Boeing 747-2D7B
Service difficulty reports · 726
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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 = '7472D7B' 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 aircraft_model_key = '7472D7B' 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 UIEA2010062500046Skin · corrodedDURING C-CHECK, A BULGE WAS DETECTED IN AN EXISTING REPAIR DOUBLER ON SKIN AT BS 460 AND S41-42L. DAMAGED REPAIR DOUBLER WAS REMOVED AND SUBSEQUENT DISCOVERED DRILL STARTS IN THE SKIN WERE TRIMMED OUT. THE DISCREPANT AREAS WERE THEN REPAIRED IAW NRC 0011 AND SDR UIEA2010062500045Skin · dentedDURING C-CHECK, A DENT WAS DETECTED IN THE SKIN AT BS 460 - 480 AND S39-40R. DAMAGE WAS TRIMMED OUT AND REPAIRED IAW IAI NRC 0012 AND SRM 53-30-03, FIG 27, SHEET 5, DETAIL III FIG 1.SDR UIEA2010062500044Skin · dentedDURING C-CHECK, A DENT WAS DETECTED IN THE OUTER SKIN 65B04514-3 OF BULK CARGO DOOR ASSY AT BS 1980-2000 S33R. DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 0062 AND SRM 52-00-03, FIG 9, SHEET 4, DETAIL I.SDR UIEA2010062500043Fairing · crackedRT LEST440-528 HORIZONTAL STAB L/E OTBD FAIRING HAS 6 CRACKS AT RIB ANGLES PERFORMED MAJOR REPAIR IAW RAM256 - NRC1141 - SRM 55-10-06 FIG 1.SDR UIEA2010062500032Rib · crackedSTABILIZER LT L/E OTBD FAIRING LEST 440-496 HAS 4 CRACKS AT RIB ANGLES. INSTALLED 4 FILLERS AND 4 ANGLES. REPAIRED IAW SRM.SDR UIEA2010062400073Stringer · crackedNRC 1115 "LOWER DECK" CRACK ON STR 35L UPPER FLANGE AT STA 420 (DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH NEW SEGMENT AND REPAIR STRINGER PN N523MC, NRC 1115 1/2 IAW SRM 53-10-03 FIG 3 FASTENER INSTL IAW SRM 51-30-02)SDR UIEA2010062400070Stringer · bentNRC: 0975 "LOWER DECK" B/T STA 380 - 400 STR 40R STRINGER UPPER FLANGE IS BENT. (DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH NEW SEGMENT AND REPAIR - STRINGER PN N523MC, NRC 0975 1/2 IAW SRM 53-10-03, FIG 3. FASTENERS INSTL IAW SRM 51-30-02).SDR UIEA2010062400064Stringer · bentNRC 0978 "LOWER DECK" B/T STA 360 - 380 STR 38R STRINGER LOWER FLANGE IS BENT. (DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH ENW REPAIR. STRINGER AND FILLER PN B523MC NRC 978 1/2 IAW SRM 53-10-03, FIG 3. INSTALL FASTENERS IAW SRM 51-30-02).SDR UIEA2010062400042Skin · corrodedFUSELAGE SKIN CORRODED AT- BS 1241, S10-11R. MAJOR REPAIR PERFORMED IAW THE RAM 177- NRC960 IAW SRM 53-30-03, FIG 47.SDR UIEA2010062400040Cargo Track · damagedDURING C-CHECK IN TLV UPPER FLANGE OF THE AFT CARGO COMPARTMENT CARGO TRACK BETWEEN BS 1500 TO BS 1520 RBL 45.5 WAS FOUND BROKEN. (THE DAMAGE WAS CUT OUT, REMOVED AND SPLICED IAW SRM 53-10-05 FIG 5 AS CATEGORY A PERMANENT REPAIR DOCUMENTED ON NRC467. SEE FIG 1SDR UIEA2010062400038Stringer · corrodedDURING C-CHECK IN TLV LEVEL 2 CORROSION WAS FOUND IN THE STRINGER BETWEEN BS1900 TO BS1920 AND STRINGER 48R. THE DAMAGE WAS CUT OUT, REMOVED AND SPLICED AT BS1880, BS1920 AND BS1940 IAW SRM 53-10-03 FIGURE 8.SDR UIEA2010062400037Skin · corrodedDURING C-CHECK IN TLV LEVEL 2 CORROSION WAS FOUND IN THE 65B04142-3 SKIN AT BS 1900 TO BS 1920 S48R. DAMAGE TRIMMED OUT, REPAIRED IAW SRM 53-30-03 FIG 1 AS A CATEGORY B PERMANENT REPAIR AND DOCUMENTED ON NRC028.SDR UIEA2010062400033Skin · dentedDURING WALKAROUND INSPECTION IN HKG, MAINTENANCE FOUND DAMAGE TO THE NR 2 ENGINE RT FAN COWL DENT DAMAGE, BELOW THE SERVICE OIL DOOR (REF FIGURE 1). DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEASDR UIEA2010062200065Stringer · crackedNRC: 1124 FWD CARGO, CRACK ON STR 38R BETWEEN STA 500-520 (DAMAGED PORTION OF STRINGER REMOVED, REINFORCED AREA WITH NEW SEGMENT AND REPAIR. STRINGER PN B523MC NRC 1124 1-2 REPAIR IAW SRM 53-10-03, FIG 3 & AMP; FASTENER INSTL IAW SRM 51-30-02).SDR UIEA2010062200036Skin · dentedDURING C-CHECK, A DENT WAS FOUND IN THE SKIN AT BS 360-380 S-38R TO -39R. DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 022 AND SRM 53-30-03, FIG 26.SDR UIEA2010062100060Stringer Clip · crackedNRC: STA 360 AFTER REMOVAL CRACKED STR CLIP FOR REPLACEMENT WAS FOUND CRACK ON THE STR 7R.(DAMAGED AREA TRIMMED OUT AREA REINFORCED WITH REPAIR STRINGER AND SPLICE PN N523MC, NRC 1333 1/3 IAW SRM 53-10-03, FIG 3, FASTENERS INSTL IAW SRM 51-30-02).SDR UIEA2010062100058Skin · corrodedNRC: 011 -BULGE BY 2.5" X 2.3" X 0.037" ON EXT FUSELAGE, SKU EXISTING REPAIR DOUBLER EDGE BS 440-460 AND STR 43L-44L. (EXISTING REPAIR REMOVED THE WORK ACCOMPLISHED IAW J/C NO 0B011-R1 USING DOUBLER PN N523MC, NRC 011-1 FASTENERS INSTALLED IAW SRM 51-30-02).SDR UIEA2010061600077Rib · crackedNRC 1142 :HORIZ STAB" LT STAB L/E OTBD FAIRING HAS 4 CRACKS AT RIB ANGLE. (CRACKED AREA TRIMMED OUT. REINFORCED AREA WITH ANGLE AND FILLER PN N523MC NRC 1142 1/2 IAW SRM 55-10-06 FIG 1 AND FASTENERS INSTL IAW SRM 51-30-02).SDR UIEA2010061400076Stringer · crackedNRC: 964 "LOWER DECK" STA 320, 2 EA CRACKS (1 EA ON STR UPPER FLANGE AND 2 ON STR WEB) ON STR 35R. (DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH NEW SEGMENT AND REPAIR STRINGER PN N523MC, NRC 964 1/2 IAW SRM 53-10-03 FIG 3 AND FASTENERS ISNTL IAW SRM 51-30-SDR UIEA2010060600028Floor Panel · damagedDURING CARGO LOADING AT DOV; MX FOUND DAMAGE TO THE MAIN DECK FLOORBOARD AT BS 1080, RBL 45. THE DAMAGE TO THE MD FLOORBOARD PANEL AT BS1080, RBL45 AIS S FOLLOWS: THE DAMAGE IS ABOUT 7 INCHES LONG AND ABOUT .5 INCH WIDE, AND .2500 INCH DEEP. (DISPOSITION WAS MSDR UIEA2010060300059Cargo Track · damagedNRC 0494 SWELLING ON AFT CARGO TRACK UPPER FLANGE BETWEEN STA1900-1920 RBL 25 (DAMAGED AREA TRIMMED OUT IAW SRM 51-10-01, REINFORCED WITH EXTRUDED REPAIR ANGLE, REPAIR STRIP, TRACK SECTION PN B523MC 494 1,2,3 IAW SRM 53-1-05 FIG 5 FASTENERS INSTL IAW SRM 51-30SDR UIEA2010053000022Skin · damagedDAMAGED AREA BY 6.0 X 3.0" ON EXTERNAL FUSELAGE SKIN AT STRINGER AREA BS 160-180 S-42AL (DAMAGED AREA FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A).SDR UIEA2010053000020Skin · bulgedBULGE BY 1.2 X 1.1 X 0.013" ON EXT. FUSELAGE SKIN STA 2160-2180 STR 42L-44L (THE BULGE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A.)SDR UIEA2010053000019Skin · bulgedBULGE BY 1.3 X 1.0 X 0.025" ON EXT FUSELAGE SKIN STA 2140 STR 36L-37L (STA AREA) (THE BULGE WAS FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-00, FIG 1A.)SDR UIEA2010052000008Skin · corrodedCORROSION ON EXT FUSELAGE SKIN STA 1720 STR 45R-46R (CORROSION REMOVED IAW SRM 51-10-01. FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1 AFTER CLEANUP AND AREA PROTECTED IAW SRM 51-10-02.)SDR UIEA2010051600018Skin · dentedDENT BY 1.8 X 1.5 X 0.016" ON EXTERNAL FUSEALGE SKIN BS 380-400 ABOVE S-41L(DENT FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A)SDR UIEA2010051600017Skin · bulgedBULGE BY 1.0 X 0.8 X 0.025" ON EXTERNAL FUSELAGE SKIN BS 320-340 ABOVE S-39R (BULGE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A.)SDR UIEA2010051600016Skin · dented2 EA ADJACENT DENTS ON INSP; EXTERNAL FUSEALGE SKIN BS 380-400 S-37R-38R UPR 1.25 X 1.0 X 0.008" AND LWR 0.8 X 0.7 X 0.010" (2 EA DENTS FOUND WITHIN ALLOWABLE DAMAGE AND INSP;LIMITS IAW SRM 53-30-01 FIG 1A)SDR UIEA2010051600015Skin · damagedPREVIOUSLY REWORKED AREA ON EXTERNAL FUSELAGE SKIN BS 380-400 S-38R-39R BY 2.0 X 1.6 X 0.011 X 0.010" (NOTED AREA FOUND WITHIN ALLOWABLE DAMAGE; LIMITS IAW SRM 53-30-01, FIG 1.)SDR UIEA2010051600014Skin · bulgedBULGE BY 2.0 X 2.0 X 0.022" ON EXTERNAL FUSELAGE SKIN BS 520-540 S42R-43R (BULGE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01.)SDR UIEA2010051600013Skin · bulged2 EA BULGES BY MAX 1.0 X 1.0 X 0.024" ON EXTERNAL FUSELAGE SKIN BS 540-560 S-41R-42R (2 EA BULGES FOUND WITHIN ALLOWABLE LIMITS).SDR UIEA2010051600012Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BY 4.0 X 2.5 X 0.039" BS 500-520 S-35R-36R (DENT FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A).SDR UIEA2010051600010Skin · dentedSEVERAL SMALL DENTS BS 340-380L S-39L-40L ON EXTERNAL FUSELAGE SKIN (SEVERAL SMALL DENTS FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM).SDR UIEA2010051600009Skin · bulgedBULGE BY 1.5X 1.0 X 0.024" AND ADJACENT DENT BY 3.2 X 1.5 X 0.014" ON EXTERNAL FUSELAGE SKIN BS 580-600 S-44R-45R (BULGE AND DENT FOUND IN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01 FIG 1A.)SDR UIEA201000194Trim System · malfunctionedMANUAL STAB TRIM LEVERS MORE THAN 1 KNOB SPLIT (AT CRUISE. (DIVERSION) ACCOMPLISHED STAB TRIM / ADJ TEST IAW 27-41-00. IN PITOT STATIC TEST SET IAW 34-11-00. BROUGHT L/E TO ORIGINAL AND 20000 FT. COULD NOT DUPLICATE. TESTED RIGGING TENSION IAW 27-41-00, FIG 50SDR UIEA201000150Intercostal · damagedDURING C-CHECK, DAMAGE WAS FOUND IN THE 65B07942-26 INTERCOSTAL ON THE NWW SIDEWALL WL 153 STIFFENER BETWEEN BS 260 AND 280.THE INTERCOSTAL WAS REPLACED USING A 141U1193-43 INTERCOSTAL WHICH IS PART OF THE MODIFICATION IAW SB 747-53A2562, REV 2. PART 1 OF THISSDR UIEA201000149Frame · damagedDURING C-CHECK AND INSPECTION IAW EO 4753A521, ADDITIONAL DAMAGE WAS FOUND IN THE BS 2231 FRAME INNER CHORD AT S-25R. THE DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 745 AND SRM 53-10-04, FIGURE 115 (SEE FIG 1, 2 AND 3). NOTE: THIS EO REPLACED EO 4753A521. TESDR UIEA201000151Skin · damagedDURING C-CHECK, DAMAGE WAS FOUND IN THE 65B04141-2 SKIN AT BS 1940, S-40L TO -41L.THE DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 270 AND SRM 53-30-03, FIGURE 18 (SEE FIGURES 1 AND 2). THE 65B04141-2 SKIN IS MADE FROM 0.063 INCH THICK 2024-T3 CLAD ALUMINUM SHSDR UIEA201000144Skin · damagedDURING C-CHECK, LIGHTNING STRIKE DAMAGE WAS FOUND IN THE 65B07658-1002 SKIN AT BS 160-180, S-45R. THE DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 094 AND SRM 53-30-03, FIGURE 26 (SEE FIGURES 1 AND 2).SDR UIEA201000152Cargo Track · damagedDURING C-CHECK, DAMAGE WAS FOUND IN THE AFT LOWER CARGO COMPARTMENT SEAT TRACK AT RBL 25 BETWEEN BS 1800 AND 1820. THE DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 476 AND SRM 53-10-05, FIG 5. THE TRACK IS MADE FROM BAC1520-1682 EXTRUSION MADE FROM 7178-T6511SDR UIEA201000148Skin · damagedTHIS EO DOCUMENTS A MAJOR REPAIR. DURING C-CHECK, CORROSION WAS DETECTED COMMON TO LST SIDE WING INTERSPAR SKIN (65B14451-3 WING UPPER SKIN PANEL NR 1) AFT OF REAR SPAR , WS 415 LOCATION - (REF FIGURE 1).THE CORROSION WAS BLENDED OUT IAW THE SRM 57-30-01 FIGURSDR UIEA201000147Stringer · crackedTHIS EO DOCUMENTS A MAJOR REPAIR. DURING C-CHECK, DAMAGE WAS FOUND IN THE BS 370 - 390, S40L STRINGER, CONSISTING OF A CRACK. THE DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 521 AND SRM 53-10-03, FIGURE 3 (SEE FIGURE 1). THE STRINGER 40L IS MADE FROM 0.040 INSDR UIEA201000146Skin · dentedDURING C-CHECK, A DENT WAS FOUND IN THE SKIN AT BS 420-440, S12AL-13L.THE DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 212 AND SRM 53-30-03, FIG 1. THE SKIN AT THE DENT LOCATION IS MADE FROM 0.063 INCH THICK 2024-T3 CLAD ALUMINUM SHEET IAW SRM 53-30-02, FIG 1, SDR UIEA201000145Skin · corrodedTHIS EO DOCUMENTS A MAJOR REPAIR. DURING C-CHECK, CORROSION WAS DETECTED COMMON TO RT WING LOWER SKIN WS1285 - WS1320 (REF FIG 1). THE CORROSION WAS BLENDED OUT IAW THE SRM 51-10-01/02 WITHIN LIMITS IAW SRM 57-30-01 FIGURE 2 (SHEET 7); THE FLANGE WAS BLENDED SDR UIEA201000143Skin · damagedDURING C-CHECK, DAMAGE WAS FOUND IN THE 65B23675-1 SKIN AND 65B23678-2 DOUBLER AT BS 720, S-40R. THE DAMAGE WAS TRIMMED OUT AND REPAIRED IAW RFTA 00694-0004 AND REA MF00694R0004, EO 4753B287.SDR UIEA201000138Blowout Door · damagedREF EO 4778A150- NR 2 T/R ACCESS AMD BLOWOUT DOOR REPAIR. PART ONE TIME LIMITED REPAIR ACCOMPLISHED. PART TWO INSPECTION REQUIRED EVERY FLIGHT CYCLE (SCHEDULE WITHIN 10 CALENDAR DAYS AFTER ACCOMPLISHMENT PART 1).SDR UIEA201000189Rib · corrodedLT STABILIZER STA 281 RIB LOWER CORD SURFACE CORRODED. LEVEL 1. DAMAGED CHORD REMOVED NEW FABRICATED. PN 65B03680-29 IAW DWG 65B03680-28 AND NR A004088G002. USING WITH FASTENERS IAW SRM 51-30-02.SDR UIEA2010022300139Fairing · puncturedWING TO BODY FAIRING AT BS 1680 WITH A PUNCTURE/DAMAGE (HONEYCOMB EXPOSURE) MEASURING 2.5 IN. X 0.5 IN (REF FIG 1) (PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4753B253 PART 1 OF WORK INSTRUCTIONS. SCHEDULE REPEAT INSP AT EVERY 3 FC AND PERMANSDR UIEA201000018Fuel Filter · dirtyNR 3 ENGINE AT DESCENT NOTICED LOW POWER AND SHUT DOWN. LOW FUEL FLOW. ENGINE FAILURE/SHUT DOWN CHECK LIST ACCOMPLISHED NO ABNORMAL INDICATIONS SO ATTEMPTED RESTART WITH INFLIGHT START. LOW FUEL FLOW 200KGS, LESS THAN 26 PERCENT N1 LESS THAN 30 PERCENT N2, SDR UIEA201000063Stringer · corrodedDURING C-CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION IN THE 65B04369-175 STRINGER AT BS 1960, S-50R. EFFECTED AREA WAS REMOVED AND REPAIRED AS PER FAA FORM 8100-9 DATED 05 FEB 2010 AND EO 4753B249.
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