N994FD

Service difficulty reports · 72

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 = 'N994FD' 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 FDEA201009213598Shear Tie · corrodedSTA 1460 FRAME SHEAR-TIE BETWEEN STRINGER 26L AND 27L CORRODED. REPLACED SHEAR TIE, FABRICATED ON TRAVELER T10/850999, IAW SRM 51-40-02/ DWG 140N2002. SHEAR TIE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL 2, FIG 101. CORROSION REWORK; L=1.74",W=.510"Sep 21, 2010 · N994FD · Boeing 75723A · Fuselage Internal Mounting StructureSDR FDEA201009203561Gate · corrodedL2 DOOR LOWER GATE EDGE HAS CORROSION L2 DOOR LOWER GATE OUT OF LIMITS MAX DEPTH MEASURED 0.15 IAW SRM 52-10-02, FIG 101, DETAIL IV SHEET 4 OF 8 PAGE 104. REPLACED GATE IAW SRM 51-10-02. MAJOR REPAIRSep 20, 2010 · N994FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201009173531Floorbeam · corrodedFLOORBEAM STA 377, BL 0, RBL 10, UPPER TEE CORRODED. REMOVED CORROSION PER SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3. REMOVED DAMAGED AREA OF THE FLOORBEAM PER SRM 53-00- 51. FABRICATED NEW TEE AND REPAIRSep 17, 2010 · N994FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA201009163506Skin · dentedPREVIOUS SKIN DENT AT BS 668, S19R. EVALUATED DENT L=1.3 W = 1.0 D= .033 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO SKIN SPLICE. CUT OUT DAMAGE & FABRICATED DOUBLER AND STRUCTURAL FILLER FROM .063 2024-T3 BATCH 1862687 AND SHIM .032 2024 - T3, BATCH Sep 16, 2010 · N994FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR FDEA201009143385Gate · corrodedR 1 DOOR LOWER GATE HAS CORROSION ALONG EDGE R1 DOOR GATE FOUND OUT OF LIMITS PER SRM 52-10-02, FIG.201, DETAIL 4, SH. 4 OF 8; MEASURED .200" LOSS. REMOVED AND REPLACED R1 DOOR LOWER GATE ASSY PER SRM 51-10-02 / 51-40-02. MAJOR REPAIR CAT. "A".Sep 14, 2010 · N994FD · Boeing 757223 · Passenger/Crew DoorsSDR FDEA201009113344Skin · misrepairedRT APU DOOR EXISTING FLUSH REPAIR AT BS 1957, STR 29R DOES NOT COMPLY WITH KNOWN APPROVED DATA. REMOVED EXISTING REPAIR IAW SRM 51-40-02. REPAIRED APU DOOR SKIN, RT, IAW SRM 52-40-01, FIG 201, P205, REPAIR NR 5. CAT "A" MAJOR REPAIR, NO REPETITIVE INSP REQUISep 11, 2010 · N994FD · Boeing 75723A · Auxiliary Power Unit (APU) DoorsSDR FDEA201009083317Fitting · misalignedAT STA 1640 LT THE 657N3161-11 FITTING HAS 2EA EXISTING SED FASTENERS AT LWR, INBD, END OF FITTING ALSO 5EA, EXISTING FASTENERS WHERE DWG SHOWS 4EA, AT LWR END OF FITTING APPROX WL 202 TO WL 208 AND JUST INBD OF THAT LOCATION 5EA EXISTING FASTENERS AT INBD, EDSep 8, 2010 · N994FD · Boeing 75723A · Fuselage Main, Attach FittingsSDR FDEA201009073309Fitting · corrodedR1 DOOR FWD LOWER TORQUE TUBE ROLLER FITTING HAS PITTING CORROSION. R & R FWD LOWER TORQUE TUBE CAM ROLLER FITTING IAW CMM 52-11-05. MAJOR REPAIR.Sep 7, 2010 · N994FD · Boeing 757223 · Passenger/Crew DoorsSDR FDEA201008313207Gate · corrodedR2 DOOR LOWER GATE HAS CORROSION ALONG EDGE CHECKED LIMITS ON CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-02, FIG.101, DETAIL 4. MEASURED .150" MATL. LOSS. REMOVED AND REPLACED R2 DOOR GATE, LOWER, P/N 143N6106-26, BATCH 0001899033,PER SRM 51-10-02 Aug 31, 2010 · N994FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201008313204Skin · wornLT WING- INBD MAIN FLAP L/E, OTBD SIDE HAS 3 WORN SECTIONS WITH TOTAL LENGTH APPROX 20 INCHES. COMPLIED WITH EA F-5750-141199, CLEANED AREAS IAW SRM 51-10-02, OUT OF LIMITS, IAW SRM 57-53-01, FIG 101, SHEET 6. DAMAGE REPAIRED IAW SRM 57-53-01, LOCATED & DRILLAug 31, 2010 · N994FD · Boeing 75723A · Trailing Edge FlapsSDR FDEA201008313203Floorbeam · mislocatedEXISTING FASTENER HOLE AT STA 440, BL-0, AFTSIDE OF FLOORBEAM WILL BE IN THE RADIUS ON LT SIDE OF L-0 SEAT TRACK CROWN IF DRILLED. AT STA 440, BL-0 EXISTING HOLE PLUGED AND RELOCATED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE MOD W/C NR 118350425BZAug 31, 2010 · N994FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA201008303196Floor Support · corrodedAFT CARGO FLOOR SUPPORT RBL 7.55 BETWEEN STA 1500 TO STA 1640 NUMEROUS BROKEN SCREWS, NUT PLATES AND ATTACHING RIVETS. REMOVED CORROSION ON FLOOR SUPPORT RBL 7.55, STA. 1500 - 1640 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL V. ORIG MATERIAL .063" MAT LOAug 30, 2010 · N994FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA201008263155Gate · corrodedL-4 DOOR LOWER GATE CORRODED ALONG EDGE AND FWD POCKET INNER SURFACE. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG. 101 DETAIL IV. REMOVED LOWER GATE FROM L-4 DOOR IAW SRM 51-40-02. REMOVED SEAL FROM GATE ASSEMBLY IAW AMM 52-09-01. RECEIVED NEW GATE ASSEAug 26, 2010 · N994FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201008263148Gate · corrodedL-2 DOOR UPPER GATE, AFT POCKETS INNER SURFACE CORRODED. REMOVED CORROSION ON L-2 DOOR UPPER GATE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02. REMOVED SEAL FOR ACCESS IAW AMM 52-09-01. REMOVED HINGE FOR ACCESS IAW SRM 51-40-02. RECEIVED NAug 26, 2010 · N994FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA201008253134Frame · gougedMAIN CABIN, FRAME BS 1280 S10-13R HAVE GOUGES. REMOVED DAMAGE AT STRG 11R- 13R IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II, REMOVED DAMAGE FRAME FROM STRG 11-13R, STOP 4(B) HFEC REWORK AREA IAW NTM 51--00-19 PH 6. NO CRACKAug 25, 2010 · N994FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA201008253136Gate · corrodedR4 DOOR, LOWER GATE EDGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02; ORIGINAL MATERIAL: .150", LOSS: .102", REMAINING: .048", FOUND OUT OF LIMITS IAW SRM 52-10-02, DETAIL 7, P 107, FIG 101. REMOVED DOOR GATE ON R4 DOOR IAW SRM 51-40-02. INSTALLED NEAug 25, 2010 · N994FD · Boeing 757223 · Passenger/Crew DoorsSDR FDEA201008213088Floorbeam · corrodedSTA 365.25 FLOORBEAM HAS CORROSION ON TOP OF BEAM AND UNDERNEATH TOP OF BEAM AT SEVERAL LOCATIONS RT OF BL 0. REMOVED CORROSION IAW SRM 51-10-02. OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. REMOVED DAMAGED FROM LBL 13-RBL 68.6. FABRICATED REPAIR PARTAug 21, 2010 · N994FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA201008203057Skin · dentedAT STA 1605 STR 26L- PROTRUDING DENT, OTWD. FOUND DENT TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101,DETAIL 3,DUE TO BEING LESS THAN 3" FROM A SKIN SPLICE. ACCOMPLISHED A FUSELAGE SKIN DOUBLER REPAIR, BS 1605, BETWEEN S26L/27L, PER SRM 53-00-01, REPAIR 7. DAug 20, 2010 · N994FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA201008193052Seat Track · gougedSEAT TRACK STA.418-440 RBL.45, GOUGED. R & R SEAT TRACK BS 418-440, RBL 45, IAW SRM 51-40-02. BLENDED AREAS IAW SRM 53-00-52, FIG 101; ORIGINAL MATERIAL: .080", AFTER REWORK: .035", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVED SEAT Aug 19, 2010 · N994FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008193051Seat Track · gougedSEAT TRACK STA 418-440 RBL-24 GOUGED R & R SEAT TRACK, BS 418-440,RBL 24, SRM 51-40-02. BLENDED AREAS IAW SRM 53-00-52, FIG.101; ORIGINAL MATERIAL: .080", AFTER REWORK; .040", ON THE FLANGE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVEAug 19, 2010 · N994FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008143002Skin · dentedAT STA.1640-1660 BETWEEN STR 27 & 28R, 2 EA. PROTRUDING DENTS. OUTWARD. CONVEX CHECKED LIMITS; DENT NR 1 L=.50", W=.50", D=.043", A/Y=11 / DENT NR 2 L=.50", W= .50", D= .035", A/Y=14. FOUND BOTH DENTS TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101. REPAIRED Aug 14, 2010 · N994FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR FDEA201007292725Frame · dentedSTA 1500 FRAME BETWEEN STR 26L AND 27L DENTED, GOUGED AND CORRODED. REMOVED CORROSION PER SRM 51-10-02; L=3", W=1", D=.004", WITHIN LIMITS PER SRM 53-00- 53, FIG.101. GOUGE AREA; L=1.2",W=.01", D=.003", WITHIN LIMITS PER SRM 53-00-53, FIG.101; DENT OUT OF Jul 29, 2010 · N994FD · Boeing 75723A · Fuselage Main, Frame
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