N9056R
Service difficulty reports · 50
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N9056R' AND registry_match = 'registration' 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 n_number = 'N9056R' AND registry_match = 'registration' 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 FXGA202212232233None · noneCRACKED TANG ON FRONT SPAR UPPER CAP. TO REPAIR A CRACKED TANG ON THE FORWARD EDGE OF THE FRONT SPAR UPPER CAP. USE THIS EO IN CONJUNCTION WITH STS EA 81-2022-151.SDR FXGA202110072132Skin · crackedCRACKED R/H HORIZONTAL STABILIZER LEADING EDGE AT STATION 109. TO REPAIR A CRACK LEADING EDGE SKIN ON THE R/H HORIZONTAL STABILIZER AT STATION 109. STOP DRILL CRACK AND REPAIR LEADING EDGE PER DC-6 A&B OVERHAUL MANUAL FIGURED 15-31 SHEET 2 OF 2.SDR FXGA20200813001Line · leakingDURING APPROACH, HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. DIVERTED. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN HYD PUMP HYDRALIC PRESSURE LINE LEAKING FROM HOSE FAILURE UNDER PROTECTIVE HOSE COVERING. NO EXTERNAL DAMAGE EVIDENT ON LINE ASSEMBLY,SDR FXGA201909261976Angle · bentFORWARD PRESSURE BULKHEAD BEAM REPAIR. TO REPAIR A BENT ANGLE ON THE FORWARD PRESSURE BULKHEAD, ON THE WHEEL WELL SIDE. AT F/STA 0. REPAIR RT END OF LOWER HORIZONTAL BEAM OF FORWARD PRESSURE BULKHEAD PER A&B OVERHAUL MANUAL FIGURE 12-5.SDR FXGA201908281969Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT STRINGER 17 W/STA 60L OUTBOARD. TO REPLACE CORRODED FITTINGS ON STRINGER 17L, OUTBOARD OF W/STA 60L. ON WING STRINGER 20L, REMOVE OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH A NEW ONE.SDR FXGA201908281970Tee Fitting · corrodedREPLACEMENT OF TEE ANGLE AT L/H OUTER WING AT W/STA 421. AFTER REMOVAL OF THE L/H OUTER WING THE CENTER SPAR TEE ANGLE (W/STA 421) WAS FOUND CORRODED. ON L/H OUTER WING, REMOVE CENTER SPAR TEE ANGLE AT W/STA 421.SDR FXGA2019082820191Tee Fitting · corrodedREPLACEMENT OF TEE ANGLE AT L/H OUTER WING AT W/STA 421. AFTER REMOVAL OF THE L/H OUTER WING THE CENTER SPAR TEE ANGLE (W/STA 421) WAS FOUND CORRODED. ON L/H OUTER WING, REMOVE CENTER SPAR TEE ANGLE AT W/STA 421.SDR FXGA201908261967Skin · crackedMULTIPLE WING SKIN CRACKS AT W/STA 168R BETWEEN STRINGERS 6 AND 11. MULTIPLE SMALL CRACKS WERE FOUND ON THE UPPER WING SKIN IN THE HELL HOLE AREA AROUND W/STA 168R BETWEEN STRINGERS 6 AND 11. GAIN ACCESS TO THE REPAIR AREA BY REMOVING A SECTION OF NACELLE, RSDR FXGA201908161966Skin · corrodedFUSELAGE SKIN CORRODED AT LOWER EDGE OF MAIN CARGO DOOR. TO REPAIR CORRODED FUSELAGE SKIN AT LOWER EDGE OF MAIN CARGO DOOR BETWEEN F/STA 768 AND 790. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.SDR FXGA2019081261963Stringer · crackedNR 4 NACELLE STRINGER AND SKIN SPLICE. TO SPLICE NR 4 NACELLE STRINGERS NR 1 AT STATION 436 AND STRINGER 32 AT STATION 432.5. THE NACELLE SKIN WILL BE SPLICED AT STRINGER 2 BETWEEN STATION 400 AND 473. NUMEROUS REPAIRS WERE PREVIOUSLY INSTALLED ON THE UPPERSDR FXGA201908061964Stringer Splice · corrodedFUSELAGE STRINGER SPLICES ON STRINGER 32L BETWEEN F/STA 625 AND 638, STRINGER REPAIRED IAW A&B OVERHAUL MANUAL FIGURE 12-2.SDR FXGA201908051958Spar Web · corrodedCORRODED REAR SPAR WEB AT W/STA 359L. TO REPAIR A CORRODED REAR SPAR WEB AT W/STA 359L. CUT OUT CORRODED AREA AND REPAIR PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-5.SDR FXGA2019080521957Spar · crackedCRACKED OUTER WING CENTER SPAR WEB AT W/STA 435L. TO REPAIR A CRACKED OUTER WING CENTER SPAR WEB AT W/STA 435L. PERFORM OUTER WING CENTER SPAR WEB REPAIR PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-7.SDR FXGA2019080541956Skin · corrodedFUSELAGE SKIN REPLACEMENT AND STRINGER REPAIRS BEHIND CABIN HEATER EXHAUST. TO REPLACE A CORRODED FUSELAGE SKIN FROM F/STA 596 TO 662; REPAIR CORRODED STRINGER #31L BETWEEN F/STA 629 AND 658, AND STRINGER 32L BETWEEN F/STA 629 AND 651. REMOVE AND REPLACE CORSDR FXGA2019080591954Skin · corrodedFUSELAGE SKIN CORRODED AT F/STA 801 STRINGER 8L. TO REPAIR CORRODED FUSELAGE SKIN LAP AFT OF THE MAIN CARGO DOOR AT F/STA 801 STRINGER 8L. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.SDR FXGA201907091953Skin · corrodedFUSELAGE SKIN CORRODED ABOVE FORWARD BAG PIT DOOR. TO REPAIR CORRODED FUSELAGE SKIN ABOVE FORWARD BAG PIT DOOR, AT F/STA 162 BETWEEN STRINGER 23R & 24R. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.SDR FXGA201906281950Rib · crackedLEADING EDGE RIB CAP REPAIR AT W/STA 184R. TO REPAIR A CRACKED LEADING EDGE RIB TEE CAP AT W/STA 184R. CUT CRACKED TEE CAP ANGLE IN A SUITABLE LOCATION FORWARD OF THE SWING PANEL HINGE. MANUFACTURE NEW TEE ANGLE AND SPLICE ANGLES PER DRAWING # 1950-01.SDR FXGA201909051942Skin · corrodedCORRODED FUSELAGE SKIN REPAIRS AROUND MULTIPLE CABIN WINDOWS. TO REPAIR CORRODED FUSELAGE SKIN AROUND CABIN WINDOWS AT THE FOLLOWING LOCATIONS: F/STA 285 LEFT SIDE, F/STA 770 LEFT SIDE, F/STA 790 RIGHT SIDE AND F/STA 930 RIGHT SIDE. THE FUSELAGE SKIN IS CORRSDR FXGA201905171943Doubler · crackedNR 2 ALT ACCESS DOOR DOUBLER REPLACEMENT. TO REPLACE A CRACKED ACCESS DOOR DOUBLER AT NR 2 ATLERNATE TANK. REMOVE AND REPLACE NR 2 ALTERNATE TANK ACCESS DOOR DOUBLER PER SERVICE BULLETIN #842.SDR FXGA201905141940Skin · corrodedCORRODED FUSELAGE SKIN AT F/STA 150 STRINGER 33L. CORROSION WAS FOUND 2 INCHES FORWARD OF AN EXISTING REPAIR MADE PER OVERHAUL MANUAL FIGURE 12-22. REMOVE EXISTING REPAIR AND CUT-OUT CORRODED AREA. EXTEND REPAIR PER OVERHAUL MANUAL FIGURE 12-22 TO COVER NEWSDR FXGA201908051955Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT STRINGER 20 W/STA 60L OUTBOARD. TO REPLACE CORRODED FITTINGS ON STRINGER 20L, OUTBOARD OF W/STA 60L. ON WING STRINGER 20L, REMOVE OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH A NEW ONE.SDR FXGA201905081937Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT W/STA 60L STRINGER 21L. TO REPLACE CORRODED FITTINGS ON STRINGER 21L, INBOARD AND OUTBOARD OF W/STA 60L. ON WING STRINGER 21L, REMOVE INBOARD AND OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH NEW ONES.SDR FXGA2019062681938Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT W/STA 60R STRINGER 21. TO REPLACE CORRODED FITTING INBOARD AND OUTBOARD OF W/STA 60R. REMOVE INBOARD AND OUTBOARD RIGHT HAND STATION 60 FITTINGS AND REPLACE WITH NEW ONES.SDR FXGA201807311816Skin · chafedCHAFED SKIN ON RT FLAP UPPER SKIN AT W/STA 370R. THE RIGHT HAND FLAP UPPER SKIN WAS FOUND CHAFED ON THE LEADING EDGE SECTION AT W/STA 370R. REMOVE DAMAGE IN A RACE TRACK SHAPE AND REPAIR PER A&B OHM FIGURE 13-47A. USE NAS1097AD RIVETS INSTEAD OF AN426AD RIVSDR FXGA201708031715Skin · crackedCRACKED SKIN AT STATION 239 AND STRINGER 33 1/2. REPAIR TO SKIN CRACK AT STATION 239. INSTALL REPAIR IN ACCORDANCE WITH DC6 OVERHAUL MANUAL FIGURE 12-21 AND 12-22.SDR 2017F00172Line · crackedCOMPLETE HYDRAULIC SYSTEM FAILURE, EMERGENCY LANDING PROCEDURES FOLLOWED. REPLACED HYDRAULIC PRESSURE LINE NR 2. FOUND CRACK AT B-NUT. REPLACED THE LINE. PREFORMED LEAK CHECK & OPS CHECK OKAY. RELEASED AIRCRAFT FOR CONT SERVICE.SDR FXGA2016080916162Stringer · corrodedCORRODED STRINGER 12L AT BS 1049. REPAIRED THE STRINGER IAW A&B OVERHAUL MANUAL FIGURE 12-2.SDR FXGA201607181618Skin · damagedFUSELAGE SKIN AND STRINGER REPAIR AT BS 341, STRINGER 27L. TO REPAIR THE CORRODED SKIN AND STRINGER 27L AT BS 341. CUT-OUT OF THE CORRODED SKIN AND REPAIR PER A&B OVERHAUL MANUAL FIGURE 12-22. CUT STRINGER 27L BETWEEN BS 332 AND 350. REPAIR PER A&B OVERHAUL MSDR FXGA201607191616Skin · damagedSKIN CORROSION AND HOLE IN SKIN AFT OF LOWER CORNER OF AFT BELLY DOOR BETWEEN STRINGERS 30 AND 31R. REPAIRED THE SKIN. REMOVE DAMAGE & PREFORM REPAIR IAW OVERHAUL MANUAL FIGURE 12-22.SDR FXGA201511111542Bulkhead · damagedHOLE IN BULKHEAD AT FS 341 ABOVE STRINGER 32R. REPAIRED DAMAGED BULKHEAD IAW DC-6A & B OVERHAUL MANUAL FIGURE 12 - 6.SDR FXGA201510281541Floor Skin · corrodedCORRODED FLOOR SKIN BETWEEN FS 520 & 540. REPAIRED CORRODED SKIN IAW DC-6 A & B OVERHAUL MANUAL FIGURE 12-15.SDR FXGA201510291540Floor Skin · corrodedCORRODED FLOOR SKIN, BETWEEN FS 866 & 902, AROUND RBL 10. REPAIR CORRODED SKIN IAW DC-6 A & B, OVERHAUL MANUAL FIG 12-16.SDR FXGA201503151512Skin · chafedCHAFED WING SKIN AT WS 297R, STRINGER 26R. TO REPAIR CHAFING, CAUSED BY A FAIRING, BEAVER TAIL, RUBBING AGAINST THE LOWER WING SKIN AT WS 297R, STRINGER 26R. CUT OUT DAMAGED AREA & INSTALLED AN EXTERNAL REPAIR DOUBLER IAW SRM AN 01-40NL-3 FIGURE 2-62.SDR FXGA20150323001Stringer · corrodedREPAIR OF CORRODED FUSELAGE STRINGER FS 541, STRINGER 33L. CUT DAMAGED STRINGER. REMOVE CORRODED SECTION & INSTALLED NEW STRINGER SECTION & SPLICES IAW DC6 A & B OVERHAUL MANUAL FIGURE 12 - 2 PAGE 3 & 4.SDR FXGA20141104001Unknown · leakingHYDRAULIC FAILURE, LOSS OF PRESS & QTY EXPERIENCED WHILE TURNING ONTO RUNWAY 33.SDR FXGA201408121428Frame · crackedFRAME CRACK AT FS 29.5L. THE LT FRAME RAIL LOCATED AT FS 29.5L CRACKED JUST ABOVE THE FWD HINGE POINT OF LT NLG DOOR. A NEW SECTION OF FRAME WILL BE SPLICED IN FROM STRINGER 22 TO 31.SDR FXGA2014010901Structure · corrodedCORROSION FOUND ON FRONT SPAR OF LT REAR HYD COMPARTMENT APPROXIMATELY STATION 412 FROM STRINGERS 26 -30. REPLACED STRINGER 25L FROM SPLICE AT STATION 341 TO ITS END AT STATION 41. INSTALLED DOUBLER OVER CUTOUT, REQUIRED BY STRINGER REMOVAL, AT STATION 341-3SDR FXGA201305131344Skin · corrodedCORROSION ON WING SKIN BETWEEN LWS 167 & WS 216. REPAIRED IAW EO 1344.SDR FXGA201212071292Floor Support · corrodedCORRODED FLOOR SUPPORT BETWEEN BS 630 & 791L. R & R FLOOR SUPPORT.SDR FXGA201210051279Structure · crackedNR 4 ENGINE AIRFOIL ANTI-ICE HEATER EXHAUST OPENING CRACKING. REPAIR OF CRACKING AROUND AIRFOIL ANTI-ICE HEATER EXHAUST DUCT ON NR 4 ENG EO 1279.SDR FXGA201208301267Structure · corrodedHEATER COMPARTMENT CORRODED BS 500 - 541. REPAIRED IAW EO 1267.SDR FXGAN9056R2Skin · corrodedFOUND SKIN CORROSION FUS STA 157 AT STR 31L. REPAIRED IAW EAC EO 1133 AND 8110-3 DATED 1-19-05.SDR FXGAN9056R8Skin · corrodedSKIN CORROSION DISCOVERED AT FUS STA 780 CENTERED UNDER FUS STR 32L. REPAIRED IAW EAC EO 11321 AND 8110-3 DATED 9/29/2011.SDR FXGAN9056R7Structure · corrodedCORROSION DISCOVERED ON THE CABIN FLOOR FROM STA 625 TO FUS STA 661. REPAIRED IAW EAC EO 1129 AND 8110-3 DATED9/27/2011.SDR FXGAN9056R6Stringer · corrodedCORROSION FOUND ON FUS STR 32L AT FUS 780. REPAIRED IAW WITH EAC EO 1131 AND 8110-3 DATED 9/29/2011.SDR FXGA20111003005Skin · dentedRT WING HAD A LARGE DENT FROM STA 655 TP 675. REPAIRED IAW EO 1128 AND 8110-3 DATED 9-29-2011.SDR FXGA20111003002Floor Skin · corrodedFOUND CORRODED FLOOR SKIN AT FUS STA 120. REPAIRED IAW EAC EO 1135 AND 8110-3 DATED 9-20-11.SDR FXGA20111003001Skin · corrodedFOUND SKIN CORROSION AT FUS STA 157 BETWEEN STR 33L AND 33R. REPAIRED IAW EAC EO 1134 AND 8110-3 DATED 9-20-2011.SDR FXGAN9056R1Skin · corrodedFUSELAGE SKIN FOUND CORRODED FUS STA 89 TO STA 111 BETWEEN STR 10L AND 13L. REPAIRED IAW EAC EO 1130 AND AND 8110-3 DATED 9/15/2011.SDR FXGA9056RStructure · corrodedDEEP CORROSION FOUND AT MULTIPLE NUT PLATE HOLES ALONG THE NR 2 NACELLE FILLET FAIRING BETWEEN THE FRONT AND CENTER SPAR. REPAIRED PER EAC EO 1044 AND 8110-3 DATED 8/20/10.
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