Boeing 767-300ER

1,122 parts applicable to this airframe — widebody

Part NumberStatus
00059-039PMA
1156518-151PMA
1303063-001PMA
1303236-001PMA
1303640-001PMA
1303651-001PMA
1303711-001PMA
141T482013OEM
141T482014OEM
4101258-204PMA
434-674-1041-3303PMA
476W2221-12GPMA
50HR10300PMA
5E2675-8PMA
6038403OEM
65446914
65B08424202
65B105097
65B13002013
65B15637OEM
65B9090179
AHY00601-001PMA
AHY00607-001PMA
AHY00608-001PMA
AHY00633-001PMA
AHY00634-001PMA
B220342-102PMA
B220342-103PMA
B220342-104PMA
B220342-105PMA
B220342-106PMA
B220342-107PMA
B220342-108PMA
B220342-109PMA
B220342-110PMA
B220342-111PMA
B220342-112PMA
B220342-113PMA
B220342-114PMA
B220342-115PMA
B220342-116PMA
B220342-117PMA
B220342-118PMA
BAC27WEL1625PMA
BAC27WEL1634PMA
BAC27WEL1635PMA
BAC27WEL1642PMA
BAC27WEL1645PMA
P2A2592PMA
S013499PMA

Top Replacement-Prone Parts(25)

From FAA SDR — directional buying signal, not a failure rate

Part #PropensitySDRs
6517583100%*74
6550570100%*72
654645268A100%*66
65C25723100%*53
6546430100%*53
6547450100%*51
6552880100%*41
6546822100%*28
6551626100%*28
6547979100%*27
6560552100%*26
6546435339100%*24
65458197100%*23
65C34356100%*20
65448517100%18
6516323100%*15
6545818100%*13
6545802100%*13
65C26714100%*11
654541039100%*10
6546547251100%*10
65B4028912100%10
6546808100%*10
65C3330498%53
655663397%232

* Structural ATA chapters use FAA K-code change rate. Verb-based propensity is suppressed there because "REPAIRED" in the SDR text usually refers to the airframe being repaired around the part.

Utilization & cargo trend(US carriers, 2015–2025)

767 family rollup — BTS T-100, domestic + international

Cycles per aircraft
4772025
2015: 361 cycles/aircraft2016: 363 cycles/aircraft2017: 382 cycles/aircraft2018: 417 cycles/aircraft2019: 438 cycles/aircraft2020: 377 cycles/aircraft2021: 462 cycles/aircraft2022: 479 cycles/aircraft2023: 480 cycles/aircraft2024: 488 cycles/aircraft2025: 477 cycles/aircraft
20152025
2020: 377
Recovered to 111% of 2019 (2024 vs 2019)
Freighter share of departures
39%75%20152025
2015: 39.2% freighter share2016: 45.8% freighter share2017: 53.9% freighter share2018: 58.9% freighter share2019: 64.2% freighter share2020: 85.8% freighter share2021: 78.9% freighter share2022: 76.8% freighter share2023: 75% freighter share2024: 76.4% freighter share2025: 75.2% freighter share
20152025
Est. US-registered fleet
5652025
20152025

US carriers only (BTS T-100, domestic + international segments) — foreign-carrier flying is excluded, so global utilization runs higher. Fleet size is reconstructed from the FAA registry (built on or before each year, not yet deregistered) — an approximation. Freighter share counts departures with zero passengers and freight aboard — a proxy for freighter/combi operations, not a tail-by-tail conversion count. Missing years render as gaps.

USM supply — retirements & teardowns(20232026)

767 family — FAA registry deregistrations

Left the US registry
91aircraft
Stayed domestic
32vs 59 exported
Avg age at retirement
30.5years
Still US-registered
565aircraft
Where this family's parts catalog concentrates — the systems most exposed to incoming teardown supply

FAA registry data. Domestic deregistration is a teardown proxy — it also captures re-registrations and some unflagged exports, so it is not a confirmed part-out count; exported aircraft left the US fleet intact and are not USM supply. ATA shares reflect where this directory's parts for the family concentrate (parts in parentheses) — a coverage signal, not the aircraft's bill of materials or a teardown-yield forecast.

Engine-program supply pressure(since 2023)

FAA registry — US-registered fleet

Engines account for roughly half of all MRO spend, so engine programs shedding aircraft are where retirement supply carries the most value.

Engine modelActive tailsEngine unitsRetired since ’23ExportedAvg age at dereg
GE CF6-692131048 yr
P&W PW4000 series14932923230 yr
GE CF6-80 series23757113236.9 yr
P & W JT9D series13373041.7 yr
GE CF6-80A9183339 yr
GE CF6-80C2B625502231.7 yr
GE CF6-80A25102242 yr
GE CF6-80C2B6F2545081429 yr

FAA registry data, US-registered aircraft only. Counts reflect the engine model as registered — generic “series” rows coexist with thrust-variant rows, so per-variant figures are partial. Retired = domestic deregistrations (a teardown proxy, not a confirmed part-out); exported aircraft left the US fleet intact. Active tails span every family the engine flies on, not just this one.

Maintenance economics(US carriers, through 2026)

767 family — BTS Form 41 filings

Direct maintenance per block hour
$358fleet avg
Airframe / engine split
$247/$111
Reporting carriers
13
Carrier range
$66$743

BTS Form 41 data (Schedule P-5.2 maintenance expense over T-2 block hours), Group III US carriers only — filers above $1B annual revenue; smaller US operators, Part 135, and all non-US carriers are not in this data. Dollars are accrual-basis from regulatory filings (reserves and depreciation included), so they benchmark fleet economics and do not track to individual repair events. Averages are block-hour- weighted across every reporting carrier; the range spans per-carrier rates after excluding marginal reporting slices, and small carrier counts are noisy.

Airworthiness Directive activity

FAA / EASA public regulatory data

18airworthiness directives affecting this fleet — recurring compliance demand for the parts and shops that serve it
Most recent
  • FAA AD 2026-13-16effective Jul 1, 2026Prohibition

    The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 757 airplanes and Model 767 airplanes. This AD was prompted by the determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G Lower C-Band) while operating in Canadian airspace, and a determination that, during approach, landings, and go-arounds, as a result of this interference, certain airplane systems may not properly function, resulting in increased flightcrew workload while on approach with the flight director, autothrottle, or autopilot engaged, which could result in reduced ability of the flightcrew to maintain safe flight and landing of the airplane. This AD requires revising the existing airplane flight manual (AFM) to incorporate limitations prohibiting certain operations requiring radio altimeter data when operating in Canadian airspace. The FAA is issuing this AD to address the unsafe condition on these products.

  • FAA AD 2026-05-07effective Apr 16, 2026Mixed actions

    The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes. This AD was prompted by discovery of a crack at one of the forward lower fastener holes following replacement of a cracked underwing longeron (UWL) fitting. This AD requires performing an open hole high frequency eddy current (HFEC) inspection for cracks of the fastener holes common to the UWL fitting, upper drag splice angle, and lower drag splice angle, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

  • FAA AD 2026-05-03effective Apr 16, 2026Mixed actions

    The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-200 and 767-300 series airplanes. This AD was prompted by reports of scribe lines found at skin lap joints and butt joints, around external repairs and antennas, and at locations where external decals had been cut. For some airplanes, this AD requires a detailed inspection for scribe lines and applicable related investigative and corrective actions. For other airplanes, this AD requires repetitive nondestructive testing inspections for cracking at certain stringers of the skin lap joint fuselage skin and applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

  • FAA AD 2026-04-10effective Apr 10, 2026Mixed actions

    The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-200, 767-300, 767-300F, and 767- 400ER airplanes. This AD was prompted by a heavy maintenance check that found corrosion damage on a Model 767 satellite communications (SATCOM) high gain antenna adapter plate. This AD requires repetitive detailed inspections (DET) of the SATCOM high gain antenna adapter plate for corrosion and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

  • FAA AD 2025-15-08effective Aug 21, 2025Mixed actions

    The FAA is superseding Airworthiness Directive (AD) 2025-01- 06, which applied to all The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes. AD 2025-01-06 required identifying the part number, and the serial number if applicable, of the Captain's and First Officer's seats and applicable on-condition actions for affected seats. AD 2025-01-06 also required a one-time detailed inspection and repetitive checks of the horizontal movement system (HMS) of the Captain's and First Officer's seats and applicable on-condition actions. Since the FAA issued AD 2025-01-06, the FAA determined that AD 2025-01-06 contains an error when providing conditions for taking credit using a previous revision of the service information. This AD requires the actions of AD 2025-01-06 and revises paragraph (j) of this AD to clarify which actions are not required. The FAA is issuing this AD to address the unsafe condition on these products.

Directives linked to this airframe family in the FAA / EASA regulatory corpus we have processed — not a complete historical AD list. An AD is a compliance requirement that drives scheduled work (inspections, replacements, modifications) across the fleet; inspection directives are not replacement directives, and none of this is a prediction that any part will fail.