N245FE, cancelled Aug 27, 2013

Service difficulty reports · 83

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 = 'N245FE' AND deregistration_id = 'N245FE-2013-08-27'
  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 FDEA201107232914Thermal Switch · failedDURING CRUISE AT FL360 ENGINE 3 BLEED AIR TRIP OFF LIGHT ILLUMINATED AND THE NR 3 BLEED AIR VALVE CLOSED, SYS WOULD NOT RESET VIA QRH PROCEDURES ( LIGHT STAYED ON ). CABIN ALTITUDE WAS RAPIDLY INCREASING THROUGH 10000FT AND AFTER DONNING OXYGEN AND DESCENDIJul 23, 2011 · N245FE · Boeing 727277 · Engine Bleed Air SystemSDR FDEA201010224147Engine · failedWHILE ADVANCING POWER FOR TAKEOFF, AT 80 PERCENT N1 ON ENG NR 2. EPR SLOW TO INCREASE, COMPRESSOR STALL OCCURED. TOWER WITNESSED FLAMES FROM NR 2 ENGINE. R & R NR 2 ENGINE IAW WORK CARD 70T0002. INSTALLED ENGINE IAW WORK CARD 70T0002.Oct 22, 2010 · N245FE · Boeing 727277 · Compressor Bleed ControlSDR FDEA201009163509Beam · corrodedHORIZONTAL WALKWAY BEAM HAS CORROSION AT BS 312 STR 27L. R & R HORIZONTAL WALKWAY BEAM. REF SRM 51-30-2.Sep 16, 2010 · N245FE · Boeing 7272Q8 · Fuselage Main, StructureSDR FDEA200908072929Indicator · failedSTANDBY ADI PRECESSED 20 MIN. AFTER TAKE OFF, AT CRUISE. RECAGED BUT 2-3 MIN. LATER, PRECESSED AGAIN. 20-30 DEG RIGHT BANK, 10 DEG NOSE HIGH. REMOVED AND REPLACED STANDY BY ATTITUDE INDICATOR IAW MM 34-25-011-4. SYSTEM OPS CHECKED NORMAL. OK TO CONTAug 7, 2009 · N245FE · Boeing 727277 · Attitude Gyro and Indicating SystemSDR FDEA200906022004Shear Tie · corrodedSHEAR TIE CORRODED STA 950E BETWEEN STR 28L AND 29L. REMOVED SHEAR TIE REPAIR, FABRICATED NEW SHEAR TIE, FABRICATED NEW VERTICAL STIFFENER , HEAT TREATED PARTS TO T6 CONDITION AND INSTALLED IAW SRM 51-30- 2, 53-10-2, 51-10-1, AND 53-10-4.Jun 2, 2009 · N245FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR FDEA200905311899Skin · damagedRT WING INBD FOREFLAP, OUTBD END, PREVIOUS REPAIR IS GOUGED REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-2 FIG 4 AND 57-50-4 FIG. ALODINED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 57-50-11 FIG 1.May 31, 2009 · N245FE · Boeing 727277 · Wing, Plate/SkinSDR FDEA200905301857Fuel Tank · damagedDAMAGE AT STA 744 ON CTR TANK WEB RBL 60. REPAIRED CENTER TANK WEB IAW EA 7-5710-126825. REPAIR BY CUTTING OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW EA 7-5710-126825.May 30, 2009 · N245FE · Boeing 727277 · Fuel StorageSDR FDEA200905301858Stringer · corrodedAFT CARGO COMPARTMENT, CORROSION AROUND FASTENERS IN STRINGER 30 AT BS 990. REMOVED CORROSION AND FOUND OUT OF LIMITS, FABRICATED NEW STRINGER SECTION, FABRICATED NEW SPLICE AND INSTALLED PARTS IAW SRM 51-10-6, 53-10-1, 51-30-2, 53-10-3, AND 51-30-5.May 30, 2009 · N245FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905291863Rib · crackedNR 5 SLAT HAS CRACKED RIB ON INBOARD SIDE OF ACTUATOR FORWARD MOUNT. REMOVED AND REPLACED RIBS WITH NEW RIBS IAW SRM 51-30-2.May 29, 2009 · N245FE · Boeing 727277 · Leading Edge DevicesSDR FDEA200905291846Stringer · corrodedSTRINGER 27L CORRODED STA'S 950F TO 1030 REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED DAMAGED STRINGER AND FABRICATED NEW STRINGER SECTIONS. FABRICATED REPAIR SPLICES AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53-10-2 AND 51-30-2.May 29, 2009 · N245FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905271940Frame · damagedSTATION 520 FRAME DAMAGED AT STRINGER 21L TO 26L. REMOVED DAMAGED FRAME, FABRICATED NEW FRAME, HEAT TREATED TO T6 CONDITION, AND INSTALLED PARTS IAW SRM 51-30-2, 53-10-2.May 27, 2009 · N245FE · Boeing 727277 · Fuselage Main, FrameSDR FDEA200905271898Skin · crackedRMLG WING DOOR SKIN CRACKED FWD OF AFT HINGE POINT REMOVED FILLER AND DOUBLER IAW SB 727-32-318 HFEC SHOWS AREA OF CUT OUT FREE OF CRACKS IAW NDTM 51-00-00 FIG 23 FABRICATED FILLER AND DOUBLER, ALODINED AND PRIMED PARTS IAW SRM 51-10-2 OPENED INNER SKIN May 27, 2009 · N245FE · Boeing 727277 · Landing Gear DoorsSDR FDEA200905271865Seat Track · corrodedSEAT TRACK CORRODED STA 690-720 LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW ONE, REPAIR SPLICES, STRAP, AND INSTALLED REPAIR PARTS IAW 53-10-5 AND 53-10-2.May 27, 2009 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905271815Shear Tie · corrodedFWD PIT BS 720C BETWEEN ST 25RT TO 26RT SHEAR TIE CORRODED.May 27, 2009 · N245FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR FDEA200905271814Shear Tie · corrodedFWD PIT BS 720C BETWEEN STR 25L TO 26L SHEAR TIE CORRODEDMay 27, 2009 · N245FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR FDEA200905261900Skin · crackedLEFT MLG WING DOOR CRACKED FWD OF AFT HINGE POINT REMOVED FILLER AND DOUBLER IAW SB B727-32-318 AND SRM 51-30-2 HFEC SHOWS AREA FREE OF CRACKS IAW NDTM 51-00-00 FIG 23 FABRICATED NEW FILLER AND DOUBLER IAW SB 727-32-318 ALODINED AND PRIMED PARTS IAW SRM 51-May 26, 2009 · N245FE · Boeing 727277 · Landing Gear DoorsSDR FDEA200905231868Stringer Splice · corrodedCORROSION ON STRINGER SPLICE AT STRINGER 30, BS 950. REMOVED DAMAGED ANGLE, LOCATED, DRILLED AND INSTALLED NEW ANGLE PN 69-44177-1 IAW SRM 51-30-2, AND 51-30-5.May 23, 2009 · N245FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905231867Fitting · corrodedCORROSION ON STRINGER 29L KEELBEAM EXTENSION FITTING AT BS 950. FOUND OUT OF LIMITS, REMOVED FITTING AND LOCATED, DRILLED AND INSTALLED NEW FITTING PART NR 69-51272-1 IAW SRM 51-30-2 AND 53-10-1.May 23, 2009 · N245FE · Boeing 727277 · Fuselage Main, Attach FittingsSDR FDEA200905191757Skin · crackedL-1 DOOR LOWER HINGE SKIN DOUBLER IS CRACKED. REPAIRED L-1 DOOR LOWER HINGE SKIN IAW EO 7-5330-7-2345 PART 2.May 19, 2009 · N245FE · Boeing 727277 · Passenger/Crew DoorsSDR FDEA200905191741Frame · crackedFORWARD CARGO DOOR, STA 540, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME, FABRICATED NEW ONE AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.May 19, 2009 · N245FE · Boeing 727277 · Cargo/Baggage DoorsSDR FDEA200905191740Frame · crackedFORWARD CARGO DOOR, STA 520, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME AND INSTALLED NEW FABRICATED ONE IAW SRM 51-30-2, 51-20-1 AND DWG 53FX1350.May 19, 2009 · N245FE · Boeing 727277 · Cargo/Baggage DoorsSDR FDEA200905191739Frame · crackedFORWARD CARGO DOOR, STA 500, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.May 19, 2009 · N245FE · Boeing 727277 · Cargo/Baggage DoorsSDR FDEA200905191738Frame · crackedFORWARD CARGO DOOR, STA 560, STRINGER 21-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME EXTENSION, FABRICATED NEW STUB FRAME, HEAT TREATED TO T-6 AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.May 19, 2009 · N245FE · Boeing 727277 · Fuselage Main, StructureSDR FDEA200905181842Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE BS 1110-1116 LBL47. CORROSION ON SEAT TRACK OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51-30-2, 53-10-5 AND 51-10-2.May 18, 2009 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905181714Fitting · corrodedCORROSION ON STRINGER 29 R KEEL BEAM EXTENSION FITTING AT BS 950. FOUND CORROSION ON FITTING OUT OF LIMITS, REMOVED FITTING AND LOCATED, DRILLED AND INSTALLED NEW FITTING PN 69-51272-2 IAW SRM 51-30-2 AND 53-10-1.May 18, 2009 · N245FE · Boeing 727277 · Fuselage Main, Attach FittingsSDR FDEA200905171699Skin · crackedRT WING INBD MID FLAP AFT LOWER ANGLE HAS 2 CRACKS, WBL 90. REMOVED R / WING I/B MID FLAP LOWER INNER SKIN PANEL IAW SRM 51-30-2. CUT OUT DAMAGE AREA ANGLE SECTION SRM 51-10-1 AND 51-40-4. FABRICATED REPAIR ANGLE AND SPLICE IAW SRM 57-50-2. TREAT AND PRIMEDMay 17, 2009 · N245FE · Boeing 727277 · Trailing Edge FlapsSDR FDEA200905171702Angle · crackedNR 3 SLAT AFT LOWER ANGLE IS CRACKED AT ACTUATOR ATTACHMENT. UPON FURTHER INVESTIGATION SLAT REPAIR NOT FEASIBLE, SLAT REMOVED AND REPLACED.May 17, 2009 · N245FE · Boeing 727277 · Wing, Control Surface Attach FittingsSDR FDEA200905171701Spar · crackedLT WING FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. CUTOUT SECTION, FABRICATED NEW SECTION, FABRICATED WEB, FABRICATED 2 ANGLES, HEAT TREAT ANGLES IAW FASI ER 2-32153-801 REV. A, FABRICATED STRAP, 2 RADIUS FILLERS, LOCATED AND DRILLED NEW PARTS, ALODINED ANMay 17, 2009 · N245FE · Boeing 727277 · Wing SparSDR FDEA200905171700Keelbeam · crackedLT W/W, LT KEEL BEAM IS CRACKED AT 2ND FASTENER STA 875, LBL 6. TRIMMED OUT CRACK DIMS 2 INCH X 1 INCH, FABRICATED DOUBLER, HEAT TREATED AND CADMIUM PLATED DOUBLER AND INSTALLED IAW EA 7-5310-127963.May 17, 2009 · N245FE · Boeing 727277 · Fuselage Main, KeelSDR FDEA200905161693Angle · crackedNR 6 SLAT AFT LOWER CHORD ANGLE IS CRACKED AT INBD UPSTOP PAD REMOVED NR 6 SLAT COVE ACCESS PANELS IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED NEW ANGLE AND SPLICE IAW SRM 51-40-4 AND 57-50-2 FIG. 2. ALODINED AND PRIMED REPAIR PARTS IAWMay 16, 2009 · N245FE · Boeing 727277 · Wing, Plate/SkinSDR FDEA200905141864Seat Track · corrodedSEAT TRACK CORRODED STA 560-620 LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW TRACK, REPAIR SPLICES, STRAP, AND INSTALLED REPAIR PARTS IAW 53-10-5 AND 53-10-2.May 14, 2009 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905131753Angle · crackedRIGHT WHEEL WELL ANGLE CRACKED 870 BULKHEAD AND KEELBEAM. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-30-5 AND 51-30-2.May 13, 2009 · N245FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR FDEA200905131655Skin · misrepairedPREVIOUS REPAIR AT STATIONS 970 TO 1010 STR 29L HAS FASTENERS WITH ZERO EDGE DISTANCE AT THE FORWARD END OF THE REPAIR. REPLACED PREVIOUS REPAIR AT STA 970-1010, S29R IAW EA NR 7-5330-127970.May 13, 2009 · N245FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR FDEA200905131650Spar · corrodedLEFT LOWER FORWARD CENTER TANK SPAR CORRODED AT STA 744 LBL 20 TO LBL 30. REMOVED CORRODED SPAR, LOCATED AND DRILLED NEW SPAR AND INSTALLED IAW EA 7-5710-127966 AND SRM 51-30-5 AND SRM 51-30-2.May 13, 2009 · N245FE · Boeing 727277 · Wing, Center BoxSDR FDEA200905121629Vertical Beam · damagedVERTICAL BEAM HAS FASTENERS WITH 0 SPACING BS 1183 LBL 17.8. REPAIRED BS 1183 BULKHEAD VERTICAL BEAM AT LBL 17.8 IAW EA NR 7-5310-127962. "BS 1183 BULKHEAD WITH INSUFFICIENT FASTENER SPACING AT LBL 20 BELOW WL190".May 12, 2009 · N245FE · Boeing 727200 · Fuselage Main, BulkheadSDR FDEA200905121929Skin · crackedNR 3 ENGINE NOSE COWL EXTERIOR SKIN CRACKED AND CHAFED AT T/E, APPX 4 O'CLOCK. CUT-OUT DAMAGE AREA IAW SRM 51-10-1 AND FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 54-30-3 FIG 3A. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 5May 12, 2009 · N245FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR FDEA200905121928Skin · crackedNR 1 ENGINE NOSE COWL AFT EXTERIOR SKIN OTBD SIDE AT 9 O'CLOCK POSITION. AFT T/E SKIN EDGE IS BENT OUT AND CRACKED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR AND FILLER AND INSTALLED REPAIR IAW SRM 54-30-3, 51-30-2, 51-10-1 AND 51-10-2.May 12, 2009 · N245FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR FDEA200905121630Skin · misrepairedFASTENER WITH ZERO EDGE DISTANCE IN MAIN CARGO DOOR DOUBLER STA 460 STR 27L. REMOVED EXISTING FASTENER, TRIMMED OUT AREA WITH A 2" RADIUS, TREATED AND PRIMED, INSTALLED FASTENER AND SEALED EDGE OF DOUBLER IAW EA 7-5330-126822. REPAIR DETERMINED TO BE MINOMay 12, 2009 · N245FE · Boeing 727277 · Cargo/Baggage DoorsSDR FDEA200812245289Wire Harness · burnedDURING CLIMB THROUGH 6,000 FT EXPERIENCED A PWR SURGE AND FOUND THE ALTERNATE FLAP MOTOR CIRCUIT BREAKERS (INBD AND OTBD) HAD POPPED. FOUND BURNED WIRE BUNDLE IN E&E COMPARTMENT, STILL TROUBLESHOOTING.Dec 24, 2008 · N245FE · Boeing 727277 · Flight Control System WiringSDR 08FDEA01838Indicator · failedCAPT'S AIRSPEED INDICATOR NOT WORKING. NO AIRSPEED INDICATION- AIARSPEED FLAG IN VIEW. REMOVED AND REPLACED CAPT'S AIRSPEED IND PER MM 34-12-021-4. AC OK TO CONTINUE.May 13, 2008 · N245FE · Boeing 727200 · Airspeed/Mach IndicatorSDR 06FDEA04253Floorbeam · corrodedMCD STA 950 FLOORBEAM BETWEEN RBL0 -24 THE 4 NUT PLATES HAVE CORROSION BETWEEN THEM AND THE FLOORBEAM. CORROSION FOUND OUT OF LIMITS. REMOVED DAMAGED AREAS AND REPAIRED IAW SRZ27-53-033.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04252Stringer · corrodedFOUND STRINGER CORRODED EXT FUSELAGE STA 1071-1080 RBL10 STR 29 R 8 RIVETS DISHED IN EXT SKIN. PERFORMED STR REPAIR IAW SRM 53-10-3 FIG 1.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 06FDEA04251Skin · corrodedFOUND SKIN CORRODED EXT FUSELAGE STA 1067 TO 1070 RBL 12, SKIN BULGE AT 3 FASTENERS STR 27R. REPAIRED FUSELAGE SKIN IAW SRM 53-30-3 FIG 3 STA 1067 - 1070 STR 29R.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04250Floorbeam · corrodedFOUND CORROSION BETWEEN RBL 9 AND RBL 2 STA 540 FLOORBEAM, UNDERSIDE FWD PIT. REMOVED CORROSION, INSTALLED NEW FLOORBEAM AND SPLICES IAW SRM 51-40-4.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04249Floorbeam · corrodedSTA 540 LBL 9 FLOOR SUPPORT CORRODED FWD PIT REMOVED CORROSION FOUND OUT OF LIMITS. INSTALLED FLOOR SUPPORT AND REPAIR SPLICES IAW SRM 51-30-2 AND 53-10-5 FIG 4.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04233Skin · corrodedEXTERNAL FUSELAGE STA 1067 TO 1070 RBL 12 SKIN BULGE AT (3) FASTENERS. REPAIRED FUSELAGE SKIN IAW SRM 53 -30-3 FIG3 STA 1067 - 1070 STR 29R.Dec 13, 2006 · N245FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04232Fitting · damagedFUSELAGE MAIN FRAME TAIL JACK FITTING DRILL START REPAIR, P/N 25FX990-45 COMPLY WITH EA 7-5310-101994. COMPLIED WITH EA 7-5310-101994 FUSELAGE MAINFRAME TALL JACK FITTING DRILL START REPAIR.Dec 13, 2006 · N245FE · Boeing 727277 · Fuselage Main, Attach FittingsSDR 06FDEA04182Seat Track · corrodedMCD SEAT TRACK AT LBL 25, STA 948 - 958 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW 51-30-5. SEAT TRACK FABBED ON TRAVELER, T6/647796.Dec 7, 2006 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04181Seat Track · corrodedMCD - SEAT TRACK SPLICE AT LBL 25, STA 950-950 PLUS 20" HAS CORRODED FASTENERS, EXFOLIATION BETWEEN PARTS REMOVED SPLICE ANGLES. REMOVED CORROSION, SPLICE ANGLES OUT OF LIMITS. FABBED NEW ANGLES BATCH NR 9R000776001. TREATED AND PRIMED NEW ANGLES, INSTALLEDDec 7, 2006 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04175Seat Track · corrodedMCD, BL 0 SEAT TRACK BETWEEN STA 870 - 880 HAS CORRODED NUT PLATE HOLES, TOP AND BOTTOM SIDES OF TRACK. BLENDED SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1,FIG 3. REMOVED SEAT TRACK IAW SRM 51-10-5, FABRICATED NEW SEAT TRACK ON TRAVELER T6/647662, Dec 5, 2006 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach Fittings
Back to N245FE, cancelled Aug 27, 2013