N826MH

Service difficulty reports · 133

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 = 'N826MH' 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.

SDR DALA2020052202418Pitot Tube · obstructedAIRCRAFT 1802, ATB RETURNED TO ATL DUE TO LOSS OF CAPTAIN'S AIRSPEED INDICATION, (FO AIRSPEED NORMAL), AND EICAS MSGS: R ENG EEC MODE, L ENG EEC MODE, RUDDER RATIO, AILERON LOCKOUT APPEARED. CORRECTIVE ACTION: FOUND DIRT CLOGGED CAPTAIN'S UPPER LEFT PITOT PROBMay 22, 2020 · N826MH · Boeing 767432ER · Pitot/Static SystemSDR DALA2020010200008Skin · dentedR/H O/B FLAP LOWER SURFACE HAS DENT FROM I/B EDGE 57 INCH CROSS L/E 13 INCH. C/A R/H O/B FLAP LOWER SURFACE REPAIRED AS PER B767-400 SRM 57-53-01 -2R-1 & SRM 51-70-03, RELEASE 58.00 (1426778)Jan 1, 2020 · N826MH · Boeing 767432ER · Trailing Edge FlapsSDR DALA2020010200007Wedge · wornR/H #8 SLAT TRAILING EDGE FOUND WORN AT LES 455 C/A ENTR 00861558 W R/H #8 SLAT TRAILING EDGE WEDGE AT LES 455 REPAIRED AS PER B767- 400 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4, RELEASE 59.00 (1426833)Jan 1, 2020 · N826MH · Boeing 767432ER · Leading Edge DevicesSDR DALA2020010200005Wedge · wornR/H #10 SLAT TRAILING EDGE WEDGE FOUND WORN AT LES 708. C/A R/H #10 SLAT TRAILING EDGE WEDGE AT LES 708 REPAIRED AS PER B767 -400 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4, RELEASE 59.00 (1426836)Jan 1, 2020 · N826MH · Boeing 767432ER · Leading Edge DevicesSDR DALA2019123007627Door Sill · corrodedCABIN PASSENGER SERVICE DOOR R2 LOWER SILL FOUND CORROSION ON TEE SUPPORT . THE TEE CHORD REMOVED AND REPLACED IAW SRM 51-40-02. THE NEW TEE CHORD WAS FABRICATED IAW DWG 143T5351.Dec 30, 2019 · N826MH · Boeing 767432ER · Fuselage Miscellaneous StructureSDR DALA2019123007626Door Sill · corroded-PASSENGER CABIN SERVICE DOOR R1 LOWER SILL TEE SUPPORT FOUND CORROSION . THE LOWER SILL WAS REMOVED AND REPLACED IAW SRM 51-40-02.Dec 30, 2019 · N826MH · Boeing 767432ER · Fuselage Miscellaneous StructureSDR DALA2019123007625Door Sill · corrodedCABIN PASSENGER ENTER DOOR L2 LOWER SILL FOUND CORROSION ON TEE SUPPORT. THE TEE CHORD REMOVED AND REPLACED IAW SRM 51-40-02. NEW TEE CHORD FABRICATED IAW DWG 143T535.1. REPLACED THE CHORD IAW SRM51-40-02 .Dec 30, 2019 · N826MH · Boeing 767432ER · Fuselage Miscellaneous StructureSDR DALA2019122607552Structure · crackedDURING PERFORMANCE OF W/C5312-01170-10B-02 STEP 3, HFEC INSPECTION. FOUND ONE CRACK AT THE LOWER HOLE ABOUT 9 O`CLOCK DIRECTION (VIEW FORM INBOARD SIDE)AND THE CRACK LENGTH IS 0.2 INCH. THE CRACK WAS REPAIRED IAW W/C 5312-01170-10B-02.Dec 26, 2019 · N826MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2019122607551Failsafe · crackedCRACK INDICATIONS IN THE RT BS 955 FAILSAFE STRAP UNDER THE ATTACHED TEE FITTING DURING UT INSPECTION. EM5312-01170 SECTION 10B WAS PERFORMED.Dec 26, 2019 · N826MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2019122607550Failsafe · crackedCRACK INDICATIONS IN THE LT BS 955 FAILSAFE STRAP UNDER THE ATTACHED TEE FITTING DURING UT INSP. EM 5312-01170 SECTION 10A WAS PERFORMED.Dec 26, 2019 · N826MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2019122607549Structure · crackedDURING PERFORMANCE OF W/C5312-01170-10A-02 STEP 2 OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT LOWER HOLE ABOUT 7 O`CLOCK DIRECTION (VIEW FORM INBOARD SIDE) THE CRACK WAS REPAIRED IAW C/N 5312-01170-10A-02.Dec 26, 2019 · N826MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2019122607548Structure · crackedDURING PERFORMANCE OF W/C5312-01170-10B-02 STEP 2 OPEN HOLE HFEC INSPECTION, FOUND ONE CRACK AT LOWER HOLE ABOUT 9 O` CLOCK DIRECTION (VIEW FORM INBOARD SIDE) THE CRACK WAS REPAIRED IAW W/C:5312-01170-10B (1417985)Dec 26, 2019 · N826MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2019122607556Seat Track · corrodedCABIN SEAT TRACK, RBL 88.5, BS 1241 TO 1351 WAS FOUND CORRODED. THE SEAT TRACK WAS REPAIRED IAW PRI 583450-14, REV 0.Dec 25, 2019 · N826MH · Boeing 767432ER · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019122607553Tee Fitting · corrodedDURING PERFORM WORK CARD 5312-01170-10B-02 CREW 02 STEP 15 DVI INSPECTION, FOUND THE TEE FITTING CORRODED. THE TEE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.Dec 25, 2019 · N826MH · Boeing 767432ER · Fuselage Main, Attach FittingsSDR DALA2019122657547Frame · crackedBS 1809.5 BULKHEAD OUTER FRAME BETWEEN STRINGERS 13AR TO 20R WAS FOUND CRACKED . THE FRAME WAS REPAIRED IAW PRI 583489-14, REV 0. PRI583489-14 REV 1.PRI583489-14 REV 2.Dec 25, 2019 · N826MH · Boeing 767432ER · Fuselage Main, FrameSDR DALA2019122657546Seat Track · corrodedCABIN SEAT TRACK AT BS 1480, LBL54.75 WAS FOUND CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02 RELEASE 58.00.09/05/2019. THE NEW SEAT TRACK WAS FABRICATED IAW DWG 146T5213 AND SERVICE REQUEST NUMBER 270414807.Dec 25, 2019 · N826MH · Boeing 767432ER · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019122657545Skin · crackedNR 2 SLAT UPPER SKIN BETWEEN WS 875 AND WS885 FOUND DEFORM . THE CRACK AT NR 2 SLAT UPPER SKIN BETWEEN WS875 AND WS885 REPAIRED AS PER B767-400 PRI583537-14 REV 0 .Dec 25, 2019 · N826MH · Boeing 767432ER · Leading Edge DevicesSDR DALA2019122657544Shear Tie · corrodedFWD CARGO SHEAR TIE AT BS 369, STRINGERS 39L TO 39R WAS FOUND CORRODED. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM51-40-02. THE SHEAR TIE WAS FABRICATED IAW DWG141T122 SHT17 .AND TOPP30-10-50.Dec 25, 2019 · N826MH · Boeing 767432ER · Fuselage Internal Mounting StructureSDR DALA2019122657543Floorbeam · corrodedFLOOR BEAM AT BS 287, LBL 86 ADJACENT TO L1 DOOR TEE SUPPORT FOUND CORROSION . THE FLOORBEAM WAS REPAIRED IAW PRI583491-14 REV 0 .Dec 25, 2019 · N826MH · Boeing 767432ER · Fuselage Main, Floor BeamSDR DALA2019122657542Floor Support · corrodedAFT GALLEY AREA FROM STA1540 TO STA1562 RBL27 FOUND CORROSION ON INTERCOSTAL . REFER TO CPCP TASK 53-400-00. THE DAMAGE INTERCOSTAL AT AFT GALLEY AREA FROM STA1540 TO STA1562 RBL 27 REPAIRED AS PER PRI 583493-14 REV 0. THE PRI583493-14 REV0 COMPAIRED AND COMPDec 25, 2019 · N826MH · Boeing 767432ER · Fuselage Miscellaneous StructureSDR DALA2019122657541Floorbeam · corrodedFLOORBEAM AT BS 303, LBL 86 ADJACENT TO THE L1 DOOR TEE SUPPORT WAS FOUND CORRODED. THE FLOOR BEAM WAS REPAIRED IAW PRI 583492-14 REV 0. THE PRI 583492-14 REV 0 COMPAIRED AND COMPLETED WITH THE ER/A 583492 -14REV ORIGINAL .Dec 25, 2019 · N826MH · Boeing 767432ER · Fuselage Main, Floor BeamSDR DALA2019122407535Stiffener · crackedAD/EM-EO TASK -FOUND ONE CRACK AT THE LT VERTICAL STIFFENER IN THE NOSE WHEEL WELL AT BS 287, LBL 25, WL 159. LENGTH IS 0.4 INCH. REPAIRED THE CRACK IAW 5312-01186-02A.Dec 24, 2019 · N826MH · Boeing 767432ER · Fuselage Miscellaneous StructureSDR DALA2019122307518Shear Tie · corrodedAFT CARGO SHEAR TIE AT BS 1219 BETWEEN STRINGERS 39R TO 39L WAS FOUND CORRODED. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-40-02.Dec 23, 2019 · N826MH · Boeing 767432ER · Fuselage Internal Mounting StructureSDR DALA2019122307517Shear Tie · corrodedFWD CARGO SHEAR TIE AT BS 654+22, STRINGERS 39L TO 39R WAS FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02.Dec 23, 2019 · N826MH · Boeing 767432ER · Fuselage Internal Mounting StructureSDR DALA2019122307514Skin · corrodedFUSELAGE INTERNAL SKIN AT BS 1065 TO 1087 BETWEEN STRINGERS 39L TO 39R, FOUND CORROSION. REF TO CPCP TASK 53-544-00. THE CORROSION ON FUSELAGE INTERNAL SKIN AT BS 1065 TO 1087 BETWEEN STRINGERS 39L TO 39R WAS REPAIRED IAW PRI 583419-14, REV 0 . THE PRI 583Dec 23, 2019 · N826MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2019122327515Frame · crackedDURING INSPECTION, FOUND ONE CRACK COMMON TO FRAME AT STA 654+121, BETWEEN S-9R AND S-10R. ONE CRACK COMMON TO FRAME AT STA 654+121, BETWEEN S-9R AND S-10R ACCOMPLISHED REPAIR IAW PRI 583789-14 REV.0 AND PRI 583789-14 REV.1, COMPARED AND COMPLIED WITH ER/A 583Dec 22, 2019 · N826MH · Boeing 767432ER · Fuselage Main, FrameSDR DALA2019122007449Strut · crackedMTC TASK - NO.1 STRUT FWD UPPER SPAR I/B CHORD AT NAC STA 230 FOUND CRACK. C/A THE CRACK AT NO.1 STRUT FWD UPPER SPAR I/B CHORD NAC STA 230. REPAIRED AS PER PRI 583479-14 REV.O COMPARED AND COMPLETED WITH THE ERA #583479-14 REV. ORIGINAL ASSOCIATED ER/A 14-583Dec 20, 2019 · N826MH · Boeing 767432ER · Nacelle/Pylon, Main FrameSDR DALA2019122007448Support · brokenMTC TASK - R/H #10 SLAT I/B SIDE SUPPORT FOUND BROKEN C/A REPAIRED THE BROKEN SUPPORT AT I/B SIDE OF R/H #10 SLAT AS PER PRI 583510-14 REV.O. THE PRI 583510-14 REV.O COMPARED AND COMPLETED WITH ERA #583510-14 REV. ORIGINAL. ASSOCIATED ER/A 14-583510 ADDED FOR Dec 20, 2019 · N826MH · Boeing 767432ER · Leading Edge DevicesSDR DALA2019040432188Connector · looseEMERGENCY LIGHTS AT 21-22 AB ARE INOPERATIVE. MAINTENANCE FOUND LOOSE CONNECTOR AT SEAT 20AB AND SECURED CONNECTOR. SYSTEM OPERATION IS NORMAL.Apr 2, 2019 · N826MH · Boeing 767432ER · Light System WiringSDR DALA2019022101107Pump · fireFLIGHT 109 - WHILE PASSENGER DEPLANING NEARLY COMPLETED DURING MAINTENANCE POST FLIGHT INSPECTION DISCOVERED THE ADP ON FIRE IN THE LEFT SIDE OF THE FUSELAGE. THE FIRE WAS EXTINGUISHED WITH A PORTABLE FIRE EXTINGUISHER. REPLACED ADP AND RELAY K684. SYSTEM OPERFeb 20, 2019 · N826MH · Boeing 767432ER · Hydraulic Pump (Electric/Engine), MainSDR DALA2019022001102Connector · disconnectedEMERGENCY LIGHTS AT SEAT 21F ARE INOPERATIVE. FOUND POWER CONNECTOR FROM SEAT 20F DISCONNECTED AND RECONNECTED. SYSTEM OPERATION IS NORMAL.Feb 13, 2019 · N826MH · Boeing 767432ER · Light System WiringSDR DALA2018102206218Battery Pack · defectiveFORWARD GALLEY EMERGENCY LIGHT BATTERY PACK FOUND BAD AND REPLACED SAME.Oct 17, 2018 · N826MH · Boeing 767432ER · Emergency LightingSDR DALA2018051003222Fuse · blownEMERGENCY LIGHTS AT SEATS 15-21FG ARE INOPERATIVE. MAINTENANCE FOUND BLOWN FUSE ON POWER SUPPLY M1209 AND REPLACED. SYSTEM OPERATION IS NORMAL.May 3, 2018 · N826MH · Boeing 767432ER · Emergency LightingSDR DALA2019122607555Seat Track · corrodedDURING A C-CHECK, FOUND NUMEROUS SPOTS OF CORROSION ON THE OUTBOARD SEAT TRACK AT RBL 54.75, BS 1417 TO 1480. THE SEAT TRACK WAS REMOVED AND PERFORMED A SPLICE REPAIR IAW SRM 53-00-52, REPAIR 15.Mar 20, 2018 · N826MH · Boeing 767432ER · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018031901840Seat Track · corrodedOTBD SEAT TRACK UNDER THE R4 LAVATORY FOUND CORRODED ON THE INBD FLANGE, 6 INCHES FROM AFT END. REMOVED AND REPLACED THE SEAT TRACK.Mar 18, 2018 · N826MH · Boeing 767432ER · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018032001841Proximity Switch · failedR4 DOOR SLIDE ARMED LIGHT BLINKING WHILE SLIDE IS DISARMED. REPLACED THE RELAY PROXIMITY SWITCHES AND LIGHTS. PERFORMED AN OPERATIONAL TEST OF THE SLIDE ARMED WARNING SYSTEM IAW AMM 52-73 ON BOTH L4 AND R4 DOORS. CHECKED GOOD.Mar 16, 2018 · N826MH · Boeing 767432ER · Emergency EquipmentSDR DALA2018031301663Skin · corrodedFUSELAGE SKIN CORRODED AT THE FWD END OF THE MARKER BEACON. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS.Mar 10, 2018 · N826MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2017111408139Ecc · malfunctionedDURING TAXI OUT AFTER ENGINE START, TOWER SAW SPARKS NEAR THE LEFT ENGINE. CENTER AIR DM AND PRESSURE LIGHT ILLUMINATED. WHEN ELECTRIC PUMPS OFF AND ADP ON, ZERO HYD PRESSURE. REMOVED AND INSTALLED THE TURBINE GEARBOX ASSY AND HYD PUMP IAW AMM 29-11-03 ANov 13, 2017 · N826MH · Boeing 767432ER · Hydraulic Pump (Electric/Engine), MainSDR DALA2017082306365Bracket · brokenFOUND SECTION OF BRACKET ON THRUST REVERSER SIDE BROKEN. BRACKET HOLDS STAND OFF FOR PRE COOLER DUCT. REMOVED AND REPLACED THE NR 2 ENGINE, INBD THRUST REVERSER HALF IAW SPC 73-7830-9-0014.Aug 21, 2017 · N826MH · Boeing 767432ER · Engine Thrust ReverserSDR DALA2017053104394Light · inoperativeON SVC CK FOUND EXTERIOR EMERG LIGHTS INOP AT LT OVERWING, L4 AND R1 DOORS INOP.May 30, 2017 · N826MH · Boeing 767432ER · Emergency LightingSDR DALA2017030601834Contact · damagedDURING A SERVICE CHECK, FOUND THE R4 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. CONTACT PUSHED BACK, SOLDERED THE CONTACT, OPS NORMAL.Mar 1, 2017 · N826MH · Boeing 767432ER · Light System WiringSDR DALA2017011700416Unknown · odorAFTER T/O F/A NOTICED AN ELECTRICAL ODOR IN FIRST CLASS. THERE WERE NO VISIBLE SIGNS OF SMOKE. F/A REPORTED ELEC SMELL STRONGEST BY L1 AND FAINT BY R1 THRU MID B/C. T/S PER B767-4 FIM 21-00-21. CKD RECIRC FANS, GASPER FANS, IFE SYS, FWD GALLEY OVENS, COFFEE MAJan 16, 2017 · N826MH · Boeing 767432ER · Air Distribution SystemSDR DALA2016112409216Bypass Valve · failedGEAR DISAGREE AND GEAR DOOR MESSAGE RETURNED TO DEPARTURE. R & R THE PSEU AND MLG SELECTOR BYPASS VALVE IAW AMM.Nov 23, 2016 · N826MH · Boeing 767432ER · Landing Gear Retraction/Extension SystemSDR DALA2016102107453Battery Pack · failedDURING EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FOUND SEVERAL PACKS FAILED. REPLACED EMERGENCY LIGHT BATTERIES SYSTEM OPERATION IS NORMAL.Oct 14, 2016 · N826MH · Boeing 767432ER · Emergency LightingSDR DALA1800131802Slat Track · not reportedLEADING EDGE SLATS DOWNSTOP/TRACK, REPAIRED IAW 5750-01179.Jan 18, 2013 · N826MH · Boeing 767432ER · Leading Edge DevicesSDR DALA1168951802Power Supply · inoperativeDURING DRC MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE AT 1D, 2D AND FWD GALLEY. THE POWER SUPPLY AT SEAT 1D WAS REPLACED. SYSTEM OPERATION IS NORMAL.Dec 9, 2011 · N826MH · Boeing 767432ER · Emergency LightingSDR DALA1126751802Aileron · crackedLEFT WING I/B AILERON L/E FAIRING I/B HINGE CUTOUT FOUND CRACKED. PREPREG LAY-UP HOT BOND REPAIR CARRIED OUT AT CRACKED AREA IAW SRM 57-60-01 REPAIR 1 SRM 57-70-05 FIG 6.Mar 29, 2011 · N826MH · Boeing 767432ER · AileronsSDR DALA1126361802Fairing · delaminatedLEFT WING I/B MID FLAP O/B LEADING EDGE NOSE FAIRING FOUND DELAMINATION. PREPREG LAY-UP HOT BOND REPAIR CARRIED OUT AT DELAMINATION AREA IAW SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.Mar 29, 2011 · N826MH · Boeing 767432ER · Trailing Edge FlapsSDR DALA1126351802Fairing · delaminatedRIGHT WING I/B MID FLAP O/B LEADING EDGE NOSE FAIRING FOUND DELAMINATION. PREPREG LAY-UP HOT BOND REPAIR CARRIED OUT AT DELAMINATION AREA IAW SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.Mar 28, 2011 · N826MH · Boeing 767432ER · Trailing Edge FlapsSDR DALA1123301802Floorbeam · corrodedSTA 325 RBL 26 TO RBL 54 FLOORBEAM FOUND CORRODED. REPAIRED PER SRM 53-00-51 REPAIR 1 FIG 201.Mar 26, 2011 · N826MH · Boeing 767432ER · Fuselage Main, Floor Beam
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