N844MH

Service difficulty reports · 126

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 = 'N844MH' 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 DALA2021032201601Failsafe · damagedDURING INSPECTION MAINTENANCE FOUND LH STA 955 FAIL-SAFE STRAP DAMAGED. REPAIRED ON 5312-01170- 10A-03. (LP 1757232)Mar 17, 2021 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2021032201600Failsafe · damagedDURING INSPECTION MAINTENANCE FOUND RH STA 955 FAIL-SAFE STRAP DAMAGED AND REPAIRED ON W/C 5312-01170-10B. (LP 1757204)Mar 17, 2021 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2021031801549Power Supply · inoperativeSHIP 1820 BATTERY SUPPLY M736 IS INOPERATIVE. MAINTENANCE REPLACED BATTERY SUPPLY. SYSTEM OPERATION IS NORMAL. (LP 1757157)Mar 17, 2021 · N844MH · Boeing 767432ER · Emergency LightingSDR DALA2021031801546Failsafe · crackedSHIP 1820 - DURING UT INSPECITON MAINTENANCE FOUND RH STA 955 FAIL-SAFE STRAP FOUND CRACK INDICATION. FAIL SAFE STRAP REPAIRED. (LP 175186)Mar 17, 2021 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2021031801543Failsafe · crackedSHIP 1820 - DURING OPEN HOLE INSEPCTION MAINTENANCE FOUND CRACK INDICAITONS ON THE LOWER OF THE THREE FASTENERS HOLES ON THE LH STA955 FAIL-SAFE STRAP. DAMAGED AREA REPAIRED (LP 1756366)Mar 16, 2021 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2021031801542Failsafe · crackedSHIP 1820 OPEN HOLE INSPECTION FOUND CRACK INDICATION ON THE FAIL-SAFE STRAP AT THE LOWER OF THE THREE FASTENER HOLES COMMON TO THE LH STA955 FAIL-SAFE STRAP AND T FITTING. DAMAGED HOLE ON FITTING REPAIRED. (LP 1756352)Mar 16, 2021 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2021031801541Failsafe · crackedSHIP 1820 - DURING INSPECTION MAINTENANCE FOUND LH STA955 FAIL-SAFE STRAP WITH CRACK INDICATION. FAIL SAFE STRAP REPAIRED. (LP 1756346)Mar 16, 2021 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2021031801540Failsafe · crackedSHIP 1820 DURING OPEN HOLE HFEC INSPECTION MAINTENANCE FOUND CRACK INDICATION ON THE LOWER OF THE THREE FASTENER HOLES ON THE RH STA955 FAIL-SAFE STRAP. DAMAGED HOLES WERE REPAIRED. (LP 1756288)Mar 16, 2021 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2021031601484Tee Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION ON "T" FITTING. FITTING REPLACED. (LP 1756344)Mar 16, 2021 · N844MH · Boeing 767432ER · Fuselage Main, Attach FittingsSDR DALA2021031801537Stiffener · crackedDURING INSPECTION MAINTENANCE FOUND CRACK ON RH NOSE WHEEL VERTICAL STIFFNER FILLET RADIUS AT WL172 APPROX 1 INCH LONG REPAIRED ON WORK CARD 5312-01186-02B, (LP 1755420)Mar 15, 2021 · N844MH · Boeing 767432ER · Fuselage Miscellaneous StructureSDR DALA2021031801536Stiffener · crackedDURING INSPECTION MAINTENANCE FOUND 01EA CRACK ON NOSE WHEEL LH VERTICAL STIFFENER FILLET RADIUS AT WL172 APPROX 1 INCH LONG. CRACKED AREA REPAIRED. (LP 1755419)Mar 15, 2021 · N844MH · Boeing 767432ER · Fuselage Miscellaneous StructureSDR DALA2021031101384Seat Track · corrodedMAINTENANCE FOUND CORROSION LEVEL 2 ON CABIN SEAT TRACK AT STA 368 RBL AND REMOVED. (LP 1741576)Feb 27, 2021 · N844MH · Boeing 767432ER · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021031101383Floor Support · corrodedDURINING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON CABIN FLOOR STRUCTURE AT STA 1350 TO 1562 RBL 83. T-CHORD REPAIRED. (LP 1741566)Feb 27, 2021 · N844MH · Boeing 767432ER · Fuselage Miscellaneous StructureSDR DALA2021031101382Seat Track · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON CABIN SEAT TRACK AROUND STA 368 LBL AND REMOVED. (LP 1741570)Feb 27, 2021 · N844MH · Boeing 767432ER · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021030101153Panel · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON AROUND STA 324, LBL 55 CABIN FLOOR STRUCTURE. THE CORROSION REMOVED AND CUT THE DAMAGED SECTION CHORD. (LP 1741583)Feb 27, 2021 · N844MH · Boeing 767432ER · Fuselage Floor PanelSDR DALA2021030101152Floorbeam · corrodedDURING INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON CABIN FLOOR BEAM AROUND STA 303, LBL 48. THE CORROSION REMOVED AND CUT THE DAMAGE SECTION CHORD. (LP 1741579)Feb 27, 2021 · N844MH · Boeing 767432ER · Fuselage Main, Floor BeamSDR DALA2020100103234Angle · crackedFOUND C CHECK FOUND NR 1 PYLON CLOSEOUT ANGLE CRACKED ON THE INBOARD SIDE AT NAC STA 290. C/W ERA 577354-14.Sep 28, 2020 · N844MH · Boeing 767432ER · Nacelle/Pylon Miscellaneous StructureSDR DALA2019050702950Skin · chafedNR 7 SPOILER LOWER SKIN HAS 2 SPOTS CHAFED FWD IB CORNER AND MID. C/W ERA 51-70-17 (LP 1063116)May 7, 2019 · N844MH · Boeing 767432ER · SpoilersSDR DALA2023011700330None · noneSECTION I REPAIR TO LT VERTICAL STABILIZER SKIN PANEL REQUIRES SECTION II REPETITIVE VISUAL INSPECTIONS EVERY C-CHECK OR 24 MONTHS (WHICHEVER OCCURS FIRST). THIS REWORK IS ACCOMPLISHED PER ERA 577568-14. ACCOMPLISHED DVI PER ERA577558-14, REV 0, SECTION II, May 6, 2019 · N844MH · Boeing 767432ER · Standard Practices/StructuresSDR DALA2019050702949Skin · delaminatedLEFT VERTICAL STAB EXTERIOR SKIN IS DELAMINATED APPROX FSS 92.25. REPAIRED PER E/RA 577568-00. (LP 1062595)May 6, 2019 · N844MH · Boeing 767432ER · Vertical Stabilizer, Plate/SkinSDR DALA2019050702948Web · crackedNR 1 PYLON UPPER IB WEB IS CRACKED BY MIDSPAR FITTING. REPAIRED PER ERA 577354-14. (LP 1062132)May 6, 2019 · N844MH · Boeing 767432ER · Nacelle/Pylon Miscellaneous StructureSDR DALA2019050702947Angle · crackedNR 1 PYLON LOOKING INSIDE PANEL 436AL ACROSS TO THE LARGE OUTBD AFT BOLT IN STEP OF CLOSE OUT ANGLE IS A CRACK ON BOTH SIDES OF BOLT. REPLACED ANGLE (LP 1062121)May 6, 2019 · N844MH · Boeing 767432ER · Nacelle/Pylon Miscellaneous StructureSDR DALA2019043002769Panel · dentedRIGHT WING LEADING EDGE PANEL 611PT HAS A DENT IN CENTER OF PANEL. REPAIRED PER SRM 51-70-10. (LP 1052274)Apr 29, 2019 · N844MH · Boeing 767432ER · Wing, Plate/SkinSDR DALA2019061103514Outlet · sparksPOWER OUTLET SPARKED WHEN PLUG WAS PULLED OUT OF OUTLET. C/B POPPED AND WAS NOT RESET. ON GALLEY POWER CONTROL PANEL BY 1R DOOR RESET CB - OUTLET CHECKS NORMALMar 28, 2019 · N844MH · Boeing 767432ER · AC Power Distribution SystemSDR DALA2019022001104Light · inoperativeEMERGENCY LIGHT ABOVE COCKPIT DOOR IS INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND BATTERIES. SYSTEM OPERATION IS NORMAL.Feb 19, 2019 · N844MH · Boeing 767432ER · Emergency LightingSDR DALA2019012700585Fseu · malfunctionedFLT 0090 - ATB, DUE TO TRAILING EDGE FLAP DISAGREE. CREW LEVELED OFF, ACCOMPLISHED QRH AND NOTIFIED DISPATCH AND MC. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED ALTERNATE FLAP SYSTEM PROCEDURE USING FLAPS 20 FOR LANDING. REPLACED FSEU, AND ADJUSTED FLAP LEVER Jan 27, 2019 · N844MH · Boeing 767432ER · Trailing Flap Position Indicating SystemSDR DALA2018060543834Wire Harness · brokenEMERGENCY LIGHTS AT SEATS 25AB AND 23GF WERE INOPERATIVE. REPLACED THE BULBS AT 25AB, AND FOUND A WIRE HARNESS BROKEN AT 23GF. REPLACED AND THE SYSTEM OPS NORMAL.Jun 3, 2018 · N844MH · Boeing 767432ER · Light System WiringSDR DALA2018042502837Skin · damagedBS 654A+45, STIRINGER 36L, RIVET DAMAGED IAW SRM 53-00-01.Apr 22, 2018 · N844MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2018042502836Unknown · damagedBS 544, STRINGER 32L, DAMAGE FOUND, REPAIRED IAW SRM 53-00-01.Apr 22, 2018 · N844MH · Boeing 767432ER · Fuselage Structure (General)SDR DALA2018042302793Skin · damagedBS 654 +28, STRINGER 34L LAP SEAM DAMAGED. REPAIRED IAW SRM 567863-14 AND 53-00-01.Apr 22, 2018 · N844MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2018042302792Skin · damagedLAP SEAM DAMAGE BS 654A TO 654A+22 AT STRINGER 36L REMOVED DAMAGE. CUT OUT DAMAGED SKIN IAW SRM 53-00-01.Apr 22, 2018 · N844MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2018042302791Lap Joint · damagedBS 654A+48 TO 654A +52 S 36L SKIN LAP SEAM DAMAGED. REPAIRED IAW SRM 53-00-01.Apr 22, 2018 · N844MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2018042302790Skin · damagedBS 654A +62.75 BETWEEN STRINGER 36L AND 37L SKIN DAMAGED. REPAIRED IAW SRM 53-00-01.Apr 22, 2018 · N844MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2018042202789Lap Joint · damagedBS 654 +30 TO 654 + 34, STRINGER 36L LAP DAMAGE. REMOVED TWO ROWS OF FASTENERS AND SEPARATED SKIN. REMOVED DAMAGE. REPAIRED IAW SRM 53-00-01. (LP 0519404)Apr 21, 2018 · N844MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2018040902289Skin · crackedFUSELAGE SKIN FOUND CRACKED AT STRINGER 13R BETWEEN BS 1660 - 1664. REPAIRED IAW SRM 53-80-01.Apr 8, 2018 · N844MH · Boeing 767432ER · Fuselage Main, Plate/SkinSDR DALA2018040902288Connector · unsecureINTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. SECURED THE CONNECTOR FOR THE CEILING EMERGENCY LIGHTS AT 19FG.Apr 5, 2018 · N844MH · Boeing 767432ER · Emergency LightingSDR DALA2018022601250Switch · malfunctionedCREW REST EMERGENCY LIGHTS ARE ON CONTINUOUSLY, SHOULD BE OFF. CYCLED THE EMERGENCY LIGHT SWITCH, OPS CHECKED NORMAL IAW AMM 33-51.Feb 24, 2018 · N844MH · Boeing 767432ER · Emergency LightingSDR DALA2017112208345Lens · detachedEMERGENCY EXIT DIFFUSER LENS DETACHED. ATTACHED THE LENS. OK FOR SERVICE.Nov 21, 2017 · N844MH · Boeing 767432ER · Emergency LightingSDR DALA2017090806730Lamp · inoperativeCREW REPORTED THE L4 SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS. CHECKED GOOD.Sep 7, 2017 · N844MH · Boeing 767432ER · Emergency LightingSDR DALA2017080906103Latch · brokenCOCKPIT DOOR HOLD OPEN LATCH BROKEN. REPLACED THE COCKPIT DOOR HOLD OPEN LATCH.Aug 5, 2017 · N844MH · Boeing 767432ER · Fixed Inner DoorsSDR DALA2017070405248Door · corrodedLEFT APU DOOR CORRODED ON FWD INBD CORNER AND IS OUT OF SRM LIMITS. R & R THE DOOR.Jul 3, 2017 · N844MH · Boeing 767432ER · Auxiliary Power Unit (APU) DoorsSDR DALA2017042403328Lens · unknownEMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS: 602. COVER RESTORED. (2987872)Apr 23, 2017 · N844MH · Boeing 767432ER · Emergency LightingSDR DALA2016080405980Switch · failedSTRONG BURNING RUBBER ODOR IN FLIGHT DECK AND L1 DOOR DURING TAKE OFF. DISSIPATED AND REOCCURRED ON INITIAL CLIMB AND THEN DISSIPATED AGAIN APPROXIMATELY 4 MINUTES DURATION THEN AGAIN DURING DESCENT WHEN LIGHTS TURNED ON BELOW 10,000 FT. MAINTENANCE FOUND RIAug 1, 2016 · N844MH · Boeing 767432ER · Light System WiringSDR DALA2015052803526Roller Tray · corrodedAFT CARGO BAY FOUND ONE ROLLER TRAY SURFACE WITH MINOR CORROSION. ROLLER TRAY REPAIRED IAW PRI 534287-14 REV 0.May 27, 2015 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2015052703525Roller Tray · corrodedAFT CARGO COMPARTMENT FOUND ONE ROLLER TRAY SURFACE WITH MINOR CORROSION. ROLLER TRAY REPAIRED IAW PRI 534287-14 REV 0.May 27, 2015 · N844MH · Boeing 767432ER · Fuselage Main, StructureSDR DALA2015052803489Floorbeam · crackedCABIN FLOORBEAM AT BS 246 FOUND WEB CRACK AT LBL 12. FLOORBEAM UPPER WEB REPAIRED IAW SRM 53-10-51, REPAIR 5 AND PRI 534286-14, REV 0, REV 1 AND REV 2. THE PRI 534286-14, REV 0, 1, 2.May 27, 2015 · N844MH · Boeing 767432ER · Fuselage Main, Floor BeamSDR DALA2015052803488Floorbeam · crackedCABIN FLOORBEAM AT BS 246, FOUND LOWER WEB CRACK AT LBL 10. CABIN FLOORBEAM LOWER WEB REPAIRED IAW PRI 534286-14, REV 0, PRI 534286-14, REV 1, AND PRI 534286-14 REV 2.May 27, 2015 · N844MH · Boeing 767432ER · Fuselage Main, Floor BeamSDR DALA2015052803487Floorbeam · corrodedCABIN FLOOR SUPPORT BEAM FOUND CORROSION AT BS 246 AND LBL 12. CABIN FLOOR SUPPORT BEAM REPAIRED IAW PRI 534286-14, REV O, PRI 534286-14, REV 1, AND PRI 534286-14, REV 2.May 27, 2015 · N844MH · Boeing 767432ER · Fuselage Main, Floor BeamSDR DALA2017052204074Floorbeam · corrodedCORROSION WAS NOTED AT THE BS 246 FLOORBEAM. REPAIRED IAW ER/A 534286-14, SECTION I, REPAIR WAS ACCOMPLISHED. REVISION A OF ER/A 534286-14.May 26, 2015 · N844MH · Boeing 767432ER · Fuselage Main, Floor BeamSDR DALA2015052603486Wedge · delaminatedLT WING L/E NR 2 SLAT WEDGE FOUND DELAMINATION FROM INBD EDGE 9.5". LT WING L/E NR 2 SLAT FOUND REMOVED AN RE-INSTALLED IAW AMM 27-81-02. THE DELAMINATION AREA REPAIRED IAW SRM 51-70-10, FIG 202, L/E SLAT SENSOR SWITCH TEST CARRIED OUT IAW AMM 27-88-01 AND PRMay 26, 2015 · N844MH · Boeing 767432ER · Leading Edge Devices
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