N996FD

Service difficulty reports · 117

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 = 'N996FD' 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 FDEA201107232922Skin · crackedRT APU DOOR AFT EDGE HAS CRACK IN SKIN ON EDGE. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 52-40-02, DET VI, FIG 101. REMOVED DAMAGE AREA IAW SRM 51-10-02. FABED DOUBLER IAW SRM 52-40-01, BATCH NR 2061447, PN 2024-T3. LOCATED & DRILLED DOUBLER IAW SRMJul 23, 2011 · N996FD · Boeing 7572Q8 · Auxiliary Power Unit (APU) DoorsSDR FDEA201107232919Frame · damagedUPPER LOBE STRUCTURE FRAME HAS DOUBLED DRILLED HOLE AT STA 800 BET. STR 2L & STR 3L. FOUND TO BE OUT OF LIMITS IAW SRM-51-40-06, BETWEEN STR 2L-3L, CUT OUT DAMAGED FRAME AND INSTALLED SPLICES AND FRAME IAW SRM-53-00-07, REPAIR 3. MAJOR REPAIR "CAT B"Jul 23, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201107192808Seat Track · damagedMAIN DECK SEAT TRACK AT LBL 25 HAS BROKEN OFF LUGS AT STA 454. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I, REMOVED SEAT TRACK STA 440- 470 LBL 25 IAW SRM 53-40-02, FABRICATED REPAIR ANGLES IAW SRM 53-00-52 FIG 201. LOCATED AND DRILLED REPJul 19, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107132682Floorbeam · corrodedFLOORBEAM TEE BETWEEN RBL 41-62 BS 324 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-08. ORIGINAL MATERIAL .0125 AFTER REWORK .110. R & R TEE IAW SRM 51-40-01. MAJOR REPAIR.Jul 13, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201107132686Seat Track · gougedGOUGE SEAT TRACK BETWEEN STA 1200-1220 LT SIDE OF CABIN INBD TRACK FOUND SEAT TRACK AT STA 1200-1220, LBL 24 OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL I. FABRICATED NEW SEAT TRACK WITH PN BAC1520-792. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02Jul 13, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107132677Seat Track · gougedSEAT TRACK BETWEEN STA 418 AND 440 GOUGED MAIN CABIN RBL24. R & R SEAT TRACK IAW SRM-53-00-52, DETAIL I, FIG 101 FOUND TO BE OUT OF LIMITS L=2.8 W=1.3 D=0.025 IAW SRM-5300-52, DETAIL I, FIG 101.Jul 13, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107122666Seat Track · gougedMAIN DECK SEAT TRACK LBL 45 HAS GOUGED LUG BETWEEN BS 418-440. BLENDED GOUGE, FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-52, FIG 101, DETAIL 1. R & R SEAT TRACK IAW-SRM-51-40-025.Jul 12, 2011 · N996FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107122665Frame · gougedAFT PIT FRAME 1340 LT DEEP GOUGE IN FRAME BETWEEN STRINGERS L25-26L. REMOVED GOUGE IAW SRM 51-10-02. ORIGINGAL MATERIAL .071 REMAINING .050 FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, ALLOWABLE DAMAGE 2. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.Jul 12, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201107122663Frame Splice · gougedAFT CARGO BAY FRAME, BS 1340 SPLICE. DEEP GOUGE BETWEEN STRINGERS 23L AND 24L. REMOVED GOUGE IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101. R & R SPLICE IAW SRM 51-40-02. MAJOR REPAIR.Jul 12, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201107012528Floorbeam · corrodedSTA 345, FLOORBEAM, RBL 60 CORRODED AND PREVIOUS BLEND ON UPPER FLANGE. REMOVED DAMAGED AREA FROM UPPER FRAME STA 345 RBL 52- RBL 70 IAW SRM 51-10-02 AND SRM 53-00-51 FIG 201. DRILLED AND LOCATED HOLES FOR REPAIR IAW SRM 51-40-05. DRILLED AND LOCATED REPAIJul 1, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201106242411Frame · gougedAFT PIT FRAME RT STA 1320 BETWEEN STR 25R AND STR 27R, GOUGED. REMOVED GOUGE IAW SRM 51-10-02 ORIG MAT .071 REMAINING = .061, OUT OF LIMITS IAW SRM 53-00-07, FIG 101 DETAIL I A. D.2. R & R FRAME AT STA 1320 STR'S 25L- 25R IAW SRM 51-40-02. MAJOR REPAIR.Jun 24, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201106232402Skin · dentedRT WING NR 6 SLAT HAS NUMEROUS DENTS ALONG NOSE SKIN.Jun 23, 2011 · N996FD · Boeing 7572Q8 · Leading Edge DevicesSDR FDEA201106222388Frame · corrodedAFT PIT 1460 FRAME, NUMEROUS AREAS ON FRAME CORRODED, TOTAL OF NINE AREAS. REMOVED CORROSION IAW SRM SRM 53-00-07 FIG 101 ORIGINAL THICKNESS .067" AFTER CORROSION REMOVED .055" FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL V. REMOVED AND REPLACED FRJun 22, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201106152275Floor Support · corrodedMAIN CABIN FLOOR SUPPORT, LBL 45 HAS CORROSION AT STA 377.7.Jun 15, 2011 · N996FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201106152274Floorbeam · corrodedSTA 377, RBL 4 TO RBL 12 FLOORBEAM CORRODED MAIN CABIN. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM-53-00-51, FIG 101, DETAIL III ORIGINAL. MATERIAL .125 REMOVED .016, REMAINING MATERIAL .109. R & R FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.Jun 15, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201106152273Floorbeam · corrodedSTA 395, RBL 54 FLOORBEAM CORRODED MAIN CABIN. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED FLOORBEAM IAW SRM 51-40-02. DRILLED AND LOCATED NEW FLOORBEAM IAW SRM 53-10-51 DETAIL II AND SRM 51-40-05.Jun 15, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201106152272Floorbeam · corrodedSTA 365, BL 0 TO RBL 17 CORROSION ON FLOORBEAM MAIN CABIN. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .125 MATERIAL REMOVED .015 REMAINING MAT .110. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED FLOORBEAM IAW SRM 51-40Jun 15, 2011 · N996FD · Boeing 7572Q8 · Fuselage Main, Floor Beam
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