N836MH
Service difficulty reports · 128
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 = 'N836MH' 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 = 'N836MH' 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 DALA2020010600061Wedge · delaminatedRH WING NO.11 SLAT I/B T/E WEDGE CORNER FOUND DELAMINATED C/A REPAIRED RH WING NO.11 SLAT I/B T/E WEDGE CORNER DELAMINATED AS PER B767-400 SRM57-43-02-2R-1 AND SRM51-70-10,RELEASE 59.00 DATE :19DEC19. (1430544)SDR DALA2020010300035Spar Web · crackedAD/MTC TASK-FOUND TWO CRACKS AT AFT HOLES AT 221.25,AT NO.1 NACELLE ONE CRACK AT 3 O'CLOCK AT RH,THE OTHER CRACK AT 9 O'CLOCK AT LH. C/A NO.1 NACELLE FWD UPPER SPAR WEB REMOVED AND REPLACED WITH NEW WEB AS PER B767-400 SRM 51-40-02 RELEASE 59.00 DATE:19.DEC.19SDR DALA2020010300034Stiffener · crackedFOUND TWO CRACKS BETWEEN WL159.00 AND WL185.00 AT LH VERTICAL AS MARKED,LENGTH:10MM,5MM C/A NOSE WHEEL WELL LH VERTICAL STIFFENER BETWEEN WL159.00 AND WL 185.00 CRACKED AREA REPAIRED REFER TO A.A WORKCARD:5312-01185- 02A FOR WORK DETAILS. (1429020)SDR DALA2020010207632Spar Web · crackedTHE NUMBER 1 PYLON FWD UPPER SPAR WEB OUTBOARD POWER FEEDER CABLE CUTOUT HAS A 0.9 IN CRACK. REPETITIVE INSPECTIONS ARE REQUIRED AT 37,500 INITIAL FLIGHT CYCLES AND REPETITIVE AT 12,000 FLIGHT CYCLES. C/A ERA 521608-14 REV A IS CURRENT, THE WEB WAS REPLACED ANSDR DALA2019122707562Strut · crackedNR 1 STRUT FOUND CRACKED AT THE FWD CORNER OF THE FWD MIDSPAR WEB CUTOUT. THE NR 1 STRUT FWD MIDSPAR WEB CUTOUT AT THE FWD CORNER CRACKED AREA REPAIRED IAW PRI583697-14 REV.0.SDR DALA2019122607554Fitting · corrodedAFT CARGO COMPARTMENT FOUND 01 EA FORWARD WEB EXTENSION FITTING UPPER SURFACE MINOR CORROSION AT ST 1087. BETWEEN S-23L AND S-24L. AFT CARGO COMPARTMENT AT STA 1087 BETWEEN S-23L AND S-24L. LONGERON CHORD CORROSION REMOVED AND ACCOMPLISHED IAW PRI 583582-14SDR DALA2024022602681Skin · dentedSHIP 1812 NO.12 SLAT UPPER SURFACE FOUND 01EA DENT AT 34 IN FROM IB EDGE,5 IN TO T/E EDGE. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON NO.12 SLAT UPPER SURFACE AT 34 IN FROM I/B EDGE,1.5 IN FROM AFT EDGE AS PER B767-400 SRM 57-43- 02-2R-1 & SRM 51-70-1SDR DALA2019121987426Skin · crackedEM-EO TASK-FOUND ONE CRACK ALONG S-13AR BETWEEN FRAMES 1629-1678 AT RH AS MARK FUSELAGE SKIN BETWEEN STA1654.5 AND STA1678,S-13AR CRACKED SKIN REPAIRED AS PER B767-400 SRM 53-80-01 REPAIR 7,RELEASE 58.00 09/ 05/2019.EXTERNAL DETAIL INSPECTION AND LOW FREQUENCYSDR DALA2019121307275Seat Track · corrodedSEAT TRACK-FOUND CORROSION ON SEAT TRACK RBL88.5,AROUND STA 1208 TO STA1428,REFER TO CPCP TASK 53-646-00 CABIN BETWEEN STA1208 AND STA1428 RBL88.5 THE CORRDED SEAT TRACK REPLACED BY P/N:654T0513-1223 AS PER ERA 583368-14 REV. ORIGINAL.THE CORROSION ON SEAT TRASDR DALA2019121907424Shear Tie · corrodedAFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1219, BETWEEN S-39R AND S-39L. REF CPCP TASK NO: 53-558-00 AFT CARGO COMPARTMENT FRAME AT STA1219 BETWEEN S-39R AND S-39L. 01 EA NEW SHEAR TIE P/N:140T2102-1080 MADE WITH RAW MATERIAL: 7075-0-0SDR DALA2019021901060Connector · corrodedL2 AND L3 EXTERIOR EMERGENCY SLIDE LIGHTS ARE INOPERATIVE. CLEANED CORRODED CONNECTIONS AND RE-LAMPED. SYSTEM OPERATION IS NORMAL.SDR DALA2019012100429Plenum · contaminatedON VECTOR TO FINAL "DIRTY SOCK" SMELL WITH NO VISIBLE HAS WAS NOTICE ON FLIGHT DECK AND THROUGHOUT CABIN AS WE WERE NEARING GATE, BEGAN TO SMELL LIKE OIL. FOUND BURNING OIL SMELL EVIDENT ONLY WITH APU BLEED. OPENED ACCESS DOOR FOUND EVIDENCE OF OIL WITH IN APUSDR DALA2019011600367Bracket · corrodedMAINTENANCE FOUND BRACKET FROM STRUCTURE WITH SERVERE CORROSION ON BOTH SURFACES REMOVED CORROSION FROM FRAME, CLEANED AND REAMED 4 HOLES THAT MOUNT APU STARTER GROUNDING BRAKCET BLENDED APU GROUNDING CHORD PER SRM 53-80-08. (LP 0895871)SDR DALA2018042102799Wedge · delaminatedRIGHT WING NR 8 SLAT UPPER WEDGE HAS A DELAMINATED SPOT AT THE INBD END, EXTERIOR SURFACE. REPAIRED IAW SRM 51-70-10.SDR DALA2018021200843Stringer · crackedFOUND A CRACK BETWEEN BS 1654.5 AND 1629 BELOW STRINGER 14A .4 INCHES LONG. ACCOMPLISHED A DETAILED VISUAL INSPECTION AND NO DEFECTS NOTED. PERFORMED HFEC ON THE STRINGER IAW NDT PART 6 51-00-19, NO DEFECT NOTED. BLENDED BOTH AREAS AND NO EXCESS MATERIAL REMSDR DALA2018020700734Battery Pack · no testWHILE PERFORMING AMDS CARD 3350-7202 DISCOVERED THE EMERGENCY LIGHT BATTERY PACKS FAILED TO TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51.SDR DALA2017111508137Bulb · burned outDURING A SERVICE CHECK, ALL BULBS BURNED OUT IN THE EMERGGENCY EXIT SIGN. REPLACED THE BULBS IAW AMM 25-29. OPS CHECKED GOOD.SDR DALA2017092507069Structure · chafedDURING IFSD CHECK, FOUND CHAFE DAMAGE TO THE NR 2 ENGINE OTBD CORE COWL . REMOVED AND REPLACED CORE COWL ASSY IAW AMM 71-11.SDR DALA2017011900488Battery · dischargedEMERGENCY LIGHTS IN FWD GALLEY INOP. REPLACED BATTERY PER AMM 33-51.SDR DALA2016112809347Wire · damagedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. INSPECTED WIRING FOR EMERGENCY LIGHTING SIGN FOUND DAMAGED WIRES REPAIR WIRES PER SWPM 20-10 EMERGENCY LIGHT OP'S NORMAL.SDR DALA2016102107447Battery Pack · failedDURING EMERGENCY LIGHT TEST 2 BATTERY PACKS FAILED. REPLACED M6756 AND M6758. SYSTEM OPERATION IS NORMAL.SDR DALA2016032602387Relay · no testMANUAL DEPLOYMENT TEST OF PASSENGER O2 MASKS FAILED DURING R4 LAV INSTALLATION CHECK OUT. REPLACED K00466 OXYGEN SYSTEM CONTROL MANUAL DEPLOY TIME DELAY RELAY IAW WDM 35-21-11. PERFORMED PASSENGER OXYGEN SYSTEM MANUAL DEPLOYMENT TEST IAW AMM.SDR DALA14019521812Fairing · delaminatedINBD MAIN FLAP L/E OTBD FAIRING FOUND DELAMINATED. LT WING INBD MAIN FLAP L/E OTBD FAIRING COMPOSITE PREPREG HOT BOND. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05, PAR.5A, 1 AND REF PROCESS CARD :KEW514086-01.SDR DALA14019531812Fairing · delaminatedRIGHT WING INBD MAIN FLAP L/E OTBD FAIRING FOUND DELAMINATED. RT WING INBD MAIN FLAP L/E OTBD FAIRING COMPOSITE PREPREG HOT BOND. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05 PAR 5A(1) AND REF PROCESS CARD KEW514094-01.SDR DALA14018951812Floorbeam · corrodedBS 246 CABIN FLOORBEAM AFT SIDE UPPER AFT ANGLE AT RBL 62 TO 68 FOUND CORRODED. FLOORBEAM REPAIRED IAW ER/A 521619-14, REV ORIG.SDR DALA14018941812Spar · crackedNR 1 PYLON UPPER SPAR WEB FOUND CRACKED AT IDG POWER FEEDER CABLE CUTOUT POSITION. C/A NR 1 PYLON UPPER SPAR WEB REPLACED IAW ER/A 521608-14, REV ORIG.SDR DALA14018931812Skin · chafedRIGHT AIR GATE FAIRING FWD CUTOUT UPPER SKIN AND ATT PLATE FOUND CHAFING. RT AIR GATE FAIRING FWD CUTOUT AREA SKIN REPLACED IAW SRM 53-80-01.SDR DALA14018921812Skin · chafedLEFT LOWER AIR GATE FAIRING FWD CUTOUT UPPER SKIN AND ATT PLATE FOUND CHAFING. LT AIR GATE FAIRING FWD CUTOUT AREA SKIN REPAIRED IAW SRM 53-80-01.SDR DALA14018911812Skin · chafedLEFT LOWER AIR GATE FAIRING FWD CUTOUT LOWER SKIN FOUND CHAFING. LT LOWER AIR GATE FAIRING FWD CUTOUT LWR SKIN REPAIRED IAW SRM 53-80-01, FIG 201, REPAIR 3, DETAIL V1.SDR DALA14018901812Failsafe · crackedBULKHEAD FAILSAFE STRAP FOUND CRACKED DURING NDT TEST. FITTING REPLACED IAW ER/A 521599-14AD, REV ORIG.SDR DALA14018891812Failsafe · crackedREAR SPAR BULKHEAD FITTING AREA AT ONE FASTENER HOLE FOUND CRACKED AT FAIL SAFE STRAP THROUGH THICKNESS IN 5 O/C POSITION. BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP REPAIR AND TEE FITTING REPLACEMENT ACCOMPLISHED IAW ER/A 521600-14AD, REV ORIG.SDR DALA14018881812Frame · crackedRIGHT BS 1809.5 FWD OUTER FRAME ANGLE CRACKED AT RADIUS AREA BETWEEN S7-8R, REPAIRED IAW SRM 53-80-08, FIG 201.SDR DALA14020161812Floorbeam · corrodedFLOORBEAM AT BS 246, RBL 65 CORRODED. REPAIRED IAW SRM 53-10-41, REPAIR 2.SDR DALA14017181812Battery · damagedL3 DOOR SLIDE BATTERY FOUND DAMAGED. L3 DOOR SLIDE REPLACED IAW AMM 25-66-10.SDR DALA13026701812Skin · crackedUPPER WING SKIN PITCH LOAD FITTING CRACKED. REPAIRED IAW PRI 515434-14AD, REV O, VERIFIED PRI 515434-14AD, REV O MATCHES ERA 515434-14AD, REV A.SDR DALA13026711812Skin · crackedLT WING SKIN UPPER LOAD FITTING ULTRASOUND CRACK INDICATION AFT FASTENER INBD ROW. REMOVED FASTENER, REAMED HOLE IAW WC 5724-01005-10. . REPAIRED COMPLETE ON PRI 515424-14AD REV 0.SDR DALA1247881812Battery Pack · inoperativeSEATS 36-42AB EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY SUPPLY BATTERY PACK AT 42AB. OPS CHECK GOOD PER B767-400 33-51.SDR DALA1204311812Harness · defectiveEMERGENCY PATH LIGHTS AT SEAT 27B ARE INOPERATIVE. JUMPER HARNESS WAS REPLACED. SYSTEM OPERATION IS NORMAL.SDR DALA1201171812Battery Pack · dischargedEMERGENCY LIGHTS BATTERY PACK AT R4 IS INOPERATIVE. MTC REPLACED THE BATTERY PACK AND CHARGER. SYS OPS NML.SDR DALA1201071812Wire Harness · disconnectedDURING DRC MAINTENANCE FOUND EMERGENCY EXIT SEAT LIGHTS AT ROWS 22AB TO 26AB INOPERATIVE. THE SEAT HARNESS AT ROW 22AB IS DISCONNECTED AND RECONNECTED THE HARNESS. SYSTEM OPERATION IS NORMAL.SDR DALA1171321812Hinge Fitting · crackedDURING OPN 5626AD MAINTENANCE FOUND THE RT O/B FLAP HINGE FITTING CRACKED AND REPLACED PER EA 14-086392-12AD REV B NE 04 OPN 401 AND 402.SDR DALA1149981812Fuse · blownMAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM SEATS 39A THROUGH 45A. MAINTENANCE REPLACED THE FUSE IN THE POWER SUPPLY.SDR DALA1137411812Wire Harness · disconnectedSUPPLEMENTAL INFORMATION - MX EMERGENCY ESCAPE PATH LIGHTING SEAT MOUNTED AT 20F INOPERATIVE. MX VERIFIED SOCKET AND BULB OPERATE NORMALLY AND NOW SUSPECT THE WIRING HARNESS IN SEAT. MX FOUND HARNESS UNPLUGGED AND RESECURED IT. LIGHTS NOW CHECK OK.SDR DALA1123651812Wedge · dentedLT WING NR 6 SLAT UPPER WEDGE EXTERNAL SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10, REPAIR 4 FIG 202.SDR DALA1123661812Fairing · delaminatedLT WING I/B MAIN FLAP LEADING EDGE O/B NOSE FAIRING FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01 TABLE 1 AND SRM 57-70-03 PARA 5.A FIG 5.SDR DALA1015150836Skin · damagedREMOVAL OF ADP FOUND FUSE SKIN DAMAGE AT STA 1175 BETWEEN STR 27L AND 28L. REPAIRED PER ERA 483001-14 REV A REFERENCE NN/R CARD 22 6-4-10.SDR DL764091412Module · malfunctionedIRREG; ON TAXI OUT GOT SPOILER MESSAGE ON EICAS. REPLACED 1R SCM PER MM OPS CHECK NORMAL.SDR DL764091281Ecu · malfunctionedON TAXI OUT WITH ENGINES SHUTDOWN APU SHUTDOWN WITH FAULT RE-STARTED AND FAILED AGAIN WITHOUT USING PNEUMATICS RETURNED TO GATE. FOUND NO APU AND PNEU LATCHED MSGS. CHECKED APU INLET PLENUM AND FOUND NO INGESTED FOD. OPERATED APU SEVERAL TIMES WITH PACK OPSSDR DL764091237Fan · failedSTRONG ODOR/FUME PRESENT THROUGHOUT THE AIRCRAFT. SMELL WENT AWAY AFTER TURNING UTILITY BUS OFF. STRONG SMELL WAS REPORTED AFT GALLEY LT SIDE/C CARRIED OUT FAULT ISOLATION FOUND LT RECIRC FAN C/B TRIPPED IN E&E BAY. RESET C/B RAN FAN SMELL APPEARED IN CABINSDR DL764091181Switch · shortedSMOKE CAME FROM OVERHEAD PANEL NEAR GLARESHIELD LIGHT RHEOSTAT. DROPPED LT OVERHEAD LIGHT PANEL. CONFIRMED BURNING ODOR FROM PANEL. FOUND LT RUNWAY TURNOFF LT SWITCH INTERNALLY SHORTED AND FIXED IN OFF POSN. PULLED AND SECURED C/B 11P6 AND CONFIRMED LT RUNWY
Back to N836MH