N903FD

Service difficulty reports · 162

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 = 'N903FD' 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 08FDEA00363Fitting · corrodedAFTER INSP FOR FINAL REAM FOUND NR 2 PYLON MID BULKHEAD FWD AND AFT LUG HOLES FOR SLEEVE BOLTS ACTUALLY REAMED TO .772", FOUND CORROSION ON EO NR F-5450-7-5005 PE STEP 10. HFEC INSPECTION FWD AND AFT SLEEVE BOLT HOLES IN THE NR 2 PYLON MID BULKHEAD FITTING PEFeb 7, 2008 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Attach FittingsSDR 08FDEA00338Intercostal · crackedINTERCOSTAL AT BETWEEN STATION 440 - 460 AT STRINGER 24L IS CRACKED, 0.75" LONG. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02. NEW INTERCOSTAL FABRICATED ON MAE TRAVELER NR T7/707194 IAW SRM 51-10-02, FROM 7075 - O - 0.063C, HEAT TREATED PER AMS 2770 HJan 31, 2008 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR 08FDEA00265Panel · corrodedNR 1 NACELLE STRUT I/B SKIN PANEL ASSY PN: 311N5046-34 HAS AREAS OF CORROSION C/M TO THE INNER SKIN SURFACE BETWEEN PP STA 153.9 AND PP 176 REMOVED CORROSION IAW SRM 54-50-01. ORIGINAL MATERIAL THICKNESS, 0.090", AFTER CORROSION REMOVAL, 0.063" AT PP STA 15Jan 24, 2008 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Plate/SkinSDR 08FDEA00246Floor Support · corrodedINTERCOSTAL FLOOR SUPPORT BRACKET BETWEEN STA 333.45 AND STA 324.0 HAS CORROSION. REMOVED CORROSION FROM SUPPORT BRACKET IAW SRM 51-10-02. UPON FURTHER INVESTIGATION FOUND SUPPORT TO BE OUT OF SRM 53-00-51 LIMITS, EXFOLIATED 100 PERCENT. REMOVED AND REPLAJan 23, 2008 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR 08FDEA00191Skin · dentedNR 1 NACELLE STRUT O/B SIDE SKIN HAS TWO DENTS, AT CUT OUT AREA OF ACCESS PANEL 433BL, AT APPROXIMATELY NAC STA 136.675, OUTBOARD SKIN HAD TWO DENTS MEASURING 1.6" WIDE BY .126" DEEP AND 1.9" WIDE BY .10" DEEP. BOTH FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01,Jan 17, 2008 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Plate/SkinSDR 08FDEA00123Strip · corrodedAFT CARGO DOOR SURROUND BETWEEN BS 1380-1440, AT RBL 24, NUT PLATE STRIP FOR DOOR SCUFF PLATE HAS SEVERAL AREAS OF CORROSION. REMOVED NUT PLATES AND FASTENERS FOR ACCESS TO CORROSION ON STRIP IAW SRM 51-40-02. CHECKED AND VERIFIED LIMITS UPON REMOVAL OF STRIJan 14, 2008 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR 08FDEA00097Bulkhead · damagedWHILE ACCOMPLISHING EO NR F-5450-7-5005 PT2, THE NR 2 PYLON MID BULKHEAD FWD LT BOLT HOLE WAS FOUND AT MAXIMUM DIAMETER OF 0.3918". MAXIMUM DIAMETER PER EO IS 0.3901-0.3911". THE FWD RT BOLT HOLE WAS FOUND TO BE 0.3934", OUT OF LIMITS PER EO. HFEC INSPECTEDJan 10, 2008 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Bulkhead/FirewallSDR 08FDEA00096Bulkhead · damagedWHILE ACCOMPLISHING FX EO F-5450-7-5005 PT, THE NR 1 PYLON MID BULKHEAD FWD RT BOLT HOLE WAS REAMED PER STEP 3.C AND FIG. 9. TOLERANCE FOR MAX DIA SHOULD BE 0.3901- 0.3911". FINAL DIA AFTER REAMING IS 0.3925". HFEC INSPECTED MID BULKHEAD FWD RT BOLT HOLE PJan 10, 2008 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Bulkhead/FirewallSDR 08FDEA00037Crease Beam · corrodedR2 DOOR, CREASE BEAM BETWEEN STA 680 TO 740, RBL 60, S17, HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .100", AFTER REWORK BLENDED AREA IS L= 48", W= 1.5", D= .085", OUT OF LIMITS IAW SRM 53-30-13, FIG 101. REMOVED AJan 5, 2008 · N903FD · Boeing 7572B7 · Fuselage Main, StructureSDR 08FDEA00036Shim · misalignedNR 1 PYLON MID BULKHEAD O/B FWD LOWER SPAR HAS SHIM MIGRATION. REMOVED FWD O/B BOLT PER STEP 1.1 OF EA F-5450-110803 DATED 11/12/07. REMOVED AND REPLACED FWD O/B SHIM WITH NEW SHIM PER STEPS 1.2 THRU 1.6 OF EA F-5450-110803 DATED 11/12/07. REAMED FWD O/B Jan 4, 2008 · N903FD · Boeing 757200 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00035Shim · misalignedNR 1 PYLON MID BULKHEAD INBOARD AFT AND FWD LOWER SPAR HAS SHIM MIGRATION. REMOVED FWD AND AFT I/B BOLTS PER STEP 2.1 OF EA F-5450-110803 DATED 11/12/07. REMOVED AND REPLACED FWD I/B SHIM WITH NEW SHIM. REMOVED AND REPLACED AFT I/B SHIM WITH NEW SHIM PER STJan 4, 2008 · N903FD · Boeing 7572B7 · Nacelle/Pylon Miscellaneous StructureSDR 07FDEA05000Floor Support · corrodedSHORT SECTION OF FLOOR SUPPORT BS 333.45 I/B OF LBL 45.5 HAS CORROSION. REMOVED CORRODED SUPPORT BEAM AT STA 333 - 335, LBL 45.5 IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG 101. FABRICATED NEW SUPPODec 4, 2007 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
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