McDonnell Douglas MD-87

8,365 parts applicable to this airframe — narrowbody

Part NumberStatus
00-12689-02OEM
10601CB-251OEM
20095-404OEM
234582-001OEM
2607027-141OEM
2607027-225OEM
2652651-507PMA
2712453
272A105-1PMA
2958490-1OEM
300117-100OEM
300117-175OEM
300117-225OEM
32178-7OEM
3520-0429-01OEM
3530-0225-01OEM
3916571-1PMA
4100310-7PMA
4559 Q4559 Q4559X TAE0728-1OEM
46-0423-3OEM
4915190-1PMA
502666-407-(denotes color)PMA
5911588OEM
5911589OEM
5951513-502PMA
600434OEM
73348-5D492OEM
7438FT972P3OEM
7438FTP3OEM
743J9MT2NOEM
743J9MT987OEM
743J9MT987NOEM
7912640-527PMA
7912643565PMA
7912643570OEM
7912646-640OEM
7912854-616
7912854-684
7912854-753unknown
7912854-774PMA
7914110-652
859176-1OEM
859615-3OEM
904-002-475-11OEM
904-002-475-61OEM
BACB10CA3OEM
BACB10FR68RJZOEM
BACB10GP12JOEM
General Ecology AL15G (770020)OEM
Grimes Aerospace P/N 46-0450-1OEM

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.