# Boeing 767-35H - Type: Aircraft model (FAA registry) - Registry code: 1385208 - Manufacturer (registry): BOEING - Model: 767-35H - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 330 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-767-35h Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (34) As reported by operators and repair stations, by the model named in the report. - [SDR MK1Y20230305001](https://openairdocs.org/sdr/MK1Y20230305001), Mar 5, 2023: NONE. NONE. SEC 43, STA 654 TO 654+22, STR 31L TO 32L: DURING MAINTENANCE INSPECTION, SHOP HAS DISCOVERED A BUCKLE ON FUSELAGE SKIN AT THE NOTED AREA, AND PERFORMED A CUT O - [SDR MK1Y20230305020](https://openairdocs.org/sdr/MK1Y20230305020), Mar 5, 2023: NONE. NONE. ENGINE #2 – LH CORE COWL, NAC STA 264.50, UPPER CORNER EDGE: DURING MAINTENANCE INSPECTION, SHOP FOUND A 0.9" LONG CRACK ON AN INCOMING REPAIR AT THE NOTED AREA - [SDR MK1Y20230305019](https://openairdocs.org/sdr/MK1Y20230305019), Mar 5, 2023: NONE. NONE. ENG #2 FAN COWL OUTER SKIN: 8 (EIGHT) DENTS WERE FOUND WITH CLOSE GAPS IN THE OUTER SKIN OF THE ENG #2 FAN COWL, ON THE OUTBD SIDE BT 4 O'CLOCK TO 5 O'CLOCK. - [SDR MK1Y20230305018](https://openairdocs.org/sdr/MK1Y20230305018), Mar 5, 2023: NONE. NONE. REPAIR – EXTERNAL FUSELAGE SKIN, STA 1809 TO 1824, 4.0" ABOVE STR 22R: DURING MAINTENANCE INSPECTION AT IAI, SHOP FOUND AN UNDOCUMENTED DOUBLER REPAIR AT THE NO - [SDR MK1Y20230305017](https://openairdocs.org/sdr/MK1Y20230305017), Mar 5, 2023: NONE. NONE. : R/H MAIN LANDING GEAR TRUNNION DOOR AT OUTER SKIN, FWD EDGE LOWER CORNER: DURING MAINTENANCE INSPECTION, SHOP FOUND UNDOCUMENTED DOUBLER REPAIR AT THE NOTED A - [SDR MK1Y20230305016](https://openairdocs.org/sdr/MK1Y20230305016), Mar 5, 2023: NONE. NONE. ENGINE #2 CF6-80C2B6F, EXHAUST, NAC STA 332.34 AND NAC STA 360.73: SHOP FOUND A DENT WITH SHARP CREASE ON THE EXTERNAL EXHAUST SKIN LOCATED ON ENGINE 2 NAC STA - [SDR MK1Y20230305015](https://openairdocs.org/sdr/MK1Y20230305015), Mar 5, 2023: NONE. NONE. ENGINE #2 CF6-80C2B6F STRUT, AFT FAIRING PANEL ASSY, BETWEEN NAC STA 304.54 AND NAC STA 308.00: SHOP FOUND AN EXISTING REPAIR ON THE OUTBD SIDE OF STRUT #2 IN T - [SDR MK1Y20230305013](https://openairdocs.org/sdr/MK1Y20230305013), Mar 5, 2023: NONE. NONE. ENGINE # 2 OUTBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND UNDOCUMENTED DOUBLER REPAIR ENG # 2 OUTBD CORE COWL AROUND FWD LATCH CUTOUT BT NAS S - [SDR MK1Y20230305012](https://openairdocs.org/sdr/MK1Y20230305012), Mar 5, 2023: NONE. NONE. ENGINE #2 INBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND EXISTING HAT FRAME REPAIR NOT ACCORDING TO SRM ON INBD CORE COWL ENG #2 NAC STA 303.75 - [SDR MK1Y20230305011](https://openairdocs.org/sdr/MK1Y20230305011), Mar 5, 2023: NONE. NONE. ENGINE #2, BT NAC STA 268.7 TO 303.7 AND BT 9 TO 10 O'CLOCK: DURING MAINTENANCE INSPECTION SEVERAL SCRATCHES DAMAGE WERE FOUND ON CORE COWL SKIN. FASTENERS REMO - [SDR MK1Y20230305010](https://openairdocs.org/sdr/MK1Y20230305010), Mar 5, 2023: NONE. NONE. ENGINE #1 OUTBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND TWO EXISTING UNDOCUMENTED DOUBLER REPAIRS ON OUTBD CORE COWL. M0149 – LOCATED NAC STA - [SDR MK1Y20230305009](https://openairdocs.org/sdr/MK1Y20230305009), Mar 5, 2023: NONE. NONE. STRUT FAIRING SKIN, INBD SIDE: EXISTING UNDOCUMENTED 2.8"X1.4" DOUBLER REPAIR ON THE INBD SIDE OF STRUT FAIRING SKIN BELOW DOOR PANEL BT STA 304.54 – 307.34. - [SDR MK1Y20230305008](https://openairdocs.org/sdr/MK1Y20230305008), Mar 5, 2023: NONE. NONE. DURING MAINTENANCE INSPECTION AT IAI, A DENT WAS FOUND ON THE LOWER SKIN PANEL OF LAP SPLICE AT STR 36L, STA 1433 (BELOW BULK CARGO DOOR). DENT DIMENSIONS: L=2. - [SDR MK1Y20230305007](https://openairdocs.org/sdr/MK1Y20230305007), Mar 5, 2023: NONE. NONE. SEC 48, STA 1854 TO 1863: FOUND EXISTING DOUBLER REPAIR ON RH DOOR EXTERNAL SKIN AROUND LATCH CUTOUT LOWER LONGERON. - [SDR MK1Y20230305006](https://openairdocs.org/sdr/MK1Y20230305006), Mar 5, 2023: NONE. NONE. DURING MAINTENANCE INSPECTION, AIRCRAFT MAINTENANCE CORRODED AREA WAS FOUND AT DRAIN MUST BETWEEN STA 1395 AND STA 1417 AND STR 35R AND STR 36R. A UT INSPECTION - [SDR MK1Y20230305005](https://openairdocs.org/sdr/MK1Y20230305005), Mar 5, 2023: NONE. NONE. FUSELAGE SKIN, STA 325 BT STR21L-22L: TWO EXISTING BLENDOUTS FOUND ON EXTERNAL FUSELAGE SKIN. NOMINAL THICKNESS: 0.130". (-0.002" THICKNESS BLENDED). ONLY ONE B - [SDR MK1Y20230305004](https://openairdocs.org/sdr/MK1Y20230305004), Mar 5, 2023: NONE. NONE. SECTION 41 – FUSELAGE SKIN AT STA 159.5 AND ABOVE STR30R: DURING MAINTENANCE INSPECTION, EXISTING BLEND OUT AND LIGHTING STRKE WERE FOUND. SKIN P/N 141T3211, IS - [SDR I5EA2022061700002](https://openairdocs.org/sdr/I5EA2022061700002), Jun 16, 2022: SLIDE RAFT. DEPLOYED. INADVERTENT ESCAPE SLIDE/RAFT DEPLOYMENT DURING MAINTENANCE ACTIVITIES, REPLACED L1 DOOR ESCAPE SLIDE/RAFT IAW B767 AMM 25-66-01. MDL 32515 ITEM 2 - [SDR CA150318012](https://openairdocs.org/sdr/CA150318012), Mar 17, 2015: BALLAST. BURNED. (CAN) AS REPORTED BY CABIN CREW, ODOR OF BURNING WIRES VERY STRONG AROUND ROW 20 AND 21. FOUND BALLAST AT 21AC WITH BLOWN FUSE AND BURNED ELECTRICAL ODOR. REPLA - [SDR CA141128001](https://openairdocs.org/sdr/CA141128001), Nov 27, 2014: MODULE. FAILED. (CAN) AIR RETURN DUE TO FLAP DISAGREE, PAN PAN DECLARED, OVERWEIGHT LANDING. RESOLUTION CENTER FLAP/STABILIZER POSITION MODULE M839 REPLACED AND FUNCTION CHECKE - [SDR CA140826024](https://openairdocs.org/sdr/CA140826024), Aug 22, 2014: OIL SYSTEM. LEAKING. (CAN) DURING THE ATLANTIC CROSSING, OIL BEGAN TO DIMINISH ON THE RIGHT ENGINE. QUANTITY FELL TO ZERO AND THE DECISION WAS MADE TO HAVE THE FLIGHT DIVERTED. A PA - [SDR CA121221008](https://openairdocs.org/sdr/CA121221008), Dec 15, 2012: SKIN. CORRODED. (CAN) CORROSION FOUND ON FUSELAGE SKIN AT THE FORWARD LAVATORY BLOWER VENT OUTLET. EXFOLIATION CORROSION BETWEEN. LT FS SKIN BS 1540-1562, BETWEEN STR 24L-25L W - [SDR CA120514002](https://openairdocs.org/sdr/CA120514002), May 12, 2012: SEAL. DEPARTED. (CAN) ON APPROACH , FLAP, AILERON SEAL CAME OFF IN FLIGHT. MOC ADVISED. LANDED WITHOUT INCIDENT. ON RT WING, T/E BETWEEN INBD AND NEXT FLAP, RUBBER SEAL FLAPPIN - [SDR CA110105007](https://openairdocs.org/sdr/CA110105007), Jan 4, 2011: BUSS. FAILED. AS A RESULT OF A MALFUNCTION OF THE ELECTRICAL BUSES, THE FLIGHT ELECTED TO RETURN WITH SUBSEQUENT OVERWEIGHT LANDING. REPEAT SNAG, L/R UTILITY BUSS OFF LIGHTS, - [SDR CA110103006](https://openairdocs.org/sdr/CA110103006), Jan 2, 2011: WIRE. BROKEN. FLIGHT RETURNED TO DUE RED EICAS FLAP/SLAT ALERT T/O CONFIG, LANDING NORMAL. FINDINGS LISTED SEQ 2 DIODE BLOCK R608 PIN LOCK BROKEN AND LOOSE WIRE. DIODE BLK R6 - [SDR CA101019007](https://openairdocs.org/sdr/CA101019007), Oct 18, 2010: VALVE. FAILED. DURING THE APPROACH TO LAND, THE CREW ADVISED THEY HAD AN ANTI-SKID FAILURE AND WERE REQUESTING A LONGER RUNWAY FOR THE LANDING. THE LANDED WITHOUT USING THE AN - [SDR CA080229007](https://openairdocs.org/sdr/CA080229007), Feb 20, 2008: LEVER. MISINSTALLED. (CAN) OVER-WING SLIDE COMPARTMENT DOOR OPENING ACTUATING MECHASIM - LEVER DESCRIPTION: A LEVER THAT JOINS THE FIRING PIN CLEVIS OF THE OFF-WING ESCAPE SLIDE COM - [SDR CA040216001](https://openairdocs.org/sdr/CA040216001), Feb 16, 2004: ODOR. DETECTED. (CAN) THE FLIGHT EXPERIENCED AN ACRID ODOR IN THE COCKPIT. AC DECLARED AN EMERGENCY LANDING AND CARRIED OUT THE QRH. AC SENT TO HANGAR FOR INVESTIGATION. - [SDR CA040120005](https://openairdocs.org/sdr/CA040120005), Jan 20, 2004: ENGINE. FLAMED OUT. (CAN) ON TAXI OUT LT ENGINE FLAMED OUT, WITH OIL ODOR IN THE CABIN. RETURNED TO GATE, AIRCRAFT CHANGED, ENGINE REPLACED IAW 71-00-02 CONF. - [SDR CA020826003](https://openairdocs.org/sdr/CA020826003), Aug 15, 2002: COOLING FAN. FAILED. (CAN) INTERMITTENT LOUD SQUEEL IN FRONT CABIN AND GALLEY WAS FOLLOWED BY MOMENTARY SMOKE IN FLIGHT DECK AND FWD EQUIPMENT BAY FAN STATUS MESSAGE WITH ASSOCIATED - [SDR EVAS91015](https://openairdocs.org/sdr/EVAS91015), Aug 6, 2002: TILLER. FAILED. TILLER STEERING RIGHT ONLY DURING TAXI, REPLACED NLG STEERING METERING VALVE & RIGGING & OPR CHECKED NORMAL. - [SDR CA010105002](https://openairdocs.org/sdr/CA010105002), Dec 11, 2000: SPUR GEAR. DAMAGED. (CAN) REMOVED ACTUATOR FROM A/C DUE REPEAT PIREP. SHOP INSPECTION FOUND SPUR GEAR SPLINE HAD A SEGMENT MISSING. THIS MISSING SEGMENT HAD BEEN REPLACED BY A ROLL - [SDR CA001214005](https://openairdocs.org/sdr/CA001214005), Dec 11, 2000: SHAFT. MISSING. (CAN) REMOVED ACTUATOR FROM A/C DUE REPEAT PREP. SHOP INSPECTION FOUND SPUR GEAR SPLINE HAD A SEGMENT MISSING. THIS MISSING SEGMENT HAD BEEN REPLACED BY A ROLL - [SDR 95ZZZX4543](https://openairdocs.org/sdr/95ZZZX4543), Jun 11, 1995: SUPPORT ROD. BROKEN. THE CREW REPORTED THERE WAS WATER LEAKAGE. AFT-FLIGHT CHECK FOUND FOUR RODS FOR LEFT WATER TANK SUPPORT BROKEN AND THE SUPPORT CRACKED. THE AIR TUBE BESIDE THE --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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