Boeing 747-200

Service difficulty reports · 651

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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 = '747200'
  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 P5CA0300919Panel · delaminatedLT IB MID FLAP OF DELAMINATION AT OUT MID FLT PANEL. CORRECTIVE ACTION TAKEN: PANEL REPLACED SRM 51-10-01 AND 51-30-02.Aug 19, 2003 · N524UP · Boeing 747200 · Trailing Edge FlapsSDR P5CA03009023Structure · crackedNR 4 PYLON SLOT CUT OUT HAS APPROX .5000 INCH CRACK AT THE IB UPPER AFT CORNER. CORRECTIVE ACTION TAKEN: CRACK TRIMMED IAW SECT 3 OF 54-2034. NO CRACK VISIBLE AFTER TRIM OUT. EXTERNAL DOUBLER INSTALLED ON THE INBND SIDE OF PYLON IAW SB 54-2034.Aug 19, 2003 · N524UP · Boeing 747200 · Nacelle/Pylon Miscellaneous StructureSDR P5CA0300920Panel · delaminatedLT INBND MID FLAP DELAMINATION AT MID UPPER FLT PNL. CORRECTIVE ACTION TAKEN: DELAMINATION PNL - REPLACED- SRM 51-30-02Aug 19, 2003 · N524UP · Boeing 747200 · Trailing Edge FlapsSDR P5CA0300922Panel · delaminatedRT IB MID FLAP WITH SIGNS OF DELAMINATION AT MID LWR FLT PANEL. CORRECTIVE ACTION TAKEN: DELAMINATION PANEL REPLACED SRM 51-10-01 / 51-30-02 MM 51-24-11Aug 19, 2003 · N524UP · Boeing 747200 · Trailing Edge FlapsSDR P5CA0300932Panel · delaminatedRT WING INBOARD TRAILING EDGE FLAP MID- FLAP PANEL DELAMINATED. REPAIRED BY BOUNDING NEW SKIN.Aug 16, 2003 · N524UP · Boeing 747200 · Trailing Edge FlapsSDR S03253067Skin · crackedFUSELAGE SKIN CRACK BETWEEN FASTENER HOLES AT BS 2060,STRINGER-26R. REPAIR IAW SRM 53-30-03,FIGURE1. SUBMIT THE CRACKED SKIN TO MFG FOR ANALYSIS.Aug 14, 2003 · Boeing 747200 · Fuselage Main, Plate/SkinSDR S03453084Bulkhead · corrodedB18752 FUSELAGE BULKHEAD 1480 WEB CORROSION AT LBL 47.7. REPAIR IAW EO 742-53-10-0043.Aug 12, 2003 · Boeing 747200 · Fuselage Main, BulkheadSDR P5CA0300902Pushrod · malfunctionedUPON ARRIVAL NOTED NR 5 & 6 CANOE FAIRING DROOPING. REMOVED AND REPLACED I/B MID FLAP PUSH RODS AND T/E FLAP PUSHROD AND SUPPORT FITTING NR 5 CANOE.Jul 12, 2003 · N524UP · Boeing 747200 · Trailing Edge Flap Control SystemSDR P5CA0300899Engine · malfunctionedAT FL 39.0 NR 4 ENGINE WOULD NOT MAINTAIN POWER AND SLOW RESPOND. ENGINE REPLACED FOR COMPANY CONVENIENCEJul 9, 2003 · N524UP · Boeing 747200 · Engine (Turbine/Turboprop)SDR UPS03440881Socket · damagedINSPECTION TYPE:PFLT FWD ENTRY DOOR AFT EMERGENCY LIGHT SOCKET ASSY PUSHED THROUGH DOOR FRAME. UNABLE TO RELAMP. SECURED SOCKET ASSY TO LIGHT ASSY TO DOOR FRAME.Jun 23, 2003 · N528UP · Boeing 747200 · Emergency LightingSDR UPS03440806Skin · crackedINSPECTION TYPE: C, FX FLAP JOINT OUTER SKIN AT BS 1688 S46R 1EA TOP ROW FASTENER HOLE (JUST AFT OF EXISTING REPAIR PATCH) FOUND CRACKED APPROX 0.040 INCH RUNNING AFT. REF NRC 7496 & 7484 FOR SKIN REPAIRED AS PER SRM 53-30-03 FIG 17.May 23, 2003 · N521UP · Boeing 747200 · Trailing Edge FlapsSDR UPS03440763Skin · crackedINSPECTION TYPE: C, LT BODY MLG WW - BODY MLG I/B STRUT DOOR EXTERNAL SURFACE SKIN FOUND CRACKED AT REAR UPPER CORNER. SKIN REPAIRED AS PER SRM 52-80-02 FIG 1.May 22, 2003 · N521UP · Boeing 747200 · Landing Gear DoorsSDR UPS03440830Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR BS 1241 KICK FTG HOLE-D FOUND CRACK AT KICK FTG APPROX 0.030 INCH RUNNING I/B. HOLE-D REPAIRED AS PER RS R57-12-35029 AND EO B747-5710-18862-A.May 21, 2003 · N521UP · Boeing 747200 · Wing, Attach FittingsSDR UPS03440816Skin · crackedINSPECTION TYPE: C, M/D - L3 DOOR CUTOUT AFT UPPER CORNER FOUND CRACK AT FX SKIN AND TRIPLER RUNNING FROM EDGE TO FASTENER HOLE. M/D - L3 DOOR CUTOUT AFT UPPER CORNER SKIN AND TRIPLER REPAIRED AS PER HX RS R-53-41-35034 AND UPS EO B747-5310-18865-A.May 21, 2003 · N521UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440772Skin · crackedINSPECTION TYPE: C, DURING RAP ACCOMPLISH, ITEM N521UP-46-26 CLASSIFY AS CATEGORY -D- REPAIR. SKIN REPAIRED AT BS 2030-2045 STR 44R - 45R AREA AS PER SRM 53-30-03 FIG 1.May 21, 2003 · N521UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440796Stringer Clip · corrodedINSPECTION TYPE: C, AFT CARGO COMPT - BELOW FLOOR STRINGER ATT TIE CLIP FOUND CORROSION AT STA 1696 TO STA 1700 STR 48R. DUE TO COR TIE CLIP OUT OF SRM 53-10-01 FIG 1 LIMIT NEED TO BE CHANGED BLENDED AERA .75 X .5 INCH AND MAT'L REMAIN 0.020 INCH. AFT CARGOMay 20, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440795Stiffener · corrodedINSPECTION TYPE: C, FX KEELBEAM BOX RT STIFFENER FOUND CORROSION CRACKED AT STA 1460 RBL 6. FX KEEL BEAM BOX AT RBL 6 STA 1460 STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. DUE TO CORROSION CRACK TO STIFFENER OUT OF SRM 53-10-01 FIG LIMITED NEED TO BE CHANGEMay 20, 2003 · N521UP · Boeing 747200 · Fuselage Main, KeelSDR UPS03440783Stringer · crackedINSPECTION TYPE: C, M/D - BS 2180-2200 STR 12L STRINGER CRACKED. M/D BS 2180-2200 STR 12L REPAIRED AS PER HX RS 53-61-35030 & UPS ENG 'R FILE 747-53-20140.May 20, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440828Bushing · corrodedINSPECTION TYPE: C, A REPAIR BUSHING IS INSTALLED ON THE KEEL BEAM INTERIOR BATH TUB FITTING AT LT FWD BOLT HOLE & THE WALL THICKNESS OF THE BUSHING IS ONLY 0.020 INCH. REPAIR BUSHING REPLACED AS PER RS R53-49-35025 AND ENG'R/FILE NR 747 -53-20139.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, KeelSDR UPS03440841Longeron · corrodedAFT CARGO STA 1696-1700 STR 48R CORROSION REVEALED. TIE CLIP AND HI-LOCKS REINSTALLED IAW SRM 51-30-02. CORROSION BLEND OUT (0.080 INCH X 1 INCH X 2 INCHES) AFT CARGO - BS 1690 - 1710 STR 48R REPAIRED IAW SRM 53-10-03 FIG 7.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440833Floorbeam · corrodedINSPECTION TYPE: C, BULK CARGO STA 2040 LBL 60 - RBL 60 FLOORBEAM STRAP FOUND CORRODED AT UPPER AND LOWER SURFACE. DEFECT TRANSVERSE FLOORBEAM REMOVED AND SERVICABLE FLOORBEAM REPLACED PER SRM 51-10-01 PG 8, CORROSION BLEND OUT (0.020 INCH X 1 X 4 INCH).May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS03440832Web · crackedINSPECTION TYPE: C, M/D - STA 560 TO 580 STR 23R ATT WEB FOUND CORROSION CRACK. SUPPORT WEB REPLACED AS PER SRM 51-10-01.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440829Fitting · corrodedINSPECTION TYPE: C, LT BS 1241 WING REAR SPAR LOWER SPLICE PLATE ONE EACH BOLT HOLE -K- LOCATION FOUND CRACK AND CORROSION AT 3 O'CLOCK POSITION 0.040 INCH DEPTH APPROX AND 5 O'CLOCK POSITION 0.040 INCH APPROX RESPECTIVELY. REPAIRED AS PER R57-12-35029 AND EMay 19, 2003 · N521UP · Boeing 747200 · Fuselage, Wing Attach FittingsSDR UPS03440819Stringer · crackedBS 1940 - 1960 STR 2R STRINGER END CRACKED. M/D BS 1940 - 1960 STR 2R STRINGER END REPAIRED AS PER HX RS R-53-61-35035 AND ENG'R 747-53-20146.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440810Stringer · crackedINSPECTION TYPE: C, M/D - BS 1720- 1740 STR 9R STRINGER END CRACKED. M/D - BS 1720-1740 STR 9R STRINGER END REPAIRED AS PER HX RS R-53-61-35035 AND ENG'R FILE NUMBER 747-53-20146.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440809Stringer · crackedINSPECTION TYPE: C, M/D- BS 1488 S10R STRINGER END FOUND CRACKED AS MARKED. M/D - BS 1488 S10R STRINGER END REPAIRED AS PER HX RS R53-61-35035 AND ENG'R FILE NUMBER 747-53-20146.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440805Stringer · crackedINSPECTION TYPE: C, M/D CROWN - S4R STR END CORROSION CRACKED AT BS 1238. M/D STRINGER BN BS 1210 AND BS 1240 S4R REPAIRED AS PER SRM 53-10-03 FIG 5 DUE TO COR CRACK LENGTH .5 INCH FROM EDGE TO 2ND FASTENER HOLE AREA EXCEEDED SRM 53-10-01 FIG 1 LIMITATION.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440793Stringer · crackedINSPECTION TYPE: C, BULK CARGO STA 1960 S47R STRINGER END CORROSION CRACKED. STRINGER REPAIRED AT BS 1960 - 1990 STR 47R AREA AS PER SRM 53-10-03 FIG 1 DUE TO CORROSION CRACK .3125 INCH LENGTH OUT OF SRM FIG 1 LIMITATION.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440791Stringer · crackedINSPECTION TYPE: C, AREA AFT OF BULK CARGO STA 2180-2200 S50L STRINGER END CORROSION CRACK FOUND. AFT OF BULK CARGO BS 2180-2200 S50L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440787Longeron · corrodedINSPECTION TYPE:C AFT CARGO BS 1745 S49R STRINGER SPLICE FITTING CORROSION CRACK. CORROSION BLEND OUT 0.063 X 1.5 X 4 INCH. STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 8.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440786Shear Tie · corrodedINSPECTION TYPE: C, AFT CARGO STA 1840 STR 45R TO 46R SHEAR TIE CORROSION REVEALED. CORROSION BLEND OUT 0.040 X 1 X 2 INCH. SHEAR TIE BRACKET REPLACED AS PER SRM 51-10-01 PG 8.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, StructureSDR UPS03440778Stringer · corrodedINSPECTION TYPE: C, M/D CROWN - S-4R STR CORRODED AT BS 1338. CORROSION BLEND OUT (0.033 X .5 X 2 INCH) STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440777Stringer · corrodedINSPECTION TYPE: C, FWD CARGO COMPT BELOW FLOOR BIGLE SURFACE STRINGER END TO SKIN SURFACE FOUND CORROSION CRACK AT STA 820 TO STA 823 STG 47L. CORROSION BLEND OUT 0.060 X 0.5 X 0.5 INCH BS 820-830 STRINGER S47L REPAIRED AS PER SRM 53-10-03 FIG 1.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440776Reveal · crackedINSPECTION TYPE: C, M/D - R5 DOOR FWD CUTOUT REVEAL CRACK AT S-16 AS MARKED. REPAIRED AS PER SRM 53-10-04 FIG 91 AT M/D R5 DOOR FWD CUT REVEAL AT S-16.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, StructureSDR UPS03440775Stringer · crackedINSPECTION TYPE: C, M/D - BS 2340 - 2360 STR 12R STRINGER END CRACKED. CRACKED STRINGER TRIMMED OUT AS PER SRM 51-10-01 AND PERFORM STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440773Shear Tie · crackedINSPECTION TYPE: C, M/D - BS 1020 FRAME SHEAR TIE FOUND CRACKED BETWEEN S-8R AND S-9R. M/D BS 1020 FRAME SHEAR TIE 1 EA REPLACE AS PER SRM 51-10-01 BETWEEN S-8R AND S-9R.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, StructureSDR UPS03440771Longeron · crackedINSPECTION TYPE: C, M/D- BS 1940-1960 STRINGER 1R STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 6.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440767Stringer · crackedINSPECTION TYPE: C, M/D - BS 1958 S13R, STRINGER END FOUND CRACK. M/D BS 1958 S13R STRINGER END CRACKED REPAIRED AS PER SRM 53-10-03 FIG 12.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440766Stringer · crackedINSPECTION TYPE: C, M/D - BS 1940 - 1960 STR 8R STRINGER END CRACKED. M/D BS 1940-1960 STR 8R STRINGER REPLACED AS PER SRM 53-10-03 FIG 12.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440761Shear Tie · crackedINSPECTION TYPE: C, M/D - BS 1020 FRAME SHEAR TIE FOUND CRACKED BETWEEN S-9R AND S-11R. M/D BS 1020 S9R-S11R FRAME SHEAR TIE (2EA) REPLACED AS PER SRM 51-10-01 PG 8.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, StructureSDR UPS03440715Stringer · corrodedINSPECTION TYPE: C, M/D CROWN - S4R STRINGER CORRODED FROM BS 1311 TO 1319. CORROSION BLEND OUT 0.030 X .5 X 2 INCH EXCEED SRM LIMIT. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2.May 19, 2003 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440839Floor Support · corrodedINSPECTION TYPE: C, BULK CARGO STA 1920-1980 RBL 15 FLOOR SUPPORT UPPER AND LOWER SURFACE CORROSION FOUND. BULK CARGO STA 1920-1950 RBL 15 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 & CORROSION REMOVED & REPROTECTED AT BS 1950-1980 AREA AS PER SRM 51-1May 18, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440838Floor Support · corrodedINSPECTION TYPE: C, BULK CARGO STA 1920-2040 RBL 22 FLOOR SUPPORT UPPER AND LWR SURFACE FOUND CORRODED. BULK CARGO STA 1920 TO 1990 RBL 22 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 DUE TO COROSION BLEND AREA (1 INCH X 6 INCH X 0.026 INCH) OUT OF SRM May 18, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440837Floor Support · corrodedINSPECTION TYPE: C, BULK CARGO STA 1920-1980 LBL 45 FLOOR SUPPORT UPPER AND LWR SURFACE CORRODED. BULK CARGO STA 1920-1950 LBL 45 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 DUE TO BLEND OUT (1.25 INCH X 3 INCH X 0.019 INCH) EXCEEDED SRM 53-10-01 FIG 1May 18, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440836Floor Support · corrodedINSPECTION TYPE: C, BULK CARGO STA 1920-1980 LBL 8 FLOOR SUPPORT STRUCTURE UPPER AND LOWER SURFACE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01& 51-10-02 & FLOOR SUPPORT REPAIRED AT BS 1920 TO 1950 LBL 8 AS PER SRM 53-10-07 FIG 20. May 18, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440835Floor Support · corrodedBULK CARGO STA 1920-1940 LBL 15 FLOOR SUPPORT STRUCTURE UPPER AND LOWER SURFACE CORRODED. BULK CARGO STA 1920-1940 LBL L5 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20. CORROSION BLEND OUT (0.020 INCH X 1.25 INCH X 6 INCH).May 18, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440834Floor Support · corrodedBULK CARGO STA 1920-1940 LBL 30 FLOOR SUPPORT STRUCTURE UPPER AND LOWER SURFACE FOUND CORRODED. BULK CARGO STA 1920-1970 LBL 30 INCH FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20. CORROSION BLEND OUT (0.025 INCH X .875 INCH X 6 INCH).May 18, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440812Hinge · corrodedINSPECTION TYPE: C, M/D - L5 DOOR T/T LWR HINGE LWR BEARING ASSY MOUNTING SUPPORT AREA CORROSION. CORROSION BLEND OUT (0.040 X 1 X 1 INCH). M/D L5 DOOR LWR HINGE LWR SUPPORT WEB REPLACED AS PER SRM 51-10-01 PG 8.May 17, 2003 · N521UP · Boeing 747200 · Emergency ExitsSDR UPS03440803Reveal · crackedINSPECTION TYPE:C M/D - L5 DOOR FUSELAGE FWD CUTOUT REVEAL FOUND CRACKED AT BS 2232 BETWEEN 16L - 17L. M/D L5 DOOR FWD CUTOUT REVEAL S-16 REPAIRED AS PER SRM 53-10-04 FIG 91.May 17, 2003 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440813Frame · crackedINSPECTION TYPE: C, M/D - FRAME FOUND CRACKED AT BS 360 BETWEEEN STR 14R AND 15R. FRAME REPAIRED AS PER RS 53-12-35026 AND UPS EO B747-5310-18852-A.May 16, 2003 · N521UP · Boeing 747200 · Fuselage Main, Frame
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