRACKED FWD END. REPAIRED IAW EA 7-5230-106835 PT1 REF WRI 52-30/8690.Dec 22, 2006 · N246FE · Boeing 727200 · Cargo/Baggage DoorsSDR 06FDEA0984Warning System · activatedON TAKEOFF ROLL LED INDICATIONS WENT AMBER THEN BACK TO GREEN, AT 45-60 KTS WENT AMBER. TAKEOFF REJECTED.Mar 8, 2006 · N246FE · Boeing 727200 · Leading Edge Slat Control SystemSDR 04FDEA02573Frame · crackedRIGHT MLG WHEEL WELL 870 BULKHEAD I/B LWR SUPPORT FRAME IS CRACKED JUST I/B OF BLEED AIR SHUTOFF VALVE.Aug 29, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02563Frame · crackedCOMPLY WITH EO 7-5310-7-3367 PT 9 FOR CRACK IN 783.95 FRAME RT. *S/D* COMPLIED WITH EO 7-5310-7-3367 PT 9.Aug 25, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02552Frame · damagedFRAME DAMAGED AT BS 1166, BETWEEN STRINGER 3 AND 4 RT. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1166 BETWEEN STR 3 & 4 IAW SRM 51-40-3.Aug 23, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02551Skin · chafedFUSELAGE SKIN CHAFED STA 720D 12 STR 19L. *S/D* REPAIRED DAMAGED UPPER SKIN AT BS 720D PLUS 12 STR 19L PER SRM 53-30-3 DETAIL 2 & FED EX SR27-57-056 DRAWING.Aug 23, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02530Skin · bentAFT CARGO DOOR CUTOUT LOWER EDGE SKIN /DOUBLERS ARE BENT. REPAIRED DAMAGED AFT CARGO DOOR CUT-OUT SKIN/DOUBLERS PER EA 7-5330-55360Aug 19, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02529Doubler · damagedNR 1400, RT STA 600-620 STR 9, SKIN REPAIR DOUBLER REQUIRES FURTHER EVALUATION. REMOVED SKIN DOUBLER AT STA 600 STR 9 RH AND REPAIRED PER SRM 53-30-3 FIG 3, REPAIRED DAMAGED STRINGER AT STA 600 9 RH PER SRM 53-10-3 AND REPAIRED DAMAGED TEAR STRAP AT STA 600 Aug 19, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02500Shear Tie · corrodedCORROSION ON FWD FLANGE OF FRAME SHEAR TIE AT BS 480 BETWEEN STR 27L AND 28L. *S/D* REMOVED CORROSION ON FWD FLANGE OF FRAME SHEAR TIE STA 480 BETWEEN STR 27L AND 28L. REMOVED 021. 1 X 1 INCH FROM .063, OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIAug 18, 2004 · N246FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA02493Frame · crackedCRACKED OUTER FRAME ANGLE STA 804.5 STR 14R. *S/D* REMOVED & REPLACED ANGLE AT BS 804.5 STR 14R PER SRM 51-30-2 & 51-10-1.Aug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02492Floorbeam · corrodedCORROSION ON FLOORBEAM BS 312 WL 208 LBL 3-47 AT FASTENER AND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM STA 312, W/L 208, LBL 3-47, AT FASTENER & NUT PLATE HOLES, REMOVED 5 X 2 INCH LBL 3 FROM .090. LBL 4 4 X 2 X .0015 INCH. LBL 20 6 X 2 X .005 INCH, LAug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA02490Frame · bentFRAME BENT BS 950F AT STR 26 LT, AFT CARGO BAY. *S/D* FRAME DENT BS 950F AT STR 26 LT AFT CARGO FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3.Aug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02474Floorbeam · corrodedCORROSION IN COCKPIT AT 25G BEAM UPPER FLANGE BS 267 WL 208. REMOVED AND REPLACED G-BEAM CHORD IAW SRM 51-30-5, 51-30-2, 51-30-8.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA02473Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 680 ABOVE STR 24L. REPAIRED BS 680. FRAME AT STR 24L IAW SRM 51-40-3 FIG 1.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02472Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 660 ABOVE STR 24L. REPAIRED BS 660 FRAME ST STR 24L IAW SRM 51-40-3 FIG 1.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02471Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 24L AND 25L. REPAIRED FRAME AT BS 520 BETWEEN STR 29L AND 25L IAW SRM 51-40-3 AND EA 7-5310- 70673.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02470Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 22L AND 23L. REPAIRED FRAME AT BS 520 BETWEEN STR 22L AND 23L IAW SRM 51-40-3 AND EA 7-5310- 70673.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA02469Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 500 BETWEEN STR 22L AND 23L. *S/D* REMOVED DAMAGE AREA OF FRAME BS 500 FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 51-40-3.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02468Stringer · crackedCRACKED STRINGER 15 RT BS 720B 4 INCHES. *S/D* REPAIRED STR 15R AT BS 720B 4 INCHES PER SRM 53-10-3.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02467Stringer · crackedCRACKED STRINGER 15 LT AT BS 720B 4 INCHES. *S/D* REPAIRED STR 15L, BS 720B 4 INCHES IAW SRM 53-10-3.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02460Angle · corrodedN00734 CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB LOWER ANGLE STA 490 TO 500 LBL 9. REMOVED ANGLE AND FABRICATED, ALODINED AND PRIMED AND INSTALLED ANGLE IAW SRM 51-20-1, SRM 51-30-2, FED-EX MM 51-20-151-7Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA02458Keelbeam · corrodedN00636 CORROSION, ON KEELBEAM STR 29L .950F 3 ON FLANGE AROUND FASTENER. ** SD COMING **Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, KeelSDR 04FDEA02461Stringer · corrodedCORROSION FOUND WHILE WORKING NRC NR00286 FOUND CORRODED STR 30 AT BS 1084 BL 0. REPAIRED STR 30 AT BS 1084 IAW SRM 53-10-3Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02459Keelbeam · corrodedCORROSION ON KEELBEAM STR 29L, 950F+9 ON FLANGE AROUND HILOCK. CORROSION ON LT KEELBEAM BS 950F+9, FOUND TO BE OUT OF LIMITS. IAW SRM 53-10-1. REPAIRED IAW MM 27-53-013.Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, KeelSDR 04FDEA02457Keelbeam · corrodedCORROSION ON RT KEELBEAM, STR 29 RT, BS 950D+15. CORROSION ON RT KEEL BEAM BS 950D15, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, KeelSDR 04FDEA02456Keelbeam · corrodedCORROSION ON RT KEELBEAM, STR 29 RT, BS 950D PLUS 8. CORROSION ON RT KEELBEAM BS 950D PLUS 8. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED IAW FED-EX 27-53-023A.Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, KeelSDR 04FDEA02454Stringer · dentedBS 848 STR 7R UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE AREA OF STRINGER 7 RT AT BS 848, FABRICATED, ALODINE, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & PER FED EX EA 7-5310-55358.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02453Stringer · dentedBS 848 STR 7L UPPER FLANGE OF STRINGER IS DENTED AND GOUGED. *S/D* REMOVED DAMAGE AREA OF STRINGER AT BS 848, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & FED EX EA 7-5310-55348.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02451Stringer · dentedSTRINGER DENTED AT BS 950C 18, STRINGER 7 LT. *S/D* REPAIRED STR 7L BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02450Stringer · dentedSTRINGER DENTED AT BS 950F 18, STRINGER 7 LT. REPAIRED STR 7L BS 950F PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL 1 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02449Stringer · dentedSTRINGER DENTED AT BS 1088, STRINGER 7 RT. REPAIRED STR 7R BS 1088 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02448Stringer · dentedSTRINGER DENTED AT BS 950F+18, STRINGER 7 RT ** SD COMING **.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02447Stringer · dentedSTRINGER DENTED AT BS 950C PLUS 18, STRINGER 7 RT. REPAIRED STR 7R. BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02446Stringer · dentedDENTED STRINGER 7R, BS 558. REPAIRED STR 7R BS 558 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02444Stringer · dentedDENTED STRINGER 7R BS678. REPAIRED STR. 7R AT BS 678 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02443Stringer · dentedDENTED STRINGER 7R BS 720C PLUS 18 INCHES. REPAIRED STR 7R, BS 720C PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL I & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02442Stringer · dentedDENTED STRINGER 7L BS 720E PLUS 18 INCHES. REPAIRED STR 7L, BS 720E PLUS 18 PER SRM 53-10-3 FIG 2. DETAIL I & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02445Stringer · dentedDENTED STRINGER 7R BS618. TRIMMED OUT DAMAGE IAW SRM 53-10-1Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02452Stringer · dentedSTRINGER DENTED AT BS 950 18, STRINGER 7 LT. *S/D* STR 7 LT ORIGINALLY FOUND OUT OF LIMITS (NO DENTS ALLOWED). REMOVED DENT BY BENDING EDGE OF STRINGER. MATERIAL LOSS A AS ALLOWABLE & STRINGER IS IN LIMITS PER SRM 53-10-1. ALODINED & PRIMED BLEND AREA PERAug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02455Floorbeam · corrodedCORROSION (C53-224-01, 1) FLOORBEAM STRUCTURE BS 344 LBL 31 TO LBL 58 WL 208. *S/D* REMOVED AND REPLACED UPPER FLOORBEAM CHORD AND REPAIR ANGLES AT BS 344, LBL 65-RBL 16, WL 208 IAW SRM 27-53-007.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA02417Skin · corrodedCORROSION BS 1090, STR 29 LT- 29 RT. CUTOUT SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02416Skin · corrodedCORROSION ON SKIN, AFT CARGO BAY BILGE NEXT TO O/B SIDE OF STR 28L BS 994 LBL 22 WL 136. REMOVED DAMAGED AREA OF SKINA T BS 994. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3.Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02415Floorbeam · corrodedCORROSION AT FLOORBEAM BS 950D, LBL 10 DAMAGED, WL 208 (C53-224-01, 3). BLENDED AREA AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE AND REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 3.Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01132Hydraulic Line · leakingPASSING 17,000 FEET IN A NORMAL CLIMB BOTH HYDRAULIC SYSTEM "A" PUMP LOW PRESSURE LIGHTS CAME ON, FOLLOWED BY A COMPLETE LOSS OF SYSTEM "A" QUANITY. PERFORMED STABILIZERS EXECUTED CHECKLIST IAW QRH. DECLARED IFE AND LANDED UNEVENTFULLY AT IAH. INSTALLED NEWJul 24, 2003 · N246FE · Boeing 727200 · Hydraulic System, MainSDR 02FDEA00423Warning System · malfunctionedFUEL HEAT ICING LIGHT ILLUMINATED ON ENG NR 3 APPROX 10-11000 MSL FOR ABOUT 1-2 MIN, THEN WENT OUT AND STAYED OUT. FUEL TEMP WAS +35DC. SUMPED ALL TANKS AND FOUND NO CONTAMINATION. FOUND FUEL FILTER PRESSURE SWITCH BACKSHELL EXTREMELY LOOSE AND WILL NEED TIJun 21, 2002 · N246FE · Boeing 727200 · Engine Fuel Indicating SystemSDR 98FDEA00771Actuator · malfunctionedWITH FLAPS RETRACT AS A/C ACCEL THRU 270 KIAS, AMBER LEAD EDGE LIGHT ILLUM ON 2ND OFFICER AUXILIARY PNL AND A/C ROLL CONTROL WAS AFFECTED. ANTI ICE WAS ON. BELOW 250 KIAS ALL IND WERE NORM, FLAP EXTENSION AND LAND, ALL APPROPRIATE CK LIST WERE COMPLETE. *S/Dec 31, 1998 · N246FE · Boeing 727277 · Leading Edge Slat Actuator
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