N166FE, cancelled Aug 21, 2007
Service difficulty reports · 71
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 = 'N166FE' AND deregistration_id = 'N166FE-2007-08-21' 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.
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 = 'N166FE' AND deregistration_id = 'N166FE-2007-08-21' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 04FDEA03016Stringer · damagedSTR L23 DAMAGED AT BS 376 TO 388. REPAIRED PER SRM 53-10-3.SDR 04FDEA03014Skin · gougedAFT CARGO DOOR EXTERNAL SKIN GOUGED AT LWR EDGE, 17 INCH FROM AFT EDGE. REPAIRED SKIN IAW SRM 52-00-3.SDR 03FDEA00997Tripler · wornMDIS 166 53-30 0004746 26JUN03 BFM CLOSER COMPLY WITH EA NR 7-5330-70966 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR (AD 2002-16-19). FACT 27JUN03 14:10 BFM R COMPLIED WITH EA NR 7-5330-70966, FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR (AD2002-16-19).SDR 00FDEA00073Switch · out of adjustAFT GEAR RETRACTION, LMG DOOR RED AND AMBER LIGHT DID NOT EXTINGUISH. RECYCLED THE GEAR AND LIGHT EXT IND ALL GEAR DOOR UP. ADJUSTED LANDING GEAR DOOR SWITCH PER 727-100 MM 32-62-011-4. OPER CK NORM.SDR 98FDEA00578Bulb · failedSHORT FINAL RUNWAY 36R MEM, NORM GEAR EXT CREW OBSERVED NO DOWN GROUND IND ON LEFT MAIN GEAR. NOSE AND R/M IND DOWN NORM. CAPT PERFORMED GO-AROUND AFTER RECYCLING GEAR TO NO AVAIL. DID MAN GEAR EXT CKLIST AND GOT VISUAL CONFIRMATION FROM TOWER. LANDED, PINSDR 97FDEA00656Skin · corrodedNR 0291 015 CORROSION ON UPPER SURFACE OF WING SKIN BS 850, LBL 82, WL 200. COMPLIED WITH EA 7-5730-35048.SDR 97FDEA00655Keel Beam · corrodedCORROSION (C53-113-01,1) ON RT KEEL BEAM BETWEEN BS 620 TO 640, WL 148. *S/D* REPAIRED RT KEEL BEAM BETWEEN BS 620 TO 640, WL 148 PER FED-EX EA 7-5310-35067.SDR 97FDEA00639Clip · corrodedNR 0165 013 CORROSION (C53-224-05) ON T-CLIP, FWD SIDE, RBL 69, BS 760, WL 205. FOUND T CLIP TO BE CORRODED OUT OF LIMITS ON BS 760, WL 205, RBL 69. FABRICATED T CLIP AND INSTALLED IAW FED-EX SRM 53-30-5, 51-10-2, M/M 51-20-151, 51-20-21.SDR 97FDEA00638Frame · crackedCRACK ON UPPER FLANGE OF FRAME BS 1050, RBL 9, WL 155 ON PREVIOUS REPAIR, CRACK EXTENDS .5 BEYOND STOP DRILL HOLE. *S/D* CUT OUT DAMAGED FRAME SECTION AND REPAIRED PER FED-EX SRM 53-40-3.SDR 97FDEA00636Access Panel · corrodedNR 0167 012 CORROSION (C53-132-02(1)) ON 870 CENTER WING ACCESS PANEL, BS 870, LBL 4, WL 170. (INTERNAL TANK ACCESS IS REQUIRED.) REMOVED .020 CORROSION IN A 2.3 BY 11.9 AREA ORIGINAL THICKNESS .050 OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED SDR 97FDEA00630Hinge · corrodedCORROSION ON NR 1 K-FLAP CENTER HINGE LUG ON AIRCRAFT SIDE UNDER BOTH I/B AND O/B LUG SCREWS. REMOVED AND REPLACED NR 1 K-FLAP CENTER HINGE FITTING.SDR 97FDEA00610Flap · delaminatedLT WING I/B MIDFLAP T/E WEDGE DELAMINATED FROM 18 TO 26 FROM I/B END. *S/D* REPAIRED LT WING I/B MIDFLAP T/E WEDGE IAW FED-EX SRM 51-40-06 AND 51-30-02.SDR 97FDEA00609Stringer · corrodedCORROSION (C53-113-01,2) IN STR 27, RIGHT BS 970 TO 1035. *S/D* REMOVED CORROSION IN STR 27 RT, BS 970 TO 1035. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED STR 27 RT, BS 970 TO 1035 PER FED-EX SRM 51-30-2, AND 51-10-1.SDR 97FDEA00607Stringer · corrodedCORROSION (C53-113-01, 2) IN STR 30, WL 148, BS 970 TO 1080. *S/D* REMOVED CORROSION IN STR 30, WL 148, BS 970 TO 1080. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED STR 30, WL 148, BS 970 TO 1080 PER FED-EX SRM 53-10-3, 51-30-2, ASDR 97FDEA00606Spar Chord · corrodedCORROSION (C53-132-02- 1/2) WING CENTER SECTION LOWER FRONT SPAR CHORD BS 740, RBL 10 AND RBL 26 TO 30, WL 164.SDR 97FDEA00605Chord · corrodedCORROSION (C53-132-02 1/2) WING CENTER SECTION UPPER REAR SPAR CHORD BS 870, LBL 70 TO RBL 70, WL 188.SDR 97FDEA00604Chord · corrodedCORROSION (C53-132-02 1/2) WING CENTER SECTION LOWER REAR SPAR CHORD VERTICAL LEG BS 870, LBL 10 TO RBL 10, WL 164.SDR 97FDEA00603Angle · corrodedCORROSION (C53-224-05) ON RT 70.5 PREVIOUS REPAIR ANGLE, BS 754 TO 760, RBL 70.5, WL 204. *S/D* CORROSION ON ANGLE, BS 754 TO 760, OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED ANGLE PER FED-EX SRM 51-10-1.SDR 97FDEA00593Beam · corrodedNR 0308 003 CORROSION (C55-300-10-2) RT HORIZONTAL STAB UPPER T/E BEAM AT APPROX ELEV STA 147.5 (IN BALANCE BAY NR 4).SDR 97FDEA00585Flap · delaminatedLEFT WING O/B MIDFLAP T/E WEDGE DELAMINATED IN SEVERAL AREAS FROM 17 TO 141 FROM I/B END. *S/D* REMOVED AND REPLACED LEFT WING OUTBOARD MIDFLAP IAW FED-EX M/M 27-51-11.SDR 97FDEA00584Flap · delaminatedRIGHT WING O/B MIDFLAP T/E WEDGE DELAMINATED FROM 66 TO 72 INCHES AND 115 TO 124 INCHES FROM O/B END. *S/D* REMOVED AND REPLACED RIGHT WING O/B MIDFLAP IAW FED M/M 27-51-13, DUE TO CORROSION ON MIDFLAP FRONT SPAR UPPER SURFACE.
Back to N166FE, cancelled Aug 21, 2007