N416UP

Service difficulty reports · 261

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 = 'N416UP' 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 UPS06548278Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, S26R. CUT OUT DAMAGED SECTION STA 1340 RT S=26R. L=.95" X W=1.0". HFEC IAW NTM 51-00-00, NO CRACK INDICATIONS NOTED COMPLIED WITH EA 757-5362-27-A1548 & UPS EO B757-5310-25385A.Sep 28, 2006 · N416UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06548277Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1300, S26R. REMOVED TRANS PNL, CUT OUT DAMAGE S=26R L=.95 X W1.10. HFEC IAW NTM 51-00-00 PT 6, NO CRACK INDICATIONS NOTED REPAIRED IAW EA 757-5362-27-A1547, UPS EO B757-5310-25366.Sep 28, 2006 · N416UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06548276Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1240, BETWEEN S26R - S27R. TRIMMED OUT FUSELAGE FRAME STA 1240 BETWEEN S26R-S27R. DAMAGE 0.790"L X .0950"W. HFEC IAW NTM 51-00-00, NO CRACK INDICATION NOTED. ENLARGED TRIM OUT BY 0.04" NEW DIM. L=0.830Sep 28, 2006 · N416UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06548275Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1300, S26L. REMOVED TRANS PNL STA 1200-1300 LT SIDE FOR ACCESS, CUT OUT DAMAGE SECT. L=1.25" W=1.0". REMOVED TIE DOWN FITTING HFEC IAW NTM 51-00-PL 6, NO CRACK INDICATIONS NOTED COMPLIED WITH EA 757-5362Sep 28, 2006 · N416UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06548271Frame · chafedINSPECTION TYPE:C MAIN CARGO DECK FRAME AT STA 365 HAS CHAFE BETWEEN STR 15R-16R. PERFORMED PARTIAL BLEND OF AREA OF FRAME DIMENSIONS ARE AS FOLLOWS: L= .6, W= .6, D= .013, ORIGINAL DAMAGE STILL EVIDENT. REPAIR ACCOM ON EA 757-5332-27-A1557 AND UPS EO B757-5Sep 28, 2006 · N416UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06548270Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1280, S25L. TRIMMED OUT FUSELAGE STA 1280 FLANGE DAMAGED PER EA 757-5362-27-A1550, STEP NR 1 DIMENSIONS ARE 0.590"L X 0.900"W. HFEC IAW NTM 51-00-00 PT 6 NO CRACK INDICATIONS NOTED. COMPLIED WITH FINAL Sep 28, 2006 · N416UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547670Lamp · inoperativeEMERG EXIT "UNARMED" LIGHT HAS 1 INOP LAMP. RELAMPED IAW M/M 33-16-02-2.Aug 11, 2006 · N416UP · Boeing 75724APF · Emergency LightingSDR UPS02537808Actuator · leakingINSPECTION TYPE:N/A UPON LANDING AT OMA CABIN SMOKE WHEN REVERSE INITIATED (NOTE: ONLY RT PACK ON DURING LANDING). INSPECTED A/C FOR LEAKS. FOUND UPPER I/B TR ACT LEAKING REPLACED RT UPPER I/B ACTUATOR. RAN PACK, OPS CHECKS NORMAL.Mar 9, 2002 · N416UP · Boeing 75724APF · Engine Thrust ReverserSDR UPS01535767Door Seal · tornCREW ENTRY DOOR SEAL TORN REF: D205294. PARTIAL TEAR, INNER SEAL OF CREW ENTRY DOOR. REPAIRED TEAR ON CREW ENTRY DOOR. OK FOR SERVICE.Apr 28, 2001 · N416UP · Boeing 75724APF · Passenger/Crew DoorsSDR UPS00533473Actuator · inoperativeINSPECTION TYPE:N/A, HORIZ STAB WILL NOT TRIM NOSE DOWN. REPLACED RT SAM PER MM OPS NORMAL.Aug 1, 2000 · N416UP · Boeing 75724APF · Stabilizer ActuatorSDR UPS97522219Fuse Pin · crackedINSPECTION TYPE:1C, FUSE PIN REPLACEMENT RIGHT HAND PYLON. REMOVED FUSE PIN, FOUND BOTH TO BE CRACKED, REPLACED BOTH FUSE PINS.Mar 3, 1997 · N416UP · Boeing 75724APF · Nacelle/Pylon Structure
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