Robinson R22
402 parts applicable to this airframe — helicopter
| Part Number | Status |
|---|---|
| 02471131 | OEM |
| 030039 | PMA |
| 032347 | PMA |
| 100060 | PMA |
| 22-100-1 | PMA |
| 22-100-3 | PMA |
| 307FCE | PMA |
| 400010 | OEM |
| 4200-002-10 | PMA |
| 4200-002-15 | PMA |
| 4200-002-20 | PMA |
| 420000225 | OEM |
| 42000025 | OEM |
| 87-05207-001 | PMA |
| 87-05207-002 | PMA |
| A-0750161-25 | OEM |
| A02020 | PMA |
| A1843 | PMA |
| A6131 | OEM |
| AB382585 | |
| ACS 2010 | PMA |
| ACS 836 | PMA |
| ACS775SL | unknown |
| B2241 | OEM |
| B28012 | OEM |
| B82312 | OEM |
| C0182 | OEM |
| C0184 | OEM |
| C12117 | OEM |
| C3102 | OEM |
| C64712REVZ | OEM |
| CCA-110-H4 | PMA |
| CCB-36000H | PMA |
| D0281 | OEM |
| D0814 | OEM |
| D2604 | OEM |
| D307PS | PMA |
| D3141 | OEM |
| D7281 | OEM |
| D7981 | OEM |
| D7997 | OEM |
| ES10361631 | OEM |
| F1014 | OEM |
| F2592 | OEM |
| G6551 | OEM |
| G76811 | OEM |
| H-47C | PMA |
| PFS-17101 | PMA |
| SS1001 | |
| SS1002 | OEM |
Top Replacement-Prone Parts(18)
From FAA SDR — directional buying signal, not a failure rate
| Part # | Propensity | SDRs |
|---|---|---|
| A1902 | 100% | 80 |
| 14924HTH | 100% | 49 |
| A7924 | 100% | 20 |
| B2862 | 100% | 15 |
| CH48108 | 100% | 13 |
| V31001 | 100% | 12 |
| D2781 | 100% | 12 |
| 10357584 | 100% | 10 |
| A5695 | 100% | 10 |
| A0511 | 96% | 40 |
| C0511 | 92% | 17 |
| B2475 | 86% | 13 |
| B1741 | 85% | 21 |
| LW17060 | 79% | 21 |
| 103571651 | 78% | 10 |
| A1593 | 67% | 31 |
| A1583 | 67% | 12 |
| 105217 | 59% | 33 |
* 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 2024-04-02effective Apr 2, 2024Prohibition
The FAA is adopting a new airworthiness directive (AD) for certain Robinson Helicopter Company Model R22, R22 Alpha, R22 Beta, R22 Mariner, R44, R44 II, and R66 helicopters. This AD was prompted by reports of helicopters losing a tail rotor blade (TRB) tip cap. This AD requires visually checking and inspecting certain part-numbered and serial-numbered TRB tip caps for evidence of corrosion and, depending on the results, removing the corrosion. This AD also requires removing all affected TRBs from service and prohibits installing them on any helicopter. 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.