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 P5CA2014021700005Seat Track · brokenMAIN DECK CARGO SEAT TRACK BROKEN BETWEEN BS 1640 TO 1680, LBL 11.33. REPAIRED DAMAGE AREA & ACCOMPLISHED EI NO T2014A53B-344. CONDITION CHECKED NORMAL.SDR P5CA2014021700006Frame · crackedCRACK ON FRAME BS 1840 BETWEEN S11-12R. REPAIRED CRACK AND ACCOMPLISHED EI NR T2014A53B-377, REV 2. CONDITION CHECKED NORMAL.SDR P5CA2014021700007Frame · crackedCRACK ON FRAME, BS 1860 BETWEEN S10-11R. REPAIRED CRACK, ACCOMPLISHED EI NR T2014A53B-378, REV 1. CONDITION CHECK NORMAL.SDR P5CA2014021400002Connector · burnedRUDDER RATIO STATUS MESSAGE AND RUDDER RATIO SINGLE ADVISORY MESSAGE APPEARED DURING TRANSIT CHECK. TROUBLESHOOTING FOUND E1-2 SHELF WIU 1420 CONNECTOR D1288A PINS; A1 AND A2 BURNED. RELOCATED PINS TO A6 AND A7 OF SAME CONNECTOR IAW EO 4424A053, REV 0. RUDDSDR P5CA2014021000001Wire · burnedRUDDER RATIO STATUS MESSAGE AND RUDDER RATIO SINGLE ADVISORY MESSAGE APPEARED DURING TRANSIT CHECK. CIRCUIT BREAKER FOR THE RUDDER RATIO CHANGER CONTROL WAS FOUND TO BE TRIPPED AND WOULD NOT RESET. FURTHER INVESTIGATION FOUND WIRES AND POSTS IN THE WIRE INTSDR P5CA2013122200039Computer · failedDUAL FMC FAIL. COMPLIED WITH QRH. R &R LEFT FLIGHT MANAGEMENT COMPUTER IAW AMM 34-61-01. SOFTWARE INSTALLED IAW AMM 34-61-00. PERFORMED GROUND TEST IAW AMM 34-61-00 AND TEST PASSED.SDR P5CA2013112600038Actuator · damagedGEAR MONITOR STATUS MESSAGE. DURING INSPECTION OF MAIN GEAR, MAINTENANCE FOUND THAT THE RT WING GEAR POSITION ACTUATOR ROD END REMOVED FROM SHAFT. R & R RT WING GEAR POSITIONING ACTUATOR IAW AMM 32-11-20. LEAK CHECK GOOD. INSPECTED WING GEAR AND TRUCK AND NOSDR P5CA2013080800035Intercostal · crackedBS 1180, RBL 107 INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB REPLACED.SDR P5CA2013080800034Intercostal · crackedBS 1200, RBL 107, INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB REPLACED.SDR P5CA2013080800033Intercostal · crackedBS 1200, RBL 107 INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB REPLACED IAW RI NO: R1-53-41-10274, REV A.SDR P5CA2013080800032Retainer · damagedLEFT WING NR 2 PYLON UPPER L/E ILES 652.37 NOSE SKIN AND SEAL RETAINER NEAR SEVERAL FASTNER HOLES FOUND ELONGATED. REPAIRED IAW R1 NO: R1-57-41-10275, REV A.SDR P5CA2013080800031Structure · crackedBS 1220, RBL 110 BELOW FLOOR INTERCOASTAL WEB, FOUND CRACKED. REPAIRED IAW SRM 53-40-51-2R-5, REPAIR 5.SDR P5CA2013080800030Structure · crackedBS 1220, LBL 110 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-51-2R- 5, REPAIR 5.SDR P5CA2013080800029Roller · crackedRT WING INBD MID FLAP, ONE ROLLER PLATE FOUND CRACKED AT UPPER RADIUS AT WBL 164.6. ROLLER PLATE REPLACED IAW SRM 51-10-02 AND SRM 51-40-02 AND EO NR: 1927A123, PART 8.SDR P5CA2013080800036Intercostal · crackedM/D BS 1180, RBL 107 INTERCOSTAL CRACKED. INTERCOSTAL REPLACED.SDR P5CA2013051300025Winglet · damagedLIGHTNING STRIKE ON RIGHT WINGLET T/E CASTING UPPER TIP. REPAIR IAW EI NO. T2013A57B-1047 REV O.SDR P5CA2013051300024Winglet · damagedLIGHNTING STRIKE ON THE LEFT WINGLET T/E CASTING UPPER TIP. REPAIR IAW EI NO. T2013A57B991 REV O.SDR P5CA2013051300023Frame · crackedCRACK ON L5 FOR FORWARD CENTER FRAME. REPAIR IAW EI NO. T2013A53B-977 REV O.SDR P5CA2013051300022Battery · dischargedFOUND EMERGENCY LIGHT POWER, M5169 &M5170 BATTERY. REPLACED BATTERIES PER NRC 712.SDR P5CA2013042900020Control Unit · failedAIRCRAFT WOULD NOT HOLD PRESSURIZATION. PERFORMED OUTFLOW VALVE LEFT AND RIGHT QRH ITEMS TO NO AVAIL. REMOVED AND REPLACED LEFT OUTFLOW VALVE INTERFACE CONTROL UNIT AS PER AMM 21-31-10. OPERATIONAL CHECK GOOD AS PER AMM 21-31-10.SDR P5CA2013042900021Actuator · failedAIRCRAFT WOULD NOT HOLD PRESSURIZATION. PERFORMED OUTFLOW VALVE L, R QRH ITEMS TO NO AVAIL. REMOVED AND REPLACED LEFT OUTFLOW VALVE ACTUATOR AS PER AMM 21-21-07. OPERATIONAL CHECK GOOD AS PER AMM 21-31-07.SDR P5CA2013042200019Angle · crackedEMP -RIGHT HORI STAB T/E CAVITY ELEV STA 406.8 WEB ANGLE FOUND CRACK P/N 65B03779-54 ( EMP-RIGHT HORI STAB T/E CAVITY ELEV STA 406.8 CRACKED ANGLE P/N 65B03779-54 FABRICATED AND REPLACED IAW RI NO: RI-55-10-10177 REV A.SDR P5CA2013042200011Seat Track · crackedMAIN DECK BS 1840 LBL 98" TIE DOWN TRACK FLANGE CRACKED. MAIN DECK BETWEEN BS 1810.45- BS 1890.45- LBL 98" SEAT TRACK IS & NBSP; REPAIRED IAW RI NO: RI-53-65-10181 REV A.SDR P5CA2013042200012Skin · damagedFUSELAGE-SECTION 48-FUSELAGE SKIN-BS 2560 BELOW STRINGER 42R-TAIL JACK PAD AREA DENT DAMAGE. CUT OUT REPAIR TAIL JACK PAD AREA FUSELAGE SKIN BS 2560 BELOW STRINGER 42R AS PER SRM 53-80-01 REPAIR 2 FIGURE 202 AND RS NO: RI-53-81-10164 REV A.SDR P5CA2013042200013Seat Track · brokenMAIN DECK- STA 1900 2 LBL 98" TIE DOWN TRACK FOUND BROKEN. MAIN DECK BETWEEN BS 1890.45-1990.45 LBL 98" BROKEN SEAT TRACK REPAIRED IAW RI NO: RI 53-65-10181 REV A.SDR P5CA2013042200014Seat Track · wornMAIN DECK-SEAT TRACK CROWN FOUND WORN AT BS 1748-1800 RBL 11". MAIN DECK- BS 1748-1800 RBL 11" DAMAGED SEAT TRACK CROWN REPAIRED IAW RI NO: RI-53-65-10179 REV A. AND RI-53-65-10180 REV A.&NBSP.SDR P5CA2013042200015Seat Track · wornMAIN DECK- SEAT TRACK CROWN FOUND WORN AT BS 1748-1800 RBL 11''. MAIN DECK BETWEEN BS 1766.45 TO BS 1810.45 RBL 11'' DAMAGED SEAT TRACK REPAIRED IAW RI NO: RI-53-65-10180 REV A AND RI-53-65-10179 REV A.SDR P5CA2013042200016Seat Track · crackedMAIN DECK- BS 1770 LBL 11" TIE DOWN TRACK FOUND CRACKED. MAIN DECK AT BS 1766.45 TO BS 1810.45 DAMAGED SEAT TRACK REPAIRED IAW SRM 53-00-52 REPAIR 12 AND RI NO: RI-53-65-10178 REV A.SDR P5CA2013042200017Floor Support · crackedMAIN DECK- BS 1800-1820 LBL 110 FLOOR SUPPORT BEAM FOUND CRACKED P/N= 65B17951-17. MAIN DECK- BS 1800-1820 LBL 110 FLOOR SUPPORT BEAM FOUND CRACKED P/N= 65B17951-17 REPAIRED IAW RI NO: RI-53-25-10176 REV A.SDR P5CA2013042200018Bracket · crackedEMP- RIGHT STABILIZER ELEV STA 426.8 SUPPORT RIB FWD ANGLE BRACKET FOUND CRACK AS MARKED. EMP- RIGHT STABILIZER ELEV STA 426.8 SUPPORT RIB FWD ANGLE WAS FABRICATED AND REPLACED IAW RI NO: RI-55-10-10177 REV A&NBSP.SDR P5CA2013041800010Seat Track · brokenM/D - BS 1840 LBL 98 TIE DOWN TRACK FLANGE CRACKED. MAIN DECK AT BETWEEN BS 1810 TO BS 1890 LBL 98 SEAT TRACK IS REPAIRED AS PER RI NO: RI-53-65-10181 REV A.SDR P5CA2013041800009Seat Track · brokenM/D - STA 1900 LBL 96 TIE DOWN TRACK FOUND BROKEN, MARKED. MAIN DECK AT BETWEEN BS 1890 TO BS 1900 LBL 98 SEAT TRACK IS REPLACED AS PER RI NO: RI-53-65-10181 REV A.SDR P5CA2013041800008Seat Track · wornM/D - SEAT TRACK CROWN FOUND WORN AT BS 1748 RBL 11 TO BS 1800. MAIN DECK AT BETWEEN BS 1730 TO BS 1800 RBL 11 SEAT TRACK IS REPAIRED AS PER RI NO: RI-53-65-10179 REV A AND RI-53-65-10130 REV A.SDR P5CA2013041800007Floor Support · crackedM/D - BS 1800-1820 LBL 105 - LBL 110 FLOOR SUPPORT BEAM FOUND CRACKED. MAIN DECK BS 1800-1820 LBL 110 FLOOR SUPPORT BEAM IS REPAIRED AS PER RI NO: R1-53-25-10176 REV A.SDR P5CA2013031800006Nozzle · crackedDURING WALKAROUND MAINTENANCE FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, CRACK IS LOCATED AT THE 11 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CRACK IS APPROXIMATELY 10" LONG. AS PER SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION ISSDR P5CA2013030500005Warning System · false activationPACK 2 EICAS MSG AFTER ENGINE START. QRH COMPLETED. DDG REFER TO REQUIRING M ACTION. RETURNED TO BLOCKS. FOUND NO MSG IN CMC. PERFORMED CMC GROUND TEST. TEST PASS. PACK NR 2 OPERATIONAL TEST NORMAL IAW MM 21-52-00.SDR P5CA2013022500004Fan · failedPRIOR TO DEPARTURE FOUND BAD SMELL CAME OUT. TROUBLESHOOTING FOUND EQUIPMENT COOLING SUPPLY FAN HAVING INTERNAL FAILURE AND BAD SMELL COMING FROM FAN. FAN WAS REPLACED PER AMM 21-58-01/401.SDR P5CA2013012400003Compressor · stalledAT ROTATION, NR 2 ENGINE COMPRESSOR STALLED 4 OR 5 TIMES WITH A FLASH. REDUCED THRUST, ENGINE STABILIZED. CLIMBING THROUGH FL210, EGT NEAR REDLINE, REDUCED THRUST TO IDLE, THEN SHUT ENGINE DOWN TO AVOID OVERTEMP. FOUND LEVER ARM BROKEN, ENGINE REPLACEMENT RSDR P5CA2013011000002Sidewall Panel · damagedDURING MAINTENANCE WALKAROUND IN NRT, MAINTENANCE FOUND THE MAIN DECK - RIGHT BS 1710 SIDEWALL PANEL DAMAGED; TEAR 14.0 INCHES LONG X 5.0 INCHES WIDE. AS PER AMM 25-52-01-308-062, THE DAMAGE EXCEEDS THE REPAIR LIMITS. DISPOSITION WAS MADE TO PERFORM A TIME LSDR P5CA2013010800001Web · crackedA CRACK WAS FOUND ON RIGHT BODY GEAR INBOARD AFT DOOR- AFT EDGE CLOSEOUT BEAM WEB. THE SRM 52-80-02 FIGURE 101 DETAIL IV - ALLOWABLE DAMAGE 3 DOESN'T ALLOW FOR A CRACK ON INBOARD AFT DOOR- AFT EDGE CLOSEOUT RIB WEB EO 4452A173 FAA 8110-3 DATED 07JAN13 ALSDR P5CA2012121200046Cowling · dentedDURING WALK AROUND INSPECTION IN CVG MAINTENANCE FOUND THE NR 2 ENGINE INLET NOSE COWL LEADING EDGE DENTED (SUSPECTED BIRD STRIKE) AT APPROX 12 O' CLOCK POSITION MEASURING 7.750 INCHES IN LENGTH X 3.0 INCHES WIDTH AND 0.2 INCH DEPTH. AFTER DETAIL VISUAL INSPESDR P5CA2012111200045Seal Depressor · damagedDAMAGE TO THE LOWER LOBE - FWD CARGO DOOR - BS 670 SEAL DEPRESSOR FOUND MEASURING 0.280 IN. X 0.250 IN. AND LOCATED 3.0 INCHES FORM THE SEAL DEPRESSOR SPLICE AREA. DAMAGE WAS DETERMINED TO BE BEYOND THE REPAIR LIMITS IN ACCORDANCE WITH THE SRM 53-00-15, FIGURSDR P5CA2012110900044Hinge · corrodedDURING WALKAROUND INSPECTION IN PVG, A/C ACCESS PANEL HINGE FOUND WITH CORROSION DAMAGE. TIME LIMITED REPAIR ACCOMPLISHED PER EO 4453A785. REPEAT INSPECTIONS EVERY FLIGHT CYCLE. PERMANENT REPAIR REQUIRED PRIOR TO THE ACCUMALATION OF 25FLIGHT CYCLES.SDR P5CA2012103000043Door · damagedLEFT WING LANDING GEAR - SHOCK STRUT INBOARD DOOR FAIRING - LEADING EDGE DAMAGE. (REF FIGURE 1). DAMAGE FOUND TO BE BEYOND THE LIMITS OF SRM 52-80-02, FIGURE 101 ALLOWABLE DAMAGE 4 PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE GENERAL. (DISPOSITION WAS MADE TOSDR P5CA2012102300042Fairing · damagedLEFT HAND WING LANDING GEAR - SHOCK STRUT INBOARD DOOR FAIRING - TRAILING EDGE DAMAGE. DAMAGE FOUND TO BE BEYOND THE LIMITS OF SRM 52-80-02 FIGURE 101 ALLOWABLE DAMAGE 4 AND PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE GENERAL. DISPOSITION WAS MADE TO PERSDR P5CA2012101700041Skin · damagedDURING WALKAROUND INSPECTION MX ANC FOUND DAMAGE TO THE UNPRESSURIZED AREA OF THE FUSELAGE SKIN AFT OF BS 2560 BELOW STRINGER 42R, CONSISTING OF A DENT MEASURING 0.37 INCH, LONG AND 0.0625 IN DEEP AND SCRATCH 1.25 INCH LONG AND 0.03125 INCH DEEP&NBSP.SDR P5CA2012101400038Trim Panel · damagedDAMAGE FOUND TO MAIN DECK SIDE CARGO DOOR AREA AT & NBSP; BS 1780 SIDEWALL TRIM/GUTTER.SDR P5CA2012101400039Trim Panel · tornTHERE IS A 2.5 INCHES LONG TEAR TO THE MAIN DECK SIDE CARGO DOOR CUTOUT AREA & NBSP;AT BS 1920 SIDEWALL TRIM.SDR P5CA2012100700037Seat Track · damagedDAMAGE TO LOWER FORWARD CARGO COMPARTMENT SEAT TRACK AT BS 560, LBL 24.75. THE DAMAGE EXCEEDS THE ALLOWABLE DAMAGE LIMITS AS PER SRM 53-00-53-1A-1. PERFORMED A TIME LIMITED REPAIR AS DESCIBED IN PART 1 OF EO 4453A780 FAA 8110-3 DATED 06 OCT 12.SDR P5CA2012092300036Door · crackedRIGHT WING LANDING GEAR - SHOCK STRUT INBOARD DOOR FAIRING - LEADING EDGE&NBSP HAS CRACK MEASURING & NBSP;1.437 IN. DAMAGE FOUND TO BE BEYOND THE LIMITS OF SRM 52-80-02, FIGURE 101 ALLOWABLE DAMAGE 4 PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE GENERAL. PER
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