N937FD

Service difficulty reports · 178

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 = 'N937FD' 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 FDEA201004281388Fitting · corrodedFWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 520, STA 540 AND STA 560 FOUND WITH CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.025" AT STA 520 LT, 0.035" AT STA 540 Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281387Fitting · corrodedAFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1300, STA 1320, STA 1360 AND STA 1380 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIAL REMOVED 0.021" STA 1300, STA 1320, STA 1340 AND STA 1360 RT ORIGINAL THICKNESS 0.180" FOUND WITHIN LIMIT IAW E.A.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281386Fitting · corrodedAFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1540, STA 1560, STA 1580 AND STA 1600 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIAL REMOVED 0.021" AT STA 1540, STA 1560, STA 1580 AND STA 1600 RT ORIGINAL THICKNESS 0.180" FOUND WITHIN LIMIT IAW Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281385Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1400, STA 1420, STA 1480, STA 1500 AND STA 1520 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIALS REMOVED 0.025" AND STA 1400, STA 1420, STA 1480, STA 1500, AND STA 1520 LT, MATERIAL REMAINED 0.155, Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004281384Fitting · corrodedAFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1220, STA 1240, STA 1260 AND STA 1260 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIAL REMOVED 0.030" AT STA 1220 RT, STA 1240 RT, STA 1260 RT AND STA 1280 RT ORIGINAL THICKNESS 0.180" FOUND WITHIN LIApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281383Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1220, STA 1240, STA 1260 AND STA 1300 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIAL REMOVED 0.022" AT STA 1220, STA 1240, STA 1260 AND STA 1300 LT ORIGINAL THICKNESS 0.180" FOUND WITHIN LIMIT IAW EApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281381Fitting · corrodedFWD CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 760, STA 780 AND STA 840. FOUND WITH CORROSION. REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.036" AT STA 760 RT, 0.025" AT STA 780 RT ANApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004281380Fitting · corrodedFWD CARGO COMPT, RT CARGO NET TIE-DOWN FITTINGS AT STA 680, STA 720 AND STA 740 FOUND WITH CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.022" AT STA 680 RT, 0.032" AT STA 720Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281379Fitting · corrodedAFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT BS 1460, 1480 AND 1500 FOUND WITH CORROSION. REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.020" AT STA 1460, STA 1480, STA 1500 AND STA 1520 RApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281378Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS STA 1320, STA 1360 AND STA 1380. (QTY2) FOUND WITH CORROSION. TIE DOWN FITTING FOUND DEEPLY CORRODED EXCEEDED LIMIT AS PER SRM 53-0053 FIG. 101, REV. 99. CORRODED PLATE AT STA 1380 R & R WITH NEW PLAT 451N5700-8Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004281374Transition Panel · corrodedAFT CARGO COMPT RT TRANSITION SIDE PANEL UNDER SURFACE AT STA 1440 FOUND WITH CORROSION. CORRODED TRANSITION PANEL AT STA 1440 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281373Panel · corrodedAFT CARGO COMPT LT TRANSITION SIDE PANEL AT STA 1445-1530 FOUND CORRODED. PANEL R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281372Panel · corrodedAFT CARGO COMPT RT TRANSITION SIDE PANEL AT STA 1440-1530 FOUND CORRODED. PANEL R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281371Panel · corrodedAFT CARGO COMPARTMENT RT TRANSITION SIDE PANEL AT STA 1310-1380 FOUND CORRODED. PANEL R & R IAW SRM 51-40- 02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281370Support · crackedNLG WHEEL WELL LT SEAL RETAINER SUPPORT PLATE AT STA 390 CRACKED. CRACKED RETAINER SUPPORT PLATE AT STA 390 R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281369Panel · corrodedAFT CARGO COMPARTMENT LT TRANSITION SIDE PANEL AT STA 1200-1300 CORRODED. CORRODED TRANSITION PANEL BETWEEN STA 1200 AND STA 1310, R & R IAW SRM 51-40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004271366Fitting · corrodedFWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 580, ST 660 AND STA 720 FOUND WITH CORROSION. FWD CARGO BS LT CARGO NET TIE-DOWN FITTINGS AT BS 580, 660 & 720. FOUND CORRODED. REMOVED & TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. MATERIAL REMOVEDApr 27, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004211263Panel · corrodedAFT CARGO COMPARTMENT LT TRANSITION PANEL AT STA 1200-1310 FOUND CORRODED. CORRODED AFT CARGO COMPARTMENT TRANSITION PANEL FROM LT STA 1200 TO STA 1310. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 21, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004211262Frame · corrodedFWD LT WING-TO-BODY FAIRING ATTACH FRAME WITH LIGHT CORROSION AT BS 860 TO BS 900, LBL 7. CORRODED FRAME FROM BS 860 TO BS 900 AT LBL 7. R & R IAW SRM 51- 40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 21, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004201256Skin · corrodedAFT RT CREASE BEAM PANEL UPPER SKIN SURFACE CORROSION ADJACENT TO CORNER FITTING AT BS 1720, RBL 45.50. CORRODED BEAM PANEL AT BS 1720 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 20, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Plate/SkinSDR FDEA201004191253Floorbeam · corrodedCABIN AFT FLOORBEAM WITH CORROSION AT UPPER CHORD SURFACE AND SURROUNDING FASTENER HOLES AREA AT BS 1661, BETWEEN RBL 58 AND LBL 58. CORRODED BEAM AT BS 1661 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 19, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201004191223Floor Support · corrodedCABIN AFT FLOOR INTERCOSTAL UPPER CAP WITH CORROSION AT FASTENER HOLES AREA BETWEEN BS 1661 AND BS 1681, AT RBL 0. R & R AS PER SRM 51-40-02, REV 99. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Apr 19, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004191222Floor Support · corrodedCABIN AFT FLOOR INTERCOSTAL WEB UPPER CAP WITH CORROSION AT FASTENER HOLES AREA BETWEEN BS 1661 TO BS 1681, AT RBL9. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 19, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004191221Floor Skin · corrodedCABIN AFT LT DECK PLATE UPPER SURFACE WITH CORROSION AT BS 1681 TO BS 1720, BETWEEN BL0 AND LBL 58. CORRODED DECK PLATE FROM BS 1681 TO BS 1720 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 19, 2010 · N937FD · Boeing 7572T7 · Fuselage Floor PanelSDR FDEA201004151200Panel · corrodedNR 1 ENGINE NACELLE STRUT ACCESS PANEL NR 433GR CUTOUT AREA AT STA 120, INTERNAL SURFACE CORROSION. CORRODED PANEL NR 433GR R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Apr 15, 2010 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/SkinSDR FDEA201004081099Floorbeam · corrodedTOP OF FLOORBEAM HAS CORROSION AT STA 377, BL 0 TO LBL 22. FLOORBEAM AT STA 377, LBL 62 TO RBL 62 FABRICATED IAW DWG 141N5123, SHEET 1, REV 1, IAW GMM 7-0-1001 REV. 110. FLOORBEAM R & R IAW SRM 51-40-02 REV 99. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-Apr 8, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201004081098Floorbeam · corrodedFUSELAGE INTERIOR CABIN AFT FLOORBEAM WITH CORROSION AT UPPER CHORD SURFACE AND SURROUNDING FASTENER HOLES AREA AT BS 1640, BETWEEN RBL 24.75 AND LBL 24.75. CORRODED FLOORBEAM R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 8, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201004051059Panel · crackedWING L/E SLAT NR2 AFT INBD PANEL HAS A CRACK WITH STOP HOLE. CRACK STARTS FROM L/B MAIN TRACK ATTACHMENT AREA. ADJUSTMENT AND OPS TEST OF THE NR 2 L/E SLAT AFTER INSTALLATION CARRIED OUT AND FOUND GOOD IAW AMM 27-81-02, REV 5.2. THIS REPAIR IS CLASSIFIED ASApr 5, 2010 · N937FD · Boeing 7572T7 · Leading Edge Devices
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