N297FE

Service difficulty reports · 47

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 = 'N297FE' AND registry_match = 'registration'
  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 FDEA202607160937Transmitter · failedON APPROACH INTO LAS, SELECTED FLAPS 25 & CAPTAIN NOTICED FLAPS BECAME ASYMMETRICAL LEAVING 20. NEVER RECEIVED ANY INDICATION ON ICAS. VERIFIED DETENT OF 25. ELECTED TO GO BACK TO 20. TRIED TO CYCLE FROM 20-25 AGAIN, STILL SHOWED A FLAP ASSYM, DECLARED AN Jul 16, 2026 · N297FE · Boeing 76732LF · Trailing Flap Position Indicating SystemSDR FDEA202602090148Skin · wornRH WING, T/E MAIN FLAP, OTBD EDGE UPPER SURFACE HAS AREA THAT IS WORN INTO COMPOSITE. REPAIRED RT WING INBD MAIN FLAP OTBD EDGE UPPER SURFACE 23 INCHES FROM T/E IAW DRAWING 113T2204 AND SRM 51-70-05-0G. MAJOR REPAIR.Feb 9, 2026 · N297FE · Boeing 76732LF · Trailing Edge FlapsSDR FDEA202602080146Floorboard · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252HFF DENTED. FABRCATED FLOORPANEL (252HFF) IAW DRAWING SR67-53-009 AND DRAWING 146T5869-10, RBL 77.50-12.85 BS 1197-1285 AND SR67-53-009.SEE JPF FOR ALL THE WORK PERFORMED. (THIS IS MAJOR REPAIR) INSTALLATION OF THISFeb 8, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202602070145Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 252GFF IS DENTED IN TWO LOCATIONS. FABRICATED NEW FLOOR PANEL 252GFF, RBL 54.75- RBL 77.5, STA 1197 22-1197 132 IAW DWG 146T5868-49, & SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. REMOVAL /Feb 7, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202602060139Floor Panel · delaminatedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222AFF HAS AREA OF DELAMINATION FABRICATED NEW FLOOR PANEL 222AFF, MPN 141T5856-107, RBL11 - RBL 33, STATION 285 - 412 IN REF TO BOEING DWG 141T5856-107 AND SR67-53-009. SEE JPF FOR ALL WORK PERFORMED. THIS IS A MAJFeb 6, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202602050134Floorboard · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF DENTED. FABRICATED NEW FLOOR PANEL MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF DENTED 222BFF, MPN 141T5856- 106,RBL33 - RBL 54.75, STATION 285 - 412 IN REF TO BOEING DWG 141T5856-106 AND SR67-53- 009.SEFeb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202602050133Floor Panel · dentedMIAN DECK CARGO COMPARTMENT, FLOOR PANEL 251LFF DENTED. JM40 FABRICATED NEW FLOOR PANEL 251LFF, MPN: 146T5869-127, LBL 11- RBL 11, STA 1208-1351 IN REF. TO BOEING DWG 146T5869-127, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR.Feb 5, 2026 · N297FE · Boeing 7673S2F · Fuselage Structure (General)SDR FDEA202602050131Floorboard · delaminatedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232MFF HAS AREA OF DELAMINATION. FABRICATED NEW FLOOR PANEL 232MFF, MPN: 148T5875-19 RBL 54.75- RB L 77.5, STA 654-784.5 IN REF. TO BOEING DWG 148T5875-19, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS Feb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202602050130Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF HAS PUNCTURE DAMAGE. JM39. (INCORRECT REF. AND REWORK PROCEDURE USED FOR DAMAGED AREAS.) FABRICATED NEW FLOOR PANEL 251KFF, MPN: 146T5869-9, LBL 77.50- LBL 86.75, STA 1087-1207 IN REF. TO BOEING DWG 146T586Feb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202602040126Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241WFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 241WFF, MPN: 145T5876-51, RBL 11- LBL 11, STA 1114.82-984.95 IN REF. TO BOEING DWG 145T5876-51, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MFeb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602040124Floorboard · damagedFLOORBOARD 241AGF IS DAMAGED. FABRICATED NEW FLOOR PANEL 241AGF, MPN: 145T5874-31, RBL 77.50 - RBL 89.50, STA 984.95-1087 IN REF. TO BOEING DWG 145T5874-31, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR.Feb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602040123Floor Panel · damagedFLOOR PANEL 242MFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 242MFF, RBL 74.25"- RBL 86.25", STA 933- 984.95 IN REF. TO BOEING DWG 145T5876-21. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED ON WO# Feb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602040122Floorboard · damagedFLOORBOARD 241QFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 241QFF, LBL 77.50"- LBL 89.50", STA 933- 984.95 IN REF. TO BOEING DWG 145T5876-15. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED ON WO# Feb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602040121Floor Panel · damagedFLOORBOARD 242LFA IS DAMAGED. FABRICATED NEW FLOOR PANEL 242LFA, MPN: 145T5874-18, RBL 54.75- RBL 74.25, STA 930-972 IN REF. TO BOEING DWG 145T5874-18. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISFeb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202602030115Floor Panel · damagedFLOORBOARD 241XFF IS DAMAGED. FABRICATED FLOOR PANEL 241XFF (MPN: 145T5874-39) AT BS 9984.95- 1114.82, BETWEEN LBL11- LBL33 IN REF TO DRAWING 145T5874-39., AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PFeb 3, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202601290098Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242VFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 242VFF, MPN: 145T5874-32, RBL 84.25 - RBL 74.25, STA 984.95-1087 IAW DWG 145T5874-32, AND SR67-53-009. PERFORMED. MAJOR REPAIR.Jan 29, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202601280096Floorboard · dentedFLOORBOARD 242VFF IS DAMAGED VFF SHOULD BE 242UFF. FABRICATED FLOOR PANEL 242UFF (MPN: 145T5874-34) AT STA 980.95 - STA1114.82, RBL 54.75 - RBL 74.25 IN REF TO BOEING DRAWING 145T5874-34., AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJORJan 28, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202404120457Skin · damagedDURING HMV 1 AT INDY, A PRIOR LIGHTNING STRIKE WAS DISCOVERED AND ONE FASTENER LOCATION AT STA 452, ON STRINGER 30L WAS BLENDED TO 0.040 THICK FROM A 0.063 MATERIAL THICKNESS AT THIS LOCATION. THIS AREA WILL BE REPAIRED WITH A SRM 53-00-01-2R REPAIR 29 DOUApr 12, 2024 · N297FE · Boeing 76732LF · Fuselage Main, Plate/SkinSDR FDEA202403290445Skin · dentedRH OUTBD WING, #11 SLAT HAS SMALL DENT ON UPPER SURFACE. MARKED MK8 REPAIRED RH WING L/E # 11 SLAT TRAILING EDGE WEDGE TOP SURFACE AT WS OSS 856 IN REF TO 767 SRM 57-43-02-2R, PG 1-2 DETAIL I & III, FIG.201 SHEETS 1 & 2, 767 SRM 51-70-10-2R, THIS IS A MAJOMar 29, 2024 · N297FE · Boeing 76732LF · Leading Edge DevicesSDR FDEA202403290442Former · mismanufacturedR/H L/E NOSE FORMER ANGLE MALFORMED AND HAS MORE THAN .037" GAP TO LEADING EDGE SKIN. ENGINEERING CONTACTED PER SEQUENCE 708 AND RECOMMENDS REPLACEMENT.Mar 29, 2024 · N297FE · Boeing 76732LF · Wing Miscellaneous StructureSDR FDEA202403290440Former · misalignedR/H L/E NOSE FORMER ANGLE MALFORMED AND HAS MORE THAN .037" GAP TO LEADING EDGE SKIN. ENGINEERING CONTACTED PER SEQUENCE 708 AND RECOMMENDS REPLACEMENT. REF. SEQ 708 ON SAME WO FOR REPLACEMENT OF FORMER AT OSS 441 IAW FDX E.O.#:H-5720-E0368563C, WING-SECONMar 29, 2024 · N297FE · Boeing 76732LF · Wing Miscellaneous StructureSDR FDEA202308241491Skin · delaminatedR/H I/B AILERON, LOWER SURFACE HAS SMALL AREA OF SKIN DELAMINATION NEAR I/B AFT CORNER. M.W.T. 0000553921 : DAVIES, ANDREW M - 24-AUG-2023 23:10 INSTALLED BONDED REPAIR ON RH IB AILERON LOWER SURFACE IN REF. TO 767 SRM: 57-60-01-2R AND 51-70-04. COMPLIED WAug 24, 2023 · N297FE · Boeing 767300 · AileronsSDR FDEA202108011918Line · leakingAFTER BLOCK IN, MX REPORTED A HYDRAULIC MIST/DRIP FROM LEFT MAIN WHEEL WELL. CRASH FIRE AND RESCUE WAS CALLED. TRACED HYDRAULIC LEAK TO BRAKE PRESSURE TUBE ASSY, P/N 373T1200-375. REF IPC 32-41-65-01 ITEM 305. FOUND TUBE WAS KINKED, WITH LEAK LOCATED AAug 1, 2021 · N297FE · Boeing 76732LF · Hydraulic System, MainSDR FDEA202105201320Warning Message · false activationFWD CARGO DOOR CAUTION ON CLIMB OUT. CHECKED FWD CARGO DOOR PROX SENSORS 150,151,152,153, AND 154 WITH BREAKOUT BOX, ALL SENSORS CHECK GOOD, READING 4.8 MH ON150,151 AND 153(FAR) AND 5.4 MH ON 152, AND 5.8MH ON 154 (NEAR) WITH DOOR CLOSED. ALL SENSORS ALSO May 20, 2021 · N297FE · Boeing 76732LF · Door Warning SystemSDR FDEA202105201315Warning Light · false activationFWD CARGO DOOR CAUTION ON CLIMB OUT. RAN QRH. DECLARED EMERGENCY. RELEASED FOR SERVICE PER MEL : 52-71-01-01-B CATEGORY C. INSPECTED FWD LOWER CARGO DOOR. IT WAS CLOSED, LOCKED, VENT DOORS CLOSED AND VERIFIED CLOSED IN THE VIEWING WINDOWS. DEBRIEFED CREW May 20, 2021 · N297FE · Boeing 76732LF · Door Warning SystemSDR FDEA202104130909Angle · crackedMAIN DECK FLOOR SPLICE IS CRACKED REMOVED & REPLACED FLOOR SPLICE ANGLE IAW BAC DWG 146T5650Apr 13, 2021 · N297FE · Boeing 76732LF · Fuselage Miscellaneous StructureSDR FDEA202104130908Angle · crackedMAIN DECK FLOOR SPLICE ANGLE IS CRACKED REMOVED & REPLACED ANGLE IAW BAC DWG 146T5650Apr 13, 2021 · N297FE · Boeing 76732LF · Fuselage Miscellaneous StructureSDR FDEA202104130907Angle · crackedLH NOSE TUNNEL @ STA 246, LBL 50, FLOOR SUPPORT ANGLE IS CRACKED REMOVED & REPLACED ANGLE IAW BAC DWG 141T5600 SHEET 4 REV - & BAC DWG 141T5146 REV FApr 13, 2021 · N297FE · Boeing 76732LF · Fuselage Miscellaneous StructureSDR FDEA202104110887Angle · crackedAFT CARGO COMPARTMENT, FWD END-WALL, @ STA 1087 HAS CRACKED ATTACH ANGLE REMOVED & REPLACED ANGLE IAW BAC DWG 140T0130Apr 11, 2021 · N297FE · Boeing 76732LF · Fuselage Miscellaneous StructureSDR FDEA202007171555Unknown · odorDURING DECENT, BELOW 16000 FT, THERE WAS A STRONG CIGARETTE LIKE SMELL EMITTING FROM AN UNKNOWN SOURCE. NO SMOKE WAS VISIBLE. THE ODOR DISSIPATED AFTER TAXI-IN. DURING DEBRIEF, CREW NOTED APU WAS NOT OPERATION DURING EVENT. INSPECTED THE FWD EQUIPMENT BAJul 17, 2020 · N297FE · Boeing 76732LF · Air Distribution SystemSDR FDEA2020021430335Bearing · failedBRAKE TEMP LT ILLUMINATED ON BLOCK IN BRAKE TEMPS WERE 23/44/22/54 FOUND THAT THE #7 BRAKE OUTER BEARING FAILED AND IMPACTING THE WHEEL/ TIRE, REPLACED THE #7 BRAKE PER M/M 32-41-08-4-4 AND THE #7 WHEEL/ TIRE PER M/M 32-45-0-4. BRAKE TEMP TEST OK. WHEFeb 13, 2020 · N297FE · Boeing 76732LF · Landing Gear Brake SystemSDR FDEA202002080299Fault Message · false activationMDIS 297 34-61 3894 08FEB20 MEM FACT U. PER CREW VERBAL: DURING APPROACH A/C FULLY CONFIGURED FLAPS 30, VREF FOR THE LANDING WEIGHT OF 302.3 WAS COMPUTING 141 KTS. AT THIS AIRSPEED THE STALL ZIPPER WAS ABOVE THE VREF SPEED APPROXIMATELY 7-8 KNOTS. THE HUD Feb 8, 2020 · N297FE · Boeing 76732LF · Central WarningSDR FDEA2020021080299Indicator · false indicationMDIS 297 34-61 3894 08FEB20 MEM FACT U PER CREW VERBAL: DURING APPROACH A/C FULLY CONFIGURED FLAPS 30, VREF FOR THE LANDING WEIGHT OF 302.3 WAS COMPUTING 141 KTS. AT THIS AIRSPEED THE STALL ZIPPER WAS ABOVE THE VREF SPEED APPROXIMATELY 7-8Feb 8, 2020 · N297FE · Boeing 767332 · Flight Management Computing Software SystemSDR FDEA201903090563Window · arcedL SIDE NR 2 WINDOW OVERHEAT WITH ARCING DELAMINATION AND CRACKING. FACT 10MAR19 04:42 DEN REMOVED AND REPLACED LEFT WINDOW NR 2 REF AMM 56-11-02-4. WINDOW OPS CHECKS GOOD REF AMM 56-11-02 AND WINDOW ANTI-ICING OPS CHECKS GOOD REF AMM 30-41-00. A/C OK FOR Mar 9, 2019 · N297FE · Boeing 76732LF · Flight Compartment WindowsSDR FDEA201901020008Wheel · damagedNR 5 TIRE WORN. UPON REMOVAL FOUND INNER HALF OF WHEEL TO BE DAMAGED FROM CONTACTING BRAKE ASSEMBLY. REMOVED AND REPLACED NR 5 WHEEL AND TIRE ASSEMBLY. REFERENCE AMM 32-45-01-4. (NOTE NR 5 BRAKE WAS FOUND TO HAVE A LOOSE OUTER AXLE BUSHING.)Jan 2, 2019 · N297FE · Boeing 76732LF · Wheel/Ski/FloatSDR FDEA2019010113625Bushing · wornNOTED NR 5 WHEEL INNER SURFACE APPEARS TO BE CONTACTING OUTER BRAKE SURFACE. UPON REMOVAL OF TIRE AND BRAKE ASSEMBLY, FOUND BRAKE AXLE BUSHING WORN ALLOWING CONTACT BETWEEN WHEEL AND BRAKE. REMOVED AND REPLACED NR 5 BRAKE ASSEMBLY. REFERENCE AMM 32-41-08-4-4. Dec 31, 2018 · N297FE · Boeing 76732LF · BrakeSDR FDEA201811093168Pseu · faultyLE SLAT DISAGREE MSG RECEIVED AFTER MOVING FLAP HANDLE TO 1 ON APPROACH. COMPLIED WITH QRH PROCEDURES. REPLACED PSEU REF AMM 32-09-04-4, NO DEFECTS NOTED. PERFORMED SENSORS S287, S299 AND S305 TARGET TEST AT SLATS RET, T/O AND LDG REF AMM 27-81-00-3, NO DEFECTNov 9, 2018 · N297FE · Boeing 76732LF · Leading Edge Slat Position Indicating SystemSDR FDEA201804070907Skin · damagedRT WING INBD AFT FLAP LOWER EDGE COMPOSITE SKIN HAS MINOR DAMAGE, 51 INCHES AWAY FROM INBD END. REPAIRED THE RT WING AFT FLAP IAW SRM 51-70-10-2R, AND EA TH-5750-T0339275. MAJOR REPAIR.Apr 7, 2018 · N297FE · Boeing 76732LF · Trailing Edge FlapsSDR FDEA201803310814Skin · dentedLEFT WING NR 4 SLAT DENTED ON THE TE WEDGE UPPER SKIN FROM OTBD BETWEEN 5 AND 8 INCHES. REPAIRED IAW SRM 51-70-10-2R, REP 2, SRM 57-43-02-02R, AND EA T-5750-T0339155 ,P1. MAJOR REPAIR.Mar 31, 2018 · N297FE · Boeing 76732LF · Trailing Edge FlapsSDR FDEA201803300806Skin · dentedLEFT WING L/E SLAT HAS DENT ON T/E WEDGE UPPER SKIN FROM INBD BETWEEN 57 & 60 INCHES. REPAIRED IAW SRM 51-70-10, REPAIR 2, SRM 57-43-02-2R, AND EA H-5750-T0339161, P1. MAJOR REPAIR.Mar 30, 2018 · N297FE · Boeing 76732LF · Leading Edge DevicesSDR FDEA201803270789Skin · dentedRIGHT WING L/E NR 10 SLAT HAS DENTS ON T/E WEDGE UPPER SKIN FROM INBD BETWEEN 62 INCHES & 71 INCHES. REPAIRED THE SLAT IAW SRM 51-70-10-2R, REPAIR 2, MAJOR REPAIR.Mar 27, 2018 · N297FE · Boeing 76732LF · Leading Edge DevicesSDR FDEA201702110524Tire · out of roundDURING TAKEOFF ROLL, ENCOUNTERED VERY NOTICABLE SHUDDER OF UNKNOWN ORIGIN. ABORTED TAKEOFF AT 100 KTS. JACKED NOSE GEAR AND FOUND BOTH NOSE TIRES OUT OF ROUND. IAW FIM 32-51 FT 805 FIGURE 104.Feb 11, 2017 · N297FE · Boeing 76732LF · TireSDR FDEA201610013406Skin · chafedRT WING I/B FLAP O/B END UPPER SURFACE HAS DEEP CHAFING MARK JUST ABOVE UPPER SEAL. REPAIRED RT WING IB FLAP OB END UPPER SURFACE IAW SRM 57-53-01-2R FIG 201 AND 51-70-05.Oct 1, 2016 · N297FE · Boeing 76732LF · Trailing Edge FlapsSDR FDEA201609263366Skin · dentedFUSELAGE SKIN DENTED AT BS 1398 BETWEEN STRINGERS 34-35L. COMPLIED WITH EA H-5330-T0328464 P1. FABRICATED A REPAIR DOUBLER AND FILLER. INSTALLED REPAIR.Sep 26, 2016 · N297FE · Boeing 76732LF · Fuselage Main, Plate/SkinSDR FDEA201609013098Duct · loosePASSING FL 220 AT 330 IAS IN CLIMB, A SUDDEN AND EXTREMELY LOUD HORN, SIREN OR WHISTLE CAME ON. LEVELED AT FL 260 AND SLOWED TO 300 KTS IAS. SOUNDS CONTINUED FOR ABOUT 10 MIN AND THEN SLOWLY DECREASED TO ZERO. F/O AND CAPT BOTH REPORTED NOISE WAS LOUD CONTINSep 1, 2016 · N297FE · Boeing 76732LF · Air Distribution SystemSDR FDEA201608222948Skin · damagedBIRD STRIKE DENTED THE LT FORWARD FUSELAGE AT STA 148.5, WL 215. DENT MEASURES 6.4" X 3.5" X 0.336". REPAIRED DAMAGE IAW SRM 53-00-01, FIG 201, TABLE 5 WHICH REQUIRES REPETITIVE INSPECTION. CONTACT MOCC AFTER 30K FLT CYCLE INSPECTION TO SET UP 12K FLT CYCLEAug 22, 2016 · N297FE · Boeing 76732LF · Fuselage Main, Plate/SkinSDR FDEA201608112880Skin · damagedBIRD STRIKE IMPACT CAUSED DENT IN STRUCTURE APPROXIMATELY 17" AFT OF RADOME AND 8" BELOW THE LT TAT PROBE. INSPECTED IAW EA H-5310-T0327414A PERFORMED HFEC OF EXTERNAL SKIN SURFACE OF DENT. ALSO BORESCOPE INSPECTED INTERNAL STRUCTURE AT DENT AREA. COMPLIED WAug 11, 2016 · N297FE · Boeing 76732LF · Fuselage Main, Plate/Skin
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