N162FE
Service difficulty reports · 26
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 = 'N162FE' 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 = 'N162FE' 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 FDEA202603210363Skin · dentedINDUCED DAMAGE SLAT #8 L/E SKIN AT INB EDGE OSS389 ON SLAT #8 WAS REPAIRED IAW E.A. H-5750-T0386687.SDR FDEA202603180357Floor Panel · damagedSCREWS THROUGH 241PFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241PFF BOTTOM SIDE WAS REPAIRED AND SCREWS WERE CORRECTLY INSTALLED IN THE FLOOR PANEL IAW SRM 53-00-50-2R REPAIR GENERAL PAR B FIG 201 AND SRM 51-40-02-0G PAR 9 REV 94 DEC 15,2025SDR FDEA202603130349Floor Panel · puncturedPUNCTURES ON 231LFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT, FLOOR PANEL 231LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B. FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202603130348Floor Panel · debondedDISBONDING FLOOR PANEL 242KFF FLOOR PANEL 242KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202603130343Floor Panel · damagedGROOVE ON 241DFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT, FLOOR PANEL 241DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PARA 4.B FIG 201 SHEET 2 REV. 94 DEC 15 / 2025SDR FDEA202603130342Floor Panel · puncturedPUCTURES ON 241DFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. MAIN CARGO COMPARTMENT, FLOOR PANEL 241DFF WAS REPAIRED IAW. B767 SRM 53-00-50-2R PARA. 4.B FIG. 201 SHEET 2 REV. 94 DEC 15 / 2025SDR FDEA202603120341Floor Panel · puncturedPUNCTURE ON 231JFF FLOOR PANEL ON MAIN CARGO COMPARTMENT 231JFF FLOOR PANEL ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV. 94 DEC 15,2025SDR FDEA202603120340Floor Panel · crackedCRACK ON FLOOR PANEL 241YFA FLOOR PANEL 241YFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 (B) REV 94 DEC 15/2025SDR FDEA202603120339Floor Panel · damagedPUNCTURE ON 251KFF FLOOR PANEL ON MAIN CARGO COMPARTMENT FLOOR PANEL 251KFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 (B) REV 94 DEC 15/2025SDR FDEA202603120338Floor Panel · damagedPUNCTURE ON 251EFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. 251EFF FLOOR PANEL ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15,2025SDR FDEA202603120337Floor Panel · damagedPUNCTURE ON 242GFF FLOOR PANEL ON MAIN CARGO COMPARTMENT 242GFF FLOOR PANEL ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV.94 DEC 15, 2025SDR FDEA202603120336Floor Panel · damagedPUNCTURE ON 231EFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. 231EFF FLOOR PANEL ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15,2025SDR FDEA202603100332Floor Panel · crackedCRACK ON 242TFA FLOOR PANEL ON MAIN DECK CARGO COMPARTMENT 242TFA FLOOR PANEL ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR.4-B FIG. 201 SHEET REV.94.SDR FDEA202603080330Floor Panel · puncturedPUNCTURES ON 232MFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT, FLOOR PANEL 232MFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4B FIG. 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202603080329Floor Panel · puncturedPUNCTURES ON 231RFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT, FLOOR PANEL 231 RFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4.B FIG. 201 SHEET 2 RE.94 DEC15/2025SDR FDEA202603080328Floor Panel · damagedPUNCTURE ON 241FFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. MAIN CARGO COMPARTMENT, FLOOR PANEL 241 FFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4B FIG 201 SHEET 2 REV.94 DEC15/2025SDR FDEA202603080327Floor Panel · puncturedPUNCTURE ON 241 JFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT FLOOR PANEL 241 JFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG.201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202603080326Floor Panel · damagedPUNCTURE ON 231NFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. MAIN CARGO COMPARTMENT, FLOOR PANEL 231 NFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV. 94 DEC15/2025SDR FDEA202408281182Lamp · failedRIGHT MAIN GEAR INDICATOR HAS BOTH BULBS OUT (OR IS INOPERATIVE). DISCONTINUED FIRST APPROACH WITH ONLY TWO GEAR INDICATIONS GREEN. RAN QRH AND DETERMINED THAT IN THE ABSENCE OF A GEAR DISAGREE MESSAGE OR CONFIG WARNING, THE RIGHT MAIN GEAR WAS INDEED DOWNSDR FDEA202404240286Nut · looseSECTION 48, LH HORIZONTAL PIVOT FITTING, INBOARD FACE, LOCKWIRE BROKEN. SECTION 48, LH HORIZONTAL PIVOT FITTING, INBOARD FACE NUT OF BEARING WAS TIGHTENED AND APPLIED TORQUE, AND INSTALLED LOCKWIRE IAW AMM 55-17-51-4 REV. 141. THE STABILIZER WAS OPERATED SSDR FDEA202404130462Skin · dentedDENT ON LOWER SKIN OF INBOARD TRAILING EDGE MAIN FLAP AT LH WING. LH WING INB. T/E MAIN FLAP LOWER SKIN WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R REPAIR 1 FIG. 201 SHEET 2 NOTE A AND B767 SRM 51-70-03-0G PARAGRAPH 5.L. FIG. 16 REV. 88.SDR FDEA202404130461Skin · dentedDENT ON LOWER SKIN OF INBOARD TRAILING EDGE AFT FLAP AT LH WING. LH WING, LOWER SKIN OF INBOARD TRAILING EDGE AFT FLAP WAS REPAIRED I.A.W. B767 SRM 57- 53-01-2R REP. 1 AND SRM 51-70-03-0G PAR. 5.L. FIG. 16 PAG. 27-52 REV. 88.SDR FDEA202404130460Skin · dentedSEVERAL DENTS, LOWER SURFACE, INBOARD TRAILING EDGE FLAP, RH WING. RH WING INB. T/E AFT FLAP LOWER SURFACE WAS EVALUATED AND FOUND 3 DENTS WITHIN LIMITS I.A.W. B767 SRM 57-53-01-1A FIG. 101 SHEET 4 NOTE C DET. IV. ONE DENT WAS FOUND OUT OF LIMITS AND WAS RSDR FDEA202204070888None · delaminatedRH WING OUTBOARD FLAP LOWER SKIN WITH DENT AT WBL: 435. RH WING OUTBOARD FLAP LOWER SKIN WITH DENT AT WBL 435 THAT WAS REPAIRED IAW SRM 57- 53-01-2R FIG. 201 PAGE 1-6 TABLE II AND SRM 51-70-17-0G-0 FIG. 10 PAGE 1, 24, 25, 36, 48 PARA. 4.A. REV. 82 DEC15/20SDR FDEA2020051320922Floor Panel · delaminatedMAIN CABIN FLOOR 241PFF IS CRACKED FABRICATED NEW FLOOR PANEL PER FEDEX SRZ-25-005 REV R.SDR FDEA202005110919Wedge · chafedLEFT WING #5 L/E SLAT TRAILING EDGE HAS A CHAFE AT APPROX LES 425 REPAIRED LEFT WING #5 SLAT L/E SLAT T/E WEDGE IAW B767 SRM 57-43-02-2R & 51-70-10-2R REPAIR 4. MAJOR REPAIR
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