N1013A
Service difficulty reports · 298
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 = 'N1013A' 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 = 'N1013A' 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 UIEA2022102101164None · noneWEAR ON OUTBOARD CORNER AT OSS 682.74 OF SLAT #9, RH WING(<P>WEAR WAS REPAIRED IN ACCORDANCE WITH B767 SRM 51-70-10-2R-4.</P>)SDR UIEA2022102101163None · noneEVIDENCE OF MICROBIAL GROWTH ON INTERNAL STRUCTURE OF CENTER AUXILIARY AND MAIN WING TANKS(<P>EVIDENCE OF MICROBIAL <SPAN>GROWTH </SPAN><SPAN>WAS ELIMINATED PER AMM 28-11-00-107-081</SPAN></P>)SDR UIEA2022102101162None · noneFUEL LEAKAGE EVIDENCE IN LH WING CENTER SECTION LOWER SURFACE AT SPLICE STRINGER L-6 AND WBL115(<P>FUEL LEAKAGE WAS REPAIRED PER AMM 28-11-00-308-013</P>)SDR UIEA2022102101161None · noneFUEL LEAKAGE EVIDENCE IN INBOARD LEFT WING AT RIB 9, ACCESS PANEL 533AB(<P>FUEL LEAKAGE WAS REPAIRED PER AMM 28-11-00-308-013</P>)SDR UIEA2022102101160None · noneMANIFOLD WITH HYDRAULIC LEAKAGE EVIDENCE WAS FOUND IN VERTICAL STABILIZER BETWEEN REAR SPAR AND FIN STA 100 / FIN STA 125.(<P>TORQUE WAS CHECKED / CORRECTED ON THE AFFECTED MANIFOLD CONNECTIONS AS WELL AS TORQUE STRIPE APPLICATION WAS PERFORMED PER EO 6729A019SDR UIEA2022102101159None · noneLEAKAGE EVIDENCE IN THE LINE CONNECTIONS OF THE LH ENG STRUT TRAILING EDGE FAIRING, 437DB ACCESS.(<P><SPAN>AFFECTED HYDRAULIC CONNECTIONS WERE CHECKED / CORRECTED AND FOR SUCH REASON THE LEAKAGE WAS ELIMINATED</SPAN></P>)SDR UIEA2022102101158None · nonePRESSURIZATION LEAKAGE EVIDENCE ON EXTERNAL DOUBLERS INSTALLED IN UPPER FUSELAGE SKIN SURFACE AT BODY STA 434 / STA 654+22(<P>SEALANT WAS REPLACED AROUND OF EXTERNAL DOUBLERS <SPAN>INSTALLED IN UPPER FUSELAGE SKIN SURFACE AT BODY STA 434 / STA 654+22</SPAN></PSDR UIEA2022102001157None · noneSEVERAL DENTS WERE FOUND BETWEEN 5:00 TO 8:00 HRS OF RH INLET COWL ACOUSTIC PANEL(<P>DENTS WERE REPAIRED IN ACCORDANCE WITH B767 SRM 54-15-01-2R-3 REPAIR 3 AND EO 1971A291</P>)SDR UIEA2022102001156None · noneSEVERAL DENTS WERE FOUND ON LH INLET COWL ACOUSTIC PANEL(<P>DENTS WERE REPAIRED IN ACCORDANCE WITH E.O 1971A291</P>)SDR UIEA2022102001155None · noneLEAKAGE EVIDENCE IN THE AFT LH ACMP HYDRAULIC LINE CONNECTION OF THE LH ENG STRUT NACELLE, 437BL ACCESS.(<P>AFFECTED HYDRAULIC LINE WAS CHECKED / CORRECTED AND FOR SUCH REASON THE LEAKAGE WAS ELIMINATED.</P>)SDR UIEA2022102001154None · noneLEAKAGE EVIDENCE IN AFT RH HYDRAULIC "T" CONNECTION OF THE LH ENG STRUT NACELLE, 437BR ACCESS.(<P>AFFECTED CONNECTION WAS CHECKED / CORRECTED AND FOR SUCH REASON THE LEAKAGE WAS ELIMINATED</P>)SDR UIEA2022102001153None · noneHYDRAULIC LINES / CONNECTIONS WITH LEAK EVIDENCE WERE FOUND IN VERTICAL STABILIZER BETWEEN REAR SPAR AND FIN STA 58 / FIN STA 79.(<P>TORQUE WAS CHECKED / CORRECTED ON THE AFFECTED HIDRAULIC LINES / CONNECTIONS AS WELL AS TORQUE STRIPE APPLICATION WAS PERFORMEDSDR UIEA2022102001152None · noneRIGHT WHEEL WELL ALTERNATING CURRET MOTOR PUMP C1 AND C2 WITH DRAIN LEAK(<P>PUMP ASSEMBLIES WERE REPLACED AND THE TEST LEAK WAS PERFORMED IN EACH PUMP ASSY (NIL FINDINGS). OFF PART SN MX629963 & MX540177 / PN 731966 & 731966</P>)SDR UIEA2022070700736None · noneCOCKPIT PORTABLE OXYGEN FULL FACE MASK LENS FRAME DAMAGED P/N 10800C15F(<P><SPAN>REMOVED AND REPLACED PORTABLE OXYGEN FULL FACE MASK AS PER B767-300 AMM 35-31-00.</SPAN></P>)SDR UIEA2022070700734None · none#1 NACELLE STRUT REAR ACCESS PANEL BOTH HOLD OPEN RODS DAMAGED(<P><SPAN>REMOVED & REPLACED BOTH HOLD OPEN RODS FOR # 1 NACELLE STRUT REAR ACCESS PANEL AS PER AMM 20-11-00.</SPAN></P>)SDR UIEA2022070700735Tape · noneMAIN DECK CARGO DOOR FORWARD AND AFT DOOR FRAME HAS LOOSE AND WORN TAPE.(<P><SPAN>REMOVED AND REPLACED LOOSE AND WORN TAPE AT MAIN DECK BY CARGO DOOR CUT OUT FWD & AFT PER B767-300 AMM 25-52-10-308-159</SPAN></P>)SDR UIEA2022070700737Sealant · deteriorated#1 ENG I/B T/REV INTERIOR SURFACE HAS DETERIORATED FIRE RESISTANT SEALANT (PREPARED CLEANED & NBSP; AND REPAIRED DETERIORATED FIRE RESISTANT SEALANT AT # 1 ENG ; T/REV&NBSP INNER SURFACE PER B767-300 AMM 78-31-00-308-H00</P>)SDR UIEA2022070700738Roller · noneLWR. FUSELAGE AVIONICS COMPTARTMENT ACCESS DOOR FWD ROLLER IS WORN - OUT(<P>REMOVED & REPLACED FWD ROLLER AT ELECTRONICS COMPARTMENT ACCESS DOOR IAW B767 AMM 20-11-00.</P> / <P>OPERATIONAL CHECK IS NORMAL IAW B767 AMM 52-48-04.</P>)SDR UIEA2022070700739None · none#2 ENG EXHAUST CASE ( CORE COWL ) RUB PADS HAS SEVERAL LOOSE/WORN PADS(<P><SPAN>REMOVED AND REPLACED LOOSE OR WORN OUT RUB PADS AT # 2 ENG. EXHAUST CORE COWL PER B767-300 SRM 51-40-02-0G-0.</SPAN></P>)SDR UIEA2022070700740Drive Shaft · none#2 ENGINE O/B T/REV FAILED MECHANICAL BRAKE TEST(<P>REMOVED AND REPLACED # 2 ENGINE O/B T/REV FLEXIBLE DRIVE SHAFT AS PER BOEING 767 AMM 78-31-18. PERFORMED MECHANICAL BRAKE TEST. OPS CHECK NORMAL AT THIS TIME AS PER BOEING 767 AMM 78-SDR UIEA2022070700750None · noneAP. 21939. FIRST OFFICERS PTT SWITCH INTERMITTENT.(<P>COMPLIED AP-21939. R/R PTT S551 & S552 IAW AMM 23-51-03. FLT INT. F/O SYS OPS CHECK OK PER AMM 23-51-00. </P>)SDR UIEA2022070700751None · noneLOWER CARGO SMOKE DETECT LOOP 2 INOP ( LOWER CARGO COMPARTMENT FIRE DETECTION SYSTEMS ( FWD AND AFT ) DETECTOR LOOPS)(<P>T/S PER W/D & SSM 26-16-01; TAIM M12281 & TAIM M12273 ARE NOT CONNECTED (NC) TO LOOP 2 LWR FWD COMPARTMENT. TESSDR UIEA2022032300220Skin · gougedDURING AIRCRAFT TOUCH UP PAINT MX FOUND GOUGE IN LOWER AFT SECTION OF FUSELAGE AT APPROX FS 1632 IN THE NON PRESSURIZED AREA(<P ><SPAN>REPAIRED FUSELAGE IAW B767 SRM 53-00-01-2R-12 REPAIR 12. EO 6753A992</SPAN></P> / <P> </P>)SDR UIEA2022021400104Mask · inoperativeLH SUPERNUMERARY OXYGEN MASK INOP(<P>TRANSFERRED TO MDDR #161209 PER MEL 35-11-02-03A, CAT C. DUE: 23FEB22. PLACARDS INSTALLED. MCC ADVISED.</P> / <P>DISP: TS@ 1003Z.</P> / <P><SPAN>REMOVED AND REPLACED O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD IAW AMM 35-11-00SDR UIEA2022010400005None · noneCREW OXYGEN PRESSURE READS 40PSI ON EICAS INDICATION INOP.(<P>TRANSFER TO MDDR 159293 IAW MEL 35-11-02-01, CAT B.</P> / <P>LP 1604090 - REMOVED AND REPLACED VOLTAGE AVERAGING UNIT IAW AMM 35-11-06. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR 159293.</P>)SDR UIEA2021111302412None · noneEMERGENCY LIGHT SWITCH WIRE CLIP IS LOOSE AND DOES NOT FUNCTION PROPERLY(<P>SECURED EMERGENCY LIGHT SWITCH WIRE CLIP IAW AMM 33-51-08. PERFORMED LIGHT TEST IAW AMM 33-51-08. OPS CHECK GOOD.</P>)SDR UIEA2021110802360Circuit Breaker · trippedAPU FIRE LP1 AFTER EXT POWER DISC(<P><SPAN>RESET FIRE LOOP BREAKER IAW B767 AMM 20-60-01</SPAN></P>)SDR UIEA2021110802364None · noneAFTER EXT POWER DISC DUCT PSI FALLS TO ABOUT 10PSI W/ PACKS ON(<P><SPAN>PLACED ON MDDR 156389 IAW MEL 49-11-01-01 CAT C DUE 17NOV21 </SPAN></P> / <P><SPAN>EH 1155Z REFENCE LOG 1386918 ITEM M14 CVG 07NOV INSPECTED APU COMPARTMENT DUCTS AND PERFORMED BLEED AIR OSDR UIEA2021110802357None · noneWHEN EXT PWR SELECTED ON AFTER BOCK IN APU SHUT DOWN WITH ASSOCIATED EICAS MESSAGE APU FAULT(<P><SPAN>PREFORMED APU BITE PROCEDURES IAW B767 FIM 49-11 FAULT TREE 987 NO FAULT S NOTED APU OPS CHECK GOOD NO FURTHER MX ACTION REQUIRED </SPAN></P>)SDR UIEA2021110802356Eec · noneWHILE DESCENDING THROUGH FL210 L/H N1 WAS 25% HIGHER THAN R/H N1. L/H N1 & ENG INDICATION WAS HIGHER THAN R/H IND SIGNIFICANTLY(<P><SPAN>PERFORMED L/H ENG PIMU BITE PROCEDURE PER FIM 71-01 FT 810, FOUND FAULT CODES 35220-A, 155/9-A, & 15519-B. INSPECTED PS3 LISDR UIEA2021110402345None · noneON DESCENT THRUST LEVER (LEFT) IN IDLE POSITION N1 57% VS RT N1 47% NO CHNAGE WITH ANTI-ICE ON. UPON MATCHING N1'S OIL PRESS 47PSI.(<P><SPAN>PERFORMED IDLE RUNS AND FOUND NO SPLIT AT THIS TIME. DONE IAW 71-00-00</SPAN></P>)SDR UIEA2021110302332None · noneEVENT RECORD @ 1900Z FL360 TAT- 28 SAT- 57: R ENG PARAMETERS HIGHER THAN L ENG CAUSING FUEL IMBALANCE LOW 1000LBS ON R TANK. RAN ENG ANTI-ICE FOR A FEW MINUTES AND R&L ENG MATCHED BACK UP.(<P>PARAMETERS WITHIN LIMITS IAW AMM 71-00-00. NO HISTORY OR DEFECTS NOSDR UIEA2021102802300Sensor · none"FWD EQ SUP FAN 1" STATUS MSG.(<P>ITEM TRANSFERRED TO MDDR 155847 PER MEL 21-58-03-02-01. CAT C, DUE 07NOV21. </P> / <P>REF LOG 1373264 - C/W AP-20899, REMOVED AND REPLACED SUPPLY EXHAUST FAN CURRENT SENSOR IAW 21-58-11. OPS CKS GOOD. THIS CLEARS MDDR 155847.<SDR UIEA2021102702293None · noneAFTER T/O DURING CLIMB R ENG CONTROL STATUS MESSAGE DISPLAYED. R ENG CONTROL ADVISORY MESSAGE DISPLAYED AFTER LANDING.(<P>PERFORMED FIM TASK 73-21 FT 878, TOOK ABOVE 70% ENGINE RUN IAW AMM 71-00-00, OPS CHECK GOOD. ALSO PERFORMED BITE ON PIMU, NO FAULTS. IAW FSDR UIEA2021102802297Ecu · none"R ENG EEC C1" STATUS MSG(<P>REMOVED AND REPLACED RH ENG EEC IAW B767 AMM 73-21-15. PERFORMED EEC STATIC TEST IAW B767 AMM 71-00-00. NO DEFECTS NOTED.</P>)SDR UIEA2021102202267Relay · noneEICAS MSG FWD EQ. SUP FAN(<P>TRANSFER TO MDDR 155529, CAT C. DUE 01NOV21, DDG 21-58-03-02-01. PLACARD INSTALLED </P> / <P>REF LOG 1386863 #4 CVG - REMOVED & REPLACED LEFT ECS FAN CONTROL CARD M861 IAW 21-58-42. NO HELP. OPS CHECK BAD. SEE LOGPAGE 1386863 ITEM SDR UIEA2021101902250Controller · noneCOCKPIT TEMP CONTROL ERRATIC IN AUTO. TRIM VALVE CYCLES FULL OPEN AND CLOSED. COCKPIT TEMP HOT. TEMPERATURE CONTROLLED IN MAN MODE ONLY.(<P>TRANSFER TO MDDR # 155413 CAT "C" PER DDG 21-61-02-03. DUE 29OCT21. PLACARDS INSTALLED.</P> / <P>LOG PAGE 1480331: REMOVSDR UIEA2021101902251None · noneFORWARD EQUIPMENT COOLING FAN EICAS MESSAGE.(<P>TRANSFER TO MDDR # 155416 CAT "C" PER DDG 21-58-03-02-01. DUE 29OCT21. PLACARDS INSTALLED. MX ACTION COMPLIED WITH.</P> / <P>LP 1480327: OPS CHECKS PER AMM 21-58-06, NO DEFECTS NOTED, THIS CLEARS MDDR 155416.</P>SDR UIEA2021101802244None · noneLH PACK TEMP LIGHT.(<P>TRANSFERRED LH PACK TO MDDR 155285 PER MEL 21-51-01-01, CAT C. DUE DATE 27OCT21.</P> / <P>CVG MX- LP 1373294 - ITEM M3: PERFORMED GVI IAW AMM 21-51-00. FOR L/H PACK, FOUND AIR LEAK BETWEEN PACK CONTROLLER AND THE "T" DUCT, MDDR 155285 RSDR UIEA2021101002211Fan · noneFWD EQUIPMENT COOLING SUPPLY FAN 1 STATUS MESSAGE.(<P>TRANSFERRED TO MDDR 154894 IAW MEL 21-58-03-02-01, CAT 'C'.</P> / <P>LOG PAGE 1373282: REMOVED AND REPLACED FORWARD RACK SUPPLY COOLING FAN IAW AMM 21-58-06. OPS CHECK GOOD. THIS CLEARS MDDR 154894.</P>)SDR UIEA2021100802206Bottle · noneO2 BOTTLE DAMAGED DURING REPLACEMENT FOR SERVICING(<P>REMOVED AND REPLACED O2 BOTTLE IAW 767 AMM 12-15-08. LEAK AND OPS CHECK GOOD IAW 767 AMM 35-11-00.</P>)SDR UIEA2021100102154None · noneFWD EQUIP COOLING SUPPLY FAN STATUS MESSAGE.(<P>TRANSFERRED TO MDDR 154436, CAT: C, MEL 21-58-03-02-01. DUE 11OCT21. MCC NOTIFIED. PLACARDS INSTALLED.</P>)SDR UIEA2021100402177Valve · inoperativeR ENG BLEED OFF ADVISORY MSG WHEN STARTING DESCENT. AFTER LEVELING OFF AT LOWER ALTITUDE AND ADDING POWER, IT WENT AWAY. REMOVED AND REPLACED PRSOV IAW AMM 36-11-09. OPS CHECK GOOD IAW AMM 71-00-00.SDR UIEA2021093002145Card · inoperativeRT ENG BLD OFF EICAS DURING DECENT PERF FIM 36-10 FT 836. AIR SUPPLY BITE HAD NO FAULTS. CHECKED FOR ANY LEAKS , LEAK CHECK GOOD. REMOVED CONNECTOR D64 HELP PRSOV OPEN AND FOUND NO CONTUITY BETWEEN PIN 1 AND 2.R/R M860 R ENG BLEED CARD PE AMM 36-11-12. PERF R SDR UIEA2021092202067Bleed Valve · false indicationRT ENG BLEED OFF CAUTION MSG WHEN DESCENDING THRU FL330. FOLLOWED QRH W/ NO FURTHER ISSUE.(<P>BITE TEST C/O IAW B767 FIM 36-20 FAULT TREE 804, BITE TEST SHOWS NO FAULTS, A/C OK FOR SERVICE.</P>)SDR UIEA2021083101917Wire · damagedAFTER TURNING ON ALL LEFT AND RIGHT MAIN FUEL PUMPS, WE RECEIVED L AFT FUEL PUMP EICAS MESSAGE. PRESS LIGHT CAME ON LEFT AFT PUMP SWITCH ON. CB PULLED. REMOVED AND REPLACED WIRE W444-301 ,R,B,Y-18 FROM AFT SPAR SPLICE TO CONNECTOR D4408P IAW SWPM CHAP 20,WDSDR UIEA2021082601879Pump · faultedL AFT FUEL PUMP EICAS MESSAGE JUST PRIOR TO ENGINE START(<P>REFERENCE LOG PAGE 1302219: T/S IAW FIM 28-22 FT 819. FOUND K10705 RELAY TRIPPED, RESET RELAY AND CHECKED POWER AT BOOST PUMP CONNECTOR D1542, FOUND 115A AT PINS 246. REMOVED AND REPLACED L AFT BOOST SDR UIEA2021081901827Valve · faultedL ENG BLD OVHT AT FL250, RAN QRH, MESSAGE CLEARED.(<P>REMOVED AND REPLACED FAN AIR VALVE ASSY PER MCC REQUEST IAW B767 AMM 36-11-16. OPS CHECK GOOD. LEAK CHECK GOOD AT THIS TIME.</P> / <P>ITEM M10: PERFORMED HIGH POWER ENGINE RUNS IAW AMM 71-00-00 TEST PROCEDUSDR UIEA2021082401861Warning Message · false activationINFO ONLY- "L ENG BLD OVHT" EICAS DURING DESCENT. IT RESET WITH QRH PROCEDURE. NO FURTHER PROBLEMS.(<P>TROUBLESHOT IAW B767 FIM 36-20 FAULT TREE 804. NO FAULTS NOTED ON AIR SUPPLY MODULE.</P>)SDR UIEA2021081601810Starter · failedDURING COMP. WASH OF #2 ENG, STARTER FAILED.(<P>REMOVED AND REPLACED #2 ENG STARTER IAW AMM 80-11-01. OPS CHECK GOOD. NO FAULTS AT THIS TIME. PERFORMED ENGINE RUNS IAW 71-00-00 IAW AMM.</P>)
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