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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 SDR 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.SDR 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 THISSDR 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 /SDR 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 MAJSDR 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.SESDR 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.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 SDR 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 146T586SDR 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 MSDR 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.SDR 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# SDR 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# SDR 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 ACCOMPLISSDR 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 PSDR 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.SDR 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 MAJORSDR 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 DOUSDR 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 MAJOSDR 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.SDR 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-SECONSDR 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 WSDR 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 ASDR 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 SDR 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 SDR FDEA202104130909Angle · crackedMAIN DECK FLOOR SPLICE IS CRACKED REMOVED & REPLACED FLOOR SPLICE ANGLE IAW BAC DWG 146T5650SDR FDEA202104130908Angle · crackedMAIN DECK FLOOR SPLICE ANGLE IS CRACKED REMOVED & REPLACED ANGLE IAW BAC DWG 146T5650SDR 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 FSDR FDEA202104110887Angle · crackedAFT CARGO COMPARTMENT, FWD END-WALL, @ STA 1087 HAS CRACKED ATTACH ANGLE REMOVED & REPLACED ANGLE IAW BAC DWG 140T0130SDR 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 BASDR 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. WHESDR 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 SDR 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 7-8SDR 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 SDR 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.)SDR 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. SDR 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 DEFECTSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 CONTINSDR 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 CYCLESDR 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 W
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