# Service difficulty reports: N297FE

A list on [N297FE](https://openairdocs.org/aircraft/N297FE.md).

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

- [SDR FDEA202607160937](https://openairdocs.org/sdr/FDEA202607160937.md): Transmitter · failed · Jul 16, 2026 · N297FE · Boeing 76732LF · Trailing Flap Position Indicating System
  > ON 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
- [SDR FDEA202602090148](https://openairdocs.org/sdr/FDEA202602090148.md): Skin · worn · Feb 9, 2026 · N297FE · Boeing 76732LF · Trailing Edge Flaps
  > RH 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.
- [SDR FDEA202602080146](https://openairdocs.org/sdr/FDEA202602080146.md): Floorboard · damaged · Feb 8, 2026 · N297FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN 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 THIS
- [SDR FDEA202602070145](https://openairdocs.org/sdr/FDEA202602070145.md): Floor Panel · damaged · Feb 7, 2026 · N297FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN 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 /
- [SDR FDEA202602060139](https://openairdocs.org/sdr/FDEA202602060139.md): Floor Panel · delaminated · Feb 6, 2026 · N297FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN 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 MAJ
- [SDR FDEA202602050134](https://openairdocs.org/sdr/FDEA202602050134.md): Floorboard · dented · Feb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN 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.SE
- [SDR FDEA202602050133](https://openairdocs.org/sdr/FDEA202602050133.md): Floor Panel · dented · Feb 5, 2026 · N297FE · Boeing 7673S2F · Fuselage Structure (General)
  > MIAN 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.
- [SDR FDEA202602050131](https://openairdocs.org/sdr/FDEA202602050131.md): Floorboard · delaminated · Feb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN 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
- [SDR FDEA202602050130](https://openairdocs.org/sdr/FDEA202602050130.md): Floor Panel · damaged · Feb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN 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 146T586
- [SDR FDEA202602040126](https://openairdocs.org/sdr/FDEA202602040126.md): Floor Panel · damaged · Feb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN 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 M
- [SDR FDEA202602040124](https://openairdocs.org/sdr/FDEA202602040124.md): Floorboard · damaged · Feb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOORBOARD 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.
- [SDR FDEA202602040123](https://openairdocs.org/sdr/FDEA202602040123.md): Floor Panel · damaged · Feb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOOR 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#
- [SDR FDEA202602040122](https://openairdocs.org/sdr/FDEA202602040122.md): Floorboard · damaged · Feb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOORBOARD 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#
- [SDR FDEA202602040121](https://openairdocs.org/sdr/FDEA202602040121.md): Floor Panel · damaged · Feb 4, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOORBOARD 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 ACCOMPLIS
- [SDR FDEA202602030115](https://openairdocs.org/sdr/FDEA202602030115.md): Floor Panel · damaged · Feb 3, 2026 · N297FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOORBOARD 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 P
- [SDR FDEA202601290098](https://openairdocs.org/sdr/FDEA202601290098.md): Floor Panel · damaged · Jan 29, 2026 · N297FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA202601280096](https://openairdocs.org/sdr/FDEA202601280096.md): Floorboard · dented · Jan 28, 2026 · N297FE · Boeing 76732LF · Fuselage Floor Panel
  > FLOORBOARD 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 MAJOR
- [SDR FDEA202404120457](https://openairdocs.org/sdr/FDEA202404120457.md): Skin · damaged · Apr 12, 2024 · N297FE · Boeing 76732LF · Fuselage Main, Plate/Skin
  > DURING 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 DOU
- [SDR FDEA202403290445](https://openairdocs.org/sdr/FDEA202403290445.md): Skin · dented · Mar 29, 2024 · N297FE · Boeing 76732LF · Leading Edge Devices
  > RH 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 MAJO
- [SDR FDEA202403290442](https://openairdocs.org/sdr/FDEA202403290442.md): Former · mismanufactured · Mar 29, 2024 · N297FE · Boeing 76732LF · Wing Miscellaneous Structure
  > R/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.
- [SDR FDEA202403290440](https://openairdocs.org/sdr/FDEA202403290440.md): Former · misaligned · Mar 29, 2024 · N297FE · Boeing 76732LF · Wing Miscellaneous Structure
  > R/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-SECON
- [SDR FDEA202308241491](https://openairdocs.org/sdr/FDEA202308241491.md): Skin · delaminated · Aug 24, 2023 · N297FE · Boeing 767300 · Ailerons
  > R/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 W
- [SDR FDEA202108011918](https://openairdocs.org/sdr/FDEA202108011918.md): Line · leaking · Aug 1, 2021 · N297FE · Boeing 76732LF · Hydraulic System, Main
  > AFTER 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 A
- [SDR FDEA202105201320](https://openairdocs.org/sdr/FDEA202105201320.md): Warning Message · false activation · May 20, 2021 · N297FE · Boeing 76732LF · Door Warning System
  > FWD 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
- [SDR FDEA202105201315](https://openairdocs.org/sdr/FDEA202105201315.md): Warning Light · false activation · May 20, 2021 · N297FE · Boeing 76732LF · Door Warning System
  > FWD 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
- [SDR FDEA202104130909](https://openairdocs.org/sdr/FDEA202104130909.md): Angle · cracked · Apr 13, 2021 · N297FE · Boeing 76732LF · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SPLICE IS CRACKED REMOVED & REPLACED FLOOR SPLICE ANGLE IAW BAC DWG 146T5650
- [SDR FDEA202104130908](https://openairdocs.org/sdr/FDEA202104130908.md): Angle · cracked · Apr 13, 2021 · N297FE · Boeing 76732LF · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SPLICE ANGLE IS CRACKED REMOVED & REPLACED ANGLE IAW BAC DWG 146T5650
- [SDR FDEA202104130907](https://openairdocs.org/sdr/FDEA202104130907.md): Angle · cracked · Apr 13, 2021 · N297FE · Boeing 76732LF · Fuselage Miscellaneous Structure
  > LH 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 F
- [SDR FDEA202104110887](https://openairdocs.org/sdr/FDEA202104110887.md): Angle · cracked · Apr 11, 2021 · N297FE · Boeing 76732LF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, FWD END-WALL, @ STA 1087 HAS CRACKED ATTACH ANGLE REMOVED & REPLACED ANGLE IAW BAC DWG 140T0130
- [SDR FDEA202007171555](https://openairdocs.org/sdr/FDEA202007171555.md): Unknown · odor · Jul 17, 2020 · N297FE · Boeing 76732LF · Air Distribution System
  > DURING 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 BA
- [SDR FDEA2020021430335](https://openairdocs.org/sdr/FDEA2020021430335.md): Bearing · failed · Feb 13, 2020 · N297FE · Boeing 76732LF · Landing Gear Brake System
  > BRAKE 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. WHE
- [SDR FDEA202002080299](https://openairdocs.org/sdr/FDEA202002080299.md): Fault Message · false activation · Feb 8, 2020 · N297FE · Boeing 76732LF · Central Warning
  > MDIS 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
- [SDR FDEA2020021080299](https://openairdocs.org/sdr/FDEA2020021080299.md): Indicator · false indication · Feb 8, 2020 · N297FE · Boeing 767332 · Flight Management Computing Software System
  > MDIS 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
- [SDR FDEA201903090563](https://openairdocs.org/sdr/FDEA201903090563.md): Window · arced · Mar 9, 2019 · N297FE · Boeing 76732LF · Flight Compartment Windows
  > L 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
- [SDR FDEA201901020008](https://openairdocs.org/sdr/FDEA201901020008.md): Wheel · damaged · Jan 2, 2019 · N297FE · Boeing 76732LF · Wheel/Ski/Float
  > NR 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.)
- [SDR FDEA2019010113625](https://openairdocs.org/sdr/FDEA2019010113625.md): Bushing · worn · Dec 31, 2018 · N297FE · Boeing 76732LF · Brake
  > NOTED 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.
- [SDR FDEA201811093168](https://openairdocs.org/sdr/FDEA201811093168.md): Pseu · faulty · Nov 9, 2018 · N297FE · Boeing 76732LF · Leading Edge Slat Position Indicating System
  > LE 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 DEFECT
- [SDR FDEA201804070907](https://openairdocs.org/sdr/FDEA201804070907.md): Skin · damaged · Apr 7, 2018 · N297FE · Boeing 76732LF · Trailing Edge Flaps
  > RT 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.
- [SDR FDEA201803310814](https://openairdocs.org/sdr/FDEA201803310814.md): Skin · dented · Mar 31, 2018 · N297FE · Boeing 76732LF · Trailing Edge Flaps
  > LEFT 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.
- [SDR FDEA201803300806](https://openairdocs.org/sdr/FDEA201803300806.md): Skin · dented · Mar 30, 2018 · N297FE · Boeing 76732LF · Leading Edge Devices
  > LEFT 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.
- [SDR FDEA201803270789](https://openairdocs.org/sdr/FDEA201803270789.md): Skin · dented · Mar 27, 2018 · N297FE · Boeing 76732LF · Leading Edge Devices
  > RIGHT 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.
- [SDR FDEA201702110524](https://openairdocs.org/sdr/FDEA201702110524.md): Tire · out of round · Feb 11, 2017 · N297FE · Boeing 76732LF · Tire
  > DURING 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.
- [SDR FDEA201610013406](https://openairdocs.org/sdr/FDEA201610013406.md): Skin · chafed · Oct 1, 2016 · N297FE · Boeing 76732LF · Trailing Edge Flaps
  > RT 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.
- [SDR FDEA201609263366](https://openairdocs.org/sdr/FDEA201609263366.md): Skin · dented · Sep 26, 2016 · N297FE · Boeing 76732LF · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1398 BETWEEN STRINGERS 34-35L. COMPLIED WITH EA H-5330-T0328464 P1. FABRICATED A REPAIR DOUBLER AND FILLER. INSTALLED REPAIR.
- [SDR FDEA201609013098](https://openairdocs.org/sdr/FDEA201609013098.md): Duct · loose · Sep 1, 2016 · N297FE · Boeing 76732LF · Air Distribution System
  > PASSING 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 CONTIN
- [SDR FDEA201608222948](https://openairdocs.org/sdr/FDEA201608222948.md): Skin · damaged · Aug 22, 2016 · N297FE · Boeing 76732LF · Fuselage Main, Plate/Skin
  > BIRD 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 CYCLE
- [SDR FDEA201608112880](https://openairdocs.org/sdr/FDEA201608112880.md): Skin · damaged · Aug 11, 2016 · N297FE · Boeing 76732LF · Fuselage Main, Plate/Skin
  > BIRD 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 W

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N297FE/reports

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