McDonnell Douglas MD-80

1,122 parts applicable to this airframe — narrowbody

Part NumberStatus
37048411OEM
37532351unknown
3923155504PMA
3924809503NOEM
4758514520NOEM
5616674OEM
5644973502unknown
57698595OEM
59101573OEM
591140197OEM
591142923OEM
591216613OEM
591216614NOEM
5912166226OEM
59131951OEM
591326218OEM
591809811OEM
59180989PMA
5936053501OEM
5936431501OEM
99115205OEM
99115497OEM
991199117OEM
991199215OEM
9912246197OEM
991500218OEM
991960373OEM
99220422OEM
9922042505OEM
992345935OEM
993053865OEM
993053877OEM
993061223OEM
99360734OEM
9936534101OEM
995160016OEM
ALC705219OEM
ARC0502506OEM
DMC5011AOEM
JT8D15OEM
JT8D15AOEM
JT8D17OEM
JT8D217COEM
JT8D219OEM
JT8D7BOEM
JT8D9AOEM
S00483OEM
S27779224OEM
S27779225OEM
V3101PMA

Top Replacement-Prone Parts(18)

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

Part #PropensitySDRs
JT8D15AHK100%28
ARC0502506100%*27
59131951100%*20
42D1091A100%18
59101573100%*18
JT8D9A100%17
99220422100%*17
JT8D17100%17
993053877100%*16
JT8D15100%15
37048411100%*15
993061223100%*15
JT8D7B100%13
JT8D15A100%11
9922042505100%*10
JT8D217C100%10
AD4002P100%531
JT8D21996%145

* 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)

MD-80 family rollup — BTS T-100, domestic + international

Cycles per aircraft
752025
2015: 809 cycles/aircraft2016: 734 cycles/aircraft2017: 739 cycles/aircraft2018: 778 cycles/aircraft2019: 613 cycles/aircraft2020: 124 cycles/aircraft2021: 35 cycles/aircraft2022: 53 cycles/aircraft2023: 58 cycles/aircraft2024: 86 cycles/aircraft2025: 75 cycles/aircraft
20152025
2020: 124
Recovered to 14% of 2019 (2024 vs 2019)
Freighter share of departures
1%44%20152025
2015: 1.2% freighter share2016: 1.2% freighter share2017: 1.5% freighter share2018: 1.7% freighter share2019: 2.3% freighter share2020: 14.2% freighter share2021: 60.2% freighter share2022: 62.4% freighter share2023: 54.3% freighter share2024: 37.6% freighter share2025: 43.5% freighter share
20152025
Est. US-registered fleet
1202025
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)

MD-80 family — FAA registry deregistrations

Left the US registry
49aircraft
Stayed domestic
42vs 7 exported
Avg age at retirement
38.3years
Still US-registered
119aircraft
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
P & W JT8D series8417229834.4 yr
P & W JT8D-21922444034.5 yr
P & W JT8D-9 series9244253.8 yr
P & W JT9D series13373041.7 yr
P & W JT8D-18213033 yr
P & W JT8D-17 series7161144 yr
P & W JT8D-156131151 yr
P & W JT8D-9A51100

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)

MD-80 family — BTS Form 41 filings

Direct maintenance per block hour
$471fleet avg
Airframe / engine split
$432/$39
Reporting carriers
3

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

2airworthiness directives affecting this fleet — recurring compliance demand for the parts and shops that serve it
Most recent
  • FAA AD 2025-09-11effective Jun 12, 2025Prohibition

    The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD- 83), DC 9-87 (MD-87), and MD-88 airplanes, and Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes. This AD was prompted by the discovery of jammed elevators during takeoff. This AD requires revising the "Certificate Limitations" section of the existing airplane flight manual (AFM) to include a procedure to confirm elevator surfaces are not jammed in the trailing edge down (TED) position. The FAA is issuing this AD to address the unsafe condition on these products.

  • FAA AD 2023-01-13effective Mar 13, 2023Mixed actions

    The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC- 9-83 (MD-83), and DC-9-87 (MD-87) airplanes; and Model MD-88 airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that certain center wing lower stringers are subject to widespread fatigue damage (WFD). WFD analysis found that fatigue cracks could grow to a critical length after the structural modification point (SMP) for these center wing lower stringers. This AD requires replacing certain left and right side center wing lower stringers. 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.