Boeing 747-211B

Service difficulty reports · 18

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '747211B'
  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 UPS06446935Floor Support · corrodedBS 2250 TO 2280 RBL80 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.025" BY 1.5" BY 3" EXCEED SRM LIMIT. BS 2220-2290 RT O/B AREA FLOOR SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.May 13, 2006 · N521UP · Boeing 747211B · Fuselage Miscellaneous StructureSDR UPS06446924Cargo Track · corrodedINSPECTION TYPE:C U/D BS560 RBL28 TIE DOWN TRACK FOUND CORROSION. CORROSION BLEND OUT 0.036" BY 1/2" BY 4" EXCEED SRM LIMIT. TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG9 AND INSTALLED AS PER SRM 51-30-02 JUST AT RBL28 BTN BS540 ANI BS570. P/N BAC1520-1567-May 13, 2006 · N521UP · Boeing 747211B · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446934Seat Track · corrodedBS 750 TO 840 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.034" BY 1/2" BY 2" EXCEED SRM LIMIT. BS 750 TO BS 850 RBL11 TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.May 12, 2006 · N521UP · Boeing 747211B · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446915Cargo Track · corrodedTIE DOWN TRACK BS480-520 LBL63-68 CORRODED. CORROSION BLEND OUT 0.030" BY 1/2" BY 3" EXCEED SRM LIMIT. TIE DOWN TRACK REPAIED AT BS480-530 LBL63-68 AS PER SRM 53-10-05 FIG4.May 11, 2006 · N521UP · Boeing 747211B · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446913Floorbeam · corrodedFLOORBEAM UPPER CHORD BS 480 LBL 33-63 CORRODED. CORROSION BLEND OUT 0.034" BY 1" BY 20" EXCEED SRM LIMIT. BS 480 BL0 TO LBL78 FLOORBEAM UPPER CHORD. REPAIRED AS PER SRM 53-10-07 FIG 10.May 11, 2006 · N521UP · Boeing 747211B · Fuselage Main, Floor BeamSDR UPS06446920Hinge Bracket · crackedBS 2598 B/H STABILIZER HINGE SUPPORT FITTING AREA 1EA HOLE CORROSION CRACK AT FRAME SUPPORT (4TH LAYER FROM AFT) CRACK LENGTH 0.030". BOTH HOLE REWORKED TO 0.500" AS PER EO B747-5310-14056 HOLE CONFIRMED CRACK FREE.May 10, 2006 · N521UP · Boeing 747211B · Horizontal Stabilizer StructureSDR UPS06446919Support Fitting · crackedBS2598 B/H STABILIZER HINGE SUPPORT FITTING AREA FOUND 1 HOLE CRACK AT FRAME SUPPORT (4TH LAYER FROM AFT) CRACK LENGTH 0.030". BOLT HOLE REWORKED TO 0.500" AS PER EO B747-5310-14056 AND HOLE CONFIRMED CRACK FREE.May 10, 2006 · N521UP · Boeing 747211B · Fuselage Main, Attach FittingsSDR UPS06446932Stiffener · crackedINSPECTION TYPE:C NWW LT SIDE PANEL BS260-280 WL 180 STIFFENER RADIUS AREA. FOUND CRACK APP 1 3/8" LONG, STIFFENER. REPLACED AS PER SRM 51-10-01 PG9 AND INSTALLED AS PER SRM 51-30-02.May 9, 2006 · N521UP · Boeing 747211B · Fuselage Main, StructureSDR UPS06446927Stiffener · crackedNWW RT SIDE PANEL BS 300-320 WL 150 STIFFENER RADIUS AREA FOUND INTERMITTENT CRACKS, CRACK LENGTH : 1/4" - 1/2". STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 9, 2006 · N521UP · Boeing 747211B · Fuselage Miscellaneous StructureSDR UPS06446926Stiffener · crackedNWW RT SIDE PANEL BS 280-300 WL 170 STIFFENER RADIUS AREA FOUND INTERMITTENT CRACKS, CRACK LENGTH 1/4" - 3/8". STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 9, 2006 · N521UP · Boeing 747211B · Fuselage Miscellaneous StructureSDR UPS06446925Stiffener · crackedNWW RT SIDE PANEL BS300-320 WL170 STIFFENER RADIUS AREA FOUND INTERMITTENT CRACKS, CRACK LENGTH 1/4-3/8. STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 9, 2006 · N521UP · Boeing 747211B · Fuselage Miscellaneous StructureSDR UPS06446916Seat Track · corrodedBS 480-520 LBL46 SEAT TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.55" BY 1/2" BY 1.5" EXCEED SRM LIMIT. BS480-530 LBL46 SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 9, 2006 · N521UP · Boeing 747211B · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446931Door Frame · crackedR3 DOOR AFT FRAME UPPER CORNER CRACKED, CRACK LENGTH 1 INCH. R3 DOOR AFT FRAME UPPER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.May 7, 2006 · N521UP · Boeing 747211B · Passenger/Crew DoorsSDR UPS06446914Cargo Track · corrodedBS 420-440 RBL88 TIE DOWN TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 1/2" BY 2" EXCEED SRM LIMIT. BS410-460 RBL88 TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 7, 2006 · N521UP · Boeing 747211B · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446933Stringer · corrodedRT LOWER FUSELAGE EXTERNAL SKIN SURFACE FOUND BILGE UP AT STA 2160 TO STA 2170 STR 45R. BULK CARGO BS 2150 TO BS 2180 S45R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.May 5, 2006 · N521UP · Boeing 747211B · Fuselage Main, Longeron/StringerSDR UPS06446921Frame · crackedLT BS 2231 FRAME INNER FLANGE BETWEEN S24L AND S25L FOUND 1 HOLE CRACK AT FRAME STRAP CRACK LENGTH 1/16". BS 2231 LT FRAME ATTACH STRAP REPAIRED BETWEEN STR 24L TO 26L AS PER SRM 53-10-04 FIG 15. CONTINUED INSPECTION IS REQUIRED AS PER SRM 53-10-04 FIG 115 TMay 5, 2006 · N521UP · Boeing 747211B · Fuselage Main, FrameSDR UPS06446917Stiffener · crackedNWW TOP PANEL BS280-300 RBL 10 STIFFENER RADIUS AREA FOUND CRACK APP 3/4". NWW TOP PANEL BS280-300 RBL10 STIFFENER REPLACED AS PER SRM 51-10-01 PG9 AND INSTALLED AS PER SRM 51-30-02.May 5, 2006 · N521UP · Boeing 747211B · Fuselage Main, StructureSDR UPS04443095Frame · crackedINSPECTION TYPE: C, M/D: BS 400 STR 15L FRAME CRACKED. M/D- BS 400 STR 15L CRACKED FRAME REPAIRED AS PER HX RS R53-12-35187 & UPS EO B747-5310-20990-A.Aug 16, 2004 · N520UP · Boeing 747211B · Fuselage Main, Frame
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