Boeing 717-200
7,596 parts applicable to this airframe — narrowbody
| Part Number | Status |
|---|---|
| 111414-401 | PMA |
| 111414-403 | PMA |
| 111414-451 | PMA |
| 13T05511012-501 | PMA |
| 2205772-1 | OEM |
| 2205774-1 | OEM |
| 2205783-1 | OEM |
| 2205783-2 | OEM |
| 2205793-1 | OEM |
| 2205956-1 | OEM |
| 2205957-1 | OEM |
| 2206419-1 | OEM |
| 279T-6TT | PMA |
| 29527CM001-301 | PMA |
| 29527CM001-303 | PMA |
| 29527CM001-304 | PMA |
| 29527CM003-301 | PMA |
| 29527CM004-301 | PMA |
| 29527CM004-303 | PMA |
| 29527CM006-303 | PMA |
| 29527CM014-201 | PMA |
| 29527CM016-301 | PMA |
| 29527EM007-301 | PMA |
| 29527EM007-302 | PMA |
| 29527EM007-303 | PMA |
| 29527MM002-201 | PMA |
| 29527MM002-203 | PMA |
| 29527MM003-203 | PMA |
| 29527SM001-301 | PMA |
| 29527SM003-303 | PMA |
| 29527SM004-301 | PMA |
| 29527SM004-302 | PMA |
| 300843-1AAR | PMA |
| 402E35010-001AAR | PMA |
| 402E35010-013AAR | PMA |
| 402E35010-014AAR | PMA |
| 560000-305-1581 | PMA |
| 612-0312-001WE | PMA |
| 6545818 | |
| 715D8001-557 | OEM |
| 90-48401-6 | OEM |
| AVUS2207333-2 | PMA |
| AVUS2207334-2 | PMA |
| B64534-3 | PMA |
| B64535-1 | PMA |
| HV92-17 | PMA |
| IW50098-01 | PMA |
| LA00200X150A50D5 | PMA |
| RD2206409-5 | PMA |
| SP3810-01-4020 | PMA |
Top Replacement-Prone Parts(11)
From FAA SDR — directional buying signal, not a failure rate
| Part # | Propensity | SDRs |
|---|---|---|
| 65C25727 | 100%* | 1,055 |
| BAC1506 | 100%* | 184 |
| 591014167 | 100%* | 37 |
| 59516395001 | 100% | 24 |
| 2929169 | 100%* | 23 |
| 6545818 | 100%* | 13 |
| 3961899501 | 97% | 62 |
| 39567851 | 96% | 56 |
| 6567380 | 91% | 222 |
| 10114 | 77% | 13 |
| 5919526508 | 73% | 11 |
* 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)
717 family rollup — BTS T-100, domestic + international
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(2023–2026)
717 family — FAA registry deregistrations
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 model | Active tails | Engine units | Retired since ’23 | Exported | Avg age at dereg |
|---|---|---|---|---|---|
| ROLLS-ROYC BR 700 series | 342 | 684 | 11 | 25 | 14.4 yr |
| BMW ROLLS BR 700 series | 164 | 328 | 6 | 7 | 24.5 yr |
| ROLLS DEUT BR700-715A130 | 6 | 12 | 0 | 0 | — |
| ROLLS-ROYC TAY 651-54 | 2 | 4 | 0 | 1 | 21 yr |
| BMW ROLLS BR700-715C130 | 1 | 2 | 0 | 0 | — |
| BMW ROLLS BR700-715A130 | 1 | 2 | 0 | 0 | — |
| ROLLS DEUT BR700-715B130 | 1 | 2 | 0 | 0 | — |
| ROLLS DEUT BR700-715C130 | 1 | 2 | 0 | 0 | — |
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)
717 family — BTS Form 41 filings
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
- FAA AD 2026-13-15effective Jul 1, 2026Prohibition
The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 707, 717, and 727 airplanes; Model DC-8, DC-9, and DC-10 airplanes; Model MD-10 and MD-11 airplanes; 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 MD 90-30 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 the 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 2025-21-05effective Jan 2, 2026Mixed actions
The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 717-200 airplanes. This AD was prompted by a report of a nose landing gear-up landing caused by the failure of the upper lock link assembly. This AD requires repetitive inspections for cracking of the upper lock link assembly and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
- FAA AD 2025-02-07effective Mar 17, 2025Prohibition
The FAA is superseding Airworthiness Directive (AD) 2020-03- 20, which applied to certain The Boeing Company Model MD-11, MD-11F, and 717-200 airplanes; all Model 737-8 and 737-9 airplanes; all Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes; certain Model 747-400 and 747-400F series airplanes; certain Model 757 and 767 airplanes; and all Model 777 airplanes. AD 2020-03-20 required revising the existing airplane flight manual (AFM) to include a limitation to prohibit operations that require less than 0.3 required navigational performance (RNP) within a specified area for airplanes having a certain multimode receiver (MMR) with certain software installed. This AD was prompted by reports from Boeing of simultaneous MMR resets related to an error in calculating Coordinated Universal Time (UTC). This AD requires the actions in AD 2020-03-20, removes an airplane model from the applicability, and would also require installing certain MMR operational software (OPS). The FAA is issuing this AD to address the unsafe condition on these products.
- FAA AD 2024-21-01effective Nov 7, 2024Mixed actions
The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 717-200 airplanes. This AD was prompted by a report of cracks found in the rear spar lower cap forward leg and lower aft skin of the right wing, during investigation of a fuel leak. This AD requires repetitive inspections for any fuel leak or crack of the lower aft skins, external doublers, and rear spar lower caps of the left and right wings, and corrective actions and inspection reports if necessary. The FAA is issuing this AD to address the unsafe condition on these products.
- FAA AD 2024-20-02effective Oct 21, 2024Mixed actions
The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 717-200 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 a report of cracked and severed structure found in the aft fuselage cant bulkhead at a certain station (STA) and the vertical stabilizer rear spar installation. This AD requires a one-time inspection of the aft fuselage cant bulkhead at certain STAs and vertical stabilizer rear spar structure, and corrective actions and an inspection report if necessary. This AD also requires an inspection of that same structure if certain conditions occur during any phase of flight. 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.