Boeing 747-46NF
Service difficulty reports · 1,079
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 = '74746NF' 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 = '74746NF' 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 P5CA2022022100044None · noneM/D STA 850 - 809 LBL 11.33" SEAT TRACK FOUND CORROSION(<P>M/D STA 805 - 809 LBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE. 1 FIG 101 LIMIT</P>)SDR P5CA2022022100045None · noneM/D - STA 1920 RBL 75.92 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 1920 RBL 75.92 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100046None · noneM/D - STA 1920 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1920 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100047None · noneM/D - STA 1900 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1900 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100048None · noneU/D STA 740 LH TENSION TIE AFT CHANNEL STARTING FROM THE FASTENER HOLE RUNNING O/B TO THE EDGE FOUND CRACKED APPROX 3/8" IN LENGTH.(<P>U/D STA 740 LBL 55" TO END OF O/B TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. THIS REPAIR IS A PERMANENT REPSDR P5CA2022022100049None · noneM/D - STA 1880 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1880 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100050None · noneM/D - STA 1840 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1840 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100051None · noneM/D STA 1270-1278 RBL 11.33" SEAT TRACK FOUND CORROSION.(<P>M/D STA 1270-1278 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100052None · noneM/D - STA 1820 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1820 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100053None · noneM/D - STA 1777 - 1784 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1777 - 1784 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100054None · noneM/D - STA 1908 RBL 33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1908 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100055None · noneM/D - STA 1877 RBL 33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1877 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100056None · noneM/D STA 1860 RBL 99 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1860 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100057None · noneM/D STA 1830-1836 RBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1830-1836 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100058None · noneM/D STA 1774-1776 RBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1774-1776 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100059None · noneM/D STA 1922 LBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1922 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100060None · noneM/D STA 1822-1825 LBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1822-1825 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100061None · noneM/D STA 1886-1890 LBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1886-1890 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100063None · noneM/D - STA 2196-2198 LBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 2196-2198 LBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT</P>)SDR P5CA2022022100064None · noneM/D - STA 2117-2120 LBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 2117-2120 LBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT </P>)SDR P5CA2022022100065None · noneM/D - STA 1470-1480 RBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1470-1480 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT</P>)SDR P5CA2022022100066None · noneM/D - STA 1350-1360 RBL 11.33" SEAT TRACK FOUND CORROSION(<P>M/D - STA 1350-1360 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE . 1 FIG 101 LIMIT</P>)SDR P5CA2022022100067None · noneM/D - STA 1410-1418 RBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1410-1418 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR P5CA2022022100068None · noneM/D STA 1310-1318 RBL 11.33" SEAT TRACK FOUND CORROSION(<P>M/D STA 1310-1318 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE.1 FIG 101 LIMIT </P>)SDR P5CA2022022100069None · noneM/D STA 1290-1298 RBL 11.33" SEAT TRACK FOUND CORROSION(<P>M/D STA 1290-1298 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE.1 FIG 101 LIMIT</P>)SDR P5CA2022022100070None · noneM/D - STA 1337 RBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1337 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT</P>)SDR P5CA2022022200072None · noneSTA 2231 1EA CRACK WAS FOUND ON REVEAL RUNNING AFT THROUGH THE FASTENER HOLE AND EXTEND TOWARDS THE EDGE(<P>M/D STA 2231 STR 21L - 22L DOOR REVEAL DOUBLER CRACK AREA REPAIRED IAW SRM 53-60-15-2R-3 REPAIR 3. THIS REPAIR IS A PERMANENT REPAIR AND CATEGORY B REPASDR P5CA2022022200073None · noneLHW O/B MID FLAP MIDDLE AREA UPPER PANEL 587MT AFT EDGE FOUND BUGLE UP (CORROSION)(<P>LHW O/B MID FLAP MIDDLE AREA UPPER PANEL 587MT AFT EDGE CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 57-53-02-1A-1 LIMIT</P>)SDR P5CA2022030100074None · noneM/D STA 1846 RBL 11.33" SEAT TRACK FOUND BROKEN(<P>M/D STA 1766.45 TO STA 1870.45 RBL 11.33" SEAT TRACK REPAIRED IAW SRM 53-00-52-2R-12 REPAIR 12 FIG 201 REV.94 DATE 20FEB 2022</P>)SDR P5CA2022030200075None · noneSTA 2598 L/H B/H LOWER CORNER 3EA FASTENER HOLE FOUND CRACK AT AFT INNER CHORD(<P>STA 2598 LOWER CORNER LH AFT INNER CHORD 3EA FASTENER HOLE CRACK AREA REPAIRED IAW RI NO: 53-80-15413 REV.A</P>)SDR P5CA2022030200076None · noneRHS CANTED HORIZONTAL FLANGE OF STA 1241 BULKHEAD FORGED FTG FOUND 2EA CRACK AT 3 O'CLOCK AND 9 O'CLOCK POSITION AND BOTH APPROX 3/16" IN DEPTH AT THE BOTTOM OF FIRST LAYER.(<P>FX - STA 1241 R/H CANTED HORIZONTAL FLANGE BULKHEAD FORGED FTG P/N: 65B07920-50 1EASDR P5CA2022030300077None · noneRHW O/B FORE FLAP O/B L/E AREA FOUND DELAM(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR.5.A REV.94 ,FEB20/2022 AND REFER TO HX PROCESS CARD CONTROL SEQUENCE NO. WO.637467 FOR REPAIR DETAILS</P>)SDR P5CA2022030300078None · noneLHW #11 KRUEGER FLAP O/B LWR CORNER FOUND DELAM(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-17 PAR.5.G REV.94.FEB20/2022 AND REFER TO HX PROCESS CARD SEQUENCE NO. WO.625865 FOR REPAIR DETAILS</P>)SDR P5CA2022030400079Shear Tie · none1EA CRACK WAS FOUND ON THE RBL 33.99 AND 1EA CRACK WAS FOUND ON THE RBL 57.5 SHEAR TIE AT 1000 FRONT SPAR(<P>STA 1000 RBL 33.99 AND RBL 57.5 SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 PART 8 AND PART 9 AND RI 53-00-15419 REV.A, RI 53-00-15420 REV.A</P>)SDR P5CA2022030400080None · noneLH BLG W/W STA 1438-1460 STR 35L INTERCOSTAL FOUND CRACK(<P>LH BLG W/W STA 1438-1460 STR 35L INTERCOSTAL P/N: 65B16948-3 REPAIRED IAW RI-53-00-15421 REV.A</P>)SDR P5CA2022030500081None · noneNO.3 PYLON #472ER ACCESS PANEL 1EA FASTENER LOCK PLATE ATT RIVET FOUND BROKEN AND 1EA FASTENER HOLE FOUND WORN(<P>NO.3 PYLON ACCESS PANEL 472ER FASTENER HOLE ELONGATION AREA REPAIRED IAW RI-54-50-15409 REV.A</P>)SDR P5CA2022030500082None · noneNO.3 PYLON 472EL ACCESS PANEL 1EA FASTENER HOLE FOUND WORN(<P>NO.3 PYLON 472EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIRED IAW RI-54-50-15410 REV.A</P>)SDR P5CA2022030500083None · noneNO.4 PYLON 482EL ACCESS PANEL 1EA FASTENER HOLE FOUND WORN(<P>NO.4 PYLON 482EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIR IAW RI-54-50-15415 REV.A</P>)SDR P5CA2022030500084None · noneNO.2 PYLON 462EL ACCESS PANEL 2EA FASTENER HOLE FOUND WORN(<P>NO.2 PYLON 462EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIRED IAW RI-54-50-15414 REV.A</P>)SDR P5CA2022030700086None · noneBS 2231 1EA CRACK WAS FOUND ON THE FASTENER HOLE AT S25L RUNNING FWD AT 4 O'CLOCK POSITION APPROX 0.040"(<P> STA 2231 STR 25L FRAME STRAP LAYER 1EA FASTENER HOLE OVERSIZE REPAIRED IAW RI-53-60-15406 REV.A</P>)SDR P5CA2022030700087None · noneBS 2231 2EA CRACK WERE FOUND ON THE FASTENER HOLE AT STR 17L RUNNING AFT AT 9 O'CLOCK POSITION APPROX 0.040"(<P>M/D - STA 2231 STA 17L FRAME STRAP LAYER CRACK AREA REPAIRED IAW RI-53-60-15406 REV.A</P>)SDR P5CA2022031000089Web · noneSECT 44 - MAIN DECK FOUND CRACK ON THE WEB OF PRESSURE DECK AT STA 1241 RHS AND LHS 106, CAT C TIME - LIMITED REPAIR(<P>SECT 44 - MAIN DECK PRESSURE DECK AT STA 1241 TO STA 1265 LBL 98- LBL 127 P/N: 65B26630-11 AND STA 1241 TO STA 1265 RBL98-RBL127 WEB P/N: 65SDR P5CA2022031000090None · noneLHS CANTED HORI FLANGE OF STA 1241 BULKHEAD FORGED FITTING FOUND CRACK RUNNING I/B AT 3 O/C POSITION AND APPROX 7/8 IN LENGTH AT UPPER SURFACE(<P>FX - STA 1241 L/H O/B CANTED HORI FLANGE OF BULKHEAD FORGED FTG P/N: 65B07920-49 CRACK AREA REPAIRED IAW RI-53-00-SDR P5CA2022030800088Duct · noneNO.4 ENG R/H C-DUCT OPEN ACTUATOR ATT FITTING BOLT HOLE FOUND ELONGATED.(<P>NO.4 ENG R/H C-DUCT REPLACED IAW AMM 78-31-01. T/R COWL P/N 683L177G13 CONVERSION TO P/N 683L179G09 REF TO CARD NO. CR.636372</P>)SDR P5CA2022021600041None · noneFUSELAGE SKIN (P/N 65B23673-4) - PUNCTURE DAMAGE AT STA 690, BETWEEN S-34R AND S-35R(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>THE DAMAGED SKIN PORTION WAS TRIMMED OUT, DETAIL VISUAL INSPECTION, SURFACE AND OPEN-HOLE HFEC INSPECTIONS WERE PERFORMEDSDR P5CA2022011700003None · noneAIRCRAFT DAMAGE LOG CONTROL ITEM D16-001 - RH NOSE GEAR DOOR STA 292 DENT 1"X0.0312" A/Y=32 WITHIN LIMITS PER SRM 52-80-01-1A-1 DETAIL V.(<P>SOLID RIVET INSTALLED AS PER SRM 52-80-01-1A-1 ALLOWABLE DAMAGE 1 REV.93, 20OCT2021.</P>)SDR P5CA2022012600018None · noneL/H STAB TIP FAIRING RIB #2 (COUNT FROM FWD) FOUND CRACKED(<P>HORI STAB TIP RIB - STRUCTURE WITH 11 RIBS-REPAIR</P>)SDR P5CA2022012600019None · noneL/H STAB TIP FAIRING RIB #9 (COUNT FROM FWD) FOUND CRACKED(<P>HORI STAB TIP RIB - STRUCTURE WITH 11 RIBS-REPAIR</P>)SDR P5CA2022012600020None · none#4 PYLON VALVE ACCESS PNL #482EL 1EA HOLE FOUND ELONGATION(<P>#4 PYLON V/V ACCESS PNL #482EL FASTENER HOLE REPAIR</P>)SDR P5CA2022012600021None · none#4 ENG R/H CORE COWL EXHAUST LWR EDGE FOUND SEVERAL RIVET HOLES CRACKED.(<P>#4 ENG R/H CORE COWL PRECOOLER EXTERNAL DOUBLER REPAIR.</P>)
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