Saab Saab 2000
320 parts applicable to this airframe — turboprop
| Part Number | Status |
|---|---|
| 11214-001 | OEM |
| 117040-5 | PMA |
| 117040-6 | PMA |
| 117053-1 | PMA |
| 117096-002 | PMA |
| 2119808-4 | PMA |
| 30191-0101 | PMA |
| 53203 | PMA |
| 68370-15 | PMA |
| 68370-16 | PMA |
| 69238-1EH | PMA |
| 69238-2EH | PMA |
| 71166-4 | PMA |
| 71166-5 | PMA |
| 71304-1 | PMA |
| 71304-2 | PMA |
| 71311-2 | PMA |
| 71311-3 | PMA |
| 7253725191 | OEM |
| 7253813007 | OEM |
| 7U7745-3 | PMA |
| 7U7750-3 | PMA |
| 7U7757-3 | PMA |
| 7U7870-1 | PMA |
| ABS-3301-31 | PMA |
| APM7239610-078 | PMA |
| APM7252600301 | OEM |
| APMA7252600-761 | PMA |
| APMB7252600-591 | PMA |
| APME7252600-153 | PMA |
| APMRSF340SAAB-1 | PMA |
| MDL D3111-000 | PMA |
| MDLTFD-4000/4100-MDL | PMA |
| MS213212 | OEM |
| PM-501 | PMA |
| PMA3510-0044-05C | PMA |
| SK2214 | PMA |
| SMR5242-01 | PMA |
| SMR5242-02 | PMA |
| SMR5242-03 | PMA |
| SMR5242-04 | PMA |
| SMR5242-07 | PMA |
| SMR5242-08 | PMA |
| SMR5242-09 | PMA |
| SMR5242-10 | PMA |
| SMR5242-13 | PMA |
| SMR5242-21 | PMA |
| SMR5242-22 | PMA |
| SMR7147-4 | PMA |
| SMR7147-5 | PMA |
Top Replacement-Prone Parts(7)
From FAA SDR — directional buying signal, not a failure rate
| Part # | Propensity | SDRs |
|---|---|---|
| 330151 | 100% | 173 |
| 13889 | 100% | 31 |
| 7253725191 | 100%* | 18 |
| 66361 | 92% | 13 |
| 72111211000 | 90% | 294 |
| MS213212 | 70% | 11 |
| 10138402518 | 16%* | 25 |
* 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.
Airworthiness Directive activity
FAA / EASA public regulatory data
- FAA AD 2024-15-12effective Oct 23, 2024Mixed actions
The FAA is superseding Airworthiness Directive (AD) 2021-26- 05, which applied to all Saab AB Model SAAB 2000 airplanes. AD 2021-26- 05 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require certain actions in AD 2021-26-05 and requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
- FAA AD 2023-25-06effective Feb 7, 2024Mixed actions
The FAA is adopting a new airworthiness directive (AD) for all Saab AB, Support and Services Model SAAB 2000 airplanes. This AD was prompted by a review of the anti-skid system that revealed the possibility of inadvertently connecting the inboard harness to the outboard channel (and vice versa) of the wheel speed transducers in the main landing gear (MLG) wheel axles. This AD requires installing color markings on the harnesses and the wheel axles, to ensure proper installation and connection of the anti-skid harnesses, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
- EASA AD 2023-0220effective Jan 4, 2024Mixed actions
EASA Safety Publications Tool
- EASA AD 2023-0135effective Jul 24, 2023Mixed actions
EASA Safety Publications Tool
- FAA AD 2021-26-05effective Feb 15, 2022Mixed actions
The FAA is superseding Airworthiness Directive (AD) 2020-07- 17, which applied to all Saab AB, Support and Services Model SAAB 2000 airplanes. AD 2020-07-17 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2020-07- 17, it has determined that new or more restrictive airworthiness limitations are necessary. This AD retains the requirements of AD 2020- 07-17 and requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a European Union Aviation Safety Agency (EASA) AD. 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.