N462FE, cancelled Dec 19, 2013

Service difficulty reports · 79

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 = 'N462FE' AND deregistration_id = 'N462FE-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 FDEA201109033647Cabin Pressure · failedTHE CABIN DEPRESSURIZED RAPIDLY ACCOMPANIED BY A "LEFT SERVICE DOOR LIGHT" ON THE DOORS PANEL. TURNED OFF PACKS AND CONTINUED UNPRESSURIZED. LT SERVICE DOOR LT WENT OUT ON TAXI INTO GATE. LIGHT REMAINED OUT. REMOVED INNER DOOR LINER REF 52-14-011. OPENED LSep 3, 2011 · N462FE · Boeing 727225 · Cabin Pressure Control SystemSDR FDEA201012294773Battery Pack · inoperative"EMERGENCY EXIT LIGHTS BATTERIES ARE DEAD. LIGHTS WON'T TEST." REPLACED BATTERIES IN BOTH PORTABLE EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0. (CLOSED)Dec 29, 2010 · N462FE · Boeing 727225 · Emergency LightingSDR FDEA200907272792Actuator · failedFLIGHT TEST-THE NR 2 LED FAILED TO RETRACT AFTER TAKEOFF. NR 2 SLAT ASSY FOUND TO BE RETRACTED WITH ACFT INBOUND AND NR 2 SLAT INTRANSIT AMBER LIGHT ILLUM IN COCKPIT ON FWD PNL AND S/O IND PNL. T/S NR 2 SLAT INDICATION IAW MM 27-82-000-1 AND FOUND TO BE FAJul 27, 2009 · N462FE · Boeing 727225 · Leading Edge Slat ActuatorSDR FDEA200907182664Skin · gougedPREVIOUS REPAIR AT BS 620 BETWEEN STR 5L AND STR 8L GOUGED. CUT-OUT DAMAGED AREA. FABRICATED FILLER REPAIR, AND DOUBLER IAW SRM 53-10-2 FIG 3A AND 51-40-2 FIG 1, TREATED AND PRIMED PARTS & AREA IAW SRM 51-10-2, INSTALLED DOUBLER, FILLER REPAIR IAW SRM 51-40Jul 18, 2009 · N462FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200907182663Skin · damagedPREVIOUS REPAIR AT BS 620 BETWEEN STR 11L AND STR 12L IS GOUGED TRIMMED AREA, FABRICATED FILLER AND DOUBLER REPAIR IAW SRM 53-10-2 FIG 3A AND 51-40-2 FIG 1. TREATED AND PRIMED DOUBLER, FILLER AND AREA IAW SRM 51-10-2, INSTALLED DOUBLER & FILLER REPAIR IAW SJul 18, 2009 · N462FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200907162647Rib · crackedNR 6 SLAT RIB IS CRACKED, OTBD SIDE OF ACTUATOR FWD ATTACHMENT. REMOVED CRACKED RIB AT NR 6 SLAT OUTBD SIDE OF ACTUATOR IAW SRM 51-30-2 FABRICATED NEW SLAT RIB, HEAT TREATED RIB TO T6 IAW FAS ENGINEERING REPORT 2-37153-801 REV A VERIFIED HARDNESS IAW NDTMJul 16, 2009 · N462FE · Boeing 727225 · Leading Edge DevicesSDR FDEA200907132608Support Angle · crackedAFT AIRSTAIR AREA, RT LWR TORQUE BOX UPPER SUPPORT ANGLE IS CRACKED AT BS 1263. FABRICATED NEW SUPPORT ANGLE IAW SRM 53-10-2, 51-30-5 AND 51-30-6 INSTALLED NEW SUPPORT ANGLE LOWER TORQUE BOX IAW SRM 51-30-2.Jul 13, 2009 · N462FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200907112587Doubler · crackedAFT AIRSTAIR AREA, LT LWR TORQUE BOX LIGHTNING HOLE HAS CRACK BS 1243 ROUTED OUT CRACKED AREA AT AFT AIRSTAIR AREA LT LWR TORQUE BOX LIGHTNING HOLE BS 1243 IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1 AND 51-30-5. TREATEJul 11, 2009 · N462FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200907022678Frame · crackedFORWARD CARGO, STA 560, STR 21L - 22L, STUB FRAME EXTENSION CRACKED IN RADIUS. REMOVED CRACKED STUB FRAME EXTENSION AT FWD CARGO STA 560 S21-22L IAW SRM 51-30-2. HEAT TREATED STUB FRAME IAW FAS ENG REPORT 2-37153-801 REV A CW CONDUCTIVITY MEASUREMENT IAW NDTMJul 2, 2009 · N462FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA200906272335Spar · damagedRT WING T/E FALSE SPAR INBD REPAIR HAS LOOSE FASTENER IN THE UPPER SECTION WBL 118. FABRICATED REPAIR PARTS , NEW LOWER CHORD, ANGLE REPAIR , HEAT TREATED 7075 'O' TO T6 CONDITION IAW FAS ER 2-37153-801 REV A, NEW STRAP, TWO RADIUS FILLERS & NEW DOUBLER Jun 27, 2009 · N462FE · Boeing 727225 · Wing SparSDR FDEA200906262320Spar · crackedCRACK ANGLE LT WING FALSE SPAR AT NR 7 SPOILER ATTACH FITTING. CUT ANGLE AT LT WING FALSE SPAR IAW FX DWG SR 27-57-038 REV C. FABRICATED 2 ANGLES. HEAT TREATED ANGLES FROM 'O' TO T6 IAW FAS ENG REPORT NR 2-37153-801 REV A, FABRICATED DOUBLER, WEB, LOWER ANGJun 26, 2009 · N462FE · Boeing 7272S2F · Wing SparSDR 08FDEA01799Transceiver · failed(AIR-TURN-BACK), WX RADAR PAINTS INTERMITTENT FALSE RETURNS ONE SIDE THEN THE OTHER, STABILIZED OR UNSTABILIZED. WHEN UNSTABILIZED, RADAR PAINTS A SINGLE SPOKE AT THE 11 -12 O'CLOCK POSITION. GOING BACK TO STABILIZED, IT PAINTS A DOUBLE SPOKE. VERIFIED OLD May 8, 2008 · N462FE · Boeing 727225 · Weather Radar SystemSDR 07FDEA04524Carriage · damagedSPLIT FLAPS OUTBOARD ON DEPARTURE. COMPLIED WITH QRH FLAPS WOULD NOT RETRACT VIA ALTERNATE METHOD. CREW DEBRIEFED OUTBD FLAPS STAYED AT 5 DEG WHILE INBD FLAPS CAME TO 2 DEG AS COMMAMDED. L/E VALVE C/B ON P6 PANEL PULLED BY CREW AS PART OF QRH. REF WRI 27-Oct 6, 2007 · N462FE · Boeing 727225 · Trailing Edge FlapsSDR 07FDEA01986Rod · unknownAFTER TAKE OFF FROM MEM, GEAR WAS RET AND THE FWD RED GEAR DOORS LT REMAINED ILLUM WITH ASSOC NOSE GEAR DOOR LT ILLUM ON S/O'S PANEL. C/W QRH, RECYCLED GEAR AND IND REMAINED. CONT'D FLT WITH APPROPRIATE RESTRICTIONS. UPON LDG IN ICT WITH NORM TOUCHDOWN, THEMay 26, 2007 · N462FE · Boeing 727225 · Nose/Tail Landing GearSDR 07FDEA01178Fitting · corrodedLOWER AFT SUPPORT TEE HAS CORROSION ON UPPER SURFACE AT FWD END OF LOWER BODY PANEL NR 3218 (INST AFT OF BEACON LIGHT). REMOVED STROBE LIGHT ASSY MOUNT IAW SRM 53-10-01. CHECK ALLOWABLE DAMAGE LIMITS IAW FOUND TO BE OUT OF LIMITS. FABRICATED T-CHORD AND SMar 29, 2007 · N462FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR 07FDEA01149Skin · crackedMCD DOOR EXTERNAL SKIN AT AFT LOWER EDGE HAS DISTORTED AND CRACKED SKIN. BLENDED AREA IAW SRM 51-10-1 AND 52-00-2, ORIG MAT'L .063IN AFTER REWORK .061IN. WITHIN LIMITS IAW SRM 52-00-2, FIG NR 1. REMOVED DAMAGED ON SKIN EDGE AMOUNT OF MAT'L. REMOVED WAS 0.Mar 27, 2007 · N462FE · Boeing 727225 · Cargo/Baggage DoorsSDR 07FDEA01148Shroud · crackedLT AFT SERVICE DOOR FWD UPPER END SHROUD HAS CRACKS 2 PLACES APPROX 8 IN AND 6 IN FROM FWD UPPER CORNER. CONTAINED CRACK IN SHROUD BY STOP DRILLING IAW SRM 51-10-1 PARA 10. TREATED AND PRIMED AREA IAW SRM 51-10-1. RESEALED AREA IAW DWG 65-56992 AND MM 51-3Mar 27, 2007 · N462FE · Boeing 727225 · Passenger/Crew DoorsSDR 07FDEA01038Floor Support · corrodedCABIN FLOOR SUPPORT (BEAM ) HAS CORROSION FS 620, LBL 35. FABRICATED REPAIR ANGLES PER DWG SR27-53-033 AND MAE TRAVELER T7/669736 CUT OUT DAMAGED AREA IAW DWG SR27-53-033. TREATED AND PRIMED CUT OUT DAMAGE IAW SRM 51-10- 2. FABRICATED FILLER FROM 7075-T6 .Mar 21, 2007 · N462FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 07FDEA00912Bracket · crackedNLG W/W CEILING THRU LT ACCESS PNL LT SUPPORT HAS CRACKS ON BOTH ENDS FS 259.50. REMOVED SEAT TRACK FOR ACCESS IAW SRM 51-30-2. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-30-2. REINSTALLED SEAT TRACK IAW SRM 51-30-2.Mar 15, 2007 · N462FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA00833Bulkhead · corrodedFOUND FWD CARGO STA 720D LWR BULKHEAD BEAM HAS CORROSION AT LBL25. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2.Mar 14, 2007 · N462FE · Boeing 727225 · Fuselage Main, BulkheadSDR 07FDEA00832Skin · crackedCABIN FWD RT GALLEY DOOR EXT UPPER HINGE CUT OUT DOOR SKIN HAS A CRACK. STOPPED DRILLED CRACK IAW SRM IAW SRM 52-00-3 FIG 3. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .080C. INSTALLED REPAIR IAW SRM 52-00-3 FIG 3. REPAIR CLASSIFIED AS A MAJOR REPAIR.Mar 14, 2007 · N462FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA00831Support Bracket · crackedNR 2 FLAP TRACK AFT SUPPORT BRACKET IS CRACKED OTBD AFT END. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.Mar 14, 2007 · N462FE · Boeing 727225 · Trailing Edge FlapsSDR 07FDEA00777Skin · unknownTHE MAIN CARGO DOOR HAS 4 EXTERNAL DOUBLERS ON ITS INTERNAL SKIN ALONG THE TOP EDGE AT STATIONS 520, 540, 560, AND 580. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.Mar 12, 2007 · N462FE · Boeing 727225 · Standard Practices/StructuresSDR 07FDEA00776Frame · unknownFOUND AFT PIT FRAME REPAIR, STA 970, ABOVE S23L TO S24L. COMPLY WITH ATTACHMENT "B" OF EO 7- 5100-7-5005 PT2. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.Mar 12, 2007 · N462FE · Boeing 727225 · Standard Practices/StructuresSDR 07FDEA00775Frame · unknownFOUND AFT PIT FRAME REPAIR STA 950, ABOVE S24L TO S25L. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.Mar 12, 2007 · N462FE · Boeing 727225 · Standard Practices/StructuresSDR 07FDEA00774Stringer · unknownAFT PIT, FUSE STRINGER REPAIR STA 1130- 1166,S29. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.Mar 12, 2007 · N462FE · Boeing 727225 · Standard Practices/StructuresSDR 07FDEA00773Stringer · unknownAFT PIT, FUSE STRINGER REPAIR, STA 1070- 1090,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.Mar 12, 2007 · N462FE · Boeing 727225 · Standard Practices/StructuresSDR 07FDEA00772Stringer · unknownAFT PIT FUSE STRINGER REPAIR, STA 1050- 1070,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.Mar 12, 2007 · N462FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 07FDEA00771Torque Box · unknownEXTERNAL DOUBLER SECTION 48, RT LOWER TORQUE BOX, ATA 1227.5,RBL 20, WL 190. COMPLY WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.Mar 12, 2007 · N462FE · Boeing 727225 · Fuselage Main, StructureSDR 07FDEA00766Torque Box · unknownFOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1237, RBL 20, WL 189. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.Mar 12, 2007 · N462FE · Boeing 727225 · Standard Practices/StructuresSDR 07FDEA00760Torque Box · unknownFOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1238, RBL20, WL 183. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2.Mar 12, 2007 · N462FE · Boeing 727225 · Standard Practices/StructuresSDR 07FDEA00687Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION SPOTS FS 620-720F LBL 45, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.Mar 7, 2007 · N462FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00686Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION SPOTS FS 620 - 700 RBL 24. REMOVED AND REPLACED SEAT TRACK FS 620 - 700 RBL 24 IAW SRM 51-30-2.Mar 7, 2007 · N462FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00685Seat Track · corrodedFOUND MAIN DECK SEAT TRACK STA 740-850 RBL-45 HAS AREA OF BARE METAL AND CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.Mar 7, 2007 · N462FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00684Floor Skin · corrodedE/E COMPT RT O/B FLOOR PNL WEB HAS CORROSION FS - 435, REMOVED AND REPLACED DAMAGED WEB AT STA 435 IAW SRM 51-30-2. NEW WEB MADE ON TRAVELER T7/665341.Mar 7, 2007 · N462FE · Boeing 727225 · Fuselage Floor PanelSDR 06FDEA1966Apu · fireDURING MTC WALKAROUND, FOUND FLAMES COMING FROM FLOW MULT FRESH AIR INLET. IMMEDIATELY SHUTDOWN APU, AND EXTINGUISHED FIRE, FIRED APU FIRED PERFORMED APU START USING ALT FIRE PROT, WITH NO DEFECTS. TURNED ON ENG NR 2 BLEED AIR AND WITHIN 30 SEC. BLEED AIR TMay 18, 2006 · N462FE · Boeing 727225 · Airborne Auxiliary Power Unit (APU) SystemSDR 05FDEA03185Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE BETWEEN STA 560 AND 600 AT LBL 24. REMOVED AND REPLACED SEAT TRACK FROM STA 480 TO 630 AT LBL, 24 IAW FX B727 SRM 53-10-5 FIG 1, 51-10-2 AND 51-30-2.Oct 1, 2005 · N462FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03183Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER SURFACE STA 560 LBL 24-62. REMOVED, FABRICATED, AND REPLACED T-CAP, WEB AND STIFFENER IAW B727 SRM 53-10-8 FIG 3, 51-10-2 AND 51-30-2.Oct 1, 2005 · N462FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 05FDEA03182Floorbeam · corrodedUPPER CHORD FLOORBEAM AT FS 344 LBL 22.5 TO RBL 22.5 CORRODED. REMOVED, FABRICATED AND INSTALLED CHORD AND HAT-CHANNEL IAW FED-EX DRAWING SR-27-53-007 AND B727 SRM 51-30-2.Oct 1, 2005 · N462FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 04FDEA02799Skin · corrodedCORROSION EXT SKIN, BS 470 WL 148 CORROSION WHERE MOD S ANT MOUNTS. *S/D* REPAIRED PER SRM 53-30-1 AND 53-30-3.Sep 22, 2004 · N462FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02770Angle · crackedRT MLG WHEEL WELL VERTICAL L-ANGLE CRACKED BS 870 RBL 6 FWD OF APU LWR CORNER . REMOVED AND REPLACED RT WHEEL WELL VERTICAL L-ANGLE BS 870 RBL 6 IAW SRM 51-30-5, 51-30-2, AND 51-10-2.Sep 20, 2004 · N462FE · Boeing 727225 · Fuselage, Landing Gear Attach FittingsSDR 04FDEA02723Door · corrodedCORROSION LT FWD OVERWING ESCAPE HATCH, ALONG LWR EDGE UNDER PRESSURE SEAL. BLENDED CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1 & REPAIRED PER SRM 51-30-5 & 51-30-2.Sep 17, 2004 · N462FE · Boeing 727200 · Emergency ExitsSDR 04FDEA02721Frame · corrodedWHILE REMOVING CORROSION ON SHEAR TIE AT BS 1148 BETWEEN STRINGERS 28L AND 28R CORROSION WAS FOUND TO BE .100 PERCENT THROUGH THE FRAME. ALL WORK DONE PER E.A. 7-5310-55378Sep 17, 2004 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02719Stringer · corrodedCORROSION ON STR 28R, AROUND FASTENER HOLES ATTACHING KEELBEAM, STA 722, FWD CARGO BAY. CORROSION ON STR NR 28 RT AROUND FASTENERS HOLES ATTACHING KEELBEAM STA 727 FWD CARGO BAY. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE AREA PER SRM 53-10-3 &Sep 17, 2004 · N462FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 02FDEA00587Brake Assy · fireFIRE IN RIGHT MAIN LANDING GEAR BRAKE AFTER SHUTDOWN CLEARED TO LAND ON 19R AT ICT. WINDS 020/8. TOOK LONGER THEN NORMAL TO SLOW DOWN TO TAXI SPEED. EVERYTHING ELSE WAS OTHERWISE NORMAL. FIRE STARTED AFTER BLOCK IN. FIRE WAS AT NR 3 BRAKE ASSEMBLY. INSPEAug 11, 2002 · N462FE · Boeing 727200 · BrakeSDR 02FDEA00381Floorbeam · corrodedCORROSION ON FLOORBEAM BS 900, LBL 43. REMOVED AND REPLACED FLOORBEAM PER EA 7- 5310-64924.Jun 1, 2002 · N462FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00379Frame · damagedMECHANICAL DAMAGE TO FRAME AT BS 720, STR 4L AND CEILING SUPPORT. REMOVED AND REPLACED FRAME PER SRM 53-10-4.May 31, 2002 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00367Web · corrodedSHEAR WEB BULGING AROUND FASTENERS BS 1147, LBL 53-61, WL 208. REMOVED AND REPLACED WEB & FLOORBEAM PER SRM 51-40-2 FIG 1 & 53-10-8 FIG 3.May 29, 2002 · N462FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 02FDEA00362Frame · crackedWHILE WORKING FOUND FRAME CRACKED AT BS 720, LBL 2, WL 154. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-64910.May 24, 2002 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00356Frame · dentedFRAME 600 DENTED AT OPEN HOLES 5R. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1.May 21, 2002 · N462FE · Boeing 727200 · Fuselage Main, Frame
Back to N462FE, cancelled Dec 19, 2013